- Registered owner
- Atlas Air Inc
- Location
- Purchase, NY
- Owner type
- Corporation
- Serial number
- 29260
- Year built
- 2000
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- February 16, 2000
- Certificate issued
- July 29, 2019
- Expires
- July 31, 2029
- Mode S code
- A6329D
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 · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports
No FAA accident or incident reports matched to N499MCMatched 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 · 267
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR UIEA2026072900665Shutoff Valve · faultedDURING TAKEOFF ROLL, BLEED 2 ADVISORY MESSAGE CAME ON. TRANSFER TO DMI 256295 PER MEL 36-11-03 CATC DUE DATE 02AUG26. REMOVED AND REPLACE HPSOV IAW B747 AMM 36-11-03 AND OPS CHECK GOOD.SDR UIEA2026063000560Clamp · leakingEQUIPMENT COOLING EICAS MESSAGE IN FLIGHT. REPLACED FLIGHT DECK LOW FLOW DETECTOR & OPS CHECKED GOOD IAW AMM 21-58-02/201. REMOVED AND REPLACED FLIGHT DECK FLOW REGULATOR VALVE & OPS CHECKED GOOD IAW AMM 21-61-09/501. DURING TROUBLESHOOTING, FOUND FOD INSIDESDR UIEA2025052700699Lug · cracked1EA CRACK WAS FOUND ON LH STA 1000 LBL 11.33 FRONT SPAR INTERCOSTAL LUG FITTING.(<P>FITTING REPLACEMENT CARRIED OUT AS PER ATLAS AIR EO: 4453C024 REV 4 PART 3 STEP 3. NO FURTHER DEFECTS NOTED.</P>)
See all 267 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