# N303UP: 1995 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: 27241
- Year built: 1995
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 6, 1995
- Certificate issued: January 28, 2026
- Expires: January 31, 2033
- Mode S code: A32C47
- 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=303UP
- Page: https://openairdocs.org/aircraft/N303UP

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/N303UP/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 N303UP.

## FAA accident and incident reports

None matched to N303UP.

## Service difficulty reports (190, 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 IPXA2026101325515](https://openairdocs.org/sdr/IPXA2026101325515), Oct 13, 2026: CONTROLLER. FAULTED. FO`S R2 WINDOW HEAT INOPERATIVE. REMOVED AND REPLACED LT FWD AND RT SIDE WINDOW HEAT CONTROLLER UNIT (M191) IAW AMM 30-41-01/401. BITE TEST PASSED IAW B767 AMM 
- [SDR IPXA2026092308451](https://openairdocs.org/sdr/IPXA2026092308451), Sep 18, 2026: SKIN. GROUND DAMAGE. MAJOR REPAIR, CAN BLEW OFF THE K LOADER DUE TO JET BLAST IS UNDER BELLY OF AIRCRAFT LT SIDE STATION 698-720 STRINGER S39-S36 FABRICATED FREEZE PLUG PER STEP 10 
- [SDR IPXA2026032629120](https://openairdocs.org/sdr/IPXA2026032629120), Mar 18, 2026: BRACKET. BROKEN. BROKEN BRACKET, LT WING NR 5 SLAT OTBD SIDE SEAL DOOR AREA. IAW AMM 57-41-50-004-001, REV 147, REPLACED THE BRACKET.
- [SDR IPXA2026032032584](https://openairdocs.org/sdr/IPXA2026032032584), Mar 18, 2026: FLOOR SUPPORT. CRACKED. CRACKED FLOOR SUPPORT, MAIN DECK CARGO, BS 1043, RBL 9. ACCOMPLISHED THE REPAIR IAW EO-96900-REQ1, REV 1, & EGAT EI F2026A53M-563, REV 2.
- [SDR IPXA2026032611084](https://openairdocs.org/sdr/IPXA2026032611084), Mar 17, 2026: PAN. BROKEN. BROKEN- PAN, R/H WING L/E NO.7 SLAT OUTBD. (REPLACE). INSTALL PART I.A.W SRM 51-40-02-0G REV.94 AND BOEING DWG NO: 114T3200 SH 3 REV: A. I.A.W PL 114T3200 REV. 
- [SDR IPXA2026032793526](https://openairdocs.org/sdr/IPXA2026032793526), Mar 16, 2026: STRAP. CORRODED. FOUND FORWARD CARGO SIDEWALL , CEILING PANEL SUPPORT STRAP ASSY TOTAL : 3 AREA AT BS 674, BS 654+66, BS 632 - 654 LT. CHECK OK. ACCOMPLISHED THE REPAIR IAW EO-9
- [SDR IPXA2026032693515](https://openairdocs.org/sdr/IPXA2026032693515), Mar 16, 2026: SEAL DEPRESSOR. CRACKED. CRACKED SEAL DEPRESSOR, FWD CARGO DOOR CUTOUT AFT EDGE. REMOVED DAMAGED DEPRESSOR IAW SRM 51-40-02-0G, REV 94. INSTALLED A NEW DEPRESSOR IAW SRM 51-40-02-0G, RE
- [SDR IPXA2026032693506](https://openairdocs.org/sdr/IPXA2026032693506), Mar 16, 2026: STRUT. CRACKED. CRACKED STRUT, LT WING OTBD L/E CAVITY, INNER RIB LWR STRUT, NEAR OSS 531, ACCESS PANEL 521HB. INSTALL NEW STRUT IAW SRM 51-40-02-0G, REV.94, DWG 114T2206, SH 1
- [SDR IPXA2026032491333](https://openairdocs.org/sdr/IPXA2026032491333), Mar 16, 2026: SEAT TRACK. WORN. FOUND CAPTAIN SEAT TRACK ASSY WORN AT: INBOARD AFT. IAW AMM 25-11-01-822-095-001, REV 147. REPLACED THE SEAT TRACK IAW AMM 25-11-01-822-095-001 REV 147. JOB COM
- [SDR IPXA2026032492359](https://openairdocs.org/sdr/IPXA2026032492359), Mar 16, 2026: SEAT TRACK. WORN. FOUND CAPTAIN SEAT TRACK ASSY WORN AT: INBOARD FOWARD. IAW AMM 25-11-01-822-095-001, REV.147 REPLACED THE SEAT TRACK. JOB COMPLETED AND CONDITION CHECK NORMAL S
- [SDR IPXA2026032490512](https://openairdocs.org/sdr/IPXA2026032490512), Mar 16, 2026: DRAIN VALVE. BROKEN. FOUND DRAIN VALVE ASSEMBLY BROKEN DURING PERFORM TASK CARD EO-89877-REQ1. REPLACED THE DRAIN VALVE ASSEMBLY IAW AMM 51-41-01-004-001 REV 147 AND AMM 51-41-01-40
- [SDR IPXA2026032091965](https://openairdocs.org/sdr/IPXA2026032091965), Mar 16, 2026: BRACKET. WORN. ENLARGED HOLE , NR 1 ENG RT THRUST REVERSER, FWD LWR CLOSURE DOOR T/E AREA. . INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND IPC 78-32-22 REV.94.
- [SDR IPXA2026032593477](https://openairdocs.org/sdr/IPXA2026032593477), Mar 16, 2026: CHANNEL. CRACKED. CRACKED CHANNEL , NR 1 PYLON INBD AFT FAIRING PNL NR 437DB INNER FWD CHORD. INSTALLED NEW CHANNEL IAW SRM 51-40-02-0G, REV 94, AND DWG 313T3380, SHT 5, REV H, &
- [SDR IPXA2026032593408](https://openairdocs.org/sdr/IPXA2026032593408), Mar 16, 2026: CHANNEL. CRACKED. CRACK - CHANNEL , NO. 2 PYLON AFT FAIRING PNL 447DB INNER. INSTALLED A NEW CHANNEL IAW SRM 51-40-02-0G, REV 94, & DWG 313T3360, SHEET 15, REV B.
- [SDR IPXA2026032590344](https://openairdocs.org/sdr/IPXA2026032590344), Mar 16, 2026: ANGLE. CRACKED. CRACKED ANGLE, NR 1 PYLON AFT FAIRING PANEL 437DB, INNER UPPER SUPPORT BEAM AREA. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 94, & DWG 313T3360, SH 15, REV 
- [SDR IPXA2026032392386](https://openairdocs.org/sdr/IPXA2026032392386), Mar 16, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 2 ENG RT CORE COWL HOLD OPEN ROD STOW BRACKET. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G REV.94. 2.INSTALL NEW BRACKET IAW SRM 51-40-02-0G R
- [SDR IPXA2026032092119](https://openairdocs.org/sdr/IPXA2026032092119), Mar 16, 2026: BRACKET. CHAFED. CHAFED BRACKET , NR 1 ENG LT CORE COWL HOLD OPEN ROD SUPPORT BRACKET. INSTALL NEW BRACKET IAW SRM 51-40-02-0G REV.94. AND CMM IPL 71-13-23, REV. 47.
- [SDR IPXA2026032092047](https://openairdocs.org/sdr/IPXA2026032092047), Mar 16, 2026: ADAPTER. CHAFED. CRACKED BRACKET , NR 2 ENGINE LT CORE COWL HOLD OPEN ROD STOW ADAPTER. INSTALL A NEW BRACKET I.A.W SRM 51-40-02-0G REV.94 AND CMM IPL 71-13-23 REV 47.
- [SDR IPXA2026032091871](https://openairdocs.org/sdr/IPXA2026032091871), Mar 16, 2026: BLOWOUT DOOR. CHAFED. CHAFED SKIN , NR 1 ENG RT THRUST REVERSER LWR BLOWOUT DOOR L/E AREA. (REPLACE). INSTALL NEW BLOWOUT DOOR IAW SRM 51-40-02-0G REV.94 AND ST ENGINEERING IPC 78-32
- [SDR IPXA2026032091850](https://openairdocs.org/sdr/IPXA2026032091850), Mar 16, 2026: BLOWOUT DOOR. CHAFED. CHAFED SKIN , NR 2 ENG RT THRUST REVERSER BLOWOUT DOOR L/E. (REPLACE). INSTALL NEW BLOWOUT DOOR I.A.W SRM 51-40-02-0G REV.94 AND BOEING AIPC 78-31-51-03 REV.141
- [SDR IPXA2026032391455](https://openairdocs.org/sdr/IPXA2026032391455), Mar 16, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR.1 ENG R/H CORE COWL HOLD OPEN ROD SUPPORT BRACKET. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 94. INSTALLED A NEW BRACKET IAW SRM 51-40-
- [SDR IPXA2026032393518](https://openairdocs.org/sdr/IPXA2026032393518), Mar 16, 2026: RIB. CRACKED. CRACKED LT WING OUTBD L/E CAVITY INNER RIB , NEAR OSS 549 , ACCESS PANEL 521HB. INSTALLED A NEW RIB IAW SRM 51-40-02-0G, REV 94, & DWG 114T2207, SH 1, REV B.
- [SDR IPXA2026032393496](https://openairdocs.org/sdr/IPXA2026032393496), Mar 16, 2026: RIB. CRACKED. CRACKED RIB , LT WING OTBD L/E CAVITY INNER RIB , NEAR OSS 514 , ACCESS PANEL 521HB. INSTALL NEW RIB IAW SRM 51-40-02-0G, REV 94, AND DWG 114T2205, SH 1, REV B.
- [SDR IPXA2026032391466](https://openairdocs.org/sdr/IPXA2026032391466), Mar 16, 2026: FAIRING. DEBONDED. DISBOND, FUSELAGE RT SIDE AFT WING TO BODY PANEL 198CR EXTERNAL SURFACE. PERFORMED NDT/UT FOR REWORKED AREA PLUS 6'' AROUND HEATED AREA I.A.W 767 NTM PART1 51-0
- [SDR IPXA2026032091829](https://openairdocs.org/sdr/IPXA2026032091829), Mar 16, 2026: ANGLE. CRACKED. CRACK - CLIP , NO. 2 PYLON AFT FAIRING PNL 447DB INNER SUPPORT CLIP L/H. REMOVED DAMAGE CLIP I.A.W SRM 51-40-02-0G REV.94. INSTALL NEW CLIP I.A.W SRM 51-40-02-0
- [SDR IPXA2026032091758](https://openairdocs.org/sdr/IPXA2026032091758), Mar 16, 2026: ANGLE. CRACKED. CRACKED ANGLE, NR 1 PYLON AFT FAIRING INNER CAVITY INBD SIDE. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G, REV 94. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 9
- [SDR IPXA2026032091887](https://openairdocs.org/sdr/IPXA2026032091887), Mar 16, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 1 ENG LT THRUST REVERSER FWD LWR CLOSURE DOOR T/E AREA. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G REV 94, AND IPC 78-32-21 REV 94.
- [SDR IPXA2026032091950](https://openairdocs.org/sdr/IPXA2026032091950), Mar 16, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 2 ENGINE RT THRUST REVERSER CLOSURE DOOR T/E AREA. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, & IPC 78-32-22, REV 94.
- [SDR IPXA2026032091954](https://openairdocs.org/sdr/IPXA2026032091954), Mar 16, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 2 ENG LT THRUST REVERSER CLOSURE DOOR T/E AREA. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G REV.94 AND ST ENGINEERING IPC 78-32-21 REV.94..
- [SDR IPXA2026032091714](https://openairdocs.org/sdr/IPXA2026032091714), Mar 16, 2026: CLAMP. CRACKED. CRACKED CLAMP, NR 2 PYLON AFT FAIRING DOOR HOLD OPEN SUPPORT ROD STOW CLAMP. REMOVED DAMAGE CLAMP I.A.W SRM 51-40-02-0G REV.94. INSTALLED A NEW CLAMP IAW SRM 51
- [SDR IPXA2026031991691](https://openairdocs.org/sdr/IPXA2026031991691), Mar 16, 2026: BRACKET. CRACKED. RIGHT WING L/E PNL NR 611KB TORQUE TUBE SUPPORT. (REPLACE). INSTALL NEW BRACKET IAW SRM 51-40-02-0G REV.94 AND DWG 114T1240, SH 2, REV E.
- [SDR IPXA2026031690471](https://openairdocs.org/sdr/IPXA2026031690471), Mar 16, 2026: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE. IAW SREO-9693-REQ001, REV 4, FABRICATE A NEW FLOOR PANEL.
- [SDR IPXA2026032783724](https://openairdocs.org/sdr/IPXA2026032783724), Mar 15, 2026: FAIRING. CRACKED. CRACKED FAIRING, NR 2 ENG LT TRANSCOWL INNER LWR AREA. INSTALLED A NEW FAIRING IAW SRM 51-40-02-0G, REV 94, & IPC 78-32-31, REV 94.
- [SDR IPXA2026032069539](https://openairdocs.org/sdr/IPXA2026032069539), Mar 14, 2026: ANGLE. CRACKED. FOUND CRACKED ANGLE, BULK CARGO BAY CEILING AREA, BS 1577, LBL 74, INBD SIDE. REMOVED THE DAMAGE ANGLE IAW SRM 51-40-02-0G, REV.94. INSTALLED A NEW ANGLE IAW SR
- [SDR IPXA2026032069514](https://openairdocs.org/sdr/IPXA2026032069514), Mar 14, 2026: ANGLE. CRACKED. FOUND A CRACKED ANGLE, BULK CARGO BAY CEILING AREA, BS 1577, LBL 74, OTBD SIDE. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 94, & DWG 146T5650, SH 5, REV C.
- [SDR IPXA2026031769683](https://openairdocs.org/sdr/IPXA2026031769683), Mar 14, 2026: FLOOR PANEL. DAMAGED. FOUND AFT CARGO FLOOR PANEL DAMAGE , P/N : 453T1996-17. (REPAIR). IAW SRM 53-00-50-2R-0 REV. 94, PERFORM REPAIR AS BELOW STEP: 1.1 CUT OUT THE DAMAGE AND CLEAN.
- [SDR IPXA2026032637236](https://openairdocs.org/sdr/IPXA2026032637236), Mar 12, 2026: SKIN. CRACKED. FOUND CRACK ON THE NR 1 FWD ENTRY DOOR AFT LWR CORNER SKIN. ACCOMPLISHED THE REPAIR IAW EO-87307-REQ7, REV 2 & EGAT WORK SHEET 60151.
- [SDR IPXA2026032038208](https://openairdocs.org/sdr/IPXA2026032038208), Mar 12, 2026: RIB. CRACKED. CRACKED FITTING, RT WING T/E NR 10 SPOILER INBD LWR. INSTALLED A NEW FITTING IAW SRM 51-40-02-0G, REV 94, & DWG 112T1001, SH 45, REV -, 113T1653, SH 1, REV I, 1
- [SDR IPXA2025012071786](https://openairdocs.org/sdr/IPXA2025012071786), Sep 30, 2024: FLOOR PANEL. BROKEN. FOUND STRUCTURE AND FLOOR PANEL COMMON TO CENTER GUIDE #262 TO BE BROKEN. INSTALLED LOCK 262 FLOOR FITTING IAW AMM 53-01-06-400-801. ALL REPAIRS FOR THIS DEFERR
- [SDR IPXA2024032349527](https://openairdocs.org/sdr/IPXA2024032349527), Mar 14, 2024: SKIN. CORRODED. *SUPPLEMENTAL SDR* *MAJOR REPAIR* FAULT - CORROSION, BULK CGO RIGHT HAND INTERIOR LOWER FUSELAGE SKIN, NEAR STA 1404, S-33R (EVALUATE) ACCOMPILISHED EO-89882-RE
- [SDR IPXA2024032249527](https://openairdocs.org/sdr/IPXA2024032249527), Mar 14, 2024: SKIN. CORRODED. *SDR FILED OPEN* *MAJOR REPAIR* FAULT - CORROSION, BULK CGO RIGHT HAND INTERIOR LOWER FUSELAGE SKIN, NEAR STA 1404, S-33R (EVALUATE) ACCOMPLISH REPAIR PER EO-89
- [SDR IPXA2024032326496](https://openairdocs.org/sdr/IPXA2024032326496), Mar 13, 2024: PLATE. CRACKED. *** SUPPLEMENTAL SDR *** FAULT - FOUND BULK CARGO PLATE CRACK AT CEILING AREA STA 1602 LBL 66 (REPLACE) INSTALLED NEW PARTS I.A.W SRM 51-40-02-0G REV.88 AND BOE
- [SDR IPXA2024032226466](https://openairdocs.org/sdr/IPXA2024032226466), Mar 13, 2024: FILLER. CORRODED. FOUND BULK CARGO PLATE CRACK AT CEILING AREA STA 1602 RBL 66 (REPLACE) I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.141 INSTALLED MAIN DECK CARGO HAN
- [SDR IPXA2024032526906](https://openairdocs.org/sdr/IPXA2024032526906), Mar 13, 2024: ROLLER TRAY. CORRODED. FAULT - FOUND AFT CARGO ROLLER TRAY DAMAGE AT STA 1197+22 RBL 42 (REPLACE) ACCOMPLISHED REPAIR I.A.W UPS EO-89883-REQ1 REV.1 AND EGAT EI NO.F2024A53M-755 REV.0 
- [SDR IPXA2024031926466](https://openairdocs.org/sdr/IPXA2024031926466), Mar 13, 2024: PLATE. CORRODED. FOUND BULK CARGO PLATE CRACK AT CEILING AREA STA 1602 RBL 66 (REPLACE) PERFORMED THE HEAT TREATMENT FROM 2024-O-071 BARE TO T42 CONDITION. I.A.W. W/S NO.:40273 
- [SDR IPXA2024031926496](https://openairdocs.org/sdr/IPXA2024031926496), Mar 13, 2024: CHANNEL. CORRODED. FAULT - FOUND BULK CARGO PLATE CRACK AT CEILING AREA STA 1602 LBL 66 (REPLACE) PERFORMED THE CHROMIC ACID ANODIZE I.A.W. EGAT WORK SHEET NO:40274 STEP 7 AND SPW
- [SDR IPXA2024032583543](https://openairdocs.org/sdr/IPXA2024032583543), Mar 10, 2024: DRAIN. DAMAGED. (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. ACCOMPLISHED SDR
- [SDR IPXA2024031183543](https://openairdocs.org/sdr/IPXA2024031183543), Mar 10, 2024: NONE. NONE. **SDR FILED OPEN** FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R.
- [SDR IPXA2023041292851](https://openairdocs.org/sdr/IPXA2023041292851), Apr 12, 2023: LIGHT. INOPERATIVE. INSPECTION TYPE:N/AEMERGENCY LIGHT UNARMED KERRY SWTICH WILL NOT STAY SEATEDREMOVED AND REPLACEED EMERGENCY LIGHTS CONTROL PANEL AIW AMM 33 51 08 404 010. OPS C
- [SDR IPXA2022100586866](https://openairdocs.org/sdr/IPXA2022100586866), Oct 5, 2022: UNKNOWN. ODOR. STRONG "FISH" ODOR IN COCKPIT. SEEM TO EMINATE FROM CARGO AREA. CLEAN UP REQUIREDUPS FIRST RESPONDER MAURICO POSADA INSP OF A/C NO SPILLS NOTED . PER GMM 03.31.

All 190: https://openairdocs.org/aircraft/N303UP/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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