DOCSLIB.ORG

Airworthiness Directives; Airbus Dated September 12, 2013

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
Airworthiness Directives; Airbus Dated September 12, 2013 Federal Register / Vol. 78, No. 220 / Thursday, November 14, 2013 / Rules and Regulations 68347 PART 39—AIRWORTHINESS in accordance with Part 2 of the (j) Related Information DIRECTIVES Accomplishment Instructions of Boeing Alert For more information about this AD, Service Bulletin 747–57A2343, dated contact Nathan Weigand, Aerospace ■ 1. The authority citation for part 39 September 12, 2013. If any cylindrical defect Engineer, Airframe Branch, ANM–120S, continues to read as follows: is found, before further flight, do the actions FAA, Seattle Aircraft Certification Office, specified in paragraph (h)(1)(i) or (h)(1)(ii) of 1601 Lind Avenue SW., Renton, WA 98057– this AD. Authority: 49 U.S.C. 106(g), 40113, 44701. 3356; phone: 425–917–6428; fax: 425–917– (i) Do a minimum thickness inspection of 6590; email: [email protected]. § 39.13 [Amended] the inboard actuator attach fitting to determine minimum wall thickness of the (k) Material Incorporated by Reference ■ 2. The FAA amends § 39.13 by adding actuator fitting assembly, in accordance with (1) The Director of the Federal Register the following new airworthiness Part 3 of the Accomplishment Instructions of approved the incorporation by reference directive (AD): Boeing Alert Service Bulletin 747–57A2343, (IBR) of the service information listed in this dated September 12, 2013. If the minimum 2013–23–03 The Boeing Company: paragraph under 5 U.S.C. 552(a) and 1 CFR thickness of the wall is less than 0.130 inch: Amendment 39–17658; Docket No. part 51. Before further flight, replace the inboard FAA–2013–0871; Directorate Identifier actuator attach fitting of the outboard flap, in (2) You must use this service information 2013–NM–187–AD. accordance with Part 4 of the as applicable to do the actions required by this AD, unless the AD specifies otherwise. (a) Effective Date Accomplishment Instructions of Boeing Alert (i) Boeing Alert Service Bulletin 747– This AD is effective November 29, 2013. Service Bulletin 747 57A2343, dated September 12, 2013. 57A2343, dated September 12, 2013. (b) Affected ADs (ii) Replace the inboard actuator attach (ii) Reserved. (3) For service information identified in None. fitting of the outboard flap, in accordance with Part 4 of the Accomplishment this AD, contact Boeing Commercial (c) Applicability Instructions of Boeing Alert Service Bulletin Airplanes, Attention: Data & Services Management, P.O. Box 3707, MC 2H–65, This AD applies to The Boeing Company 747–57A2343, dated September 12, 2013. Seattle, WA 98124–2207; telephone 206– Model 747–100, 747–100B, 747–100B SUD, (2) Replace the inboard actuator attach 544–5000, extension 1; fax 206–766–5680; 747–200B, 747–200C, 747–200F, 747–300, fitting of the outboard flap, in accordance Internet https://www.myboeingfleet.com. 747–400, 747–400D, 747–400F, and 747SR with Part 4 of the Accomplishment (4) You may review copies of the series airplanes, certificated in any category, Instructions of Boeing Alert Service Bulletin referenced service information at the FAA, as identified in Boeing Alert Service Bulletin 747–57A2343, dated September 12, 2013. 747–57A2343, dated September 12, 2013. Transport Airplane Directorate, 1601 Lind (i) Alternative Methods of Compliance Avenue SW., Renton, Washington. For (d) Subject (AMOCs) information on the availability of this Joint Aircraft System Component (JASC)/ (1) The Manager, Seattle Aircraft material at the FAA, call 425–227–1221. Air Transport Association (ATA) of America Certification Office (ACO), FAA, has the (5) You may view this service information Code 57, Wings. authority to approve AMOCs for this AD, if that is incorporated by reference at the requested using the procedures found in 14 National Archives and Records (e) Unsafe Condition CFR 39.19. In accordance with 14 CFR 39.19, Administration (NARA). For information on This AD was prompted by a report of the send your request to your principal inspector the availability of this material at NARA, call fracture of an inboard actuator attach fitting or local Flight Standards District Office, as 202–741–6030, or go to: http:// of the outboard flap. An inspection of the appropriate. If sending information directly www.archives.gov/federal-register/cfr/ibr- attach fitting revealed that it was incorrectly to the manager of the ACO, send it to the locations.html. attention of the person identified in machined with a cylindrical profile instead Issued in Renton, Washington, on October paragraph (j) of this AD. Information may be of a conical profile, resulting in reduced wall 31, 2013. thickness. We are issuing this AD to detect emailed to: 9-ANM-Seattle-ACO-AMOC- and correct defective inboard actuator attach [email protected]. Jeffrey E. Duven, fittings which, combined with loss of the (2) Before using any approved AMOC, Acting Manager, Transport Airplane outboard actuator load path, could result in notify your appropriate principal inspector, Directorate, Aircraft Certification Service. uncontrolled retraction of the outboard flap, or lacking a principal inspector, the manager [FR Doc. 2013–27015 Filed 11–13–13; 8:45 am] of the local flight standards district office/ damage to flight control systems, and BILLING CODE 4910–13–P consequent reduced controllability of the certificate holding district office. airplane. (3) An AMOC that provides an acceptable level of safety may be used for any repair (f) Compliance required by this AD if it is approved by the DEPARTMENT OF TRANSPORTATION Comply with this AD within the Boeing Commercial Airplanes Organization compliance times specified, unless already Designation Authorization (ODA) that has Federal Aviation Administration done. been authorized by the Manager, Seattle ACO, to make those findings. For a repair 14 CFR Part 39 (g) Part Number Inspection method to be approved, the repair must meet Within 90 days after the effective date of the certification basis of the airplane, and the [Docket No. FAA–2013–0329; Directorate this AD: Inspect to determine the part approval must specifically refer to this AD. Identifier 2012–NM–032–AD; Amendment number of the inboard actuator attach fittings (4) If the service information contains steps 39–17596; AD 2013–19–14] of the outboard flaps, in accordance with Part that are labeled as RC (Required for RIN 2120–AA64 1 of the Accomplishment Instructions of Compliance), those steps must be done to Boeing Alert Service Bulletin 747–57A2343, comply with this AD; any steps that are not Airworthiness Directives; Airbus dated September 12, 2013. labeled as RC are recommended. Those steps Airplanes that are not labeled as RC may be deviated (h) Actions for Certain Attach Fittings from, done as part of other actions, or done AGENCY: Federal Aviation If, during the inspection required by using accepted methods different from those Administration (FAA), Department of paragraph (g) of this AD, any inboard identified in the specified service Transportation (DOT). actuator attach fitting having part number information without obtaining approval of an (P/N) 65B08564–7 is found, before further AMOC, provided the steps labeled as RC can ACTION: Final rule. flight, do the actions specified in paragraph be done and the airplane can be put back in (h)(1) or (h)(2) of this AD. a serviceable condition. Any substitutions or SUMMARY: We are superseding (1) Do a detailed inspection of the inboard changes to steps labeled as RC require Airworthiness Directives (ADs) 2009– actuator attach fitting for a cylindrical defect, approval of an AMOC. 04–07 and 2011–02–09 for certain VerDate Mar<15>2010 15:50 Nov 13, 2013 Jkt 232001 PO 00000 Frm 00021 Fmt 4700 Sfmt 4700 E:\FR\FM\14NOR1.SGM 14NOR1 TKELleY on DSK3SPTVN1PROD with RULES 68348 Federal Register / Vol. 78, No. 220 / Thursday, November 14, 2013 / Rules and Regulations Airbus Model A330–200, A330–200 1601 Lind Avenue SW., Renton, [with mechanical rudder], through Airbus Freighter, A300–300, A340–200, A340– Washington 98057–3356; telephone SB A330–27–3177, 300, A340–500, and A340–600 series 425–227–1138; fax 425–227–1149. —software standard L22A on FCPC 2K1 hardware and L22A on FCPC 2K0 airplanes. AD 2009–04–07 required SUPPLEMENTARY INFORMATION: revising the airplane flight manual hardware for A340–200/–300 aeroplanes Discussion [with mechanical rudder], through Airbus (AFM) to include appropriate SB A340–27–4174, and operational procedures to prevent the We issued a notice of proposed — software standard L21A on FCPC 2K2 air data inertial reference unit (ADIRU) rulemaking (NPRM) to amend 14 CFR hardware for A340–300 aeroplanes [with from providing erroneous data to other part 39 by adding an AD that would electrical rudder], through Airbus SB airplane systems. AD 2011–02–09 apply to the specified products. The A340–27–4162. required revising the AFM to provide NPRM was published in the Federal * * * * * appropriate operational procedures to Register on April 16, 2013 (78 FR EASA has also issued MCAI 2013– prevent the airplane flight directors 22432), and proposed to supersede AD 0107, dated May 17, 2013, which states: (FDs), autopilot (AP), and auto-thrust re- 2009–04–07, Amendment 39–15813 (74 An A330 aeroplane experienced a sudden engagement in the event of airspeed FR 7549, February 18, 2009); and AD nose down movement while in cruise. This sources providing similar but erroneous 2011–02–09, Amendment 39–16583 (76 event was preceded by an automatic data. This new AD requires that FR 4219, January 25, 2011). The NPRM autopilot disconnection, which triggered the operators modify or replace all three proposed to correct an unsafe condition ‘‘NAV IR1 FAULT’’ Electronic Centralised flight control primary computers for the specified products. Aircraft Monitor (ECAM) Caution. (FCPCs) with new software standards. The European Aviation Safety Agency Investigation results highlighted that at the Since we issued ADs 2009–04–07 and (EASA), which is the Technical Agent time of the event, the Air Data Reference 1 2011–02–09, we have determined that for the Member States of the European (ADR) part of ADIRU1 was providing Community, has issued EASA AD 2011– erroneous and temporary wrong parameters new software standards for the FCPCs in a random manner.
Load more

Recommended publications
  • Facts & Figures & Figures
    OCTOBER 2019 FACTS & FIGURES & FIGURES THE STAR ALLIANCE NETWORK RADAR The Star Alliance network was created in 1997 to better meet the needs of the frequent international traveller. MANAGEMENT INFORMATION Combined Total of the current Star Alliance member airlines: FOR ALLIANCE EXECUTIVES Total revenue: 179.04 BUSD Revenue Passenger 1,739,41 bn Km: Daily departures: More than Annual Passengers: 762,27 m 19,000 Countries served: 195 Number of employees: 431,500 Airports served: Over 1,300 Fleet: 5,013 Lounges: More than 1,000 MEMBER AIRLINES Aegean Airlines is Greece’s largest airline providing at its inception in 1999 until today, full service, premium quality short and medium haul services. In 2013, AEGEAN acquired Olympic Air and through the synergies obtained, network, fleet and passenger numbers expanded fast. The Group welcomed 14m passengers onboard its flights in 2018. The Company has been honored with the Skytrax World Airline award, as the best European regional airline in 2018. This was the 9th time AEGEAN received the relevant award. Among other distinctions, AEGEAN captured the 5th place, in the world's 20 best airlines list (outside the U.S.) in 2018 Readers' Choice Awards survey of Condé Nast Traveler. In June 2018 AEGEAN signed a Purchase Agreement with Airbus, for the order of up to 42 new generation aircraft of the 1 MAY 2019 FACTS & FIGURES A320neo family and plans to place additional orders with lessors for up to 20 new A/C of the A320neo family. For more information please visit www.aegeanair.com. Total revenue: USD 1.10 bn Revenue Passenger Km: 11.92 m Daily departures: 139 Annual Passengers: 7.19 m Countries served: 44 Number of employees: 2,498 Airports served: 134 Joined Star Alliance: June 2010 Fleet size: 49 Aircraft Types: A321 – 200, A320 – 200, A319 – 200 Hub Airport: Athens Airport bases: Thessaloniki, Heraklion, Rhodes, Kalamata, Chania, Larnaka Current as of: 14 MAY 19 Air Canada is Canada's largest domestic and international airline serving nearly 220 airports on six continents.
    [Show full text]
  • Airbus A340-300 Technical Specifications
    Technical Specifications Airbus A340-300 AIRCRAFT ZS-SXD (0643) TECHNICAL SPECIFICATION AIRCRAFT Aircraft Type: A340-300 Current Registration: ZS -SXD TT : 63319 As of : 2019-09-30 Serial No: 0643 Date of Manufacture: 25 November 2004 TC : 7935 ENGINE Manufacturer: CFM Model : CFM56=5C4/P International Thrust Rating Engine 1 Engine 2 Engine 3 Engine 4 Serial Number: 567278 567276 567277 567279 56000 lbs (249KN) TT: FH 57016 56317 54787 58026 FC 7134 7060 6944 7385 AS OF 2019-09-30 WEIGHTS AND FUEL Weights Pounds Kilograms Maximum Taxi Weight 608 248 lbs. 275000 kg Maximum Take-Off Weight 606 264 lbs. 275000 kg Maximum Landing Weight 423 287 lbs. 192000 kg Maximum Zero Fuel Weight 396 823 lbs. 180000 kg LANDING GEAR Nose Centre Main LH Wing Main RH Wing Part Number D23581100-20 37100-1001 201490001 201490002 Serial Number B558 DCL331/03 MDL582 MDL582 Status As Of 2019-09-30 2017-12-31 2017-12-31 2017-12-31 Next O/H Date 2024-11-22 2024-11-22 2024-11-22 2024-11-22 WHEELS Nose Centre Main LH Wing Main RH Wing Vendor Goodrich Honeywell Honeywell Honeywell Part Number 3-1596 2612201-3 2612201-3 2612201-3 BRAKES Vendor N/A N/A Honeywell Honeywell Part Number N/A N/A 2612202-4 2612202-4 TYRES Vendor Bridgestone Bridgestone Bridgestone Bridgestone Part Number APR06500 APR06911 APR06911 APR06911 APU Manufacturer: Honeywell Total Time (TT) : FH =16563 FC = 12212 Type /Model : 3800454-6 AS OF 2019-09-30 Serial number : P791 INTERIOR CONFIGURATION Passengers J/C=38 Y/C=215 Total=253 Galleys 9 Lavatories 9 Refer to the attached LOPA and Equipment
    [Show full text]
  • Transatlantic Airline Fuel Efficiency Ranking, 2017
    WHITE PAPER SEPTEMBER 2018 TRANSATLANTIC AIRLINE FUEL EFFICIENCY RANKING, 2017 Brandon Graver, Ph.D., and Daniel Rutherford, Ph.D. www.theicct.org [email protected] BEIJING | BERLIN | BRUSSELS | SAN FRANCISCO | WASHINGTON ACKNOWLEDGMENTS The authors thank Tim Johnson, Andrew Murphy, Anastasia Kharina, and Amy Smorodin for their review and support. We also acknowledge Airline Data Inc. for providing processed BTS data, and FlightGlobal for Ascend Fleet data. International Council on Clean Transportation 1225 I Street NW Suite 900 Washington, DC 20005 USA [email protected] | www.theicct.org | @TheICCT © 2018 International Council on Clean Transportation TRANSATLANTIC AIRLINE FUEL EFFICIENCY RANKING, 2017 TABLE OF CONTENTS EXECUTIVE SUMMARY ............................................................................................................ iii 1. INTRODUCTION .................................................................................................................... 2 2. METHODOLOGY ................................................................................................................... 3 2.1 Airline selection .................................................................................................................................3 2.2 Fuel burn modeling..........................................................................................................................5 2.3 Fuel efficiency calculation ............................................................................................................6
    [Show full text]
  • Fast 49 Airbus Technical Magazine Worthiness Fast 49 January 2012 4049July 2007
    JANUARY 2012 FLIGHT AIRWORTHINESS SUPPORT 49 TECHNOLOGY FAST AIRBUS TECHNICAL MAGAZINE FAST 49 FAST JANUARY 2012 4049JULY 2007 FLIGHT AIRWORTHINESS SUPPORT TECHNOLOGY Customer Services Events Spare part commonality Ensuring A320neo series commonality 2 with the existing A320 Family AIRBUS TECHNICAL MAGAZINE Andrew James MASON Publisher: Bruno PIQUET Graham JACKSON Editor: Lucas BLUMENFELD Page layout: Quat’coul Biomimicry Cover: Radio Altimeters When aircraft designers learn from nature 8 Picture from Hervé GOUSSE ExM Company Denis DARRACQ Authorization for reprint of FAST Magazine articles should be requested from the editor at the FAST Magazine e-mail address given below Radio Altimeter systems Customer Services Communications 15 Tel: +33 (0)5 61 93 43 88 Correct maintenance practices Fax: +33 (0)5 61 93 47 73 Sandra PREVOT e-mail: [email protected] Printer: Amadio Ian GOODWIN FAST Magazine may be read on Internet http://www.airbus.com/support/publications ELISE Consulting Services under ‘Quick references’ ILS advanced simulation technology 23 ISSN 1293-5476 Laurent EVAIN © AIRBUS S.A.S. 2012. AN EADS COMPANY Jean-Paul GENOTTIN All rights reserved. Proprietary document Bruno GUTIERRES By taking delivery of this Magazine (hereafter “Magazine”), you accept on behalf of your company to comply with the following. No other property rights are granted by the delivery of this Magazine than the right to read it, for the sole purpose of information. The ‘Clean Sky’ initiative This Magazine, its content, illustrations and photos shall not be modified nor Setting the tone 30 reproduced without prior written consent of Airbus S.A.S. This Magazine and the materials it contains shall not, in whole or in part, be sold, rented, or licensed to any Axel KREIN third party subject to payment or not.
    [Show full text]
  • A STUDY of AIRBUS A380 (A3XX) by Serhat Hosder
    A STUDY of AIRBUS A380 (A3XX) by Serhat Hosder Figure source: Ref 3 March 22, 2001 AOE 4984 Configuration Aerodynamics Project 1 1 AOE 4984 Configuration Aerodynamics Project #1 Project title: A study of Airbus A380 (A3XX) Presented by: Serhat Hosder Course Instructor: Dr. W. A. Mason Presentation Date: March 22, 2001 Department of Aerospace and Ocean Engineering Virginia Tech, Blacksburg, VA. 1 AIRBUS A380-100 Figure source: Ref 3 • BIGGEST AIRLINER EVER DESIGNED • FIRST CIVIL TRANSPORT WITH THREE DECKS • NEW TECHNOLOGIES March 22, 2001 AOE 4984 Configuration Aerodynamics Project 1 2 Airbus A380 is the biggest airliner ever designed. It will become the first full- triple decked large-body, long-range civil transport. Despite its large size, basic configuration of A380 is similar to a typical civil transport. Because of the customer imposed constraints, A380 is designed to fulfill current airport gate and runway requirements (80 m gatebox limitation). In the case of A380-100 (baseline configuration), the customers asked for direct operating costs 15% below current 747-400. Since A380 is a unique design, the production of the airplane depends on the improvements and new technologies in aerodynamics, structures, avionics, material science and system integration. 2 Motivation for the Development of A380 • World Air Traffic will double in 15 years and nearly triple in 20 years • First B-747 in 1970 – Turbofan powered – more than twice the size of its Figure source: Ref 7 predecessors MODELS – Since then no significant -50R ……...Shortened
    [Show full text]
  • Airbus A320 Family Equipment Catalogue Incl
    AIRBUS A320 EQUIPMENT CATALOGUE EQUIPMENT A320 AIRBUS | HYDRO AIRBUS A320 FAMILY EQUIPMENT CATALOGUE INCL. NEO 5 HYDRO | Airbus A320 Equipment HYDRO | Airbus A320 Equipment 6 1 _INDEX 12 9.4 TEST EQUIPMENT FOR RAM-AIR TURBINE 111 9.5 RAT SAFETY INTERFACE KIT 113 2 _EQUIPMENT LIST 16 9.6 TEST EQUIPMENT FOR RAM-AIR TURBINE 114 3 _DIMENSIONS & AREAS 23 10 _LANDING GEAR (ATA CHAPTER 32) 117 3.1 AIRCRAFT MAINTENANCE ACCESS STAND 24 10.1 WHEEL AND BRAKE CHANGE EQUIPMENT (UNIVERSAL) 118 3.2 MULTI-PURPOSE PLATFORM 26 10.2 WHEEL AND BRAKE CHANGE EQUIPMENT 120 4 _LIFTING & SHORING (ATA CHAPTER 07) 29 10.3 LANDING GEAR TRANSPORTATION TROLLEY 122 4.1 FORTEVO TRIPOD-JACKS 30 10.4 MAIN LANDING GEAR INSTALLATION TROLLEY 123 4.2 SMARTLINE TRIPOD-JACKS 46 10.5 MLG COMPRESSION TOOL 125 4.3 SHORING STANCHION 50 10.6 LANDING GEAR ACCESS STAND 126 4.4 AXLE-JACK / STANDARD AXLE-JACK (RT) 52 10.7 AIRCRAFT WHEEL CHOCKS 128 4.5 AXLE-JACK / UNIVERSAL AXLE-JACK (RC) 56 10.8 AIRCRAFT STRUT AND ACCUMULATOR SERVICE TOOL 129 4.6 AXLE-JACK / FLY-AWAY AXLE-JACK (RH) 58 10.9 AIRCRAFT WHEEL AND TYRE HANDLING 130 4.7 AXLE-JACK / RECOVERY AXLE-JACK (RL) 60 11 _WASTE LINE CLEANING (ATA CHAPTER 38) 132 4.8 RECOVERY AXLE-JACK BEAM 62 11.1 WASTE LINE CLEANING 134 4.9 AXLE-JACK HOSE PRESSURE KIT 64 11.2 MOBILE LAVATORY VACUUM BLOCKAGE REMOVER 137 4.10 STEERING TEST EQUIPMENT 65 11.3 WASTE WATER TRAILER FOR WLC1 139 5 _TOWING AND TAXING (ATA CHAPTER 09) 66 12 _FUSELAGE (ATA CHAPTER 53) 140 5.1 TOW-BAR (STANDARD) 68 12.1 IGLOOMX FUSELAGE SHELTER 142 5.2 TOW-BAR (UNIVERSAL) 70 12.2
    [Show full text]
  • Titel Der Präsentation
    Lufthansa Group Conference & Roadshow Presentation March / April 2016 Disclaimer in respect of forward-looking statements Information published in this presentation concerning the future development of the Lufthansa Group and its subsidiaries consists purely of forecasts and assessments and not of definitive historical facts. These forward-looking statements are based on all discernible information, facts and expectations available at the time. They can, therefore, only claim validity up to the date of their publication. Since forward-looking statements are by their nature subject to uncertainties and imponderable risk factors – such as changes in underlying economic conditions – and rest on assumptions that may not occur, or may occur differently, it is possible that the Group’s actual results and development may differ materially from the forecasts. Lufthansa makes a point of checking and updating the information it publishes. However, the Company is under no obligation to update forward-looking statements or adapt them to subsequent events or developments. Accordingly, it neither explicitly nor implicitly accepts liability, nor gives any guarantee for the actuality, accuracy or completeness of this data and information. Page 2 The Lufthansa Group is based on three strong pillars - Synergetic portfolio of premium hub airlines, profitably growing P2P airlines and high margin aviation services - New organizational structure to create efficiencies and to help implementing seven fields of action The Lufthansa Group benefits from a sound financial setup - Strong balance sheet, investment grade rating, sustainable free cash flow generation - Clear and consistent dividend policy with industry leading pay-out ratio The Lufthansa Group has good FY15 results - Passenger airlines drive results improvement; improvements at MRO and Catering; Logistics below PY - Adj.
    [Show full text]
  • Airbus A340-300 9H JAI
    Airbus A340-300 9HJAI Max Volume Max Cargo Range Capacity Capacity 12.700 km 253 m³ 51.300 kg A340-300 9HJAI CARGO CAPACITY 02 VOLUME (m) MAX WEIGHT kg UPPER DECK 114 20.540 LOWER DECK 139 44.836 TOTAL 253 51.300* * Aircraft Maximum Structural Payload A340-300 9HJAI UPPER DECK 03 Upper Deck Section OM33 OM31 OL29 OL27 OL25 OL23 OL21 OL19 OL17 OL15 OL13 OL11 CM10 CM9 CL8 CL7 CL6 CL5 CL4 CL3 CL2 CL1 OM34 OM32 OL30 OL28 OL26 OL24 OL22 OL20 OL18 OL16 OL14 OL12 Cargo Crew Class 1 Compartment Crew Rest AVAILABLE VOLUME OHSC* FLOOR TOTAL 14 m 100 m 114 m * Overhead Stowage Compartment A340-300 9HJAI UPPER DECK SECTION 04 OHSC* LATERAL OHSC* CENTRAL OPTIMIZED BOX SIZE OHSC* LATERAL OHSC* CENTRAL FLOOR B 200 mm A 300 mm B 200 mm A 300 mm B 200 mm C 500 mm 400 mm 270 mm 400 mm 270 mm 400 mm 270 mm 400 mm 400 mm 400 mm 400 mm 520 mm 420 mm Max weight/box = 12 kg Max weight/box = 17 kg Maximum weight of each compartment/zone might limit the number of boxes or weight per box. * Overhead Stowage Compartment A340-300 9HJAI LOWER DECK 05 BULK AFT COMP. FWD COMP. Lower Deck Section BULK PAG PAG PMC PMC PMC PMC PMC PMC PMC PMC PMC FWD COMP. AFT COMP. BULK TOTAL CARGO 6 PMC (66 m) 3 PMC + 2 PAG (53 m) 20 m 139 m DISCLAIMER The volume mentioned in this document for the dierent areas and compartments are for illustration purposes only and do not constitute any kind of guarantee or covenant that such volume can be used in full.
    [Show full text]
  • The Strategic Deployment of the Airbus A350-900XWB Aircraft in a Full-Service Network Carrier Route Network: the Case of Singapore Airlines
    infrastructures Article The Strategic Deployment of the Airbus A350-900XWB Aircraft in a Full-Service Network Carrier Route Network: The Case of Singapore Airlines Glenn Baxter ID and Panarat Srisaeng * ID School of Tourism and Hospitality Management, Suan Dusit University, Hua Hin, Prachaup Khiri Khan 77110, Thailand; [email protected] * Correspondence: [email protected]; Tel.: +66-32-522-508 Received: 7 June 2018; Accepted: 17 July 2018; Published: 19 July 2018 Abstract: In the global airline industry, an airline’s fleet routing affects its profitability, level of service and its competitive position. Using a qualitative research approach, this paper examines Singapore Airlines Airbus A350-900XWB fleet deployment and route network development for the period 2016 to 2018. The qualitative data was examined using document analysis. The study found that Singapore Airlines has deployed the Airbus A350-900XWB aircraft on new air routes from Singapore to Cape Town via Johannesburg, Düsseldorf and Stockholm via Moscow and return. The Airbus A350-900XWB aircraft are also replacing older, less efficient aircraft as part of the company’s fleet modernization strategy. Singapore Airlines is also acquiring the new ultra-long-range variant of the Airbus A350-900XWB for use on its proposed new non-stop services from Singapore to Los Angeles and Newark Liberty Airport in New Jersey, USA. The longest flight stage length is the Singapore to San Francisco route which is 7339 nautical miles (13,594 km) in length. The shortest stage length is between Singapore and Kuala Lumpur (160 nautical miles or 297 km). The new non-stop services from Singapore to Los Angeles and New York City will be the longest non-stop services operated by Singapore Airlines.
    [Show full text]
  • Temporary Denial Order to Add Additional Respondents
    UNITED STATES DEPARTMENT OF COMMERCE BUREAU OF INDUSTRY AND SECURITY WASHINGTON, D.C. 20230 ) Mahan Airways ) Mahan Tower ) No. 21, Azadegan St. ) M.A. Jenah Exp. Way ) Tehran, Iran ) ) Pejman Mahmood Kosarayanifard ) aJk/a Kosarian Fard ) P.O. Box 52404 ) Dubai, United Arab Emirates; ) ) Mahmoud Amini ) G#22 Dubai Airport Free Zone ) P.O. Box 393754 ) Dubai, United Arab Emirates ) ) and ) ) P.O. Box 52404 ) Dubai, United Arab Emirates ) ) and ) ) Mohamed Abdulla Alqaz Building ) Al Maktoum Street ) Al Rigga ) Dubai, United Arab Emirates; ) ) Kerman Aviation ) aJk/a GIE Kerman Aviation ) 42 Avenue Montaigne 75008 ) Paris, France ) ) Sirjanco Trading LLC ) P.O. Box 8709 ) Dubai, United Arab Emirates ) ) Mahan Airways, et al. Modification of January 16,2015 TDO Renewal Order Page 2 of 15 Ali Eslamian ) 4thFloor ) 33 Cavendish Square ) London,VVIGOPVV ) United Kingdom ) ) and ) ) 2 Bentinck Close ) Prince Albert Road St. Johns Wood ) London NVV87RY ) United Kingdom ) ) Mahan Air General Trading LLC ) 19thFloor Al Moosa Tower One ) Sheik Zayed Road ) Dubai40594 ) United Arab Emirates ) ) Skyco (UK) Ltd. ) 4thFloor, 33 Cavendish Square ) London, VVIG OPV ) United Kingdom ) ) Equipco (UK) Ltd. ) 2 Bentinck Close ) Prince Albert Road ) London, NVV87RY ) United Kingdom ) ) Mehdi Bahrami ) Mahan Airways- Istanbul Office ) Cumhuriye Cad. Sibil Apt No: 101 D:6 ) 34374 Emadad, Sisli Istanbul ) Turkey ) ) Mahan Airways, et al. Modification of January 16, 20 I5 TDO Renewal Order Page 3 of 15 AI Naser Airlines ) a1k/a ai-Naser Airlines ) a1k/a Alnaser Airlines and ) Air Freight Ltd. ) Home 46 ) Al-Karrada, Babil Region, ) District 929, St 21 ) Beside Al Jadirya Private Hospital ) Baghdad, Iraq ) ) and ) ) Al Amirat Street, ) Section 309, St.
    [Show full text]
  • Aviation Profiles and Cases
    Ashfords has unique air accident claims and aviation expertise - AVIATION specialist lawyers have represented the victims of air accidents PROFILES AND dating back to 1977. The Aviation Team is dedicated to representing injured victims CASES and families who have lost loved ones as a result of aviation accidents around the world. The head of the Aviation Team is Jim Morris, a RAF pilot for 12 years before qualifying as a barrister to specialise in air accident litigation. The Team’s class leading expertise means that Ashfords has the resources and ability to act in all types of air accidents, from single engine pleasure flights to major airline disasters and acts of terrorism. Ashfords LLP ashfords.co.uk THE AVIATION TEAM Jim Morris Stephen Walker Partner & Barrister Legal Director Head of the Aviation Team [email protected] [email protected] Mobile +44 (0)7974 244769 Mobile +44 (0)7850 506057 Jim specialises in representing the victims of Stephen is a Legal Director in the Aviation Team. He has international air accidents. He was a professionally dealt with a wide range of civil litigation matters over the qualified Royal Air Force pilot prior to becoming an past 28 years. He advises private individuals, sole traders aviation lawyer, and has over 26 years’ experience in and small/medium enterprises in relation to civil litigation aviation and litigation. matters including misrepresentation/ estoppel, breach of contract, defamation, debt recovery, professional During Jim’s 12 years as a pilot, he was qualified on a negligence and high value personal injury cases. number of military aircraft (single piston, single turbo prop, fast jet, twin turbo prop, heavy jet) and his last Prior to joining Ashfords, Stephen worked for the TSB flying tour was on the Boeing E-3D AWACS.
    [Show full text]
  • Development of Trent Series Large Turbo Fan Engines
    Technical Description Development of Trent Series Large Turbo Fan Engines As the demand for aircraft has been increasing, fuel efficiency needs to be improved. Therefore, the performance of the engine as well as the fuselage must be enhanced. We are in charge of design, part manufacturing and module assembly of the intermediate pressure compressor (IPC) at development of all the Trent Series large turbo fan engines from Rolls-Royce after the Trent 1000, the first model of which helped develop in 2004, as their strategic partner. Going forward, we will promote activities to take charge of the overall IPC module as an IPC module integrator by developing ©Rolls-Royce plc proprietary design and manufacturing technologies. Introduction Aircraft are an essential means of transportation in To be launched in 2018 global society, and aircraft manufacturers are competing Trent 7000 Thrust: to develop new types of aircraft. Engines equipping such 68,000-72,000lb Airbus A330neo aircraft must be highly reliable, lightweight and fuel efficient, as well as environmentally friendly (low NOx, low Trent XWB noise). Thrust: 84,000-97,000lb Airbus A350 XWB 1 Background Trent 1000 The demand for aircraft is expected to grow by about Thrust: 53,000-74,000lb 5% annually even in the long term, pushed by factors Boeing 787 such as the rapid expansion of Low-Cost Carriers (LCCs). To meet such market needs, The Boeing Company in the Trent 900 US and Airbus in Europe are developing new types of Thrust: 80,000lb aircraft. Rolls-Royce plc (Rolls-Royce) in the UK, one of the Airbus A380 world's major aircraft engine manufacturers, has been developing and supplying its Trent series for such aircraft, Trent 500 Thrust: and we are participating in programs to manufacture the 60,000lb series as a Risk- and Revenue-Sharing Partner (RRSP).
    [Show full text]