# N325UP: 1998 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: 27751
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 12, 1998
- Certificate issued: January 29, 2026
- Expires: January 31, 2033
- Mode S code: A382B3
- 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=325UP
- Page: https://openairdocs.org/aircraft/N325UP

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/N325UP/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 N325UP.

## FAA accident and incident reports

None matched to N325UP.

## Service difficulty reports (117, 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 IPXA2026101092858](https://openairdocs.org/sdr/IPXA2026101092858), Oct 10, 2026: LIFE RAFT. PARTIAL DEPLOY. LIFE RAFT IN STOWAGE COMPARTMENT PARTIALLY DEPLOYED. REPLACED LIFE RAFT REF MM 25-62-01/401
- [SDR IPXA2025071295380](https://openairdocs.org/sdr/IPXA2025071295380), Jul 7, 2025: BEAR STRAP. CRACKED. CRACK, FWD ENTRY DOOR AFT LOWER CORNER BEAR STRAP. INSTALLED INSULATION BLANKET IAW AMM 25-80-00-400-803 REV. 145, JOB COMPLETED AND CONDITION CHECK NORMAL. IAW
- [SDR IPXA2025072374238](https://openairdocs.org/sdr/IPXA2025072374238), Jul 5, 2025: LINK. DAMAGED. WORN OUT - SUPPORT LINK, NO.2 ENG R/H HPT CASE COOLING FWD DUCT UPPER SIDE, NEAR FUEL SUPPLY LINE. I.A.W AMM 70-50-00-912-001-H00 REV.145, REPLACED THE LINK OF 
- [SDR IPXA2025072374286](https://openairdocs.org/sdr/IPXA2025072374286), Jul 5, 2025: LINK. DAMAGED. WORN OUT - SUPPORT LINK, NO.2 ENG L/H LPT CASE COOLING FWD DUCT LOWER SIDE, NEAR EGT. I.A.W. AMM 70-50-00-912-001-H00, REV.145, REPLACED THE LINK OF NO.2 ENGINE
- [SDR IPXA2025071272165](https://openairdocs.org/sdr/IPXA2025071272165), Jul 5, 2025: RIB. CRACKED. NUMBER 10 SPOILER ACTUATOR SUPPORT HINGE RIB CRACK WS 640. INSTALL NEW FITTING I.A.W SRM 51-40-02-0G REV.92 AND BOEING DWG 112T1000 SH 14 REV: B, 113T1422 SH 1 
- [SDR IPXA2025071173048](https://openairdocs.org/sdr/IPXA2025071173048), Jul 5, 2025: STRAP. CRACKED. CRACK - STRAP, FWD LOWER CARGO MAIN DECK FLOOR STRUCTURE STA 610 RBL 64.5. INSTALL THE REPAIR PARTS WET WITH BMS 5-95 FAYING SURFACE SEALANT. REFER TO FIGURE 2.
- [SDR IPXA2025070774321](https://openairdocs.org/sdr/IPXA2025070774321), Jul 5, 2025: HINGE FITTING. CRACKED. CRACK - FITTING, INBD SIDE OF L/H WING T/E INBD MAIN FLAP T/E MID LINK FITTING, WBL 174. PERFORM SRM 57-53-02-2R-1 REV.92 AND EGAT WORK SHEET NO. 50533 STEP 14 
- [SDR IPXA202507074238](https://openairdocs.org/sdr/IPXA202507074238), Jul 5, 2025: LINK. WORN. WORN OUT SUPPORT LINK, NO.2 ENG R/H HPT CASE COOLING FWD DUCT UPPER SIDE, NEAR FUEL SUPPLY LINE. (REPLACE) OK TO WORK
- [SDR IPXA2025072362233](https://openairdocs.org/sdr/IPXA2025072362233), Jul 4, 2025: FAN. DAMAGED. FOUND SUPPLY FAN JOINT SLEEVE WORN OUT. I.A.W AMM 21-58-06-004-283 REV.145 AND AMM 21-58-06-404-284 REV.145 REPLACED THE SLEEVE.
- [SDR IPXA2025072363772](https://openairdocs.org/sdr/IPXA2025072363772), Jul 4, 2025: VALVE. DAMAGED. CRACK - FLANGE, NO. 2 PYLON FAN AIR VALVE INLET. I.A.W. AMM 36-11-16-004-001-006, AND 36-11-16-404-015-006, REV.145, REPLACED THE FAN AIR VALVE OF NO.2 ENGINE. 
- [SDR IPXA2025070762233](https://openairdocs.org/sdr/IPXA2025070762233), Jul 4, 2025: SLEEVE. WORN. FOUND SUPPLY FAN JOINT SLEEVE WORN OUT.
- [SDR IPXA2025070763772](https://openairdocs.org/sdr/IPXA2025070763772), Jul 4, 2025: INLET. CRACKED. CRACK - FLANGE, NO. 2 PYLON FAN AIR VALVE INLET. (REPLACE) OK TO WORK
- [SDR IPXA2025070762480](https://openairdocs.org/sdr/IPXA2025070762480), Jul 4, 2025: MANIFOLD. BROKEN. BROKEN - MANIFOLD, NO.2 ENG LPT CASE COOLING, NEAR 11:00 AREA. I.A.W. AMM 75-24-03-004-050-H00 AND 75-24-03-404-037-H00, REV.145, REPLACED THE LPT COOLING MANIF
- [SDR IPXA2025071247542](https://openairdocs.org/sdr/IPXA2025071247542), Jul 3, 2025: INTERCOSTAL. CRACKED. FOUND THE INTERCOSTAL WITH CRACK DAMGE IN CEILING AREA OF BULK CARGO COMPARTMENT A STA 1602 LBL 59. REMOVED DAMAGE INTERCOSTAL I.A.W SRM 51-40-02-0G REV.92. INS
- [SDR IPXA2025071225363](https://openairdocs.org/sdr/IPXA2025071225363), Jul 2, 2025: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA. INSTALL NEW ANGLE I.A.W SRM 51-40-02-0G REV.92 AND BOEING DWG NO: 146T565
- [SDR IPXA2025071224874](https://openairdocs.org/sdr/IPXA2025071224874), Jul 2, 2025: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. INSTALL NEW ANGLE I.A.W SRM 51-40-02-0G REV.92 AND BOEING DWG NO: 146T56
- [SDR IPXA2025071224994](https://openairdocs.org/sdr/IPXA2025071224994), Jul 2, 2025: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578 RBL 80 INBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. I.A.W AMM 25-57-05-004-001 AND AMM 25-58-04-004-010 REV.145 REMOVED MAIN 
- [SDR IPXA2025071225374](https://openairdocs.org/sdr/IPXA2025071225374), Jul 2, 2025: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578 LBL 80 INBOARD IN BULK CARGO COMPARTMENT LEFT AREA. INSTALL NEW ANGLE I.A.W SRM 51-40-02-0G REV.92 AND BOEING DWG NO: 146T5650
- [SDR IPXA2023070884057](https://openairdocs.org/sdr/IPXA2023070884057), Jul 1, 2023: STIFFENER. CRACKED. MAJOR REPAIR FAULT - CRACK - STIFFENER, FORWARD CARGO COMPANTMENT, WING CENTER SECTION FRONT SPAN, STA 785, LBL 55 (REPAIR). REPAIR DAMAGE AREA I.A.W SRM 57-10-
- [SDR IPXA2023070884049](https://openairdocs.org/sdr/IPXA2023070884049), Jul 1, 2023: STIFFENER. CRACKED. MAJOR REPAIR FAULT - CRACK - STIFFENER, FORWARD CARGO COMPANTMENT, WING CENTER SECTION FRONT SPAN, STA 785, RBL 11 (REPAIR). REPAIR DAMAGE AREA I.A.W SRM 57-10-
- [SDR IPXA2023062694152](https://openairdocs.org/sdr/IPXA2023062694152), Jun 25, 2023: RADAR. WARNING MESSAGE. **ATB**€ŒWXR FAIL€? WXR SYS STATUS MSG BANGING SOUND COMING FROM NOSE OF AIRCRAFT. AIR TURN BACK OPEN RADOME, OPS TEST RADAR NML,NO DMG FOUND ,R/R TRANSCEIVER
- [SDR IPXA2022070783909](https://openairdocs.org/sdr/IPXA2022070783909), Jul 7, 2022: GUARD. BROKEN. INSPECTION TYPE:N/AEMER LIGHT SWITCH GUARD BROKER&R EMERGENCY LIGHT OVERHEAD SWITCH PANEL IAW AMM 33-51-08-02A. OPS CHECK NORMAL
- [SDR IPXA2022051081945](https://openairdocs.org/sdr/IPXA2022051081945), May 10, 2022: FUEL SYS. FAULT MESSAGE. INSPECTION TYPE:ETOP**ETOPS FILED OPEN** AFTER PUSH BACK BTB THERE WAS A L FWD PRESS LIGHT. ITEM DEFERRED IAW MEL 28-22-1 C/W DMP PULLED AND COLLORD C/B G24 PLA
- [SDR IPXA2021100674677](https://openairdocs.org/sdr/IPXA2021100674677), Oct 6, 2021: NONE. NONE. INSPECTION TYPE:ETOP**ETOPS FILED OPEN** L FWD FUEL PUMP EICAS AND L PRESS LIGHT ILLUMINATED WITH FUEL PUMP ON. DEFERRED L FWD FUEL PUMP PER MEL 28-22-1 ON M758
- [SDR IPXA2021061970756](https://openairdocs.org/sdr/IPXA2021061970756), Jun 12, 2021: STIFFENER. CRACKED. INSPECTION TYPE:C12CRACK ON VERTICAL STIFFENER AT WHEEL WELL BULKHEAD AT STA 287, RBL 25.REPAIR I.A.W UPS EO B767-5310-20118-F AND 767-300F SRM 51-70-12 GENERAL
- [SDR IPXA2020121863569](https://openairdocs.org/sdr/IPXA2020121863569), Dec 17, 2020: WARNING MESSAGE. FALSE ACTIVATION. ATB NO EMERGENCY DECLARED. FWD CARGO EICAS AND OVER HEAD LIGHT. DEFFERED PER MEL 52-71-1-1, AMC M729593. VERIFIED DOOR CLOSED SECURED WITH NO FAULTS OR DISCREPA
- [SDR IPXA2019102548265](https://openairdocs.org/sdr/IPXA2019102548265), Oct 24, 2019: POSITION UNIT. DAMAGED. INSPECTION TYPE:N/AAIR TURN BACK - GEAR DOORS WITH GEAR DISAGREE VIBRATION & WIND NOISE NOTED IN FLIGHT. AIRCRAFT TAKEN OOS.R&R L/MLG TRUCK POSITIONER, LEAK CHE
- [SDR IPXA2019090846450](https://openairdocs.org/sdr/IPXA2019090846450), Sep 7, 2019: WARNING SYSTEM. FALSE ACTIVATION. INSPECTION TYPE:N/A ATB - GEAR DISAGREE, GEAR DOOR EICAS, LEFT MAIN GEAR DOWN WITH GEAR LEVER UP. ACCOMP PSEU BITE IAWFIM32-09-00-815-803-001. ACCOP PSEU SENSOR
- [SDR IPXA2019062843826](https://openairdocs.org/sdr/IPXA2019062843826), Jun 19, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE: C11, DAMAGE FOUND ON THE MAIN DECK CARGO FLOOR PANEL 222DFF AT BS 285 - 412, RBL 77 - 88. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B767-5320
- [SDR IPXA2019062843825](https://openairdocs.org/sdr/IPXA2019062843825), Jun 19, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE: C11, DAMAGE FOUND ON MAIN DECK CARGO FLOOR PANEL 231KFF AT BS 412 - 544, LBL 77 - 88. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B767-5320-969
- [SDR IPXA2019011437798](https://openairdocs.org/sdr/IPXA2019011437798), Jan 13, 2019: FLOOR PANEL. DENTED. INSPECTION TYPE:N/A MAIN CARGO CARGO FLOOR BOARD DENT AT POSITION 8. REPAIRED PANEL IAW SRM 53-00-50-2DR.
- [SDR IPXA201812036460](https://openairdocs.org/sdr/IPXA201812036460), Nov 30, 2018: STARTER. FAILED. RIGHT ENGINE DID NOT START, RIGHT ENG STARTER EICAS MESSAGE. R & R THE RIGHT ENGINE STARTER IAW AMM 80-11-02.
- [SDR IPXA2017111923699](https://openairdocs.org/sdr/IPXA2017111923699), Nov 19, 2017: COVER. DAMAGED. NR 2 ENGINE GEAR BOX DRIVE COVER FOUND DAMAGED DURING BOROSCOPE. REPLACED COVER REF MM 72-60-00 EFF SOURCE REF 72-69-01-10-155.
- [SDR IPXA2017101922773](https://openairdocs.org/sdr/IPXA2017101922773), Oct 19, 2017: SEAL. OUT OF ALIGNMENT. PRESSURIZATION SQUEAL COMING FROM MAIN ENTRY AREA CLIMB THRU FL230, ABATED PASSING 290. FOUND AFT CREW ENTRY DOOR SEAL MISALIGNED IN TRACK. ALINGNED THE SEAL, N
- [SDR IPXA2017071819439](https://openairdocs.org/sdr/IPXA2017071819439), Jul 18, 2017: WATER SEPARATOR. ODOR. AIR CONDITIONING HAS A DIRTY SOCK ACRID ODOR WITH A/C PACKS RUNNING ON GROUND AND IN THE AIR. WHEN TEMP WARM. OFFENSIVE ODOR ALWAYS PRESENT WITH LEFT PACK RUNNI
- [SDR IPXA2017062018413](https://openairdocs.org/sdr/IPXA2017062018413), Jun 10, 2017: STIFFENER. CRACKED. INSPECTION TYPE: C10, CRACK ON CENTER WING FRONT SPAR STIFFENER UPPER SIDE AT BS 785.9, RBL 55. REPAIRED IAW SRM 57-10-10-2R-2, REPAIR 2, REV 68 AND EO B767-574
- [SDR IPXA2016112911163](https://openairdocs.org/sdr/IPXA2016112911163), Nov 28, 2016: BATTERY PACK. NO TEST. EMERGENCY LIGHTS WILL NOT TEST. R & R THE BATTERY PACK IAW AMM 33-51-07-201. OPS CHECKED NORMAL
- [SDR IPXA2016100308866](https://openairdocs.org/sdr/IPXA2016100308866), Sep 28, 2016: HANDLE. INOPERATIVE. EMERGENCY EGRESS WINDOW HANDLE PROTRUDING BELOW F/O WINDOW. THE WINDOW HANDLE IAW AMM 56-11-00-001.
- [SDR IPXA2016072706390](https://openairdocs.org/sdr/IPXA2016072706390), Jul 26, 2016: WARNING MESSAGE. FALSE ACTIVATION. CENTER HYDRAULIC PRIMARY 1 EICAS MESSAGE DISPLAYED. DIVERTED FLT. OPS CHECKED C HYD PRIMARY PUMP IAW MM 29-11-00-715-896, NO DEFECTS NOTED.
- [SDR IPXA2015091893677](https://openairdocs.org/sdr/IPXA2015091893677), Sep 17, 2015: RING. CHAFED. INSPECTION TYPE:C, DURING MAJOR MAINTENANCE VISIT 6779 FOUND CHAFING - POS 1 ENGINE RT T/R CASCADE AFT SUPPORT RING UPPER, NEAR AGB ACTUATOR CHAFING MARK TRANSF
- [SDR IPXA2015091893676](https://openairdocs.org/sdr/IPXA2015091893676), Sep 17, 2015: FRAME. CRACKED. INSPECTION TYPE:C, DURING MAJOR MAINTENANCE VISIT NR 6779, FOUND CRACK POS 1 ENGINE LT T/R INNER FAN AIR DUCT SUPPORT FRAME CRACK TRANSFERRED TO EGAT NRC DCU050
- [SDR IPXA2018091764034](https://openairdocs.org/sdr/IPXA2018091764034), Sep 15, 2015: STRUT. WORN. WHEN GEAR WAS RAISED AFTER TAKEOFF, RECEIVED A GEAR DOOR LIGHT AND MESSAGE. MAX SPEED WAS 230, MODERATE TO SEVERE VIBRATION IN NOSE GEAR AREA. VIBRATION DECREAS
- [SDR IPXA2015091693578](https://openairdocs.org/sdr/IPXA2015091693578), Sep 3, 2015: STRINGER. CRACKED. INSPECTION TYPE: C9, A CRACK, 0.6" WAS FOUND ON THE STRINGER 20R, BS 1550. REPAIRED IAW SR: 3-3374429228.
- [SDR IPXA2015091693577](https://openairdocs.org/sdr/IPXA2015091693577), Sep 3, 2015: STRINGER. CRACKED. INSPECTION TYPE: C9, FOUND A CRACK ONE INCH LONG ON LT SIDE FUSELAGE STRINGER 20L, BS 1504. REPAIRED IAW SR: 3-3374328483.
- [SDR IPXA2014062083355](https://openairdocs.org/sdr/IPXA2014062083355), Jun 17, 2014: SEAT TRACK. OVERSERVICED. ENROUTE, NOTICED A PERSISTENT ODOR. AFTER ABOUT AN HOUR, BOTH PILOTS HAD SLIGHT EYE IRRITATION. BOTH PILOTS USED OXYGEN. ODOR SEEMED TO DIMINISH LATER IN FLIGHT
- [SDR IPXA3679743](https://openairdocs.org/sdr/IPXA3679743), Aug 11, 2013: FLOOR PANEL. DENTED. INSPECTION TYPE:C08, FOUND DENT ON MAIN DECK CARGO FLOOR PANEL 252HFF AT BS 1197+70, RBL 83. REPAIR IAW EO B767-5320-9693-H.
- [SDR IPXA3679742](https://openairdocs.org/sdr/IPXA3679742), Aug 11, 2013: FLOOR PANEL. DENTED. INSPECTION TYPE: C08, FOUND TWO DENTS ON MAIN DECK CARGO FLOOR PANEL 251UFF AT BS 1380, LBL 65 AND 70. . REPAIR IAW EO B767-5320-9693-H.
- [SDR IPXA3679741](https://openairdocs.org/sdr/IPXA3679741), Aug 11, 2013: FAIRING. CORRODED. INSPECTION TYPE: C08, FOUND LIGHT CORROSION ON LT HORIZONTAL STABILIZER TIP FAIRING UPPER SURFACE AT HSBL 358. REPAIRED IAW SRM 55-10-30-2R-1, TABLE II .
- [SDR IPXA13679796](https://openairdocs.org/sdr/IPXA13679796), Aug 8, 2013: SEAT TRACK. WORN. INSPECTION TYPE:C08, THE STUD HOLE OF SEAT TRACK FOUND WORN AT BS 1509.5, RBL 11.00. REPAIR IAW SRM 53-00-52, REPAIR 9, REV 56.
- [SDR IPXA13679795](https://openairdocs.org/sdr/IPXA13679795), Aug 8, 2013: SEAT TRACK. WORN. INSPECTION TYPE:C08, STUD HOLE OF SEAT TRACK WORN AT BS 1509.5, LBL 11.00. REPAIR IAW SRM 53-00-52, REPAIR 9, REV 56.

All 117: https://openairdocs.org/aircraft/N325UP/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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