# N320UP: 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: 27747
- Year built: 1997
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 24, 1997
- Certificate issued: September 25, 2009
- Expires: May 31, 2028
- Mode S code: A37020
- 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=320UP
- Page: https://openairdocs.org/aircraft/N320UP

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/N320UP/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 N320UP.

## FAA accident and incident reports

None matched to N320UP.

## Service difficulty reports (185, 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 IPXA2026090120360](https://openairdocs.org/sdr/IPXA2026090120360), Aug 31, 2026: BATTERY PACK. NO TEST. DURING PDC, FOUND EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-07. OPS CHECK GOOD.
- [SDR IPXA2026062990060](https://openairdocs.org/sdr/IPXA2026062990060), Jun 27, 2026: INDICATOR. STUCK. EMERGENCY DECLARED, FLAP INDICATOR DISAGREE ,RAN QRH CHECKLIST.RT TE PLAP INDICATOR EVENTUALLY UNSTUCK REMOVED AND REPLACED FLAP INDICATOR AS PER AMM 27-58-02, 
- [SDR IPXA2026050519564](https://openairdocs.org/sdr/IPXA2026050519564), Apr 22, 2026: COLLAR. CRACKED. CRACKED COLLAR, NR 2 PYLON AFT LWR FAIRING AFT FRAME OTBD SIDE FWD SURFACE. INSTALLED NEW COLLAR IAW SRM 51-40-02-0G, REV 95, & DWG 313T3380, SH 3, REV F.
- [SDR IPXA2026050519511](https://openairdocs.org/sdr/IPXA2026050519511), Apr 22, 2026: COLLAR. CRACKED. CRACKED COLLAR , NR 1 PYLON AFT FAIRING AFT BULKHEAD FWD CHANNEL INBD SIDE TOTAL 2 EA. INSTALLED NEW COLLAR IAW SRM 51-40-02-0G, REV 95, & DWG 313T3380, SH 3, R
- [SDR IPXA2026043020504](https://openairdocs.org/sdr/IPXA2026043020504), Apr 22, 2026: BRACKET. BROKEN. FOUND RT WING NR 12 SLAT OTBD SIDE MAIN TRACK SKEW DETECTION BRACKET BROKEN. REPLACED IAW AMM 27-81-34-404-014, REV 147, INSTALLED RT WING NR 12 SLAT OTBD SIDE 
- [SDR IPXA2026050222041](https://openairdocs.org/sdr/IPXA2026050222041), Apr 22, 2026: RING. CRACKED. FOUND ENG-1 RT THRUST REVERSER CASCADE SUPPORT RING CRACK AT 9 O'CLOCK. REFERENCED TASK T3F18E008RMGN INSTALLED THE T/R, FAN COWL AND ACCOMPLISHED THE INSTALLAT
- [SDR IPXA2026050119808](https://openairdocs.org/sdr/IPXA2026050119808), Apr 22, 2026: ANGLE. CRACKED. FAULT - CRACK - ANGLE, NO.2 ENG L/H T/R DRAIN TUBE SUPPORT BRACKET. (REPLACE) INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND ST ENGINEERING IPC 78-32-51 R
- [SDR IPXA2026050119881](https://openairdocs.org/sdr/IPXA2026050119881), Apr 22, 2026: PAN. BROKEN. BROKEN - PAN - SEAL, R/H WING SLAT NO.7 OUTBD SIDE. IAW PL 114T3200 REV. W DWG 114T3200 SHEET 3 REV. A & AMM 20-11-00-910-802 REV. 147 TO INSTALL THE SEAL PAN P
- [SDR IPXA2026042619384](https://openairdocs.org/sdr/IPXA2026042619384), Apr 22, 2026: CHANNEL. CHAFED. CHAFING - CHANNEL , NO. 1 ENG L/H T/R AFT LWR FAIRING L/E AREA (REPLACE) INSTALL NEW CHANNEL I.A.W SRM 51-40-02-0G REV.95 AND ST ENGINEERING IPC 78-32-01 REV.96
- [SDR IPXA2026050119905](https://openairdocs.org/sdr/IPXA2026050119905), Apr 22, 2026: CLAMP. BROKEN. BROKEN - CLAMP, CREW ENTRY DOOR UPPER CUTOUT AREA. (REPLACE) I.A.W SWPM 20-10-12 REV.91 REPLACED CLAMP AT CREW ENTRY UPPER CUTOUT AREA AND CONDITION CHECK NORMA
- [SDR IPXA2026042819227](https://openairdocs.org/sdr/IPXA2026042819227), Apr 22, 2026: SEAL. BROKEN. BROKEN SEAL, NR 1 PYLON FAIRING PANEL NR 436 CR SPRING SEAL BROKEN. INSTALLED A NEW SEAL STRIP IAW SRM 51-40-02-0G, REV 95, AND DWG 311T2570, SHT 14, REV -.
- [SDR IPXA2026042619261](https://openairdocs.org/sdr/IPXA2026042619261), Apr 22, 2026: RUB STRIP. CHAFED. CHAFED STRIP, NR 1 ENG RT CORE COWL INNER AFT UPPER STRIP CHAFING. INSTALLED A NEW WEAR STRIP IAW SRM 51-40-02-0G, REV.95, AND CMM IPL 71-13-24 REV. 50
- [SDR IPXA2026042619281](https://openairdocs.org/sdr/IPXA2026042619281), Apr 22, 2026: DOOR. CHAFED. CHAFED EDGE, NR 2 ENG RT T/R BLOW OUT DOOR L/E AREA. INSTALL WITH DOOR ASSY IAW SRM 51-40-02-0G, REV 95, AND AIPC 78-31-51-03, REV 141 AND IPC 78-32-22 REV.96 A
- [SDR IPXA2026042619249](https://openairdocs.org/sdr/IPXA2026042619249), Apr 22, 2026: DOOR. CHAFED. CHAFED DOOR , NR 1 ENG RT T/R LWR BLOW OUT DOOR L/E AREA. INSTALL WITH DOOR ASSY I.A.W SRM 51-40-02-0G REV.95 AND BOEING AIPC 78-31-51-03 REV. 141 AND ST ENGINE
- [SDR IPXA2026042619321](https://openairdocs.org/sdr/IPXA2026042619321), Apr 22, 2026: ADAPTER. CHAFED. CHAFED BRACKET, NR 1 ENG RT CORE COWL HOLD OPEN ROD SUPPORT BRACKET. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND GOODRICH AEROSTRUCTURES CMM IPL 71-13-
- [SDR IPXA2026042619349](https://openairdocs.org/sdr/IPXA2026042619349), Apr 22, 2026: BRACKET. CHAFED. CHAFED BRACKET , NR 1 ENG LT CORE COWL HOLD OPEN ROD SUPPORT BRACKET. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND GOODRICH AEROSTRUCTURES CMM IPL 71-13
- [SDR IPXA2026042821802](https://openairdocs.org/sdr/IPXA2026042821802), Apr 22, 2026: SCUFF PLATE. DENTED. DENTED SCUFF PLATE, LOWER SIDE OF BULK CARGO DOOR CUTOUT. IAW AMM 53-13-02-404-007, REV 147, TO INSTALL BULK CARGO DOOR SCUFF PLATE CENTER.
- [SDR IPXA2026042618157](https://openairdocs.org/sdr/IPXA2026042618157), Apr 22, 2026: SEAL. BROKEN. BROKEN SEAL, NR 1 ENG LT TRANSLATING COWL AFT LWR FAIRING INNER AREA. INSTALLED A NEW SEAL IAW SRM 51-40-02-0G, REV 95, AND IPC 78-32-31, REV 96.
- [SDR IPXA2026042619433](https://openairdocs.org/sdr/IPXA2026042619433), Apr 22, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 2 ENG, RT T/R CLOSURE DOOR T/E AREA. INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND IPC 78-32-22 REV.96
- [SDR IPXA2026042619452](https://openairdocs.org/sdr/IPXA2026042619452), Apr 22, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 1 ENG LT T/R LWR CLOSURE DOOR T/E AREA. INSTALL NEW BRACKET IAW SRM 51-40-02-0G REV.95 AND IPC 78-32-21 REV.96
- [SDR IPXA2026042621792](https://openairdocs.org/sdr/IPXA2026042621792), Apr 22, 2026: SEAL. FRAYED. FRAYED SEAL, NR 1 ENG LT TRANSLATING COWL AFT LWR FAIRING INNER AREA. REMOVED DAMAGE SEAL IAW SRM 51-40-02-0G, REV 95,
- [SDR IPXA2026042621981](https://openairdocs.org/sdr/IPXA2026042621981), Apr 22, 2026: LONGERON. CHAFED. CHAFED LONGERON, NR 1 ENG RT CORE COWL AFT LWR INNER CHORD EDGE AREA. INSTALLED A NEW LONGERON IAW SRM 51-40-02-0G REV.95 AND CMM IPL 71-13-24, REV 50.
- [SDR IPXA2026042320504](https://openairdocs.org/sdr/IPXA2026042320504), Apr 22, 2026: SLAT TRACK. DAMAGED. FOUND RT WING NO.12 SLAT OTBD SIDE MAIN TRACK SKEW DETECTION BRACKET BROKEN.
- [SDR IPXA2026042219905](https://openairdocs.org/sdr/IPXA2026042219905), Apr 22, 2026: CLAMP. BROKEN. BROKEN CLAMP, CREW ENTRY DOOR UPPER CUTOUT AREA.
- [SDR IPXA2026050202306](https://openairdocs.org/sdr/IPXA2026050202306), Apr 21, 2026: SPLICE PLATE. DEFORMED. LEFT WING AT LEADING EDGE SPAR AREA LWR PANEL ATTACH STRUCTURE AT NR 1 SLAT INBD DRIVE MOTOR LINK IS DEFORMED. REPAIR DAMAGE AREA IAW SRM 57-41-01-2R-4, REPAIR 
- [SDR IPXA2026050202373](https://openairdocs.org/sdr/IPXA2026050202373), Apr 21, 2026: SPLICE PLATE. DEFORMED. LEFT WING AT LEADING EDGE SPAR AREA LWR PANEL ATTACH STRUCTURE AT NR 2 SLAT OUTBD DRIVE MOTOR LINK IS DEFORMED. REPAIR DAMAGE AREA IAW SRM 57-41-01-2R-4, REPAIR
- [SDR IPXA2026050202651](https://openairdocs.org/sdr/IPXA2026050202651), Apr 21, 2026: FRAME. CHAFED. NR 1 PYLON AFT LEFT SIDE FRAME WAS CHAFED. REPAIR DAMAGE AREA IAW EO-97331-REQ1 REV 1 AND EI F2026A54M-937 REV. 0.
- [SDR IPXA2026043002803](https://openairdocs.org/sdr/IPXA2026043002803), Apr 21, 2026: ANGLE. BENT. FAULT - BENT ANGLE IN LOWER FORWARD CARGO COMPARTMENT CEILING AT STA 478-500, RBL 80 (NO.6623) (AGING AIRRCAFT INSPECTION) INSTALL NEW CLIP-ANGLE I.A.W SRM 51-4
- [SDR IPXA2026043002883](https://openairdocs.org/sdr/IPXA2026043002883), Apr 21, 2026: DEPRESSOR. BENT. FAULT - AFT LOWER CARGO DOOR SEAL DEPRESSOR BENT AT LOWER AFT CORNER (NO.6625) (AGING AIRCRAFT INSPECTION) INSTALL NEW DEPRESSOR SEAL I.A.W SRM 51-40-02-0G REV.
- [SDR IPXA2026043003364](https://openairdocs.org/sdr/IPXA2026043003364), Apr 21, 2026: DEPRESSOR. GOUGED. GOUGED DEPRESSOR SEAL AT MAIN DECK CGO DOOR CUTOUT AREA FWD SIDE STA 492 2EA (REPLACE) INSTALLED MAIN DECK CARGO DOOR DEPRESSOR SEAL AT FWD SIDE I.A.W AMM 20-10
- [SDR IPXA2026042700943](https://openairdocs.org/sdr/IPXA2026042700943), Apr 21, 2026: FAIRING. CRACKED. CRACKED FAIRING , INBD SIDE FWD EDGE OF LT WING NR 3 FLAP TRACK AFT FAIRING. IAW AMM 51-21-10-307-020, REV 147, REPAINTED AREA. I.A.W AMM 27-51-15-424-029 REV 1
- [SDR IPXA2026042601924](https://openairdocs.org/sdr/IPXA2026042601924), Apr 21, 2026: ANGLE. CRACKED. CRACKED ANGLE AT BULK CARGO, BS 1578, LBL 78, INBD. INSTALL NEW ANGLE I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 146T5650 SH 5 REV: C
- [SDR IPXA2026042601951](https://openairdocs.org/sdr/IPXA2026042601951), Apr 21, 2026: ANGLE. CRACKED. CRACKED ANGLE, BULK CARGO BS 1578, LBL 78 OTBD. REMOVED THE DAMAGED ANGLE IAW SRM 51-40-02-0G, REV 95. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 95, AND DW
- [SDR IPXA2026042803406](https://openairdocs.org/sdr/IPXA2026042803406), Apr 21, 2026: SEAL. BROKEN. BROKEN SEAL, NR 2 PYLON RT FAIRING PANEL 446CR. INSTALLED A NEW SEAL STRIP IAW SRM 51-40-02-0G, REV 95, & DWG 311T2570, SHT 14, REV -.
- [SDR IPXA2026042803562](https://openairdocs.org/sdr/IPXA2026042803562), Apr 21, 2026: ANGLE. CRACKED. CRACKED ANGLE, NR 1 PYLON AFT FAIRING AFT BULKHEAD INNER INBD. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 95, AND DWG 313T3380, SHT 3, REV F.
- [SDR IPXA2026042803602](https://openairdocs.org/sdr/IPXA2026042803602), Apr 21, 2026: ANGLE. CRACKED. CRACKED ANGLE, NR 2 PYLON AFT LWR FAIRING AFT FRAME OUTBD SIDE SUPPORT ANGLE. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 95, AND DWG 313T3380, SHT 3, REV F.
- [SDR IPXA2026042803621](https://openairdocs.org/sdr/IPXA2026042803621), Apr 21, 2026: SEAL. BROKEN. BROKEN SEAL, NR 2 PYLON LT FAIRING PANEL 446CL AREA. INSTALLED A NEW SEAL STRIP IAW SRM 51-40-02-0G, REV 95, & DWG 311T2570, SHT 14, REV -.
- [SDR IPXA2026042604547](https://openairdocs.org/sdr/IPXA2026042604547), Apr 21, 2026: ANGLE. CRACKED. CRACKED ANGLE, LT WING L/E REFUELINGS STATION LOWER DOOR CUTOUT INBD STOP SPRING, ACCESS PANEL NR 521QB. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 95, & DW
- [SDR IPXA2026042703429](https://openairdocs.org/sdr/IPXA2026042703429), Apr 21, 2026: FIRESHIELD. CHAFED. CHAFED FIRESHIELD, NR 1 PYLON FAIRING PANEL 436BL INNER PLATE. INSTALLED A NEW FIRESHIELD IAW SRM 51-40-02-0G, REV 95, AND DWG 311T2570, SH 14, REV -.
- [SDR IPXA2026042703484](https://openairdocs.org/sdr/IPXA2026042703484), Apr 21, 2026: FIRESHIELD. CHAFED. CHAFED FIRESHIELD, NR 2 PYLON LT FAIRING PANEL 446BL. INSTALLED A NEW FIRESHIELD IAW SRM 51-40-02-0G, REV 95, AND DWG 311T2570, SH 14, REV -.
- [SDR IPXA2026042703493](https://openairdocs.org/sdr/IPXA2026042703493), Apr 21, 2026: ANGLE. CRACKED. CRACK, NR 1 PYLON AFT FAIRING AFT BULKHEAD INNER OUTBD ANGLE CRACKED. INSTALLED A NEW CLIP IAW SRM 51-40-02-0G, REV 95, AND DWG 313T3380, SH 3, REV F.
- [SDR IPXA2026042604137](https://openairdocs.org/sdr/IPXA2026042604137), Apr 21, 2026: BRACKET. CRACKED. CRACKED BRACKET, NR 2 PYLON AFT LWR FAIRING INBD SIDE DRAIN TUBE SUPPORT BRACKET. INSTALL NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND DWG 272T0333, SH 8, REV A
- [SDR IPXA2026042604261](https://openairdocs.org/sdr/IPXA2026042604261), Apr 21, 2026: GUARD. CHAFED. CHAFED QUARD, MEC DOOR CUTOUT RT AREA. INSTALLED A NEW GUARD IAW SRM 51-40-02-0G, REV 95, AND DWG 141T6300, SH 1, REV J.
- [SDR IPXA2026050282674](https://openairdocs.org/sdr/IPXA2026050282674), Apr 20, 2026: SKIN PANEL. CORRODED. MAJOR REPAIR, CORROSION-FUSELAGE SKIN IMMEDIATELY SURROUNDING THE DRAIN VALVE AT STA 1410 BETWEEN S-38R AND S-39R. (REPAIR) INSTALLED BULK CARGO FLOOR PANEL IAW
- [SDR IPXA2026042185805](https://openairdocs.org/sdr/IPXA2026042185805), Apr 20, 2026: SKIN. DEBONDED. DEBONDED SKIN, INBD EDGE LOWER FACE OF LT WING T/E, OTBD FLAP LOWER SKIN, WBL 355. IAW CMM 57-53-51, REV 38, AND AMM 20-11-00-910-802 REV 147 INSTALLED THE OTBD
- [SDR IPXA2026042974070](https://openairdocs.org/sdr/IPXA2026042974070), Apr 19, 2026: PCA. LEAKING. FAULT- FOUND THE LOWER RUDDER PCA LEAK. (REPLACE) AMM 27-21-02-422-038 REV 147 STEP 5A TO 5H INSTALL LOWER RUDDER PCA
- [SDR IPXA2026042673479](https://openairdocs.org/sdr/IPXA2026042673479), Apr 19, 2026: SUPPORT BRACKET. CRACKED. FAULT- CRACK- TORQUE TUBE SUPPORT BRACKET, RH WING INBD LE COMPARTMENT. INSTALL NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND DWG 114T1240, SH 4, REV D.
- [SDR IPXA2026050262860](https://openairdocs.org/sdr/IPXA2026050262860), Apr 18, 2026: HINGE FITTING. CRACKED. CRACKED FITTING, RT WING NR 10 SPOILER SUPPORT FITTING WS 638. REPLACED IAW AMM 27-61-01-424-019, REV 147, STEP 3A, TO 3H (11) INSTALLED NR 10 SPOILER.
- [SDR IPXA2026043063775](https://openairdocs.org/sdr/IPXA2026043063775), Apr 18, 2026: SKIN. CRACKED. DURING PERFORM J/C : MXP-57-117-00-1-JIC, FOUND LEFT WING LOWER SKIN NEAR RIB 32, WSTA 1018.2 SKIN CRACKED. ACCOMPLISHED JOB I.A.W UPS EO-97334-REQ1 REV1 2.
- [SDR IPXA2026042160589](https://openairdocs.org/sdr/IPXA2026042160589), Apr 18, 2026: ROLLER. WORN. FAULT - FOUND MAIN DECK CARGO HANDLING SHAFT OF ROLLER RAIL ASSY WORN TOTAL: 2EA AT STA 456 ~ STA 500 LBL 77.50, LBL 55.50. I.A.W AMM 25-57-05-004-001 AND AMM 2

All 185: https://openairdocs.org/aircraft/N320UP/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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