- Registered owner
- Atlas Air Inc
- Location
- Purchase, NY
- Owner type
- Corporation
- Serial number
- 29253
- Year built
- 1998
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- August 10, 1998
- Certificate issued
- February 9, 2022
- Expires
- February 28, 2029
- Mode S code
- A6189C
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every GE CF6-80 model are included below.
On this page
Airworthiness directives that may apply · 61
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1985 | 1 |
|---|---|
| 1986 | 1 |
| 1989 | 1 |
| 1990 | 2 |
| 1991 | 6 |
| 1992 | 1 |
| 1993 | 1 |
| 1994 | 3 |
| 1995 | 2 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 2 |
| 1999 | 4 |
| 2000 | 6 |
| 2001 | 2 |
| 2002 | 2 |
| 2003 | 4 |
| 2004 | 3 |
| 2005 | 2 |
| 2006 | 3 |
| 2007 | 5 |
| 2008 | 3 |
| 2009 | 7 |
| 2011 | 1 |
| 2012 | 2 |
| 2013 | 1 |
| 2014 | 1 |
| 2016 | 1 |
| 2017 | 1 |
| 2018 | 2 |
| 2020 | 2 |
| 2021 | 2 |
| 2022 | 2 |
| 2023 | 1 |
| 2025 | 1 |
Engine · GE CF6-80 series
AD 2024-24-03Engine ExhaustAD 2023-20-08Engine (Turbine/Turboprop)AD 2021-26-22Turbine SectionInformation bulletins that may apply · 5
Advisory, not mandatory.
Engine · GE CF6-80 series
SAIB 2023-15Falsified Forms from AOG TechnicsSAIB NE-11-27Fuel Injector Nozzle - CF6-80 Improperly Welded Fuel NozzlesSAIB NE-10-37Engine Fuel and Control: FADEC Fuel Metering Valve Resolver Feedback FaultsSAIB NE-08-44Engine Thrust Reverser Transcowl Clevis PinSAIB NE-07-01Dual engine flameouts on twin engine airplanesNTSB investigations
No NTSB investigations matched to N492MCMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Boeing 747-47UF aircraft
FAA incident reports
No FAA accident or incident reports matched to N492MCMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Boeing 747-47UF aircraft
Service difficulty reports · 205
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR UIEA2026100600963Relay · faultedREJECTED TAKE OFF DUE TO #2 ENG REVERSER EICAS MSG(<P>TRANSFER TO DMI 260447 PER MEL 78-31-01A CAT C DUE DATE 16OCT2026</P> / <P>LP 2029709 M5: T/S AND PERFORMED WIRING CHECK. FOUND GRD SAFETY RELAY R8016 DEFECTIVE. REMOVED AND REPLACED RELAY & PERFORMED #2 T/SDR UIEA2026070900586Compressor · stalledAFTER V1 COMPRESSOR STALL ON #2 ENGINE, RAN QRH CHECKLIST AND RETURNED TO HAN. A/C WAS 265,656KG N1 TARGET 934. NO FUEL DUMPED. MX IN WORK WHILE IN AOGM FOR ATB ENG 2 COMPRESSOR. AOGM ETR: 12JUL26. FERRIED FLIGHT REQ FOR #2 ENG COMPRESSOR STALL. 3 ENGINES FESDR UIEA2025021800151Tire · failed#8 TIRE FAILURE ON TAKEOFF WITH NO FLIGHT DECK INDICATIONS. NORMAL FLAPS 30 LANDING WAS ACCOMPLISHED. REPLACED MLG TIRE #7 & #8 PER AMM 32-45-01 & IPC 32-45-01-02A. VERIFIED PN PER IPC 32-45-03-02. VERIFIED TIRE PRESSURE 210 PSI. RO INSTALLED. C/W INSPECTION
See all 205 reportsSTCs that may be installed · 6
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Engine · GE CF6-80 series
STC SE01543CHReplace Hamilton Sundstrand P/N 778839-13, 778839-14, 778839-19, 778839-20, 778839-37, 778839-38, 816682-1, 840618-2, 880724 carbon bushings with Cook Airtomic P/N AIR22947 Slotted Entry Busing in the High Pressure Shutoff Valve.STC SE01478CHInstallation of Cook Airtomic alignment joint p/n AIR 22912.STC SE00969CHInstall AeroControlex P/N 2605290-001 variable stator feedback control cable.STC SE01471ATReplace right and left side Rohr, Inc. fire detection harness on GE CF6-80C2 engine.STC SE00463LAInstall fireproof blankets on the engine fan reverser intermediate fireseal, in lieu of fireproof intumescent coating. This STC is jointly by owned by Hi Temp Insulation and MRA Systems acting through Middle River Aircraft Systems, 103 Chesapeake Park Plaza, Baltimore, MD 21220STC SA2227SOInstallation of wiring and associated components for utilization of the Rolls Royce, Inc., ARINC, interface/readers UT1317 or UT1317/1, for the purpose of acquisition, recording, and analysis in real time of engine/aircraft/ systems. (767 SERIES POWERED BY RR RB-11-524 SERIES