31st Annual Report 2015 - 2016

“PAPERS TO BE LAID ON THE TABLE OF LOK/RAJYA SABHA”

New Delhi AUTHENTICATED Date :

REVIEW REPORT

In the present case, the Accounts have been audited by the statutory auditors

appointed by the Government on the advice of the C & AG of India. The Annual Report

was approved by the General Body of ADA after clearance with the Ministry. The

Government is in agreement with these Reports and hence “No Review” is being laid

before the Parliament.

New Delhi AUTHENTICATED Date :

Annual Report 2015 -2016

MEMBERS OF THE GENERAL BODY OF AERONAUTICAL DEVELOPMENT AGENCY DURING THE FINANCIAL YEAR 2015-2016

01 Shri Manohar Parrikar President Hon'ble Raksha Mantri South Block New Delhi

02 Shri Arun Jaitley Vice-President Hon'ble Vitta Mantri North Block New Delhi

03 Shri Rao Inderjit Singh Member Hon'ble Raksha Rajya Mantri South Block New Delhi

04 Air Chief Marshal Arup Raha Member PVSM, AVSM, VM, ADC Chief of Air Staff Air HQ New Delhi

05 Admiral R K Dhowan Member PVSM, AVSM, YSM, NM, VSM, ADC Chief of the Naval Staff Naval HQ New Delhi

06 Shri G Mohan Kumar Member Defence Secretary South Block New Delhi

07 Shri R P Watal Member Finance Secretary North Block New Delhi

08 Shri R P Watal Member Secretary – Expenditure North Block New Delhi

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09 Dr S Christopher Member Secretary Dept of Defence R&D & DG-ADA DRDO Bhawan New Delhi

10 Shri Ashok Kumar Gupta Member Secretary – Defence Production South Block New Delhi

11 Air Marshal PP Reddy, VM Member Chief of Integrated Defence Staff (CISC) HQ Integrated Defence Staff South Block New Delhi

12 Shri S S Mohanty Member FA (DS) Ministry of Defence South Block New Delhi

13 Shri A S Kiran Kumar, Member Secretary – Dept of Space Anthariksh Bhawan Bangalore

14 Shri T Suvarnaraju Member Chairman & Managing Director Hindustan Aeronautics Ltd Bangalore

15 Dr Kota Harinarayana Member Distinguished Scientist (Former LCA Programme Director & Vice Chancellor of Hyderabad University)

16 Dr A R Sihag Member DG – Acquisition, MoD

17 Shri CD Balaji Secretary-ADA DS & Programme Director (CA) & Director - ADA

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18 Air Marshal SBP Sinha Permanent Invitee AVSM, VM DCAS – Air Hq

19 Shri R G Viswanathan Permanent Invitee Addl FA (RV) & JS

20 Shri K Ravi Kumar Permanent Invitee FA to DG-ADA

21 Air Marshal Rajesh Kumar, VM Permanent Invitee Director (IAF PMT)

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MEMBERS OF THE GOVERNING BODY OF AERONAUTICAL DEVELOPMENT AGENCY DURING THE FINANCIAL YEAR 2015-2016

01 Dr S Christopher Chairman Secretary, Dept of Defence R&D & DG-ADA DRDO Bhawan New Delhi

02 Air Chief Marshal Arup Raha Member PVSM, AVSM, VM, ADC Chief of Air Staff Air HQ New Delhi

03 Shri G Mohan Kumar Member Defence Secretary South Block New Delhi

04 Shri R P Watal Member Finance Secretary North Block New Delhi

05 Shri R P Watal Member Secretary –Expenditure North Block New Delhi

06 Shri Ashok Kumar Gupta Member Secretary – Defence Production South Block New Delhi

07 Vice Admiral P Murugesan Member AVSM, VSM Vice Chief of the Naval Staff

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08 Shri S S Mohanty Member FA (DS) Ministry of Defence South Block New Delhi

09 Air Marshal SBP Sinha, AVSM, VM Member DCAS Air - HQ

10 Shri T Suvarnaraju Member Chairman & Managing Director Hindustan Aeronautics Ltd Bangalore

11 Shri C D Balaji Secretary-ADA DS & Programme Director (CA) & Director - ADA

12 Rear Admiral P G Pynumootil Permanent Invitee ACNS (Air), IN

13 Shri K Ravi Kumar Permanent Invitee FA to DG-ADA

14 Shri R G Viswanathan Permanent Invitee Addl FA (J) & Jt Secretary Dept of Defence (R&D)

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ANNUAL REPORT FOR THE YEAR 2015-16

1. AERONAUTICAL DEVELOPMENT Mantri (RM) as the President and Vitta Mantri AGENCY (ADA) (VM) as the Vice President. The General Body meets once in a year to review the progress of ADA is a Society under the Department of Defence projects, provides policy guidelines and Research and Development, Ministry of Defence (MoD), Government of India (GoI). ADA was approves the annual report / accounts. registered as a Society under the Societies The affairs of the Society are managed, Registration Act, XXI of 1860 on June 16, 1984 at administered, directed and controlled by the New Delhi. The functioning of ADA is governed by Governing Body of the Society. The Governing a Memorandum of Association with well defined Body, which directs major activities of the rules, regulations and Bye-laws. ADA has its Society, has Secretary, Department of Defence headquarters in Bangalore and its registered office R&D as its Chairman. Secretary (Defence), at New Delhi. The primary objectives of ADA are: Secretary (Defence Production), Secretary (Finance)/Secretary (Economic Affairs), Ÿ Undertake, aid, promote, guide, manage, Secretary (Expenditure), Secretary (Defence co-ordinate and execute research in Finance)/ Financial Advisor (Defence aeronautical sciences. Services), Chief of Air Staff, Indian Air Force Ÿ Design and develop various types of (IAF), Vice Chief of Naval Staff (VCNS), Indian aircraft. Navy (IN), Chairman, HAL and Director Ÿ Establish, maintain and manage facilities for General, ADA are Members of the Governing the acquisition, storage, retrieval, Body of ADA. dissemination, evaluation, scrutiny & interpretation of information relating to Director General, ADA appointed by the GoI is technologies required for its Programmes. the Principal Executive of the Society. Ÿ Collaborate with scientific agencies, Dr S Christopher, Secretary, Department of r e s e a r c h c e n t r e s a n d e d u c a t i o n a l Defence R&D and Chairman, Defence institutions on specific projects & Research & Development Organisation investigations in areas of technology relevant to the objects of the Society. (DRDO) is the Director General of ADA. Ÿ Conduct field experimentation, flight testing, evaluation and other such activities 3. TASKS ASSIGNED TO ADA necessary for the proving of aircraft. Initial task assigned to ADA by GoI was design 2. ORGANISATION OF ADA and development of Light Combat Aircraft (LCA) to meet the Air Staff Requirements The Society is managed by the General Body (ASR) specified by the IAF. Subsequently, and the Governing Body. General Body of the design and development of carrier borne Society is the apex body and it has Raksha Naval variant of LCA was also assigned to ADA.

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Government sanction for Air Force variant of order to shorten the development time frame. Government is also keen in development of LCA was accorded initially in three Phases viz., Advanced Medium Combat Aircraft (AMCA) Project Definition Phase (PDP), Full Scale and Indian Unmanned Strike Aircraft Vehicle Engineering Development (FSED) Phase 1 and (IUSAV) with the technologies developed for LCA. Development studies are in progress at FSED Phase 2. ADA.

In November 2009, Government sanction was 4. LCA obtained for continuing Full Scale Engineering Indigenously developed LCA is an advanced Development of LCA till 31 Dec 2018 i.e. for technology, single seat, single engine, completing LCA FSED Phase 2 activities supersonic, light weight, all-weather, multi- [Probable Date of Completion (PDC): Dec role, air superiority fighter designed for air-to- 2012], LCA FSED Phase 3 - development of air, air-to-ground and air-to-sea combat roles. LCA is the smallest, light-weight, fourth Tejas Mark 2 aircraft with alternate engine to generation combat aircraft being developed in optimize the performance of the aircraft (PDC: the world. LCA promises to be the most Dec 2018) and Technology Development - for economical combat aircraft of its type in the development of improved technologies for world. On 04 May 2003, Honorable Prime various subsystems of the aircraft (PDC: Dec Minister of India has named LCA as 'Tejas'. 2018) with additional cost. 5. LCA PROGRAMME Government sanction for Naval variant of LCA Development of LCA is spearheaded by ADA was also accorded in three phases viz., PDP, with Hindustan Aeronautics Limited (HAL), a Pre-Project Phase (PPP) and FSED Navy Phase. Public Sector Undertaking (PSU) under the Ministry of Defence, GoI as the principal In December 2009, Government sanction was partner. LCA Programme involves more than obtained for continuing FSED of LCA (Navy) 40 scientific/technical disciplines. Nearly 100 till 31st Dec 2018 i.e. for completing LCA (Navy) major Work Centres and 300 smaller Work FSED Phase 1 activities (PDC: Dec 2014) Centres spread across the country including & LCA (Navy) FSED Phase 2 - development of DRDO laboratories, Council of Scientific and LCA (Navy) Mark 2 aircraft with alternative Industrial Research (CSIR) laboratories, engine (PDC: Dec 2018) with additional cost. Public/Private Sector Undertakings, educational institutes, Certification Agencies, G o v e r n m e n t a p p r o v a l s f o r L C A t o IAF / IN establishments, Indian Space Research Programme have been accorded in Phases Organisation (ISRO) and Ordnance Factories based on the confidence level gained during are actively participating in the LCA various stages of indigenous development Programme. The investments made in LCA activities carried out byADA and concurrent Programme have significantly contributed to development strategy has been approved the development of infrastructure within the based on the demonstration of capabilities in country besides developing core-advanced technologies incorporated in LCA.

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6. TEJAS PRODUCTION PHASE 7.2 Tejas Full Scale Engineering Development (FSED) Phase 2 Programme (in progress) Tejas Production Phase has been initiated Tejas FSED Phase 2 Programme was concurrently with Tejas FSED activity. IAF has sanctioned at a total cost of Rs.3301.78 th approved induction of Tejas into operational Crores (Rs. 1526.49 Crores FE) on 20 service with the first Tejas Squadron with Initial November 2001 with PDC up to December Operational Clearance (IOC) configuration and 2008. the second squadron with Final Operational The scope of FSED Phase 2 is: Clearance (FOC) configuration. Establishment Ÿ Fabrication of two Prototype Vehicle of production facilities for production rate of 08 Tejas (PV3) & Tejas (PV4) and one two aircraft per annum has been completed. Tejas seater Trainer variant Prototype Vehicle Series Production (SPs) activities are in Tejas (PV5) /Later fighter variant Tejas progress. (PV4) has been converted into Trainer variant Tejas (PV6). Ÿ 7. LCA PROGRAMME HIGHLIGHTS Weapon Integration covering Close Combat Missile (CCM), Beyond Visual 7.1 Tejas Full Scale Engineering Develop- Range (BVR) Missiles, and Conventional ment (FSED) Phase 1 Programme Bombs. (completed) Ÿ Integration of Electronic Warfare (EW) LCA FSED Phase 1 Programme was suite. sanctioned at a total cost of Rs. 2188 Crores Ÿ Integration of Multi Mode Airborne on 23rd June 1993 based on October 1991 Radar. price level with Foreign Exchange (FE) Ÿ Obtaining Initial Operational Clearance component of Rs. 873 Crores. Programme (IOC) & Final Operational Clearance was initially sanctioned up to June 1998 and (FOC). Ÿ later extended up to 31st March 2004. Establishment of production facilities (at HAL) for production rate of 08 aircraft Overall objectives of LCA FSED Phase 1 st per annum. Manufacture and delivery of Programme were achieved on 31 March 08 Limited Series Production (LSP) 2004 with limited flight testing (202 flight production aircraft. tests). Flight Test Phase (FTP) of LCA Ÿ In November 2009, sanction was th Programme was initiated on 04 January obtained for continuing FSED Phase 2 2001 with the maiden flight of LCA (TD1). Programme till 31st December 2012 with LCA (TD2) was inducted into FTP from 06th an estimated additional cost of Rs. June 2002 and LCA (PV1) also joined FTP 2475.78 Cr. With this additional sanction, from 25th November 2003. Roll out of Tejas the total fund sanctioned for LCA FSED (PV2) was carried out in FSED Phase 1 and Phase 2 Programme is Rs. 5777.56 Cr. In flight trials initiated in FSED Phase 2. With January 2013, sanction was obtained to efficient management of funds, four incur expenditure in LCA FSED Phase 2 Programme beyond 31st December 2012 aircraft-Tejas (TD1, TD2, PV1 & PV2) were (within the balance funds available) till built within the funds sanctioned for two the approval of CCS is obtained for aircraft development. extension of PDC of the Programme.

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In March 2015, approval of Hon'ble Raksha Ø Major Achievements in the Programme: Mantri has been obtained under the Provisions § Initial Operational Clearance (IOC) for Tejas of 2nd schedule Rule-7 (h) IV (ii) of the fighter aircraft (Air Force Version) obtained Transaction of Business Rule of Cabinet to on 20th December 2013. commit and incur expenditure 5% more than § Two Tejas Series Production aircraft SP1 and the sanctioned funds of Rs.5777.56 Cr i.e., SP2 (built to IOC Standard) were inducted Rs.288.87 Cr. With this the total sanction for the into Indian Air Force (IAF) as 45th Squadron Programme is Rs. 6066.43 Cr. on 01st July 2016 at Bengaluru.

Further, based on the recommendations of the Governing Body and General Body of ADA in their 57th meeting & 30th meeting respectively, a case was put up for additional funds under the Provisions of 2nd schedule Rule-7 (h) IV (1) (i) of the Transaction of Business Rule of Cabinet to commit and incur expenditure 15% more than

the sanctioned funds of Rs. 5777.56 Crores i.e., Tejas induction to IAF on 01.07.2016 Rs. 866.64 Crores and in March 2016 approval of Ø Achievements made during 2015-16 FY are: Hon'ble Raksha Mantri has been obtained. With § 180 flight tests were conducted on Tejas this the total sanction for the Programme is Rs. during 2015-16 FY. Total of 3051 flight tests 6933.07 Crores (Rs.6066.43 Cr + Rs.866.64 Cr). have been completed till 31st March 2016, th The Governing Body of ADA in its 57 meeting out of which about 2849 flight tests were also endorsed the extension of PDC of the flown after initiation of FSED Phase 2 Programme up to 31st March 2017 and financial Programme. § closure of FSED Phase 2 Programme by 30th June Tejas aircraft (LSP4 & LSP7) participated in Bahrain International Air Show 2016. 2017. § Tejas aircraft participated in IAF Exercise Iron Fist 2016. LCA FSED Phase 2 activities are in progress. § Maiden flight of Second Series Production Build of Tejas (PV3), Tejas (PV5), Tejas (PV6) & ( S P 2 ) T e j a s a i r c r a f t b u i l t t o I O C Tejas (LSP1, LSP2, LSP3, LSP4, LSP5, LSP7 and configuration occurred on 22nd March 2016. § LSP8) and integration of Close Combat Missile Integration of Derby and Python Air to Air (CCM), Conventional Bombs, Electronic missile on LCA was carried out. One Derby missile was fired successfully over the sea Warfare (EW) suite & Multi Mode Airborne range at Jamnagar. Python missile carriage Radar has been completed. Flight tests are in trials were carried out towards envelope progress. expansion.

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§ New Cobham Quartz Radome integrated § Performance test points in Operational Clean on Tejas (LSP3) aircraft and flight test in Configuration towards validation of Operating progress. Data Manual (ODM) conducted covering § 03 sorties were flown on Tejas (LSP5) Climb performance, Cruise, Descent and aircraft towards Multi Mode Radar trials, Sustained Turn. with a Hawk aircraft as target for § Establishment of facilities for production rate of comparative data gathering (MMR with a 08 aircraft per annum is 85% completed. new wave guide and Rotary Joint). Ø § Integration of Air to Air Fuel Refueling Flight Test efforts (AAR) probe on Tejas (LSP8) aircraft is in Flight Test Phase on Tejas to obtain FOC is progress. progressing satisfactorily. Aircraft per- § Mandatory Special and Periodical checks on formance test, Air Data Calibration, Parametric pipeline butting issues were undertaken on Identification, Expansion of flight envelope in all Tejas aircraft and completed. clean & stores configurations and stores § Tejas aircraft was evaluated on wet runway separation, Advanced Autopilot Modes were surface with BHEEM software version 1.9.4 main objectives during these flight tests. with aircraft mass of 9600 Kg. Handling Quality has been adjudged as “very § One ASR concession (No. 17) related to good” by Indian Air Force (IAF) and Indian “Secure Mode communication” of Tejas RDI Navy (IN) Test Pilots. set was closed. § Envelope expansion up to “8g” manoeuvre Flight test related assistance is obtained from performance and 23 deg Angle of Attack M/s. AIRBUS DS to accelerate Tejas flight test was completed and cleared for operational activities. clean configuration of Tejas. Ø § Envelope expansion of the Tejas trainer in Stores separation and weapon release trials: supersonic flight up to 1.3 Mach speed was Air-to-Ground weapon carriage and release completed. trials with 25 lb, 1000 lb and 3 kg are in progress. § Flight Trials towards assessment of aircraft Trials with Laser Guided Bomb (LGB) Environment Control System, with completed. FOC weapon Standard of Indigenous Cooling Pack Temperature Preparation (SOP) with Multi Mode Radar, Control Valve (CPTCV) successfully Helmet Mounted Display System and Litening completed. targeting pod is in progress.

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Ø Sensors integration Ø Ejection Seat Mk 16G integration · Multi Mode Radar (MMR): Integration of Ejection Seat Mk 10L is installed in Tejas (TD1, the Multi-Mode Radar (MMR), co- TD2). Ejection Seat Mk 16G is installed on Tejas developed with M/s ELTA Systems Ltd., (PV1 to PV3, PV5, PV6, LSP1, LSP2, LSP3, Israel has been completed on Tejas (LSP3, LSP4, LSP5, LSP7 and LSP8). Flight trials with LSP4, LSP5, LSP7 and LSP8). Flight trials of Mk 16G Ejection Seat is in progress. MMR on Tejas are in progress. MMR Ø Aircraft status detected and tracked targets during flight Ÿ Tejas (TD1 & TD2): Total 538 flight tests trials. Integration of the MMR on Tejas [233 on Tejas (TD1) and 305 on Tejas (TD2)] (PV6) is in progress. have been completed. All flight test points to · Helmet Mounted Display and Sight be covered with these aircraft build standard (HMDS): Integration of DASH-IV Helmet have been completed. Presently the aircraft Mounted Display and Sight (HMDS) from are not participating in flight trials. Tejas M/s Elbit, Israel has been completed and (TD1) aircraft is showcased in DRDO flight tested. Bhawan, New Delhi. Tejas (TD2) aircraft is · Other Sensors: Integration of Very-High being utilized for RCS studies at AFS Frequency Omni Range / Instrument Dundigal. Landing System (VOR /ILS) and Tactical Air Navigation (TACAN) on Tejas (LSP3, Ÿ Tejas (PV1): Total 245 flight tests (164 Hrs: LSP4, LSP5, LSP7 and LSP8) has been 2.0 Mins) have been completed. The aircraft completed. Flight trials are in progress. has flown with upgraded Flight Control Ÿ Electronic Warfare (EW) suite: Integration System (FCS) and Avionics software compatible with carriage of external Stores of Radar Warning Receiver (RWR) and (800 ltr & 1200 ltr Drop Tanks and R73E Counter Measures Dispensing System CCMs). Presently the aircraft is integrated (CMDS), which are part of EW suite have with Unified Electronic Warfare System been completed on Tejas and flight trials are (UEWS) and Two EGRs have been carried in progress. out ensure satisfactory performance of various Aircraft systems. Aircraft has been Ø GE - F404 - IN20 Engine integration inducted for 12 Year Calendar Based GE - F404 - F2J3 Engine is powering Tejas (TD1, TD2, PV1 to PV3, PV5 & LSP1). Overhaul. Upgraded GE - F404 - IN20 Engine is powering Tejas (PV6, LSP2 to LSP8). Flight Ÿ Tejas (PV2): Total 222 flight tests (123 Hrs: tests with upgraded GE - F404 - IN20 Engine 3.0 Mins) have been completed. The aircraft integrated on Tejas (PV6, LSP2, LSP3, LSP4, has flown with upgraded FCS and Avionics LSP5, LSP7 & LSP8) are satisfactory. System software for carriage of external

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Stores and Identification Friend or Foe – Air executed the first outstation detachment of to Ground (IFF A/G). All flight test points the trainer variant, and participated in hot to be covered with this aircraft build weather trials at AFS Jaisalmer during June standard have been completed. 2015. Subsequently, Tejas (PV6) has been used towards evaluation of flutter, Ÿ Tejas (PV3): Total 387 flight tests (228 Hrs: performance and validation of the 7.0 Mins) have been completed. The aircraft Operating Data Manual of the trainer variant of LCA. Rain Water Protection has flown with upgraded Flight Control Schemes and Lightning Protection Schemes System (FCS) and Avionics System have been complied on aircraft to obtain All software for carriage of external Stores Weather Clearance. including Drop tank. The aircraft has completed all test points envisaged for it. Ø Tejas Limited Series Production (LSP) GSH 23mm Gun Integration on aircraft has Ÿ Tejas (LSP1): Total 74 flight tests (40 Hrs: 7.0 been completed and Butt-Firing (Phase-1) Mins) have been completed. The aircraft has completed. Presently, indigenous OBOGS / been earmarked for fuel test points. Wet runway trials initiated on this aircraft. Rain ILSS integration on Tejas (PV3) is in protection modifications, Fuel system and progress. Brake Management System design modifications 3im-plemented on aircraft. Ÿ Tejas (PV5): Tejas (PV5) is a dual Seat All flight test points related to the aircraft trainer Variant. As on 31st March 2016, total have been completed. 124 flight tests (62 Hrs: 26.0 Mins) have been Ÿ Tejas (LSP2): As on 31st March 2016, total 314 completed. Upgradation of aircraft to IOC flight tests (195 Hrs: 11.0 Mins) have been Standard has been completed. PV5 has been completed. The aircraft has been used utilized towards pilot familiarization & towards strain measurement of MLG and conversion, PID testing and towards evaluation of Brake Management System expansion of flight envelope of the trainer improvements, which is in progress. variant. Further flight tests are in progress. Ÿ Tejas (LSP3): As on 31st March 2016, total 278 flight tests (188 Hrs: 55.0 Mins) have Ÿ Tejas (PV6): Tejas (PV6) is being developed been completed. The aircraft is the primary as the second dual Cockpit Trainer Variant platform for Envelope Expansion (High AOA) flight test. The aircraft was one of the by converting Tejas (PV4), which was aircraft earmarked for the aerobatic display originally planned as a Fighter Variant. As at Bahrain International Air Show 2016 and on 31st March 2016, total 39 flight tests (24 was utilized extensively for practicing the Hrs: 3.0 Mins) have been completed. The display profile. The aircraft has also participated in the Exercise Iron-Fist 2016, a aircraft build standard is close to Tejas live-fire demonstration exercise of the Series Production Trainer. Tejas (PV6) Indian Air Force.

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Ÿ Tejas (LSP4): As on 31st March 2016, total and demonstrated the aerobatic prowess of the 208 flight tests (159 Hrs: 32.0 Mins) have LCA at the Bahrain International Air Show been completed. Aircraft is built to Tejas 2016. Another major milestone in the LCA (LSP3) standard. Tejas (LSP4) had been Programme has been the commence-ment of utilized towards tasks such as pilot separation flight tests of the Derby (Beyond Visual Range) Missile. First Derby BVR Missile conversion and assessment of Environ- was fired from this aircraft to assess its mental Control System performance with separation characteristics, plume-engine the new indigenously developed Cabin compatibility and aspects of avionics Shutoff Valve. Tejas (LSP4) participated integration. and demonstrated the aerobatic prowess of the LCA at the Bahrain International Air Ÿ Tejas (LSP8): As on 31st March 2016, total 156 Show 2016. Also, Tejas (LSP4) had flight tests (119 Hrs: 47.0 Mins) have been demonstrated the swing-role abilities of the completed. Tejas (LSP8) is built to production LCA at Exercise Iron-Fist 2016. standard aircraft. Aircraft is identified for User Evaluation Trials (UET). Aircraft has been utilized for demonstrating Pressure refueling, Ÿ st Tejas (LSP5): As on 31 March 2016, total RWR evaluation and Radar evaluations. LSP8 290 flight tests (232 Hrs: 10.0 Mins). Aircraft had been utilized towards captive (carriage) had been utilized towards evaluating a new flight trials of the Derby BVR Missile, and to landing technique while approaching at a practice the display profile for Bahrain higher angle of attack, and evaluating the International Air Show 2016. Integration of Air performance of the Multi Mode Radar after to Air Fuel Refuelling Probe on Tejas (LSP8) is in progress. modification of some internal components. Ø Tejas Fighter FOC

System development for integrating Ÿ Tejas (LSP6): LSP6 will be built to Series additional weapons package for FOC and Production Standard of Preparation (SOP), further envelope expansion (High AOA if required. and Nz) has been initiated. Derby Beyond Visual Range (BVR) missile and Python-5 Close Combat Missile (CCM) were Ÿ st Tejas (LSP7): As on 31 March 2016, total integrated on Tejas aircraft. Carriage trials 176 flight tests (142 Hrs: 10.0 Mins) have were conducted with the missile. One been completed. Tejas (LSP7) is built to Derby BVR missile was fired in the production standard aircraft with Night unguided mode, successfully over the sea at an altitude of 30000 ft & 0.8 mach to flying & All Weather flying capability. Tejas study separation and plume character- (LSP7) had been utilized towards tasks such istics. Python-5 CCM was not fired as as strain measurement of MLG, evaluation vibrations were experienced at 0.9 mach. of improvements to the Pilot-Vehicle Analysis of test results is in progress. Integration of Air to Air Fuel Refuelling Interface, assessment of TACAN software system on Tejas aircraft is in progress. improvements and evaluation of the new Advanced autopilot modes have been take-off technique. Tejas (LSP7) participated designed and are planned to be flight

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tested. Novel auto recovery modes like of Avionics, General Systems, Propulsion Aut omat ic Low Speed Recovery and System, Airframe, Flight Control System, Disorientation Recovery Mode will also be Aerodynamics, Flight Testing Advanced flight tested towards attaining Carefree Maneuvering capability. materials etc., are projected. These activities are basically intended to be used in LCA Ø Tejas Trainer FOC Programme for product improvements and Tejas PV5 and PV6 will be utilized for obtaining also to see that country is not left behind in the FOC for Trainer. Associated flight testing is in areas of critical technologies. progress. In November 2009, Government sanction was obtained for undertaking Technology 7.3 Tejas Production Phase Development with a cost of Rs.395.65 Crores Tejas Production Phase has been initiated (FE Rs.68.30 Crores) and PDC of Dec 2018. concurrently with Tejas FSED activity. Establishment of production facilities for 8.1 Current Status production rate of 08 aircraft per annum at Development of critical advanced various Divisions of HAL is nearing technologies for indigenous equipments completion. IAF has approved induction of and systems is in progress. Project Tejas into operational service with the first sanctions for development of technologies Tejas Squadron with Initial Operational have been given to identified work centers. Clearance (IOC) configuration and the The following projects have been second squadron with Final Operational completed; Clearance (FOC) configuration. Two Tejas Ÿ DALIA actuators, Series Production aircraft (SP1 & SP2) were Ÿ inducted into Indian Air Force (IAF) as 45th Indigenous development of high Squadron on 01st July 2016 at Bengaluru. strength titanium alloy Ti-10, Further SP aircraft will be delivered Ÿ Development of Friction Stir Waelding progressively by HAL to IAF for induction. Technology for Aircraft Structures, Ÿ Aerodynamic studies of per-formance 8. Technology Development Programme Technology Development is a continuous of LCA wing with Vortex Generators, process, which leads to product improvement Ÿ LCF data generation testing on 15-5 PH and also reduces the import dependency. Many of the technologies related to Aerospace could steel, be developed within the country and these Ÿ Digital Communication Scheme for technologies would cater to LCA Programme as Tejas, well as future Aerospace Programmes. Keeping this in view Technology Development in areas

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8.2 On-going Projects b) After its maiden flight on 27 Apr 2012, The following major projects have been the LCA Navy Trainer (NP1) has completed 64 flights. The NP1 Aircraft initiated and are in progress: has been integrated with 725L Centre Ÿ Development of V/UHF Conformal Line Drop Tank and ferried to Goa. The Antenna maiden Ski-jump take-off was Ÿ Development of Digital Audio Control demonstrated by NP1 on 20 Dec 2014 at System (DACS), Shore Based Test Facility (SBTF), INS H a n s a , G o a . T h e a i r c r a f t h a s Ÿ Digital Liquid Oxygen (LOX) Indicators/ participated in the Air Display at Transmitters, DefExpo-2016, Goa, during March Ÿ Development of improved RAM, 2016. During the Mar-April 2016 Ÿ Fatigue data generation on AA 7010 detachment to SBTF Goa, NP1 has successfully completed 07 Ski jump Aluminium alloy, launches including launches from Ÿ Development of Zn-Ni plating as an Restraining Gear System (RGS) with alternate to cadmium plating, R73 missiles. As a part of the Carrier Ÿ Development of high temperature beta Compatibility Testing (CCT), Field Carrier Landing Practice (FCLP) titanium alloy DMR 700, approaches at the SBTF landing area Ÿ Development of On-Board Oxygen integrated with Optical Landing Generation System (OBOGS) System (OLS) and TV monitoring Ÿ Development of Cabin Shut Off Valve system were also carried out. The aircraft has also carried out assessment (CBSOV) of ECS, at SBTF, Goa of the specially designed Ÿ Development of AMAGB Bearings, Deck Landing Mode Control Law (viz. Ÿ Advanced Subminiature Telemetry System, Approach Angle of Attack Hold Ÿ Jet Fuel Starter (JFS) Mark 2, Control (AAHC)) which assists higher Ÿ Development of MEMS based Pressure sink rate landings. Transducers and temperature sensors for Following are the major milestones of Hydraulics system. LCA Navy Trainer (NP1). i) Aircraft has flown Supersonic 9. LCA Navy ii) Higher Angle of Attack of 23 deg 9.1 LCA Navy Mk1 achieved a) Govt. of India sanctioned development of iii) Integrated with Center Line Drop two LCA (Navy) prototypes in Mar 2003 Tank, 725 Ltrs (Revised in Dec 2009). The Programme iv) First Ski-jump launch at SBTF Goa: 20 Dec 14 also envisaged building a structural test v) High Sink rate Landing to 3.1 m/s specimen and specialized test facilities, vi) Partial Pressure Refueling up to 25 inclusive of a Shore Based Test Facility psi demonstrated (SBTF) at the Naval Air Station, Goa. vii) Ski Jump from RGS with R73 missile carried out viii) Has completed 07 Ski jumps

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The NP1 aircraft is currently being c. The second LCA Navy prototype (NP2) integrated with Arrester Hook System is a single seat fighter, integrated with (AHS) & Levcon Air Data Computer state of the art technologies such as (LADC) along with major modifications Multi Mode Radar (MMR), RWR, such as installation of Ni-Cd Battery, RDI TACAN, VOR-ILS and CMDS. The and BVR missile towards its system Aircraft has been built to production upgrade. standard incorporating special functionalities such as i) Fuel Dump System ii) Pressure and Hot refueling iii) Fuel auto transfer functionality iv) SPJ pod and Derby missile integration v) MMR with Data link facility vi) Updated ECFM systems vii) Attitude Compensated Fuel System NP1 Ski-jump take-off
viii) 03 - Auxiliary Air Intake Door for Additional thrust

Field Carrier Landing Practice (FCLP)

NP2 - Maiden Ski-Jump at SBTF, Goa

The NP2 aircraft had successfully completed its maiden flight on 07 Feb 2015 and participated in Aero India 2015 as a part of static display. The aircraft has undergone 02 detachments at SBTF, INS Hansa, Goa between 28th March to 01st June 2016. The aircraft has seen a record number of 34 flights (48 NP1- Flying Display at DefExpo 2016, Goa sorties) during the detachment.

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The aircraft has successfully completed its Day and Night Ski-Jump from RGS at SBTF INS Hansa, Goa. Hot Refueling capability at 50 psi was demonstrated on this aircraft and during 40th flight the aircraft undertook 3 Hot Refueling resulting in 04 sorties with flight duration of 02 hr 43 min and total of 08 test points executed. In-Flight Fuel Night Flying Jettison, one of the major NASR requirements, was demonstrated by NP2 aircraft on 19 April 2016, the by dumping 250 Kg @ 3.5Kg/sec) at 8000ft altitude. Advance features like MMR - Air to Sea mode and Data Link functionalities has been demonstrated both with Sea Harrier and Ground Station (Simulating the Aircraft carrier scenario). LEVCON -30° Flight

As a part of CCT a total number of 83 FCLP's and 10 High sink rate Touch- and-Go's also been undertaken. The aircraft achieved 3.2 m/s high sink rate landing, flown with LEVCON-30° position and also flown supersonic (1.1 M) The aircraft has been Mechanically Integrated with Derby Missile & Centre Field Carrier Landing Practice (FCLP) Line Drop Tank, SCT/GVT for the same has also been completed. The Aircraft has completed 51 flights (69 Sorties) covering 294 ground/flight test points till date. Presently the aircraft is undergoing Arrester Hook installation and other modifications/upgrades towards post monsoon detachment to INS Hansa, Goa.

NP2 Hot Refueling at 50 psi

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d) Structural Test Specimen (STS-N) and Modifications: Main Airframe Static Test (MAST) Rig : 1. Modified cockpit with 19deg Field The LCA Navy Structural Test Specimen of View HUD has been integrated with MAST. Limit 2. Ni-Cd Battery in place of Ag-Zn load tests for two point landing, three battery in NP1 point landing, Arrested landing, 3. V/UHF Radio in place of INCOM Negative 'g' loads, positive bending load 4. Implementation of three Auxiliary and LEVCON loading cases has been Air Intake Door(AAID) successfully completed. Test set up for Additional LRUs : maximum torque test case are under 1. SPJ POD integration progress. Ultimate load test cases are 2. Laser Designator Pod planned post upgradation of MAST 3. Air to Air Refueling probe control system. (as retro mod) 4. HMDS 5. CMDS 6. TACAN 7. VOR/ILS 8. SLB f) Cost Revision Committee has been constituted under the Chairmanship of FA to DG-ADA for additional time and fund required for build of three more Naval Prototypes. Draft report has been LCA Navy MAST and STS-N prepared and circulated for scrutiny by e) General Body of ADA in its 25th meeting committee members. Several discussions held on 09 Nov 2010 and the 26th /deliberations being held between all the stakeholders for finalization. meeting held on 13 Dec 2011, under the Chairman ship of the Hon'ble Raksha g) Additional LCA Navy Trainer (NP5): Second LCA Naval Trainer (NP5) Mantri indicated that only two deemed to be a production standard prototype aircraft were grossly trainer aircraft, is an improved version of insufficient & recommended build of NP1. Presently aircraft is in build stage one additional LCA Navy Trainer and and all major modules are under two LCA Navy Fighter Prototypes. The assembly. The Rear fuselage assembly, Radome assembly and Fin & Rudder are second Trainer aircraft (NP5) is being successfully completed. 90% of Front built close to production standard Fuselage Assembly is completed. Centre incorporating modification and Fuselage Assembly build under progress. additional functionalities compare to M a j o r L R U s a r e a v a i l a b l e a n d procurement of remaining LRUs is under NP1 aircraft as follows: p r o g r e s s . I n s t a l l a t i o n d r a w i n g s

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are released and kit preparations are The LCA Navy Structural Test under progress for equipping. The Specimen (STS) testing at Main Maiden flight of NP5 aircraft is being Airframe Structural Test Rig (MAST) planned by first quarter of 2017. is under progress. Three Landing Limit Load test cases and three flight h) Additional LCA Navy Fighter (NP6 & load limit load cases has been Np7): The cost element for the 3 completed. Limit load test case for additional aircraft (NP5, NP6 & NP7) has Maximum Torque load is under been provided by HAL and the cost progress. Ultimate Load Test case will be done after completion of limit committee duly constituted has had load cases. several discussions. This is expected to be finalised by end 2016. HAL has b. Landing gear: intimated that NP6 will be built in Post Maiden Ski-jump take-off on 20 To +30 m and NP7 will be built in Dec 2014, based on higher recoil To +39 m, with To being CCS approval, followed by signing an MoU between velocity of Nose Landing Gear ADA and HAL. (NLG) than expected, modifications 9.1.1 Aircraft Systems / rectification were carried out tested 9.1.2 Aerodynamics & Wind Tunnel testing and integrated with both NP1 and a. Aerodata studies conducted for NP2 aircraft. Ski jump take-off o deployment of LEVCON at 30 and carried out successfully with 25o upward positions. modified Nose Landing Gear during b. P e r f o r m a n c e s t u d i e s w e r e April 2016 flight trials at SBTF, Goa. conducted for take-off and landing with LEVCON deflected at 30oand Ski Jump launch from Restraining 25o upward positions. Gear System (RGS) has also been c. Aerodata studies conducted for the carried out with R-73 CCM missiles. aircraft with Arrestor Hook System and fairing integrated. Clearance for high sink rate flareless landing up to 4 m/sec has been 9.1.3 Airframe and Mechanical Systems obtained based on STS-MAST a. Airframe: Structural clearance for higher sink testing. Flareless landing up to 3.2 rate (4 m/s) has been obtained from m/sec sink rates was carried out RCMA (A/c). Higher sink rate landing during the May 2016 detachment to tests were carried out at SBTF, Goa. SBTF, Goa.

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Intermittency of Main Undercarriage high subsonic flight to improve L/D extension was observed during ratio, has been integrated on to the ground operation. A detailed defect aircraft with a modified stub wing that investigation was carried out and sustains higher loads. Rotary gear rectified by introduction of modified actuators procured from M/s MOOG pin-roller and structural stopper. Up- has also been tested on rig and lock rigging based on Ground test integrated on the NP1 & NP2. Flight results was carried out and cleared for o testing with LEVCON at 0 , 30 and -25 further flight testing. positions have been successfully 9.1.4 Engine completed. NP2 has been integrated with 03 Auxiliary Air Intake Doors (AAID) in order to 9.1.7 Arrestor Hook System (AHS) augment pressure recovery to facilitate The Arrestor Hook Assembly and the better Ski-jump take-off characteristics. It actuator-cum-damper assembly are developed and integrated with Iron Bird II has been successfully validated during the for testing. The AHS has been integrated on Ski-Jump take off trials of NP2 during the LCA Navy Fighter NP2 and SCT/GVT detachment to SBTF, Goa and found testing successfully completed. Assembly satisfactory. of Arrestor Hook System for integration on 9.1.5 FCS and Control Law NP1 is under progress. a) Based on the inputs from Maiden Ski-jump launch in Dec 2014, Control Law for Ski jump was updated and tested during April-May 16 Ski Jump launches at SBTF, Goa. b) Approach Angle of Attack Hold Control (AAHC) mode of CLAW for landing has been developed, and flight evaluation was carried out at Bangalore and Goa. c) CLAW for flights with LEVCON positioned at 30o and 25o upward positions has been developed and flight testing has been carried out successfully. 9.1.6 LEVCON L e a d i n g E d g e V o r t e x C o n t r o l l e r (LEVCON), a moveable control surface hinged along the wing apex inboard region with 3 position operation, viz., 0° for normal flight & take-off, 30o 'up' for landing Arrestor Hook System Integrated on on an aircraft carrier and 20° 'down' for LCA Navy Fighter (NP2)

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9.1.8 Avionics & Electrical System exploitation by Indian Navy MiG29K for Field Carrier Landing Practices (FCLPs). a) Software for the additional / changed functionalities has developed and Carrier Compatibility Tests are initiated on ported to the Open Architecture LCA Navy Trainer at SBTF. Computer (OAC).

b) 17 degree HUD has been installed on Following activities are carried out during NP1 aircraft for better over the nose first phase of trials: vision. Ÿ Two blocks of flight trials at SBTF has c) M u l t i M o d e R a d a r ( M M R ) , c o - been successfully completed during developed with M/s.ELTA, Israel, has April and May 2016. been successfully integrated on LCA Ÿ Restraining Gear Compatibility Navy Fighter (NP2). The LCA Navy has evaluations and roll over successfully data link as additional feature in MMR. completed at the Take-off Area. d) Validated software of advance Ski-jump Ÿ Ski Jump launches of LCA (Navy) from is updated and integrated on OAC, Restraining Gear carried out. MF-UFCP, SSDU & FSDU and installed Ÿ Night Ski jump take-off completed in NP1. successfully. e) ECFM software is updated, integrated Ÿ Shake down flights at OLS and TV and tested on LCA Navy A/c for Enhanced Fuel gauging, F2 Pump Auto monitoring system carried out at Operation, Fuel dumping and Hot Landing Area. refueling. Ÿ Aircraft Landing approaches and 9.1.9 Test Facilities parallel run carried out on Landing a) Iron Bird-2 Area Iron Bird-2 has been installed with LCA For further Operations and Maintenance Navy standard landing gear system, support, following actions have already Arrester Hook System and LEVCON actuation system. The fault free testing been taken / being taken: of DFCC and ADC software was carried (i) Project Sanction / MoU with GSL, Goa out in Iron Bird-2 and is cleared for Ski- and CCE R&D (W), Pune are signed for jump take-off. continued Operation and Maintenance Support. b) Shore Based Test Facility (SBTF) (ii) MoU has been signed between ADA The Shore Based Test Facility (SBTF) at Goa is now fully operational and and Indian Navy for SBTF exploitation evaluated using MiG29K in January SOPs. 2014. Since then SBTF is under active

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assemblies were integrated. Structural strength testing has been completed and necessary flight clearance obtained from CEMILAC.

9.1.12 Interface with Aircraft Carrier Details of interface requirements for Carrier operations have been documented. Interactions with Naval Headquarters and other naval authorities are being conducted SBTF - Take-off Area periodically for these requirements.

9.1.13 Arrestor Hook System (AHS) Testing Arrester Hook System Qualification Testing is under progress. Endurance and Burst pressure Qualification of Assistor Jack completed. Qualification testing for Burst Pressure for Jack Damper Assembly is under progress. Endurance test of Jack

SBTF - Landing Area Damper assembly is also under progress. Limit Load Test for Arrester Hook System 9.1.10 Landing Gear Drop Test Rig Assembly is completed along with STS. LCA Navy Main Landing Gear is tested and certified for 6.8 m/s and Nose Landing Gear 9.2 LCA Navy Mk2 tested for up to 6.1 m/s sink rate in drop test 9.2.1 Programme rig at Ground Test hangar. Based on the test feedback the landing gears have been Govt. of India sanctioned development of modified. Drop test specimens of modified two LCA(Navy) Mk2 single seat Fighter Landing Gears are under manufacturing. prototypes (NP3 & NP4) under FSED Navy Development of a new Drop Test Facility for full qualification testing (7.1 m/s) of both Ph-2. Main and Nose Landing Gears of LCA The LCA(Navy) Mk2 is being designed (Navy) has been completed at HAL -ARDC. primarily to provide air defence to the fleet onboard Carrier and meeting all the 9.1.11 LEVCON Structure Test Rig mission objectives set out by the Indian LEVCON, a new flight control surface Navy. Significantly improved aircraft per- introduced in LCA Navy, had a mandatory requirement for strength test qualification. formance largely better than AF-Mk1 and A special test rig was developed and the integration of full suite of weapons are LEVCON, Stub Wing & Air Intake capabilities inherent in the design.

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The main contributors to improvement in A meeting chaired by RM on 27 April 2016 LCA(Navy) Mk2 have been identified as was conducted at MoD, Delhi with higher thrust engine, an increased wing participation of IN to review LCA(Navy) area, an area ruled and streamlined Mk2 Programme. IN had brought out configuration, lighter landing gear and performance comparison of LCA(Navy) structure, and improved systems layout Mk2 with MiG-29K with respect to towards better safety and maintainability. ASR/85. Flight control features to reduce approach speed even with an increase of around 2.5 In order to improve aircraft performance tons of Carrier landing mass is a critical dedicated task teams have been constituted capability over LCA(Navy) Mk1. working towards mass and drag reduction. A comparative performance study of various naval combat aircraft was carried System Requirements Review (SRR) with out with Airbus DS consultants and participation of Indian Navy (IN) was presented to stakeholders. carried out in detail with requirements 9.2.2 Design & Development Activities capture and document prepared. (a) Aerodynamics & Configuration: Concept design of LCA(Navy) Mk2 has been Air Vehicle Configuration of LCA (Navy) completed and detail design phase initiated. Mk2 is a critical activity during the concept A detailed Preliminary Design Document design phase. The major activities carried for LCA(Navy) Mk2 has been prepared and out are: provided to IN. Carrier compatibility Ø NMG V0.6L has been base lined for requirements of INS Vikramaditya and INS detail design Vikrant have been captured and necessary Ø Improving performance in terms of low features incorporated in design. supersonic wave drag, acceptable cg limits for stability and control criteria . Based on requirement to consider wing for zero ballast design. Ø folding to overcome the aft lift interference Optimized LEVCON & Shelf Flaps to on INS Vikramaditya, a Technical Note was achieve approach speed reduction for carrier landing. prepared and submitted to IN. The note Ø LEVCON converted into an active details rationale behind Wing outboard shift surface permitting operations with for LCA(Navy) Mk2. Issues in not opting higher instability to achieve improved for a wing fold and also restrictions in agility and performance. carrier take of mass if the wing is retained as Ø Ventral Airbrakes for performance with in Navy Mk1 was brought out. low interference

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Ø Air intake redesigned for bigger GE- (b) Airframe and Mechanical systems: F414-INS6 engine, with lip and cowl Airframe: profiles and auxiliary doors optimized for Preliminary Structure Layout with zero superior performance at low speeds for thickness model for NMG Version V0.06L improved carrier launch capability for Front, Centre and Rear Fuselage incorporating 1020 mm longitudinal plug, 700 mm lateral plug. Concept studies of alternate Structural Layout for iterations on Inboards layout based on System requirement were undertaken.

Three view of V0.06L

Ø 1:10 scale low speed wind tunnel model fabricated at NAL and was tested in the HAL wind tunnel. Ø Wind tunnel data correlation study with CFD simulation carried out and found to Schematic of Structural & match very well. Equipment layout for V0.06L. Based on the iterations carried out in Main Landing Gear (MLG) interface with configuration performance evaluation was Airframe has been defined. This involved also computed to arrive at optimum studies for MLG load path and definition of solution. The major activities undertaken structural attachment to fuselage. Structure are: layout for Nose Landing Gear (NLG) to suit Ø Installed performance estimation of new the modified aircraft geometry is in GE-F414-INS6 engine in LCA (Navy) progress. Arrestor hook structural integration concepts for different schemes Mk2 was carried out were carried out. Ø A comparative study on performance with contemporary Naval aircraft was Finite Element Model (FEM) of Airframe carried out and shared with IN. was prepared and detailed stress analysis Ø Mission performance analysis for three for critical carrier landing load conditions IN profiles viz., Air Defence, Anti ship evaluated. As a result of this analysis it is and Ground strike were carried out and found that the bending moment loads for has been established to meet the IN most critical 2 point landing case on the requirements. Maximum capabilities in fuselage is around 30% lesser than in Navy various IN defined missions to bring out Mk1. This was identified as a potential margins available has also been weight reduction opportunity and a evaluated. detailed study undertaken.

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Fuel tank layout to meet increased internal Engine: capacity and c.g management has been Higher thrust Engine GE-F414-INS6 is to be defined to carryout detail design. installed in LCA(Navy) Mk2. Updated Performance Cycle Deck(PCD) and CAD The Airframe team took active participation model of the Engine made available for in workshops and webex discussions with design studies. ASMET and other Airbus DS team at ADA to converge on a qualification tests have been successfully feasible structural design solution. completed by GE, USA and delivery of engines scheduled. Detail design of Airframe is in progress and CAD models/drawings are being created in Fuel Systems: concurrent design environment. Top level requirements of fuel system was finalized with the involvement of Indian Landing gear & Arrestor Hook: Navy. LCA(Navy) Mk2 is conceptualised The MLG configuration of LCA (Navy) Mk2 with active fuel flow proportioner transfer with optimized structural interface made system. The concept was finalized based on feasible by means of 350 mm additional interface definition with interdisciplinary space in the Y-direction of the aircraft has design teams. Fuel system design of been finalized. LCA(Navy) Mk2 is supported by Airbus DS as part of engineering support in the Following actions have been carried out: Ø General Arrangement of Landing Gear Design Consultancy. System. Ø Estimation of Landing Impact & Ground Manoeuvring Loads. Based on the above, Interface control Ø Kinematics of Main Landing Gear & LG documents for Fuel system with other Doors Ø Sizing of tyre and wheel size systems that include Propulsion system, Avionics, Secondary Power System, Kinematics of Nose Landing Gear & Doors Hydraulic system, structures, Environment has been updated to suit the new geometry Control System and Control law were V0.06L prepared and provided to Airbus DS team for their comments and feedback. Arrestor Hook design as a conformal As an inherent feature of active fuel transfer concept with Y-hook arrangement is being progressed by ARDC. Forcing function system, pumps are installed in all fuel loads & Estimation of AHS Jack Loads has tanks. Electrical Power requirements in been carried out. normal and emergency modes for this system was estimated.

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Development activities initiated for (d) Avionics & Weapon systems: procurement of smart fuel system The Avionics architecture of LCA(Navy) Mk2 is to be adapted from the LCA-AF components such as digital fuel gauging Mk2. Navy specific features are to be probe, optical level sensor, transfer pumps implemented based on interactions with inbuilt pressure transducer and Non- currently in progress with Indian Navy. return valves, intelligent line replaceable units(LRUs) for pressurization and venting Feedback on AESA Radar and Communi- cation interface has been received from IN. system, etc., with original equipment Network communications requirements manufacturer (OEM). has been sought from IN.

(c) Flight Control System and Control Law: Preliminary cockpit layout study for 19.8 Degree HUD has been carried out and Preliminary Design Document for IFCS feedback provided to CSIO, Chandigarh including IFCS Architecture released. Study who are developing this LRU. of alternate configurations for Active LEVCON including Single / Multiple Studies for integrating Automatic Carrier Linear Actuators was carried out. TEX flap Landing System (ACLS) have been introduced for reducing approach speed initiated with participation of IN. which would provide ~5 knots speed Interaction with NEC, Mumbai, to capture reduction. EMI/EMC interface requirements on Carrier carried out. Usage of available Electromechanical / Electro hydraulic actuators for Shelf flap is (e) Test Facilities / Rigs: Shore Based Test Facility (SBTF): The under finalization. existing SBTF at Goa would be utilised for shore based testing of LCA(Navy) Mk2. Control Law (CLAW): Landing gear test rig: Development of test Based on the configuration changes carried rigs to undertake full qualification of MLG out in LCA(Navy) Mk2 and the Aero data & NLG and Nose wheel steering is provided by Aerodynamics group, planned. simulations were carried out and based on Fuel System Rig: A fuel system test rig to results obtained, detailed interactions with evaluate the fuel system performance with Airbus DS consultants have been effective emphasis on transfer sequence and its towards finalizing LCA(Navy) Mk2 reliability is planned. configuration. Iron Bird: Iron Bird-3 is planned to be set up at ARDC for qualification of FCS.

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9.2.3 Airbus DS Design Consultancy Ÿ Necessary changes in the structure Quarterly workshops involving Aircraft and systems to integrate the new design experts in major disciplines is in engine Ÿ effect as part of Design Consultancy with Weight reduction to improve per formance M/s Airbus DS, Germany. The experts visit Ÿ Unified EW Suite (UEWS) ADA for interactions with respective design Ÿ Development of new DFCC, its test teams. Based on the Design suggestions, facilities and integration design teams involving Aerodynamics, Ÿ Upgrade/modification/main- Structures and various groups have evolved tenance of test facilities. Concept design of LCA (Navy) Mk2. ARDC, HAL as principal partner is involved in 10.2 Additional Scope: these design activities. Extensive studies were carried out at ADA to make suitable changes in LCA AF Mk2 to address the maintainability The last 3 quarterly workshops (Total 11) issues observed in LCA AF Mk1, planned as part of detail design phase has to improve the systems like fuel, landing be rescheduled and hence a requirement for gear and brakes, electrical, armament PDC extension of this design consultancy etc. Also a number of new/upgraded up to Dec 2017 is needed. systems have been incorporated to make the aircraft more contemporary. 9.2.4 Follow Up Activities planned As a result, the scope for FSED Phase 3 a) Detail design of LCA(Navy) Mk2 increased substantially due to b) High speed wind tunnel model extensive changes incorporated to have fabrication and tests for force & moment an improved aircraft with improved and air intake performance in all aspects. Important c) Development of Assembly Jigs d) Raw material procurement new/ upgrades of systems are listed e) Fuel test rig below: Ÿ Introduction of 500mm plug in fuselage 10. LCA AF Mk2 Ÿ Active Electronically Scanned Array 10.1 Backg r ound: LCA AF Mk 2 was (AESA) radar conceived as the performance of LCA AF Ÿ Mk1 was found inadequate with GE- On Board Oxygen Generation F404-IN20 engine The scope of FSED System (OBOGS) Ÿ Phase 3 as per project sanction is as New Cockpit with larger size smart follows:- displays Ÿ Ÿ Design, develop and build two One Mission Management and Display Computer (MMDC) in aircraft with place of two Open Architecture Ÿ New Engine Computers Ÿ HMDS based on optical sensor

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Ÿ Smart HUD with improved Field of 10.5 Progress of Design and Development Vision Activities: Ÿ Higher power Jet Fuel Starter 10.5.1 Configuration & NMG: Ÿ Servo controlled Airbrake under the The configuration of LCA AF Mk2 has command of DFCC control been frozen. The Numerical Master Ÿ Pressurized Fuel System Geometry (NMG) has been revised Ÿ Unified Pylon Interface Computer based on recommendations of PDR (UPIC) in place of individual Pylon Committee to improve performance. Interface Boxes The changes in NMG have resulted in Ÿ Combined Interrogator Transponder drag reduction and increase in fuel (CIT) c o n t e n t b y a b o u t 2 0 K g . T h e s e Ÿ Indigenous Actuators improvements are going to result in i m p r o v e d p o i n t a n d m i s s i o n Ÿ NVG compatible lighting performance.

10.3 Activities Carried out: 10.5.2 Inboards & Layout: The inboards have Presently, the configuration of LCA AF b e e n f i n a l i s e d a d d r e s s i n g t h e Mk2 has been frozen with all the design accessibility and maintainability issues improvements and Preliminary Design observed in LCA Mk1. Review (PDR) has been carried out in Ÿ Layouts preparation is in progress. June 2014 and detail design is in Ÿ The station wise mass distribution is under finalisation. progress. GE-F414 engine was selected as the higher thrust engine for LCA AF 10.5.3 A e r o d y n a m i c s : A n u m b e r o f Mk2 and a contract was signed with M/s aerodynamics improvements have GE, USA in September 2012. The CDR of been carried out to reduce drag and alternate engine has been completed. improve performance: Engine is undergoing final qualification Ÿ Drag reduction studies have been and lifing evaluation tests. completed. Canopy reshaping, outer cowl modification, actuator fairing 10.4 Milestones Achieved: extension and supersonic pylons Following milestones have been have resulted in approx 20 counts (8%) drag reduction in supersonic achieved: regimes. Ÿ Configuration freeze Ÿ Wind Tunnel studies have been Ÿ Engine contract finalization completed. Ÿ In-board and NMG freeze Ÿ Aero loads computations have been Ÿ PDR completed.

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10.5.4 Airframe: 10.5.7 Integrated Flight Control System: Ÿ Three door AAID finalised. Ÿ DFCC: CDR completed. Realization Ÿ BMI material developed for high of QT unit by 31st Dec 2016. temperature applications. Ÿ Ÿ Composite pipelines developed for Indigenous Actuators: Primary ECS. Actuators QT completed, Iron Bird Ÿ Spine widened for providing testing completed. Being evaluated accessibility and maintainability. on LCA Mk1. Secondary Actuators Ÿ Pilot step provided for pilot's under development. Air worthy emergency egress. units will be available by December Ÿ SPS bay redesigned to improve 2016. maintainability.

10.5.5 Engine: 10.5.8 Avionics: Ÿ Aircraft engine bay ventilation Ÿ Avionics architecture has been scheme has been finalised. finalised. Ÿ Engine-Airframe Interface Control Ÿ New cockpit with bigger size (6”x8”) Diagram (ICD) has been prepared. Ÿ Aircraft Qualification Tests have been displays has been designed. c o m p l e t e d . A S M E T ( A i r c r a f t Ÿ Development of new LRUs is in Simulated Mission Endurance Tests) progress. results are under discussion. Ÿ Avionics will be ready by Dec 2018. Ÿ New JFS with higher torque GTSU- Ÿ Configuration of Active Phased 135 is under development. Array based Unified Electronic 10.5.6 Mechanical Systems: Warfare Suite (UEWS) finalised. Ÿ Layouts preparation and detail Ÿ The number of elements that can be design is in progress. incorporated with the existing Ÿ Feasibility to increase wheel size for geometry for the Antenna Array unit increasing the capacity of brake of AESA Radar has been finalised system are in progress. and performance parameters like Ÿ Trials to offload one hydraulic system range and Effective Radiated Power to reduce the load on JFS during (ERP) computed. starting are going on. This will help in Ÿ cold weather high altitude opera- N i g h t V i s i o n G o g g l e ( N V G ) tions. c o m p a t i b l e L E D l i g h t s f o r Ÿ Liquid Cooling System configura- Navigation lights and Taxi / tions, separate for AESA and UEWS Landing Lights are being developed. have been finalised. Engineering models have been Ÿ Studies to shift the Air to Air refueling developed. Performance is being probe to right are in progress to evaluated. obviate probe coming in Field of View Ÿ Conformal antenna developed for of Head Up Display (HUD). V/UHF.

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10.5.9 Consultancy in Select Areas: Design Ÿ Electrical modeling of LCA AF Mk2 to consultancy is being sought in specific study indirect effect of lightning is in areas like Fuel System, Landing Gear & progress at IISc, Bangalore. Brake System, Lightning Compliance Ÿ Studies to bring out necessary changes and Design for Manufacturing and in LRUs to have Push-fit type A s s e m b l y . T h e p r o p o s a l f r o m connectors for quick removal/fitment M/s Airbus DS has been received. TEC of the same have been completed. is under progress. Ÿ Weight reduction studies have been carried out and design improvements 10.5.10 Training on Modularization: required to reduce weight have been As LCA AF Mk2 design is planned to be identified. modular, a training to ADA & ARDC 11. ADVANCED MEDIUM COMBAT designers on modularization by a AIRCRAFT – AMCA global design house is being pursued. The Government sanction for feasibility studies Response to RFP has been received. of design and development of Advanced TEC has been completed. Medium Combat Aircraft (AMCA) was accorded on 5th Oct 2010, at a cost of Rs.90.5 10.5.11 Design Outsourcing: Crores, for a duration of 1 ½ years initially and The commercial process to augment the subsequently PDC was extended upto 31st existing resources by utilizing the March 2017, in order to facilitate the services of Indian private industry to continuation of next generation advanced assist Designers of ADA and HAL in technology development projects. Detail Design is in progress. 11.1 AMCA Feasibility Report: Feasibility studies have been carried out 10.5.12 Interdisciplinary Studies: Following studies are in progress to bring out based on IAF's Top Level Operational improvements in design: Requirements and completed the scope of the project. Feasibility Report was Ÿ LCA AF Mk2 cockpit assessment for compiled and Review held in November new anthropometric data received 2013. Feasibility Report was updated in from IAF is in progress. October 2015 with various activities carried Ÿ Thermal mapping studies of aircraft out post the reviews and submitted to Air are in progress. HQ and Hon'ble Raksha Mantri. Ÿ New installation scheme in Avionics 11.2 Present Status: Bay for better accessibility /maintain- ability is under finalisation. AMCA configuration has been arrived after Ÿ Rationalisation of drop tanks is in considerable refinements and it was progress to reduce variety of drop accepted by Indian Air Force. Currently, tanks. the validation tests are being conducted.

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These are AMCA intake model of 1:1 11.3 PSQR Finalization: scale for RCS test, 2nd campaign of high ADA received Draft Preliminary Services speed wind tunnel tests, static intake test, Qualitative Requirements (PSQRs) for dynamic & rotary derivative tests for AMCA in September 2014 from Air HQ for generating un-steady data etc. Also a study and feedback. Appreciation of simulator has been developed which requirements document was forwarded to would be used for sizing the system and Air HQ for finalizing PSQRs. Reviews r e f i n i n g t h e a r c h i t e c t u r e . T h e have been held by VCAS, DCAS and technology development and testing ACAS (Plans). AMCA latest Configuration projects are being continued at various and development approach are accepted work centres. by IAF. First two/three prototypes will fly with proven 90kN class engine and 110 kN class engine will be installed in a phased manner from 4th prototype onwards. PSQR is being amended by IAF towards finalization.

11.4 Powerplant: It has been communicated by Air HQ that the AMCA should be powered by 110 kN class engine. GE, Euroject and Rolls Royce have proposed G-G route for AMCA powerplant. A final decision is awaited.

11.5 Business Models and Execution Methods: As part of AMCA feasibility, various possible scenarios of AMCA Programme execution were studied which includes participation of Indian and foreign aircraft houses in various collaborative modes. AMCA team with the help of Indian Institute of Management, Bangalore (IIMB) has carried out the strategic analysis of possible candidate Programme Execution Models (i) Joint Venture (JV)

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with International Aircraft House (IAH) & 12. GHATAK PROJECT FOR UNMANNED Domestic Aircraft House (DAH), (ii) JV COMBAT AERIAL VEHICLE with IAH, (iii) JV with DAH and IAH as 12.1 Present Status: consultant and (iv) IAH as consultant), for

the Design & Development, Production 1. Draft PSQR compliance document sent and Product Support phases of AMCA to Air Hq. PSQR is finalized by Air Hq on th Programme. 10 June, 2016.

Based on the Analysis & Discussions, it can be concluded that the Execution Model 'JV 2. A lead-in project for “Design of with IAH & DAH' is the unanimous first GHATAK and Development of Critical choice of the Experts for attaining the Advanced Technologies for GHATAK defined Programme Goals in the AMCA and AMCA” is sanctioned for Rs.231.00 Programme. The Execution Model 'JV with crores on 13th May 2016. IAH' stands in the second place followed by 'JV with DAH and IAH as Consultant' Major technologies to be developed under and 'IAH as Consultant' in the third and this lead-in project are broadly classified fourth places respectively. under five technology areas viz., (a) Model Based Systems Engineering (MBSE) 11.6 Way Forward: (b) Autonomous flight control Permission may be given to initiate next technologies phase of activities. In-principle approval (c) Aerodynamics and Propulsion for submission of CCS papers and Lead-in technologies (d) Stealth computations, project has been sought. measurements, structures & 11.7 AMCA - NAVY: materials (e) Technologies for GHATAK systems Indian Navy (IN) Projected requirement

for Naval variant of AMCA and Focused advanced design tools for Multi- forwarded Top Level Operational Disciplinary Optimization (MDO) using a R e q u i r e m e n t s ( V i d e L e t t e r N o : HPC computing infrastructure will be AO/9670/NAMCA, dated 7th Sep 2015). developed for flying wing configuration improvement studies. Levels of flight Meeting held with VCNS on 24th Nov 2015 autonomy will be increased through at Naval Head Quarters and discussions testing of ATOL and FADS on LCA and held on Way Forward for AMCA – Navy. scaled autonomous flight demonstration th of GHATAK. Through 1/6 scaled flight

32 Annual Report 2015 -2016

model of GHATAK, technologies like 4. Preliminary cost has been estimated by an control law for flying wing, fluidic thrust ADA internal cost committee and a vectoring and stealth materials will be preliminary draft CCS proposal report is tested and evaluated in a cost effective way. prepared based on this cost estimates for TRLs of critical advanced technologies like possible submission later. conformal antenna, SAR, EO/IR, FADS shall be improved and adapted for 5. Work on latest GHATAK configuration 2.3 GHATAK. Full scale GHATAK RCS model will be tested at ORANGE facility to evaluate RCS hot spots and to enable RCS reduction. Weapon release studies and deployment mechanism would be studied using high fidelity unsteady CFD modeling

of URANS. Effective ejector based cooling Latest GHATAK Configuration 2.3 mechanism for embedded high aspect ratio nozzle will be combined with ECS cooling requirements along with compact heat exchangers.

Financial Aspect:

a. Commitments for 2016-17 : Rs.43.00 Cr. b. Cash Out Flow for 2016-17 :Rs.30.00 Cr. c. Planned Commitments for 2017-18 : Rs. 82.00 Cr. 1:7.8 scale GHATAK intake model at IITK

3. Several Advanced Technology proposals for GHATAK and AMCA from DRDO Labs is received and reviewed. First Review meeting for 16 Advanced Technology proposals received from DRDO is completed on 12th and 13th of July, 2016. Based on this review, suggestion for modifications of these proposals has been made.

1:11 scale GHATAK WT model at HAL

33 Annual Report 2015 -2016

12.2 Status of Power plant & “In-principle” of GHATAK Project: GTRE had submitted a draft CCS proposal for a Dry engine for the GHATAK along with “In-principle” approval of GHATAK Program to ADA. After clearance from MoD and MoF, draft was submitted by GTRE to the PMO. A High Level Committee was set up under the Chairmanship of Dr. R Chidambaram (PSA to GoI), with Dr. V K Saraswat (Member, Niti Aayog) and Dr. K Radhakrishnan (Former Chairman ISRO) as members. The committee has submitted its report to CFD simulation on latest GHATAK configurations the PMO.

12.3 Confidence in development of GHATAK aircraft by ADA

The committee endorsed the confidence in the GHATAK aircraft development by ADA based on the design capability assimilated in ADA in developing the

1:7 scale model for autonomous flight testing at Light Combat Aircraft (LCA) being IITK getting ready utilized for configuration finalization for “GHATAK” aircraft.

12.4 Recommendations of the committee

The UCAV aircraft and engine technology is highly classified and is unlikely that any country would share this technology with India. Hence it is 1:14 scale model for flight testing getting ready inescapable requirement to develop an

34 Annual Report 2015 -2016

Indian UCAV and its engine considering the future combat warfare scenario. The development of an unmanned combat aircraft is a “national imperative” toward self reliance in aerospace technologies. The committee strongly recommended the sanction of the project at the earliest to be at par with other developed countries. Tejas at Bahrain Air Show 2016 13.2 Tejas aircraft participated in IAF 12.5 Work share allocations for the program Exercise Iron Fist 2016. 14 VIP Visits The committee also submitted the work 14.1 Air Chief Marshal Arup Raha, PVSM, share allocation of for executing the AVSM, VM, ADC, Chief of Air Staff GHATAK aircraft program with visit to ADA and flying Tejas on program office and prime responsibility 17.05.2015. with ADA, and indicated responsibility to DRDO, HAL & other labs.

12.6 Way Forward: At the moment no GHATAK aircraft program has been sanctioned to ADA and only funds for developing advanced Technologies have been sanctioned. CAS flew Tejas on 17.05.2015 Using these funds some of the critical 14.2 Air Marshal PP Reddy, VM ADC, Chief technologies will be developed within of Integrated Defence Staff (CISC) visit the country through sponsored projects. to ADA on 19.05.2015.

13. ADA PARTICIPATION 14.3 Rear Admiral Phillipose G Pynumootil, Assistant Chief of the Naval Staff (Air) 13.1 ADA along with DRDO participated in visit to ADA on 11.07.2015.

Bahrain International Air Show 2016 14.4 Wing Commander HL Gowtham, during 21st to 23rd January 2016. Deputy AA (Designate) EOL, Paris, France visit to ADA on 27.07.2015.

35 Annual Report 2015 -2016

14.5 Shri Manohar Parrikar, Hon'ble Raksha 15.2 Air HQ Reviews Mantri vist to ADA on 06.09.2015. Monthly Review of Tejas Programme with Deputy Chief of Air staff (DCAS), IAF as 14.6 Shri G Mohan Kumar, Defence Secretary th visit to ADA on 25.09.2015. Chairman has been initiated w.e.f 12 14.7 Dr A R Sihag, DG (Acquisition) visit to ADA August 2006. Last Monthly Review on 08.10.2015. meeting was conducted at ADA on 29th 14.8 Shri S S Mohanty, Financial Adviser April 2016. (Defence Services) visit to ADA on Quarterly Review of Tejas Programme 28.11.2015. with Chief of Air staff (CAS), IAF as 15. Meetings of the Managing Bodies Chairman & with participation of all stake holders has been initiated w.e.f 29th th The 30 Annual General Body Meeting was December 2006. 32nd Quarterly meeting th held on 18 December 2015. The meeting was conducted at Air Head Quarters, IAF, adopted the Annual Report of ADA nd New Delhi on 22 March 2016. including the Audited Accounts for the year 2014-15. Thereafter, the reports were placed 15.3 Administration on the tables of both the Houses of During the year, 24 persons joined ADA Parliament. Two Governing Body meetings and 10 persons retired on superannuation, were held during the year. The Agenda for 5 persons resigned their jobs for better the meetings included presentation of the prospects, 4 officials repatriated and 2 status of the LCA and LCA (Navy) persons expired. Programmes.

15.1 Programme Reviews held during 2015-16 15.4 National Flight Test Centre (NFTC) FY are: NFTC is headed by an Air Vice Marshal of Programme Review meetings with all stake the Indian Air Force. During the year holders are held regularly to monitor under report, 5 Test Pilots and 3 Flight Test closely the progress of the Programme. Engineers (FTE) of IAF / IN were on Ÿ Programme Co-ordination Team (PCT) deputation to the NFTC of ADA. meeting held on every Monday. Ÿ Tejas Programme Review by Director 15.5 Project Monitoring Team (PMT) General (DG) – ADA is held at regular IAF and IN have constituted PMT's to have intervals. lateral interaction with ADA, NFTC, ASTE Ÿ Review of Tejas Programme with Honorable Raksha Mantri was held and HAL for timely accomplishment of the continuously to monitor the progress. IOC and smooth induction of LCA into the Last Meeting was held on 6th September IAF and monitoring progress of LCA 2015 at New Delhi. Navy activities respectively.

36 ADA Annual Report 2015-16

INDEPENDENT AUDITOR'S REPORT TO THE MEMBERS OF THE GENERAL BODY OF ADA

1.
Reports on the Financial Statements and perform the audit to obtain reasonable assurance about whether the financial We have audited the accompanying financial statements are free of material misstatement. s t a t e m e n t s o f M / s . A e r o n a u t i c a l Development Agency (hereinafter referred to An audit involves performing procedures to st as 'ADA', Bangalore as at 31 March 2016), obtain audit evidence about the amounts and which comprises the Balance Sheet as at March the disclosures in the financial statements. 31, 2016 & Statement of Income & Expenditure The procedures selected depend on the Account and Receipts & Payments Account for auditor's judgement, including the the year then ended and a summary of assessment of the risks of material significant accounting policies and other misstatement of the financial statements, explanatory information. whether due to fraud or error. In making those risk assessments, the auditor considers 2.
Management Responsibility for the internal financial control relevant to the Financial Statements Society's preparation of the financial statements that give a true and fair view in Management is responsible for the preparation order to design audit procedures that are and presentation of these Financial Statements appropriate in the circumstances, but not for that give a true and fair view of the financial the purpose of expressing an opinion on position and performance of the society. This whether the Society has in place an adequate responsibility also includes maintenance of internal financial controls system over adequate accounting records for safeguarding financial reporting and the operating the assets of the Society and for preventing and effectiveness of such controls. An audit also detecting frauds and other irregularities; includes evaluating the appropriateness of selection and application of appropriate the accounting policies used as applicable to a accounting policies; making judgements and Non Profit organisation and the reason- estimates that are reasonable and prudent; and ableness of the accounting estimates made by design, implementation and maintenance of the Governing Body, as well as evaluating the adequate internal financial controls, that were overall presentation of the financial state- operating effectively for ensuring the accuracy ments. and completion of the accounting records, relevant to the preparation and presentation of We believe that the audit evidence we have the financial statements that give a true and fair obtained is sufficient and appropriate to view and are free from material misstatement, provide a basis for our audit opinion. whether due to fraud or error. 4.
ADA is a Non-Profit Organization registered 3. Auditor's Responsibility under Societies Registration Act, 1860 with the main object of Scientific Research in We conducted our audit in accordance with Aeronautical Science. The Balance Sheet, the auditing standards generally accepted in Income and Expenditure Account and India. Those standards require that we plan Receipts and Payments Account are prepared in accordance with the guidelines /

37 Annual Report 2015-16 ADA

instructions issued by the Ministry of Defense 7.
Opinion while sanctioning the Grants-In-Aid for a specific project. The Accounting Standards
In our opinion and to the best of our issued by Institute of Chartered Accountants information and according to the explanations of India are applicable to the entities which are given to us, the aforesaid financial statements engaged in Commercial, Industrial or read with the Accounting Policies and Business activities. As ADA is not engaged in Explanatory Notes give the information these activities, in our view, such Accounting required and give a true and fair view. Standards are not applicable. a) In the case of the Balance Sheet, of the state 5. As mentioned in the Accounting Policy, the of affairs of the Society as at March 31, society follows Cash basis of accounting, the 2016. society prepares Balance Sheet, Income and b) In the case of the Income and Expenditure Expenditure Account on the cash receipts and Account, of the net deficit transferred to disbursements basis. On this basis, income Management activities for the year ended and the related assets are recognized when on that date; and received rather than when earned and c) In the case of the Receipts and Payments expenses are recognized when paid rather Account for the year ended on that date. than when the obligation is incurred. 8.
Report on Other Requirements: 6. Expenditure / balance stage payments of work centers incorporated in the accounts
We report that: (Limited to sanctions issued by ADA) is as per the terms of the systems approved by the a) we have obtained all the information and Government and consistently followed by Society. These expenditure statements are explanations which to the best of our certified by the statutory auditors or their knowledge and belief were necessary for the internal auditors or authorized persons of the purpose of our audit; respective agencies accepted by ADA. As per b) in our opinion proper books of account have the notification No.1/1/92/4089/D(R&D) been kept by the Society so far as appears from dated 07.10.1992 issued by the Department of our examination of those books; Defense (R&D), Ministry of Defence, c) the Balance Sheet, Income and Expenditure Government of India those statements need Account and Receipts and Payments Account not be further audited by us. Hence, the said dealt with by this report are in agreement with statement of account received from work the books of account. centers have not been audited by us.

for ABS & CO. CHARTERED ACCOUNTANTS FRN : 008203S Date : 12.09.2016 Sd/- Place : Bangalore (H.G. ANAND) Partner M.No. 206226

38 ADA Annual Report 2015-16

SIGNIFICANT ACCOUNTING POLICIES 1 GENERAL:

Ÿ Aeronautical Development Agency (ADA) is a Non-Profit organization registered under Societies Registration Act, 1860 on June 16, 1984. Ÿ The objectives of ADA is to execute research in aeronautical science, design & development of various types of aircrafts and to collaborate with scientific agencies, research centres & educational institutions etc., in the areas of technology relevant to the objectives of the society. Ÿ Government of India, Ministry of Defence, Department of Defence Research & Development, New Delhi is funding the projects of ADA.

2 METHOD OF ACCOUNTING:

ADA follows cash basis of accounting.

Ÿ The depreciation does not arises in the case of ADA as the entire expenditure is classified as R & D expenditure and there is no distinction between capital & revenue. The R & D expenditure for the project sanctioned to work centres Viz. HAL divisions, DRDO Labs, CSIR Labs, Academic Labs and other PSUs included certain expenditure on facility establishment. Ÿ The Grants-in-Aid drawn from time to time towards projects has been disclosed as 'Liability' and the Research & Development expenditure incurred has been disclosed as 'Assets' in the Balance Sheet. Ÿ The expenditure incurred towards projects is disclosed as Research & Development expenditure and not reduced from Grants-in-Aid. Ÿ The unspent Grants-in-aid is refunded after completion /closure of the projects. Ÿ Expenditure in foreign currency is accounted on the basis of rates of exchange prevailing on the dates of actual remittance. Ÿ As per the advice of Expert Advisory Committee of Institute of Chartered Accountants Of India, New Delhi, ADA discloses the Interest earned on short term deposits made out of temporary surplus from Grants-In-Aid under both Income side & Expenditure side as contra entries in the Income & Expenditure Account. It is also disclosed in the liability side of the Balance Sheet to the extent of the interest earned on the Grants-In-Aid.

3 BALANCE SHEET:

Contributory Provident Fund:

The CPF is established u/s 8(2) of the PF Act of 1925 approved by Government of India vide Office Memorandum dated 27.04.1987. Subscription from employees & employer's contribution is invested in approved securities.

39 Annual Report 2015-16 ADA

Ÿ Research & Development expenditure on projects are disclosed in Balance Sheet in accordance with the FSED line items. Year end inventory if any, is also shown as expenditure against respective FSED line items.

Work Centre Expenditure:

Ÿ Funds are advanced by ADA to workcentres to meet expenditure on approved work packages assigned to them.

Ÿ Utilization of these funds by the workcentres for work packages is accounted based on Provisional/ Audited monthly / quarterly / annual accounts received from them.

Ÿ In respect of consultancy and fixed price contracts, stage payments made in accordance with the milestones of agreements with workcentres are treated as expenditure.

Ÿ Expenditure incurred by the workcentres is accounted based on the certificates furnished by the Competent Authorities of respective agencies or their Internal Auditors or their Statutory Auditors. This is in accordance with the Government of India, Ministry of Defence letter no. 1/1/92/4089/D(R&D) dated 7.10.1992.

4 INCOME AND EXPENDITURE ACCOUNT:

Ÿ Income & expenditure Account reflects expenditure incurred under the head “Project Management Activities” for which a distinct provision has been made in the sanctioned cost estimates. The net deficit (after taking into account the income received) is transferred to Project Management Activities. Ÿ The net excess of expenditure over income, of Income and Expenditure Account has been transferred @ 85% to Air Force FSED Phase 3 (AF MK2) and 15% to Navy FSED Phase-1. This allocation is as per the recommendation of the cost revision committee and the same approved by the Cabinet Committee for Security. Ÿ Interest on CPF accumulations is credited to subscribers' account at rates notified by the Government each year. The interest credited to subscribers accounts and interest earned on CPF investments are treated as Expenditure & Income of the ADA respectively.

5 RECEIPTS AND PAYMENTS ACCOUNT:

Ÿ Transactions shown in Receipts & Payments account are net. Hence, the receipts and payments shown in Receipts and Payments Account do not reflect actual Cash and Bank receipts and payments relating to the accounting period.

40 ADA Annual Report 2015-16

Ÿ Funds released to work centres against work packages are accounted as advances less expenditure booked during the year based on their expenditure statements. Negative balances appear in cases where expenditure booked in the year is in excess of funds released in the year. The excess expenditure is met from balances remaining with work centres at the commencement of the financial year or further fund release to work centre will be under process.

for ABS & CO. CHARTERED ACCOUNTANTS FRN 008203S

Sd/- Sd/- Sd/- H G ANAND M.S. KRISHNA MURTHY M A ANANDAN PARTNER Chief Finance Officer Offtg. Jt. Director (Finance) Membership No. 206226

Sd/- Sd/- CMDE. (RETD.) C.D. BALAJI K. RAVI KUMAR Secretary FA to DG-ADA

Place : Bangalore Date : 12.09.2016

41 Annual Report 2015-16 ADA

BALANCE SHEET as at March 31, 2016

Amount in Rs.

Particulars Schedule Current Year Previous Year

Funds & Liabilities:

Grants-in-aid for Projects 1 1,12,71,16,60,144 1,07,81,94,60,144 Interest on Grants-in-aid 2 3,01,29,93,027 2,86,69,99,713 Software Support Activities 3 75,58,40,628 69,84,73,598 Current Liabilities 4 68,19,78,140 55,29,32,844

Total 1,17,16,24,71,939 1,11,93,78,66,298

Assets: R & D Expenditure for Projects 5 1,15,54,40,87,950 1,07,83,23,13,348 Software Support Activities 6 1,11,90,218 1,11,90,218 Investments 7 55,42,15,210 51,07,28,303 Current Assets, Loans & Advances 8 1,47,01,971 1,46,61,673 Cash & Bank balances 9 1,03,82,76,590 3,56,89,72,756

Total 1,17,16,24,71,939 1,11,93,78,66,298

Explanatory Notes 16

Accounting Policies and Explanatory Notes forming part of accounts annexed.

This is the Balance Sheet referred to in our report of even date.

for ABS & CO. CHARTERED ACCOUNTANTS FRN 008203S

Sd/- Sd/- Sd/- H G ANAND M.S. KRISHNA MURTHY M A ANANDAN PARTNER Chief Finance Officer Offtg. Jt. Director (Finance) Membership No. 206226

Sd/- Sd/- CMDE. (RETD.) C.D. BALAJI K. RAVI KUMAR Secretary FA to DG-ADA

Place : Bangalore Date : 12.09.2016

42 ADA Annual Report 2015-16

Schedules Forming part of the Balance Sheet as at March 31, 2016 Amount in Rs.

Particulars Current Year Previous Year

SCHEDULE NO 1: GRANTS-IN-AID for projectsLCA -AIR FORCE

FSED PHASE 1 21,879,959,482 21,879,959,482

FSED PHASE 2 : Opening Balance 53,586,700,000 50,386,700,000

Add: Received during the year 1,360,000,000 54,946,700,000 3,200,000,000 53,586,700,000

FSED PHASE 3: Opening Balance 8,374,400,000 6,274,400,000

Add: Received during the year 1,750,000,000 10,124,400,000 2,100,000,000 8,374,400,000

LCA - NAVY

PDP ACTIVITIES 140,425,000 140,425,000

FSED PHASE 1 : Opening Balance 14,473,800,000 12,973,800,000

Add: Received during the year 600,000,000 15,073,800,000 1,500,000,000 14,473,800,000

FSED PHASE 2 : Opening Balance 4,331,300,000 2,831,300,000

Add: Received during the year 650,000,000 4,981,300,000 1,500,000,000 4,331,300,000

TECH. DEV. TO DEVELOP INDG.

TECHNOLOGY Opening Balance 815,000,000 715,000,000

Add: Received during the year 200,000,000 1,015,000,000 100,000,000 815,000,000

OTHER PROJECTS

IFCAP 199,500,000 199,500,000

KAVERI POLYMER COMPOSITES 33,152,008 33,152,008

NATIONAL PROGRAMME FOR SMART 710,314,509 710,314,509 MATL. (NPSM) DISMAS 147,000,000 147,000,000

FIN FORMING MACHINE 88,300,000 88,300,000

MIG BIS (UPG) TRAINING DEVICES 37,699,975 37,699,975

43 Annual Report 2015-16 ADA

Schedules Forming part of the Balance Sheet as at March 31, 2016 Amount in Rs.

Particulars Current Year Previous Year

TACTICAL MISSION SYSTEM (TMS) 150,000,000 150,000,000

NP - MASS: Opening Balance 1,950,000,000 1,545,700,000

Add: Received during the year - 1,950,000,000 404,300,000 1,950,000,000

INDIAN UNMANNED STRIKE VEHICLE:

Opening Balance 125,000,000 125,000,000

HIGH PERFORMANCE COMPUTING FACILITY: Opening Balance 154,409,170 154,409,170

ADVANCED MEDIUM COMBAT AIRCRAFT - AMCA Opening Balance 600,000,000 400,000,000 Add: Received during the year 273,700,000 873,700,000 200,000,000 600,000,000

OVERHEADS FROM NPSM 22,500,000 22,500,000

OVERHEADS FROM NP-MASS 58,500,000 - Total 112,711,660,144 107,819,460,144

SCHEDULE NO 2: INTEREST RECEIVED ON

GRANTS-IN-AID LCA AIRFORCE (STATE BANK OF 1,384,497,159 1,302,186,785 HYDERABAD) LCA AIRFORCE (STATE BANK OF MYSORE) 898,105,683 898,105,683

FSED NAVY (STATE BANK OF HYDERABAD) 614,002,186 584,262,661

LCA AIRFORCE (ICICI BANK LTD) 42,608,478 42,214,401

LCA AIRFORCE (STATE BANK OF INDIA, NAL) 8,608,801 -

NP-MASS (STATE BANK OF HYDERABAD) 64,964,522 40,075,918

DR. KOTA HARINARAYANA 206,198 154,265

Total 3,012,993,027 2,866,999,713

SCHEDULE NO 3: SOFTWARE SUPPORT

ACTIVITIES CV TECH & MECH SUPPORT 8,887,742 8,887,742

AUTOLAY 281,351,076 281,351,076

INTEREST EARNED 465,601,810 408,234,780

Total 755,840,628 698,473,598

44 ADA Annual Report 2015-16

Schedules Forming part of the Balance Sheet as at March 31, 2016 Amount in Rs.

Particulars Current Year Previous Year

SCHEDULE NO 4: CURRENT LIABILITIES CONTRIBUTORY PROVIDENT FUND 566,465,982 532,143,347

Less: PF Advance (7,017,256) 559,448,726 (8,502,936) 523,640,411

NEW CONTRIBUTORY PENSION SCHEME 329,794 324,934

SECURITY DEPOSIT 474,000 474,000

RECOVERIES & REMITTANCES 405,973 175,347

SUNDRY CREDITORS 74,491 -

AERO-INDIA 2015 - 27,299,527

BIAS 2016 199,800,000

LESS: EXPENDITURE INCURRED 88,435,590 111,364,411

DEFEXPO 2016 12,340,000

LESS: EXPENDITURE INCURRED 2,904,755 9,435,245

DR. DS KOTHARI DRDO CHAIR 7,759,348 7,957,441

Less : BALANCE REFUNDED TO GOVT. - 198,093

Less : Amount Utilised 7,724,755 34,593 7,724,755 34,593

DR. KOTA HARINARAYANA - RESEARCH - 816,301 GRANTS

DR. RAJA RAMANNA DRDO DISTINGUISHED 3,000,000 1,200,000 FELLOW

Less : Amount Utilised 2,718,577 281,423 1,200,000 -

COMMITTEE TO STUDY ORGN ASPECTS &

PROD OF TECHNOLOGIES 1,802,994 1,844,875

Less : BALANCE REFUNDED TO GOVT. - 41,881 Less : Amount Utilised 1,802,994 - 1,802,994 -

REPUBLIC DAY PARADE 6,251,162 7,425,581

Less : BALANCE REFUNDED TO GOVT. - 1,174,419

Less : Amount Utilised 6,251,162 - 6,251,162 - AR & DB PROJECT 200,000 200,000

Less : Amount Utilised 70,515 129,485 32,269 167,731 Total 681,978,140 552,932,844

45 Annual Report 2015-16 ADA

Schedules Forming part of the Balance Sheet as at March 31, 2016 Amount in Rs.

Particulars Current Year Previous Year

SCHEDULE NO 5: R&D EXPENDITURE FOR

PROJECTS LCA -AIR FORCE : FSED PHASE 1 21,879,959,482 21,879,959,482

FSED PHASE 2 :

INFRASTRUCTURE 1,381,995,137 1,352,167,617

AIRCRAFT DESIGN & INTEGRATION 4,286,344,958 3,792,191,574

PROTOTYPE - TOOL FABRICATION 275,130,688 264,187,677

PROTOTYPE - CFC COMPONENTS 829,175,197 788,784,799

PROTOTYPE - AIRCRAFT MATERIAL 1,012,463,613 948,965,219

PROTOTYPE - AIRCRAFT FABRICATION 2,111,437,322 1,988,986,102

GENERAL SYSTEMS 2,510,065,922 2,290,807,927

FLIGHT CONTROL SYSTEM 1,784,166,214 1,306,308,370

AVIONICS - COCKPIT DISPLAY & 1,342,356,230 1,261,870,177 CONTROL PANEL AVIONICS - RING LASER GYRO 146,389,852 137,227,486

AVIONICS - MULTI MODE RADAR 1,085,878,678 1,022,101,241

AVIONICS - EW SUIT DEVELOPMENT 175,517,535 175,517,535

AVIONICS - COMMUNICATION 157,121,141 141,845,506 EQUIPMENT AVIONICS - ELECTRICAL SYSTEM 79,084,655 73,157,203

AVIONICS - OTHER ITEMS 1,165,997,059 1,079,722,607

GROUND TESTING 1,418,174,260 1,319,117,372

FLIGHT TESTING 6,593,563,224 6,340,861,496

TRAINING CONSULTANCY & TECH. 1,607,971,992 1,563,087,766 ASSISTANCE TECHNOLOGY DEVELOPMENT - 555,517,370 481,807,539 DESIGN ANALYSIS TECHNOLOGY DEVELOMENT - 120,454,258 92,751,522 COMPOSITE MATERIALS TECHNOLOGY DEVELOMENT - 12,158,983 921,249 AVIONICS DISPLAY PRODUCT SUPPORT 324,342,595 294,628,465

PROJECT MANAGEMENT EXPENDITURE 4,684,469,062 4,684,469,062

GE ENGINE 3,078,625,188 3,071,552,215

ENGG. CHANGE ORDER 1,463,178,310 1,373,896,542

BALANCES WITH HAL-ARDC (199,828,775) 181,403,809 (Inventory, Work in progress etc) HALs PROFIT 756,482,315 689,396,085

LIMITED SERIES PRODUCTION - HAL BC:

CAPITAL FACILITIES 1,142,173,131 1,142,173,131

46 ADA Annual Report 2015-16

DEFERRED REVENUE EXPENDITURE 1,351,981,666 1,351,981,666

MANUFACTURING COST OF 8 10,482,183,538 10,482,183,538 AIRCRAFTS ADDL. SCOPE OF WORK 2,668,622,035 2,251,107,513

HAL BC: BALANCE STAGE PAYMENT (2,740,983,522) (2,740,652,000)

ADA SUPPLY ITEMS 4,584,585,096 4,497,184,706

56,246,794,927 53,701,712,716

ADD: ADVANCES TO SUPPLIERS 345,580,784 56,592,375,711 371,222,330 54,072,935,046

FSED PHASE 3:

INFRASTRUCTURE 346,360,850 148,117,820

AIRCRAFT DESIGN & INTEGRATION 468,391,531 428,496,703

AIRCRAFT TOOLING, 2,573,698 4,075,718 MTRL&FABRICATION AIRCRAFT MATERIALS 39,311,616 15,064,100

PROTOTYPE - AIRCRAFT FABRICATION 26,553,103 10,970,930

GENERAL SYSTEMS 5,403,672,100 4,606,991,189

FLIGHT CONTROL SYSTEMS 439,143,857 332,553,964

AVIONICS - COCKPIT DISPLAY & 40,695,915 29,437,303 CONTROL PANEL AVIONICS - MULTIMODE RADAR 52,801,583 20,936,579

AVIONICS - ELECTRICAL SYSTEM 13,463,830 -

GROUND TESTING 142,992,350 113,096,516

FLIGHT TESTING 378,409 378,409

TECH. DEVELOPMENT 22,103,501 16,123,814

PRODUCT SUPPORT 371,964 -

PROJECT MANAGEMENT EXPENDITURE 3,312,360,129 2,176,449,129

BALANCES WITH HAL-ARDC 198,200,695 160,544,021 (Inventory, Work in progress, etc) HALs PROFIT 40,366,604 38,032,129

10,549,741,735 8,101,268,324

ADVANCE TO SUPPLIERS 471,410,322 11,021,152,057 587,991,158 8,689,259,482

LCA NAVY :

PDP ACTIVITES 140,425,000 140,425,000

FSED PHASE 1:

INFRASTRUCTURE 199,748,781 184,738,134

AIRCRAFT DESIGN & INTEGRATION 2,596,962,414 2,190,380,404

TOOLING 40,802,656 34,544,666

PROTOTYPE - CFC COMPONENTS 5,802,000 5,802,000

PROTOTYPE - AIRCRAFT MATERIAL 668,246,449 571,096,625

PROTOTYPE - AIRCRAFT FABRICATION 1,454,359,566 1,243,252,157

47 Annual Report 2015-16 ADA

Schedules Forming part of the Balance Sheet as at March 31, 2016 Amount in Rs.

Particulars Current Year Previous Year

TOOLING 40,802,656 34,544,666

PROTOTYPE - CFC COMPONENTS 5,802,000 5,802,000

PROTOTYPE - AIRCRAFT MATERIAL 668,246,449 571,096,625

PROTOTYPE - AIRCRAFT 1,454,359,566 1,243,252,157 FABRICATION GENERAL SYSTEMS 1,181,767,385 1,076,084,497

FLIGHT CONTROL SYSTEMS 822,339,786 796,646,875

AVIONICS - COCKPIT DISPLAY & 229,018,591 205,781,869 CONTROL PANEL AVIONICS - RING LASER GYRO 19,445,696 19,445,696

AVIONICS - MULTIMODE RADAR 239,149,115 234,274,710

EW SUIT DEVELOPMENT 6,686,800 6,686,800

AVIONICS - COMMUNICATION 30,933,815 30,932,248 EQUIPMENT AVIONICS - ELECTRICAL SYSTEM 35,618,564 34,035,495

AVIONICS - OTHER ITEMS 70,066,746 63,762,343

GROUND TESTING 4,768,526,790 4,719,877,402

FLIGHT TESTING 367,151,058 315,148,856

TRAINING, CONSULTANCY & TECH. 378,403,755 378,403,755 ASSISTANCE TECH. DEV - DESIGN ANALYSIS 7,275,674 1,402,704

TECH DEV. -COMPOSITE 2,614,523 2,614,523 MATERIALS TECH DEV - AVIONICS 2,654,480 2,654,480

PRODUCT SUPPORT 217,384 217,384

PROJECT MANAGEMENT 1,264,359,124 1,063,904,241 EXPENDITURE ENGINE INTEGRATION 883,047,322 853,043,372

HALs PROFIT 372,215,464 307,682,649

BALANCES WITH HAL-ARDC 213,683,298 197,741,547 (Inventory, Work in progress, etc) 15,861,097,234 14,540,155,430

ADD: ADVANCES TO SUPPLIERS 78,063,480 15,939,160,714 78,559,389 14,618,714,819

48 ADA Annual Report 2015-16

Schedules Forming part of the Balance Sheet as at March 31, 2016 Amount in Rs.

Particulars Current Year Previous Year

FSED PHASE 2

INFRASTRUCTURE 104,153,079 79,487,281

AIRCRAFT DESIGN & INTEGRATION 207,044,559 104,720,343

AIRCRAFT MATERIALS 41,473,180 41,473,180

GENERAL SYSTEM 49,912,273 44,237,605

FLIGHT CONTROL SYSTEMS 25,855,577 11,724,439

AVIONICS - MULTIMODE RADAR 52,197,333 20,547,578

GROUND TESTING 647,122,861 344,543,427

FLIGHT TESTING 2,843,942 395,988

TRAINING CONSULTANCY & TECH. 609,075,093 294,309,765 ASST TECHNOLOGY DEVELOPMENT - 12,007,389 - DESIGN ANALYSIS GE ENGINE 2,383,425,537 2,014,688,014

BALANCES WITH HAL-ARDC 2,604,933 18,685,061 (Inventory, Work in progress, etc)

HALs PROFIT 23,147,783 13,137,629

4,160,863,539 2,987,950,310

ADVANCE TO SUPPLIERS 752,671,446 4,913,534,985 816,854,138 3,804,804,448

TECH. DEV. TO DEVELOP INDG. TECHNOLOGY: AVIONICS & ELECTRICAL SYSTEM 39,714,151 35,748,339

GENERAL SYSTEM 357,760,675 289,312,337

PROPULSION SYSTEM 150,000,000 150,000,000

AIRFRAME 135,506,963 87,498,186

INTEGRATED FLIGHT CONTROL 147,052,887 107,465,593 SYSTEM AERODYNAMICS 5,940,234 2,260,234

PROTOVEHICLES & MANUFACTURING 121,312,887 121,100,175

ADVANCED PROJECTS 33,253,970 20,194,173

FLIGHT TESTING 9,674,902 1,000,216,669 8,290,302 821,869,339

49 Annual Report 2015-16 ADA

Schedules Forming part of the Balance Sheet as at March 31, 2016 Amount in Rs.

Particulars Current Year Previous Year

OTHER PROJECTS:

IFCAP 199,500,000 199,500,000

KAVERI POLYMER COMPOSITES 33,152,008 33,152,008

NATIONAL. PROG. ON SMART 710,314,509 710,314,509 MATERIAL DISMAS 147,000,000 147,000,000

FIN FORMING MACHINE 81,808,015 81,651,192

MIG 21 BIS (UPG) 37,699,975 37,699,975 TRG./MAIN.SIMULATOR TACTICAL MISSION SYSTEM - TMS 150,000,000 150,000,000

NP - MASS 1,773,607,922 1,660,127,539

INDIAN UNMANNED STRIKE AIR 118,555,239 116,512,766 VEHICLE HIGH PERFORMANCE COMPUTING 154,409,170 154,409,170 FACILITY ADVANCED MEDIUM COMBAT 651,216,495 513,978,574 AIRCRAFT - AMCA TOTAL 115,544,087,950 107,832,313,348

SCHEDULE NO 6: SOFTWARE SUPPORT ACTIVITES CV MECH & TECH SUPPORT 360,655 360,655

AUTOLAY 10,829,563 10,829,563

TOTAL 11,190,218 11,190,218

SCHEDULE NO 7: INVESTMENTS

CPF INVESTMENT 554,215,210 510,728,303

Total 554,215,210 510,728,303

50 ADA Annual Report 2015-16

Schedules Forming part of the Balance Sheet as at March 31, 2016 Amount in Rs.

Particulars Current Year Previous Year

SCHEDULE NO 8: CURRENT ASSETS, LOANS & ADVANCES Current Assets:

OTHER DEPOSITS 8,164,863 8,163,863

TAX DEDUCTED AT SOURCE 449,608 8,614,471 330,144 8,494,007 ACCOUNTS RECEIVABLE - 820,615

Loans & Advances:

MISC. ADVANCE 839,167 -

MOTOR CAR LOAN 1,598,475 1,530,870

MOTOR CYCLE LOAN 248,765 252,272

PC LOAN 444,095 443,878

FESTIVAL ADVANCE 49,650 63,525

RENT ADVANCE 2,907,348 6,087,500 3,056,506 5,347,051 TOTAL 14,701,971 14,661,673

SCHEDULE NO 9: CASH AND BANK BALANCES

CASH ON HAND 78,278 85,810

STATE BANK OF INDIA, BANGALORE 87,744,428 47,102,038

STATE BANK OF MYSORE,BANGALORE 5,657,958 181,979

STATE BANK OF HYDERABAD, BLR (A/F) 68,396,298 2,181,777,086

STATE BANK OF HYDERABAD, BLR (ECS) 22,153,607 13,759,527

STATE BANK OF HYDERABAD, BLR (NAVY) 52,125,168 277,259,154

STATE BANK OF HYDERABAD, BLR (NP-MASS) 45,876,764 330,876,059

ICICI BANK LIMITED, BLR 2,451,430 2,202,955

STATE BANK OF INDIA, BLR (AERO INDIA 2015) - 27,299,527

STATE BANK OF INDIA, BLR (BIAS 2016) 8,974,225 -

SYNDICATE BANK, NEW DELHI 127,573 97,945

STATE BANK OF INDIA, HYDERABAD 40,451 76,730

SHORT TERM DEPOSIT WITH BANKS 744,650,410 687,283,380

STATE BANK OF HYDERABAD - BLR (DR. - 970,566 KOTA HARINARAYANA A/C) Total 1,038,276,590 3,568,972,756

51 Annual Report 2015-16 ADA

Income & Expenditure Account for the year ended March 31, 2016 Amount in Rs. Particulars Schedule Current Year Previous Year Income:

Other Income 10 5,34,12,208 4,97,26,124 Interest Earned (As per Contra) 11 20,33,60,344 40,80,87,485

Net Deficit Transferred to Project Management Expenditure of :

NAVY FSED PHASE 1 - 15% -- 20,04,54,882 18,93,31,962 LCA FSED PHASE 3 (Mk2) - 85% -- 1,13,59,11,000 1,07,28,81,117 Total 1,59,31,38,435 1,72,00,26,687 Expenditure:

Pay & Allowances 12 1,03,08,16,437 89,99,87,574 Administrative Expenses 13 28,78,10,581 34,94,72,722 Repairs & Maintenance 14 7,11,51,073 6,24,78,906 Interest Earned (As per Contra) 15 20,33,60,344 40,80,87,485 Total 1,59,31,38,435 1,72,00,26,687 Explanatory Notes 16

Accounting Policies and Explanatory Notes forming part of accounts annexed.

This is the Income & Expenditure Account referred to in our report of even date.

for ABS & CO. CHARTERED ACCOUNTANTS FRN 008203S

Sd/- Sd/- Sd/- H G ANAND M.S. KRISHNA MURTHY M A ANANDAN PARTNER Chief Finance Officer Offtg. Jt. Director (Finance) Membership No. 206226

Sd/- Sd/- CMDE. (RETD.) C.D. BALAJI K. RAVI KUMAR Secretary FA to DG-ADA

Place : Bangalore Date : 12.09.2016

52 ADA Annual Report 2015-16

Schedule forming part of the Income & Expenditure Account for the year ended March 31, 2016 Amount in Rs. Particulars Current Year Previous Year

SCHEDULE NO 10: OTHER INCOME LICENCE FEE 70,720 61,820 CONVEYANCE RECOVERY 4,900 17,750 CONTRIBUTORY HEALTH SERVICE SCHEME 3,183,586 2,922,062 INTEREST ON CPF INVESTMENTS 46,288,256 44,178,204 INTEREST ON LOANS AND ADVANCES 484,485 790,146 MISCELLANEOUS INCOME 3,380,261 1,756,142 Total 53,412,208 49,726,124 SCHEDULE NO 11: INTEREST EARNED (AS PER CONTRA) INTEREST ON SOFTWARE SUPPORT ACTIVITIES 57,367,030 58,772,298 INTEREST ON A/C DR. DS KOTHARI DRDO CHAIR - - INTEREST ON A/C DR. KOTA HARINARAYANA 51,933 66,150 INTEREST ON GRANTS-IN-AID:

LCA FSED PHASE - 2 - ICICI BANK LTD. 394,077 2,195,403 LCA FSED PHASE - 2 - STATE BANK OF HYDERABAD 82,310,374 226,495,380 NP-MASS - STATE BANK OF HYDERABAD 24,888,604 2,821,362 LCA FSED PHASE - 2 - STATE BANK OF INDIA NAL 8,608,801 - FSED NAVY PHASE - 1 - STATE BANK OF HYDERABAD 29,739,525 117,736,892 Total 203,360,344 408,087,485 SCHEDULE NO 12: PAY & ALLOWANCES SALARY 892,052,448 771,626,316 INTEREST SUBSIDY 1,241,848 1,043,207 TUTION FEE REIMBURSEMENT 4,719,110 4,912,781 ALLOWANCE - OVERTIME 1,011,212 2,200,646 WELFARE EXPENSES 11,705,199 9,173,864 MEDICAL REIMBURSEMENT 27,388,252 25,345,824 LEAVE TRAVEL CONCESSION 13,144,777 15,084,737 PENSION & LEAVE SALARY CONTRIBUTION 4,322,363 4,279,109 GRATUITY AND CPF CONTRIBUTION 48,072,784 41,388,547 INTEREST ON CPF 27,158,444 24,932,543 Total 1,030,816,437 899,987,574

53 Annual Report 2015-16 ADA

Schedule forming part of the Income & Expenditure Account for the year ended March 31, 2016 Amount in Rs. Particulars Current Year Previous Year

SCHEDULE NO 13: ADMINISTRATIVE EXPENSES TRAVELLING ALLOWANCES: ON TRANSFER 226,987 975,033 ON TOUR - INDIA 49,424,198 70,174,940 ON TOUR - ABROAD 25,135,645 36,077,858 TO OUTSIDERS 1,291,000 1,548,902 HONORARIUM 868,800 602,478 PROFESSIONAL CHARGES 38,148,491 45,422,449 ADVERTISEMENT & PUBLICITY 1,703,281 22,770,214 SEMINARS AND CONFERENCE FEES 1,643,714 3,157,374 RENT - OFFICE AND RESIDENTIAL ACCOMODATION 2,625,236 3,082,710 TELEPHONE & TELEX 13,790,544 11,705,747 POSTAGE & TELEGRAM 203,980 219,772 PRINTING & STATIONERY 12,738,291 12,421,439 BOOKS & PERIODICALS 5,340,509 1,419,139 WAGES TO CONTRACT EMPLOYEES 27,074,788 22,396,047 COURTESY EXPENSES 12,087,128 12,068,564 SECURITY CHARGES 18,236,312 17,040,826 WATER & ELECTRICITY 37,050,317 33,944,847 AUDIT FEES 119,618 117,978 MISCELLANEOUS EXPENSES 209,976 1,365,333 VEHICLE HIRE CHARGES 37,902,710 49,789,506 VEHICLE FUEL CHARGES 1,989,055 3,171,566 Total 287,810,581 349,472,722 SCHEDULE NO 14: REPAIRS & MAINTENANCE: BUILDING MAINTENANCE 45,697,236 48,281,671 COMPUTER MAINTENANCE 21,249,521 11,587,728 VEHICLE MAINTENANCE 1,176,173 1,596,906 OFFICE EQUIPMENT MAINTENANCE 3,028,143 1,012,601 Total 71,151,073 62,478,906

54 ADA Annual Report 2015-16

Schedule forming part of the Income & Expenditure Account for the year ended March 31, 2016 Amount in Rs. Particulars Current Year Previous Year

SCHEDULE NO 15: INTEREST EARNED (AS PER CONTRA) INTEREST ON SOFTWARE SUPPORT ACTIVITIES 57,367,030 58,772,298 INTEREST ON A/C DR. DS KOTHARI DRDO CHAIR - - INTEREST ON A/C DR. KOTA HARINARAYANA 51,933 66,150 INTEREST ON GRANTS-IN-AID:

LCA FSED PHASE - 2 - ICICI BANK LTD. 394,077 2,195,403 LCA FSED PHASE - 2 - STATE BANK OF HYDERABAD 82,310,374 226,495,380 NP-MASS - STATE BANK OF HYDERABAD 24,888,604 2,821,362

LCA FSED PHASE - 2 - STATE BANK OF INDIA NAL 8,608,801 - FSED NAVY PHASE - 1 - STATE BANK OF HYDERABAD 29,739,525 117,736,892 Total 203,360,344 408,087,485

SCHEDULE NO.16:EXPLANATORY NOTES

1. Government of India, Ministry of Defence vide their letter No.DARO/01/27524/M/I/ 2255/D(R&D) dated July 11, 2005 have conveyed post-facto sanction for closure of FSED Phase-I of LCA with effect from March 31, 2004 within the sanctioned cost of Rs.2188 crore. The Research & Development expenditure of the programme relating to FSED Phase - I is continued to be shown under Assets at Rs.2188 crore with corresponding amount as Liability under 'Grants-in-aid'.

2. Other Closed Projects are: IFCAP, Kaveri Poloymer Composites, National Program on Smart Material (NPSM), DISMAS, High Performance Computing Facility, MIG 21 BIS (UPG) Training/Maintenance, Simulator and Tactical Mission System (TMS) are continued to be shown under assets with corresponding amount as liability.

3. The approved cost estimates for each project includes certain amount for the establishment of the capital/test facilities needed therefor. The Research & Development expenditure on project also includes the cost of such infrastructure located at various work centres. Physical verification of assets is being carried out by the respective work centres in accordance with their internal procedures.

4. The Revenue generated and interest earned on Software Support Activities is shown as a separate item in the Balance Sheet under liabilities based on the inprinciple approval given by President General Body, ADA/Raksha Mantri for operating the Pension Fund pending finalization / approval of the operational aspects by the Governing Body, ADA.

55 Annual Report 2015-16 ADA

5. The Society is exempted from Income Tax as per CBDT Notification No.11535 dt. 19.10.2000 issued under the provisions of the Section 35 (i) (ii) as it is a society formed for scientific research. The exemptions granted earlier expired on 31.03.2003 and renewed by CBDT vide Notification No.08/2009 dated 07.01.2009 with effect from 01.04.2006 onwards. As on 31.03.2016 a sum of Rs.4,49,608/- is shown as an asset in the Balance Sheet as this is refundable from the Income Tax Department [Rs.54,167/- for 2013-14, Rs.2,38,604/- for 2014-15 & Rs.1,76,937/- for 2015-16]. Rs.20,100/- refund received from IT Department towards Assessment Year 2014 along with interest of Rs.2,300/-.

6. DRDO vide their letter No.ERIP/ER/1008001/M/01/1276 dated December 13,2010 have accorded a Grant of Rs.83,06.400/- to ADA for instituting Dr.DS Kothari Chair for a period of 3 years. Overall Grants received upto 2014-15 is Rs.77,64,772/-, Rs.1,92,669/- interest earned on grants and a sum of Rs.77,24,755/- has been utilised. Rs.1,98,093/- has been refunded to Government. The unspent balance of Rs.34,593/- (Interest earned) has been reflected under Current Liabilities and will be refunded during 2016-17.

7. During the year 2011-2012, NAL has transferred a sum of Rs.8,16,301/- vide cheque No.979895 dated 31.05.2011 as Research Grant to Dr. Kota Harinarayana for pursuing research in the area of Multi- disciplinary Design Optimisation (MDO) which was originally released to NAL by India Science Lab of General Motors, Bangalore and subsequently transferred to ADA. A sum of Rs.8,16,301/- (Excluding Interest) has been refunded to Dr.Kota Harinarayana and Interest earned on Rs.8,16,301/- is retained and decision yet to take for utilisation. Rs.2,06,198/- has been reflected under the head Interest received on Grant in aid.

8. It is stated by CAG Auditors that a transit loss of the stores valuing Rs.10.63 crs (Additional Shipset of Actutators) had occurred during the year 2008 at 'ADE' under work package relating to LCA Project (09/550). The matter was taken up by ADE and it is reported by ADE as under,

a) DRDO Hqrs and CBI conducted inquiries on the missing consignment. b) Recommendations of the enquiry committee have been forwarded to RM and still in process in MOD.

c) While the "missing of consignment" is construed as "loss of stores in transit", a statement of case for "Loss" could be initiated for approval of CFA. However, final enquiry results are still awaited. On receipt of the same, the expenditure would be taken as "Loss" or otherwise. (Ref: ADE letter No.ADE/12608/FIN CORRES/LCA-FCS/1 dated 13.07.2016)

9. DRDO vide their letter No.ERIP/ER/0706100/M/01/1515/D(R&D) dated 30th May, 2012 for C r e a t i o n o f D r . R a j a R a m a n n a D R D O D i s t i n g u i s h e d F e l l o w s h i p s a n d l e t t e r No.DOP/05/50104/ARU/M/01/2419(i)/D(R&D) dated 4th Sept. 2012 for Appointment of Dr. AR Upadya as Dr. Raja Ramanna DRDO Distinguished Fellow for a period of 3 years. Overall Grants received upto 2015-16 is Rs.30,00,000/- (Rs.12,00,000/- during 2013-14 and Rs.18,00,000/- during 2015-16) and a sum of Rs.27,18,577/- has been utilised. The unspent balance of Rs.2,81,423/- has been reflected under the head Current Liabilities.

56 ADA Annual Report 2015-16

10. During 2014-15, a sum of Rs.20,58,00,000/- drawn from DRDO for participation of DRDO-ADA in Aero India 2015 Exhibition and Rs.4,62,790/- towards interest credited by SBI NAL Branch, Bangalore. During 2015-16 a sum of Rs.40,00,000/- has been refunded to DRDO vide letter dated 28.05.2015. The net amount received and expenditure incurred for Aero India 2015 is Rs.20,22,62,790/-. Separate books of account have been maintained by DRDO-ADA Exhibition Organising Committee for this purpose. The net of receipts and payments incurred during the year have been routed through Receipts & Payments Account of ADA based on the accounts certified by DRDO-ADA Exhibition Organising Committee.

11. During January 2016, Rs.19,98,00,000/- has been allotted to ADA for showcasing DRDO /ADA products in "Bahrain International Air Show (BIAS)" vide letter No.DRDO/DBF&A/BE/820269 /M/06 dated 05.01.2016. Out of Rs.1,50,00,000/- transferred to BIAS 2016 Exhibition Organising Committee. The Expenditure incurred towards BIAS 2016 is Rs.8,84,35,589.50 (Expenditure incurred by ADA is Rs.8,24,09,815/- and Expenditure incurred by BIAS 2016 Exhibition Organising Committee is Rs.60,25,775/-) and unspent balance of available is Rs.11,13,64,410.50 (Rs.10,23,90,185.50 available with ADA and Rs.89,74,225/- available with BIAS 2016 Exhibition Organising Committee. The net of receipts and payments incurred during the year have been routed through Receipts & Payments Account of ADA based on the accounts certified by BIAS 2016 Exhibition Organising Committee. Balance amount shown under liabilities side of the Balance Sheet.

12. During March 2016, Rs.1,23,40,000/- has been allotted to ADA for participating in "DEFEXPO-2016" at Goa vide letter No.DRDO/DBF&A/BE/82026/M/06 dated 16.03.2016. Expenditure incurred is Rs.29,04,755/- and unspent balance of Rs.94,35,245/- available with ADA shown under liabilities side of the Balance Sheet.

for ABS & CO. CHARTERED ACCOUNTANTS FRN 008203S

H G ANAND M.S. KRISHNA MURTHY M A ANANDAN PARTNER Chief Finance Officer Offtg. Jt. Director (Finance) Membership No. 206226

CMDE. (RETD.) C.D. BALAJI K. RAVI KUMAR Secretary FA to DG-ADA

Place : Bangalore Date : 12.09.2016

57 Annual Report 2015-16 ADA

Receipts & Payments for the year ended March 31, 2016 Amount in Rs. Receipts Current Year Previous Year

OPENING BALANCES: CURRENT ACCOUNT IN: STATE BANK OF INDIA, NAL BRANCH 47,102,038 50,962,599 STATE BANK OF MYSORE, CITY BRANCH 181,979 104,224,927 STATE BANK OF HYDERABAD, LCA MAIN 2,181,777,086 3,437,658,177 HAL BRANCH STATE BANK OF HYDERABAD , ECS HAL BRANCH 13,759,527 12,150,807 STATE BANK OF HYDERABAD LCA NAVY 277,259,154 1,766,193,858 HAL BRANCH STATE BANK OF HYDERABAD -NPSM HAL BRANCH 330,876,059 48,274,332 ICICI BANK LTD., INDIRANAGAR BRANCH 2,202,955 118,644,239 SYNDICATE BANK - NEW DELHI 97,945 38,472 STATE BANK OF HYDERABAD-HYD 76,730 24,938 SHORT TERM DEPOSIT WITH BANKS 687,283,380 628,511,082 STATE BANK OF INDIA (AERO INDIA 2015) 27,299,527 9,231,444 SBH-BLR DR. DS KOTHARI DRDO CHAIR - 1,260,657 ADA - A/C DR. KOTA HARINARAYANA 970,566 904,416 CASH ON HAND 85,810 81,423 3,568,972,756 6,178,161,370 GRANTS-IN-AID:

LCA FSED PHASE - 2 (A/F) 1,360,000,000 3,200,000,000 LCA FSED PHASE - 3 1,750,000,000 2,100,000,000 FSED NAVY PHASE - 1 600,000,000 1,500,000,000 FSED NAVY PHASE 2 650,000,000 1,500,000,000 NP - MASS - 404,300,000 ADV. MEDIUM COMBAT A/C - AMCA 273,700,000 200,000,000 TECH. DEV. TO DEVELOP INDG. TECH. 200,000,000 100,000,000 4,833,700,000 9,004,300,000

58 ADA Annual Report 2015-16

Receipts & Payments for the year ended March 31, 2016

Amount in Rs. Payments Current Year Previous Year

PAY & ALLOWANCES 1,030,816,437 899,987,574 ADMINISTRATIVE EXPENDITURE 287,810,581 349,472,722 REPAIRS & MAINTENANCE 71,151,073 62,478,906 1,389,778,091 1,311,939,202 LCA AIRFORCE FSED PHASE 2:

INFRASTRUCTURE 29,827,520 162,757,566 AIRCRAFT DESIGN & INTEGRATION 502,135,395 433,688,348 PROTOTYPE - TOOL FABRICATION 10,943,011 16,223,523 PROTOTYPE - CFC COMPONENTS 40,390,398 63,018,373 PROTOTYPE - AIRCRAFT MATERIAL 72,813,009 32,357,195 PROTOTYPE - AIRCRAFT FABRICATION 122,451,220 161,897,035 GENERAL SYSTEMS 235,106,857 150,720,081 FLIGHT CONTROL SYSTEM 484,594,216 150,500,975 AVIONICS - COCKPIT DISPLAY & CONTROL PANEL 80,486,053 83,407,826 AVIONICS - RING LASER GYRO 9,162,366 36,726,994 AVIONICS - MULTI MODE RADAR 63,777,437 (25,899,718) AVIONICS - COM. EQUIPMENT 238,615 36,286,894 AVIONICS - ELECTRICAL SYSTEM 5,927,452 8,491,881 AVIONICS - OTHER ITEMS 86,849,034 6,670,450 GROUND TESTING 94,855,245 76,283,047 FLIGHT TESTING 276,776,802 1,597,305,206 TRAINING CONSUTANCY & TECH. ASSISTANCE 44,884,226 9,187,861 TECHNOLOGY DEVELOPMENT - DESIGN ANALYSIS 67,472,409 43,379,023 TECHNOLOGY DEVELO. - COMPOSITE MATERIALS 24,449,483 9,763,861 TECHNOLOGY DEVELOPMENT - DESIGN ANALYSIS 977,734 35,955 GE ENGINE 7,072,973 15,866,453 PRODUCT SUPPORT 29,079,442 18,681,268 ENGG. CHANGE ORDER 91,638,322 63,922,804 HALs PROFIT 67,086,230 66,259,253 LSP ACTIVITIES:

ADDL. SCOPE OF WORK 417,514,522 494,914,364 AIRCRAFT MATERIAL 612,329 -

59 Annual Report 2015-16 ADA

Receipts & Payments for the year ended March 31, 2016

Amount in Rs. Receipts Current Year Previous Year DEBTS & DEPOSITS:

CONTRIBUTORY PROVIDENT FUND 34,322,635 50,318,443 AERO INDIA 2015 - 212,979,915 DR. RAJARAMANNA 1,800,000 - BIAS 2016 199,800,000 - DEFEXPO 2016 12,340,000 - 248,262,635 263,491,027 RECOVERIES & REMITTANCES: 230,626 - OTHER RECEIPTS:

LICENCE FEE 70,720 61,820 CONVEYANCE RECOVERY 4,900 17,750 C H S S 3,183,586 2,922,062 INTEREST ON CPF DEPOSITS 46,288,256 44,178,204 INTEREST ON LOANS & ADVANCES 484,485 790,146 MISCELLANEOUS INCOME 3,380,261 1,756,142 INTEREST ON AERO INDIA 2013 - 316,735 INTEREST ON AERO INDIA 2015 461,037 1,753 53,873,245 50,044,612 INTEREST ON GRANTS-IN-AID :

LCA - ICICI BANK LTD. 394,077 2,195,403 LCA - SBH 82,310,374 226,495,380 NP - MASS - SBH 24,888,604 2,821,362 NAVY - SBH 29,739,525 117,736,892 LCA - SBI NAL 8,608,801 - 145,941,381 349,249,037 INTEREST ON SOFTWARE SUPPORT ACTIVITIES 57,367,030 58,772,298 INTEREST ON DR. KOTA HARINARAYA 51,933 66,150 TAX DEDUCTED AT SOURCE (REFUND OF IT) 20,100 - SUNDRY CREDITORS 74,491 - OVERHEAD NP - MASS 58,500,000 - ACCOUNTS RECEIVABLE 820,615 - TOTAL 8,967,814,812 15,904,084,494

60 ADA Annual Report 2015-16

Receipts & Payments for the year ended March 31, 2016

Amount in Rs. Payments Current Year Previous Year

GENERAL SYSTEMS 4,594,304 1 FLIGHT CONTROL SYSTEM 22,259,775 5,245,183 AVIONICS DISPLAY 378,380 628,711 AVIONICS - MULTI MODE RADAR 22,593,791 (50,936,900) FLIGHT TESTING (665,334) (1,306,943) LRU FLOATS 42,340,252 86,019,593 2,958,623,468 3,752,096,162

LCA FSED PHASE - 3 (MK II) INFRASTRUCTURE 198,243,030 90,995,208 AIRCRAFT DESIGH & INTEGRATION 39,894,828 209,762,961 AIRCRAFT TOOLING, MTRL & FABRICATION (1,502,020) 4,075,718 PROTOTYPE - AIRCRAFT MATERIAL 24,052,504 (30,779,346) PROTOTYPE - AIRCRAFT FABRICATION 11,988,267 4,455,572 GENERAL SYSTEMS 803,636,629 2,185,138,530 FLIGHT CONTROL SYSTEMS 51,463,456 30,098,562 AVIONICS - COCKPIT DISPLAY & CONTROL PANEL 8,389,611 2,648,299 AVIONICS - MULTI MODE RADAR 9,378,982 52,256,288 AVIONICS - ELECTRICAL SYSTEM 7,887,528 - GROUND TESTING 27,938,681 28,804,875 FLIGHT TESTING - 378,409 TECH. DEVELOPMENT 5,989,517 2,344,012 PRODUCT SUPPORT 371,964 - HALs PROFIT 2,334,475 17,676,409 1,190,067,452 2,597,855,497

61 Annual Report 2015-16 ADA

Receipts & Payments for the year ended March 31, 2016

Amount in Rs. Receipts Current Year Previous Year

TOTAL 8,967,814,812 15,904,084,494

62 ADA Annual Report 2015-16

Receipts & Payments for the year ended March 31, 2016

Amount in Rs. Payments Current Year Previous Year

FSED NAVY PHASE - 1 INFRASTRUCTURE 15,010,647 25,247,404 AIRCRAFT DESIGN & INTEGRATION 418,423,938 350,552,162 TOOLING 6,257,990 6,527,146 PROTOTYPE - AIRCRAFT MATERIAL 99,451,077 100,053,195 PROTOTYPE - AIRCRAFT FABRICATION 211,107,409 334,612,784 GENERAL SYSTEMS 118,754,607 84,010,037 FLIGHT CONTROL SYSTEMS 31,931,771 30,588,154 AVIONICS - COCKPIT DISPLAY & CP 20,329,983 14,667,308 AVIONICS - MULTIMODE RADAR 4,874,405 (19,194,471) AVIONICS - COMMUNICATION EQUIPMENT 1,567 (100,000) AVIONICS - ELECTRICAL SYSTEM 4,237,518 13,556 AVIONICS - OTHER ITEMS 6,304,403 71,492 GROUND TESTING 48,192,532 273,225,571 FLIGHT TESTING 52,002,202 12,037,765 TRAINING, CONSULTANCY & TECH. ASSISTANCE - 2,232,743 TECHNOLOGY DEV - DESIGN ANALYSIS 5,872,970 - GE ENGINE 30,003,950 49,724,373 HALs PROFIT 64,532,815 66,289,234 1,137,289,784 1,330,558,453

63 Annual Report 2015-16 ADA

Receipts & Payments for the year ended March 31, 2016 Amount in Rs. Receipts Current Year Previous Year

TOTAL 8,967,814,812 15,904,084,494

64 ADA Annual Report 2015-16

Receipts & Payments for the year ended March 31, 2016

Amount in Rs. Payments Current Year Previous Year

FSED NAVY PHASE - 2

INFRASTRUCTURE 24,665,798 78,727,864 AIRCRAFT DESIGH & INTEGRATION 102,324,216 32,461,671 AIRCRAFT MATERIAL - 2,146,731 GENERAL SYSTEMS 8,435,849 2,098,033 FLIGHT CONTROL SYSTEMS 19,776,012 12,688,828 AVIONICS - MULTIMODE RADAR 9,131,746 51,903,176 GROUND TESTING 254,559,755 222,927,792 FLIGHT TESTING 2,447,954 395,988 TRAINING, CONSULTANCY & TECH. ASSISTANCE 314,765,328 (294,745,427) TECH DEV. - DESIGN ANALYSIS 12,007,389 - GE ENGINE 368,737,523 858,636,148 HALs PROFIT 10,010,154 6,978,631 1,126,861,724 974,219,435 TECH. DEVLPT. TO DEVELOP INDG. TECHNOLOGIES AVIONICS & ELECTRICAL SYSTEM 21,171,893 5,081,937 GENERAL SYSTEM 90,166,708 161,213,771 AIRFRAME 43,856,852 17,539,609 INTEGRATED FLIGHT CONTROL SYSTEM 50,101,647 20,919,432 AERODYNAMICS 4,601,751 657,540 PROTOVEHICLES & MNUFACTURING 325,572 2,693,427 ADVANCED PROJECTS 14,268,744 8,483,518 FLIGHT TESTING 990,622 - 225,483,789 216,589,234 ADV. MEDIUM COMBAT AIRCRAFT - AMCA 137,237,921 162,621,355 INDIAN UNMANNED STRIKE AIR VEHICLE 2,042,473 - NP - MASS 113,480,383 129,999,908 FIN FORMING MACHINE 156,823 - REPUBLIC DAY PARADE (Including Refund to Govt.) - 4,705,020 AR & DB 38,246 12,655

65 Annual Report 2015-16 ADA

Receipts & Payments for the year ended March 31, 2016

Amount in Rs. Receipts Current Year Previous Year

TOTAL 8,967,814,812 15,904,084,494

66 ADA Annual Report 2015-16

Receipts & Payments for the year ended March 31, 2016

Amount in Rs. Payments Current Year Previous Year

REVIEW COMMITTEE (Including Refund to Govt.) - 306,320 DR. RAJA RAMANNA 1,518,577 75,702 DR. DS KOTHARI CHAIR AT ADA - 766,452 INT. TRANSFERRED TO DR. DS KOTHARI CHAIR AT ADA - 315,671 DR. KOTAHARINARAYANA - RESEARCH GRANTS 816,301 - ADVANCE TO WORKCENTRES 3,447,826,887 4,783,385,790 LESS: EXPENDITURE 3,756,761,002 4,765,951,404 (308,934,115) 17,434,386 AERO INDIA 2015 [Rs.4000000/- refunded to Govt.] 27,760,564 185,682,141 ADVANCE TO SUPPLIERS (206,900,983) 1,535,819,355 BIAS 2016 88,435,590 - DEFEXPO 2016 2,904,755 - REMITANCES - 595,822 LOANS & ADVANCES (OTHER ADVANCES) 740,449 1,353,061 PF ADVANCE (1,485,680) 975,442 TAX DEDUCTED AT SOURCE 139,564 238,604 CPF INVESTMENTS 43,486,907 100,000,000 KEB DEPOSITS 1,000 - SECURITY DEPOSITS - 908,000 ACCOUNTS RECEIVABLE - 820,615 AERO INDIA 2013 [Rs.8615058/- refunded to Govt.] - 9,548,179 CLOSING BALANCES :

CURRENT ACCOUNT IN:

STATE BANK OF INDIA, NAL BRANCH 87,744,428 47,102,038 STATE BANK OF MYSORE, CITY BRANCH 5,657,958 181,979 STATE BANK OF HYDERABAD, LCA MAIN HAL 68,396,298 2,181,777,086 BRANCH STATE BANK OF HYDERABAD , ECS HAL BRANCH 22,153,607 13,759,527 STATE BANK OF HYDERABAD, LCA NAVY HAL 52,125,168 277,259,154 BRANCH

67 Annual Report 2015-16 ADA

Receipts & Payments for the year ended March 31, 2016

Amount in Rs. Receipts Current Year Previous Year

TOTAL 8,967,814,812 15,904,084,494

68 ADA Annual Report 2015-16

Receipts & Payments for the year ended March 31, 2016

Amount in Rs. Payments Current Year Previous Year

STATE BANK OF HYDERABAD -NPSM HAL 45,876,764 330,876,059 BRANCH ICICI BANK LTD., INDIRANAGAR BRANCH 2,451,430 2,202,955 SYNDICATE BANK, NEW DELHI 127,573 97,945 STATE BANK OF INDIA, HYD 40,451 76,730 STATE BANK OF INDIA, BLR (AERO INDIA 2015) - 27,299,527 SHORT TERM DEPOSIT WITH BANKS 744,650,410 687,283,380 STATE BANK OF INDIA, BLR (BIAS 2016) 8,974,225 - SBH - DR. KOTA HARINARAYANA A/C - 970,566 CASH ON HAND 78,278 85,810 1,038,276,590 3,568,972,756 TOTAL 8,967,819,672 15,904,409,428

Accounting Policies and Notes on accounts forming part of accounts annexed.

This is the Receipts & Payments Account referred to in our report of even date.

for ABS & CO. CHARTERED ACCOUNTANTS FRN 008203S

Sd/- Sd/- Sd/- H G ANAND M.S. KRISHNA MURTHY M A ANANDAN PARTNER Chief Finance Officer Offtg. Jt. Director (Finance) Membership No. 206226

Sd/- Sd/- CMDE. (RETD.) C.D. BALAJI K. RAVI KUMAR Secretary FA to DG-ADA

Place : Bangalore Date : 12.09.2016

69 Annual Report 2015-16 ADA

Investments in LCA Airforce FSED Phase 2 upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

54.44.00.00 INFRASTRUCTURE

OFFICE BUILDINGS 259,593,352 257,931,912 MAIN FRAME H/W UPDATES 118,882,668 115,452,212 MAIN FRAME S/W UPDATES 74,210,744 71,117,685 PCs,H/W,S/W,PRINTERS,PLOTTERS ETC., 160,054,194 154,654,067 WORK STATION H/W, S/W 267,027,054 253,640,145 COMPUTER MAINTENANCE 2,581,932 2,581,932 PARALLEL COMPUTERS 25,965,911 25,965,911 OFFICE EQUIPMENT - PURCHASES 23,627,417 23,353,117 OFFICE EQUIPMENT - MAINTENANCE - 2,940 FURNITURE & FIXTURES 28,329,833 26,834,560 MOTOR VEHICLES 4,696,185 4,696,185 PLANT & MACHINERY - NC SHOP 87,301,131 86,801,093 PLANT & MACHINERY - MACHINE SHOP 1,199,387 1,199,387 PLANT & MACHINERY - COMPOSITE SHOP 24,781,884 24,781,884 PLANT & MACHINERY - TOOL ROOM 20,634 20,634 ASSEMBLY SHOP 1,213,407 1,213,407 PLANT ENGINEERING 4,513,996 4,501,676 PUBLICATION, REPROGRAPHY & ARCHIVES 17,207 17,207 INSTRUMENTS & EQUIP.-QUALITY CONTROL 73,019 73,019 COMMUNICATION FACILITIES 19,340,199 19,271,682 GROUND TEST FACILITIES 27,392,321 27,392,321 OFFICE EQUIPT. CANTEEN, SECURITY & COMM-HAL 2,196,329 2,196,329 DESIGN EFFORT 277,393 319,963 PCs, & WORKSTATION - HAL ARDC 79,228,022 79,228,022 PLOTTERS, PRINTERS & NETWORKING-HAL ARDC 6,080,140 6,080,140 OFFICE BUILDING - HAL ARDC 26,546,591 26,546,591 CONSUMABLES - 3,950 TRANSPARENCY COATING FACILITY 136,779,198 136,224,657 BALANCE STAGE PAYMENT WITH : CRE, LD 64,989 64,989 1,381,995,137 1,352,167,617

70 ADA Annual Report 2015-16

Investments in LCA Airforce FSED Phase 2 upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

54.45.00.00 AIRCRAFT DESIGN & INTEGRATION

VERIFICATION & VALIDATION OF S/W & TOOLS 87,048,315 77,970,320 SYSTEMS SIMULATOR 40,212,322 31,383,366 CEF TRAINER 237,383,291 219,004,612 ENGINEERING COST - ADA 118,290,580 108,478,467 BALANCE STAGE PAYMENT WITH : CEMILAC 160,319 160,319 ENGINEERING COST - HAL ARDC 3,477,316,397 3,073,693,487 A/C DESIGN - CON. OF DESIGN DWG TO PRO DWG 5,555,309 5,551,656 AVIONICS SOFTWARE UPDATE 136,379,188 108,230,082 BALANCE STAGE PAYMENT WITH : NAL (523,596) - WEAPON & SENSOR S/W DEVELOPMENT 121,773,190 107,424,556 CONTROL LAW DESIGN - NAL 63,783,637 53,870,288 BALANCE STAGE PAYMENT WITH : NAL (5,880,924) 1,577,491 CONTROL LAW - ADA 4,846,930 4,846,930 4,286,344,958 3,792,191,574 54.47.00.00 PROTOTYPE - TOOL FABRICATION

TOOLING 274,746,570 263,803,559 TOOLING ICY GAGES 384,118 384,118 275,130,688 264,187,677 54.50.00.00 PROTOTYPE - CFC COMPONENTS

CFC WING 774,601,752 734,211,354 BALANCE STAGE PAYMENT WITH : NAL (1,229,694) (1,229,694) C0-CURED WING DEVELOPMENT 55,803,139 55,803,139 829,175,197 788,784,799 54.51.00.00 PROTOTYPE - AIRCRAFT MATERIAL

RAW MATERIAL/CONSUMABLES 101,250,485 101,235,485 BOUGHT OUT ITEMS 148,383,175 140,900,842 RADOME 47,677,023 35,657,826 BALANCE STAGE PAYMENT WITH : DRDL - 1,184,039 HAL O/H DIV (2,782,355) 3,513,681

71 Annual Report 2015-16 ADA

Investments in LCA Airforce FSED Phase 2 upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

RUDDER 21,152,603 20,465,603 BALANCE STAGE PAYMENT WITH : NAL (87,000) - FIN 50,119,759 45,832,287 BALANCE STAGE PAYMENT WITH : NAL - 1,747,540 CANOPY DEVELOPMENT FOR TRAINER 613,512 613,512 WIND SHEILD DEVELOPMENT 17,314,319 10,422,547 FUSELAGE METALLIC MATERIALS 142,232,018 142,232,018 FUSELAGE COMPOSITES - ADA 225,404,203 225,404,203 STANDARD PARTS 155,846,311 114,416,076 NAL COMPONENT SUPPLY 105,339,560 105,339,560 1,012,463,613 948,965,219 54.52.00.00 PROTOTYPE - A/C FABRICATION

FABRICATION, ASSEMBLY & EQUIPPING 1,928,287,695 1,808,493,079 LRUs FOR COMPOSITE DROP TANKS - ADA 6,788,134 6,788,134 COMPOSITE DROP TANKS 113,801,343 112,176,849 BALANCE STAGE PAYMENT WITH : ASL 20,000 20,000 TOT FOR COMPOSITE MANUFACTURE 14,822,750 14,822,750 AIRCRAFT FABRICATION - ADA 47,717,400 46,685,290

2,111,437,322 1,988,986,102 54.53.00.00 GENERAL SYSTEM

GE ENGINE 300,392,534 227,891,781 JET FUEL STARTER 129,911,079 128,144,181 BALANCE STAGE PAYMENT WITH : HAL EDB (1,882,400) (7,882,400) AMAGB 87,795,467 87,592,467 SENSORS & SWITCHES 29,068,530 29,068,530 BALANCE STAGE PAYMENT WITH : CSIO - 181,990 HAL-LD (1,366,100) (1,366,100) CONTROLLERS FOR EEMS,ECS,DFM- 151,657,418 105,093,169 EU & DH-EU DFM SENSORS 14,857,783 14,857,783 GENERAL SYSTEMS - LRUs 371,271,845 364,791,845

72 ADA Annual Report 2015-16

Investments in LCA Airforce FSED Phase 2 upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

HYDRAULIC SYSTEM - LD DEVELOPED ITEMS 76,697,532 55,997,034 BALANCE STAGE PAYMENT WITH : HAL LD (3,605,090) (3,605,090) HYDRAULIC SYSTEM - INDIGENOUS ITEMS 489,727,678 480,194,402 BALANCE STAGE PAYMENT WITH : HAL LD 968,870 3,393,838 : GTTC - 2,625,677 : CMTI - (924,635) HYDRAULIC FILTERS 28,464,246 24,482,984 BALANCE STAGE PAYMENT WITH : CTTC (43,824) (43,824) : DEBEL 517,186 3,000,000 ACTIVE FUEL PROPORTIONER 16,209,634 13,173,547 AIRCREW PROTECTIVE CLOTH 34,519,852 34,419,099 DESIGN & DEVELOPMENT OF ECS 69,190,065 69,001,352 ENVIRNOMENT CONTROL SYSTEM 90,604,333 90,589,183 BALANCE STAGE PAYMENT WITH : HAL LD 4,984,850 - ECS INDIGENOUS ITEMS - ADA 4,957,219 4,957,219 BALANCE STAGE PAYMENT WITH : HAL LD (1,072,840) (1,072,840) OBOGS 6,565,157 6,565,157 UPLOCKS 17,155,698 12,417,362 UC DOOR JACKS 18,398,217 18,398,217 WHEEL & BRAKES ASSEMBLY 58,857,241 40,293,010 BALANCE STAGE PAYMENT WITH : DMRL 38,864 38,864 : HAL LD 572,980 - : GTTC 2,077,080 - CARBON HEAT PACKS 138,912,612 119,151,012 BALANCE STAGE PAYMENT WITH: ASL 354,800 20,101,512 BRAKE PARACHUTE 4,337,538 4,036,283 BALANCE STAGE PAYMENT WITH : ADRDE 5,695,447 5,996,702 ANTI SPIN PARACHUTE SYSTEM 103,570,447 103,452,857 BALANCE STAGE PAYMENT WITH : ADRDE 3,746,289 3,746,289 ASL - 2,695,516

73 Annual Report 2015-16 ADA

Investments in LCA Airforce FSED Phase 2 upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

SEAT & ACCESSORIES 229,367,910 204,619,179 MINIATURE DETONATING CORD 23,497,000 21,692,525 BALANCE STAGE PAYMENT WITH : ARDE 3,092,775 3,042,250 2,510,065,922 2,290,807,927 54.54.00.00 FLIGHT CONTROL SYSTEM

DFCC FABRICATION 576,312,030 171,312,030 LRUs & COMPONENT SHIPSET 677,228,265 641,550,357 BALANCE STAGE PAYMENT WITH : ADE 5,885,423 4,609,093 ACTUATORS FOR LEVCON 6,403,647 6,390,448 FCP & FTP 15,800,128 15,800,128 MAIN. & UPDATE OF FACILITIES AT ADE 118,784,786 117,401,799 BALANCE STAGE PAYMENT WITH : ADE - (179,172) NAL 2,151,843 2,151,843 FCS/STTEs 5,389,904 5,389,904 COCKPIT CONTROLS 7,191 7,191 SUPPORT FOR S/W DEVELOPMENT AT ADE 54,183,311 46,751,805 BALANCE STAGE PAYMENT WITH : ADE 3,294,103 4,388,908 PRIMARY ACTUATORS - VSSC 114,983,172 113,258,172 LES ACTUATOR 2,364,570 2,364,570 AIR BRAKE ACTUATOR 3,772,440 3,772,440 ELECTRO HYDRAULIC SERVO VALVES 7,380,804 7,380,804 AIR DATA TRANSDUCERS 24,929,848 24,820,778 DE-ICING CURRENT SENSOR UNIT 133,990 133,990 ACCELERMETER SENSOR ASSEMBLY (1,241,249) (1,241,249) AIR DATA SYSTEM 14,190,358 14,190,358 ACTUATOR TEST SET - ATS 2,969 2,969 OUTSOURCING OF IFCS ACTIVITIES 5,979,882 2,410,748 MAINTENANCE/MODs OF FCS LRUS 145,886,411 116,200,999 BALANCE STAGE PAYMENT WITH : ADE 342,388 7,439,457 1,784,166,214 1,306,308,370

74 ADA Annual Report 2015-16

Investments in LCA Airforce FSED Phase 2 upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

54.55.00.00 AVIONICS - COCKPIT DISPLAY & CONTROL PANEL HEAD UP DISPLAY 212,365,538 212,003,147 BALANCE STAGE PAYMENT WITH : CSIO (238,628) (238,628) MULTI FUNCTION DISPLAY - IMPORTED 224,947,843 213,746,852 DP, MC, CCU, VSU COMBINED UNITS & OSA 408,355,444 374,552,148 LCD DISPLAY SYSTEM AND UFCP 186,564,061 172,913,835 SIB, SSB, & PIB 270,682,182 256,727,588 COCKPIT LIGHTS 39,679,790 32,165,235 1,342,356,230 1,261,870,177 54.57.00.00 AVIONICS - RING LASER GYRO

RING LASER GYRO 146,389,852 137,227,486 146,389,852 137,227,486 54.59.00.00 AVIONICS - MULTIMODE RADAR

MULTIMODE RADAR 1,085,878,678 1,022,101,241 1,085,878,678 1,022,101,241 54.60.00.00 AVIONICS - EW SUITE DEVELOPMENT

EW SUITE DEVELOPMENT 175,517,535 175,517,535 175,517,535 175,517,535 54.61.00.00 AVIONICS - COMMUNICATION EQUPT

COMMUNICATION EQUIPMENT 157,121,141 156,882,526 BALANCE STAGE PAYMENT WITH: HAL-HYD - (15,037,020) 157,121,141 141,845,506 54.62.00.00 AVIONICS - ELECTRICAL SYSTEM

EXTERNAL LIGHTING 41,477,557 35,601,732 ELEC. POWER GENERATION & DISTR. SYSTEM 35,097,671 35,046,044 BALANCE STAGE PAYMENT WITH : HAL LD (60,447) (60,447) DISTRIBUTION BOXES 2,569,874 2,569,874 79,084,655 73,157,203

75 Annual Report 2015-16 ADA

Investments in LCA Airforce FSED Phase 2 upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

54.63.00.00 AVIONICS - OTHER ITEMS

MISSION PREPARATION & DATA RETRIVAL UNIT 24,796,222 22,980,789 CRASH DATA RECORDER 51,552,964 47,319,964 BALANCE STAGE PAYMENT WITH : HAL-MCSRDC - (500,000) ANTENNA 8,759,714 8,767,714 CENTRALISED WARNING SYSTEM 52,511,749 52,511,749 FLIR & IRST 415,089,953 414,940,141 HMD PROCUREMENT 510,192,979 452,968,711 COCKPIT COMMAND CONTROLLER & CIU 54,330,680 54,330,680 MOD. / MAINT OF AV LRUs 45,651,704 22,217,183 BALANCE STAGE PAYMENT WITH : BEL 3,111,094 4,185,676 1,165,997,059 1,079,722,607 54.64.00.00 GROUND TESTING

WIND TUNNEL TESTING - IN INDIA 208,595,967 202,882,854 BALANCE STAGE PAYMENT WITH : NAL 1,460,000 (2,553,210) : IIT KANPUR (421,200) - WIND TUNNEL TESTING - ABROAD 215,445,480 215,445,480 ECS 107,854,322 106,180,235 BALANCE STAGE PAYMENT WITH : GTRE 3,299,867 4,632,998 : NAL - (3,341,556) GE TEST BED 67,394,800 63,604,381 BALANCE STAGE PAYMENT WITH : GTRE 1,513,747 2,057,219 SYSTEM TEST RIGS (MAIN. & SPARES) 884,178 884,178 DAIR (ADE) 47,409,556 35,543,544 EMI/EMC FACILITY 51,655,851 51,148,117 LIGHTNING TEST FACILITY 33,802,066 29,654,565 BALANCE STAGE PAYMENT WITH : MS RAMAIAH 39,486 327,292 AVIONICS INTEGRATION - TEST EQUIPMENT 57,493,686 54,385,511 RADAR RIG 118,803,671 64,341,324

76 ADA Annual Report 2015-16

Investments in LCA Airforce FSED Phase 2 upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

IFCS INTEGRATION EQUIPMENTS AT HAL 28,475,213 28,473,580 AMAGB TEST RIG OPERATION & MNTCE 46,845,972 44,788,494 BALANCE STAGE PAYMENT WITH : CVRDE 859,818 2,917,296 BRAKE DYNAMO METER 10,933,778 10,880,322 SPARES FOR GRAPH & HIP FURNACE 3,562,409 2,885,369 BALANCE STAGE PAYMENT WITH : GTTC 1,489,964 - IRON BIRD AUGUMENTATION & MAINTENANCE 164,422,693 159,139,327 GROUND CHECKOUT SYSTEM 52,517,108 52,187,724 GCS MAINTENANCE 10,864,838 9,681,338 DAIR MAINTENANCE 7,567,342 7,567,342 HAL SHOP EFFORT 175,403,648 175,403,648 1,418,174,260 1,319,117,372 54.65.00.00 FLIGHT TESTING

TELEMETRY EQUIPMENT 196,393,040 185,735,169 FLIGHT TEST INTEGRATION RIG 144,476,675 137,242,666 PHOTOGRAPHY & VIDEO ANALYSIS 41,312,152 41,306,770 COMPUTING SYSTEM 56,074,035 53,606,419 AUGUMENTATION TO GROUND FACILITIES 393,686,794 391,167,064 SENSORS 138,484,270 138,484,270 SPARES & CONSUMABLES 215,023,938 208,149,705 FLIGHT TEST INSTRUMENTATION 672,524,650 576,776,546 FUEL & OIL FOR 3400 HRS OF FLIGHT 269,047,068 262,582,467 FLIGHT TEST EFFORTS 1,333,475,104 1,240,648,264 SPARES LRUs FOR FLIGHT TESTING 2,208,649,648 2,157,246,162 BALANCE STAGE PAYMENT WITH : HAL HYD - (37,152) : RCI 2,889,549 1,389,549 : HAL-BC (15,202,372) 10,431,000 HACK A/C - MODIFICATIONS TO AIRCRAFT 211,499,985 211,499,985 R73E, RVV-AE MISSILES,KH 31A BOMBS & ROCKETS 725,173,115 724,598,185 BALANCE STAGE PAYMENT WITH : ADE 55,573 34,427 6,593,563,224 6,340,861,496

77 Annual Report 2015-16 ADA

Investments in LCA Airforce FSED Phase 2 upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

54.66.00.00 TRAINING CONSULTANCY & TECH ASSISTANCE CONSULTANCY FOR DEV. OF CONTROL LAW 2,152,643 2,152,643 REAL TIME & INFLIGHT SIMULATOR 110,856,896 110,856,896 TRAINING & CONSULTANCY IN OTHER AREAS 1,441,359,202 1,441,235,326 CCOONNSSULMTTAANNCCYY IN WEAPON INTEGRATION 6,835,509 - FLIGHT TEST CONSULTANCY 46,767,742 8,842,901 1,607,971,992 1,563,087,766 54.68.00.00 TECHNOLOGY DEVELOPMENT - DESIGN ANALYSIS CFD CODES 68,386,510 61,689,556 BALANCE STAGE PAYMENT WITH : NAL 809,968 370,670 SIGNATURE STUDIES 34,982,785 33,599,897 BALANCE STAGE PAYMENT WITH : RCI, HYD 908,860 908,860 CAM-CAD-CAQ SOFTWARE 40,698,081 23,835,026 CAD & GRAPHICS 289,605,862 268,957,811 STRUCTURAL ANALYSIS CODES 88,268,056 73,678,266 BALANCE STAGE PAYMENT WITH : NAL 5,797,133 (991) DIGITAL/VIRTUAL PROTOTYPE 26,060,116 18,768,445 555,517,370 481,807,539 54.70.00.00 TECHNOLOGY DEVELOPMENT – COMPOSITE MATERIALS COMPOSITES - MATERIALS & PROCESSES 120,269,501 95,820,018 BALANCE STAGE PAYMENT WITH : NAL 184,757 (3,068,496) 120,454,258 92,751,522 54.71.00.00 TECHNOLOGY DEVT - AVIONICS DISPLAY COMMAN CONTROL SYSTEM 1,898,983 921,249 BALANCE STAGE PAYMENT WITH : ADE 10,260,000 - 12,158,983 921,249 54.74.00.00 GE ENGINE

GE ENGINE 3,078,625,188 3,071,552,215 3,078,625,188 3,071,552,215

78 ADA Annual Report 2015-16

Investments in LCA Airforce FSED Phase 2 upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

54.84.00.00 PRODUCT SUPPORT

GROUND SUPPORT EQUIPMENT 176,566,586 149,035,627 BALANCE STAGE PAYMENT WITH : NID 49,526 49,526 SPECIFIC SUPPORT EQUIPMENT - STTE 24,594,225 24,415,403 AUTOMATIC TEST EQUIPMENT COMPLEX-ATEC 370,222 370,222 FLIGHT SIMULATOR 42,458,906 42,182,156 MAINTENANCE SIMULATOR 72,498,604 71,405,693 BALANCE STAGE PAYMENT WITH : NID (219,574) (219,574) PUBLICATIONS 8,024,100 8,024,100 BALANCE STAGE PAYMENT WITH : ADE - (634,688) 324,342,595 294,628,465 54.86.00.00 ENGG. CHANGE ORDER

SIGNAL & DATA PROCESSOR 159,886,497 159,886,497 HIP FACILITY - CARBON BRAKE DISC 100,000,000 100,000,000 AC MASTER BOX 14,770,050 14,770,050 EXTERNAL LIGHTING 444,573 444,573 FLIGHT CONTROL SYSTEM 614,994,423 585,506,936 BALANCE STAGE PAYMENT WITH : ADE 17,732,576 20,089,130 HEEM - EU 220,039,003 170,915,412 FCG PROBES 38,323,960 38,323,960 CWS HARDWARE IMPROVEMENTS 29,918,812 29,918,812 HEAT EXCHANGERS 2,378,005 2,378,005 VIDEO DIGITAL RECORDER 171,066,521 171,066,521 JET FUEL STARTER 40,000,000 40,000,000 SEAT & ACCESSORIES 53,623,890 40,596,646 1,463,178,310 1,373,896,542 54.92.00.00 PROJECT MANAGEMENT EXPENDITURE 4,684,469,062 4,684,469,062 BALANCES WITH HAL-ARDC FOR FACILITY ESTABLISHMENT AND WORK PACKAGES (BREAK-

UP AS CERTIFIED BY THEM) INVENTORY HELD BY THEM 328,253,722 356,209,970

79 Annual Report 2015-16 ADA

Investments in LCA Airforce FSED Phase 2 upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

GOODS IN TRANSIT - 754,347 CAPITAL ADVANCE 9,264,091 16,315,366 CAPITAL WORK IN PROGRESS :

PLANT & MACHINERY UNDER ERECTION 7,018,516 7,246,674 BALANCE STAGE PAYMENT (544,365,104) (199,122,548) (199,828,775) 181,403,809 HALs PROFIT 756,482,315 689,396,085 64.00.00.00 LIMITED SERIES PRODUCTION

HAL BC

CAPITAL FACILITY 1,142,173,131 1,142,173,131 DEFERRED REVENUE EXPENDITURE 1,351,981,666 1,351,981,666 MANUFACTURING COST OF AIRCRAFT 10,482,183,538 10,482,183,538 ADDITIONAL SCOPE OF WORK 2,668,622,035 2,251,107,513 BALANCE STAGE PAYMENT WITH : HAL-BC (2,740,983,522) (2,740,652,000) 12,903,976,848 12,486,793,848 ADA SUPPLY ITEMS

CAPITAL & DRE 14,822,750 14,822,750 AIRCRAFT MATERIAL 5,003,357 4,391,028 AIRCRAFT FABRICATION 5,004,516 5,004,516 GENERAL SYSTEMS 288,198,903 283,604,599 FLIGHT CONTROL SYSTEM 1,204,458,054 1,182,198,279 BALANCE STAGE PAYMENT WITH : ADE 35,465,153 40,178,260 AVIONICS - COCKPIT DISPLAY 347,250,122 346,871,742 AVIONICS - RLG WITH INS-GPS 44,213,068 44,213,068 AVIONICS - MULTIMODE RADAR 630,369,720 607,775,929 AVIONICS- COMMUNICATION EQUIPMENT 81,810,287 81,810,287 AVIONICS - ELECTRICAL SYSTEM 5,616,000 5,616,000 ELECTRICAL SYSTEM 181,882,962 181,882,962 GROUND TESTING 11,290,243 11,290,243 FLIGHT TESTING 68,611,953 69,277,287

80 ADA Annual Report 2015-16

Investments in LCA Airforce FSED Phase 2 upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

LRU FLOATS 171,034,046 128,693,794 GE ENGINE 1,489,553,962 1,489,553,962 TOTAL 4,584,585,096 4,497,184,706 LIMITED SERIES PRODUCTION 17,488,561,944 16,983,978,554 TOTAL 56,246,794,927 53,701,712,716

for ABS & CO. CHARTERED ACCOUNTANTS FRN 008203S

Sd/- Sd/- Sd/- H G ANAND M.S. KRISHNA MURTHY M A ANANDAN PARTNER Chief Finance Officer Offtg. Jt. Director (Finance) Membership No. 206226

Sd/- Sd/- CMDE. (RETD.) C.D. BALAJI K. RAVI KUMAR Secretary FA to DG-ADA

Place : Bangalore Date : 12.09.2016

81 Annual Report 2015-16 ADA

Investments in LCA Airforce FSED Phase 3 upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

84.44.00.00 INFRASTRUCTURE

CIVIL WORKS - BUILDING 161,164,062 49,546,604 MAINFRAME SOFTWARE UPDATES 46,791,859 15,638,917 PCs,H/W,S/W,PRINTERS,PLOTTERS ETC., 41,153,975 22,069,806 WORKSTATION H/W S/W 24,375,516 20,899,410 OFFICE EQUIPMENT - PURCHASES 13,150 - FURNITURE & FIXTURES 5,226,329 2,041,746 PC & WIRJ STATUIB - HAL ARDC 66,799,402 37,566,919 COMMUNICATION FACILITIES 836,557 354,418 346,360,850 148,117,820 84.45.00 AIRCRAFT DESIGN & INTEGRATION

SIMULATION & SOFTWARE TOOLS 49,099,618 37,087,498 ENGINEERING COST - ADA 14,896,908 187,341,178 ENGINEERING COST - HAL 402,782,767 203,557,201 AVIONICS S/W UPDATES 1,612,238 510,826 468,391,531 428,496,703 84.47.00 AIRCRAFT TOOLING, MTRL&FABRICATION

TOOLING (SDC CONSULTANCY ETC.) 2,573,698 4,075,718 2,573,698 4,075,718.00 84.51.00 AIRCRAFT MATERIALS

MATERIAL COST 3 SETS (RUDDER, FIN, RADOME, 21,932,335 - MATERIAL ETC) REAR FUSELAGE DESIGN 17,775,778 15,655,609 BALANCE STAGE PAYMENT WITH : NAL (396,497) (591,509) 39,311,616 15,064,100 84.52.00 PROTOTYPE-AIRCRAFT FABRICATION

WEIGHT REDUCTION 16,257,394 4,986,501 BALANCE STAGE PAYMENT WITH : NAL (4,857,569) 5,818,525 : DMRL 14,270,000 - FAB ASSEMBLY & EQUIPPING 883,278 165,904 26,553,103 10,970,930

82 ADA Annual Report 2015-16

Investments in LCA Airforce FSED Phase 3 upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

84.53.00 GENERAL SYSTEMS

GE ENGINE 5,330,216,070 4,551,487,864 JET FUEL STARTER 80,698,409 80,722,909 BALANE STAGE PAYMENT WITH: HAL EDB (76,501,256) (76,501,256) AMAGB 1,146,000 1,146,000 CONTROLLER FOR COMBINED UNITS 2,200,674 2,200,674 THROTTLE QUADRANT ASSEMBLY (QTA) 21,780,800 21,780,800 HYDRAULIC SYSTEMS - -2 SETS 1,172,012 - BALANCE STAGE PAYMENT WITH : GTTC 2,979,927 - ADA DEVELOPED ITEMS 9,803,537 2,926,518 BALANE STAGE PAYMENT WITH: BHEL HPVP 3,313,573 5,090,592 : CTTC (62,689) (62,689) WEIGHT & PERFORMANCE OPTIMISATION OF HEs 8,510,555 2,414,017 BALANE STAGE PAYMENT WITH: NAL (985,273) (229,875) : BHEL HPVP 3,838,860 7,380,000 ENVIRONMENT CONTROL SYSTEM 290,411 - BALANE STAGE PAYMENT WITH: NAL 1,609,590 - WHEELS & BRAKES 2 SETS 1,372,460 - BALANE STAGE PAYMENT WITH: ASL 88,700 5,025,378 CARBON HEAT PACKS 7,591,300 2,654,622 MAINT. OF GENERAL SYSTEM TEST RIG FOR 6 YRS 5,143,440 955,635 BALANE STAGE PAYMENT WITH: CMTI (535,000) - 5,403,672,100 4,606,991,189 84.54.00 FLIGHT CONTROL SYSTEM

DFCC FABRICATION 152,275,156 144,360,378 BALANCE STAGE PAYMENT WITH : ADE 53,705,546 11,480,206 : RCI, HYD 2,470,771 2,500,000 ENGINEERING TEST STATION (STE) 106,798,268 82,795,833 BALANCE STAGE PAYMENT WITH : ADE 21,936,732 9,939,167 STTE MAINTENANCE FACILITY 871,488 - NEW DFCC DEV INCLUDING TWO BRASS BOARDS 86,220,860 69,883,889

83 Annual Report 2015-16 ADA

Investments in LCA Airforce FSED Phase 3 upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

BALANCE STAGE PAYMENT WITH : ADE 12,426,229 9,939,142 OPERATIONAL FLIGHT PROGRAMME (OFP) 994,597 225,681 MANPOWER COST FOR IFCS ACTIVITIES 3,920,771 2,366,445 BALANCE STAGE PAYMENT WITH : ADE (2,491,103) (936,777) ON BOARD RECORDING & BACK UP TELEMETRY UNITS 14,542 - 439,143,857 332,553,964 84.55.00 AVIONICS - COCKPIT DISPLAY & CONTROL PANEL PANEL MULTIFUNCTION DISPLAY 2,331,600 - OPEN ARCHITECTURE COMPUTER 30,235,743 28,028,848 SIB, SSB,PIB 2,613,814 1,408,455 COCKPIT LIGHTS 2,645,757 - BALANCE STAGE PAYMENT WITH : CSIO 2,869,001 - 40,695,915 29,437,303 84.59.00 AVIONICS - MULTIMODE RADAR

AVIONICS MULTIMODE RADAR 73,000,349 63,621,367 BALANCE STAGE PAYMENT WITH : ECIL (20,202,668) (42,720,675) : VIT VELLORE 3,902 35,887 52,801,583 20,936,579 84.62.00 AVIONICS - ELECTRICAL SYSTEM

ELECTRICAL LIGHTS - 3 SETS 750,388 - BALANCE STAGE PAYMENT WITH : CSIO 3,126,662 - ELECTRICAL SYSTEM - GPPU, SI, TRU 7,137,140 - BALANCE STAGE PAYMENT WITH : HAL LD 2,449,640 - 13,463,830 - 84.64.00 GROUND TESTING

WIND TUNNEL TESTS IN INDIA 65,740,516 56,928,331 BALANCE STAGE PAYMENT WITH : NAL (432,713) (3,414,155) : IIT KANPUR (1,830,600) 217,116 WIND TUNNEL TESTS IN ABROAD 52,771,121 52,771,121 AVIONICS INTEGRATION 25,720,599 6,594,103 BALANCE STAGE PAYMENT WITH : IISC 1,023,427 - 142,992,350 113,096,516

84 ADA Annual Report 2015-16

Investments in LCA Airforce FSED Phase 3 upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

84.65.00 FLIGHT TESTING

GROUND FACILITY 378,409 378,409 378,409 378,409 84.68.00 TECHNOLOGY DEVELOPMENT

NEW ENGINE AIRFRAME INTEGRATION STUDIES 391,575 391,575 STRUCTURAL ANALYSIS CODES - S/W 6,314,119 3,228,093 BALANCE STAGE PAYMENT WITH : NAL 394,854 - MISSION EFFECTIVENESS STUDIES 597,022 192,338 BALANCE STAGE PAYMENT WITH : NAL (68,565) 336,119 CFD 13,967,714 11,871,074 NMG MODIFICATION FOR PPERFORMANCEERFOR,AMCE IMPROVEMENT 506,782 104,615 22,103,501 16,123,814 84.84.00 PRODUCT SUPPORT

GROUND SUPPORT EQUIPMENT 371,964 - 371,964 - 84.92.00.00 PROJECT MANAGEMENT EXPENDITURE 3,312,360,129 2,176,449,129 BALANCES WITH HAL-ARDC FOR FACILITY ESTABLISHMENT AND WORK PACKAGES

(BREAK-UP AS CERTIFIED BY THEM) INVENTORY HELD BY THEM 204,289,521 75,714,749 GOODS IN TRANSIT - 5,331,138 CAPITAL WORK IN PROGRESS 123,070 123,070 BALANCE STAGE PAYMENT (6,211,896) 79,375,064 198,200,695 160,544,021 HALs PROFIT 40,366,604 38,032,129 TOTAL 10,549,741,735 8,101,268,324

for ABS & CO. CHARTERED ACCOUNTANTS FRN 008203S Sd/- Sd/- Sd/- H G ANAND M.S. KRISHNA MURTHY M A ANANDAN PARTNER Chief Finance Officer Offtg. Jt. Director (Finance) Membership No. 206226 Sd/- Sd/- CMDE. (RETD.) C.D. BALAJI K. RAVI KUMAR Place : Bangalore Secretary FA to DG-ADA Date : 12.09.2016 85 Annual Report 2015-16 ADA

Investments in Navy FSED Phase 1 upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

74.44.00.00 INFRASTRUCTURE

CIVIL WORKS - BUILDING - ADA 26,248,425 26,170,529 CIVIL WORKS - AMENITY BUILDING - HAL 684,574 684,574 COMPUTERS - HARDWARE PURCHASES 1,951,102 1,951,102 COMPUTERS - SOFTWARE PURCHASES 6,581,638 6,581,638 PCs,H/W,S/W,PRINTERS,PLOTTERS ETC., 18,754,200 17,859,350 WORK STATION H/W, S/W 41,892,960 40,818,823 OFFICE EQUIPMENT - PURCHASES 860,819 755,819 FURNITURE & FIXTURES 3,515,902 2,838,255 MOTOR VEHICLE 2,345,572 2,345,572 PLANT & MACHINERY - NC SHOP 29,327,885 19,816,112 PLANT & MACHINERY - COMPOSITE SHOP 862,920 862,920 TELECOMUNICATIONS 24,960 24,960 TEST EQUIPMENT, INSTRUMENT & MACHINE 125,037 - PCs & WORKSTATION 56,822,881 56,822,881 PLOTTERS, PRINTERS & NETWORKING 9,749,906 7,205,599 199,748,781 184,738,134 74.45.00.00 AIRCRAFT DESIGN & INTEGRATION

VERIFICATION & VALIDATION OF S/W TOOLS 3,199,929 2,696,885 CEF TRAINER 22,615,762 19,633,707 ENGINEERING COST - ADA 805,996,789 422,426,803 ENGINEERING COST - HAL ARDC 1,314,525,169 1,314,353,578 AVIONICS SOFTWARE UPDATE 2,199 2,199 CONTROL LAW DESIGN - NAL 50,296,665 47,198,705 BALANCE STAGE PAYMENT WITH : NAL (8,762,277) (7,164,317) WEAPON & SENSORS S/W DEVELOPMENT 345,891,677 345,928,646 BALANCE STAGE PAYMENT WITH : ADE 6,877,049 22,951 CONTROL LAW -ADA 47,764,047 19,627,776 BALANCE STAGE PAYMENT WITH : ADE 4,736,555 5,152,197 : NAL 3,818,850 20,501,274 2,596,962,414 2,190,380,404

86 ADA Annual Report 2015-16

Investments in Navy FSED Phase 1 upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

74.47.00.00 TOOLING

JIG & DRILL PLATES 40,802,656 34,544,666 74.50.00.00 PROTOTYPE – CFC COMPONENTS CFC WING - LABOUR EFFORT 5,802,000 5,802,000 74.51.00.00 PROTOTYPE - AIRCRAFT MATERIAL RAW MATERIAL 59,866,262 50,684,445 BOUGHT OUT ITEMS 52,999,941 46,095,053 RADOME 17,299,109 13,900,740 BALANCE STAGE PAYMENT WITH : HAL O/H DIV - 1,827,637 BALANCE STAGE PAYMENT WITH : DRDL - 473,616 RUDDER 117,139 117,139 FUSELAGE METALLIC MATERIALS 243,834,502 209,433,447 FUSELAGE COMPOSITES - ADA 52,773,405 44,225,123 STANDARD PARTS 241,356,091 204,339,425 668,246,449 571,096,625 74.52.00.00 PROTOTYPE - AIRCRAFT FABRICATION FABRICATION, ASSEMBLY & EQUIPPING 1,453,557,279 1,242,449,870 COMPOSITE DROP TANKS 802,287 802,287 1,454,359,566 1,243,252,157 74.53.00.00 GENERAL SYSTEMS JET FUEL STARTER 43,640,857 43,640,857 BALANCE STAGE PAYMENT WITH : HAL EDB (470,600) (1,970,600) AMAGB 39,175,834 39,175,834 BALANCE STAGE PAYMENT WITH : CVRDE 242,179 242,179 SENSORS & SWITCHES 3,836,750 3,836,750 ENGINE HEALTH MONITORING 57,483,583 32,416,498 GENERAL SYSTEM LRU'S - HAL ARDC 680,463,048 617,248,785 BALANCE STAGE PAYMENT WITH : HAL-LD (953,110) (953,110) HYDRAULIC SYSTEM - INDIGENOUS ITEMS 64,105,343 63,500,433 BALANCE STAGE PAYMENT WITH : DMRL 98,169 98,169 : GTTC 2,193,947 1,013,796 : CTTC (62,689) (62,689)

87 Annual Report 2015-16 ADA

Investments in Navy FSED Phase 1 upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

HYDRAULIC SYSTEM - LD DEVELOPED ITEMS 22,013,824 21,975,588 HYDRAULIC FILTERS 7,321,024 7,321,024 AIR CREW PROTECTIVE CLOTH 4,448,645 4,286,335 DESIGN & DEV. OF ECS 19,164,272 19,164,272 E C S BOF 33,655,845 33,655,845 UPLOCKS 4,490,037 148,392 DOOR JACKS 12,885,290 12,885,290 WHEELS & BRAKE ASSEMBLY 75,479,452 59,727,582 BALANCE STAGE PAYMENT WITH : HAL LD (12,197,770) 3,554,100 CARBON HEAT PACKS 36,028,513 36,028,513 UNDER CARRIAGE & ARRESTER HOOK DVLPT 15,667,787 15,667,787 ESCAPE AID SYSTEM - SEATS & ACCESSORIES 73,057,155 63,482,867 1,181,767,385 1,076,084,497 74.54.00.00 FLIGHT CONTROL SYSTEM

ADDITIONAL SHIPSETS 499,178,144 480,611,927 BALANCE STAGE PAYMENT WITH : ADE 14,498,052 16,005,532 ACTUATORS FOR LEVCON 250,260,137 249,625,963 FCP & FTP 7,882,334 7,882,334 SUPPORT FOR S/W DEVELOPMENT AT ADE 50,292,861 37,561,481 BALANCE STAGE PAYMENT WITH : ADE 228,258 4,959,638 822,339,786 796,646,875 74.55.00.00 AVIONICS-COCKPIT DISPLAY & CONTROL PANEL HUD - HEAD UP DISPLAY 40,042,927 39,071,856 BALANCE PAYMENT WITH : CSIO 3,384,752 355,823 MFD - MULTI FUNCTION DISPLAY 22,195,028 21,049,667 OPEN ARCHITECTURE COMPUTER 60,272,793 53,218,165 LCD DISPLAY SYSTEM AND UCP 39,196,184 35,180,024 SIB, SSB & PIB 54,297,544 47,154,781 BALANCE PAYMENT WITH : BEL 353,762 475,952 COCKPIT LIGHTS 9,275,601 9,275,601 229,018,591 205,781,869

88 ADA Annual Report 2015-16

Investments in Navy FSED Phase 1 upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

74.57.00.00 AVIONICS - RING LASER GYRO

RING LASER GYRO 19,445,696 19,445,696 74.59.00.00 AVIONICS - MULTIMODE RADAR

DEVELOPMENT - CONSULTANCY 239,149,115 234,274,710 239,149,115 234,274,710 74.60.00.00 EW SUITE DEVELOPMENT

EW SUITE 6,686,800 6,686,800 74.61.00.00 AVIONICS – COMMUNICATION EQUIPMENT

COMMUNICATION EQUIPMENT 30,933,815 30,932,248 30,933,815 30,932,248 74.62.00.00 AVIONICS - ELECTRICAL SYSTEM

EXTERNAL LIGHTING 1,978,414 1,497,600 BALANCE STAGE PAYMENT WITH : HAL-LD 425,310 3,079,759 DISTRIBUTION BOXES 33,214,840 29,458,136 35,618,564 34,035,495 74.63.00.00 AVIONICS - OTHER ITEMS

MISSION PREPARATION & DATA RETRIEVAL UNIT 1,027,563 - CRASH DATA RECORDER 11,785,723 11,785,723 BOIs - AHCP, MAGNETO METER 24,801,265 24,801,265 ANTENNA 5,432,007 5,432,007 CENTRALISED WANRING PANEL - CWP/CWS 10,644,750 10,644,750 HMD - HELMET MOUNTED DISPLAY 16,136,047 10,859,207 SPECIAL AVIONICS FIT FOR NAVAL REQ SONAR LOCATOR 239,391 239,391 BEACONS 70,066,746 63,762,343 74.64.00.00 GROUND TESTING

WIND TUNNEL TESTING - IN INDIA 32,730,793 28,084,409 BALANCE STAGE PAYMENT WITH : NAL 939,238 1,668,170 WIND TUNNEL TESTING - ABROAD 21,390,670 21,229,908 SYSTEM TEST RIGS 4,984,954 4,009,017 EMI/EMC FACILITY 3,923,910 3,923,910

89 Annual Report 2015-16 ADA

Investments in Navy FSED Phase 1 upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

LIGHTENING TEST FACILITY 1,651,527 1,651,527 AVIONICS INTEGRATION - TEST EQUIPMENT 17,528,673 15,870,051 IRON BIRD AUGMENTATION & MAINTENANCE 45,625,755 45,345,868 ENGINEERING TEST STATION 737,088 737,088 MINI BIRD 664,186 664,186 SKI JUMP & ARRESTING GEAR TEST 4,491,001,537 4,486,620,241 BALANCE STAGE PAYMENT WITH : RDE, PUNE 2,399,948 1,019,590 GOA SHIPYARD COMPANY - (38,347) GROUND TEST FACILITY FOR U/C ARRESTOR HOOK 27,845,254 27,845,254 GROUND TEST SHOP EFFORT (ADB) 116,454,509 80,364,865 BALANCE STAGE PAYMENT WITH : GTRE 648,748 881,665 4,768,526,790 4,719,877,402 74.65.00.00 FLIGHT TESTING

FLIGHT TEST INSTRUMENTATION 115,053,555 87,166,527 SPARES FOR LRUs FOR FLIGHT TESTING 252,097,503 227,982,329 367,151,058 315,148,856 74.66.00.00 TRAINING CONSULTANCY & TECH ASSISTANCE CONSULTANCY FOR DEVELOPMENT OF CONTROL LAW 325,525,808 325,525,808 TRAINING & CONSULTANCY IN OTHER AREAS 52,877,947 52,877,947 378,403,755 378,403,755 74.68.00.00 TECH. DEVELOPMENT - DESIGN ANALYSIS

DIGITAL/VIRTUAL PROTOTYPE 7,275,674 1,402,704 7,275,674 1,402,704 74.70.00.00 TECHNOLOGY DEVELOPMENT - COMPOSITE MATERIALS COMPOSITES - MATERIALS & PROCESSES 2,614,523 2,614,523 74.71.00.00 TECHNOLOGY DEVELOPMENT - AVIONICS

SPECIAL STUDIES FOR A/C OPERATION DECK 2,654,480 2,654,480 74.84.00.00 PRODUCT SUPPORT

GSE-GROUND SUPPORT EQUIPMENT 217,384 217,384 217,384 217,384

90 ADA Annual Report 2015-16

Investments in Navy FSED Phase 1 upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

74.92.00.00 PROJECT MANAGEMENT EXPENDITURE 1,264,359,124 1,063,904,241 74.74.00.00 ENGINE INTEGRATION

ENGINE COST 843,894,142 841,404,956 DEVELOPMENT COST FOR NAVAL REQUIREMENTS 27,095,493 - NAVAL SPECIFIC TESTING 12,058,077 11,638,806 BALANCE STAGE PAYMENT WITH : HAL-LD (390) (390) 883,047,322 853,043,372 BALANCES WITH HAL-ARDC FOR FACILITY ESTABLISHMENT AND WORK PACKAGES INVENTORY HELD BY THEM 358,068,332 298,588,323 GOODS IN TRANSIT - 36,609,515 CAPITAL WORK IN PROGRESS :

PLANT & MACHINERY UNDER ERECTION 3,011,421 3,011,421 BALANCE STAGE PAYMENT (147,396,455) (140,467,712) 213,683,298 197,741,547 HALs PROFIT 372,215,464 307,682,649 TOTAL 15,861,097,234 14,540,155,430

for ABS & CO. CHARTERED ACCOUNTANTS FRN 008203S

Sd/- Sd/- Sd/- H G ANAND M.S. KRISHNA MURTHY M A ANANDAN PARTNER Chief Finance Officer Offtg. Jt. Director (Finance) Membership No. 206226

Sd/- Sd/- CMDE. (RETD.) C.D. BALAJI K. RAVI KUMAR Secretary FA to DG-ADA

Place : Bangalore Date : 12.09.2016

91 Annual Report 2015-16 ADA

Investments in Navy FSED Phase 2 upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

94.44.00.00 INFRASTRUCTURE

OFFICE BUILDINGS 35,263,159 30,316,944 PCs, H/W,S/W,PRINTER,PLOTTER 2,217,181 1,928,434 WORK STATION H/W S/W 12,648,574 9,219,666 FURNITURE & FIXTURES 1,034,654 469,000 TRANSPORT - HAL ARDC 682,582 - INTRUMENT & EQUIP - QUALITY CONTROL 37,553,237 37,553,237 COMMUNICATION FACILITIES 25,847 - TRANSPARENCY COATING FACILITY 14,727,845 - 104,153,079 79,487,281 94.45.00.00 AIRCRAFT DESIGN & INTEGRATION

SIMULATION & SOFTWARE TOOLS 410,650 - ENGINEERING COST - HAL ARDC 192,381,094 92,049,838 ENGINEERING COST - ADA 14,252,815 12,670,505 207,044,559 104,720,343 94.51.00.00 AIRCRAFT MATERIALS

MATERIAL COST 3 SETS 40,173,173 40,173,173 FUSELAGE METALLIC MATERIALS 423,107 423,107 FUSELAGE COMPOSITES 444,755 444,755 STANDARD PARTS 432,145 432,145 41,473,180 41,473,180 94.53.00.00 GENERAL SYSTEM

PROPULSION SYSTEMS 34,412,274 34,412,274 BALANCE STAGE PAYMENT WITH: ADE - 825,331 HYDRAULIC SYSTEMS - INDIGENOUS ITEMS 8,831,711 686,272 BALANCE STAGE PAYMENT WITH: BHEL HPVP 4,768,289 8,313,728 ENVIRONMENT CONTROL SYSTEM 290,410 - BALANCE STAGE PAYMENT WITH: NAL 1,609,589 - 49,912,273 44,237,605 94.54.00.00 FLIGHT CONTROL SYSTEM

ADDL SHIPSETS 32,464,840 12,688,828 BALANCE STAGE WITH: ADE (6,609,263) (964,389) 25,855,577 11,724,439 94.59.00.00 AVIONICS - MULTIMODE RADAR

AVIONICS - MULTIMODE RADAR 72,400,001 63,268,255 BALANCE STAGE WITH: ECIL (20,202,668) (42,720,677) 52,197,333 20,547,578

92 ADA Annual Report 2015-16

Investments in Navy FSED Phase 2 upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year 94.64.00 GROUND TESTING

WIND TUNNEL TESTING IN INDIA 5,158,205 4,721,973 BALANCE STAGE PAYMENT WITH : NAL 2,627,252 103,035 : IIT KANPUR - 217,117 ENGINEERING TEST STATION AUGMENTATION 8,496,882 5,174,669 & MAINTENANCE BALANCE STAGE PAYMENT WITH : ADE 518,118 - SBTF 599,368,150 348,566,840 BALANCE STAGE PAYMENT WITH : GSL 30,210,461 (14,899,256) : CCE (R&D) 743,793 659,049 647,122,861 344,543,427 94.65.00.00 FLIGHT TESTING

FLIGHT TESTING 2,843,942 395,988 2,843,942 395,988 94.66.00.00 TRAINING CONSULTANCY & TECH. ASST

CONSULTANCY FORDEVELP OF CONTROL LAW 609,075,093 294,309,765 609,075,093 294,309,765 94.68.00.00 TECHNOLOGY DEVELOPMENT - DESIGN ANALYSIS DIGITAL/VIRTUAL PROTOTYPE 12,007,389 - 12,007,389 - 94.74.00 GE ENGINE

ENGINE COST 249,025,371 230,424,869 ENGINE DEVELOPMENT COST 2,134,400,166 1,784,263,145 2,383,425,537 2,014,688,014 BALANCES WITH HAL-ARDC FOR FACILITY ESTABLISHMENT AND WORK PACKAGES (BREAK-UP AS

CERTIFIED BY THEM) BALANCE STAGE PAYMENT 2,604,933 18,685,061 2,604,933 18,685,061 HALs PROFIT 23,147,783 13,137,629 TOTAL 4,160,863,539 2,987,950,310

for ABS & CO. CHARTERED ACCOUNTANTS FRN 008203S Sd/- Sd/- Sd/- H G ANAND M.S. KRISHNA MURTHY M A ANANDAN PARTNER Chief Finance Officer Offtg. Jt. Director (Finance) Membership No. 206226 Sd/- Sd/- CMDE. (RETD.) C.D. BALAJI K. RAVI KUMAR Place : Bangalore Secretary FA to DG-ADA Date : 12.09.2016 93 Annual Report 2015-16 ADA

Investments in Technology Development upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

44.29.00.00 TECH. DEV. TO DEVELOP INDIGENOUS TECH.

44.29.01 AVIONICS & ELECTRICAL SYSTEM

CONFORMAL ANTENNA 6,531,021 6,493,243 BALANCE STAGE PAYMENT WITH: SAMEER - (1,600,000) S/W DEFINED RADIO 8,904,970 8,904,970 BALANCE STAGE PAYMENT WITH: HAL HYD (470) (890,470) SENSOR DATA FUSION 26,723,721 11,451,721 BALANCE STAGE PAYMENT WITH: HAL HYD (10,695,000) 4,577,000 DIGITAL HUD 7,541,059 1,678,944 BALANCE STAGE PAYMENT WITH: HAL LD 708,850 5,132,931 39,714,151 35,748,339 44.29.02 GENERAL SYSTEMS

AMAGB 5,205,482 5,205,481 BALANCE STAGE PAYMENT WITH : CVRDE - 8,142,982 CSD (CONSTANT SPEED DRIVE) 6,472,612 2,899,542 BALANCE STAGE PAYMENT WITH : IIT BOMBAY 1,000,000 50,000 : BARC 1,049,832 1,795,094 HIGH TEMPEATURE VALVES 41,096,127 8,446,314 BALANCE STAGE PAYMENT WITH : HAL LD 3,623,670 9,081,070 : CVRDE 7,346,681 4,827,095 : GTTC 665,458 - : CTTC 354,008 - : SITAR (1,931,216) - ELECTRICAL BRAKING 9,065,880 5,016,694 BALANCE STAGE PAYMENT WITH: ASL 6,287,654 9,305,617 OBOGS 274,392,535 224,497,897 BALANCE STAGE PAYMENT WITH : DEBEL 3,131,952 10,044,551 357,760,675 289,312,337 44.29.03 PROPULSION SYSTEM

JFS WEIGHT REDUCTION 150,000,000 150,000,000 150,000,000 150,000,000

94 ADA Annual Report 2015-16

Investments in Technology Development upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

44.29.04 AIRFRAME AEROELASTICITY 20,116,921 19,375,413 BALANCE STAGE PAYMENT WITH : NAL 1,111,500 - : CMERI 1,750,000 - MATERIALS 13,502,882 11,402,918 BALANCE STAGE PAYMENT WITH : NAL 992,487 (1,372,194) : DMRL - 521,032 : HAL F & F - 10,411 : CECRI - 145,338 COMPOSITES 86,570,202 45,554,822 BALANCE STAGE PAYMENT WITH : NAL 1,243,300 (9,475,675) : ASL 4,129,588 14,360,876 : CTTC 3,014,015 1,999,177 : BATL (2,624,554) (724,554) : HAL (CMD) 5,700,622 5,700,622 135,506,963 87,498,186 44.29.05 INTEGRATED FLIGHT CONTROL SYSTEM

INTG. FLIGHT & PROPULSION - THRUST VECTOR 9,215,025 6,928,879 CONTROL-CONSULTANCY BALANCE STAGE PAYMENT WITH: NAL (483,780) 1,802,366 RATE COMMAND ATTITUDE HOLD CLAW 9,559,249 6,306,801 BALANCE STAGE PAYMENT WITH: NAL (1,320,477) 1,640,549 TECHNOLOGY DEVELOPMENT FOR ETS 6,265,793 1,097,506 BALANCE STAGE PAYMENT WITH: ADE (1,185,357) (446,067) UPGRADATION OF FDS 16,038,059 16,038,059 TECHNOLOGY DEVELOPMENT FOR OFP 51,851,254 50,000,000 BALANCE STAGE PAYMENT WITH: ADE (2,035,313) (184,059) DEV OF LEADING EDGE SLAT ACTUATORS 43,086,213 7,498,726 BALANCE STAGE PAYMENT WITH : CMTI (2,676,637) - TECH DEV FOR NEW TESTING & INTEGRATION TOOLS 10,124 - FTI DEVELOPMENT 1,807,844 - DEV OF AUTOMATED TEST EQUIPMENT 16,920,890 16,782,833 147,052,887 107,465,593

95 Annual Report 2015-16 ADA

Investments in Technology Development upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

44.29.06 AERODYNAMICS

PARALLEL COMPUTER 5,811,985 1,210,234 BALANCE STAGE PAYMENT WITH : IISC 128,249 1,050,000 5,940,234 2,260,234 44.29.07 PROTO VEHICLES & MANUFACTURING

ADVANCED TESTING, NEW CONCEPTS AND PROCEDURES 2,187,788 1,862,216 BALANCE STAGE PAYMENT WITH: ANNAMALAI - 112,860

NEW CONCEPT IN FASTENINGM SEALING ETC. 855,570 855,570 ADVANCED FINISHING & SPECIAL PROCESSES 118,269,529 118,269,529 121,312,887 121,100,175 44.29.08 ADVANCED PROJECTS

DECISION SUPPORT SYSTEM 4,851,066 4,537,614 SPECIAL COATING 15,615 - IR PAINTS 1,204,293 - RCS STUDIES 1,470,072 - BALANCE STAGE PAYMENT WITH : NAL 1,051,650 - : IIT KANPUR 1,434,278

AUTONOMOUS UNMANNED RESEARCH AIRCRAFT 25,939,785 14,674,473 BALANCE STAGE PAYMENT WITH : NAL 15,757 15,757 : IIT BOMBAY 101,948 1,549,516 : SAMEER BOMBAY (899,705) (297,686) : IISC (72,850) 81,150 : IIT KANPUR (1,402,479) (1,402,479) : DEAL (455,460) 968,000 : MS RAMAIAH - 67,828 33,253,970 20,194,173

96 ADA Annual Report 2015-16

Investments in Technology Development upto 31st March 2016 Amount in Rs. Head of Account Current Year Previous Year

44.29.09 FLIGHT TESTING

ADVANCED SUBMINIATURE 990,622 - BALANCE STAGE PAYMENT WITH: IISC 393,978 - NEXT GENERATION TRANSMITTERS & RECEIVERS 8,290,302 8,290,302 9,674,902 8,290,302 TOTAL 1,000,216,669 821,869,339

for ABS & CO. CHARTERED ACCOUNTANTS FRN 008203S

Sd/- Sd/- Sd/- H G ANAND M.S. KRISHNA MURTHY M A ANANDAN PARTNER Chief Finance Officer Offtg. Jt. Director (Finance) Membership No. 206226

Sd/- Sd/- CMDE. (RETD.) C.D. BALAJI K. RAVI KUMAR Secretary FA to DG-ADA

Place : Bangalore Date : 12.09.2016

97