- Registered owner
- Atlas Air Inc
- Location
- Purchase, NY
- Owner type
- Corporation
- Serial number
- 25864
- Year built
- 1992
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- March 19, 2014
- Certificate issued
- January 27, 2016
- Expires
- January 31, 2029
- Mode S code
- A88752
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 N649GTMatched 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 767-300ER aircraft
FAA incident reports
No FAA accident or incident reports matched to N649GTMatched 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 767-300ER aircraft
Service difficulty reports · 574
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR UIEA2026102300995Battery · inoperativeEMERGENCY FLASHLIGHT NEXT TO LAV LED NOT FLASHING. R & R FLASHLIGHT BATTERY IAW AMM 25-64-02. OPS CHECK GOOD.</P>)SDR UIEA2026101500987Limit Switch · failedREJECTED T/O AT 60KTS DUE TO EICAS MESSAGE. UNSCHEDULED STAB TRIM MESSAGE ALSO APPEARED TWICE DURING TAXI OUT(<P>RIGHT STAB TRIM LIMIT SWITCH/POSITION INDICATOR EXPERIENCED AN INTERNAL SHORT. R&R R/H STAB TRIM LIMIT SWITCH AND POSITION TRANSMITTER MODULE PER ASDR UIEA2026100900972Failsafe · damagedDETECTED DEFECT INDICATION DURING EO 6753A070 (SB 767-53A0100 R3/AD 2021-09-04) STA 955 REAR SPAR BULKHEAD SIDE FITTING FAILSAFE STRAP ULTRASONIC INSPECTION. DEFECT SIGNAL LOCATION: FAILSAFE STRAP (RH)(<P>REMOVED PLATE ASSY OF R/H MAIN L/G W/W LONGN AND L/G BE
See all 574 reportsReports on N649GT not matched to an aircraft · 1
They name N649GT, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
STCs 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