# N308UP: 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: 27761
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 4, 1996
- Certificate issued: September 6, 1996
- Expires: May 31, 2028
- Mode S code: A33EDA
- 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=308UP
- Page: https://openairdocs.org/aircraft/N308UP

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/N308UP/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 N308UP.

## FAA accident and incident reports

None matched to N308UP.

## Service difficulty reports (175, 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 IPXA2026062330088](https://openairdocs.org/sdr/IPXA2026062330088), Jun 12, 2026: HANDLE. BROKEN. BULK CAGO DOOR EXTERIOR HANDLE IS BROKEN. R&R BULK CARGO DOOR LATCH ASSY IAW AMM 52-36-07, OPS CHECK GOOD. REVERSED DMP, REMOVED PLACARD THIS CLEARS MEL 52=36-1
- [SDR IPXA2026061230088](https://openairdocs.org/sdr/IPXA2026061230088), Jun 12, 2026: HANDLE. BROKEN. BULK CAGO DOOR EXTERIOR HANDLE IS BROKEN. C/W DMP. DEFERRAL ADDED.
- [SDR IPXA2026032397630](https://openairdocs.org/sdr/IPXA2026032397630), Mar 21, 2026: ACTUATOR. BROKEN. EMERGENCY DECLARED, LEVEL AT 15,000 JUST PRIOR TO DESCENT, SMELLED SMOKE AND SAW A LIGHT BLUE HUE IN THE COCKPIT. DECLARED AN EMERGENCY AND WENT THRU SMOKE IN C
- [SDR IPXA2025120337341](https://openairdocs.org/sdr/IPXA2025120337341), Dec 3, 2025: WARNING MESSAGE. FALSE ACTIVATION. EMERGENCY DECLARED, LE SLAT ASYM AT FL 340 FOUND LE SLAT ASYM EICAS MSG AND LEADING EDGE LIGHT ON, PERFORMED PSEU BITE IAW FIM 27-51 FAULT TREE 803 REV.146, FOU
- [SDR IPXA2025070198049](https://openairdocs.org/sdr/IPXA2025070198049), Jun 30, 2025: WARNING LIGHT. FALSE ACTIVATION. FUEL CONFIGURATION ANNUNCIATOR LIGHT ILLUMINATED AFTER REACHING CRUISE AT 36000€™ DUE TO AN IMBALANCE BETWEEN LEFT MAIN AND RT MAIN TANK.(RT TANK LOWER THAN LE
- [SDR IPXA2025041486761](https://openairdocs.org/sdr/IPXA2025041486761), Apr 13, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 143T5876-84 PANEL NO.232FFF (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 53-01-06-400
- [SDR IPXA2025041872949](https://openairdocs.org/sdr/IPXA2025041872949), Apr 12, 2025: SKIN. CORRODED. CORROSION - SKIN, AFT CARGO NEAR STA 1395, BETWEEN S-32R AND S-33R. (REPAIR). I.A.W AMM 25-53-15-404-011 REV.144 AND AMM 25-53-02-404-004 REV.144 INSTALLED SIDE
- [SDR IPXA2025041752135](https://openairdocs.org/sdr/IPXA2025041752135), Apr 11, 2025: ANGLE. CRACKED. FOUND CRACK-ANGLE, BULK CGO CEILING AREA STA 1577 RBL 74 INBD SIDE (REPLACE) 1.I.A.W AMM 53-01-06-400-801 REV.144 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDIT
- [SDR IPXA2025041750805](https://openairdocs.org/sdr/IPXA2025041750805), Apr 11, 2025: ANGLE. CRACKED. FOUND CRACK-ANGLE, BULK CGO CEILING AREA, STA 1577 RBL 74 OUTBD SIDE (REPLACE) I.A.W AMM 25-59-01-404-019 REV.144 INSTALL MAIN DECK CARGO DADO PANEL AT STA 1578
- [SDR IPXA2025041152818](https://openairdocs.org/sdr/IPXA2025041152818), Apr 11, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N:143T5876-49 PANEL NO:231FFF (REPAIR).FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 53-01-06-400-8
- [SDR IPXA2025041151123](https://openairdocs.org/sdr/IPXA2025041151123), Apr 11, 2025: FLOOR PANEL. DAMAGED. MAJOR REPAIR. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N:143T5876-83 PANEL NO.231GFF (REPAIR) I.A.W AMM 53-01-06-400-801 REV.144 INSTALL MAIN DECK CARGO FLOOR PANE
- [SDR IPXA2025041151150](https://openairdocs.org/sdr/IPXA2025041151150), Apr 11, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE P/N:143T5876-75 PANEL NO.231CFF (REPAIR) I.A.W AMM 53-01-06-400-801 REV.144 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION
- [SDR IPXA2025041151972](https://openairdocs.org/sdr/IPXA2025041151972), Apr 11, 2025: FLOOR PANEL. DAMAGED. MAJOR REPAIR. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N:146T5869-88 PANEL NO.252UFF (REPAIR) I.A.W AMM 53-01-06-400-801 REV.144 INSTALL MAIN DECK CARGO FLOOR PANE
- [SDR IPXA2025041153541](https://openairdocs.org/sdr/IPXA2025041153541), Apr 11, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N:143T5876-73 PANEL NO:231DFF (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 53-01-06-400-
- [SDR IPXA2025041152808](https://openairdocs.org/sdr/IPXA2025041152808), Apr 11, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N:143T5876-81 PANEL NO:231HFF (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 53-01-06-400-
- [SDR IPXA2025041152206](https://openairdocs.org/sdr/IPXA2025041152206), Apr 11, 2025: FLOOR PANEL. DAMAGED. MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N:143T5876-77 PANEL NO.231BFF (REPAIR) I.A.W AMM 53-01-06-400-801 REV.144 INSTALL MAIN DECK CARGO FLOOR PANE
- [SDR IPXA2025041153552](https://openairdocs.org/sdr/IPXA2025041153552), Apr 11, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N:143T5876-79 PANEL NO:231JFF (REPAIR). I.A.W AMM 53-01-06-400-801 REV.144 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITI
- [SDR IPXA2025041730076](https://openairdocs.org/sdr/IPXA2025041730076), Apr 10, 2025: SKIN PANEL. CRACKED. CRACK, FWD ENTRY DOOR AFT LOWER CORNER SKIN (REPAIR) I.A.W AMM 25-80-00-400-803 REV.144 INSTALL MAIN DECK CARGO INSULATION AT STA 343 ~ 368 AND CONDITION CHECK 
- [SDR IPXA2025041129383](https://openairdocs.org/sdr/IPXA2025041129383), Apr 10, 2025: FLOOR PANEL. DAMAGED. MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N:146T5869-89 PANEL NO:251XFF (REPAIR) I.A.W AMM 53-01-06-400-801 REV.144 INSTALL MAIN DECK CARGO FLOOR PANE
- [SDR IPXA2025041706768](https://openairdocs.org/sdr/IPXA2025041706768), Apr 9, 2025: STIFFENER. CRACKED. MAJOR REPAIR, CRACK-STIFFENER, FWD CARGO STA 785.9 RBL 54.81.(REPAIR) I.A.W AMM 53-01-06-400-801 REV.144 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK
- [SDR IPXA2025021161356](https://openairdocs.org/sdr/IPXA2025021161356), Feb 9, 2025: BATTERY PACK. NO TEST. *SUPPLEMENTAL SDR* EMERGENCY LIGHT TEST FAILED. NO LIGHTS TURN ON R&R EMERGENCY LIGHT BATTERY IAW AMM 33-51-07. OPS CHECKS GOOD
- [SDR IPXA2025021061356](https://openairdocs.org/sdr/IPXA2025021061356), Feb 9, 2025: BATTERY PACK. NO TEST. EMERGENCY LIGHT TEST FAILED. NO LIGHTS TURN ON R&R EMERGENCY LIGHT BATTERY IAW AMM 33-51-07. OPS CHECKS GOOD
- [SDR IPXA2025012822462](https://openairdocs.org/sdr/IPXA2025012822462), Jan 28, 2025: SWITCH. FAULTED. EMER LIGHTS REPOSITIONED RETAINING CLIP ON EMERGENCY LIGHT GUARDED SWITCH. EMER LIGHTS OPS NORMAL IN ALL THREE SWITCH POSITIONS REF AMM 33-51-00.
- [SDR IPXA2024100454655](https://openairdocs.org/sdr/IPXA2024100454655), Sep 28, 2024: ENGINE. LEAKING. ON DEPARTURE , AT HIGH POWER SETTING, STRONG SMELL OF DIRTY SOCKS? ON FLIGHT DECK. DISSIPATED AFTER POWER REDUCTION T/S PER B767 FIM79-21FAULT TREE 807,PERFROME
- [SDR IPXA2024093054655](https://openairdocs.org/sdr/IPXA2024093054655), Sep 28, 2024: ENGINE. LEAKING. ON DEPARTURE , AT HIGH POWER SETTING, STRONG SMELL OF DIRTY SOCKS? ON FLIGHT DECK. DISSIPATED AFTER POWER REDUCTION T/S PER B767 FIM79-21FAULT TREE 807,PERFROME
- [SDR IPXA2024092345726](https://openairdocs.org/sdr/IPXA2024092345726), Sep 22, 2024: PITOT TUBE. WARNING MESSAGE. *** DIVERSION *** R AUX PITOT ANNUNCIATED AFTER ROTATION DURING TAKEOFF. RESULTED IN DIVERSION TO KONT REMOVED AND REPLACED RH AUX PITOT PROBE IAW AMM 34-11-01.
- [SDR IPXA2024072662192](https://openairdocs.org/sdr/IPXA2024072662192), Jul 17, 2024: CONNECTOR. DAMAGED. DURING T/S OF FLAP / SLAT ELEC STATUS MESSAGE FOUND BURNED PINS ON PLUG D464 (S28 AIR HYD PUMP PRESS SWITCH) SECURED D464 WITH CONNECTOR BACC63BP12R3S10 IAW WDM
- [SDR IPXA2024071862192](https://openairdocs.org/sdr/IPXA2024071862192), Jul 17, 2024: CONNECTOR. BURNED. *** DIVERSION *** SDR FILED OPEN *** DURING T/S OF FLAP / SLAT ELEC STATUS MESSAGE FOUND BURNED PINS ON PLUG D464 (S28 AIR HYD PUMP PRESS SWITCH) DEFERRED ADP I
- [SDR IPXA2024030497753](https://openairdocs.org/sdr/IPXA2024030497753), Feb 28, 2024: PUMP. FAULTED. *** DIVERSION *** SUPPLEMENTAL SDR *** AT FL 360 WE HAD A LEFT HYD DEM PUMP. WE NOTICED THE LEFT HYD QTY DROPPING RAPIDLY. EVENTUALLY THE LEFT HYD QTY EICAS CAM
- [SDR IPXA2024022897753](https://openairdocs.org/sdr/IPXA2024022897753), Feb 28, 2024: TUBE. BROKEN. *SDR FILED OPEN* *DIVERSION* AT FL 360 WE HAD A LEFT HYD DEM PUMP. WE NOTICED THE LEFT HYD QTY DROPPING RAPIDLY. EVENTUALLY THE LEFT HYD QTY EICAS CAME ON. WE T
- [SDR IPXA2023051877478](https://openairdocs.org/sdr/IPXA2023051877478), May 10, 2023: ANGLE. CRACKED. FAULT - CRACK - ANGLE, AFTER CARGO FORWARD BULKHEAD LH FLOOR BEAM SUPPORT ANGLE STA 1087 LBL 26. (REPLACE). INSTALL NEW PART I.A.W SRM 51-40-02-0G REV 86.00 AND
- [SDR IPXA2023050845302](https://openairdocs.org/sdr/IPXA2023050845302), May 6, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - FOUND CREW ENTRY DOOR AFT SIDE DOORWAY LOWER RETAINER ASSY BROKEN. (REPLACE) OK TO WORK
- [SDR IPXA2023041092773](https://openairdocs.org/sdr/IPXA2023041092773), Apr 9, 2023: DOOR. INOPERATIVE. INSPECTION TYPE:NACREW ENTRY DOOR CLOSED SENSOR S194 WIRES CHAFFED AT SENSOR.REMOVED AND REPLACED DOOR CLOSED SENSOR S194 W/REF TO B767 MM 52-71-01-401, OPS CK 
- [SDR IPXA2023022291242](https://openairdocs.org/sdr/IPXA2023022291242), Feb 22, 2023: CONTROL UNIT. NONE. INSPECTION TYPE:N/A**ATB** DURING TAKEOFF ROLL AT ABOUT 115-120 KTS ANTISKID EICAS MESSAGE ILLUMINATED. CONTINUED THE TAKEOFF ROLL AND RUN ANTISKID CHECKLIST IA
- [SDR IPXA2022092886677](https://openairdocs.org/sdr/IPXA2022092886677), Sep 28, 2022: PUMP. FAULTED. AIR TURN BACK, ON CLIMB OUT L HYD DEMAND PUMP EICAS MESSAGE FOLLOWED QRH PROCEDURE SHUT AFFECTED PUMP OFF RETURNED TO ICN PER MMOC.T/S PER FIM 29-11-00-815-806.
- [SDR IPXA2021071271549](https://openairdocs.org/sdr/IPXA2021071271549), Jul 9, 2021: BRACKET. BENT. INSPECTION TYPE:NAL1 DOOR SENSOR BRACKET HAS BENTR&R L1 DOOR SENSOR BRACKET IAW AMM 20-11-00. SENSOR ADJUSTEMENT WAS VERIFIED ON TC 52-000-100, IPC: 52-11-01-10
- [SDR IPXA2021051269313](https://openairdocs.org/sdr/IPXA2021051269313), May 6, 2021: SEAT TRACK. CORRODED. INSPECTION TYPE:C13CORROSION ON TRACK (P/N:143T5243-10) OF MAIN DECK CARGO COMPARTMENT NEAR STA 513 TO STA 595 , RBL 88.5.REPAIR I.A.W. SR :4-5078180888 AND EO 
- [SDR IPXA2021051269312](https://openairdocs.org/sdr/IPXA2021051269312), May 5, 2021: SKIN. WORN. INSPECTION TYPE:C13WORN FASTENER HOLE ON THE NO.3 SLAT SKIN (P/N:114T4103-3) NEAR OSS 723.941.REPAIR I.A.W. 767-300F SRM 57-43-01-2R-2 REV.80.00
- [SDR IPXA2021041468204](https://openairdocs.org/sdr/IPXA2021041468204), Apr 14, 2021: AUTOBRAKE SYS. INOPERATIVE. INSPECTION TYPE:NA**SDR FILED OPEN** UPON PUSHBACK AUTO BRAKES WOULD NOT ARM IN RTO POS. AUTO BRK SYS/AUTO BRK (LT NOT ILLUMINATED).C/W MEL:32-42-4-1A.
- [SDR IPXA2020040353834](https://openairdocs.org/sdr/IPXA2020040353834), Apr 2, 2020: LIGHT. INOPERATIVE. INSPECTION TYPE:N/ADURING AS-E FOUND CEILING ENTRY EMERGENCY LT INOP.LAMP CORRECTED AND TESTED SATIS IAW AMM 33-51-11 R. 129.02
- [SDR IPXA2019081215534](https://openairdocs.org/sdr/IPXA2019081215534), Aug 11, 2019: UNKNOWN. ODOR. APPROX 1 HOUR INTO FLIGHT DETECTED HOT/OVERHEATED ELECTRICAL EQUIPMENT ODOR. NO SMOKE PRESENT IN COCKPIT OR CARGO COMT. ODOR LASTED APPROX ONE MINUTE THEN DISSI
- [SDR IPXA2019052542466](https://openairdocs.org/sdr/IPXA2019052542466), May 21, 2019: SKIN. CORRODED. INSPECTION TYPE:C12 CORROSION ON FUSELAGE SKIN NEAR STA 655, S-34L - S-35L. REPAIR IAW SRM 53-00-01 ALLOWABLE DAMAGE 1, REV 74.00.
- [SDR IPXA2019052542465](https://openairdocs.org/sdr/IPXA2019052542465), May 21, 2019: SKIN. CORRODED. INSPECTION TYPE:C12 CORROSION ON FUSELAGE SKIN NEAR STA 654 PLUS 128, S-34L - S-35L. REPAIR IAW SRM 53-00-01 ALLOWABLE DAMAGE 1, REV 74.00.
- [SDR IPXA2019052542469](https://openairdocs.org/sdr/IPXA2019052542469), May 15, 2019: STIFFENER. CRACKED. INSPECTION TYPE:C12 CRACK WAS FOUND ON STIFFENER (P/N:111T2011-5) OF CTR WING TANK FWD BULKHEAD, AT STA 785 LBL 55. REPAIR IAW EO B767-5740-58151-B.
- [SDR IPXA2019052542468](https://openairdocs.org/sdr/IPXA2019052542468), May 15, 2019: STIFFENER. CRACKED. INSPECTION TYPE:C12 CRACK WAS FOUND ON STIFFENER (P/N:111T2008-12) OF CTR WING TANK FWD BULKHEAD, AT STA 785 RBL 33. REPAIR IAW EO B767-5740-58151-B.
- [SDR IPXA2019052542467](https://openairdocs.org/sdr/IPXA2019052542467), May 15, 2019: STRINGER. CRACKED. INSPECTION TYPE:C12 CRACK WAS FOUND ON STRINGER S-20R (P/N:146T3443-3) BETWEEN STA 1540- STA 1562. REPAIR IAW SRM 53-00-03 REPAIR 5 DETAIL III REV 74.00.
- [SDR IPXA2019052642487](https://openairdocs.org/sdr/IPXA2019052642487), May 13, 2019: SKIN PANEL. DENTED. INSPECTION TYPE:C12 DENT WAS FOUND ON UPR SKIN (P/N:113T2320-5) OF LT WING INBD AFT FLAP NEAR IFS149. REPAIR IAW SRM 57-53-01 REPAIR 1 REV.74.00, SRM 51-70-10 R
- [SDR IPXA2019052642486](https://openairdocs.org/sdr/IPXA2019052642486), May 13, 2019: SKIN PANEL. DENTED. INSPECTION TYPE:C12 DENT WAS FOUND ON UPR SKIN (P/N:113T2320-5) OF LT WING INBD AFT FLAP NEAR IFS161. REPAIR IAW SRM 57-53-01 REPAIR 1 REV.74.00, SRM 51-70-10 R
- [SDR IPXA2019021539028](https://openairdocs.org/sdr/IPXA2019021539028), Feb 15, 2019: HANDLE. OBSTRUCTED. CREW ENTRY DOOR YELLOW RELEASE HANDLE DOES NOT WORK. DOOR CANNOT BE OPENED FROM THE OUTSIDE. REMOVED ICE FROM CREW ENTRY DOOR EXTERIOR HANDLE CUT-OUT. EXTERIOR 
- [SDR IPXA2018112636298](https://openairdocs.org/sdr/IPXA2018112636298), Nov 25, 2018: SENSOR. OUT OF TOLERANCE. CREW ENTRY DOOR PROXIMITY SENSOR CLEARANCE SENSOR S194 WAS OUT OF TOLERANCE AND IS MEASURING .100 AND IS TO BE BETWEEN 0.07 AND 0.08. ADJUSTED THE CLEARANCE ON 

All 175: https://openairdocs.org/aircraft/N308UP/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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