# N332UP: 2001 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: 32843
- Year built: 2001
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 23, 2001
- Certificate issued: October 29, 2019
- Expires: October 31, 2029
- Mode S code: A39F0D
- 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=332UP
- Page: https://openairdocs.org/aircraft/N332UP

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/N332UP/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 N332UP.

## FAA accident and incident reports

None matched to N332UP.

## Service difficulty reports (120, 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 IPXA2026042439581](https://openairdocs.org/sdr/IPXA2026042439581), Apr 23, 2026: ACTUATOR. NOISY. NOISE DURING AFT CARGO DOOR OPERATION. I.A.W AMM 52-37-04-004-001 REV.147 AND AMM 52-37-04-404-009 REV.147 REPLACE AFT CARGO DOOR ROTARY ACTUATOR AND OPERATION 
- [SDR IPXA2026042483757](https://openairdocs.org/sdr/IPXA2026042483757), Apr 20, 2026: BRACKET. CRACKED. CRACK-BRACKET, FWD AND MID SIDE OF LT WING NR 2 SLAT INBD SEAL DOOR, REPLACED IAW AMM 57-41-56-004-001 REV 147 AND AMM 57-41-56-404-009 REV 147.
- [SDR IPXA2026042563148](https://openairdocs.org/sdr/IPXA2026042563148), Apr 18, 2026: SEAL. TORN. LEFT WING NR 6 SPOILER HAS A TORN SEAL LOCATED AT THE 3RD ATTACH POINT FROM INBD END. IAW AMM 20-11-00-910-802, REV 147, REPLACED THE SEAL.
- [SDR IPXA2026042563692](https://openairdocs.org/sdr/IPXA2026042563692), Apr 18, 2026: HINGE. WORN. FOUND NR 8 TAI DOOR AFT HINGE WORN OUT. IAW AMM 57-41-58-434-044, ADJUSTED AND PERFORMED A BONDING TEST OF NR 8 TAI DOOR AFTER HINGE,RESULT WAS SATISFACTORY.
- [SDR IPXA2026042463695](https://openairdocs.org/sdr/IPXA2026042463695), Apr 18, 2026: BEARING. MIGRATED. MIGRATED BEARING, RT WING T/E NR 7 SPOILER LOWER FITTING. IAW AMM27-61-02-424-023 REV.147 CONNECT RH WING NO.7 SPOILER PCA ROD END AND THE SPOILER TO FLAP CLEAR
- [SDR IPXA2026042263719](https://openairdocs.org/sdr/IPXA2026042263719), Apr 18, 2026: DOOR. CHAFED. CHAFED SKIN, NR 2 ENG RT THRUST REVERSER LOWER BLOWOUT DOOR L/E AREA. REFER TO FAULT: T3F18E008P5SF FOR NEW DOOR REPLACEMENT.
- [SDR IPXA2026042262880](https://openairdocs.org/sdr/IPXA2026042262880), Apr 18, 2026: ANGLE. CRACKED. RIGHT PYLON ANGLE AT LOWER SURFACE RIGHT SIDE, BELOW AFT THRUST LINK IS CRACKED. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO.313T2380 SH.
- [SDR IPXA2026042263867](https://openairdocs.org/sdr/IPXA2026042263867), Apr 18, 2026: FAIRING. BROKEN. BROKEN FAIRING NR 1 ENG RT THRUST REVERSER TRANSLATING COWL FAIRING INNER 12:00 POS. ACCOMPLISHED JOB I.A.W UPS SREO-45403-REQ003 REV.1 AND SRM 51-40-02-0G REV.
- [SDR IPXA2026042146211](https://openairdocs.org/sdr/IPXA2026042146211), Apr 17, 2026: SEAL. BROKEN. BROKEN-SEAL, NR 2 PYLON FAIRING PANEL 446CR SPRING SEAL. REMOVED DAMAGED SEAL IAW SRM 51-40-02-0G REV.95. INSTALL NEW SEAL IAW SRM 51-40-02-0G, REV.95, AND DWG 
- [SDR IPXA2026042146228](https://openairdocs.org/sdr/IPXA2026042146228), Apr 17, 2026: DOOR. CHAFED. CHAFED DOOR, NR 2 ENG RT THRUST REVERSER LWR LATCH PNL INNER AREA (REPLACE) REMOVED DAMAGE DOOR I.A.W SRM 51-40-02-0G REV.95. INSTALL NEW DOOR IAW SRM 51-40-02-
- [SDR IPXA2026042146161](https://openairdocs.org/sdr/IPXA2026042146161), Apr 17, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 2 ENG LT CORE COWL HOLD OPEN ROD SUPPORT BRACKET. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 95. INSTALLED A NEW BRACKET IAW SRM 51-40-0
- [SDR IPXA2026042146248](https://openairdocs.org/sdr/IPXA2026042146248), Apr 17, 2026: BRACKET. CRACKED. CRACK-ANGLE, NR 1 ENG RT THRUST REVERSER INNER DRAIN TUBE SUPPORT. REMOVE DAMAGE BRACKET IAW SRM 51-40-02-0G REV.95. .INSTALLED A NEW BRACKET IAW SRM 51-40-02-0
- [SDR IPXA2026042428033](https://openairdocs.org/sdr/IPXA2026042428033), Apr 16, 2026: BULB SEAL. BROKEN. AERODYNAMIC SEAL BROKEN, FORWARD LH ENTRY DOOR. INSTALL NEW SILICONE RUBBER SEAL I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO:141T6121 SH13 REV.B.
- [SDR IPXA2026042428172](https://openairdocs.org/sdr/IPXA2026042428172), Apr 16, 2026: SCUFF PLATE. DENTED. DENTED SCUFF PLATE, BULK CARGO DOOR CUTOUT LOWER AFT CORNER AREA. REPLACED IAW AMM 53-13-02-404-007 REV.147 TO INSTALL SCUFF PLATE. IAW AMM 53-13-02-404-007 REV
- [SDR IPXA2026042428272](https://openairdocs.org/sdr/IPXA2026042428272), Apr 16, 2026: ACTUATOR. LEAKING. FOUND THE OUTBOARD SIDE PCA OF LEFT WING OUTBOARD AILERON HYDRAULIC LEAK. I.A.W AMM 27-11-49-422-028 REV.147 STEP 3.A TO 3.H(7) INSTALLED LH WING OUTBOARD AILER
- [SDR IPXA2026042227994](https://openairdocs.org/sdr/IPXA2026042227994), Apr 16, 2026: SUPPORT ANGLE. BROKEN. FOUND MAIN DECK CARGO CREW ENTRY DOOR LOWER SILL DAMAGE UNDER SCUFF PLATE. (REPLACE) INSTALL NEW LLIPLAY I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO: 141T831
- [SDR IPXA2026042026781](https://openairdocs.org/sdr/IPXA2026042026781), Apr 16, 2026: GUIDE. WORN. FOUND MAIN DECK CARGO HANDLING ROLLER BROKEN OF LATERAL GUIDE ASSY AT BS 620 LBL 66.00. IAW AMM 25-57-08-004-015 AND AMM 25-57-08-404-020 REV.147 REPLACED LATER
- [SDR IPXA2026042026761](https://openairdocs.org/sdr/IPXA2026042026761), Apr 16, 2026: RESTRAINT. BROKEN. FOUND MAIN DECK CARGO HANDLING CL DOOR AREA RESTRAINT ASSY BROKEN AT : STA 522 BL 0.00 I.A.W AMM 25-58-03-404-031 AND AMM 25-58-03-404-017 REV.147 REPLACED CL D
- [SDR IPXA2026041828803](https://openairdocs.org/sdr/IPXA2026041828803), Apr 16, 2026: SKIN. DAMAGED. L/H WING T/E OUTBD FLAP INBD SIDE AFT CAP , WBL 355. .I.A.W AMM 20-11-00-910-802 REV147 INSTALL L/H OUTBD FLAP INBD SIDE P-SEAL & RETAINER UPPER AND LOWER.
- [SDR IPXA2026041628033](https://openairdocs.org/sdr/IPXA2026041628033), Apr 16, 2026: SEAL. BROKEN. AERODYNAMIC SEAL BROKEN, FORWARD LH ENTRY DOOR. OPEN
- [SDR IPXA2026042410374](https://openairdocs.org/sdr/IPXA2026042410374), Apr 15, 2026: SCUFF PLATE. DENTED. DENTED SCUFF PLATE, BULK CARGO DOOR CUTOUT LOWER MID AREA. REPLACED IAW AMM 53-13-02-404-007 REV.147 TO INSTALL SCUFF PLATE.
- [SDR IPXA2026041711117](https://openairdocs.org/sdr/IPXA2026041711117), Apr 15, 2026: ROLLER. WORN. FOUND MAIN DECK CARGO HANDLING ROLLER RAIL ASSY WORN AT : STA 785 ~ STA 795 LBL 33.00, STA 797 ~ STA 807 LBL 33.00, STA 895 ~ STA 925 RBL 33. STEP 2 I.A.W AMM 2
- [SDR IPXA2026041710726](https://openairdocs.org/sdr/IPXA2026041710726), Apr 15, 2026: SEAT TRACK. WORN. FOUND FIRST OFFICER SEAT TRACK ASSY WORN AT : INBOARD AFT AND INBOARD FORWARD. I.A.W AMM 25-11-01-822-095-001 REV.147 REPLACED TRACK ASSY TOTAL : 2 EA.
- [SDR IPXA2026041711106](https://openairdocs.org/sdr/IPXA2026041711106), Apr 15, 2026: GUIDE. BROKEN. FOUND MAIN DECK CARGO HANDLING LATERAL GUIDE ASSY BROKEN AT BS 500 RBL 22. REPLACED IAW AMM 25-57-08-004-015 AND AMM 25-57-08-404-020 REV.147.
- [SDR IPXA2026041710867](https://openairdocs.org/sdr/IPXA2026041710867), Apr 15, 2026: SEAT TRACK. WORN. FOUND CAPTAIN SEAT TRACK ASSY WORN AT : INBOARD AFT. I.A.W AMM 25-11-01-822-095-001 REV.147 REPLACED TRACK ASSY CONDITION CHECK NORMAL.
- [SDR IPXA2026041711079](https://openairdocs.org/sdr/IPXA2026041711079), Apr 15, 2026: LOCK. WORN. FOUND MAIN DECK CARGO HANDLING ROLLER HOLE WORN OF LOCK ASSY AT : STA 1131 LBL 77.50 TOTAL: 1EA. I.A.W AMM 25-58-01-004-001 AND AMM 25-58-01-404-005 REV.147 REP
- [SDR IPXA2026042010664](https://openairdocs.org/sdr/IPXA2026042010664), Apr 15, 2026: STIFFENER. CRACKED. DURING PERFORM EO-63470-JIC002 FOUND CRACK AT NWW STA 287,RBL 25 STIFFENER. PERFORMED HEAT TREATED. REPAIRED IAW EO-63472-JIC001 REV.5 STEP 7. MAJOR REPAIR.
- [SDR IPXA2026042010700](https://openairdocs.org/sdr/IPXA2026042010700), Apr 15, 2026: STIFFENER. CRACKED. MAJOR REPAIR. DURING PERFORM EO-63470-JIC001 FOUND CRACK AT NWW BS 287, LBL 25, STIFFENER. .ACCOMPLISH THE REPAIR I.A.W UPS EO-63472-JIC001 REV5.
- [SDR IPXA2026042471246](https://openairdocs.org/sdr/IPXA2026042471246), Apr 13, 2026: ACTUATOR. LEAKING. FOUND RT LCC ACTUATOR LEAKING. IAW AMM 27-11-14-424-016 REV.147 STEP 3.A TO STEP 3.F(9), INSTALLED RH WING LCCA.
- [SDR IPXA2026041772172](https://openairdocs.org/sdr/IPXA2026041772172), Apr 13, 2026: PANEL. BROKEN. FOUND MAIN DECK CARGO DADO PANEL WITH DAMAG ACCOMPLISH UPS SREO-29536-REQ002 REV.2.
- [SDR IPXA2026041472404](https://openairdocs.org/sdr/IPXA2026041472404), Apr 13, 2026: FLOOR PANEL. DAMAGED. MAJOR REPAIR. FOUND MAIN DECK FLOOR PANEL DAMAGED, IAW AMM 53-01-06-400-801 REV.147 INSTALLED MAIN DECK CARGO FLOOR PANEL.
- [SDR IPXA2026041472413](https://openairdocs.org/sdr/IPXA2026041472413), Apr 13, 2026: FLOOR PANEL. DAMAGED. MAJOR REPAIR. FOUND MAIN DECK FLOOR PANEL DAMAGE, IAW AMM 53-01-06-400-801 REV.147 INSTALLED MAIN DECK CARGO FLOOR PANEL.
- [SDR IPXA2025092972337](https://openairdocs.org/sdr/IPXA2025092972337), Sep 27, 2025: SIGN. INOPERATIVE. EMERGENCY EXIT LIGHTED SIGN BY THE COCKPIT ENTRYWAY DOOR IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY CHARGER POWER SUPPLY UNIT IN REFERENCE TO AMM 33-51-07. 
- [SDR IPXA2025031385751](https://openairdocs.org/sdr/IPXA2025031385751), Jul 12, 2024: SKIN. DAMAGED. LEFT INBOARD AFT FLAP DAMAGED ON UPPER SURFACE AT APPROXIMATELY AFT OUTBOARD CORNER. COMPLETED REPAIR OF FLAP PER SRM 51-70-10-2R AND EO 90887-REQ5
- [SDR IPXA2024071941894](https://openairdocs.org/sdr/IPXA2024071941894), Jun 13, 2024: SKIN. CRACKED. LEFT PYLON HAS A CRACK ABOVE INBD SERVICE PANEL, ABOUT 1.5 INCHES LONG. MARKED. ALL REPAIR STEPS ACCOMPLISHED PER EO-90663-REQ2. LEFT ACCESS DOOR REINSTALL ADDR
- [SDR IPXA2024061441894](https://openairdocs.org/sdr/IPXA2024061441894), Jun 13, 2024: SKIN. CRACKED. LEFT PYLON HAS A CRACK ABOVE INBD SERVICE PANEL, ABOUT 1.5 INCHES LONG. MARKED. PERFORMED CONDUCTIVITY TEST ON CORD MATERIAL 7075 T6XXX IAW NDT 51-00-00. ALL 4 
- [SDR IPXA2024042918728](https://openairdocs.org/sdr/IPXA2024042918728), Apr 16, 2024: BRACKET. CORRODED. FAULT - CORROSION - BRACKET, R/H LOWER SURFACE OF UPPER RIGHT HORIZONTAL STABILIZER BOX STA 1805 (REPLACE) REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 89. IN
- [SDR IPXA2024042462866](https://openairdocs.org/sdr/IPXA2024042462866), Apr 12, 2024: ANGLE. CRACKED. CRACK - ANGLE BULK CARGO COMPARTMENT LEFT AREA STA 1578 LBL 60 (REPLACE) 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 89. 2. INSTALLED NEW PART I.A.W SRM 5
- [SDR IPXA2024041364183](https://openairdocs.org/sdr/IPXA2024041364183), Apr 12, 2024: NONE. NONE. FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. ACCOMPLISHED SDR PER E0-82173-J1C001.
- [SDR IPXA2024041964132](https://openairdocs.org/sdr/IPXA2024041964132), Apr 12, 2024: ANGLE. CRACKED. FAULT - CRACK - ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60 (REPLACE) REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 89. INSTALLED NEW PART I.A.W SR
- [SDR IPXA2024042246123](https://openairdocs.org/sdr/IPXA2024042246123), Apr 11, 2024: SKIN. CRACKED. SKIN, FWD LOWER FACE OF R/H WING NO.9 SLAT L/E SKIN, NEAR INBD TRACK. (REPAIR) ACCOMPLISHED REPAIR I.A.W SRM 57-43-01-2R-2 REV. 89 AND EGAT WORK SHEET NO. 40316
- [SDR IPXA2024081211321](https://openairdocs.org/sdr/IPXA2024081211321), Aug 7, 2023: SKIN. DENTED. FUESLAGE DENT @ STA 654 +88 BETWEEN 35-36R PERFORMED PERMANENT REPAIR IAW EO-87841-REQ3.
- [SDR IPXA2023071303512](https://openairdocs.org/sdr/IPXA2023071303512), Jul 13, 2023: DOOR. NOISY. VERY LOUD PRESSURIZATION AIR NOISE FROM MAIN ENTRY DOOR SEAL QUIT AT BETWEEN 4.0 & 5.0 PSI CABIN PRESSURE CLEANED MAIN ENTRY DOOR SEAL, PRESSURIZED A/C PER AMM 
- [SDR IPXA2023080898884](https://openairdocs.org/sdr/IPXA2023080898884), May 11, 2023: SKIN. DENTED. *MAJOR REPAIR* RH HORIZONTAL STABILIZER UPPER SKIN DENT***SM40/LMX4*** COMPLETED E0-86923-REQ2. THIS CLEARS MOC 2301223.
- [SDR IPXA2023020890760](https://openairdocs.org/sdr/IPXA2023020890760), Feb 8, 2023: INDICATOR. NOT REPORTED. INSPECTION TYPE:NAFUEL QUANTITY INDICATOR ON OVERHEAD PANEL INTERMITTENT.PERFORMED FUEL QTY TEST PER FIM 28 41 00 815 861. NO FAULTS FOUND. SYSTEM OK. FUEL QTY 
- [SDR IPXA2022081585251](https://openairdocs.org/sdr/IPXA2022081585251), Aug 15, 2022: WARNING MESSAGE. ILLUMINATED. INSPECTION TYPE:ETOP** ETOPS FILED OPEN ** AFTER LANDING - R REV ISLN VALVE CAUTION MSG. DEFERRED PER MEL 78-31-1 PERFORMED DMP 78-31-1,DMI M788792 ASSIGNED INS
- [SDR IPXA2022051382066](https://openairdocs.org/sdr/IPXA2022051382066), May 13, 2022: CIRCUIT BREAKER. POPPED. INSPECTION TYPE:NA**SUPPLENTAL SDR** AT 1 H 43 MIN LH AFT FUEL PUMP C/B POPPED.1.R/R LH MAIN FUEL TANK AFT BOOST PUMP IAW AMM 28-22-03. 2. FUEL BOOST PUMP OPERA
- [SDR IPXA2022050981860](https://openairdocs.org/sdr/IPXA2022050981860), Apr 29, 2022: SKIN. DAMAGED. INSPECTION TYPE:C11 LIGHTNING STRIKE DAMAGE WAS FOUND ON FUSELAGE SKIN (P/N:141T3840-77)BETWEEN STA 139 - STA 148.75, WL 224.5 - WL 216.REPAIR I.A.W 767-300F SR
- [SDR IPXA2022050881845](https://openairdocs.org/sdr/IPXA2022050881845), Apr 29, 2022: STIFFENER. CRACKED. INSPECTION TYPE:C11CRACK 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.83.01, AND UPS 
- [SDR IPXA2022050881844](https://openairdocs.org/sdr/IPXA2022050881844), Apr 29, 2022: STIFFENER. CRACKED. INSPECTION TYPE:C11CRACK 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.83.01, AND UPS 

All 120: https://openairdocs.org/aircraft/N332UP/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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