# N310UP: 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: 27762
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 8, 1996
- Certificate issued: October 11, 1996
- Expires: August 31, 2028
- Mode S code: A348A1
- 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=310UP
- Page: https://openairdocs.org/aircraft/N310UP

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/N310UP/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 N310UP.

## FAA accident and incident reports

None matched to N310UP.

## Service difficulty reports (169, 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 IPXA2026072859394](https://openairdocs.org/sdr/IPXA2026072859394), Jul 25, 2026: UNKNOWN. ODOR. ON DEPARTURE @ HIGH POWER SETTINGS STRONG SMELL OF DIRTY SOCKS? ON THE FLIGHT DECK. STAY UNTIL PASSING 10000 COULD NOT DUPLICATE PROBLEM UNPIN ARRIVAL. T/S PER 
- [SDR IPXA2026070679800](https://openairdocs.org/sdr/IPXA2026070679800), Jun 3, 2026: SKIN. DENTED. DENT ON LEADING EDGE SLAT #7. VIEW ATTACHMENTS. WILL REQUIRE LINE MX 8 HOURS EXTEND AND LOTO L/E SLATS. S/M SHOP 40 HOURS TO REPAIR PER SRM 57-43-01-2R-2 RP. 2 
- [SDR IPXA2026040628817](https://openairdocs.org/sdr/IPXA2026040628817), Apr 3, 2026: A/C PACK. ODOR. ON TAKEOFF A PUNGENT SMELL ENTERD THE FLIGHT DECK. AFTER POWER REDUCTION, TURNED THE LEFT PACK OFF AND SMELL DISSAPATED. OPERATED L/H PACK SYSTEM FOR 30 MINUTES
- [SDR IPXA2025092255412](https://openairdocs.org/sdr/IPXA2025092255412), Sep 20, 2025: UNKNOWN. ODOR. ON DEPARTURE AT HIGH POWER SETTING STRONG SMELL OF DIRTY SOCK .SMELL DISSUPTED APPROX 10000FT. ++PERFORMED OPS CHECKS IAW FIM 21-00 TASK SUPPORT - AIR CONDITION
- [SDR IPXA2025072727420](https://openairdocs.org/sdr/IPXA2025072727420), Jul 8, 2025: SKIN PANEL. GOUGED. GROUND CREW REPORTS GOUGE ON DOUBLER OF PREVIOUSLY REPAIRED AREA OF DAMAGE ON THE LOWER FORWARD CARGO DOOR FRAME. FUSELAGE STATION 478, WL 121. INSTALLED LINER 
- [SDR IPXA2025020201790](https://openairdocs.org/sdr/IPXA2025020201790), Jan 21, 2025: RIB. CRACKED. L/H WING OUTBD L/E UPPER RIB LOWER CHORD, OSS 531.71 (REPLACE). REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 91. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV.
- [SDR IPXA2025020593203](https://openairdocs.org/sdr/IPXA2025020593203), Jan 20, 2025: STRAP. CORRODED. FAULT - A LOT OF SCREW HOLES OF CEILING SUPPORT CORROSION AT FWD CGO BETWEEN STA 478 TO STA 610, RBL 40 (REPLACE) 1.ACCOMPLISHED REPAIR I.A.W UPS EO-92566-REQ1 
- [SDR IPXA2025020591355](https://openairdocs.org/sdr/IPXA2025020591355), Jan 20, 2025: SUPPORT. CORRODED. FAULT - CORROSION - FOUND FWD CGO PNL SUPPORT CORROSION AT STA 654+110 ~ 654+121, RBL 70 (REPAIR) 1. REMOVED AFFECTED FASTENERS TO GET ACCESS I.A.W SRM 51-40-02
- [SDR IPXA2025020693211](https://openairdocs.org/sdr/IPXA2025020693211), Jan 20, 2025: CHANNEL. CORRODED. FAULT - CORROSION - FND AFT CGO RH CEILING PNL SUPPORT CORROSION BETWEEN STA 1197+132 TO STA 1351, RBL 63 (REPLACE) ACCOMPLISHED REPAIR I.A.W UPS EO NO: EO-9266
- [SDR IPXA2025020593206](https://openairdocs.org/sdr/IPXA2025020593206), Jan 20, 2025: STRAP. CRACKED. FAULT - CEILING SUPPORT CRACK AT FWD CGO STA 610, RBL 64 (REPLACE). ACCOMPLISHED REPAIR I.A.W UPS EO NO: EO-92665-REQ1 REV.1. JOB COMPLETED. REVIEWED.
- [SDR IPXA2025020290828](https://openairdocs.org/sdr/IPXA2025020290828), Jan 20, 2025: TEE FITTING. CRACKED. TEE CHORD AT STA 246 LBL 40 (REPAIR). ACCOMPLISHED REPAIR I.A.W UPS EO NO: EO-92600-REQ1 REV.1. JOB COMPLETED. ACCOMPLISHED REPAIR I.A.W UPS EO NO: EO-92666-REQ
- [SDR IPXA2025012193764](https://openairdocs.org/sdr/IPXA2025012193764), Jan 20, 2025: NONE. NONE. (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R). COMPLIED WITH EO-82173. CONDITION CHECK OK.
- [SDR IPXA2025012691492](https://openairdocs.org/sdr/IPXA2025012691492), Jan 20, 2025: LATCH. CORRODED. FAULT - CORROSION - LATCH, KEEL BEAM ACCESS PNL NO.149BL AFT LATCH INNER FACE. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 91.INSTALLED NEW PART I.A.W SRM 51
- [SDR IPXA2025011969709](https://openairdocs.org/sdr/IPXA2025011969709), Jan 18, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 143T5876-83 PANEL NO : 231GFF (REPAIR) 1.TO FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. 2.CONDITION CHE
- [SDR IPXA2025011969781](https://openairdocs.org/sdr/IPXA2025011969781), Jan 18, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 143T5876-81 PANEL NO : 231HFF (REPAIR) 1.TO FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. 2.CONDITION CHE
- [SDR IPXA2025011969787](https://openairdocs.org/sdr/IPXA2025011969787), Jan 18, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 143T5876-78 PANEL NO : 231AFF (REPAIR) 1.TO FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. 2.CONDITION CHE
- [SDR IPXA2025011969801](https://openairdocs.org/sdr/IPXA2025011969801), Jan 18, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 143T5876-84 PANEL NO : 232FFF (REPAIR) 1.TO FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. 2.CONDITION CHE
- [SDR IPXA2025011966777](https://openairdocs.org/sdr/IPXA2025011966777), Jan 18, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 146T5869-19 PANEL NO : 232OFF (REPAIR) 1.TO FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. 2.CONDITION CHE
- [SDR IPXA2025011969803](https://openairdocs.org/sdr/IPXA2025011969803), Jan 18, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 143T5876-77 PANEL NO : 231BFF (REPAIR) 1.TO FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. 2.CONDITION CHE
- [SDR IPXA2025012169709](https://openairdocs.org/sdr/IPXA2025012169709), Jan 18, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 143T5876-83 PANEL NO : 231GFF (REPAIR) REQUEST PERFORM MAIN DECK CARGO FLOOR PANEL OK TO INSTALL CHECK.<BR> P/N:143T58
- [SDR IPXA2024121869082](https://openairdocs.org/sdr/IPXA2024121869082), Dec 18, 2024: FMC. FAILED. *AIR TURN BACK* ATB LFMC FAIL QRH PROCEDURE COMPLETE BOTH ND DISPLAYS BLANKED, R FMC UNABLE TO LOAD NAV DATA, QRH BOTH FCM FAIL PROCEDURE. NO ACCESS TO ANY ROUT
- [SDR IPXA2024060320163](https://openairdocs.org/sdr/IPXA2024060320163), May 30, 2024: WINDOW. SCRATCHED. **SUPPLEMENTAL SDR** PILOT SIDE WINDOW HAS TOO MANY SCRATCHES. VERY HARD TO SEE OUT OF IT WHEN SUN HITS IT. OS VISION. REMOVED AND REPLACED L2 WINDOW IAW AMM 56
- [SDR IPXA2024053120163](https://openairdocs.org/sdr/IPXA2024053120163), May 30, 2024: WINDOW. SCRATCHED. **SDR FILED OPEN** PILOT SIDE WINDOW HAS TOO MANY SCRATCHES. VERY HARD TO SEE OUT OF IT WHEN SUN HITS IT. OS VISION.
- [SDR IPXA2024032667475](https://openairdocs.org/sdr/IPXA2024032667475), Mar 26, 2024: UNKNOWN. LEAKING. FUEL LEAKING FROM LEFT ENGINE ACCOMPLISHED LEFT ENGINE RUN AT IDLE (CREW RAN IT) AS PER B767 71-00-00 TEST NO.3 IDLE LEAK CHECK AND CHECKED DRAINS PER B767 AMM 
- [SDR IPXA2023021290912](https://openairdocs.org/sdr/IPXA2023021290912), Feb 10, 2023: BATTERY. NO TEST. INSPECTION TYPE:C14FOUND EMERGENCY LIGHT POWER SUPPLY DEEP CYCLING TEST FAIL.1.I.A.W AMM 33-51-07-022-001 AND 33-51-07-422-012 REV.138.01 REPLACED EMERGENCY LIG
- [SDR IPXA2023021090850](https://openairdocs.org/sdr/IPXA2023021090850), Feb 9, 2023: SKIN. CRACKED. INSPECTION TYPE:C14*MAJOR REPAIR* CRACK WAS FOUND ON RH SKIN(P/N:148T3121-2)AT STA 1725.5,S-7R.REPAIR I.A.W 767-300F SRM 53-80-01 REPAIR 5,DETAIL III,REV.85.01
- [SDR IPXA2023020490595](https://openairdocs.org/sdr/IPXA2023020490595), Jan 31, 2023: ANGLE. CRACKED. INSPECTION TYPE:C14CRACK ON ANGLE(P/N:146T5651-6)OF CANTILEVER INSTL IN BULK CARGO COMPARTMENT AT STA 1578,RBL 60.REPLACE THE PART PER 767-300F SRM 51-40-02-0G,
- [SDR IPXA2023020490594](https://openairdocs.org/sdr/IPXA2023020490594), Jan 31, 2023: ANGLE. CRACKED. INSPECTION TYPE:C14CRACK ON ANGLE(P/N:146T5651-5)OF CANTILEVER INSTL IN BULK CARGO COMPARTMENT AT STA 1578,LBL 60.REPLACE THE PART PER 767-300F SRM 51-40-02-0G,
- [SDR IPXA2023020790724](https://openairdocs.org/sdr/IPXA2023020790724), Jan 30, 2023: SKIN. CRACKED. INSPECTION TYPE:C14*MAJOR REPAIR* CRACK ON NOSE SKIN (P/N: 114T4104-4) OF NO. 9 SLAT AT OSS 572.55REPAIR I.A.W. 767-300F SRM 57-43-01-2R-2 REV.85.01.
- [SDR IPXA2023020690650](https://openairdocs.org/sdr/IPXA2023020690650), Jan 30, 2023: NOT REPORTED. DAMAGED. INSPECTION TYPE:C14DAMAGE ON M/D CGO FLOOR BEAM SUPPORT AT STA 246,LBL 40.REPLACE PART I.A.W 767-300F SRM 51-40-02-0G REV.85.01 AND BOEING DWG NO.141T5600SHEET 
- [SDR IPXA2022101287098](https://openairdocs.org/sdr/IPXA2022101287098), Oct 12, 2022: INDICATOR. INOPERATIVE. **ATB**-SUSPECT L MAIN FUEL INDICATOR GIVING INACCURATE INDICATIONS. POSSIBLE FUEL LEAK. NO FUEL LEAK DETECTED. DEFERRED RH FUEL QTY INDICATION INOP PER MEL 28-
- [SDR IPXA2022012678291](https://openairdocs.org/sdr/IPXA2022012678291), Jan 25, 2022: NONE. NONE. INSPECTION TYPE:NASUPPLEMENATAL ATB SDR FILED * NO EMERG DEC'D* CRUISE, FUEL CONFIG LIGHT/INDICATIONS & DROPPING FUEL QTY IN R MN TANK. FUEL QTY FLUCTUATED, THE
- [SDR IPXA2021122977388](https://openairdocs.org/sdr/IPXA2021122977388), Dec 29, 2021: NONE. NONE. INSPECTION TYPE:N/A** SUPPLEMENTAL SDR ** DIVERSION ** IFSD** FL 370 GOT FUEL CONFIG EICAS RIGHT ENG FUEL QUANTITY DROPPING L12.5 R 6.5 ALSO GOT FUEL DISAGREE O
- [SDR IPXA2021021665720](https://openairdocs.org/sdr/IPXA2021021665720), Feb 3, 2021: STIFFENER. CRACKED. INSPECTION TYPE:C13CRACK ON CENTER WING TANK STIFFENER(P/N:111T2005-7) ON STA 785.9,LBL 11.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.79.01 AND UPS EO
- [SDR IPXA2021021665719](https://openairdocs.org/sdr/IPXA2021021665719), Feb 3, 2021: STIFFENER. CRACKED. INSPECTION TYPE:C13CRACK ON CENTER WING TANK STIFFENER(P/N:111T2005-8) ON STA 785.9,RBL 11.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.79.01 AND UPS EO
- [SDR IPXA2019122450353](https://openairdocs.org/sdr/IPXA2019122450353), Dec 21, 2019: CIRCUIT CARD. MALFUNCTIONED. FWD CARGO DOOR EICAS AND LT ILLUM AFTER TAKEOFF AT APPROX 4000 FT AGL, COMPLETED QRN PROD. RETURNED TO DEPARTURE AIRPORTT/S AND FOUND CODE "006" ON PSEU BITE CK
- [SDR IPXA2019020438590](https://openairdocs.org/sdr/IPXA2019020438590), Jan 26, 2019: STIFFENER. CRACKED. INSPECTION TYPE:C12CRACK ON THE CENTER WING FRONT SPAR STIFFENER(P/N:111T2008-12 ) UPPER SIDE AT STA 785.9, RBL 33.REPAIR I.A.W. 767-300F SRM 57-10-10-2R-2 REPA
- [SDR IPXA2018090733665](https://openairdocs.org/sdr/IPXA2018090733665), Sep 5, 2018: VALVE. DEFECTIVE. WHEN PARKING BRAKE WAS SET, WITH BRAKE LIGHT ON AND WHITE PARKING BRAKE LIGHT ON, ACFT ROLLED FWD 1 1/2 FEET. RESET BRAKE AND IT SELF RELEASED 3 TIMES. REMOVED 
- [SDR IPXA2018032927976](https://openairdocs.org/sdr/IPXA2018032927976), Mar 29, 2018: ACOUSTIC LINER. PUNCTURED. RIGHT ENGINE HAS SMALL HOLE IN FWD FAN CASE LINER ON PANEL 5,M APPROXIMATELY 8 INCHES FROM LOWER EDGE AND 15/16 INCH AFT PANEL EDGE 11/16 INCH LONGX 5/16 TALL. 
- [SDR IPXA2018010425113](https://openairdocs.org/sdr/IPXA2018010425113), Jan 3, 2018: PANEL. INFLT SEPARATION. L/E THERMAL ANTI-ICE PANEL MISSING FROM RT WING NR 10 SLAT, THE PANEL 624AT DEPARTED THE ACFT. REPLACED L/E ANTI-ICE PANEL IAW AMM 57-41-01-404-003, CHECKED OK,
- [SDR IPXA2017080620164](https://openairdocs.org/sdr/IPXA2017080620164), Aug 5, 2017: RIB. DEBONDED. NR 2 ENGINE RT THRUST REVERSER INNER BARREL ZEE RIB DISBONDED, THIRD INNER BARREL FRAME. COMPLIED WITH EO B767-78-30-65175-A.
- [SDR IPXA2017031415103](https://openairdocs.org/sdr/IPXA2017031415103), Mar 9, 2017: ROLLER TRAY. CORRODED. INSPECTION TYPE: C11, CORROSION ON AFT CARGO ROLLER TRAY AT BS 1197 + 44 TO 1197 + 132, RBL 6.5. REPLACED THE ROLLER TRAY.
- [SDR IPXA2017031415102](https://openairdocs.org/sdr/IPXA2017031415102), Mar 9, 2017: ROLLER TRAY. CORRODED. INSPECTION TYPE: C11, CORROSION ON AFTER CARGO ROLLER TRAY AT BS 1197 + 44 TO 1197 + 132, RBL 20. REPLACED THE ROLLER TRAY.
- [SDR IPXA2017031415106](https://openairdocs.org/sdr/IPXA2017031415106), Mar 7, 2017: BULKHEAD. CORRODED. INSPECTION TYPE: C11, CORROSION ON PRESSURE BULKHEAD CENTER UPPER SIDE AT BS 1809, BL 0. REPAIRED THE BULKHEAD.
- [SDR IPXA2017031415105](https://openairdocs.org/sdr/IPXA2017031415105), Mar 7, 2017: SPLICE. CORRODED. INSPECTION TYPE: C11, CORROSION ON KEEL BEAM SPLICE TEE AT BS 916, BL 0. THE SPLICE WAS REPLACED.
- [SDR IPXA2017031415104](https://openairdocs.org/sdr/IPXA2017031415104), Mar 7, 2017: SPLICE. CORRODED. INSPECTION TYPE: C11, CORROSION ON THE FUSELAGE KEEL BEAM SPLICE TEE, BS 962, BL 0. REPLACED THE KEEL. SPLICE TEE
- [SDR IPXA2017031315037](https://openairdocs.org/sdr/IPXA2017031315037), Mar 7, 2017: PANEL. CORRODED. INSPECTION TYPE: C11, CORROSION ON FUSELAGE KEEL BEAM PANEL 149BL NEAR BS 1013, LBL 6. PART REPLACED
- [SDR IPXA2017031515161](https://openairdocs.org/sdr/IPXA2017031515161), Mar 5, 2017: CHANNEL. CORRODED. INSPECTION TYPE: C11, CORROSION ON MOP SILL OF MAIN DECK CARGO FLOOR BS 1605, LBL 54. REPLACED THE MOP SILL.
- [SDR IPXA2017031515160](https://openairdocs.org/sdr/IPXA2017031515160), Mar 5, 2017: FLOOR SUPPORT. CORRODED. INSPECTION TYPE: C11, CORROSION ON THE FLOOR SUPPORT OF MAIN DECK CAGRO BS 1605, LBL 54. REPLACED THE FLOOR SUPPORT.
- [SDR IPXA2016061704751](https://openairdocs.org/sdr/IPXA2016061704751), Jun 17, 2016: WARNING SYSTEM. FALSE ACTIVATION. EMERGENCY DECLARED ON APPROACH. ANTI-SKID LIGHT ON APPROACH, RAN CHECKLIST. DEFERRED ANTI-SKID SYSTEM IAW MEL 32-42-1-0-1 AND C/W CMP-32-42-1-0-1, INSTALLED CIR

All 169: https://openairdocs.org/aircraft/N310UP/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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