CF6-80E1A3 CF6-80E1A4 CF6-80E1A4/B 2. Type Certificate Holder General Electric Company GE Aviation 1 Neumann Way Cincinnati, OH 45215-6301 USA 3. Manufacturer General Electric Company GE Aviation 1 Neumann Way Cincinnati, OH 45215-6310 USA 4. Date of Application Models Application Date (*) CF6-80E1A1 11 July 1991 CF6-80E1A2 …
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The proposed AD applies to GE CF6-80C2 and CF6-80E1 series turbofan engines with HPCR spool shaft stage 14 disks, P/N 1703M49G02, 1703M49G03, or 1509M71G10 installed. We published the proposed AD in the Federal Register on November 26, 2008 (73 FR 71949). That action proposed to require a one-time ECI of …
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The most popular engine model, the CF6-80C2, boasts the largest installed base of any widebody engine in history. Getting better and better Compared to the first CF6-6, …
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bracket P/N 2021M83G01, as previously recommended by CF6-80C2 S/B 73-0242. C. Compliance Category 2 GE recommends that you do this Alert Service Bulletin as soon as possible without effect on revenue service but before February 7, 2013. If CF6-80C2 S/B 73-0242 was previously incorporated, then this Alert Service Bulletin does not need to be
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One commenter states that the AD should clarify that if Middle River Aircraft Systems (MRAS) Service Bulletin (SB) No. CF6-80C2 S/B 78-1077 is incorporated, incorporating MRAS SB No. CF6-80C2 S/B 78-1068 is not necessary. Likewise, if MRAS SB No. CF6-80C2 S/B 78-1068 is incorporated, incorporating MRAS SB No. CF6-80C2 S/B …
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The CF6-6 was the first variant developed for the McDonnell Douglas DC-10-10 before the CF6-50 powering the -30 variant of the aircraft. 1982 saw the CF6-80A enter service with the Boeing 767 and Airbus A310 and a year after, it acquired ETOPS approval to fly longer ranges, with the CF6-80C2 then being developed for the Boeing 747-400 …
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(see CF6-80C2 maintenance analysis & budget, page 18). The CF6-80C2 is not generally removed due to exhaust gas temperature (EGT) margin erosion, but more due to technical deterioration. The original stage 1 HPT blade was a major example of the CF6-80C2 being prone to deterioration. The HPT upgrade programme used advanced materials and ...
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92453-11 CF6-80C2 79 CD Contents: GEK 92453-2KAC (Kuwait) GEK 92453-2UAE (Emirates) A310 CF6-80C2A2/A8 Power Plant Illustrated Parts Catalog 12/01/16 ** Book …
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In 2003, GE issued service bulletins for the CF6-80C2 and CF6-80E1series turbofan engines recommending repetitive visual inspection of the fuel manifolds at intervals of 4,500 flight-hours (FH). Despite these recommendations, five fuel leak events occurred in 2006; one resulting in an under-cowl fire on a CF6-80C2B6F turbofan engine.
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July 7, 2006. CINCINNATI, Ohio - CF6-80C2 engines powered the newly modernized Lockheed Martin C-5M Super Galaxy on its initial flight at Dobbins Air Reserve Base, Georgia, on June 19, launching an 18-month flight-test program that is expected to deliver enhanced airlift capability to the United States Air Force (USAF) in 2010. "We are proud …
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CF6-80C2 SERIES VARIANTS, THRUST RATING & APPLICATIONS Engine Thrust Aircraft Mature EGT variant rating (lbs) application margin - degrees C CF6-80C2A1 57,860 A300-600 35-50 CF6-80C2A2 52,460 A310-200/-300 38, up to 90 CF6-80C2A3 58,950 A300-600 25-45 CF6-80C2A5 60,100 A300-600R 25-45
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CF6-80C2 Service Bulletin 78-1133 entitled "EXHAUST - Fan Reverser – Identification Plate for Recording Service Bulletin Accomplishment" FAA AD FAA AD FAA AD For MRAS internal use: ECS 10-00709 J. Publications Affected CF6-80C2 Fan Reverser Illustrated Parts Catalog (IPC), MR 92464 K. Interchangeability
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CF6-80C2 . high-bypass turbofan engines . a low emissions combustor and advanced high pressure turbine, maximize customer value in the 21st century . The engine entered …
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The FAA reviewed GE CF6-80C2 Temporary Revision (TR) 05-0276, dated July 13, 2021 (GE TR 05-0276), and GE CF6-80C2 TR 05-0277, dated July 9, 2021 (GE TR 05-0277). GE TR 05-0276 and GE TR 05-277 provide the new life limit to be updated into the ALS, for the affected left-hand rear mount link assembly, in the existing engine …
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747s, 767s and MD-11s with CF6-80C2 and -80A engines. In the notices of proposed rule making (NPRMs), the FAA said that 747s and 767s have been involved in "several in-flight flame-out events," including four dual flameouts, and that MD-11s have been involved in six events, including two dual flameouts. All the events
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After the effective date of this AD, perform an ultrasonic inspection (UI) for cracks in HPT stage 1 and stage 2 disks on the CF6-80C2 turbofan engine and in HPT stage 2 disks on the CF6-80A turbofan engine at each piece-part level exposure in accordance with the Accomplishment Instructions, paragraph 3.A.(2), in GE CF6-80C2 SB 72-1562 …
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CF6-80E1A3 CF6-80E1A4 CF6-80E1A4/B 2. Type Certificate Holder General Electric Company GE Aviation 1 Neumann Way Cincinnati, OH 45215-6301 USA 3. Manufacturer General Electric Company GE Aviation 1 Neumann Way Cincinnati, OH 45215-6310 USA 4. Date of Application Models Application Date (*) CF6-80E1A1 11 July …
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This AD was prompted by an uncontained failure of an HPT stage 2 disk and the manufacturer's determination to expand the population of affected HPT disks. The FAA is issuing this AD to prevent failure of the HPT stage 1 disk (CF6-80C2 engines) and the HPT stage 2 disk (CF6-80C2 and CF6-80A Start Printed Page 63195 engines). The …
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CF6-80C2 5,200 lbs 2,359 kg CF6-80A CF6-50 Forward Pedestals AGSE P/N: AGSE-T016 Shipping Cover Protecting Engine on AM-1928 Stand Engine OEM P/N: 2C18024 Interchangeable Mounts PROTECTIVE COVERS Lasting defense against dirt, water, and contamination! PART NUMBER: ENGINE OEM ENGINE(S)
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capabilities for the CF6-80C2. Kelly Aviation Centre in Texas, for example, already has CF6-50 capability, and is now adding the -80C2. Design & upgrades The CF6-80C2 is a high reliability turbofan engine with a high-bypass ratio of 5.0-5.3:1. The single-stage fan is followed by a four-stage low pressure compressor (LPC) and 14-stage high
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Technical Manual Index – September 1, 2023 Page 1/1 Following is the CF6 Component Maintenance Manual Section and Appendix A of the Technical Manual Index. APPENDIX A reflects the BAE General Practices Manual sections; previously issued as CMM GEK 99373. Section copies are available by contacting aviation.fleetsupport@ge or from BAE at …
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CF6의 파생형으로 해군 함정용 가스 터빈 엔진인 LM2500이 있다. 오리지널 LM2500은 최대 약 33,600 마력의 힘을 발생시킬 수 있고 대략 36%의 열효율을 지니는데, 2기를 묶어서 COGAG 방식을 채택하는 경우가 많다. 최초 스프루언스급 구축함을 시작으로 미 해군 의 각종 ...
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CF6-80C2 Engine. The CF6-80C2 is certified on several widebody aircraft models, and Delta TechOps has serviced these engines since 1982. Services. Modification, repair and overhaul. Full Restoration/Overhaul …
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Pre-CF6-80C2 S/B 73-0253 (non PTFE taped drained fuel manifold): (1) Engines with used clamps installed at the last inspection or overhaul, inspect the manifold and replace the clamps within 4,500 hours since the last inspection or overhaul using paragraph 3.B., ACCOMPLISHMENT INSTRUCTIONS.
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CF6-80C2 Boeing Service Bulletins (SBs) SB 72-1562 R03 ENGINE - General (72-00-00) - CF6-80C2 Stage 1 and Stage 2 HPTR Disk Ultrasonic Inspection Date Printed: 2018/08/02 GE PROPRIETARY INFORMATION - Not to be used, disclosed to others or reproduced without the express written consent of GE. Technical data is considered ITAR and/or …
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