- Registered owner
- United Parcel Service Co
- Location
- Louisville, KY
- Owner type
- Corporation
- Serial number
- 27242
- Year built
- 1995
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- November 17, 1995
- Certificate issued
- November 21, 1995
- Expires
- November 30, 2028
- Mode S code
- A32FFE
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 N304UPMatched 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 767-34AF aircraft
FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 20170629015229ILanding: Touchdown · Louisville, KYUps flight 421, tail number N304UP, a Boeing 767, landed on runway 17R at approximately 0503 z, 0103 EDT, and taxied to the ramp without incident. It was later reported by ups that the aircraft was damaged by foreign object debris (FOD) on the runway. The…Incident 20030717016449IClimb · Oakland, CA(-23) Left a/c pack service panel (4'X12') departed the aircraft while in flight. Flight crew said they felt a bang at FL270 during climb approx over gth VOR (lubbock, TX). All cockpit indications were normal, no eicas messages, no control problems. Pilot…
Service difficulty reports · 245
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR IPXA2026071310637Strip · missingFOUND LIFE RAFT STOWAGE BIN CAP STRIP-EDGE MISSING. INSTALLED CAP STRIPE EDGE IAW DWG 232T4150, SHEET 1, REV A, AND PSDL 232T4150, SHEET DL, REV -.SDR IPXA2026070610637Strip · missingFOUND LIFE RAFT STOWAGE BIN CAP STRIP-EDGE MISSING.SDR IPXA2026070694047Rub Strip · chafedCHAFED RUB STRIP, NR 2 ENG RT CORE COWL INNER FACE T/E UPPER SIDE. REMOVED DAMAGE RUB STRIP IAW SRM 51-40-02-0G, REV 95. INSTALLED A NEW RUB STRIP IAW SRM 51-40-02-0G, REV 95, AND CMM IPL 71-13-24, REV 50.
See all 245 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