# N316UP: 1997 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: 27744
- Year built: 1997
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 23, 1997
- Certificate issued: June 3, 1997
- Expires: August 31, 2027
- Mode S code: A35EEB
- 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=316UP
- Page: https://openairdocs.org/aircraft/N316UP

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/N316UP/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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB FTW98FA380](https://openairdocs.org/ntsb/FTW98FA380), Sep 11, 1998: Boeing 767-34AF (N316UP), Houston, TX, substantial damage. Probable cause: The flight crew's decision to land with convective activity over the airport with a prevailing crosswind to a quartering tailwind, on an ungrooved, flooded runway, which resulted in hydroplaning and…

## FAA accident and incident reports (1)

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.

- [Accident 19980911034919A](https://openairdocs.org/incident/19980911034919A), Sep 11, 1998: Boeing 76734AF (N316UP), Houston, TX, Substantial damage. On September 11, 1998, at 0624 central daylight time, a Boeing 767-34AF airplane, N316UP, operating as ups flight 774, was substantially damaged following a…

## Service difficulty reports (143, 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 IPXA2026092450293](https://openairdocs.org/sdr/IPXA2026092450293), Sep 15, 2026: SEAL DEPRESSOR. CORRODED. CORROSION - SEAL DEPRESSOR, LOWER FUSELAGE L/H ECS DOOR 193NL FWD HINGE FWD SIDE BRACKET. REMOVED DAMAGE SEAL DEPRESSOR I.A.W SRM 51-40-02-0G REV.96. INSTALLED 
- [SDR IPXA2026092450484](https://openairdocs.org/sdr/IPXA2026092450484), Sep 15, 2026: SEAL DEPRESSOR. CORRODED. CORROSION - SEAL DEPRESSOR, LOWER FUSELAGE L/H ECS DOOR 193NL AFT HINGE AFT SIDE BRACKET. REMOVED DAMAGE SEAL DEPRESSOR I.A.W SRM 51-40-02-0G REV.96. INSTALLED 
- [SDR IPXA2026092350550](https://openairdocs.org/sdr/IPXA2026092350550), Sep 15, 2026: TEE ANGLE. BROKEN. - BROKEN - SPLICE TEE, LOWER FACE OF KEEL BEAM AT LOWER PANEL NO.149AL FWD SUPPORT, NEAR STA 962, LBL 5. REMOVED DAMAGE SPLICE TEE I.A.W SRM 51-40-02-0G REV.96.
- [SDR IPXA2026092347262](https://openairdocs.org/sdr/IPXA2026092347262), Sep 15, 2026: ANGLE. GOUGED. PREVIOUS REPAIR ON MAIN DECK FLOOR SUPPORT STRUCTURE, LOCATED AT APPROXIMATE STA. 710 OUTBD OF LT. FWD CARGO PIT SIDEWALL, IS GOUGED IN THREE PLACES. ACCOMPLISH
- [SDR IPXA2026092350293](https://openairdocs.org/sdr/IPXA2026092350293), Sep 15, 2026: SEAL DEPRESSOR. CORRODED. CORRODED SEAL DEPRESSOR, LOWER FUSELAGE LT ECS DOOR 193NL FWD HINGE FWD SIDE BRACKET.
- [SDR IPXA2026092350484](https://openairdocs.org/sdr/IPXA2026092350484), Sep 15, 2026: SEAL DEPRESSOR. CORRODED. CORRODED SEAL DEPRESSOR, LOWER FUSELAGE L/H ECS DOOR 193NL AFT HINGE AFT SIDE BRACKET.
- [SDR IPXA2026091847947](https://openairdocs.org/sdr/IPXA2026091847947), Sep 15, 2026: ANGLE. CRACKED. THE BULK CARGO INBOARD ANGLE AT STA 1578 LBL 80 IS CRACKED. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV.96. INSTALL NEW ANGLE I.A.W SRM 51-40-02-0G REV.96 AN
- [SDR IPXA2026091847888](https://openairdocs.org/sdr/IPXA2026091847888), Sep 15, 2026: ANGLE. CRACKED. THE BULK CARGO OUTBOARD ANGLE AT STA 1578 RBL 80 IS CRACKED. (REPLACE) ACCOMPLISHED OK TO INSTALL CHECK. PANEL NO:252YFF, 252QFS,252PSF.
- [SDR IPXA2026091845796](https://openairdocs.org/sdr/IPXA2026091845796), Sep 15, 2026: FLOOR PANEL. DENTED. MAJOR REPAIR, DENTS ON THE FLOOR PANEL NO.231AFF (P/N 143T5876-78) IN THE MAIN DECK CARGO COMPARTMENT. (REPAIR) I.A.W AMM 25-57-02-404-016 AND AMM 25-58-03-404-
- [SDR IPXA2026091845779](https://openairdocs.org/sdr/IPXA2026091845779), Sep 15, 2026: FLOOR PANEL. DENTED. MAJOR REPAIR, DENTS ON THE FLOOR PANEL NO.231FFF (P/N 143T5876-49) IN THE MAIN DECK CARGO COMPARTMENT. (REPAIR) I.A.W AMM 25-57-02-404-016, AMM 25-57-90-424-011
- [SDR IPXA2026092422876](https://openairdocs.org/sdr/IPXA2026092422876), Sep 13, 2026: KEELBEAM. CORRODED. FORWARD RIGHT SIDE OF EXPOSED KEEL BEAM AT STA 785 RBL 9 HAS CORROSION AROUND NUT PLATE. REPAIR DAMAGE AREA I.A.W EO-98691-REQ1 REV 1 AND EGAT EI F2026A53M-1944
- [SDR IPXA2026092322876](https://openairdocs.org/sdr/IPXA2026092322876), Sep 13, 2026: KEELBEAM. CORRODED. FORWARD RIGHT SIDE OF EXPOSED KEEL BEAM AT STA 785 RBL 9 HAS CORROSION AROUND NUT PLATE.
- [SDR IPXA2026091811782](https://openairdocs.org/sdr/IPXA2026091811782), Sep 12, 2026: PANEL. ERODED. ERODED SKIN, LOWER FACE L/H WING NO.5 SLAT LOWER CLOSURE PNL, NEAR INBD TRACK. REMOVE THE EROSION MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT
- [SDR IPXA2026091811821](https://openairdocs.org/sdr/IPXA2026091811821), Sep 12, 2026: SKIN. DEBONDED. DEBONDED SKIN, INBD EDGE OF LT WING T/E OUTBD FLAP T/E SKIN, WBL 355, TOTAL: 2 AREA. REMOVE THE DISBOND MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CU
- [SDR IPXA2026091512611](https://openairdocs.org/sdr/IPXA2026091512611), Sep 12, 2026: ANTENNA. DAMAGED. FOUND V.S.T HF ANTENNA (321E) EROSION. REMOVE THE DAMAGED MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260°F FOR 130 MINUTES WITH MIN
- [SDR IPXA2026092174292](https://openairdocs.org/sdr/IPXA2026092174292), Sep 10, 2026: HINGE FITTING. CRACKED. CRACKED HINGE FITTING, RT WING T/E NR 10 SPOILER.
- [SDR IPXA2026052061751](https://openairdocs.org/sdr/IPXA2026052061751), May 19, 2026: WINDOW. CRACKED. R FWD WINDOW ARCED AND THEN SPLINTERED/ CRACKED ACROSS ENTIRE AREA. NO LEAKS OR BOWING NOTED. RAN CHECKLIST FOR R FWD WINDOW EICAS. C/W RII VERIFICATION IAW GMM
- [SDR IPXA2026020246402](https://openairdocs.org/sdr/IPXA2026020246402), Jan 30, 2026: HANDLE. FOD. CANNOT SECURE THE ENTRY DOOR FROM THE INSIDE. REMOVED DEBRIS FROM EXTERIOR DOOR HANDLE, OPERATED DOOR FROM INSIDE AND OUTSIDE OPS CHK NORMAL IAW AMM: 52-12-00/2
- [SDR IPXA2026011504578](https://openairdocs.org/sdr/IPXA2026011504578), Jan 14, 2026: DOOR. BINDING. CABIN ENTRY DOOR LOCK LATCH LEVER STICKS/STICKY. DIFFICULT TO LOCK. C/W INSPECTION/TEST OF CREW ENTRY DOOR SECONDARY CAPTURE LEVER 52-12-00-735-137. NO FAULTS F
- [SDR IPXA2026030277639](https://openairdocs.org/sdr/IPXA2026030277639), Nov 8, 2025: FLOOR PANEL. DAMAGED. MAJOR REPAIR, DAMAGE TO MAIN DECK FLOOR PANEL POSITION 2 RIGHT OUTBOARD. INSTALLED FLOOR PANEL IAN AMM 53-01-01.
- [SDR IPXA2025091098119](https://openairdocs.org/sdr/IPXA2025091098119), Sep 9, 2025: DOOR. BINDING. UNABLE TO SECURE SMALL YELLOW HANDLE FOR MAIN CABIN DOOR TO SECURE DOOR FOR FLIGHT FROM THE INSIDE. CLEANED DEBRIS AND LUBED ARMING HANDLE AS REQ. PERFORMED OPS
- [SDR IPXA2025080126694](https://openairdocs.org/sdr/IPXA2025080126694), Jul 31, 2025: LEVER. BINDING. UPON CREW ENTRY DOOR CLOSURE, CAPTURE LEVER DIFFICULT TO MOVE OUTBOARD. INSPECTED CREW ENTRY DOOR HANDLE CAPTURE LEVER AND FOUND NO DEFECTS. OPERATED DOOR AND T
- [SDR IPXA2024100929642](https://openairdocs.org/sdr/IPXA2024100929642), Sep 27, 2024: DRAIN. NONE. ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R). ACCOMPLISHED SDR. PERFORM MODIFICATION 
- [SDR IPXA2024100829642](https://openairdocs.org/sdr/IPXA2024100829642), Sep 27, 2024: DRAIN. NONE. **SDR FILED OPEN** ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) ACCOMPLISHED SDR
- [SDR IPXA2024021449080](https://openairdocs.org/sdr/IPXA2024021449080), Feb 13, 2024: DOOR. WARNING MESSAGE. L FWD ENTRY DOOR EICAS AND LIGHT ON AFTER BLOCK OUT PERFORMED DOOR WARNING SENSOR TEST AS PER AMM 52-71-00, SYST IS WORKING NORMAL.
- [SDR IPXA2024032007633](https://openairdocs.org/sdr/IPXA2024032007633), Jan 6, 2024: INLET. DENTED. ENGINE 1 INLET COWL HAS 1 DENT NEAR THE 11:00 POSITION NEAR THE LEADING EDGE. INSTALLED LH #1 ENGINE INLET COWL I/A/W AMM 71-11-01. NO DEFECTS NOTED AT THIS TIM
- [SDR IPXA2024010707633](https://openairdocs.org/sdr/IPXA2024010707633), Jan 6, 2024: UNKNOWN. UNKNOWN. ENGINE 1 INLET COWL HAS 1 DENT NEAR THE 11:00 POSITION NEAR THE LEADING EDGE.***PLEASE ORDER PARTS AND TOOLING*** ACCOMP ALL MX AND INSP STEPS OF EO 89109-REQ1.
- [SDR IPXA2023042710160](https://openairdocs.org/sdr/IPXA2023042710160), Apr 27, 2023: COVER. BROKEN. MAIN ENTRY DOOR ARMING LEVER HINGE COVER SPRING BROKEN REPLACED MAIN ENTRY DOOR ARMING LEVER COVER HINGE PER MM 52-11-26.
- [SDR IPXA2023022191200](https://openairdocs.org/sdr/IPXA2023022191200), Feb 20, 2023: DOOR. INOPERATIVE. DAMAGE OF LIGHTNING STRIKE FND ON UPR SIDE OF CRW ENTRY DR, LOCATED 6 INCH UP, 4 INCHES AFT FROM THE ENTRY DR LEFTHAND TOP CORNER. DAMAGE OF THE REVET WITHIN LI
- [SDR IPXA2023011189786](https://openairdocs.org/sdr/IPXA2023011189786), Dec 29, 2022: STRUCTURE. CRACKED. INSPECTION TYPE: C13, MAJOR REPAIR. CRACK ON BS 1809.5 BULKHEAD HORIZONTAL INNER CHORD AT APPROXIMATELY WL 257, RBL 28. SRM 53-80-08 REPAIR 10 REV.85.01 AND EO 
- [SDR IPXA2023010689627](https://openairdocs.org/sdr/IPXA2023010689627), Dec 29, 2022: SKIN. CRACKED. INSPECTION TYPE:C13*MAJOR REPAIR* CRACK FOUND ON FUSELAGE SKIN AT STA 1654.5,S-13AR.REPAIR I.A.W 767-300F SRM 53-80-01-2R-7 REV.85.01.
- [SDR IPXA2023010489562](https://openairdocs.org/sdr/IPXA2023010489562), Dec 28, 2022: STIFFENER. CRACKED. INSPECTION TYPE:C13*MAJOR REPAIR* CRACK ON CENTER WING TANK STIFFENER (P/N: 111T2011-5) ON STA 785.9, LBL 55.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 RE
- [SDR IPXA2022102987605](https://openairdocs.org/sdr/IPXA2022102987605), Oct 29, 2022: FLOOR PANEL. DAMAGED. MAIN DECK FLOOR PANEL R/H STATION 412 HAS HOLE DAMAGEFABBED NEW REPLACEMENT PANEL 141T5856-13U IAW SREO B767-5320-9693-I
- [SDR IPXA2022072084352](https://openairdocs.org/sdr/IPXA2022072084352), Jul 19, 2022: EICAS. FAULT MESSAGE. INSPECTION TYPE:** ETOPS FILED OPEN**ON TAXI IN PREV ISLN VAL STATUS MESSAGE. DEFERRED PER MEL 78-31-1. DMP ACCOMPLISHED PLACARD INSTALLED
- [SDR IPXA2022050681814](https://openairdocs.org/sdr/IPXA2022050681814), May 5, 2022: HANDLE. INOPERATIVE. INSPECTION TYPE:N/AMAIN ENTRY DOOR YELLOW SECURING HANDLE JAMMEDOPENED AND CLOSED CREW ENTRY DOOR SEVERAL TIMES SECONDARY CAPTURE SHOWED NO SIGNS OF JAMMIN OK F
- [SDR IPXA2022040880976](https://openairdocs.org/sdr/IPXA2022040880976), Apr 7, 2022: LANDING GEAR. NONE. INSPECTION TYPE:NA**DIVERSION**AFTER TAKEOFF THE GEAR WAS RETRACTED NORMALLY. WHEN THE GEAR HANDLE WAS PLACED IN THE OFF POSITION, THE RIGHT GEAR SHOWED GREEN A
- [SDR IPXA2022040180717](https://openairdocs.org/sdr/IPXA2022040180717), Mar 31, 2022: WARNING MESSAGE. ILLUMINATED. INSPECTION TYPE:NA**SUPPLEMENTAL SDR** DURING CLIMBOUT L ENG FIRE LP 1 STATUS MESSAGE DISPLAYED. DURING LEVEL FIGHT MESSAGE DISAPPEARED.T/S PER FIM 26-11-00-815
- [SDR IPXA2021112876388](https://openairdocs.org/sdr/IPXA2021112876388), Nov 28, 2021: NONE. NONE. INSPECTION TYPE:N/AMAIN CARGO COMPT FLOOR PANEL REPAIR POS 2R DELAMINATION UPPER SKINREPAIRED PER EO B767-5320-9693-I
- [SDR IPXA2021021665731](https://openairdocs.org/sdr/IPXA2021021665731), Feb 15, 2021: WARNING MESSAGE. FALSE ACTIVATION. EMERG DECLARED - NO EMERG EQUIP USED. ** ON CLIMB OUT GOT AFT CARGO DOOR EICAS MESSAGE AND CARGO DOOR OVERHEAD LIGHT. DEFERRED AFT CARGO DOOR INDICATION & C/W D
- [SDR IPXA2020092760669](https://openairdocs.org/sdr/IPXA2020092760669), Sep 27, 2020: SKIN. DENTED. INSPECTION TYPE: N/A DENT ON LOWER SKIN OF AFT FLAP. REPAIRED IN ACCORDANCE WITH B767-5750-77322-B.
- [SDR IPXA2020040653911](https://openairdocs.org/sdr/IPXA2020040653911), Apr 5, 2020: FLOORBOARD. DAMAGED. INSPECTION TYPE:N/AMCD FLOOR BOARD AT POS 2 RT SIDE DMGEDFABRICATED NEW FLOOR BOARD AT MCD POS 1/2 AGAINST RT SIDE WALL PER EO B767-5320-9693-I
- [SDR IPXA2019073145148](https://openairdocs.org/sdr/IPXA2019073145148), Jul 31, 2019: LENS. UNSECURE. INSPECTION TYPE:N/A EXIT LIGHT COVER WILL NOT STAY SECURE. R&R EXIT SIGN LENS COVER PER AMM 33-57-01. ESR: IPC 52-11-02-10-A ITEM 075.
- [SDR IPXA2019041984177](https://openairdocs.org/sdr/IPXA2019041984177), Apr 17, 2019: LENS. DETACHED. FOUND DURING PS1 CHECK,ENTRY DOOR EMERGENCY EXIT SIGN LENS DETACHEDLENS RESECURED IAW AMM 33-51-01 REV126.01
- [SDR IPXA2019010537522](https://openairdocs.org/sdr/IPXA2019010537522), Dec 27, 2018: STIFFENER. CRACKED. INSPECTION TYPE:C11 CRACK ON VERTICAL STIFFENER AT WHEEL WELL BULKHEAD AT STA 287, LBL 25, WL 159. EO B767-5310-20118-F AND SRM 51-70-12 GENERAL, FIGURE 1, REV 
- [SDR IPXA2019010737584](https://openairdocs.org/sdr/IPXA2019010737584), Dec 27, 2018: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C11 DAMAGE ON M/D CARGO FLOOR PANEL AT STA 930 - STA 972, RBL 55 - RBL 77, PNL NR 242LFF. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR B767-5
- [SDR IPXA2019010737583](https://openairdocs.org/sdr/IPXA2019010737583), Dec 27, 2018: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C11 DAMAGE ON M/D CARGO FLOOR PANEL AT STA 412 - STA 533, LBL 33- LBL 55, PNL NR 231CFF. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR B767-53
- [SDR IPXA2019010737582](https://openairdocs.org/sdr/IPXA2019010737582), Dec 27, 2018: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C11 DAMAGE ON M/D CARGO FLOOR PANEL AT STA 412 - STA 533, LBL 11 - LBL 33, PNL NR 231BFF. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR B767-5
- [SDR IPXA2019010737581](https://openairdocs.org/sdr/IPXA2019010737581), Dec 27, 2018: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C11 DAMAGE ON M/D CARGO FLOOR PANEL AT STA 412 - STA 533, RBL 11 - RBL 33, PNL NR 232AFF. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR B767-5
- [SDR IPXA2019010737580](https://openairdocs.org/sdr/IPXA2019010737580), Dec 27, 2018: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C11 DAMAGE ON M/D CARGO FLOOR PANEL AT STA 412 - STA 533, RBL 33 - RBL 55, PNL NR 232BFF.FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR B767-53
- [SDR IPXA2019010737578](https://openairdocs.org/sdr/IPXA2019010737578), Dec 27, 2018: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C11 DAMAGE ON M/D CARGO FLOOR PANEL AT STA 533 - STA 654 PLUS 22, LBL 55 - LBL 77, PNL NR 231JFF. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO N

All 143: https://openairdocs.org/aircraft/N316UP/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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