# N324UP: 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: 27750
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 29, 1998
- Certificate issued: October 30, 1998
- Expires: August 31, 2028
- Mode S code: A37EFC
- 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=324UP
- Page: https://openairdocs.org/aircraft/N324UP

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/N324UP/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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA25LA085](https://openairdocs.org/ntsb/DCA25LA085), Jan 10, 2025: Boeing 767 (N324UP), San Bernardino, CA, substantial damage. Probable cause: Encounter with windshear during landing which resulted in a tailstrike.

## 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 20060720015389I](https://openairdocs.org/incident/20060720015389I), Jul 20, 2006: Boeing 76734AF (N324UP), Ontario, CA. (-23) During approach to ont, the crew heard a "pop" noise. The crew declared an emergency and safely landed at ont. The crew departed the aircraft and the…

## Service difficulty reports (155, 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 IPXA2026092364703](https://openairdocs.org/sdr/IPXA2026092364703), Sep 22, 2026: UNKNOWN. ODOR. VERY STRONG ACID ELECTRICAL SMELL LIKE BURNING PLASTIC IN THE DESCENT STARTING AT FL180 REF AMM 71-00-00-795-034-H03 TEST NO. 3 - GROUND TEST - IDLE LEAK TEST. 
- [SDR IPXA2026092264703](https://openairdocs.org/sdr/IPXA2026092264703), Sep 22, 2026: UNKNOWN. ODOR. VERY STRONG ACID ELECTRICAL SMELL LIKE BURNING PLASTIC IN THE DESCENT STARTING AT FL180. PERFORMED GVI IN BOTH PACK BAYS WITH NO OBVIOUS FAULTS NOTED. DURING RI
- [SDR IPXA2025082044859](https://openairdocs.org/sdr/IPXA2025082044859), Aug 19, 2025: STRUCTURE. DELAMINATED. DELAMINATE- COMPOSITE, VERICAL STABILIZER AUXILIARY SPA AFT FSS 18.037 AREA. (RAPAIR) REQUEST UPS ENGINEERING DETERMINE MAJOR OR MINOR REPAIR.
- [SDR IPXA2025082301209](https://openairdocs.org/sdr/IPXA2025082301209), Aug 16, 2025: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578 LBL 80 INBOARD IN BULK CARGO COMPARTMENT LEFT AREA. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G, REV 93. INSTALL NEW ANGLE IAW SR
- [SDR IPXA2025082301719](https://openairdocs.org/sdr/IPXA2025082301719), Aug 16, 2025: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. REMOVED FLOOR PANEL 252YFF I.A.W AMM 53-01-06-000-801 REV. 145, G.V.I AN
- [SDR IPXA2025082301758](https://openairdocs.org/sdr/IPXA2025082301758), Aug 16, 2025: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA. REMOVED FLOOR PANEL NO. 251CGF IAW AMM 53-01-06-000-801 REV. 145, GVI AND
- [SDR IPXA2025090801808](https://openairdocs.org/sdr/IPXA2025090801808), Aug 16, 2025: HINGE. DAMAGED. FOUND THE ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY WITH DEFORM DAMAGE. REPLACED HINGE ASSY. I.A.W AMM 20-11-00-910-802 REV.146. INSTALLED PLACARD I.A.W AMM 20
- [SDR IPXA202508261209](https://openairdocs.org/sdr/IPXA202508261209), Aug 16, 2025: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578 LBL 80 INBOARD IN BULK CARGO COMPARTMENT LEFT AREA. (REPLACE) ATTACHMENT ARE UPLOADED.
- [SDR IPXA202508261758](https://openairdocs.org/sdr/IPXA202508261758), Aug 16, 2025: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA. (REPLACE) PAPER CHECK OK.
- [SDR IPXA202508261719](https://openairdocs.org/sdr/IPXA202508261719), Aug 16, 2025: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. (REPLACE) PAPER CHECK OK.
- [SDR IPXA2025082501844](https://openairdocs.org/sdr/IPXA2025082501844), Aug 16, 2025: BUMPER. MISSING. FOUND CREW ENTRY DOORWAY LINING BUMPER WITH MISSING. INSTALLED THE BUMPER IAW DWG 411T2036, SHEET 1, REV H & PSDL 411T2240, SHEET DL, REV A.
- [SDR IPXA2025081800044](https://openairdocs.org/sdr/IPXA2025081800044), Aug 16, 2025: BUMPER. MISSING. FOUND CREW ENTRY DOORWAY LINING BUMPER WITH MISSING.
- [SDR IPXA2025081800008](https://openairdocs.org/sdr/IPXA2025081800008), Aug 16, 2025: HINGE. DEFORMED. FOUND THE ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY WITH DEFORM DAMAGE.
- [SDR IPXA2025090884241](https://openairdocs.org/sdr/IPXA2025090884241), Aug 15, 2025: PAWL. DAMAGED. THE PAWL BEHIND THE CREW ENTRY DOOR HANDLE HAS WEAR DAMAGE. REMOVED THE PAWL IAW AMM 52-11-26-004-001, REV 145. INSTALLED A NEW PAWL IAW AMM 52-11-26-404-003, R
- [SDR IPXA202508154241](https://openairdocs.org/sdr/IPXA202508154241), Aug 15, 2025: PAWL. WORN. THE PAWL BEHIND THE CREW ENTRY DOOR HANDLE HAS WEAR DAMAGE OK TO WORK
- [SDR IPXA2025043032293](https://openairdocs.org/sdr/IPXA2025043032293), Apr 24, 2025: SKIN PANEL. DAMAGED. DAMAGE SKIN PANEL FROM STA. 1405 TO STA. 1540, STRINGER 38L TO 38R DUE TO TAIL STRIKE. ALL WORK COMPLETED ON ATTACHED BOEING WORK DOCUMENTS.
- [SDR IPXA2025050588602](https://openairdocs.org/sdr/IPXA2025050588602), Jan 14, 2025: FLOOR SUPPORT. DAMAGED. REMOVED 5 FLOOR STRINGERS AT STA 1417- 1540 FOR FOM AREA RESTORED ON BOEING DOC REM 1 AND 2 ATTACHED. ENTIRE BOEING WORK PACKAGE WILL BE ATTACHED TO LINE ITEM 1
- [SDR IPXA2025050588728](https://openairdocs.org/sdr/IPXA2025050588728), Jan 14, 2025: STIFFENER. DAMAGED. REMOVED 4 VERTICAL L SHAPED STIFFNERS FROM FRAME AT STA 1502 AREA RESTORED ON BOEING DOC REM-10 & 11 (SEE ATTACHED). ENTIRE REPAIR DOCUMENTED ON LINE 103.
- [SDR IPXA2025050588609](https://openairdocs.org/sdr/IPXA2025050588609), Jan 14, 2025: SHEAR TIE. DAMAGED. REMOVED 4 STRINGER SHEAR TIES AND 3 SHEAR CLIPS FROM FRAME AT STA 1439 AREA RESTORED ON REM 12, 13 & 14 (SEE ATTACHED). ENTIRE BOEING REPAIR PACKAGE ATTACHED TO
- [SDR IPXA2025050588685](https://openairdocs.org/sdr/IPXA2025050588685), Jan 14, 2025: SHEAR TIE. DAMAGED. REMOVED 4 SHEAR TIES AND 3 STRINGER TIES FROM FRAME STA 1461 AREA RESTORED ON BOEING DOC REM-15 & 16 (ATTACHED). ENTIRE BOEING WORK PACKAGE WILL BE ATTACHED TO 
- [SDR IPXA2025050588569](https://openairdocs.org/sdr/IPXA2025050588569), Jan 14, 2025: STIFFENER. DAMAGED. REMOVE 4 DAMAGED VERTICAL L SHAPED STIFFNERS FROM FRAME AT STA 1439 4 VERTICAL STIFFENERS REPLACED ON BOEING DOCUMENT REM 8 & 13
- [SDR IPXA2025050588712](https://openairdocs.org/sdr/IPXA2025050588712), Jan 14, 2025: STIFFENER. NOT REPORTED. REMOVED 2 VERTICAL L SHAPED SATIN EARS FROM FRAME AT STA 1480 AREA RESTORED ON REM-12
- [SDR IPXA2025050588745](https://openairdocs.org/sdr/IPXA2025050588745), Jan 14, 2025: FAILSAFE. DAMAGED. CUT OUT DAMAGED SECTION OF LOWER TEE CHORD ON FRAME AT STA 1439 PART REPLACED ON REM-13.
- [SDR IPXA2025050588761](https://openairdocs.org/sdr/IPXA2025050588761), Jan 14, 2025: FAILSAFE. DAMAGED. CUT OU DAMAGED SECTION OF TEE CHORD FROM FRAME AT STA 1461 PART REPLACED ON BOEING REPAIR DOC REM-14 (ATTACHED). ENTIRE BOEING WORK PACKAGE ATTACHED TO LINE ITE
- [SDR IPXA2025011317523](https://openairdocs.org/sdr/IPXA2025011317523), Jan 10, 2025: SKIN. PILOT ERROR. *SDR FILED OPEN* TAIL STRIKE IDENTIFIED ON WALK AROUND INSPECTION
- [SDR IPXA2024013038949](https://openairdocs.org/sdr/IPXA2024013038949), Jan 26, 2024: SUPPORT. BROKEN. FOUND BROKEN INBOARD LEADING EDGE SUPPORT LINK DOORS (SUPPORT ASSY THAT CONNECTED TO WEB ASSY) REMOVED THE BROKEN INBD LE SUPPORT LINK DOORS AND REPLACED NEW IN
- [SDR IPXA2024012638949](https://openairdocs.org/sdr/IPXA2024012638949), Jan 26, 2024: SUPPORT. BROKEN. *SDR FILED OPEN* FOUND BROKEN INBOARD LEADING EDGE SUPPORT LINK DOORS (SUPPORT ASSY THAT CONNECTED TO WEB ASSY)
- [SDR IPXA2023082131089](https://openairdocs.org/sdr/IPXA2023082131089), Aug 9, 2023: SKIN. CHAFED. *** SUPPLEMENTAL SDR *** FAULT - CHAFED - SKIN SURFACE, LOWER FUSELAGE MAIN EQUIPMENT CENTER ACCESS DOOR EXTERNAL. (AGING A/C INSPECTION) (EVALUATE) REVIEWED
- [SDR IPXA20230816089](https://openairdocs.org/sdr/IPXA20230816089), Aug 9, 2023: UNKNOWN. UNKNOWN. FAULT - CHAFED - SKIN SURFACE, LOWER FUSELAGE MAIN EQUIPMENT CENTER ACCESS DOOR EXTERNAL. (AGING A/C INSPECTION) (EVALUATE) PAPER OK
- [SDR IPXA2023081296740](https://openairdocs.org/sdr/IPXA2023081296740), Aug 5, 2023: STIFFENER. CRACKED. FAULT - STIFFENER CENTER WING FRONT SPAR CRACK IS STIFFENER AT STA 785.9 LBL 33 (REPAIR) PERFORM REPAIR I.A.W SRM 57-10-10-2R-2 REPAIR INSTRUCTIONS 4.O~Q REV.86
- [SDR IPXA2023081296743](https://openairdocs.org/sdr/IPXA2023081296743), Aug 5, 2023: STIFFENER. CRACKED. FAULT - STIFFENER CENTER WING FRONT SPAR CRACK IS STIFFENER AT STA 785.9 RBL 11 (REPAIR) PERFORM REPAIR I.A.W SRM 57-10-10-2R-2 REPAIR INSTRUCTIONS 4. O~Q REV.8
- [SDR IPXA2022081985422](https://openairdocs.org/sdr/IPXA2022081985422), Aug 19, 2022: NONE. INOPERATIVE. INSPECTION TYPE:N/AENTRY DOOR GASKET NOT IN TRACKACCOMPLISHED EO B767-5210-84538-A
- [SDR IPXA2022063083650](https://openairdocs.org/sdr/IPXA2022063083650), Jun 29, 2022: FAN. ODOR. STRONG ODOR ON FINAL FWD EQIP COOLING EXH FAN STATUS AFTER LANDING. DEF FWD EQPT COOLING EXH FAN PER MEL 21-58-4-2-1 C/W DMP ACCESS FWD EQPT EXH FAN VERIFIED FA
- [SDR IPXA2021081372700](https://openairdocs.org/sdr/IPXA2021081372700), Aug 5, 2021: FLOOR SUPPORT. CORRODED. INSPECTION TYPE:C12CORROSION WAS FOUND ON INTERCOSTAL(P/N:146T5649-8)ON MAIN DECK FLOOR NEAR STA 1602.64, RBL 54.75.INSTALL NEW PART I.A.W BOEING DWG 146T5650 S
- [SDR IPXA2021081372699](https://openairdocs.org/sdr/IPXA2021081372699), Aug 5, 2021: ANGLE. CORRODED. INSPECTION TYPE:C12CORROSION WAS FOUND ON ANGLE (P/N:146T5628-22) ON MAIN DECK FLOOR BETWEEN STA 1581.845 AND STA 1597.940, RBL 33.INSTALL NEW PART I.A.W. BOEIN
- [SDR IPXA2021081372698](https://openairdocs.org/sdr/IPXA2021081372698), Aug 5, 2021: INTERCOSTAL. CORRODED. INSPECTION TYPE:C12CORROSION WAS FOUND ON INTERCOSTAL(P/N:146T5649-3) ON MAIN DECK FLOOR NEAR STA 1597.04, BETWEEN RBL 11 AND RBL 33.INSTALL NEW I.A.W BOEING DW
- [SDR IPXA2021081372697](https://openairdocs.org/sdr/IPXA2021081372697), Aug 5, 2021: FILLER. CORRODED. INSPECTION TYPE:C12CORROSION WAS FOUND ON FILLER (P/N:146T5609-67) ON MAIN DECK FLOOR NEAR STA 1601,LBL 60.INSTALL NEW PART I.A.W BOEING DWG 146T5650 SH 5, REV 
- [SDR IPXA2021081372696](https://openairdocs.org/sdr/IPXA2021081372696), Aug 5, 2021: ANGLE. CORRODED. INSPECTION TYPE:C12CORROSION WAS FOUND ON CLIP(P/N:146T5619-357) ON MAIN DECK FLOOR NEAR STA 1586.51, LBL 54.75.INSTALL NEW PART I.A.W BOEING DWG 146T5650 SH 4,
- [SDR IPXA2021081372695](https://openairdocs.org/sdr/IPXA2021081372695), Aug 5, 2021: INTERCOSTAL. CORRODED. INSPECTION TYPE:C12CORROSION WAS FOUND ON INTERCOSTAL (P/N;146T5649-7) ON MAIN DECK FLOOR NEAR STA 1602.64, LBL 54.75.INSTALL NEW PART I.A.W BOEING DWG 146T5650
- [SDR IPXA2021081372694](https://openairdocs.org/sdr/IPXA2021081372694), Aug 5, 2021: FILLER. CORRODED. INSPECTION TYPE:C12CORROSION WAS FOUND ON FILLER(P/N:146T5649-67) ON MAIN DECK FLOOR NEAR STA 1601, RBL 60.INSTALL NEW PART I.A.W BOEING DWG 146T5650 SH 5,REV"C
- [SDR IPXA2021081372693](https://openairdocs.org/sdr/IPXA2021081372693), Aug 5, 2021: CHANNEL. CORRODED. INSPECTION TYPE:C12CORROSION WAS FOUND ON MOPSILL(P/N:146T5651-15) ON MAIN DECK CARGO FLOOR STRUCTURE AT STA 1605, LBL54.INSTALL NEW PART I.A.W BOEING DWG 146T5
- [SDR IPXA2021081072606](https://openairdocs.org/sdr/IPXA2021081072606), Aug 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.80.03 AND UPS EO 
- [SDR IPXA2020012751443](https://openairdocs.org/sdr/IPXA2020012751443), Jan 25, 2020: UNKNOWN. ODOR. ON DESCENT INTO ONT PASSING THROUGH 17,000, STRONG ODOR OF BURNING RUBBER FILLED THE COCKPIT LASTED FOR APPROXIMATELY 3 MINUTES. THEN DISSIPATEDA/C POWERED FOR 
- [SDR IPXA2020011550914](https://openairdocs.org/sdr/IPXA2020011550914), Jan 13, 2020: PITOT TUBE. OBSTRUCTED. INSPECTION TYPE:N/A**AIR TURN BACK** AIRSPEED UNRELIABLE, SINGLE AIR DATA, RUDDER RATIO, L ENG EEC, R ENG EEC, AILERON LOCKOUT.FLUSHED PITOT STATIC SYS AS PER A
- [SDR IPXA2019091346699](https://openairdocs.org/sdr/IPXA2019091346699), Sep 4, 2019: SKIN. CRACKED. INSPECTION TYPE:C11 CRACK ON FUSELAGE SKIN (P/N: 148T3121-2) ON STA 1725.5, NEAR S-7R. REPAIR IAW EO B767-5330-24301 APPX C AND 5330-73933-A, SR:4-4555838821, A
- [SDR IPXA2019091146598](https://openairdocs.org/sdr/IPXA2019091146598), Sep 2, 2019: STIFFENER. CRACKED. INSPECTION TYPE:C11 CRACK ON VERTICAL STIFFENER AT WHEEL WELL BULKHEAD AT STA 287, RBL 25. REPAIR IAW EO B767-5310-20118-F AND SRM 51-70-12 GENERAL, FIGURE 1, R
- [SDR IPXA2019082876060](https://openairdocs.org/sdr/IPXA2019082876060), Aug 26, 2019: SWITCH. FAILED. EMERGENCY LIGHT SWITCH INOP. R&R'D CONT PNL PER AMM 33 51 08. OS CHK GOOD. IPC 32 51 08 01A, 010
- [SDR IPXA201906143225](https://openairdocs.org/sdr/IPXA201906143225), Jun 12, 2019: SEAL. OUT OF POSITION. MAIN ENTRY DOOR IS DIFFICULT TO LIFT AFTER FLIGHT.FOUND AFT DOOR LINER SEAL OUT OF RETAINER. REINSTALLED SEAL AND CLEANED. DOOR OPS NORMAL PER AMM 52-12-00
- [SDR IPXA2019050341714](https://openairdocs.org/sdr/IPXA2019050341714), May 3, 2019: DOOR SEAL. UNSECURE. INSPECTION TYPE:N/A CREW ENTRY DOOR SEAL (INNER) IS COMING OFF. REINSTALLED CREW ENTRY DOOR FWD INNER TRIM SEAL REF AMM 52 09 01 OPERATED DOOR SEVERAL TIMES REF
- [SDR IPXA2019031340010](https://openairdocs.org/sdr/IPXA2019031340010), Mar 12, 2019: DOOR SEAL. NOT SEATED. INSPECTION TYPE:N/A CREW ENTRY DOOR RUBBER SEAL WILL NOT STAY STRAIGHT WHEN CLOSING THE CREW ENTRY DOOR. RESEATED SEAL ON TRACK RE AMM 52-09-01.

All 155: https://openairdocs.org/aircraft/N324UP/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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