# N311UP: 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: 27741
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 24, 1996
- Certificate issued: October 24, 1996
- Expires: August 31, 2028
- Mode S code: A34C58
- 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=311UP
- Page: https://openairdocs.org/aircraft/N311UP

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/N311UP/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 N311UP.

## 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.

- [Incident 20080529834149I](https://openairdocs.org/incident/20080529834149I), May 29, 2008: Boeing 76734AF (N311UP), Omaha, NE, No damage. (-23) N311UP, B767-34AF, was operated by united parcel service from anc-sdf as ups 109. The crew reported that the flight management computer was showing a…

## Service difficulty reports (171, 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 IPXA2026072316966](https://openairdocs.org/sdr/IPXA2026072316966), Jul 23, 2026: CONTROL PANEL. INOPERATIVE. EMERGENCY DECLARED, DIVERTED. RECEIVED CABIN ALT WARNING AT 40,000 FT. AUTO 1 AND AUTO 2 NOT WORKING. WAS ABLE TO REGAIN PRESSURIZATION CONTROL IN MANUAL MODE R
- [SDR IPXA2026052169974](https://openairdocs.org/sdr/IPXA2026052169974), May 20, 2026: SPRING. INOPERATIVE. EMER LIGHT GUARDED SWITCH SPRING INOP. REMOVED AND REPLACED EMER LIGHT PANEL IAW AMM 33-51-08. OPS CHECK GOOD.
- [SDR IPXA2026031820365](https://openairdocs.org/sdr/IPXA2026031820365), Mar 17, 2026: WINDOW. FAULTED. L FWD WINDOW EICAS ADVISORY SWAPPED AND CLEANED L FWD MAIN TEMPERATURE SENSORS TO SPARE SENSOR ON BLOCK TB322 IAW AMM 30-41-00-968-001. PERFORMED OPS IAW AMM 30
- [SDR IPXA2025112983935](https://openairdocs.org/sdr/IPXA2025112983935), Nov 28, 2025: PUMP. LEAKING. *** AIR TURN BACK *** SUSPECT FUEL LEAK L SIDE. RAN QRH. TOTALIZER GOT UP TO 2.2 LESS THAN CALCULATED FUEL. AS WELL AS LEFT MAIN TANK 2.0 LESS THAN R MAIN TANK 
- [SDR IPXA2025032270655](https://openairdocs.org/sdr/IPXA2025032270655), Mar 15, 2025: CYLINDER. CORRODED. **SUPPLEMENTAL SDR** FAULT - CORROSION - FOUND CORROSION ON INNER SURFACE OF R/H MAIN LANDING GEAR OUTER CYLINDER. (REPAIR). ACCOMPLISHED JOB I.A.W UPS EO-93133
- [SDR IPXA2025031870655](https://openairdocs.org/sdr/IPXA2025031870655), Mar 15, 2025: CYLINDER. CORRODED. **SDR FILED OPEN** FOUND CORROSION ON INNER SURFACE OF R/H MAIN LANDING GEAR OUTER CYLINDER. (REPAIR) PERFORMED NDT/PT FOR THE REWORKED AREA I.A.W SOPM 20-20-02
- [SDR IPXA2025031871789](https://openairdocs.org/sdr/IPXA2025031871789), Mar 11, 2025: TEE ANGLE. CORRODED. CORROSION - SPLICE TEE, KEEL BEAM AREA, PNL NO. 149AL FWD SPLICE TEE.REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV.91.INSTALLED NEW PART I.A.W SRM 51-40-02-0G R
- [SDR IPXA2025031171533](https://openairdocs.org/sdr/IPXA2025031171533), Mar 11, 2025: FLOOR PANEL. DENTED. MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N : 143T5876-90 PANEL NO : 232JFF.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4
- [SDR IPXA2025031171447](https://openairdocs.org/sdr/IPXA2025031171447), Mar 11, 2025: FLOOR PANEL. DENTED. MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N : 143T5876-72 PANEL NO : 232CFF.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4
- [SDR IPXA2025031171470](https://openairdocs.org/sdr/IPXA2025031171470), Mar 11, 2025: FLOOR PANEL. DENTED. MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N : 143T5876-38 PANEL NO : 232BFF.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4
- [SDR IPXA2025031171255](https://openairdocs.org/sdr/IPXA2025031171255), Mar 11, 2025: FLOOR PANEL. DENTED. MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N : 143T5876-89 PANEL NO : 231KFF.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4
- [SDR IPXA2025031171229](https://openairdocs.org/sdr/IPXA2025031171229), Mar 11, 2025: FLOOR PANEL. DENTED. MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N : 143T5876-79 PANEL NO : 231JFF.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4
- [SDR IPXA2025031171597](https://openairdocs.org/sdr/IPXA2025031171597), Mar 11, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N : 143T5876-83 PANEL NO : 231GFF.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4
- [SDR IPXA2025031171506](https://openairdocs.org/sdr/IPXA2025031171506), Mar 11, 2025: FLOOR PANEL. DENTED. MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N : 143T5876-63 PANEL NO : 231EFF.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4
- [SDR IPXA2025031171484](https://openairdocs.org/sdr/IPXA2025031171484), Mar 11, 2025: FLOOR PANEL. DENTED. MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N : 143T5876-73 PANEL NO : 231DFF.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4
- [SDR IPXA2025031171373](https://openairdocs.org/sdr/IPXA2025031171373), Mar 11, 2025: FLOOR PANEL. DENTED. MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N : 143T5876-75 PANEL NO : 231CFF.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4
- [SDR IPXA2025031171287](https://openairdocs.org/sdr/IPXA2025031171287), Mar 11, 2025: FLOOR PANEL. DENTED. MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N : 143T5876-77 PANEL NO : 231BFF.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4
- [SDR IPXA2025031171556](https://openairdocs.org/sdr/IPXA2025031171556), Mar 11, 2025: FLOOR PANEL. DENTED. MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N : 143T5876-78 PANEL NO : 231AFF.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4
- [SDR IPXA2025030711177](https://openairdocs.org/sdr/IPXA2025030711177), Mar 7, 2025: SKIN. DEBONDED. DISBOND, VERTICAL STABILIZER COMPOSITE PANEL DISBOND, P/N: 175T2001-2..PERFORMED NDT/UT FOR REPAIRED AND 8 INCHES HEAT BLANKET AREA, I.A.W.767 NDT MANUAL PART 1
- [SDR IPXA2025031393437](https://openairdocs.org/sdr/IPXA2025031393437), Mar 6, 2025: SUPPORT. CORRODED. CORROSION - SUPPORT, FWD CGO ENGWALL CURTAIN SUPPORT STRUCTURE RH SIDE STANCHION NUTPLATE AREA.REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.91.PERFORMED THE H
- [SDR IPXA2025031071222](https://openairdocs.org/sdr/IPXA2025031071222), Mar 5, 2025: SKIN. CRACKED. SKIN CRACK - L/H AFT FUSELAGE UPPER AREA AT STA 1659~STA 1665 S-13AL.REPAIRED DAMAGED AREA I.A.W SRM 53-80-01-2R-7 REV.91 AND EGAT WORK SHEET NO. 50153.ACCOMPLI
- [SDR IPXA2025031746104](https://openairdocs.org/sdr/IPXA2025031746104), Mar 4, 2025: ANGLE. CRACKED. FAULT - FOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV.91.INSTALL NEW PART
- [SDR IPXA2025031350087](https://openairdocs.org/sdr/IPXA2025031350087), Mar 4, 2025: FILLER. CORRODED. FOUND MAIN DECK CARGO FLOOR STRUCTURE CORROSION AT STA 1502 ~ STA 1580 , RBL 42.5 ~ RBL 88.5.REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV.91.INSTALLED FABRICAT
- [SDR IPXA2025030548372](https://openairdocs.org/sdr/IPXA2025030548372), Mar 4, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N : 143T5876-28 PANEL NO : 232SFF STA680~STA764 RBL77~RBL88. (REPAIR). I.A.W AMM 25-57-05-404-006, AMM 25-58-01-
- [SDR IPXA2025030548368](https://openairdocs.org/sdr/IPXA2025030548368), Mar 4, 2025: FLOOR PANEL. DAMAGED. MAJOR REPAIR FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N : 146T5869-135 PANEL NO : 251XFF STA 1450-STA 1560 LBL55~LBL88.FABRICATED A NEW FLOOR PANEL I.A.W
- [SDR IPXA2024121733579](https://openairdocs.org/sdr/IPXA2024121733579), Dec 10, 2024: WINDOW. CRACKED. F/O WINDOW CRACKED AND SPARKED DURING FLIGHT. RAN CHECKLIST REMOVED AND REPLACED F/O€™S WINDSHIELD IAW AMM 56-11-01. OPS CK OK.
- [SDR IPXA2024121133579](https://openairdocs.org/sdr/IPXA2024121133579), Dec 10, 2024: WINDOW. CRACKED. F/O WINDOW CRACKED AND SPARKED DURING FLIGHT. RAN CHECKLIST
- [SDR IPXA2024101042879](https://openairdocs.org/sdr/IPXA2024101042879), Oct 9, 2024: TAG. MISSING. LIFE RAFT MISSING PART TAG AND INSPECTION STICKER. R & R LWR LIFE RAFT ASSY IAW AMM 25-62-01.
- [SDR IPXA2024071402137](https://openairdocs.org/sdr/IPXA2024071402137), Jul 1, 2024: FLOORBOARD. CRACKED. FOUND MAIN CARGO DECK FLOORBOARD (POS 3R-4R ) DAMAGED. CRACK MEASURING 12 INCHES IN LENGTH. REMOVED FLOOR PANEL IAW AMM 53-01-06. FABRICATED NEW FLOOR BOARD IAW
- [SDR IPXA2024063087795](https://openairdocs.org/sdr/IPXA2024063087795), Jun 29, 2024: FLOOR PANEL. DAMAGED. DAMAGE NOTED ON REMOVED MAIN CARGO DECK FLOORBOARD (POS 3C-4C ) FLOORBOARD REMOVED REF AMM TASK 53-01-06-000-801 AND ROUTED TO S/M SHOP . 3 DAMAGE LOCATIONS NOT
- [SDR IPXA2024061041048](https://openairdocs.org/sdr/IPXA2024061041048), Jun 7, 2024: WINDOW. SCRATCHED. **SUPPLEMENTAL SDR** RT. L-2 WINDOW HAS NUMEROUS SCRATCHES OBSTRUCTING VIEW. INSTALLED R2 SLIDING WINDOW PER AMM 56-11-02. OPS TEST GOOD.
- [SDR IPXA2024060741048](https://openairdocs.org/sdr/IPXA2024060741048), Jun 7, 2024: WINDOW. DAMAGED. R-2 WINDOW HAS NUMEROUS SCRATCHES OBSTRUCTING VIEW. REMOVED R2 WINDOW IAW AMM 56-11-02-004-001
- [SDR IPXA2024030365327](https://openairdocs.org/sdr/IPXA2024030365327), Mar 2, 2024: FITTING. DAMAGED. POS 4C. CENTERLINE RESTRAINT ASSEMBLY FITTING DAMAGED, CAUSING RESTRAINT TO BE LOOSE IN THE TRACK. P/N 457T4102-1. FOR INSPECTION RII OK TO INSTALL, AND ALSO IN
- [SDR IPXA2023101218618](https://openairdocs.org/sdr/IPXA2023101218618), Oct 11, 2023: FAIRING. DAMAGED. FUSELAGE AERODYNAMIC FAIRING BELOW INBD FLAP DAMAGED ACCOMPLISHED EO-88442-REQ1 (LEFT INBOARD TRAILING EDGE FLAP FAIRING PANEL AND S.O.B. DOOR DAMAGE - TEMPORAR
- [SDR IPXA2023101218566](https://openairdocs.org/sdr/IPXA2023101218566), Oct 11, 2023: UNKNOWN. BROKEN. LEFT WING INBD FLAP PIVOT ARM ASSY BROKEN ACCOMPLISHED EO-88442-REQ1 (LEFT INBOARD TRAILING EDGE FLAP FAIRING PANEL AND S.O.B. DOOR DAMAGE - TEMPORARY REPAIR RE
- [SDR IPXA18566](https://openairdocs.org/sdr/IPXA18566), Oct 11, 2023: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** LEFT WING INBD FLAP PIVOT ARM ASSY BROKEN REMOVED DAMAGED(BENT) PIVOT ARM
- [SDR IPXA2023101118618](https://openairdocs.org/sdr/IPXA2023101118618), Oct 11, 2023: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** FUSELAGE AERODYNAMIC FAIRING BELOW INBD FLAP DAMAGED
- [SDR IPXA2023050830635](https://openairdocs.org/sdr/IPXA2023050830635), May 5, 2023: CONTROLLER. FAULTED. *EMERGENCY DECLARED* CABIN ALT AND CABIN ALTITUDE LIGHTS ILLUMINATED EICAS MSG CABIN WAS ALTITUDE WAS DISPLAYED.OPERATION IN IN MANUAL MODE RESTORED CABIN PRESS
- [SDR IPXA2023042625701](https://openairdocs.org/sdr/IPXA2023042625701), Apr 19, 2023: UNKNOWN. CRACKED. FAULT - CRACK - VERTICAL CHORD CRACK AT NOSE W/W STA 287 RBL 25 (REPAIR) PERFORMED NDT/ET FOR THE BEND RADIUS AREA OF REPAIR PARTS ,PER 767 NDT MANUAL PART6 51-
- [SDR IPXA2022050681810](https://openairdocs.org/sdr/IPXA2022050681810), May 2, 2022: GEAR. INOPERATIVE. INSPECTION TYPE:N/A**ATB** - GEAR WOULD NOT RETRACT AFTER TAKEOFFREMOVED MLG DOWN LOCK PINS FROM FWD HOLES IAW AMM CH 32-00-20
- [SDR IPXA2021072071872](https://openairdocs.org/sdr/IPXA2021072071872), Jul 19, 2021: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS INOP.REMOVED AND REPLACED EMERGEMCY BATTERY PACK IAW AMM 33-51-07.
- [SDR IPXA2021053069965](https://openairdocs.org/sdr/IPXA2021053069965), May 30, 2021: WEDGE. GOUGED. INSPECTION TYPE:N/AGOUGE TO THE TRAILING EDGE WEDGE OF THE NO. 5 SLATMETAL BOND REPAIR PER EO B767-5750-80313-B
- [SDR IPXA2021041368160](https://openairdocs.org/sdr/IPXA2021041368160), Apr 7, 2021: SKIN. CRACKED. INSPECTION TYPE:C13CRACK DAMAGE WAS FOUND ON NO.1 PYLON OUTBD SKIN ASSEMBLY(P/N:311T2450-25) NEAR NAC STA 237.5.PERFORM REPAIR I.A.W BOEING SR 4-5025368309 AND 
- [SDR IPXA2021041368159](https://openairdocs.org/sdr/IPXA2021041368159), Apr 7, 2021: SKIN. CRACKED. INSPECTION TYPE:C13CRACK DAMAGE WAS FOUND ON NO.2 PYLON INBD SKIN ASSEMBLY(P/N:311T2450-25)NEAR NAC STA 237.5.PERFORM REPAIR I.A.W BOEING SR 4-5025348916 AND EO
- [SDR IPXA2021040867936](https://openairdocs.org/sdr/IPXA2021040867936), Apr 7, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C13DAMAGE ON M/D FLOOR PANEL BETWEEN STA 731.11 AND 834,AND BETWEEN RBL 33.00 AND 54.75.FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO.B767-532
- [SDR IPXA2021040867935](https://openairdocs.org/sdr/IPXA2021040867935), Apr 6, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C13DAMAGE ON M/D FLOOR PANEL BETWEEN STA 1043 AND 1114.82,AND BETWEEN RBL 33.00 AND 54.75.FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO.B767-5
- [SDR IPXA2019122350237](https://openairdocs.org/sdr/IPXA2019122350237), Dec 19, 2019: SMOKE DETECTOR. FAILED. AFT CARGO DETECTOR 2 FAILED. R & R THE AFT CARGO SMOKE DETECTOR LOOP 2 IAW AMM 26-16-01. OPS CHECKED GOOD.
- [SDR IPXA2019040140655](https://openairdocs.org/sdr/IPXA2019040140655), Mar 22, 2019: FLOORBEAM. CORRODED. INSPECTION TYPE:C12CORROSION ON THE FLOOR BEAM OF MAIN DECK FLOOR STRUCTURE ON STA 266.5,LBL 53,WL200.REPAIR I.A.W. 767-300F SRM 53-00-51 ALLOWABLE DAMAGE 1 REV
- [SDR IPXA2019040140657](https://openairdocs.org/sdr/IPXA2019040140657), Mar 21, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C12DAMAGE ON M/D CARGO FLOOR PANEL AT STA 535 - STA654 PLUS 22 , LBL 33- LBL 55 , PNL NO.231HFF.FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO.
- [SDR IPXA2019040140656](https://openairdocs.org/sdr/IPXA2019040140656), Mar 21, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C12DAMAGE ON M/D CARGO FLOOR PANEL AT STA 535 - STA 654 PLUS 22 , RBL55-RBL 77 , PNL NO.232HFF.FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO.B

All 171: https://openairdocs.org/aircraft/N311UP/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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