DOCSLIB.ORG

Technical Specification for Hal-Dornier-228-202 Aircraft System

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
Technical Specification for Hal-Dornier-228-202 Aircraft System ANNEXURE - 1 TECHNICAL SPECIFICATION FOR HAL-DORNIER-228-202 AIRCRAFT SYSTEM HINDUSTAN AERONAUTICS LIMITED TRANSPORT AIRCRAFT DIVISION POST CHAKERI KANPUR INDIA This document is the property of HAL and should Be treated in strict confidence for the intended purpose. The information contained in this document should not be divulged to any third party. CONTENTS CHAPTERS DESCRIPTION 1 HAL-DO-228 Aircraft: General Description……………………………….3 2 Standard HAL-DO-228 Aircraft: Equipment Fit…………………………10 3 Aircraft Performance………………………………………………………………20 4 Aircraft Cabin and Seat Rail details.............................................22 5 Aircraft Antenna Layout...............................................................25 Page 2 of 25 CHAPTER-1 1 HAL-DO-228 AIRCRAFT: GENERAL DESCRIPTION 1.1 The HAL-DO-228 aircraft is a high wing monoplane with a cantilevered wing and two turboprop engines in wing-mounted pod designed for multipurpose utility and commuter services. Characteristics like low fuel consumption, short take off and landing capabilities, operation from semi prepared runways, comfortable air- conditioned cabin and long range make this aircraft ideally suitated for such applications. The leading particulars of the aircraft are: Type HAL-DO-228 AIRCRAFT No. of Crew 2 Maximum Take-off Weight 6400 Kg Maximum Landing Weight 5900 Kg Power Plant 2 Garrett TPE 331-5-252D Turboprops Propellers 2 four bladed reversible pitch Hartzell propellers – HC-B4TN-5ML/LT10574FS Overall Length 16.56 M (54 ft, 4 in) Wing Span 16.97 M (55 ft, 8 in) Maximum Height 4.86 M (15 ft, 11 in) Landing Gears Hydraulically actuated fully retractable Electrical systems 28V, 300 amps DC Page 3 of 25 1.2 Design philosophy 1.2.1 The aircraft is designed to meet normal category requirement of FAA/FAR23. The standard aircraft and associated equipment conform to the certification requirements of LBA and FAA. 1.2.2 The design features include Functional multiplicity – easily and quickly convertible for various roles and missions. Minimum dependence on ground equipment. Operation from short, semi-prepared airfields. Glass cockpit layout. Low internal and external noise level. Open architecture to ensure easy and economical upgradations and long service life. 1.3 Operating Condition 1.3.1 The HAL-DO-228 aircraft has been designed and time tested to operate in all weather conditions (day and night), in tropical (high temperature and high humidity) and other adverse environmental conditions such as low level flight in marine condition. 1.3.2 The aircraft will function satisfactorily within the temperature range of -40 deg C to +55 deg C. 1.4 STOL Capability Specially designed wing airfoil and platform shape coupled with single-slotted Fowler Flap system provide short Take-off and Landing capability to HAL-DO-228 aircraft. 1.5 Rough Field characteristics The sturdy retractable landing gear, a wide wheel base and turboprop engines mounted well clear off the ground on the high wing, permit HAL-DO-228 a/c operation from short strips and semi-prepared airfields. The fuselage mounted main gear retracts into fairings on the fuselage sides. Page 4 of 25 1.6 Power Plant The aircraft is powered by two Garrett TPE-331-5-252D engines each driving a four bladed Hartzell HC-B4TN-5ML/LT 10574 constant speed, fully feathering , reversible pitch propellers of dia. 2.69 m & rpm 1591. Nominal engine power is 715 SHP (flat rated at ISA +18 deg C, sea level). The engine is manufactured under licence from Honeywell at HAL Engine Division and is featured by Propeller Control system. Anti-icing and Foreign Object damage resistance. Reverse thrust. Negative torque sensing. Low emission, low noise. Page 5 of 25 1.7 Wing The main wing is made of three principal sections: a constant chord centre section extending just outboard of the engines ; and outer wing panels left and right incorporating taper and twist (nose down). Each wing embodies two integral fuel tanks between front and rear spars. The external dimensions of wing are – Span 16.97 M Area 32.00 Sq. M. Airfoil DO A5 Aspect ratio 9.0 Taper ratio 0.7 Sweep back (Leading Edges) • Inboard 0 deg. • Outboard 8 deg. 1.8 Fuselage The HAL-DO-228 features a rectangular non-pressurised fuselage which allows economical and trouble free structural maintenance with minimum down time as compared to pressurised aircraft. The flight openable roller door located behind the wing contributes to the ease of operations and adds to versatility in such utility applications. Easily accessible baggage areas are available in the aircraft’s nose section and aft of the cabin area. The external dimensions of fuselage are: Length 16.56 M Max. Height 1.90 M Max. Width 1.50 M 1.9 Air Conditioning System The aircraft is equipped with an air-conditioning system which is capable of maintaining the flight compartment temperatures at comfortable levels. Temperatures in the cabin and flight compartment is maintained between +18 deg C and +28 deg C and is selected and controlled automatically. Manual regulation of temperature is also provided. Flow limited bleed air from both engines passes through a venturi and a heat exchanger to a cold air unit. In the mixing chamber, cold air and warm bleed air is mixed according to the control panel settings. After dehydration, the conditioned air Page 6 of 25 is routed to the fixed floor level outlets, the adjustable individual outlets in the cabin ceiling and the equivalent outlets in the cockpit. If required, the air duct system can be fed with ram air. The air-conditioning system is then automatically shut off. On the ground the air-conditioning system can be actuated only when both RPM- levers are at a setting below 96%. In the region above 96% with the landing gear lowered, either on the ground or in the air, the system is deactivated automatically. The seat area is furnished with an array of adjustable air outlets. The air outlets provide individual control of flow rate and direction of the heating, cooling or ram air stream. The outlets are installed in the side ceiling panels and are accessible from the passenger seats. 1.10 Flight Deck/Cockpit The cockpit accommodates two crew members. The aircraft has dual controls and is normally flown by two pilots. Access to the cockpit is either through the cabin or through a separate cockpit door. Excellent visibility is provided for both the pilots. The wind shield provided is capable of absorbing impact energies and incorporates heating arrangements for de-icing. Flight instruments and indicators are provided on front panel while navigation and communication controls on central pedestal and switches on two overhead panels. Cockpit has a separate entry/exit door for the pilot and is equipped with a bad weather window. The seats and pedals are of adjustable type. 1.11 Hydraulic System The hydraulic system operates the landing gear, brakes and nose wheel steering. Hydraulic power is generated by a self regulating pump driven by a DC powered electrical motor. Nominal system pressure is 206 bar (3000 psi). The normal hydraulic power supply system consists of: An electrically driven hydraulic pump. A hydraulic reservoir with a maximum filling volume of 2.6 litres. A pressure gauge. A pneumatic emergency blow down system caters for emergency extension of landing gears. The blow down bottle is filled with nitrogen at a pressure of 170 bars at 20 deg C. The charging pressure of the bottle is indicated by a pressure indicator which can be checked from the outside through an inspection window in the fuselage. Page 7 of 25 1.12 Landing Gear The hydraulically operated landing gear consists of a forward retracting twin wheel nose leg and sideways retracting single wheel main legs. The main landing gear consists of two oleo-pneumatic shock absorbers which are integrated in the gear structure. The main wheels retract sideways below the fuselage from attachment points at the side of the fuselage. The landing gear actuators are secured by an internal mechanical lock at the extended position. The twin wheel nose landing gear consists of a steerable oleo-pneumatic shock absorber which is integrated in the gear strut. Extension and retraction of the main gear and nose gear is powered by the hydraulic system. 1.13 Fuel System The fuel system consists of two independent systems which can be connected by cross feed. The LH fuel system is identical to the RH fuel system. During normal operation, each fuel system feeds the corresponding engine. Each system comprises of: Fuel tanks. Fuel Booster Pumps. Jet pumps. Fire Cock. Crossfeed System. Indicating System. Three integral tanks are fitted in each wing. The total useable fuel capacity is 2850 litres (2250 kgs). The tanks in each wing are interconnected. Fuel transfer to the feeder tanks is made by jet pumps. Fuel system includes a Fuel Dumping System which allows for discharge of additional fuel to maintain maximum admissible landing weight in the event of an emergency immediately after take off. The system consists of a fuel dump valve controlled from an overhead panel in cockpit. 1.14 Wing Hard points The wings are fitted with hard points to provide for mounting of four external stores. The inboard and outboard hard points have load carrying capacity of 295 kgs and 220 kgs each respectively. The total load capacity of hard points is 1030 kgs. Page 8 of 25 1.15 Electrical System The electric system is a 28V DC single wire installation with the airframe used as ground return. The primary DC power is supplied by two engine-driven starter generators and two nickel-cadmium batteries for ground or emergency operation. For external 28V DC power supply a ground power connection is installed in the nose section.
Load more

Recommended publications
  • Report on the Aircraft Accident at Bodø Airport on 4 December 2003 Involving Dornier Do 228-202 Ln-Hta, Operated by Kato Airline As
    SL Report 2007/23 REPORT ON THE AIRCRAFT ACCIDENT AT BODØ AIRPORT ON 4 DECEMBER 2003 INVOLVING DORNIER DO 228-202 LN-HTA, OPERATED BY KATO AIRLINE AS This report has been translated into English and published by the AIBN to facilitate access by international readers. As accurate as the translation might be, the original Norwegian text takes precedence as the report of reference. June 2007 Accident Investigation Board Norway P.O. Box 213 N-2001 Lillestrøm Norway Phone:+ 47 63 89 63 00 Fax:+ 47 63 89 63 01 http://www.aibn.no E-mail: [email protected] The Accident Investigation Board has compiled this report for the sole purpose of improving flight safety. The object of any investigation is to identify faults or discrepancies which may endanger flight safety, whether or not these are causal factors in the accident, and to make safety recommendations. It is not the Board’s task to apportion blame or liability. Use of this report for any other purpose than for flight safety should be avoided. Accident Investigation Board Norway Page 2 INDEX NOTIFICATION .................................................................................................................................3 SUMMARY.........................................................................................................................................3 1. FACTUAL INFORMATION..............................................................................................4 1.1 History of the flight..............................................................................................................4
    [Show full text]
  • Quarterly Aviation Report
    Quarterly Aviation Report DUTCH SAFETY BOARD page 14 Investigations Within the Aviation sector, the Dutch Safety Board is required by law to investigate occurrences involving aircraft on or above Dutch territory. In addition, the Board has a statutory duty to investigate occurrences involving Dutch aircraft over open sea. Its October - December 2020 investigations are conducted in accordance with the Safety Board Kingdom Act and Regulation (EU) In this quarterly report, the Dutch Safety Board gives a brief review of the no. 996/2010 of the European past year. As a result of the COVID-19 pandemic, the number of commercial Parliament and of the Council of flights in the Netherlands was 52% lower than in 2019. The Dutch Safety 20 October 2010 on the Board therefore received fewer reports. In 2020, 27 investigations were investigation and prevention of started into serious incidents and accidents in the Netherlands. In addition, accidents and incidents in civil the Dutch Safety Board opened an investigation into a serious incident aviation. If a description of the involving a Boeing 747 in Zimbabwe in 2019. The Civil Aviation Authority page 7 events is sufficient to learn of Zimbabwe has delegated the entire conduct of the investigation to the lessons, the Board does not Netherlands, where the aircraft is registered and the airline is located. In the conduct any further investigation. past year, the Dutch Safety Board has offered and/or provided assistance to foreign investigative bodies thirteen times in investigations involving Dutch The Board’s activities are mainly involvement. aimed at preventing occurrences in the future or limiting their In this quarterly report you can read, among other things, about an consequences.
    [Show full text]
  • 75 Jahre Forschungsstandort Oberpfaffenhofen 3 Vialight Communications Gmbh 41
    INHALT VORWORT VORWORT INFORMATIONS- & TELEKOMMUNIKATIONSTECHNOLOGIE 75 JAHRE FORSCHUNGSSTANDORT Martin Zeil, Bayerischer Staatsminister für Wirtschaft, Infrastruktur, Concat AG 12 Verkehr und Technologie Eureka Navigation Solutions AG 38 OBERPFAFFENHOFEN 75 Jahre Forschungsstandort Oberpfaffenhofen 3 ViaLight Communications GmbH 41 GRUSSWORT LUFT- & RAUMFAHRT Der Forschungsstandort Oberpfaffenhofen dass es uns gelang, eines der beiden Galileo 20 neue Unternehmen zu gründen, von denen Karl Roth, Landrat des Landkreises Starnberg 4 328 Support Services GmbH / 328 Design GmbH 8 feiert dieses Jahr sein 75-jähriges Bestehen. Kontrollzentren nach Oberpfaffenhofen zu der größte Teil auch später dem Standort treu Anwendungszentrum GmbH Oberpfaffenhofen 9 Dazu meinen herzlichen Glückwunsch. holen. bleibt. HISTORIE bavAIRia e. V. 11 In der Anfangszeit hätte es wohl niemand für Neben dem DLR wird der Standort Ober- Der Freistaat Bayern misst der Luft- und Forschungsstandort Oberpfaffenhofen – ein Rückblick 5 Deutsches GeoForschungsZentrum GFZ 14 möglich gehalten, dass das kleine Oberpfaffen- pfaffenhofen maßgeblich durch erfolgreiche Raumfahrt eine hohe Bedeutung bei. Bayern- BRANCHENVIELFALT Deutsches Zentrum für Luft- und Raumfahrt (DLR) 15 hofen, in einer ländlichen Umgebung weit Unternehmen, die von der Luftfahrt bis hin weit sind in diesem Industriezweig rund 36.000 außerhalb der Stadt München, einen derartigen zur Automotive Branche reichen, geprägt. Die Mitarbeiter beschäftigt und erwirtschaften einen Die Mischung macht’s 7 DLR GfR mbH 20 EDMO-Flugbetrieb GmbH 22 Bekanntheitsgrad erlangen wird. Heute ist der Palette umfasst neben international agieren- jährlichen Umsatz von rund 6,9 Mrd. Euro. Standort ein Synonym für internationale Spitzen- den Konzernen innovative mittelständische Um der Bedeutung der Luft- und Raumfahrt GCT Gruppe 24 AUS- & WEITERBILDUNG leistungen in der Luft- und Raumfahrt.
    [Show full text]
  • Shownews Farnsborough Day 4
    D A Y 4 AVIATION WEEK & SPACE TECHNOLOGY / AIR TRANSPORT WORLD / SPEEDNEWS July 14, 2016 Farnborough Airshow Engine War Intensifies P&W’s geared turbofan and CFM LEAP battle to power A320s.PAGE 3 Qatar Cools on A350s Al Baker considers 777-300ERs to fill gap in delivery schedule. PAGE 3 Apache Fires Brimstone MBDA completes live firing trials of the direct-fire missile. PAGE 4 Norsk Titanium Wins Deals Additive manufacturing company to supply major OEMs. PAGE 6 Airbus Halves A380 Production ISTAR Chief Speaks Out Airbus is making a large cut to its A380 output, innovating and investing in the A380,” he RAF’s intelligence head criticizes as the manufacturer continues to struggle with added. In an effort to defer concerns that reduction of Sentinel fleet. PAGE 8 securing additional sales for its largest aircraft. Airbus may abandon the A380, Bregier said, The company said on Tuesday that in 2018 “The A380 is here to stay.” Personal Health for Engines it will reduce production of the aircraft from Airbus currently has orders for 319 A380s. It GE Aviation applies data analyt- the current 2.5 per month to one. has delivered a total of 193, 27 of which were ics on an industrial scale. PAGE 10 “With this prudent, proactive step we delivered in 2015. This year it has handed over are establishing a new target for our indus- 14 aircraft, as of mid-July. trial planning, meeting current commercial The decision to reduce production further Airship, C-130J: Cargo Duo demand, but keeping all our options open will result in a huge challenge to keep the pro- Lockheed markets civil C-130 and to benefit from future A380 markets,” CEO gram profitable on a recurring cost basis.
    [Show full text]
  • Sluggish Economy Stalls New Turboprops G-21 Super Goose by Mark Huber
    new (AND BORN-AGAIN) R E B R turboprops U H T T T Comp Air CA-12 A M Sluggish economy stalls new turboprops G-21 Super Goose by Mark Huber he sluggish economy has stalled investment into new turboprop development, but updates of established models from legacy manufacturers are still coming to market pretty much on t schedule. While overall sales of new turboprops are down, the decrease is nowhere near the 37-percent decline in new business jet sales. New sales of established turboprop models are down slightly for everyone year over year through the second quarter. Collectively, new turboprop shipments were down 13.6 percent, according to the General Aviation Manufacturers Association. Several companies that last year claimed to have funds in hand to finish their development programs for all-new aircraft encountered financing difficulties this year. Epic LT the aircraft for Farnborough collapsed and ize and it would be moved in at Melbourne recently has Germany’s Dornier family Hints of trouble began to emerge at Farnborough filed for bankruptcy in Sep- by year-end. A new date for first flight of a made a serious attempt at building an order Bend, Ore.-based Epic more than a year tember last year after failing to attract suffi- conforming prototype–previously scheduled book and planning for production. So far ago when a deal for a $200 million infusion cient investment capital. A new ownership for July of this year–has not been set. the company has letters of intent (LOI) for from an Indian billionaire collapsed, the group took over the company this year and A preliminary nonconforming proto- more than 25 of the $6 million, 180-knot, company skipped EAA AirVenture and plans to continue development, but details type of the Model 12 first flew in 2007.
    [Show full text]
  • World Air Forces Flight 2011/2012 International
    SPECIAL REPORT WORLD AIR FORCES FLIGHT 2011/2012 INTERNATIONAL IN ASSOCIATION WITH Secure your availability. Rely on our performance. Aircraft availability on the flight line is more than ever essential for the Air Force mission fulfilment. Cooperating with the right industrial partner is of strategic importance and key to improving Air Force logistics and supply chain management. RUAG provides you with new options to resource your mission. More than 40 years of flight line management make us the experienced and capable partner we are – a partner you can rely on. RUAG Aviation Military Aviation · Seetalstrasse 175 · P.O. Box 301 · 6032 Emmen · Switzerland Legal domicile: RUAG Switzerland Ltd · Seetalstrasse 175 · P.O. Box 301 · 6032 Emmen Tel. +41 41 268 41 11 · Fax +41 41 260 25 88 · [email protected] · www.ruag.com WORLD AIR FORCES 2011/2012 CONTENT ANALYSIS 4 Worldwide active fleet per region 5 Worldwide active fleet share per country 6 Worldwide top 10 active aircraft types 8 WORLD AIR FORCES World Air Forces directory 9 TO FIND OUT MORE ABOUT FLIGHTGLOBAL INSIGHT AND REPORT SPONSORSHIP OPPORTUNITIES, CONTACT: Flightglobal Insight Quadrant House, The Quadrant Sutton, Surrey, SM2 5AS, UK Tel: + 44 208 652 8724 Email:LQVLJKW#ÁLJKWJOREDOFRP Website: ZZZÁLJKWJOREDOFRPLQVLJKt World Air Forces 2011/2012 | Flightglobal Insight | 3 WORLD AIR FORCES 2011/2012 The French and Qatari air forces deployed Mirage 2000-5s for the fight over Libya JOINT RESPONSE Air arms around the world reacted to multiple challenges during 2011, despite fleet and budget cuts. We list the current inventories and procurement plans of 160 nations.
    [Show full text]
  • NASA Technical Memorandum 0000
    NASA/TM–2018-219833 Short-Haul Revitalization Study Final Report Ty V. Marien, Kevin R. Antcliff, Mark D. Guynn, and Douglas P. Wells Langley Research Center, Hampton, Virginia Steven J. Schneider and Michael Tong NASA Glenn Research Center, Cleveland, Ohio Antonio A. Trani and Nicolas K. Hinze Virginia Polytechnic Institute and State University, Blacksburg, Virginia Samuel M. Dollyhigh Analytical Mechanics Associates Inc., Hampton, Virginia May 2018 NASA STI Program . in Profile Since its founding, NASA has been dedicated to the CONFERENCE PUBLICATION. advancement of aeronautics and space science. The Collected papers from scientific and technical NASA scientific and technical information (STI) conferences, symposia, seminars, or other program plays a key part in helping NASA maintain meetings sponsored or this important role. co-sponsored by NASA. The NASA STI program operates under the auspices SPECIAL PUBLICATION. Scientific, of the Agency Chief Information Officer. It collects, technical, or historical information from NASA organizes, provides for archiving, and disseminates programs, projects, and missions, often NASA’s STI. The NASA STI program provides access concerned with subjects having substantial to the NTRS Registered and its public interface, the public interest. NASA Technical Reports Server, thus providing one of the largest collections of aeronautical and space TECHNICAL TRANSLATION. science STI in the world. Results are published in both English-language translations of foreign non-NASA channels and by NASA in the
    [Show full text]
  • Security & Defence European
    a 7.90 D 14974 E D European & Security ES & Defence 10/2019 International Security and Defence Journal ISSN 1617-7983 • US Army Priorities • The US and NATO • European Combat Helicopter Acquisition • EU Defence Cooperation • Surface-to-Air Missile Developments www.euro-sd.com • • New Risks of Digitised Wars • Italy's Fleet Renewal Programme • Light Tactical Vehicles • UGVs for Combat Support • Defence Procurement in Denmark • Taiwan's Defence Market • Manned-Unmanned Teaming • European Mortar Industry October 2019 Politics · Armed Forces · Procurement · Technology LIFETIME EXCELLENCE At MTU Aero Engines, we always have your goals in mind. As a reliable partner for military engines, our expertise covers the entire engine lifecycle. And our tailored services guarantee the success of your missions. All systems go! www.mtu.de Militaer_E_210x297_European_Security_Defence_20191001_01.indd 1 17.09.19 08:06 Editorial Juncker’s Heritage The end of October marks the conclusion of the term of office of Jean-Claude Juncker as President of the European Commission. His legacy to his successor Ursula von der Leyen is largely a heap of dust and ashes. Five years ago he came to power with a fanfare for the future. The European Union was to be given a new burst of vitality, become closer to its citizens, at last put an end to its constant preoccupation with itself, and work towards solving the real problems of our times. None of these good intentions have been transformed into reality, not even notionally. Instead, the situation has become worse – a whole lot worse. This is due not least to the fact that the United Kingdom is on the verge of leaving the Euro- pean Union.
    [Show full text]
  • Standard Report Format
    Aircraft Accident Report Operator: Sita Air Pvt. Ltd. Aircraft Type and Model: Dornier 228-202(K) Registration: 9N-AHA Location: 420 m south-east of the threshold of Runway 02 at Tribhuvan International Airport, Kathmandu, Nepal N 27° 40’ 51.8” E 085° 21’ 22.6’ Date and Time: 28 September 2012 at 0033 hrs All times in this report are UTC Synopsis On 28 September 2012 at 0032 hrs, a Dornier 228-202(K) aircraft, registration 9N-AHA, took off from Runway 20 at Tribhuvan International Airport, Nepal for a flight to Tensing/Hillary Airport, Nepal. It climbed approximately 100 ft before flying level during which time the speed decayed to stalling speed. The aircraft stalled, departed controlled flight and crashed 420 m South-East of the threshold of Runway 02 at 0033 hrs. The impact was not survivable. The accident was notified to the International Civil Aviation Organization (ICAO), European Aviation Safety Agency (EASA), BFU Germany, RUAG Aerospace Services GmbH/RUAG Aviation, National Transportation Safety Board (NTSB), USA, Air Accidents Investigation Branch (AAIB), UK and Honeywell International Inc. on 28th September 2012 by Civil Aviation Authority of Nepal. The Government of Nepal constituted an Aircraft Accident Investigation Commission to determine the cause and the circumstances of the accident. The Commission determined that there was more drag on the aircraft during level flight than thrust from the engines and the aircraft decelerated to stall speed. The Commission was unable to determine the reason for the lack of thrust. Fifteen Safety Recommendations are made including three interim safety recommendations for the advancement of aviation safety.
    [Show full text]
  • Type Rating of an Aircraft, Compare the Aircraft Model from Block 2 of the Airworthiness Certificate to the Civil Model Designation Column Below
    FAA Order 8900.1, Volume 5, Chapter 2, Section 19 06/28/2021 FIGURE 5-88, PILOT CERTIFICATE AIRCRAFT TYPE DESIGNATIONS – AIRPLANE NOTE: 1. As of November 2015 the FAA has begun removing marketing names from the Civil Model Designation column. When determining the appropriate type rating of an aircraft, compare the aircraft model from Block 2 of the Airworthiness Certificate to the Civil Model Designation column below. The column titled Current Type Rating Designation will show the appropriate type rating for this aircraft. EQUIVALENT CURRENT TYPE TYPE CERTIFICATE CIVIL MODEL PRIOR MODEL MILITARY RATING HOLDER DESIGNATION DESIGNATION DESIGNATION DESIGNATION 328 Support Services GmbH Dornier 328-100 C-146A DO-328 Dornier 328-300 None D328JET Aero Commander Division (See Israel Aircraft Industries None Ltd.) Aérospatiale, France SN 601 Corvette None SN-601 Aérospatiale/Aeritalia, France (See ATR – GIE Avions de None Transport Régional) Airbus A340-200 Series: None A-340 Models: A340-211, -212, -213 A340-300 Series: Models: A340-311, -312, -313 A340-500 Series: Models: A340-541 A340-600 Series: Models: A340-642 Airbus Canada Limited BD-500-1A10 None BD500 Partnership BD-500-1A11 Airbus Defense and Space S.A. Model: C-212-CB, C-212-CC, None CA-212 C-212-CD, C-212-CE, C-212-CF, C-212-DF, C-212-DE Model CN-235, CN-235 CN-235 Series C-295 CN-235-100, CN-235-200, CN-235-300, C-295 Airbus SAS A300, Model B2-1A None A-300 A300, Model B2-1C A300, Model B4-2C A300, Model B2K-3C A300, Model B4-103 A300, Model B2-203 A300, Model B4-203 A300, Model B4-601
    [Show full text]
  • Aviation Week & Space Technology
    STARTS AFTER PAGE 36 20 Twenties Aerospace’s Has Aircraft Leasing Class of 2020 Perfect Storm Gone Too Far? ™ $14.95 MARCH 9-22, 2020 BOEING’S ATTACK CONTENDER Digital Edition Copyright Notice The content contained in this digital edition (“Digital Material”), as well as its selection and arrangement, is owned by Informa. and its affiliated companies, licensors, and suppliers, and is protected by their respective copyright, trademark and other proprietary rights. Upon payment of the subscription price, if applicable, you are hereby authorized to view, download, copy, and print Digital Material solely for your own personal, non-commercial use, provided that by doing any of the foregoing, you acknowledge that (i) you do not and will not acquire any ownership rights of any kind in the Digital Material or any portion thereof, (ii) you must preserve all copyright and other proprietary notices included in any downloaded Digital Material, and (iii) you must comply in all respects with the use restrictions set forth below and in the Informa Privacy Policy and the Informa Terms of Use (the “Use Restrictions”), each of which is hereby incorporated by reference. Any use not in accordance with, and any failure to comply fully with, the Use Restrictions is expressly prohibited by law, and may result in severe civil and criminal penalties. Violators will be prosecuted to the maximum possible extent. You may not modify, publish, license, transmit (including by way of email, facsimile or other electronic means), transfer, sell, reproduce (including by copying or posting on any network computer), create derivative works from, display, store, or in any way exploit, broadcast, disseminate or distribute, in any format or media of any kind, any of the Digital Material, in whole or in part, without the express prior written consent of Informa.
    [Show full text]
  • 8900.1 05/31/2012 Figure 5-88, Pilot Certificate Aircraft
    8900.1 05/31/2012 FIGURE 5-88, PILOT CERTIFICATE AIRCRAFT TYPE DESIGNATIONS - AIRPLANE MANUFACTURER MODEL PRIOR CURRENT DESIGNATION DESIGNATION DESIGNATION Aero Commander Division 1121 Jet Commander AC-1121 IA-JET (Also See North American Rockwell Commodore Jet 1123 CJ-1123 Corporation, USA) Aérospatiale, France SN 601 Corvette SN-601 Aérospatiale/Aeritalia, France ATR-42, ATR-72 ATR-42, ATR-72 Airbus (formerly known as Groupement A-300B Airbus A-300 d’Inerte Economique Airbus Industires, France) A-300-600R, A-310 Airbus A-310 A-319, A-320, A-321 Airbus A-320 A-330-200/300 Series A-330 A-340 200/300 Series Airbus A-340 A-380-800 A-380 Armstrong Whitworth Aircraft Co., Ltd., Argosy AW 650 Armstrong Whitworth AW-650 UK AW-650 Avions Dassault, General Aéronautique Falcon 7X DA-7X Marcel, Dassault, France Mystère 10 Falcon DA-10 Mystère 20 Falcon, Fan Jet GAMD/SUD-20 DA-20 Falcon 50-A, DA 900, DA-50 DA 900C, DA 900EX Fan Jet Model 200 DA-200 Falcon DA-2000, DA-2000 Dassault 2000EX DA-900DX, DA-EASY DA-900EX EASY DA-900LX DA-2000EX-EASY DA-2EASY Beech Aircraft Corporation, USA BE-200T/200TC, RC/FWC BE-200 BE-300, BE-B300, BE-300FF BE-300F BE-300 BE-300LW, BE-350, RC-12K, RC-12N, RC-12P, RC-12Q Diamond I, MU-300, MU-300 MU-300, BE-400 MU-300-10, BE-400, and 400T (USAF T-1A Jayhawk) BE-400-A BE-1900, BE-1900C, BE-1900 BE-1900D, C-12J (Military) BE-2000 Starship BE-2000 (SIC Required) BE-2000S Starship (Single Pilot) BE-2000S Boeing Co., USA B-17 Boeing B-17, B-B17 B-17 247-D Boeing 247 B-247 S-307, SA-307 Boeing 307 B-307 314 Boeing 314 B-314
    [Show full text]