# N329UP: 1999 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: 27755
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 23, 1999
- Certificate issued: June 25, 1999
- Expires: August 31, 2027
- Mode S code: A3918F
- 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=329UP
- Page: https://openairdocs.org/aircraft/N329UP

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/N329UP/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 N329UP.

## FAA accident and incident reports

None matched to N329UP.

## Service difficulty reports (128, 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 IPXA2026100259603](https://openairdocs.org/sdr/IPXA2026100259603), Oct 2, 2026: DOOR LATCH. BINDING. ENTRY DOOR SECURE LATCH IS VERY HARD TO CLOSE /LATCH. LUBRICATED CREW ENTRY DOOR SECURE LATCH PER AMM 12-21-18/301.OPS CHECK OF CREW DOOR OK.
- [SDR IPXA2026093001662](https://openairdocs.org/sdr/IPXA2026093001662), Sep 30, 2026: SEAL. DETACHED. FORWARD UPPER L1 DOOR SEAL PARTIALLY DETACHED. REINSTALLED FORWARD UPPER UNPRESSURIZED SEAL IN RETAINER OF FWD SIDE DOORWAY LINING PER AIPC 25-20-00-01B.
- [SDR IPXA2026051373091](https://openairdocs.org/sdr/IPXA2026051373091), May 13, 2026: LINK. BROKEN. ON APPROACH TO DUB AND UPON SELECTING GEAR DOWN RECEIVED DOOR LIGHT; GEAR LIGHT, AND GEAR DISAGREE EICAS, AFTER ALT EXTENSION ALL WARNING AND CAUTION LIGHTS REM
- [SDR IPXA2026043057389](https://openairdocs.org/sdr/IPXA2026043057389), Apr 30, 2026: PAWL. DAMAGED. CREW ENTRY DOOR EXTERIOR HANDLE NOT GOING TO FAIRED POSITION WITH DOOR CLOSED. FOUND ARMING SYSTEM EXTERNAL LOCK PAWL DAMAGED. REMOVED AND REPLACED ARMING SYSTE
- [SDR IPXA2025092530404](https://openairdocs.org/sdr/IPXA2025092530404), Sep 25, 2025: ROLLER. NOT REPORTED. ON TAKEOFF NOTICED WIND NOISE COMING FROM MAIN CABIN DOOR. CONTINUED TO GET LOUDER AS AIRSPEED INCREASED. SUSPECT DOOR SEAL. CABIN PRESSURE REMAINED NORMAL. INS
- [SDR IPXA2025091116154](https://openairdocs.org/sdr/IPXA2025091116154), Sep 10, 2025: PAWL. DAMAGED. CREW DOOR LATCH PAWL DAMAGED. ++REPLACED THE DOOR PAWL PER AMM 52-12-25, AND 20-00-00. OPS CHECKS GOOD.
- [SDR IPXA2025091109961](https://openairdocs.org/sdr/IPXA2025091109961), Sep 10, 2025: DOOR. BINDING. UNABLE TO SECURE L FWD ENTRY DOOR. MULTIPLE ATTEMPS MADE OPERATED DOOR IAW B767 AMM 52-12-00 OPS CHECK OK
- [SDR IPXA2025090512124](https://openairdocs.org/sdr/IPXA2025090512124), Sep 4, 2025: DOOR. BINDING. MAIN PAX DOOR WILL NOT CLOSE PROPERLY. LEADING EDGE SIDE OF DOOR HAS MAIN GUIDE ROLLER THAT HAS POPPED OUT OF TRACK. ++RE-POSITIONED GUIDE ROLLER PER AMM 52-12-
- [SDR IPXA2025060434318](https://openairdocs.org/sdr/IPXA2025060434318), Jun 4, 2025: HANDLE. INOPERATIVE. MAIN CABIN DOOR HANDLE HAS A LOT OF PLAY WHEN OPEN OR SHUT. €ŒLOOSE€? <BR>MAIN CABIN DOOR INDICATOR YELLOW HANDLE LOCKED AND JAMMED, WONT EVEN CLOSE WHEN BIG 
- [SDR IPXA2025032041995](https://openairdocs.org/sdr/IPXA2025032041995), Mar 14, 2025: SKIN. DAMAGED. BROKEN - PANEL, RIGHT WING INBOARD AFTER FLAP UPPER SURFACE WBL 104. (REPAIR). I.A.W AMM 51-21-10-307-020 REV.144 REPAINT REWORK AREA. ACCOMPLISH THE REPAIR PER
- [SDR IPXA2025031939427](https://openairdocs.org/sdr/IPXA2025031939427), Mar 14, 2025: ANGLE. CRACKED. FOUND CRACK - ANGLE, BULK CGO COMPT CEILING AREA, STA 1577 LBL 74 INBD SIDE. (REPLACE). I.A.W AMM 53-01-06-400-801 REV.144 INSTALL MAIN DECK CARGO FLOOR PANEL A
- [SDR IPXA2025031399423](https://openairdocs.org/sdr/IPXA2025031399423), Mar 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 143T5876-82 PANEL NO : 232GFF (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 53-01-06-
- [SDR IPXA2025031399895](https://openairdocs.org/sdr/IPXA2025031399895), Mar 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 146T5869-71 PANEL NO : 251FFF (REPAIR). .FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. .I.A.W AMM 53-01-0
- [SDR IPXA2025031399323](https://openairdocs.org/sdr/IPXA2025031399323), Mar 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 143T5876-73 PANEL NO : 231DFF (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-02-
- [SDR IPXA2025031399469](https://openairdocs.org/sdr/IPXA2025031399469), Mar 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 143T5876-80 PANEL NO : 232HFF (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-02-
- [SDR IPXA2025031399336](https://openairdocs.org/sdr/IPXA2025031399336), Mar 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 143T5876-81 PANEL NO : 231HFF (REPAIR). .FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 53-01-06
- [SDR IPXA2025031399222](https://openairdocs.org/sdr/IPXA2025031399222), Mar 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 143T5876-84 PANEL NO : 232FFF (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.. I.A.W AMM 53-01-06
- [SDR IPXA2025031399507](https://openairdocs.org/sdr/IPXA2025031399507), Mar 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 143T5876-78 PANEL NO : 231AFF (REPAIR). .FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. .I.A.W AMM 53-01-0
- [SDR IPXA2025031398502](https://openairdocs.org/sdr/IPXA2025031398502), Mar 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 141T5856-47 PANEL NO: 221CFF. (REPAIR) I.A.W AMM 53-01-06-000-801 REV.144 REMOVE MAIN DECK CARGO FLOOR PANEL SEALANT AN
- [SDR IPXA2025031398647](https://openairdocs.org/sdr/IPXA2025031398647), Mar 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-64 PANEL NO: 251AFF. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. .I.A.W AMM 53-01-06-
- [SDR IPXA2025031398586](https://openairdocs.org/sdr/IPXA2025031398586), Mar 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-89 PANEL NO: 251XFF. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 53-01-06-4
- [SDR IPXA2025031398504](https://openairdocs.org/sdr/IPXA2025031398504), Mar 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 143T5876-63 PANEL NO: 231EFF. (REPAIR) I.A.W AMM 53-01-06-000-801 REV.144 REMOVE MAIN DECK CARGO FLOOR PANEL SEALANT AN
- [SDR IPXA2025031398493](https://openairdocs.org/sdr/IPXA2025031398493), Mar 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 141T5856-47 PANEL NO: 221CFF. (REPAIR). .FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. .I.A.W AMM 53-01-06
- [SDR IPXA2025031398629](https://openairdocs.org/sdr/IPXA2025031398629), Mar 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-72 PANEL NO: 252MFF. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 53-01-06-4
- [SDR IPXA2025031398667](https://openairdocs.org/sdr/IPXA2025031398667), Mar 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-77 PANEL NO: 251MFF. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. .I.A.W AMM 53-01-06-
- [SDR IPXA2025031398487](https://openairdocs.org/sdr/IPXA2025031398487), Mar 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 143T5876-87 PANEL NO: 231LFF. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. .I.A.W AMM 53-01-06-
- [SDR IPXA2025031398564](https://openairdocs.org/sdr/IPXA2025031398564), Mar 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-80 PANEL NO: 252RFF. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 53-01-06-4
- [SDR IPXA2025031398611](https://openairdocs.org/sdr/IPXA2025031398611), Mar 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-65 PANEL NO: 251JFF. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. .I.A.W AMM 53-01-06-
- [SDR IPXA2025032474279](https://openairdocs.org/sdr/IPXA2025032474279), Mar 11, 2025: BEAR STRAP. CRACKED. CRACK, FWD ENTRY DOOR AFT LOWER CORNER BEAR STRAP.(REPAIR). I.A.W AMM 25-80-00-400-803 REV.144 INSTALL FORWARD CARGO INSULATION BLANKET AT STA 303 ~ 368 AND CON
- [SDR IPXA2025031172740](https://openairdocs.org/sdr/IPXA2025031172740), Mar 11, 2025: SEAL. BROKEN. FOUND THE CREW ENTRY DOOR FORWARD DOORWAY SEAL BROKEN.
- [SDR IPXA2025032556614](https://openairdocs.org/sdr/IPXA2025032556614), Mar 10, 2025: SKIN. CRACKED. DURING PFM J/C:EO-24301-JIC001 FOUND SKIN CRACK AT STA 1725.50 NEAR S-7R.(REPAIR). ACCOMPLISHED REPAIR I.A.W EO-93158-REQ1 REV1.
- [SDR IPXA2025031356614](https://openairdocs.org/sdr/IPXA2025031356614), Mar 10, 2025: SKIN. CRACKED. DURING PFM J/C:EO-24301-JIC001 FOUND SKIN CRACK AT STA 1725.50 NEAR S-7R.(REPAIR) I.A.W. EGAT W/S NO.50164 PAGE:4 OF 16 STEP:11 TABLE:II (PAGE:11 OF 16) PART NO
- [SDR IPXA2025011873256](https://openairdocs.org/sdr/IPXA2025011873256), Jan 18, 2025: LENS. DAMAGED. L1271 DOME/EMER CLG LIGHT LENSE IS CRACKED. INSTALLED NEW COVER ASSY PER MM 33-11-00
- [SDR IPXA2025012183259](https://openairdocs.org/sdr/IPXA2025012183259), Jan 18, 2025: BULB. BURNED OUT. L1271 COCKPIT RIGHT EMERGENCY CEILING LIGHT INOP. RELAMPED PER AMM 33-51-11. OPS CHECK GOOD.
- [SDR IPXA2024121872254](https://openairdocs.org/sdr/IPXA2024121872254), Dec 12, 2024: INLET. CRACKED. *SUPPLEMENTAL SDR* R/H ENGINE INLET, INNER LIP, AT APPROXIMATE 12 O€™CLOCK POSITION, HAS 6 INCH CRACK SPANNING SEVERAL FASTENERS. REMOVED AND REPLACED R/H INLE
- [SDR IPXA2024121372254](https://openairdocs.org/sdr/IPXA2024121372254), Dec 12, 2024: INLET. CRACKED. R/H ENGINE INLET, INNER LIP, AT APPROXIMATE 12 O€™CLOCK POSITION, HAS 6 INCH CRACK SPANNING SEVERAL FASTENERS. REMOVED R/H ENGINE INLET COWL ASSEMBLY IN REF TO
- [SDR IPXA2024110439101](https://openairdocs.org/sdr/IPXA2024110439101), Nov 2, 2024: HANDLE. UNSECURE. MAIN DOOR. EXTERIOR HANDLE SECURE LEVER CANNOT BE MOVED TO THE SECURED POSITION FROM INSIDE OF AIRCRAFT WORKS NORMAL FROM OUTSIDE OF AIRCRAFT PERFORMED OPS CHEC
- [SDR IPXA2024080227380](https://openairdocs.org/sdr/IPXA2024080227380), Aug 1, 2024: SLIDING WINDOW. FAULTED. HEARD A LOUD SNAPPING SOUND ON F/O'S WINDOW WHILE CLOSING. THE LINK ON THE F/O'S SIDE ALSO DOESN'T REMAIN IN THE REQUIRED POSITION (SLIGHTLY OVER 90') F/O WINDO
- [SDR IPXA2023112950104](https://openairdocs.org/sdr/IPXA2023112950104), Nov 25, 2023: DOOR. UNKNOWN. **SUPPLEMENTAL SDR**MAIN CABIN DOOR DOES NOT CLOSE CORRECTLY OR EASILY LUBRICATED CREW ENTRY DOOR OUTER HANDLE & DOOR TROLLY ASSEMBLY AMM 12-21-18-603-009 & 12-
- [SDR IPXA2023112750104](https://openairdocs.org/sdr/IPXA2023112750104), Nov 25, 2023: UNKNOWN. UNKNOWN. **SDR FILED OPEN**MAIN CABIN DOOR DOES NOT CLOSE CORRECTLY OR EASILY LUBRICATED CREW ENTRY DOOR OUTER HANDLE & DOOR TROLLY ASSEMBLY AMM 12-21-18-603-009 & 12-21
- [SDR IPXA2023082060424](https://openairdocs.org/sdr/IPXA2023082060424), Aug 20, 2023: CDU. INOPERATIVE. DURING CRUISE FL 350 EXPERIENCED FAILURE OF F/O'S FMC UNIT, ALONG WITH STRONG ACRID ELECTRICAL ODAR IN COCKPIT DECLARED EMERGENCY DIVERTED TO CARDIFF REMOVED AN
- [SDR IPXA2023040792683](https://openairdocs.org/sdr/IPXA2023040792683), Mar 31, 2023: SKIN. UNKNOWN. INSPECTION TYPE:C13*MAJOR REPAIR* FUSELAGE DRAIN HOLES ADDITION AND INSPECTION AFT OF STA 1725.5 BETWEEN S-36L AND S-36R.PERFORM UPS EO B767-2740-82173-C APPX B
- [SDR IPXA2023041292842](https://openairdocs.org/sdr/IPXA2023041292842), Mar 30, 2023: UNKNOWN. CRACKED. INSPECTION TYPE:C13*MAJOR REPAIR* CRACK DAMAGE WAS FOUND ON MID CHORD(P/N:141T5147-12)OF FLOOR BEAM AT STA 246,NEAR LBL 40.REPAIR I.A.W BOEING SRID 3-5601269388
- [SDR IPXA2022111888220](https://openairdocs.org/sdr/IPXA2022111888220), Nov 18, 2022: SEAL. UNSECURE. MAIN ENTRY DOOR FORWARD RUBBER SEAL IS BECOMING DETACHED AT TOP. SECURED SEAL IN PLACE. PER TASK 52-09-01-424-019
- [SDR IPXA2022011878009](https://openairdocs.org/sdr/IPXA2022011878009), Jan 17, 2022: NONE. TORN. INSPECTION TYPE:N/A** SUPPLEMENTAL SDR **UPON CLOSING THE MAIN CABIN DOOR FOR DEPARTURE, A PIECE OF RUBBER STRIPPING WAS OBSERVED TO BE TORN. TORN SECTIONOF SEA
- [SDR IPXA2021041368152](https://openairdocs.org/sdr/IPXA2021041368152), Apr 5, 2021: STIFFENER. CRACKED. INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER(P/N:111T2008-12) ON STA 785.9, RBL 33.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV. 79.01 AND UPS
- [SDR IPXA2021041368150](https://openairdocs.org/sdr/IPXA2021041368150), Apr 4, 2021: STIFFENER. CRACKED. INSPECTION TYPE:C12CRACK 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 E
- [SDR IPXA2021041368149](https://openairdocs.org/sdr/IPXA2021041368149), Apr 4, 2021: STIFFENER. CRACKED. INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER(P/N:111T2011-6) ON STA 789.5, RBL 55.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV. 79.01 AND UPS 
- [SDR IPXA2020122163647](https://openairdocs.org/sdr/IPXA2020122163647), Dec 18, 2020: FEEDER CABLE. DAMAGED. INSPECTION TYPE: N/A ATB. INFLIGHT ENGINE ANTI ICE EICAS MESSAGE LT ENGINE ANTI ICE CHECKLIST ACCOMPLISHED. NO LT ENGINE ANTI ICE AVAILABLE. PERFORMED VISUAL IN
- [SDR IPXA2020111162260](https://openairdocs.org/sdr/IPXA2020111162260), Nov 11, 2020: SUPPORT ANGLE. CORRODED. INSPECTION TYPE: MOD CORRODED SUPPORT ANGLE AT FS 212-237 LBL 64. SUPPORT ANGLE REPLACED WITH MADE REPAIR PART, IAW CASCADE AEROSPACE ERO 13938. UPS B767-5310-7

All 128: https://openairdocs.org/aircraft/N329UP/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

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.