# N322UP: 1997 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: 27748
- Year built: 1997
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 2, 1997
- Certificate issued: December 3, 2009
- Expires: February 28, 2029
- Mode S code: A3778E
- 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=322UP
- Page: https://openairdocs.org/aircraft/N322UP

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/N322UP/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 N322UP.

## FAA accident and incident reports

None matched to N322UP.

## Service difficulty reports (144, 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 IPXA2026102133469](https://openairdocs.org/sdr/IPXA2026102133469), Oct 20, 2026: FLOOR PANEL. DAMAGED. MAJOR REPAIR. FOUND MAIN DECK FLOOR PANEL DAMAGE ,
- [SDR IPXA2026102108780](https://openairdocs.org/sdr/IPXA2026102108780), Oct 18, 2026: FLOOR PANEL. DAMAGED. MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL DAMAGE. IAW AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-04-004-010 REV.149 REMOVED MAIN DECK CARGO HANDLI
- [SDR IPXA2026102268685](https://openairdocs.org/sdr/IPXA2026102268685), Oct 9, 2026: SKIN. DAMAGED. MAJOR REPAIR, PANEL AFT OF 321D RHT SIDE OF VERTICAL STABILIZER HAS LIGHTNING STRIKE DAMAGE 7.5€? FROM BOTTOM & 12€? FROM LEADING EDGE. PERFORMED NDT/UT FOR T
- [SDR IPXA2026102268850](https://openairdocs.org/sdr/IPXA2026102268850), Oct 9, 2026: SKIN. DAMAGED. MAJOR REPAIR, PANEL AFT OF 321C RHT SIDE OF VERTICAL STABILIZER HAS LIGHTNING STRIKE DAMAGE 43€? FROM TOP & 14€? FROM TRAILING EDGE. SEE ATTACHED PICTURE. PER
- [SDR IPXA2026092264312](https://openairdocs.org/sdr/IPXA2026092264312), Sep 22, 2026: WARNING MESSAGE. FALSE ACTIVATION. EMERGENCY DECLARED ON APPROACH TO LANDING. FLAPS 25 SELECTED AND LE-SLAT DISAGREE EICAS CAME ON. TROUBLESHOT IAW FIM 27-51 FT 808, NO FAULTS NOTED. EXTENDED AND
- [SDR IPXA2026091329466](https://openairdocs.org/sdr/IPXA2026091329466), Sep 13, 2026: PUMP. FAULTED. RECEIVED A CHYD PUMP1 OVERHEAT. RAN QRH PROCEDURE, RAN QRH PROCEDURE, DECLARED EMERGENCY FOR PRIORITY HANDLING. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED CT
- [SDR IPXA2026062555305](https://openairdocs.org/sdr/IPXA2026062555305), Jun 7, 2026: SWIVEL FITTING. CORRODED. AFTER REMOVAL RT MLG STRUT SWIVEL FITTING FOUND OUTER SHAFT OF INBOARD CRANK AND DRIVE ARMS WITH CORROSION IN THE TEETH, FLL-023, ATA 57. NEW SHAFT ASSEMBLY PRO
- [SDR IPXA2026062532624](https://openairdocs.org/sdr/IPXA2026062532624), May 23, 2026: SWIVEL. CORRODED. RT MLG, SIDE STRUT SWIVEL (PART OF THE MLG SUPPORT BEAM ASSEMBLY) HAS CORROSION AROUND AND UNDERNEATH THE O/B BUSHING, FLL-005, REMOVE CORROSION OF RH MLG, SIDE
- [SDR IPXA2025081104151](https://openairdocs.org/sdr/IPXA2025081104151), Aug 11, 2025: SENSOR. OUT OF ADJUST. BTD DUE TO FWD ENTRY DOOR EICAS L FWD ENTRY DOOR ON PUSH BACK. ADJUSTED SENSOR AND TESTED SATIS PER AMM TASK 52-12-00-715-119 REV 137.
- [SDR IPXA2025022030552](https://openairdocs.org/sdr/IPXA2025022030552), Feb 19, 2025: SENSOR. FAULTED. IN FLIGHT, AIR/GND DISAGREEE€? STATUS MESSAGE PERFORMED PSEU BITE TEST. R GEAR TILT SENSOR S268 FAULTED. REMOVED AND REPLACED RH TILT SENSOR PER AMM 32-09-07. 
- [SDR IPXA2024101654112](https://openairdocs.org/sdr/IPXA2024101654112), Oct 10, 2024: CARGO TRACK. BROKEN. FOUND MAIN DECK CARGO TRACK ASSY BROKEN AT : STA 1510 LBL 33.00 (REPAIR) ATTACHEMENTS ARE UPLOADED. OPEN
- [SDR IPXA2024101697157](https://openairdocs.org/sdr/IPXA2024101697157), Oct 7, 2024: BEAR STRAP. CRACKED. FAULT - FOUND CRACK ON THE NO.1 FORWARD ENTRY DOOR AFT LOWER CORNER BEAR STRIP. (REPAIR) REVIEWED
- [SDR IPXA2024100894916](https://openairdocs.org/sdr/IPXA2024100894916), Oct 7, 2024: FLOOR PANEL. DAMAGED. *** MAJOR REPAIR *** FAULT - DAMAGE - FLOOR PNL , AT MAIN DECK , PANEL P/N: 145T5876-64 PNL NO.242CFF. (REPAIR) REQUEST PERFORM MAIN DECK CARGO FLOOR PANEL OK T
- [SDR IPXA2024100895541](https://openairdocs.org/sdr/IPXA2024100895541), Oct 7, 2024: FLOOR PANEL. CRACKED. MAJOR REPAIR *** FAULT - CRACK - FLOOR PNL , AT MAIN DECK STA 1043~ STA 1109 , PANEL P/N: 145T5876-44 , PNL NO.242WFF. (REPAIR) REQUEST PERFORM MAIN DECK CARGO 
- [SDR IPXA2024101684508](https://openairdocs.org/sdr/IPXA2024101684508), Oct 6, 2024: RIB. CRACKED. CRACK - FITTING, RIGHT WING NO.10 SPOILER HINGE INBD SIDE (REPLACE) 1.OK TO INSTALL CHECK SATISFIED. 2.I.A.W AMM 20-10-03-404-037 REV.143 RECONNECT RH OUTBOARD 
- [SDR IPXA2024100876218](https://openairdocs.org/sdr/IPXA2024100876218), Oct 5, 2024: FLOOR PANEL. BROKEN. *** MAJOR REPAIR *** FAULT - BROKEN - FLOOR PNL, AT MAIN DECK, PANEL P/N: 145T5876-63, PNL NO.241DFF. (REPAIR) REQUEST PERFORM MAIN DECK CARGO FLOOR PANEL OK TO
- [SDR IPXA2024100876234](https://openairdocs.org/sdr/IPXA2024100876234), Oct 5, 2024: FLOOR PANEL. DAMAGED. *** MAJOR REPAIR *** FAULT - DAMAGE - FLOOR PNL, AT MAIN DECK, PANEL P/N: 145T5876-60 PNL NO.241FFF. (REPAIR) REQUEST PERFORM MAIN DECK CARGO FLOOR PANEL OK TO 
- [SDR IPXA2024100871727](https://openairdocs.org/sdr/IPXA2024100871727), Oct 5, 2024: FLOOR PANEL. DAMAGED. *** MAJOR REPAIR *** FAULT - FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE PANEL NO.251UFF P/N: 146T5869-79 (REPAIR) I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404
- [SDR IPXA2024100872662](https://openairdocs.org/sdr/IPXA2024100872662), Oct 5, 2024: FLOOR PANEL. DENTED. *** MAJOR REPAIR *** FAULT - FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE PANEL NO.251LFF P/N: 146T5869-78 (REPAIR) I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404
- [SDR IPXA2024100876223](https://openairdocs.org/sdr/IPXA2024100876223), Oct 5, 2024: FLOOR PANEL. DAMAGED. MAJOR REPAIR *** FAULT - CRACK - FLOOR PNL, M/D STA 977~STA 1043, PANEL P/N: 145T5876-71, PNL NO.241YFF. (REPAIR) REQUEST PERFORM MAIN DECK CARGO FLOOR PANEL OK
- [SDR IPXA2024100871732](https://openairdocs.org/sdr/IPXA2024100871732), Oct 5, 2024: FLOOR PANEL. DAMAGED. MAJOR REPAIR *** FAULT - FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE PANEL NO.231RFF P/N: 143T5876-58 (REPAIR) I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404-005
- [SDR IPXA2024102287628](https://openairdocs.org/sdr/IPXA2024102287628), Oct 1, 2024: NONE. NONE. (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R)
- [SDR IPXA2024102291536](https://openairdocs.org/sdr/IPXA2024102291536), Oct 1, 2024: LENS. CRACKED. FOUND ENTRY DOOR FWD SIDE DOORWAY SIGN ASSY LENS CRACK. (REPLACE) 1. I.A.W AMM 33-51-01-022-029, 33-51-01-402-030 REV 143 REPLACED EXIT SIGN, AND CONDITION CHEC
- [SDR IPXA2024100287628](https://openairdocs.org/sdr/IPXA2024100287628), Oct 1, 2024: NONE. NONE. FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) OK TO WORK
- [SDR IPXA2024100191536](https://openairdocs.org/sdr/IPXA2024100191536), Oct 1, 2024: LENS. CRACKED. *SDR FILED OPEN* FAULT - FOUND ENTRY DOOR FWD SIDE DOORWAY SIGN ASSY LENS CRACK. (REPLACE)
- [SDR IPXA2024101674413](https://openairdocs.org/sdr/IPXA2024101674413), Sep 30, 2024: ANGLE. CRACKED. FOUND BULK CARGO COMPARTMENT LEFT AREA ANGLE CRACK AT STA 1578 LBL 80 INBOARD. (REPLACE) 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 90. 2. INSTALLED NEW 
- [SDR IPXA2024101674438](https://openairdocs.org/sdr/IPXA2024101674438), Sep 30, 2024: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA. (REPLACE) I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.143 INS
- [SDR IPXA2024090764443](https://openairdocs.org/sdr/IPXA2024090764443), Sep 6, 2024: FLOOR PANEL. DAMAGED. FOUND DAMAGE ON PREVIOUS REPAIR OF REMOVED FLOORBOARD FROM POS 9/10 CENTER. ROUTED FLOOR PANEL TO SHEET METAL FOR EVAL INSTALLED MAIN CARGO DECK FLOOR PANEL IAW
- [SDR IPXA2024032136997](https://openairdocs.org/sdr/IPXA2024032136997), Mar 13, 2024: SKIN. CORRODED. FUSELAGE DRAIN VALVE ASSY AT BELLY ZONE 155/156 ,APPROXIMATE FUSELAGE STA. 1373 HAS PULLED THROUGH SKIN AND HAS EXTENSIVE CORROSION AROUND HOLE CREATED,ON OUTER
- [SDR IPXA2024031436997](https://openairdocs.org/sdr/IPXA2024031436997), Mar 13, 2024: DRAIN VALVE. CORRODED. FUSELAGE DRAIN VALVE ASSY AT BELLY ZONE 155/156 ,APPROXIMATE FUSELAGE STA. 1373 HAS PULLED THROUGH SKIN AND HAS EXTENSIVE CORROSION AROUND HOLE CREATED,ON OUTER
- [SDR IPXA2024012052414](https://openairdocs.org/sdr/IPXA2024012052414), Jan 20, 2024: CABIN PRESSURE. FAULTED. *ETOPS FILED OPEN* STATUS MSG CABIN ALT AUTO 2 APPEARED ENROUTE AT CRUISE ALTITUDE WHILE SWITCH WAS IN AUTO 2 DEFERRED CABIN ALT AUTO 2 INOP PER MEL 21-31-1A. P
- [SDR IPXA2024013124637](https://openairdocs.org/sdr/IPXA2024013124637), Jan 13, 2024: TRIM PANEL. BROKEN. **SUPPLEMENTAL SDR**TRIM BROKEN L1 DOOR SIDE WALL PANEL INSTALLED NEW SPLINE TRIM PIECE I/A/W INDUSTRY STANDARD PRACTICES AND IPC 52-11-02-10A. NO DEFECTS NOTED
- [SDR IPXA2024011424637](https://openairdocs.org/sdr/IPXA2024011424637), Jan 13, 2024: UNKNOWN. UNKNOWN. RIM BROKEN L1 DOOR SIDE WALL PANEL ASSIGNED EO-89173-REQ1 TO FAULT.
- [SDR IPXA2024020776726](https://openairdocs.org/sdr/IPXA2024020776726), Sep 16, 2023: COVER. BROKEN. PLASTIC DOOR HANDLE COVER ON MAIN ENTRY DOOR BROKE OFF. INSTALLED HINGE AND ACCESS DOOR IAW SRM 51-40-02. C/W REINSTALLED ACCEST PANEL
- [SDR IPXA2023091676726](https://openairdocs.org/sdr/IPXA2023091676726), Sep 16, 2023: UNKNOWN. UNKNOWN. **SDR FILED OPEN**PLASTIC DOOR HANDLE COVER ON MAIN ENTRY DOOR BROKE OFF.***REQ 465504***SM4/LMX4*** DEFERRED PER MEL 52-11-2
- [SDR IPXA2023050846048](https://openairdocs.org/sdr/IPXA2023050846048), May 6, 2023: ESCAPE REEL. DAMAGED. 3RD (FROM FWD) EMERGENCY DESCENT DEVICE DAMAGED WILL NOT STOW PROPERLY R&R'D EMERGENCY DESCENT DEVICE ( POS 3) IAW AMM 25-61-03-201
- [SDR IPXA2023050847127](https://openairdocs.org/sdr/IPXA2023050847127), May 6, 2023: ESCAPE REEL. PARTIAL DEPLOY. EMERGENCY DESCENT DEVICE (4TH FROM FWD) PARTIALLY DEPLOYED R&R'D EMERGENCY DESCENT DEVICE #4 IAW AMM 25-61-03-201
- [SDR IPXA2023051393098](https://openairdocs.org/sdr/IPXA2023051393098), Feb 22, 2023: FLOORBOARD. DAMAGED. MAIN CARGO COMPARTMENT FLOOR PANEL REPAIR (SREO) 27379. REF EO-27379 * PARTS REQ 438130 *)***SM13/LMX8*** ALL STEPS COMPLIED WITH, REF SREO-9693-REQ001 T3F18E00
- [SDR IPXA2022110287740](https://openairdocs.org/sdr/IPXA2022110287740), Oct 28, 2022: SKIN. CORRODED. INSPECTION TYPE:C13, CORROSION WAS FOUND ON SKIN (P/N:114T4103-4) OF NO.10 SLAT BETWEEN OSS 684 AND 693.REPAIR I.A.W 767-300F SRM 57-43-01-1A-1, ALLOWABLE DAMAG
- [SDR IPXA2022110387788](https://openairdocs.org/sdr/IPXA2022110387788), Oct 25, 2022: SKIN. CRACKED. INSPECTION TYPE:C13, CRACK DAMAGE WAS FOUND ON NR 1 PYLON OUTBD SKIN ASSEMBLY (P/N:311T2450-25) NEAR NAC STA 237.5. PERFORM REPAIR I.A.W UPS EO B767-5430-85116-
- [SDR IPXA2022110287741](https://openairdocs.org/sdr/IPXA2022110287741), Oct 25, 2022: SKIN. CORRODED. INSPECTION TYPE:C13CORROSION WAS FOUND ON SKIN(P/N:114T4104-4) OF NO.9 SLAT BETWEEN OSS 670 AND 682.REPAIR I.A.W 767-300F SRM 57-43-01-1A-1, ALLOWABLE DAMAMGE 1
- [SDR IPXA2021022466057](https://openairdocs.org/sdr/IPXA2021022466057), Feb 23, 2021: SHUTOFF VALVE. MALFUNCTIONED. INSPECTION TYPE: ETOP** ETOPS FILED OPEN ** ON TAKEOFF @70 KTS, RECEIVED A L ENG HPSOV VALVE EICAS CAUTION LIGHT. RESULTED IN A RTO. DEFERRED LEFT ENG HPSOV PER
- [SDR IPXA2021020465312](https://openairdocs.org/sdr/IPXA2021020465312), Feb 4, 2021: BATTERY. NO TEST. INSPECTION TYPE:NAEMER. LIGHT TEST INOP.R&R BATTERY IAW AMM 33-51-01 EMER. LIGHT TEST OK.
- [SDR IPXA2021020265212](https://openairdocs.org/sdr/IPXA2021020265212), Feb 1, 2021: BATTERY PACK. INOPERATIVE. INSPECTION TYPE:NAEMERGENCY LIGHT'S WOULD NOT ILLUMINATE WITH SWITCH IN ON POSITION.R&R BATTERY PACK I/A/W AMM 33-51-07-422-012, OP'S CK'ED OK. REF 33-51-07-32-
- [SDR IPXA2021011864558](https://openairdocs.org/sdr/IPXA2021011864558), Jan 16, 2021: CONTROL PANEL. INTERMITTENT. INSPECTION TYPE: NA EMERGENCY LIGHTS COME ON FOR 1-2 SECONDS, THEN GO OUT. RESET SWITCHES SEVERAL TIMES, PROBLEM CONTINUES. R & R THE EMERGENCY LIGHT CONTROL PA
- [SDR IPXA2020101261186](https://openairdocs.org/sdr/IPXA2020101261186), Oct 2, 2020: STIFFENER. CRACKED. INSPECTION TYPE: C12 CRACK ON CENTER WING TANK STIFFENER (P/N: 111T2011-6) ON STA 785, RBL 55. REPAIR IAW 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV 78.00 AND UPS 
- [SDR IPXA2020101261185](https://openairdocs.org/sdr/IPXA2020101261185), Oct 2, 2020: STIFFENER. CRACKED. INSPECTION TYPE: C12 CRACK ON CENTER WING TANK STIFFENER (P/N: 111T2008-12) ON STA 785, RBL 33. REPAIR IAW 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV 78.00, AND UP
- [SDR IPXA2019112749468](https://openairdocs.org/sdr/IPXA2019112749468), Nov 26, 2019: WINDOW. CRACKED. CAPTAIN FWD WINDOW IS CRACKED, PRESSURE HOLDING, NO AIR LEAK NOTED. R & R THE LEFT FWD AND RT SIDE WINDOW HEAT CONTROL UNIT IAW AMM 30-40-01. OPS CHECKED GOOD. 
- [SDR IPXA2019112544328](https://openairdocs.org/sdr/IPXA2019112544328), Nov 24, 2019: SKIN. PUNCTURED. INSPECTION TYPE:N/ALEFT ELEVATOR UPPER SKIN HAS SMALL PUNCTUREREPAIRED PER EO B767-5520-74726-A
- [SDR IPXA2018120236483](https://openairdocs.org/sdr/IPXA2018120236483), Dec 1, 2018: O-RING. LEAKING. NR 2 ENGINE, NR 1 BEARING MANIFOLD WAS LEAKING. R & R THE BEARING MANIFOLD O-RING IAW 72-31-03-401.

All 144: https://openairdocs.org/aircraft/N322UP/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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