# N304UP: 1995 Boeing 767-34AF

- Status: Valid registration
- Airframe: [Boeing 767-34AF](https://openairdocs.org/model/boeing-767-34af) (registry code 1385212, 190 seats)
- Engine: [GE CF6-80 series](https://openairdocs.org/engine/ge-cf6-80-series) (registry code 30025)
- Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs)
- Serial number: 27242
- Year built: 1995
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 17, 1995
- Certificate issued: November 21, 1995
- Expires: November 30, 2028
- Mode S code: A32FFE
- Registered owner: [United Parcel Service Co](https://openairdocs.org/faa-owner/UNITED%20PARCEL%20SERVICE%20CO)
- Location: [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville)
- Owner type: Corporation
- Owner's area on the map: 38.2585° N, 85.5398° W: Placed by OpenAirDocs at the center of ZIP code 40223, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=304UP
- Page: https://openairdocs.org/aircraft/N304UP

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every GE CF6-80 model are included.

## ADs that may apply (OpenAirDocs): 61 in force

### Matched by airframe (Boeing 767-34AF)

None in force.

### Matched by engine (GE CF6-80 series)

- [AD 2024-24-03](https://openairdocs.org/ad/2024-24-03): Engine Exhaust · Boeing MD-11, MD-11F and CF6-80C2D1F. Effective Jan 13, 2025
- [AD 2023-20-08](https://openairdocs.org/ad/2023-20-08): Engine (Turbine/Turboprop) · General Electric CF6-80C2B1F, CF6-80C2B2F, CF6-80C2B4F and 4 more. Effective Oct 19, 2023
- [AD 2021-26-22](https://openairdocs.org/ad/2021-26-22): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Mar 14, 2022
- [AD 2022-02-18](https://openairdocs.org/ad/2022-02-18): Engine Mount Section · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 3 more. Effective Feb 25, 2022
- [AD 2021-14-11](https://openairdocs.org/ad/2021-14-11): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 25 more. Effective Aug 27, 2021
- [AD 2021-03-02](https://openairdocs.org/ad/2021-03-02): Fuel Control/Turbine Engines · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Mar 31, 2021
- [AD 2020-22-02](https://openairdocs.org/ad/2020-22-02): Engine Fuel and Control · General Electric CF6-80C2A5F, CF6-80C2B1F, CF6-80C2B2F and 13 more. Effective Dec 3, 2020
- [AD 2018-07-05](https://openairdocs.org/ad/2018-07-05): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 11, 2018
- [AD 2017-11-15](https://openairdocs.org/ad/2017-11-15): Turbine/ Turboprop Engine--Turbine Section · General Electric CF6-80C2L1F. Effective Jul 13, 2017
- [AD 2016-08-10](https://openairdocs.org/ad/2016-08-10): Accessory heat shield · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Jun 1, 2016
- [AD 2014-21-01](https://openairdocs.org/ad/2014-21-01): Fuel manifold · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Nov 28, 2014
- [AD 2013-08-20](https://openairdocs.org/ad/2013-08-20): Fuel tube · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 14 more. Effective May 31, 2013
- [AD 2012-03-12](https://openairdocs.org/ad/2012-03-12): No. 3 bearing packing · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Apr 5, 2012
- [AD 2012-04-05](https://openairdocs.org/ad/2012-04-05): Electronic control unit (ECU) · General Electric CF6-80C2B1F, CF6-80C2B1F1, CF6-80C2B1F2 and 8 more. Effective Mar 30, 2012
- [AD 2011-23-04](https://openairdocs.org/ad/2011-23-04): Forward engine mount assembly side links · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Dec 12, 2011
- [AD 2009-21-07](https://openairdocs.org/ad/2009-21-07): Thrust and thrust control · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Dec 1, 2009
- [AD 2009-14-08](https://openairdocs.org/ad/2009-14-08): High-pressure compressor rotor (HPCR) stages 11-14 spool/ shafts · General Electric CF6-80C2B5F. Effective Aug 5, 2009
- [AD 2009-08-06](https://openairdocs.org/ad/2009-08-06): Stage 1 high-pressure turbine (HPT) rotor  
 disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 18, 2009
- [AD 2009-07-10](https://openairdocs.org/ad/2009-07-10): High-pressure turbine rotor (HPTR) · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 6, 2009
- [AD 2009-07-03](https://openairdocs.org/ad/2009-07-03): Eddy current inspection (ECI) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Apr 30, 2009
- [AD 2009-04-10](https://openairdocs.org/ad/2009-04-10): Critical life-limited parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 30 more. Effective Mar 30, 2009
- [AD 2008-21-11](https://openairdocs.org/ad/2008-21-11): Low-pressure turbine (LPT) cases · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Nov 28, 2008
- [AD 2008-02-17](https://openairdocs.org/ad/2008-02-17): Thrust reverser actuation systems · General Electric CF6-50A, CF6-50C, CF6-50C1 and 16 more. Effective Feb 28, 2008
- [AD 2007-24-07](https://openairdocs.org/ad/2007-24-07): Thermal spray coating on certain stage 1 fan disks · General Electric CF6-80C2B1. Effective Jan 2, 2008
- [AD 2007-22-07](https://openairdocs.org/ad/2007-22-07): Electronic control unit (ECU) · General Electric CF6-80C2D1F. Effective Nov 28, 2007
- [AD 2007-21-06](https://openairdocs.org/ad/2007-21-06): Electronic control unit (ECU) · General Electric CF6-80C2A5F. Effective Nov 15, 2007
- [AD 2007-11-20](https://openairdocs.org/ad/2007-11-20): Fuel shroud retaining rings · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 22 more. Effective Jul 10, 2007
- [AD 2007-05-14](https://openairdocs.org/ad/2007-05-14): Cast titanium weld- repaired forward engine mount platforms · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 9, 2007
- [AD 2006-16-06](https://openairdocs.org/ad/2006-16-06): Certain stage 1 high- pressure turbine (HPT) rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Sep 5, 2006
- [AD 2006-06-08](https://openairdocs.org/ad/2006-06-08): Latching system of the fan reverser · General Electric CF6-80C2D1F. Effective Apr 25, 2006
- [AD 2005-17-05](https://openairdocs.org/ad/2005-17-05): High pressure compressor rotor (HPCR) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Sep 27, 2005
- [AD 2005-06-07](https://openairdocs.org/ad/2005-06-07): Directional pilot valve (DPV) assembly · General Electric CF6-80A1, CF6-80A3, CF6-80C2A1 and 5 more. Effective Apr 25, 2005
- [AD 2004-22-07](https://openairdocs.org/ad/2004-22-07): Stage 2 nozzle guide vanes (HPT S2 NGVs) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 1, 2004
- [AD 2004-07-13](https://openairdocs.org/ad/2004-07-13): High pressure turbine (HPT) stage 1 disks · General Electric CF6-80C2A5F, CF6-80C2B5F, CF6-80C2B7F and 1 more. Effective May 6, 2004
- [AD 2003-12-08](https://openairdocs.org/ad/2003-12-08): Directional pilot valve · General Electric CF6-80A1, CF6-80A3, CF6-80C2A1 and 5 more. Effective Jul 23, 2003
- [AD 2003-02-07](https://openairdocs.org/ad/2003-02-07): Low pressure turbine (LPT) shrouds · General Electric CF6-50A, CF6-50C, CF6-50C1 and 30 more. Effective Mar 3, 2003
- [AD 2002-25-08](https://openairdocs.org/ad/2002-25-08): High pressure compressor rotor · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Jan 23, 2003
- [AD 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002
- [AD 2001-06-09](https://openairdocs.org/ad/2001-06-09): Aft Engine Mount Link Assemblies · General Electric CF6-80A3. Effective May 1, 2001
- [AD 2000-12-08](https://openairdocs.org/ad/2000-12-08): Mount Link Assemblies · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 4 more. Effective Aug 28, 2000
- [AD 2000-03-04](https://openairdocs.org/ad/2000-03-04): General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Apr 10, 2000
- [AD 99-01-01](https://openairdocs.org/ad/99-01-01): Accessory Gearbox (AGB) idler adapters · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Jan 21, 1999
- [AD 98-22-06](https://openairdocs.org/ad/98-22-06): Fan Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 41 more. Effective Nov 23, 1998
- [AD 97-22-14](https://openairdocs.org/ad/97-22-14): (HPCR) 3-9 Spool · General Electric CF6-50A, CF6-50C, CF6-50C1 and 29 more. Effective Nov 17, 1997
- [AD 96-16-07](https://openairdocs.org/ad/96-16-07): Rear Right Hand Mount Link · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective Aug 28, 1996
- [AD 95-17-16](https://openairdocs.org/ad/95-17-16): Compressor Rear Frame · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective Nov 7, 1995
- [AD 95-10-11](https://openairdocs.org/ad/95-10-11): Fan Reversers · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective May 31, 1995
- [AD 94-20-06](https://openairdocs.org/ad/94-20-06): Oil System · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 27, 1994
- [AD 94-07-04](https://openairdocs.org/ad/94-07-04): High Pressure Turbine Disk · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 23, 1994
- [AD 94-06-03](https://openairdocs.org/ad/94-06-03): High Pressure Turbine Disk · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 29, 1994

### Historical (superseded or no longer in force)

- [AD 2020-20-13](https://openairdocs.org/ad/2020-20-13) (historical): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Nov 12, 2020
- [AD 2018-15-04](https://openairdocs.org/ad/2018-15-04) (historical): Turbine/Turboprop Engine--Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Oct 2, 2018
- [AD 2009-05-02](https://openairdocs.org/ad/2009-05-02) (historical): Drainless fuel manifold assemblies · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Mar 31, 2009
- [AD 2007-12-07](https://openairdocs.org/ad/2007-12-07) (historical): Electronic control units (ECUs) · General Electric CF6-80C2B1F, CF6-80C2B2F, CF6-80C2B4F and 5 more. Effective Jul 11, 2007
- [AD 2006-12-24](https://openairdocs.org/ad/2006-12-24) (historical): Five-link forward mount assembly · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Jul 21, 2006
- [AD 2004-04-07](https://openairdocs.org/ad/2004-04-07) (historical): Stage 1 HPT rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Mar 12, 2004
- [AD 2003-01-05](https://openairdocs.org/ad/2003-01-05) (historical): Dovetail slots · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective Jan 28, 2003
- [AD 2002-07-12](https://openairdocs.org/ad/2002-07-12) (historical): Life Limits Section of Continued Airworthiness (ICA) - Selected Critical Life-limited Parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 27 more. Effective May 15, 2002
- [AD 2001-10-07](https://openairdocs.org/ad/2001-10-07) (historical): High Pressure Turbine Rotor Disks · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Jun 18, 2001
- [AD 2000-08-12](https://openairdocs.org/ad/2000-08-12) (historical): Life-limited Parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 10 more. Effective Oct 23, 2000
- [AD 2000-16-12](https://openairdocs.org/ad/2000-16-12) (historical): High Pressure Compressor Rotor Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Sep 5, 2000
- [AD 2000-04-14](https://openairdocs.org/ad/2000-04-14) (historical): Fuel tube flange seating · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 12 more. Effective May 1, 2000
- [AD 99-24-15](https://openairdocs.org/ad/99-24-15) (historical): High Pressure Compressor Rotor (HPCR) Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Jan 28, 2000
- [AD 99-18-20](https://openairdocs.org/ad/99-18-20) (historical): Inadvertent In-flight Thrust Reverser · General Electric Aircraft Engines CF6-50 Series (all), CF6-80A1, CF6-80A3 and 6 more. Effective Nov 2, 1999
- [AD 99-18-19](https://openairdocs.org/ad/99-18-19) (historical): Inadvertent Thrust Reverser · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 7 more. Effective Sep 24, 1999
- [AD 99-08-13](https://openairdocs.org/ad/99-08-13) (historical): General Electric CF6-80A, CF6-80A1, CF6-80A2 and 26 more. Effective May 13, 1999
- [AD 98-15-17](https://openairdocs.org/ad/98-15-17) (historical): Link Assembly · General Electric CF6-80A3. Effective Aug 7, 1998
- [AD 91-20-02](https://openairdocs.org/ad/91-20-02) (historical): Fuel Manifolds · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 12 more. Effective Nov 25, 1991
- [AD 90-26-01](https://openairdocs.org/ad/90-26-01) (historical): Fuel Manifold Systems · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 11 more. Effective Dec 20, 1990

All 80: https://openairdocs.org/aircraft/N304UP/ads.md

## Information bulletins (advisory) (5 in force)

- [SAIB 2023-15](https://openairdocs.org/saib/2023-15): Falsified Forms from AOG Technics. Issued Dec 19, 2023
- [SAIB NE-11-27](https://openairdocs.org/saib/NE-11-27): Fuel Injector Nozzle - CF6-80 Improperly Welded Fuel Nozzles. Issued Apr 5, 2011
- [SAIB NE-10-37](https://openairdocs.org/saib/NE-10-37): Engine Fuel and Control: FADEC Fuel Metering Valve Resolver Feedback Faults. Issued Jul 12, 2010
- [SAIB NE-08-44](https://openairdocs.org/saib/NE-08-44): Engine Thrust Reverser  Transcowl Clevis Pin. Issued Sep 3, 2008
- [SAIB NE-07-01](https://openairdocs.org/saib/NE-07-01): Dual engine flameouts on twin engine airplanes. Issued Oct 12, 2006

## NTSB investigations

None matched to N304UP.

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20170629015229I](https://openairdocs.org/incident/20170629015229I), Jun 29, 2017: Boeing 767-34AF (N304UP), Louisville, KY, Minor damage. Ups 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…
- [Incident 20030717016449I](https://openairdocs.org/incident/20030717016449I), Jul 17, 2003: Boeing 76734AF (N304UP), Oakland, CA, Minor damage. (-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…

## Service difficulty reports (245, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR IPXA2026071310637](https://openairdocs.org/sdr/IPXA2026071310637), Jul 5, 2026: STRIP. MISSING. FOUND 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 IPXA2026070610637](https://openairdocs.org/sdr/IPXA2026070610637), Jul 5, 2026: STRIP. MISSING. FOUND LIFE RAFT STOWAGE BIN CAP STRIP-EDGE MISSING.
- [SDR IPXA2026070694047](https://openairdocs.org/sdr/IPXA2026070694047), Jun 28, 2026: RUB STRIP. CHAFED. CHAFED 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
- [SDR IPXA2026070395239](https://openairdocs.org/sdr/IPXA2026070395239), Jun 28, 2026: FORMER. CRACKED. CRACKED FORMER, RT WING LE NR 9 SLAT INBD TRACK, OSS 565. INSTALL NEW FORMER IAW SRM 51-40-02-0G, REV 95, SREO-50900-REQ001, REV 2 AND DWG 114T2512, SH 1, REV D
- [SDR IPXA2026070395238](https://openairdocs.org/sdr/IPXA2026070395238), Jun 28, 2026: FORMER. CRACKED. CRACKED FORMER, RT WING NR 8 SLAT OTBD TRACK, OSS 499. INSTALL A NEW FORMER IAW SRM 51-40-02-0G, REV 95, AND SREO-50900-REQ001, REV.2 AND DWG 114T2511, SH 1, RE
- [SDR IPXA2026070294028](https://openairdocs.org/sdr/IPXA2026070294028), Jun 28, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 1 ENG LT CORE COWL OPEN ROD HOLD BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND CMM IPL 71-13-23 REV. 47.
- [SDR IPXA2026070886027](https://openairdocs.org/sdr/IPXA2026070886027), Jun 27, 2026: PANEL. DEBONDED. DEBONDED AT RIGHT SIDE HST LEADING EDGE FIXED PANEL INTERNAL SURFACE FROM FS STA 157 TO FS STA 194.
- [SDR IPXA2026070684487](https://openairdocs.org/sdr/IPXA2026070684487), Jun 27, 2026: BRACKET. DEFORMED. DEFORMED BRACKET, NR 1 ENG L1 CORE COWL UPPER FLANGE. REMOVED DAMAGED BRACKET IAW SRM 51-40-02-0G, REV 95. INSTALLED THE NEW BRACKET IAW SRM 51-40-02-0G, REV 95
- [SDR IPXA2026070686680](https://openairdocs.org/sdr/IPXA2026070686680), Jun 27, 2026: FLANGE. CHAFED. CHAFED FLANGE, NR 1 ENGINE LT THRUST REVERSER LOWER FWD FAIRING AFT SIDE. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 95. INSTALLED THE NEW BRACKET IAW SRM 
- [SDR IPXA2026070684503](https://openairdocs.org/sdr/IPXA2026070684503), Jun 27, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 1 ENG RT CORE COWL OPEN ROD HOLD BRACKET. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 95. INSTALLED THE NEW BRACKET IAW SRM 51-40-02-0G, 
- [SDR IPXA2026070384542](https://openairdocs.org/sdr/IPXA2026070384542), Jun 27, 2026: ANGLE. CRACKED. CRACK ANGLE, RT WING LE CAVITY OSS 531. INSTALL A NEW ANGLE IAW SRM 51-40-02-0G, REV.95, AND DWG 114T2206, SH 1, REV B.
- [SDR IPXA2026070384515](https://openairdocs.org/sdr/IPXA2026070384515), Jun 27, 2026: RIB. CRACKED. CRACKED RIB, LT WING OTBD L/E UPPER RIB LOWER ANGLE, OSS 549.75. INSTALLED THE NEW RIB ANGLE IAW SRM 51-40-02-0G, REV. 95 AND DWG 114T2207, SH 1, REV B.
- [SDR IPXA2026070283407](https://openairdocs.org/sdr/IPXA2026070283407), Jun 27, 2026: WEDGE. CRACKED. CRACKED WEDGE, RT WING OUTBD FLAP INBD WEDGE. REMOVE THE CRACK MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMU
- [SDR IPXA2026070866895](https://openairdocs.org/sdr/IPXA2026070866895), Jun 26, 2026: ANGLE. WORN. WORN ANGLE ASSY AND BEARING, NR 2 PYLON LT FAIRING DOOR NR 3 HINGE. REMOVED DAMAGED ANGLE IAW SRM 51-40-02-0G REV. 95. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G
- [SDR IPXA2026070867122](https://openairdocs.org/sdr/IPXA2026070867122), Jun 26, 2026: ANGLE. WORN. WORN ANGLE ASSY BEARING, NR 2 PYLON RT FAIRING DOOR NR 4 HINGE. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G REV. 95. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV
- [SDR IPXA2026070666884](https://openairdocs.org/sdr/IPXA2026070666884), Jun 26, 2026: CHANNEL. CRACKED. CRACKED CHANNEL, NR 2 PYLON LOWER FAIRING T/E OTBD SIDE. REMOVED DAMAGED CHANNEL IAW SRM 51-40-02-0G, REV 95. INSTALLED THE NEW CHANNEL IAW SRM 51-40-02-0G, REV
- [SDR IPXA2026070267641](https://openairdocs.org/sdr/IPXA2026070267641), Jun 26, 2026: BRACKET. WORN. WORN OUT BRACKET ASSY , NR 2 ENG LT CORE COWL HOLD OPEN ROD STOWAGE. INSTALLED THE NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND CMM IPL 71-13-23, REV 47.
- [SDR IPXA2026070267274](https://openairdocs.org/sdr/IPXA2026070267274), Jun 26, 2026: BRACKET. WORN. WORN OUT BRACKET ASSY, NR 2 ENG RT CORE COWL HOLD OPEN ROD STOWAGE. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 95 AND CMM IPL 71-13-24, REV 50.
- [SDR IPXA2026072622413](https://openairdocs.org/sdr/IPXA2026072622413), Jun 24, 2026: STRUT. DAMAGED. FOUND THE LT MLG OUTER CYLINDER INNER SURFACE SCRATCH AND THE GLAND NUT THREADS CORROSION. TASK CARD MXP-32-045-02-1-JIC T3F18E00983AV ISSUED TO REPLACE LT MAIN
- [SDR IPXA2026070819890](https://openairdocs.org/sdr/IPXA2026070819890), Jun 24, 2026: CHANNEL. CRACKED. THE U CHANNEL ON THE AFT MAIN DECK CARGO DOOR AT BS 632 WAS CRACKED. IAW DWG 453T7019, SHT 1 REV A. REMOVED & REPLACED THE U CHANNEL IAW AMM 20-11-00-910-802, R
- [SDR IPXA2026070822555](https://openairdocs.org/sdr/IPXA2026070822555), Jun 24, 2026: ANGLE. CRACKED. FOUND FIRE DETECTION LOOP FASTENER ANGLE CRACKED AT BS 1562, LBL 96 IN BULK CARGO BAY. REMOVED THE DAMAGED ANGLE IAW SRM 51-40-02-0G, REV 95. INSTALLED A FABRIC
- [SDR IPXA2026070121828](https://openairdocs.org/sdr/IPXA2026070121828), Jun 24, 2026: ANTENNA. ERODED. FOUND V.S.T HF ANTENNA (321E) EROSION. REMOVE THE EROSION MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260 F FOR 130 MINUTES WITH MINI
- [SDR IPXA2026070222600](https://openairdocs.org/sdr/IPXA2026070222600), Jun 24, 2026: ANGLE. CORRODED. FOUND FLOOR SUPPORT CORRODED IN THE AREA AFT OF BULK CARGO BAY AT BS 1588, LBL 33. REMOVED THE DAMAGED ANGLE IAW SRM 51-40-02-0G REV. 95. INSTALLED A NEW ANGLE 
- [SDR IPXA2026070121913](https://openairdocs.org/sdr/IPXA2026070121913), Jun 24, 2026: BUMPER. MISSING. THE BUMPER IS MISSING FROM THE CREW ENTRY DOORWAY LINING. (REPLACE) INSTALL THE BUMPER IS FROM THE CREW ENTRY DOORWAY LINING. IAW PSDL 411T2240 SH DL REV.A AND 
- [SDR IPXA2026062421913](https://openairdocs.org/sdr/IPXA2026062421913), Jun 24, 2026: BUMPER. MISSING. THE BUMPER IS MISSING FROM THE CREW ENTRY DOORWAY LINING.
- [SDR IPXA2026082598212](https://openairdocs.org/sdr/IPXA2026082598212), Jun 23, 2026: PAWL. WORN. *** SUPPLEMENTAL SDR *** FAULT - THE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. (REPLACE) REPLACED THE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HA
- [SDR IPXA2026062398212](https://openairdocs.org/sdr/IPXA2026062398212), Jun 23, 2026: PAWL. WORN. THE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN.
- [SDR IPXA2026062915824](https://openairdocs.org/sdr/IPXA2026062915824), May 10, 2026: FAN COWL. DENTED. RIGHT ENGINE OTBD FAN COWL OUTER SKIN TWO DENTS AT 1 O'CLOCK POSITION IAW AMM 71-11-04-714-002-H00, REV 148, INSTALLED THE FAN COWL OF NR 2 ENGINE. CONDITION CH
- [SDR IPXA2025052801275](https://openairdocs.org/sdr/IPXA2025052801275), May 21, 2025: CRANK ASSY. INOPERATIVE. **SUPPLEMENTAL SDR** CAPT #2 WINDOW CRANK IS BINDING WHEN TRYING TO OPEN FOUND AFT OUTBOARD GEARBOX TO BE SERVICEABLE, RE-INSTALLED SAME AFT OUTBOARD GEARBOX, F
- [SDR IPXA2025052101275](https://openairdocs.org/sdr/IPXA2025052101275), May 21, 2025: ROLLER. OUT OF ADJUST. *** SDR FILED OPEN *** CAPT #2 WINDOW CRANK IS BINDING WHEN TRYING TO OPEN ADJUSTED AFT LINK ARM AND AFT UPPER ROLLER CLUSTER PER AMM 56-11-02. CRANK CLUTCH STI
- [SDR IPXA2024071613354](https://openairdocs.org/sdr/IPXA2024071613354), Jul 15, 2024: SKIN. GOUGED. MAJOR REPAIR - GOUGES - SKIN, R/H WING NO.8 SLAT INNER SURFACE UPPER SIDE. (REPAIR) REPAIR I/A/W B767-300F (REV. 89) SRM 51-70-10-2R-4 AND 51-70-10-2R-0 PER SRM
- [SDR IPXA2024072905616](https://openairdocs.org/sdr/IPXA2024072905616), Jul 14, 2024: SPLINE. CRACKED. FOUND ENTRY DOOR FWD SIDE DOORWAY LINING SPLINE - TRIM CRACK IAW AMM 52-12-02-004-001 REV.142 AND AMM 52-12-02-404-025 REV.142 REPLACED DOORWAY SPLINE TRIM. JOB
- [SDR IPXA2024071505616](https://openairdocs.org/sdr/IPXA2024071505616), Jul 14, 2024: LINER. CRACKED. FOUND ENTRY DOOR FWD SIDE DOORWAY LINING SPLINE - TRIM CRACK. OK TO WORK. OPEN
- [SDR IPXA2024072975073](https://openairdocs.org/sdr/IPXA2024072975073), Jul 12, 2024: HINGE. DEFORMED. FOUND MAIN ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY DEFORM. (REPLACE) I.A.W AMM 52-12-02-404-025 REV.142 INSTALLED DOORWAY LINING. I.A.W AMM 33-51-01-402-030 
- [SDR IPXA2024072677503](https://openairdocs.org/sdr/IPXA2024072677503), Jul 12, 2024: STRINGER. CORRODED. *SUPPLEMENTAL SDR* FAULT - CORROSION SKIN AFT CARGO COMPARTMENT LOWER AT STA 1175~STA 1197+11, S-36R. (REPAIR) ACCOMPLISHED REPAIR I.A.W UPS EO-98978-REQ1 REV.1
- [SDR IPXA2024072076571](https://openairdocs.org/sdr/IPXA2024072076571), Jul 12, 2024: BRACKET. CRACKED. CRACKED BRACKET MEC INTERIOR COMPARTMENT LH FWD UPPER FLIGHT DECK COCKPIT FLOOR BEAM SUPPORT AT STA 246 LBL 50. (REPLACE) 1.FABRICATE P/N(141T5146-16) PER BOEIN
- [SDR IPXA2024071976451](https://openairdocs.org/sdr/IPXA2024071976451), Jul 12, 2024: ANGLE. CRACKED. CRACKED ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 LBL 60. (REPLACE) REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.89. INSTALLED NEW PARTS I.A.W SRM 51-4
- [SDR IPXA2024071976402](https://openairdocs.org/sdr/IPXA2024071976402), Jul 12, 2024: ANGLE. CRACKED. CRACKED ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60. REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.89. INSTALLED NEW PARTS I.A.W SRM 51-40-02-0G RE
- [SDR IPXA2024071877503](https://openairdocs.org/sdr/IPXA2024071877503), Jul 12, 2024: SKIN. CORRODED. CORROSION SKIN AFT CARGO COMPARTMENT LOWER AT STA 1175~STA 1197+11, S-36R. (REPAIR) PERFORM NDT INSPECTION I.A.W EGAT EI NO.F2024A53M-1771 SEQUENCE B PARTA STEP
- [SDR IPXA2024071276599](https://openairdocs.org/sdr/IPXA2024071276599), Jul 12, 2024: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 231DFF, P/N: 143T5876-37. (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. I.A.W AMM 53-01-06-400
- [SDR IPXA2024071276585](https://openairdocs.org/sdr/IPXA2024071276585), Jul 12, 2024: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 231CFF, P/N: 143T5876-39. (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. I.A.W AMM 53-01-06-400
- [SDR IPXA2024071275073](https://openairdocs.org/sdr/IPXA2024071275073), Jul 12, 2024: HINGE. DEFORMED. FOUND MAIN ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY DEFORM. (REPLACE) OK TO WORK
- [SDR IPXA2024071276610](https://openairdocs.org/sdr/IPXA2024071276610), Jul 12, 2024: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 252WFF, P/N: 146T5869-55. (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. I.A.W AMM 53-01-06-400
- [SDR IPXA2024071259276](https://openairdocs.org/sdr/IPXA2024071259276), Jul 11, 2024: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL DENT. PANEL NO.251SFF, P/N:146T5869-37 (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. I.A.W AMM 25-57-05-404-00
- [SDR IPXA2024071259270](https://openairdocs.org/sdr/IPXA2024071259270), Jul 11, 2024: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL DENT. PANEL NO.231QFF, P/N:143T5876-19 (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. I.A.W AMM 53-01-06-400-80
- [SDR IPXA2024071259282](https://openairdocs.org/sdr/IPXA2024071259282), Jul 11, 2024: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL DENT, PANEL NO.232AFF, P/N: 143T5876-40 (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. I.A.W AMM 53-01-06-400-8
- [SDR IPXA2024071041602](https://openairdocs.org/sdr/IPXA2024071041602), Jul 10, 2024: INSPECTION. NONE. *SUPPLEMENTAL SDR* FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) C/W EO-82173.
- [SDR IPXA2024070572572](https://openairdocs.org/sdr/IPXA2024070572572), Jul 5, 2024: LIGHT. INOPERATIVE. EMERGENCY LIGHT IN COCKPIT AND PRM CAME ON INFLIGHT. WE HAD NO EICAS MESSAGE. WE CYCLED THE EMERGENCY LIGHT OFF+ON SEVERAL TIMES. FINALLY THE LIGHTS WOULD STAY 
- [SDR IPXA2022102187349](https://openairdocs.org/sdr/IPXA2022102187349), Oct 21, 2022: WARNING MESSAGE. ILLUMINATED. INSPECTION TYPE:N/A**ATB** **EMERGENCY DECLARED** C" HYDR SYS PRESS" CAUTION MESSAGER/R'D CENTER HYD PRESSURE SWITCH AND THEN CENTER HYD SYS OPS CHKD NML. HYD L
- [SDR IPXA2022100386790](https://openairdocs.org/sdr/IPXA2022100386790), Sep 21, 2022: SKIN. CRACKED. INSPECTION TYPE:C14CORROSION AND CRACK DAMAGE WAS FOUND ON FUSELAGE SKIN(P/N:146T3241-14) BETWEEN STA 1395-STA 1417,S-38R-S-39R.REPAIR I.A.W BOEING SRID:4-56119

All 245: https://openairdocs.org/aircraft/N304UP/reports.md

## STCs that may be installed (OpenAirDocs) (6)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (GE CF6-80 series)

- [STC SE01543CH](https://openairdocs.org/stc/SE01543CH): Replace 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. Cook Airtomic. Lists CF6-80A
- [STC SE01478CH](https://openairdocs.org/stc/SE01478CH): Installation of Cook Airtomic alignment joint p/n AIR 22912. Cook Airtomic. Lists CF6-80C2 Series
- [STC SE00969CH](https://openairdocs.org/stc/SE00969CH): Install AeroControlex P/N 2605290-001 variable stator feedback control cable. AeroControlex Group TransDigm Inc. Lists CF6-80A
- [STC SE01471AT](https://openairdocs.org/stc/SE01471AT): Replace right and left side Rohr, Inc. fire detection harness on GE CF6-80C2 engine. Unison Industries. Lists CF6-80C2 Series
- [STC SE00463LA](https://openairdocs.org/stc/SE00463LA): Install 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 21220. Hi Temp Insulation Inc. Lists CF6-80C2A1
- [STC SA2227SO](https://openairdocs.org/stc/SA2227SO): Installation 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. Rolls Royce, Inc

## Related

- Other Boeing 767-34AF aircraft: https://openairdocs.org/model/boeing-767-34af/aircraft.md
- The GE CF6-80 series engine: https://openairdocs.org/engine/ge-cf6-80-series.md

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