# N326UP: 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: 27752
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 24, 1998
- Certificate issued: November 27, 1998
- Expires: November 30, 2028
- Mode S code: A3866A
- 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=326UP
- Page: https://openairdocs.org/aircraft/N326UP

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/N326UP/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 N326UP.

## FAA accident and incident reports

None matched to N326UP.

## Service difficulty reports (146, 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 IPXA2026072007978](https://openairdocs.org/sdr/IPXA2026072007978), Jul 17, 2026: WINDOW. CRACKED. CAPTAINS L2 WINDOW FOUND CRACKED FROM TOP TO BOTTOM! REPLACED LT SLIDING FLIGHT DECK WINDOW IAW AMM 56-11-02. PRESSURIZED AIRCRAFT WITH NO LEAKS NOTED. WINDOW H
- [SDR IPXA2026071707978](https://openairdocs.org/sdr/IPXA2026071707978), Jul 17, 2026: WINDOW. CRACKED. CAPTAINS L2 WINDOW FOUND CRACKED FROM TOP TO BOTTOM!
- [SDR IPXA2026060105255](https://openairdocs.org/sdr/IPXA2026060105255), May 29, 2026: WINDOW. CRACKED. L SIDE WINDOW EICAS. INNER PANE CRACKED. WINDOW HEAT SWITCH OFF IAW QRH. PERFORMED RII INSPECTION PER GMM 04-02 AND AMM 56-11-10 VERIFIED PROPER INSTALL AND TOR
- [SDR IPXA2026052900055](https://openairdocs.org/sdr/IPXA2026052900055), May 29, 2026: WINDOW. CRACKED. LEFT SIDE WINDOW EICAS. INNER PANE CRACKED. WINDOW HEAT SWITCH OFF IAW QRH.
- [SDR IPXA2026052906642](https://openairdocs.org/sdr/IPXA2026052906642), May 29, 2026: WINDOW. FAILED. L3 WINDOW BURNED AT TEMP CONTROL SENSORS. CREW REPORTED BURNING SMELL PRIOR TO WINDOW CRACKING. REF BARCODE [T3F18E008X3R6] FOR WINDOW REPLACEMENT. R+R RIGHT FO
- [SDR IPXA2026021059426](https://openairdocs.org/sdr/IPXA2026021059426), Jan 31, 2026: SKIN PANEL. CORRODED. MAJOR REPAIR, CORROSION FUSELAGE SKIN STA 1410 BETWEEN S-38R AND S-39R. (REPAIR. ACCOMPLISHED THE REPAIR I.A.W SRM 53-00-01 REPAIR 29 REV. 94 AND EGAT EI NO.F20
- [SDR IPXA2026020707464](https://openairdocs.org/sdr/IPXA2026020707464), Jan 28, 2026: SKIN PANEL. CRACKED. MAJOR REPAIR, FOUND CRACK ON THE NO.1 FWD ENTRY DOOR LH AFT LOWER CORNER SKIN. ACCOMPLISHED THE REPAIR I.A.W SRM 53-10-01-2R-1 REV. 94 AND EGAT WORK SHEET NO: 6
- [SDR IPXA2026020977464](https://openairdocs.org/sdr/IPXA2026020977464), Jan 28, 2026: SKIN. CRACKED. MAJOR REPAIR. FOUND A CRACK ON THE NR1 FWD ENTRY DOOR LT AFT LOWER CORNER SKIN. INSTALLED ENTRY DOOR SCUFF PLATE IAW AMM 53-13-01-424-005, REV 147. INSTALLED EN
- [SDR IPXA2025063074896](https://openairdocs.org/sdr/IPXA2025063074896), Jun 29, 2025: LIGHT. INOPERATIVE. COCKPIT EMERGANCY LIGHT EXIT INOP REMOVED AND REPLACED EMERGANCY BATTERY CHARGER ASSY PER MM 33-51-07. OPS CK GOOD
- [SDR IPXA2024102127737](https://openairdocs.org/sdr/IPXA2024102127737), Oct 19, 2024: COVER. DETACHED. EXIT LIGHT COVER FOR LIGHT OVER CREW DOOR HANDLE FELL OFF WILL NOT STAY ATTACHED. C/W EO-91789-REQ1
- [SDR IPXA2024101927838](https://openairdocs.org/sdr/IPXA2024101927838), Oct 19, 2024: CHARGER. INOPERATIVE. MAIN ENTRY DOOR EMERGENCY LIGHT WILL NOT ILLUMINATE AFTER ATTACHING COVER REMOVED AND REPLACED EMERGENCY BATTERY CHARGER ASSEMBLY IAW AMM 33-51-07. OPS CHECK GO
- [SDR IPXA2024030705540](https://openairdocs.org/sdr/IPXA2024030705540), Mar 5, 2024: WINDOW. LEAKING. R2 WINDOW HAS LOUD SQUEAL WHICH STARTED ON CLIMB THROUGH DESCENT, AND IN CRUISE. EVIDENCE OF AIR LEAKAGE. PERFORMED R2 WINDOW ADJUSTMENT PER AMM 56-11-02-825-12
- [SDR IPXA2024030605540](https://openairdocs.org/sdr/IPXA2024030605540), Mar 5, 2024: WINDOW. LEAKING. *** SDR FILED OPEN *** R2 WINDOW HAS LOUD SQUEAL WHICH STARTED ON CLIMB THROUGH DESCENT, AND IN CRUISE. EVIDENCE OF AIR LEAKAGE. C/W RII
- [SDR IPXA2024012302696](https://openairdocs.org/sdr/IPXA2024012302696), Jan 12, 2024: ANGLE. BROKEN. FAULT - FOUND THREE OF CLIPS WITH BROKEN ON CREW ENTRY DOOR LOWER SILL (REPLACE). 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 88. 2. INSTALLED NEW PART I.
- [SDR IPXA2024012301393](https://openairdocs.org/sdr/IPXA2024012301393), Jan 12, 2024: SCUFF PLATE. CRACKED. FAULT - FOUND THE SCREW ENTRY DOOR SCUFF PLATE WITH CRACK DAMAGE (REPLACE). 1.I.A.W AMM 53-13-01-424-005 REV.141 INSTALLED THE SCUFF PLATE. 2.ACCOMPLISHED THE E
- [SDR IPXA2024011202696](https://openairdocs.org/sdr/IPXA2024011202696), Jan 12, 2024: UNKNOWN. UNKNOWN. FOUND THREE OF CLIPS WITH BROKEN ON CREW ENTRY DOOR LOWER SILL (REPLACE)
- [SDR IPXA2024011201393](https://openairdocs.org/sdr/IPXA2024011201393), Jan 12, 2024: UNKNOWN. UNKNOWN. FOUND THE SCREW ENTRY DOOR SCUFF PLATE WITH CRACK DAMAGE (REPLACE) OK TO WORK
- [SDR IPXA2024012382386](https://openairdocs.org/sdr/IPXA2024012382386), Jan 11, 2024: PAWL. WORN. FAULT - FOUND CREW ENTRY DOOR EXTERNAL HANDLE PAWL WORN. (REPLACE). I.A.W AMM 52-11-26-004-001 REV.141 AND AMM 52-11-26-404-003 REV.141 REPLACED PAWL, OPERATION
- [SDR IPXA2024012382163](https://openairdocs.org/sdr/IPXA2024012382163), Jan 11, 2024: CAP. CRACKED. FAULT - CRACK EDGE, LH WING OUTBD FLAP INBD SIDE END CAP (REPAIR). REMOVE THE DAMAGE AREA (L:0.2", W:0.1 , 5" FROM AFTER EDGE AT LOWER EDGE) AND CLEAN. BOND THE
- [SDR IPXA2024012382059](https://openairdocs.org/sdr/IPXA2024012382059), Jan 11, 2024: WEB. CRACKED. *SUPPLEMENTAL SDR* FAULT - CRACK WEB, LH WING LE STRUCTURE INTERNAL WEB NEAR LES 594 (REPAIR). ACCOMPLISHED REPAIR I.A.W UPS EO-89236-REQ1 REV.1. JOB COMPLETED.
- [SDR IPXA2024012282141](https://openairdocs.org/sdr/IPXA2024012282141), Jan 11, 2024: SPAR. BROKEN. FAULT - BROKEN PLATE, LH WING T/E REAR SPAR LOWER SURFACE NEAR WS 698 (REPLACE). 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 88. 2. INSTALLED NEW PART I.A
- [SDR IPXA2024011182059](https://openairdocs.org/sdr/IPXA2024011182059), Jan 11, 2024: UNKNOWN. UNKNOWN. CRACK WEB, LH WING LE STRUCTURE INTERNAL WEB NEAR LES 594 (REPAIR) OK TO WORK
- [SDR IPXA2024011182386](https://openairdocs.org/sdr/IPXA2024011182386), Jan 11, 2024: UNKNOWN. UNKNOWN. FOUND CREW ENTRY DOOR EXTERNAL HANDLE PAWL WORN. (REPLACE) OK TO WORK
- [SDR IPXA2024011182163](https://openairdocs.org/sdr/IPXA2024011182163), Jan 11, 2024: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** FAULT - CRACK EDGE, LH WING OUTBD FLAP INBD SIDE END CAP (REPAIR) OK TO WORK
- [SDR IPXA2024012360713](https://openairdocs.org/sdr/IPXA2024012360713), Jan 10, 2024: SKIN. DAMAGED. FAULT - CRACK - SPLICE, RH WING OUTBD FXD LE NOSE SKIN, OSS 694.55. (REPLACE). 1.REMOVED DAMAGE PARTS I.A.W. SRM 51-40-02-0G REV.88 2.INSTALLED NEW PARTS I.A.W.
- [SDR IPXA2024012355631](https://openairdocs.org/sdr/IPXA2024012355631), Jan 10, 2024: SKIN. ERODED. *SUPPLEMENTAL SDR* FAULT - EROSION, LH WING NO.4 SLAT OUTBD CLOSURE PNL (REPAIR). REMOVE THE DAMAGE MATERIALS AND CLEAN.MEASURE THE DAMAGE AREA(LENGTH:0.5", WID
- [SDR IPXA2024011060713](https://openairdocs.org/sdr/IPXA2024011060713), Jan 10, 2024: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** FAULT - CRACK - SPLICE, RH WING OUTBD FXD LE NOSE SKIN, OSS 694.55. (REPLACE)
- [SDR IPXA2024011055631](https://openairdocs.org/sdr/IPXA2024011055631), Jan 10, 2024: UNKNOWN. UNKNOWN. EROSION, LH WING NO.4 SLAT OUTBD CLOSURE PNL (REPAIR) OK TO WORK
- [SDR IPXA2024011635744](https://openairdocs.org/sdr/IPXA2024011635744), Jan 9, 2024: ANGLE. CRACKED. FAULT - CRACK - ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60 INBOARD SIDE (REPLACE). 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 88. 2. INSTALL
- [SDR IPXA2024012337994](https://openairdocs.org/sdr/IPXA2024012337994), Jan 9, 2024: BUMPER. DEFORMED. FAULT - FOUND FWD ENTRY DOORWAY LINING BUMPER DEFORM (REPLACE). I.A.W AMM 52-12-02-004-001 REV.141 AND AMM 52-12-02-404-025 REV.141 REPLACED BUMPER. PARTS INFO 
- [SDR IPXA2024012335573](https://openairdocs.org/sdr/IPXA2024012335573), Jan 9, 2024: SEAL. BROKEN. FAULT - FOUND ENTRY DOORWAY AFT LINING SEAL BROKEN (REPLACE). I.A.W AMM 52-09-01-024-018 REV. 141 AND AMM 52-09-01-424-019 REV.141 REPLACED DOORWAY LINING SEAL.
- [SDR IPXA2024011735666](https://openairdocs.org/sdr/IPXA2024011735666), Jan 9, 2024: ANGLE. CRACKED. FAULT - CRACK - ANGLE, MAIN EQUIPMENT CENTER LEFT SIDE AT STA 246 LBL 49.3.(REPLACE). REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-05 REV. 88. PERFORMED THE HEAT TRE
- [SDR IPXA2024011635775](https://openairdocs.org/sdr/IPXA2024011635775), Jan 9, 2024: ANGLE. CRACKED. *SUPPLEMENTAL SDR* FAULT - CRACK - ANGLE, BULK CARGO COMPARTMENT LEFT AREA STA 1578 LBL 60 INBOARD SIDE (REPLACE) 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G R
- [SDR IPXA2024011635793](https://openairdocs.org/sdr/IPXA2024011635793), Jan 9, 2024: ANGLE. CRACKED. FAULT - CRACK - ANGLE BULK CARGO COMPARTMENT LEFT SIDE STA 1578 LBL 60 OUTBOARD SIDE (REPLACE). 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 88. 2. INSTALL
- [SDR IPXA2024011635810](https://openairdocs.org/sdr/IPXA2024011635810), Jan 9, 2024: ANGLE. CRACKED. *SUPPLEMENTAL SDR* FAULT - CRACK - ANGLE BULK CARGO COMPARTMENT RIGHT SIDE STA 1578 RBL 60 OUTBOARD SIDE (REPLACE). 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G
- [SDR IPXA2024011037994](https://openairdocs.org/sdr/IPXA2024011037994), Jan 9, 2024: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** FAULT - FOUND FWD ENTRY DOORWAY LINING BUMPER DEFORM (REPLACE) OK TO WORK
- [SDR IPXA2024011035573](https://openairdocs.org/sdr/IPXA2024011035573), Jan 9, 2024: UNKNOWN. UNKNOWN. FOUND ENTRY DOORWAY AFT LINING SEAL BROKEN (REPLACE) OK TO WORK
- [SDR IPXA2024010935666](https://openairdocs.org/sdr/IPXA2024010935666), Jan 9, 2024: UNKNOWN. UNKNOWN. CRACKED ANGLE, MAIN EQUIPMENT CENTER LEFT SIDE AT STA 246 LBL (REPLACE) OK TO WORK
- [SDR IPXA2024010935810](https://openairdocs.org/sdr/IPXA2024010935810), Jan 9, 2024: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** FAULT - CRACK - ANGLE BULK CARGO COMPARTMENT RIGHT SIDE STA 1578 RBL 60 OUTBOARD SIDE (REPLACE) OK TO WORK
- [SDR IPXA2024010935744](https://openairdocs.org/sdr/IPXA2024010935744), Jan 9, 2024: UNKNOWN. UNKNOWN. CRACK - ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60 INBOARD SIDE (REPLACE) OK TO WORK
- [SDR IPXA2024010935793](https://openairdocs.org/sdr/IPXA2024010935793), Jan 9, 2024: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** FAULT - CRACK - ANGLE BULK CARGO COMPARTMENT LEFT SIDE STA 1578 LBL 60 OUTBOARD SIDE (REPLACE) OK TO WORK
- [SDR IPXA2024010935775](https://openairdocs.org/sdr/IPXA2024010935775), Jan 9, 2024: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** FAULT - CRACK - ANGLE, BULK CARGO COMPARTMENT LEFT AREA STA 1578 LBL 60 INBOARD SIDE (REPLACE) OK TO WORK
- [SDR IPXA2024012322914](https://openairdocs.org/sdr/IPXA2024012322914), Jan 8, 2024: BEAM. CRACKED. FAULT - CRACK - BEAM, NO.2 NACELLE AFT LOWER FAIRING R/H UPPER UNDER THE 4TH LATCH FITTING AT NAC STA 373 (REPLACE). 1. REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-
- [SDR IPXA2024012322940](https://openairdocs.org/sdr/IPXA2024012322940), Jan 8, 2024: BEAM. CRACKED. FAULT - CRACK - BEAM, NO.2 NACELLE AFT LOWER FAIRING L/H UPPER UNDER THE 4TH LATCH FITTING AT NAC STA 373 (REPLACE). 1. REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-
- [SDR IPXA2024010822914](https://openairdocs.org/sdr/IPXA2024010822914), Jan 8, 2024: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** FAULT - CRACK - BEAM, NO.2 NACELLE AFT LOWER FAIRING R/H UPPER UNDER THE 4TH LATCH FITTING AT NAC STA 373 (REPLACE)
- [SDR IPXA2024010822940](https://openairdocs.org/sdr/IPXA2024010822940), Jan 8, 2024: UNKNOWN. UNKNOWN. CRACK - BEAM, NO.2 NACELLE AFT LOWER FAIRING L/H UPPER UNDER THE 4TH LATCH FITTING AT NAC STA 373 (REPLACE)
- [SDR IPXA2022110787881](https://openairdocs.org/sdr/IPXA2022110787881), Nov 6, 2022: LOCK. INOPERATIVE. INSPECTION TYPE:NACREW ENTRY DOOR SECURE LOCK STICKING.LUBED EXTERIOR APPR LATCH IN MECHANISM. DOOR OPERATES AS ADVERTISED.Ï¿½52-12-00-715-119
- [SDR IPXA2022082785667](https://openairdocs.org/sdr/IPXA2022082785667), Aug 27, 2022: NONE. NONE. INSPECTION TYPE:NA**ATB**AT APPROXIMIMATELY 3000FT, ON DEPARTURE "TAT PROBE" EICAS MESSAGE AND FAILURE.REPLACED TAT PROBE PER AMM 34-12-02-404-008, BUT SAME CON
- [SDR IPXA2022080985047](https://openairdocs.org/sdr/IPXA2022080985047), Aug 8, 2022: LIGHT. INOPERATIVE. INSPECTION TYPE:N/ADURING PDC FOUND EMG LIGHTS INOP.R/R EMG BATT PACK IAW AMM 33-51-07. OPS CHECK SAT.
- [SDR IPXA2022072584563](https://openairdocs.org/sdr/IPXA2022072584563), Jul 24, 2022: EICAS. FAULT MESSAGE. INSPECTION TYPE:ETOP** ETOPS FILED OPEN**GOT A "R PACK TEMP" EICAS MSG ON SHORT FINAL. RAN QRH AND INOP LIGHT EXTINGUISHED. DEFERRED R PACK TEMP CONTROL AUTO MO

All 146: https://openairdocs.org/aircraft/N326UP/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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