# N309UP: 1996 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: 27740
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 20, 1996
- Certificate issued: September 24, 1996
- Expires: May 31, 2028
- Mode S code: A34291
- 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=309UP
- Page: https://openairdocs.org/aircraft/N309UP

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/N309UP/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 N309UP.

## FAA accident and incident reports

None matched to N309UP.

## Service difficulty reports (172, 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 IPXA2026083182839](https://openairdocs.org/sdr/IPXA2026083182839), Aug 8, 2026: ESCAPE ROPE. UNWANTED DEPLOY. ESCAPE ROPE AT CREW ENTRY DOOR DEPLOYED. REPLACED FLIGHT COMPARTMENT DESCENT ROPE COVER ASSY AND REINSTALLED DESCENT ROPE PER AMM 25-61-04
- [SDR IPXA2026013054938](https://openairdocs.org/sdr/IPXA2026013054938), Jan 11, 2026: DRIVER UNIT. FAULTED. EMERGENCY DECLARED, CARGO DOOR INDICATION EICAS PERFORMED BITE TEST ON PSEU IAW FIM 32-09 FAULT TREE 803. FOUND INTERNAL PSEU DRIVER CARD 006 AND SENSOR 892 FAU
- [SDR IPXA2026011154938](https://openairdocs.org/sdr/IPXA2026011154938), Jan 11, 2026: WARNING MESSAGE. ILLUMINATED. EMERGENCY DECLARED. CARGO DOOR INDICATION EICAS ITEM PLACED ON MEL 52-71-1-2 ACCOMPLISHED DMP AND PLACARD INSTALLED
- [SDR IPXA2025071525054](https://openairdocs.org/sdr/IPXA2025071525054), Jul 2, 2025: SKIN. CORRODED. MAJOR REPAIR, CORROSION-SKIN, AFT CGO COMPT FWD SIDE LWR SKIN, NEAR STA 1081 S-39L~S-39R. ACCOMPLISHED REPAIR I.A.W UPS EO NO:EO-94375-REQ1 REV.1 AND BOEING DWG
- [SDR IPXA2025071524693](https://openairdocs.org/sdr/IPXA2025071524693), Jul 2, 2025: SHAFT. CORRODED. CORROSION AT LH SIDE NO.4 FLAP SUPPORT MECHANISM 6-6 OUTER SHAFT, STEP 3. PERFORM OK TO INSTASLL CHECK SATISFIED & INSTALL NEW LH WING NO.4 FLAP SUPPORT MECHANI
- [SDR IPXA2025071521351](https://openairdocs.org/sdr/IPXA2025071521351), Jul 2, 2025: CHANNEL. CORRODED. MAJOR REPAIR, CORROSION AT CARGO COMPARTMENT CEILING PANEL SUPPORT BETWEEN STA 1219 AND STA 1351 , RBL 63.5. ACCOMPLISHED CHANNEL REPAIR I.A.W UPS EO NO: EO-943
- [SDR IPXA2025071120737](https://openairdocs.org/sdr/IPXA2025071120737), Jul 2, 2025: SUPPORT. BROKEN. MAJOR REPAIR, BROKEN FORWARD CARGO COMPARTMENT CEILING SUPPORT AT STA 610 AND RBL 64.50. COMPLETED STRAP REPAIR IAW EO NR EO-94373-REQ1 REV1.
- [SDR IPXA2025070100627](https://openairdocs.org/sdr/IPXA2025070100627), Jul 1, 2025: FLOOR PANEL. DAMAGED. MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL DAMAGE, PANEL NR 231GFF. IAW AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL AND PERFORM G.V.I CHECK R
- [SDR IPXA2025070100576](https://openairdocs.org/sdr/IPXA2025070100576), Jul 1, 2025: FLOOR PANEL. DAMAGED. MAJOR REPAIR , FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 143T5876-90 PANEL NO.232JFF. IAW AMM 25-57-02-404-016 AND AMM 25-58-04-404-015 REV.145 INSTALLED MAIN DE
- [SDR IPXA2025070100773](https://openairdocs.org/sdr/IPXA2025070100773), Jul 1, 2025: FLOOR PANEL. DAMAGED. MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N:141T5856-13 PANEL 222DFF, IAW AMM 25-57-05-404-006, AMM 25-58-01-404-005 AND AMM 25-58-04-404-015 REV.145 
- [SDR IPXA2025070100572](https://openairdocs.org/sdr/IPXA2025070100572), Jul 1, 2025: FLOOR PANEL. DAMAGED. MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 143T5876-75 PANEL NO.231CFF. IAW AMM 25-57-02-404-016, AMM 25-58-01-404-005 AND AMM 25-58-05-404-052 REV.
- [SDR IPXA2025070100500](https://openairdocs.org/sdr/IPXA2025070100500), Jul 1, 2025: FLOOR PANEL. DAMAGED. MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL DAMAGE, PANEL NO.231AFF (REPAIR) 1.I.A.W AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL AND PERFORM G
- [SDR IPXA2025070885769](https://openairdocs.org/sdr/IPXA2025070885769), Jun 30, 2025: ANGLE. CRACKED. FOUND CRACK - ANGLE, BULK CGO COMPT CEILING AREA, STA 1577 RBL 74 INBD SIDE (REPLACE) I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.145 INSTALLED MAIN
- [SDR IPXA2025070885761](https://openairdocs.org/sdr/IPXA2025070885761), Jun 30, 2025: ANGLE. CRACKED. FOUND CRACK - ANGLE, BULK CGO COMPT CEILING AREA, STA 1577 RBL 74 OUTBD SIDE (REPLACE) I.A.W AMM 25-59-01-404-019 REV.145 INSTALL MAIN DECK CARGO DADO PANEL AND
- [SDR IPXA2025070185943](https://openairdocs.org/sdr/IPXA2025070185943), Jun 30, 2025: FLOOR PANEL. DENTED. MAJOR REPAIR, FOUND MAIN DECK CARGO FLOOR PANEL DENT AT PANEL NR 232NFF. IAW AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL AND PERFORM G.V.I C
- [SDR IPXA2025070186019](https://openairdocs.org/sdr/IPXA2025070186019), Jun 30, 2025: FLOOR PANEL. CRACKED. MAJOR REPAIR, FOUND MAIN DECK CARGO FLOOR PANEL CRACK AT PANEL NR 232BFF. IAW AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL AND PERFORM G.V.I 
- [SDR IPXA2025070185937](https://openairdocs.org/sdr/IPXA2025070185937), Jun 30, 2025: FLOOR PANEL. CRACKED. MAJOR REPAIR, FOUND MAIN DECK CARGO FLOOR PANEL CRACK AT NR 251XFF I.A.W AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL AND PERFORM G.V.I CHECK
- [SDR IPXA2025031297838](https://openairdocs.org/sdr/IPXA2025031297838), Mar 12, 2025: HEATER. INOPERATIVE. DURING PREFLIGHT, €ŒL SIDE WINDOW€? EICAS MESSAGE DISPLAYED. €ŒINOP€? LIGHT OBSERVED.CW ADDITIONAL 2 TORQUES OF WINDOW BOLTS REF AMM 56-11-10. VERIFIED WIRE
- [SDR IPXA2025021843128](https://openairdocs.org/sdr/IPXA2025021843128), Feb 3, 2025: SLIDING WINDOW. INOPERATIVE. CAPT. WINDOW ASSY-NO. 2 OPENABLE LH (CAPT.) WINDOW ASSY NR 2 OPENABLE INSPECTED IAW AMM 56-11-02/401 REV 144. TEST SATIS.
- [SDR IPXA2025020343128](https://openairdocs.org/sdr/IPXA2025020343128), Feb 3, 2025: WINDOW. LEAKING. CAPT. WINDOW ASSY-NO. 2 OPENABLE CAPTAIN WINDOW ASSY-NO.2 OPENABLE STILL HAS MOISTURE INGRESS/HAZING AFTER PERFORMING METHOD 2 (ALTERNATIVE) PER AMM 57-11-00-21
- [SDR IPXA2024082151039](https://openairdocs.org/sdr/IPXA2024082151039), Aug 20, 2024: WINDOW. DAMAGED. WINDOW R2 IS OPAQUE. DIFFICULT TO VIEW AT NIGHT. ESPECIALLY ON THE GROUND. AIR TRAFFIC HARD TO SEE AS WELL. R&R R2 WINDOW IAW AMM 56-11-02-404-026. OPS CHECK AN
- [SDR IPXA2024081357668](https://openairdocs.org/sdr/IPXA2024081357668), Aug 8, 2024: CONTROL PANEL. FAULTED. *** EMERGENCY DECLARED *** SUPPLEMENTAL SDR *** FL 370 CABIN ALT EICAS MESSAGE MODE SELECT WAS AUTO 2 WITH BOTH PACKS IN AUTO. CABINDIFFERENTIAL WAS APPROXIMATE
- [SDR IPXA2024080857668](https://openairdocs.org/sdr/IPXA2024080857668), Aug 8, 2024: OUTFLOW VALVE. FAULTED. *** EMERGENCY DECLARED *** SDR FILED OPEN *** FL 370 CABIN ALT EICAS MESSAGE MODE SELECT WAS AUTO 2 WITH BOTH PACKS IN AUTO. CABINDIFFERENTIAL WAS APPROXIMATELY
- [SDR IPXA2024080969072](https://openairdocs.org/sdr/IPXA2024080969072), Aug 8, 2024: PAWL. WORN. L FWD ENTRY DOOR WON€™T LATCH. FOUND EXTERIOR DOOR HANDLE CLOSING PAWL WORN, REPLACED SAME USING 20-11-00 AND 52-12-00 DOOR CLOSES NORMALLY AND ALL DOOR WARNIN
- [SDR IPXA2024040774919](https://openairdocs.org/sdr/IPXA2024040774919), Apr 6, 2024: SKIN. DAMAGED. L/E SKIN DAMAGE AT #1 SLAT O/B CURTAIN SEAL SCREW HOLES-L/E SKIN DAMAGE AT #1 SLAT O/B CURTAIN SEAL SCREW HOLES. DAMAGE TO UPPER SKIN CONSISTING ON 4 GOUGES, 2 
- [SDR IPXA2023082060594](https://openairdocs.org/sdr/IPXA2023082060594), Aug 20, 2023: CONTROL PANEL. UNKNOWN. CAB ALT AUTO1 STS MSG REF FIM 21-31 TASK 801 , 21-31 TASK 809 AND 21-31 FAULT TREE 803 CANBIN PRESSURE CONTROLLER BITE PROCEDURE . FOUND THE "SELECTOR" FAULT LT
- [SDR IPXA2023071004096](https://openairdocs.org/sdr/IPXA2023071004096), Jul 4, 2023: BATTERY. EXPIRED. FAULT - FOUND BATTERY PACK EXPIRY DATE JUN 30 (REPLACE) ++ I.A.W AMM 33-51-07-422-012 REV 139 PERFORMED BATTERY PACK TEST, RESULT WAS SATISFACTORY. REVIEW COMPL
- [SDR IPXA2022120788797](https://openairdocs.org/sdr/IPXA2022120788797), Dec 7, 2022: SHUTOFF VALVE. FAULTED. EICAS MESSAGE FWD EQPT VAL LIGHT ILLUMINATED ON CLIMB OUT. RAN QRH PROCEDURE EQUIPMENT VALVE SELECTOR TO STBY LIGHT EXTINGUISHED. R&R FDAR SHUTOFF VALVE PER MM 
- [SDR IPXA2022111488114](https://openairdocs.org/sdr/IPXA2022111488114), Nov 13, 2022: FLOOR PANEL. DAMAGED. MAIN CARGO POS 11 CENTER FLOOR PANEL REPAIRFLOOR BOARD POS 11 CENTERLINE ROUTED TO SHEET METAL FOR REPAIR, REF AMM 25-58-1. [JPC 1984163 11-12-22] THIS IS A MAJ
- [SDR IPXA2021062670984](https://openairdocs.org/sdr/IPXA2021062670984), Jun 26, 2021: BATTERY PACK. FAILED. INSPECTION TYPE:C13CREW REST MODULE(STC ST02568SE) - EMERGENCY LIGHT BATTERY PACK FAILED. REPLACED EMERGENCY LIGHT BATTERY PACK AND PERFORMED BATTERY PACK TEST,
- [SDR IPXA2021062670972](https://openairdocs.org/sdr/IPXA2021062670972), Jun 17, 2021: TEE FITTING. CORRODED. INSPECTION TYPE:C13CORROSION WAS FOUND ON 2EA SPLICE TEES (P/N:145T8629-3) OF FAIRING INSTL, KEEL BEAM NEAR STA 917, STA 962 BETWEEN RBL 10 - LBL 10.INSTALL NEW
- [SDR IPXA2021062670976](https://openairdocs.org/sdr/IPXA2021062670976), Jun 17, 2021: TEE FITTING. CORRODED. INSPECTION TYPE:C13CORROSION WAS FOUND ON SPLICE TEE(P/N: 145T8629-2) OF FAIRING INSTL, KEEL BEAM NEAR STA 872, BETWEEN RBL 10 - LBL 10.INSTALL NEW PART I.A.W. 
- [SDR IPXA2021062770996](https://openairdocs.org/sdr/IPXA2021062770996), Jun 14, 2021: SEAT TRACK. CORRODED. INSPECTION TYPE:C13CORROSION ON SEAT TRACK ON MAIN DECK CGO COMPARTMENT BETWEEN STA 434 AND STA 654, RBL 88.5REPAIR I.A.W. BOEING SR: 4-5138071445 AND UPS EO B7
- [SDR IPXA2021012965044](https://openairdocs.org/sdr/IPXA2021012965044), Jan 29, 2021: LIGHT. LOOSE. INSPECTION TYPE: NA O/H EMERGENCY LIGHT SW GUARD SPRING IS LOOSE. REMOVED & REPLACED EMERGENCY LIGHT PANEL. THEN EMERGENCY LIGHT FUNCTION CHECK SATISFIED. ALSO 
- [SDR IPXA2020081438999](https://openairdocs.org/sdr/IPXA2020081438999), Aug 11, 2020: SWITCH PANEL. INOPERATIVE. INSPECTION TYPE:N/AEMERG EXIT LIGHT WILL NOT DISARM.R&R EMERGENCY LIGHT SWITCH PANEL OPS CHK OK REF. AMM 33-51-08.
- [SDR IPXA2019103048466](https://openairdocs.org/sdr/IPXA2019103048466), Oct 29, 2019: PNEUMATIC SYSTEM. INOPERATIVE. INSPECTION TYPE:N/AAFTER INITIAL APU START, APU WOULD NOT SUPPLY PNEUMATIC AIR, APU OPERATION NORMAL AFTER SHUTDOWN & RESTARTED IAW AOM PROCEDURE.ACCOMPLISHED A
- [SDR IPXA2019062103530](https://openairdocs.org/sdr/IPXA2019062103530), Jun 13, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE: C12, DAMAGE ON M/D CARGO FLOOR PANEL 232FFF AT BS 533 - 654 +22 , RBL 11 - RBL 33 , FABRICATED A REPLACEMENT FLOOR PANEL PER EO NO. B767-5320-9
- [SDR IPXA201906213529](https://openairdocs.org/sdr/IPXA201906213529), Jun 11, 2019: FILLER. DAMAGED. INSPECTION TYPE: C12, BURN DAMAGE ON FILLER AND DOUBLER OF FWD UPR SPAR WEB ON #1 PYLON NEAR NAC STA 228.19.REPAIR IAW SRID : 4-4504150598 AND EO B767-5410-7296
- [SDR IPXA2019061943475](https://openairdocs.org/sdr/IPXA2019061943475), Jun 10, 2019: STIFFENER. CRACKED. INSPECTION TYPE:C12, CRACK ON THE CENTER WING FRONT SPAR STIFFENER. UPPER SIDE AT STA 785.9 , RBL55. REPAIR IAW SRM 57-10-10-2R-2 REPAIR 2 REV .74.00 AND EO B76
- [SDR IPXA2019062104531](https://openairdocs.org/sdr/IPXA2019062104531), Jun 9, 2019: FLOOR PANEL. DAMAGED. DAMAGE ON M/D CARGO FLOOR PANEL 231FFF AT STA 533 - STA 654 PLUS 22 , RBL 11 - LBL 11 , .FABRICATED A REPLACEMENT FLOOR PANEL PER EO B767-5320-9693-I.
- [SDR IPXA2018092654401](https://openairdocs.org/sdr/IPXA2018092654401), Sep 24, 2018: SKIN. PUNCTURED. LEFT INBD ELEVATOR UPPER SURFACE HAD A PUNCTURE, 21.75 INCHES FROM T/E AND 13 INCHES FROM THE INBD END, ELEVATOR STATION 61. REPAIRED THE SKIN IAW SRM 51-70-17-
- [SDR IPXA2016101909605](https://openairdocs.org/sdr/IPXA2016101909605), Oct 18, 2016: WARNING SYSTEM. FALSE ACTIVATION. INSPECTION TYPE:N/A, EMERGENCY DECLARED, RECEIVED IAS DISAGREE EICAS MSG. THEN RECEIVED AILERON LOCKOUT, EEC, RUDDER RATIO, ETC EICAS MSG. ACCOMPLISHED FIM 34-1
- [SDR IPXA2016032301151](https://openairdocs.org/sdr/IPXA2016032301151), Mar 23, 2016: CHARGER. INOPERATIVE. EMERGENCY EXIT LIGHTS COME ON INTERMITTENTLY WITH SWITCH IN ARMED POSITION. LIGHTS GO OUT WITH SWITCH OFF, REPLACED CHARGER ASSY AND TEST OK, IAW AMM 33-51-04, 
- [SDR IPXA2015063090668](https://openairdocs.org/sdr/IPXA2015063090668), Jun 18, 2015: STIFFENER. CRACKED. INSPECTION TYPE: C10, CRACK ON CENTER WING FRONT SPAR STIFFENER UPPER SIDE AT BS 785.9, LBL 11. REPAIR IAW SRM 57-10-10, REPAIR 2, REV 62, SRID 4-2928737651 AND
- [SDR IPXA2015063090667](https://openairdocs.org/sdr/IPXA2015063090667), Jun 18, 2015: STIFFENER. CRACKED. INSPECTION TYPE: C10, CRACK ON CENTER WING FRONT SPAR STIFFENER UPPER SIDE AT BS 785.9, RBL 33. REPAIR IAW SRM 57-10-10, REPAIR 2, REV 62, SRID : 4-2928737651 A
- [SDR IPXA2015063090666](https://openairdocs.org/sdr/IPXA2015063090666), Jun 18, 2015: STIFFENER. CRACKED. INSPECTION TYPE: C10, CRACK ON CENTER WING FRONT SPAR STIFFENER UPPER SIDE AT BS 785.9, LBL 33. REPAIR IAW SRM 57-10-10, REPAIR 2, REV 62, SRID: 4-2928737651 AN
- [SDR IPXA2015063090665](https://openairdocs.org/sdr/IPXA2015063090665), Jun 17, 2015: STRINGER. DAMAGED. INSPECTION TYPE:C10, CRACK DAMAGE ON LT SIDE FUSELAGE STRINGER S-20L AT BS 1511 AND BS 1518. REPAIR IAW SR 4-2916528521.
- [SDR IPXA2015020985625](https://openairdocs.org/sdr/IPXA2015020985625), Feb 9, 2015: FLOOR PANEL. DAMAGED. DAMAGED FLOOR PANEL MAIN DECK, PN 145T5876-82 FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H & EOB767-5320-56659.
- [SDR IPXA2014071483580](https://openairdocs.org/sdr/IPXA2014071483580), Jul 10, 2014: CONTROL UNIT. MALFUNCTIONED. ANTI-SKID EICAS AND LIGHT ILLUMINATED AT TOP OF CLIMB, FL 390. ALTN ANTI-SKID FAULT MESSAGE ALSO DISPLAYED. LIGHT AND EICAS EXTINGUISHED AFTER 25 MINUTES, ACFT 
- [SDR IPXA3678780](https://openairdocs.org/sdr/IPXA3678780), Jun 3, 2013: FLOOR PANEL. DENTED. INSPECTION TYPE:C09, DENT ON MAIN DECK CARGO FLOOR PANEL 232AFF AT BS 493, RBL 30. DIMENSIONS OF DAMAGE:1.5"L X 1.0" W. REPAIR IAW EO NR B767-5320-9693-H.

All 172: https://openairdocs.org/aircraft/N309UP/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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