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SUPPLEMENTARY INFORMATION: A proposal to amend part 39 of the Federal Aviation Regulations (14 CFR part 39) to include an AD that is applicable to General Electric Company CF6-50 and CF6-80C2 turbofan engines was published in the Federal Register on May 17, 2001 (66 FR 27475).That action proposed to require replacement of certain existing CF6 …
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CF6-80C2 Military Applications adminavalon T13:25:20+00:00 CF6-80C2 Military Applications Nacelle MRO Capabilities MRAS, a division of ST Engineering operates a 100,000 sq. ft. state-of-the-art maintenance, repair, and overhaul (MRO) with extensive capabilities and leverages our over 95 years of history including composite materials ...
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The CF6-80C2 engine evolved from the CF6-80A engine and particularly for the Boeing 767 aircraft it is a very common choice. The Boeing 767 has itself been powered by many engines including the Rolls Royce …
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CF6 -- 80C2. 79 -- 00. ATA -- 79 OIL SYSTEM. TABLE OF CONTENT. General Oil System 002 Oil Storage 004 Oil Servicing 006 Oil Distribution 008 Lub and Scavange Pump 010 Supply and Scavange Inlet Screen 012 Master Magnetic Chip Detector 014 Servo Fuel Heater 016 Fuel / Oil Heater Exchanger 018 Scavange Oil Filter 020 Distribution System Operation ...
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AGSE-T016-G12 for CF6-80A/-80C2 engines. Click image to enlarge. REQUEST QUOTE. REQUEST PART. TECH DOCS. CF6 ENGINES LITERATURE V2500 ENGINES LITERATURE SPECIFICATIONS SPECIAL FEATURES. STABLE & RELIABLE SUPPORT. for horizontal build-up & long-term storage. BALL TRANSFERS & FORKLIFT POCKETS ...
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CF6-80C2 main properties . Manufacture . AGSE Cradle PN . AM-1928-A51 Base PN . AM-1928-A52 Towing capability . Towable at a maximum speed of 3 MPH (5 Km/h) Location . Miami (USA) Dimensions (cm) 378/617x244x244/109 Weight (kg) ...
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The FAA is adopting a new airworthiness directive (AD) for General Electric Company (GE) CF6-80C2 and CF6-80E1 series turbofan engines with fuel manifolds part numbers (P/Ns) 1303M31G12 and 1303M32G12, installed in drainless fuel manifold assemblies (introduced by GE Aircraft Engines (GEAE) Service Bulletins (SB) CF6-80C2 S/B 73-0253 and …
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the CF6-80E1, which powers the A330-200 and A330-300. For this technical support survey, coverage for the CF6-80C2 will be provided. Mature engine considerations The CF6-80C2 is a mature engine, so is now powering a declining number of aircraft. Today, the CF6-80C2 still powers about 460 aircraft in service, most of which are 747-400s and 767 ...
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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 the HPCR spool shaft stage 14 disk …
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In maintenance terms, the CF6-80C2 is a mature engine, with the majority having gone through their third shop visit. All have had their first shop visit, and only a minority have yet to go.
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Model: CF6-80C2B CF6-80C2B (CF6-80C2B1, CF6-80C2B2, CF6-80C2B4, CF6-80C2B5, CF6-80C2B6, CF6-80C2B7 & CF6-80C2B8) engines are manufactured by General Electric for …
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The GE CF6 80C2 high-bypass turbofan combines a proven design with the latest technical advances to provide the highest possible reliability in its class of engine.LPT Static Tool. The CF6 80C2 stages 1-5 are statically balanced on a taper pin tool. The static tool provides support for each of the 5 stages on a single plate.
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powers, mean that the CF6-80C2 will continue to operate for at least another 20 years. Configuration The CF6-80A and -80C2 are derived from the CF6-50, developed to power the DC-10 and later the A300B2/B4 and 747-200 in the 1970s. The CF6-50 and -80 are two-shaft engines. The -50 has an 86.4-inch fan diameter, a three-stage low pressure
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The CF6-80C2 is certified on several widebody aircraft models, and Delta TechOps has serviced these engines since 1982.
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92471 CF6-80C2 Nondestructive Testing Manual 3 08/31/93. CF6 Technical Manual Index – December 1, 2024 Supplementary Support Manuals SUPPLEMENTARY SUPPORT MANUALS ARE REVISED AS REQUIRED AND ARE AVAILABLE BY CONTACTING FLEET SUPPORT aviation.fleetsupport@ge. GEK # ...
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FS2004/FSX General Electric CF6-80C2 Sound Set. A soundset for CF6-80C2 to be used with the Level-D 767 and PMDG 747 only (for the others, see CF6-80SND.ZIP). This is a whole new level of sound set with a truely imersive sensation. Created with real high quality records, this sound set was made with cockpit perspective in mind, not the cabin as ...
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he CF6-80C2 family of engines is rated at between 52,460lbs and 60,690lbs of static thrust. The family powers two main Airbus, two main Boeing, and one McDonnell Douglas widebody families. The first engines entered service in the mid-1980s, and the CF6-80C2 is still being manufactured for the last 767-
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CF6-80C2 . LICENSED BY PART NO. CONFIGURATIONS AM-1965-100 Airbus A300-600 & A310-300 bootstrap configuration. AM-1965-133 Boeing 747 & B767 bootstrap configuration. AM-1965-134 Airbus A300-600, A310-300 & Boeing 747, 767 bootstrap configuration. AM-1965-135 for storage only. AM-1965-138 Douglas MD ...
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CF6-80C2. Para el CF6-80C2-A1, el diámetro del ventilador aumenta a 93 pulgadas (2,36 m), con un flujo de aire de 1750 lb/s (790 kg/s). La relación de presión general es de 30,4, con una relación de derivación de 5,15. El empuje estático es de 59.000 lb (263 kN). Se agrega una etapa extra al compresor LP y una quinta a la turbina LP.
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در این مقاله تاریخچه و روند تکامل موتور سیاف6-80سی2 از موتورهای توربوفن خانواده سیاف6 که بر اساس طراحی کلاسیک دو محوری هستند به طور کامل تشریح شده است.
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CF6-80C2 Engine; CF6-80C2 Engine . GE Aviation. Technical Specifications. Max Thrust. 282 kN. Air Mass Flow. 874 kg/s. Bypass Ratio. 5.3:1. Pressure Ratio. 32.6:1. Length. 4270 mm. Max Diameter. 2690 mm. Weight. 4472 kg. The CF6-80C2 is certified on several widebody aircraft models, and Delta TechOps has serviced these engines since 1982.
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CF6-80C2 Engine . GE Aviation. Technical Specifications. Max Thrust. 282 kN. Air Mass Flow. 874 kg/s. Bypass Ratio. 5.3:1. Pressure Ratio. 32.6:1. Length. 4270 mm. Max Diameter. 2690 mm. Weight. 4472 kg. The CF6-80C2 is certified on several widebody aircraft models, and Delta TechOps has serviced these engines since 1982.
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ENGINE - General (72-00-00) - CF6-80C2 Stage 1 and Stage 2 HPTR Disk Ultrasonic Inspection H. Weight and Balance Weight and balance are not changed. I. References (Use the latest version of these documents) GEK 92451, CF6-80C2 Engine Manual (EM) J. Publications Affected None. K. Interchangeability Not applicable. L. Software Accomplishment Summary
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models and with 16 ratings, the CF6-80C2 has received FAA 180- minute Extended Range Operations (ETOPS) approval for A300, A310, 747, and 767 aircraft, offering route structuring flexibility and added economic benefits. The CF6-80C2. high-bypass turbofan engine combines a proven core with the latest technical innovations to
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MD-11. There are more than 2,850 CF6-80C2s installed on 1,135 aircraft. The CF6-80C2 repair and overhaul market is estimated to be about 1,000 shop visits per year. CF6-80C2 in operation The CF6-80C2 operates a wide range of flight cycle times on the aircraft it powers. The shortest are routes where it powers the A300-600R, with flight times
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CF6-80C2 Boeing Service Bulletins (SBs) SB 73-0436 R02 ENGINE FUEL AND CONTROL - HMU (73-21-10) - HMU EHSV Overhaul Date Printed: 2019/08/20 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 EAR controlled;
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The CF6-80C2B1 is rated at 56,700lbs thrust and flat rated to 86 degrees. It was used to power the last 747-200/-300s built in the mid-1980s. The -80C2B1F is rated at 58,090lbs thrust, and …
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The Airbus A300, A310, Boeing 767, 747, MD-11, and the Air Force One (a modified B747-200) are powered by CF6-80C2 engines. Recently, Japan and Italy selected the same engine to …
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Design. Site Transport 3 MPH (5 KM/H) maximum towing speed5" (13 cm) wide x 10" (25 cm) diameter shock-absorbing polyurethane tread wheels for smooth mobility5,000 lbs. (2,268 kg) weight capacity per casterCaster brakes & swivel …
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The CF6-80C2 has experienced 16 events where the debris escaped the engine case, six where the debris escaped the case and nacelle, and two where the debris impacted the aircraft. Many different upstream failures have led to the secondary breakup and separation of LPT blades, and resulted in low energy LPT case penetrations. High pressure ...
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