# N305UP: 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: 27243
- Year built: 1995
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 11, 1995
- Certificate issued: December 12, 1995
- Expires: February 28, 2029
- Mode S code: A333B5
- 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=305UP
- Page: https://openairdocs.org/aircraft/N305UP

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/N305UP/ads.md

## Information bulletins (advisory) (5 in force)

- [SAIB 2023-15](https://openairdocs.org/saib/2023-15): Falsified Forms from AOG Technics. Issued Dec 19, 2023
- [SAIB NE-11-27](https://openairdocs.org/saib/NE-11-27): Fuel Injector Nozzle - CF6-80 Improperly Welded Fuel Nozzles. Issued Apr 5, 2011
- [SAIB NE-10-37](https://openairdocs.org/saib/NE-10-37): Engine Fuel and Control: FADEC Fuel Metering Valve Resolver Feedback Faults. Issued Jul 12, 2010
- [SAIB NE-08-44](https://openairdocs.org/saib/NE-08-44): Engine Thrust Reverser  Transcowl Clevis Pin. Issued Sep 3, 2008
- [SAIB NE-07-01](https://openairdocs.org/saib/NE-07-01): Dual engine flameouts on twin engine airplanes. Issued Oct 12, 2006

## NTSB investigations (1)

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

- [NTSB DCA16CA113](https://openairdocs.org/ntsb/DCA16CA113), Mar 5, 2016: Boeing 767 34AF (N305UP), Albuquerque, NM, substantial damage. Probable cause: the pilot flying's failure to maintain airspeed and correct pitch attitude. Contributing to the accident was the pilot's failure to maintain appropriate thrust after disconnecting the autothrottles.…

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20160305002309A](https://openairdocs.org/incident/20160305002309A), Mar 5, 2016: Boeing 767-34AF (N305UP), Albuquerque, NM, Substantial damage. Approach to abq was normal. Winds at the time of approach were reported to be 09019G26. Approach was made to runway 3. The pilot disconnected the autothrottles…

## Service difficulty reports (216, 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 IPXA2026090398854](https://openairdocs.org/sdr/IPXA2026090398854), Aug 30, 2026: FITTING. CRACKED. FOUND MAIN DECK CARGO FLOOR FITTING CRACK DAMAGE AT BS 1109 BL 0. REMOVED DAMAGE FITTING IAW SRM 51-40-02-0G REV. 96. INSTALLED NEW FITTING IAW SRM 51-40-02-0G 
- [SDR IPXA2026090447613](https://openairdocs.org/sdr/IPXA2026090447613), Aug 27, 2026: NOSE COWL. DENTED. FAULT - DENT - SKIN , NO. 2 ENG NOSE COWL INLET AT 9 O'CLOCK POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUTOUT ( DIA : 0.2", 16" FROM L/E AND AT 9 O'CL
- [SDR IPXA2026090443491](https://openairdocs.org/sdr/IPXA2026090443491), Aug 27, 2026: NOSE COWL. DENTED. DENT - SKIN , NO.1 ENG NOSE COWL INNER BARREL NEAR 9:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUTOUT ( DIA : 0.3", 9" FROM AFT EDGE, AT 9 O'CLOCK ON TH
- [SDR IPXA2026090446102](https://openairdocs.org/sdr/IPXA2026090446102), Aug 27, 2026: STRAP. CORRODED. FOUND FORWARD CARGO CEILING STRUCTURE CORROSION AT STA 566 RIGHT SIDE. REMOVED DAMAGE STRAP I.A.W SRM 51-40-02-0G REV. 96. ACCOMPLISHED REPAIR I.A.W EO-98506-RE
- [SDR IPXA2026090346191](https://openairdocs.org/sdr/IPXA2026090346191), Aug 27, 2026: ANGLE. CRACKED. FAULT - FOUND THE FIRE DETECTION LOOP FASTENER ANGLE CRACK AT STA 1562 LBL 76 IN BULK CARGO COMPARTMENT. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G RE.96. INSTA
- [SDR IPXA2026090346129](https://openairdocs.org/sdr/IPXA2026090346129), Aug 27, 2026: FORMER. CRACKED. CRACKED FORMER , RT WING CAVITY FORMER OF THE CRACK AT OSS 648. REMOVED DAMAGE FORMER IAW SRM 51-40-02-0G REV. 96. INSTALLED NEW FORMER IAW SRM 51-40-02-0G, REV
- [SDR IPXA2026090428170](https://openairdocs.org/sdr/IPXA2026090428170), Aug 26, 2026: SUPPORT ANGLE. CRACKED. FOUND FWD CARGO DOORWAY CEILING SUPPORT CRACK AT BS 600. REMOVED DAMAGE SUPPORT ANGLE IAW SRM 51-40-02-0G, REV. 96. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-40-02
- [SDR IPXA2026090324513](https://openairdocs.org/sdr/IPXA2026090324513), Aug 26, 2026: BULKHEAD. CRACKED. CRACKED BULKHEAD, NR 1 PYLON AFT FAIRING PANEL 437DD, INNER AREA. REMOVED DAMAGE BULKHEAD IAW SRM 51-40-02-0G, REV. 96. INSTALLED NEW BULKHEAD IAW SRM 51-40-02-
- [SDR IPXA2026090324466](https://openairdocs.org/sdr/IPXA2026090324466), Aug 26, 2026: BRACKET. CRACKED. CRACKED BRACKET, NR 1 AFT FAIRING INNER DRAIN TUBE SUPPORT BRACKET. REPLACEED. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 96. INSTALLED A NEW BRACKET IAW S
- [SDR IPXA2026090126837](https://openairdocs.org/sdr/IPXA2026090126837), Aug 26, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 1 ENG RT CORE COWL INNER OPEN ROD STOW AREA. REMOVED THE DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 96. INSTALLED A NEW BRACKET IAW SRM 51-40-02
- [SDR IPXA2026090123388](https://openairdocs.org/sdr/IPXA2026090123388), Aug 26, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 2 ENG LT CORE COWL OPEN HOLE ROD BRACKET. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 96. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, RE
- [SDR IPXA2026090123395](https://openairdocs.org/sdr/IPXA2026090123395), Aug 26, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 2 ENG RT CORE COWL OPEN HOLD ROD BRACKET. REMOVED THE DAMAGED BRACKETS IAW SRM 51-40-02-0G, REV 96. INSTALLED A NEW BRACKET IAW SRM 51-40-02-
- [SDR IPXA2026082726958](https://openairdocs.org/sdr/IPXA2026082726958), Aug 26, 2026: DOUBLER. CRACKED. CRACKED DOUBLER, LT WING OTBD L/E CAVITY UPPER FIXED PANEL LOWER RIB LWR CHORD. REPAIRED AREA, NEAR OSS 531. ACCOMPLISH REPAIR ON DAMAGE AREA IAW SRM 57-41-09-2
- [SDR IPXA2026090407154](https://openairdocs.org/sdr/IPXA2026090407154), Aug 25, 2026: FLAP TRACK. ERODED. ERODED SKIN, LT WING NR 1 FLAP TRACK FWD FAIRING EXTERNAL SKIN. REMOVED THE DAMAGED MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200 F FOR 220
- [SDR IPXA2026090907726](https://openairdocs.org/sdr/IPXA2026090907726), Aug 25, 2026: PAWL. WORN. THE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. IAW AMM 52-11-26-004-001, REV 149 AND AMM 52-11-26-404-003, REV 149. REPLACED THE PAWL.
- [SDR IPXA2026090307096](https://openairdocs.org/sdr/IPXA2026090307096), Aug 25, 2026: FAIRING. DEBONDED. DISBOND - SKIN, L/H WING NO. 3 FLAP TRACK MID FAIRING INBD T/E SKIN. REMOVE THE DAMAGED MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 2
- [SDR IPXA2026090107073](https://openairdocs.org/sdr/IPXA2026090107073), Aug 25, 2026: SKIN. ERODED. EROSION SKIN, L/H WING NO. 2 SLAT OUTBD CLOSURE PANEL. REMOVED DAMAGE CLOSURE PANEL I.A.W SRM 51-40-02-0G REV.96. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED
- [SDR IPXA2026090107012](https://openairdocs.org/sdr/IPXA2026090107012), Aug 25, 2026: SKIN. ERODED. EROSION SKIN, L/H WING NO. 2 SLAT INBD CLOSURE PANEL AREA. REMOVED DAMAGE CLOSURE PANEL I.A.W SRM 51-40-02-0G REV.96. MEASURE THE DAMAGE SIZE AND LOCATION ( L :
- [SDR IPXA2026082507726](https://openairdocs.org/sdr/IPXA2026082507726), Aug 25, 2026: PAWL. WORN. THE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. (REPLACE)
- [SDR IPXA2026090192196](https://openairdocs.org/sdr/IPXA2026090192196), Aug 24, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 1 ENGINE, LT THRUST REVERSER LOWER CLOSURE DOOR, T/E AREA. REMOVED THE DAMAGED BRACKET IAW SRM 51-40-02-0G, REV 96. INSTALLED A NEW BRACKET I
- [SDR IPXA2026090192222](https://openairdocs.org/sdr/IPXA2026090192222), Aug 24, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 1 ENG RT THRUST REVERSER LOWER CLOSURE DOOR, T/E AREA. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 96. INSTALLED A NEW BRACKET IAW SRM 51
- [SDR IPXA2025043003663](https://openairdocs.org/sdr/IPXA2025043003663), Apr 29, 2025: DOOR. BINDING. GEAR DISAGREE JACKED AIRCRAFT REF MM 07-11-01. RETRACTED GEAR SEVERAL TIMES REF MM 32-32-00. OBSERVED THAT WHEN GEAR WAS EXTENDING, THERE APPEARED TO BE BINDING
- [SDR IPXA2025042903663](https://openairdocs.org/sdr/IPXA2025042903663), Apr 29, 2025: WARNING MESSAGE. ILLUMINATED. *** SDR FILED OPEN *** GEAR DISAGREE
- [SDR IPXA2025042353243](https://openairdocs.org/sdr/IPXA2025042353243), Apr 20, 2025: SEQUENCE VALVE. FAULTED. AFTER TAKE OFF DURING GEAR RETRACTION RECEIVED €ŒGEAR DISAGREE AMD GEAR DOORS€? EICAS MESSAGES. FELT VIBRATION AS IF GEAR DOORS WERE EXTENDED. GEAR DID NOT FE
- [SDR IPXA2025042153243](https://openairdocs.org/sdr/IPXA2025042153243), Apr 20, 2025: LANDING GEAR. FAULTED. ATB, AFTER TAKE OFF DURING GEAR RETRACTION RECEIVED €ŒGEAR DISAGREE AMD GEAR DOORS€? EICAS MESSAGES. FELT VIBRATION AS IF GEAR DOORS WERE EXTENDED. GEAR DID N
- [SDR IPXA2025031312341](https://openairdocs.org/sdr/IPXA2025031312341), Mar 12, 2025: LOCK. INOPERATIVE. MAIN ENTRY DOOR SECONDARY LOCK WILL NOT CLOSE PERFORMED ADJ/TEST OF CREW ENTRY DOOR HANDLE AND SECONDARY LOCK REF MM 52-12-25/201. OPS CK NORMAL.
- [SDR IPXA2024112569925](https://openairdocs.org/sdr/IPXA2024112569925), Nov 24, 2024: HF COMM. MALFUNCTIONED. *AIR TURN BACK* TRANSMISSION FROM ANY CREW POSITION ON LHF NOT POSSIBLE. LH HF OPS NML REF AMM 23-11-00.
- [SDR IPXA2024080555098](https://openairdocs.org/sdr/IPXA2024080555098), Aug 2, 2024: FLOORBEAM. CRACKED. CRACKED FLOORBEAM MID CHORD CRACK AT STA 246 NEAR LBL 40 (REPAIR) ACCOMPLISHED REPAIR I.A.W UPS EO NO: EO-91052-REQ1 REV1.
- [SDR IPXA2024072218159](https://openairdocs.org/sdr/IPXA2024072218159), Jul 20, 2024: DRAIN. DISCOVERED. FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) ACCOMPLISHED SDR PER EO 82173-JIC001
- [SDR IPXA2024080596006](https://openairdocs.org/sdr/IPXA2024080596006), Jul 19, 2024: SUPPORT. CRACKED. **SUPPLEMENTAL SDR**FAULT - CRACK - BRACKET, R/H WING NO.7 SLAT LOWER DOOR. REMOVED DAMAGED PART IAW SRM 51-40-02 REV 89. PERFORMED CHROMIC ACID ANODIZE IAW EGA
- [SDR IPXA2024080170071](https://openairdocs.org/sdr/IPXA2024080170071), Jul 18, 2024: INTERCOSTAL. CORRODED. CORROSION - INTERCOSTAL, BULK CARGO COMPARTMENT FLOOR BEAM SUPPORT INTERCOSTAL AT STA 1602 LBL 40 - LBL 54" (EVALUATE) REVIEWED TASK PER GMM-MTX 09.05.01.09.PER
- [SDR IPXA2024080169998](https://openairdocs.org/sdr/IPXA2024080169998), Jul 18, 2024: FLOOR SUPPORT. CORRODED. BULK CARGO COMPARTMENT FLOOR SUPPORT INSTERCOSTAL AT STA 1602 RBL 10" ~ 15" (EVALUATE) CONDITION CHECK OK. REMOVED DAMAGED PART I.A.W. SRM 51-40-02-0G REV. 89. 
- [SDR IPXA2024080169950](https://openairdocs.org/sdr/IPXA2024080169950), Jul 18, 2024: FLOOR SUPPORT. CORRODED. BULK CARGO COMPARTMENT FLOOR SUPPORT AT 1602 RBL 54". REMOVED DAMAGED PART. FRABRICATED FLOOR SUPPORT IAW EGAT WORK SHEET NO. 40599 STEP 2.
- [SDR IPXA2024080169472](https://openairdocs.org/sdr/IPXA2024080169472), Jul 18, 2024: SUPPORT BRACKET. CORRODED. CORROSION, PANEL 149BL FWD SIDE SUPPORT BRACKET, ACCOMPLISHED REPAIR PER EO-90997-REQ1 AND EGAT EI F2024A53M-1830, REV. 0.
- [SDR IPXA2024080449680](https://openairdocs.org/sdr/IPXA2024080449680), Jul 17, 2024: SKIN. CORRODED. **SUPPLEMENTAL SDR**FAULT - CORROSION - SKIN, AFT CARGO COMPARTMENT LOWER LOBE SKIN AT STA 1197~STA 1197+22 S-35R TO S-36R.PERFORMED THE HEAT TREATMENT FROM 707
- [SDR IPXA2024080549718](https://openairdocs.org/sdr/IPXA2024080549718), Jul 17, 2024: SKIN. CORRODED. CORROSION - SKIN, AFT CARGO COMPARTMENT LOWER SKIN AT STA 1197+88~STA 1197+132 S-35R~S-36R.PERFORMED THE HEAT TREATMENT FROM 7075-O TO T62 CONDITION. I.A.W. EGA
- [SDR IPXA2024080549715](https://openairdocs.org/sdr/IPXA2024080549715), Jul 17, 2024: STRINGER. CORRODED. CORROSION - STRINGER, AFT CARGO COMPARTMENT LOWER SIDE SKIN AT STA 1197+66~STA 1197+88 S-34R. PERFORMED THE HEAT TREATMENT FROM 7075-O-080 CLAD TO T62 CONDITION
- [SDR IPXA2024080249680](https://openairdocs.org/sdr/IPXA2024080249680), Jul 17, 2024: SKIN. CORRODED. CORRODED SKIN, AFT CARGO COMPARTMENT LOWER LOBE SKIN AT STA 1197~STA 1197+22 S-35R TO S-36R. (REPAIR) I.A.W. EGAT EI NO.F2024A53M-1821 REV.2 SEQUENCE:C PAGE:1 O
- [SDR IPXA2024080246010](https://openairdocs.org/sdr/IPXA2024080246010), Jul 17, 2024: ANGLE. CRACKED. FOUND BULK CARGO COMPARTMENT LEFT AREA ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 89.INSTALLED NEW PART I.A.W SRM 5
- [SDR IPXA2024080245873](https://openairdocs.org/sdr/IPXA2024080245873), Jul 17, 2024: ANGLE. CRACKED. FOUND BULK CARGO COMPARTMENT RIGHT AREA ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD.REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 89, INSTALLED NEW PART I.A.W SRM 
- [SDR IPXA2024072945731](https://openairdocs.org/sdr/IPXA2024072945731), Jul 17, 2024: RIB. CRACKED. CRACKED RIB, L/H WING NO.3 SLAT OUTBD AUXILIARY TRACK FWD ARM AREA.REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 89. INSTALLED NEW PART I.A.W SRM 51-40-02-0G R
- [SDR IPXA2024080727695](https://openairdocs.org/sdr/IPXA2024080727695), Jul 16, 2024: MASTER CAUTION. INOPERATIVE. DFDR REPORT FAR #30 MASTER WARNING CAPT FAIL. (TROUBLESHOOTING/REPAIR) I.A.W AMM 33-13-00-902-045 REV 142 REPLACED MASTER WARNING SWITCH S507, AND CONDITION CHE
- [SDR IPXA2024071728963](https://openairdocs.org/sdr/IPXA2024071728963), Jul 16, 2024: FLOOR PANEL. DENTED. FOUND MAIN DECK CARGO FLOOR PANEL DENT, PANEL NO: 251FFF P/N: 146T5869-17.FLOOR PANEL SEALANT REMOVE AND OK TO INSTALL CHECK OK.FABRICATED A NEW FLOOR PANEL I.A
- [SDR IPXA2024071728884](https://openairdocs.org/sdr/IPXA2024071728884), Jul 16, 2024: FLOOR PANEL. DENTED. FOUND MAIN DECK CARGO FLOOR PANEL DENT, PANEL NO: 231LFF P/N: 143T5876-51.FLOOR PANEL SEALANT REMOVED AND OK TO INSTALL. FABRICATED A NEW FLOOR PANEL I.A.W. SRE
- [SDR IPXA2024071728900](https://openairdocs.org/sdr/IPXA2024071728900), Jul 16, 2024: FLOOR PANEL. DENTED. FOUND MAIN DECK CARGO FLOOR PANEL DENT, PANEL NO: 231CFF P/N: 143T5876-39.FLOOR PANEL SEALANT REMOVED AND OK TO INSTALL. FABRICATED A NEW FLOOR PANEL I.A.W. SRE
- [SDR IPXA2024071728851](https://openairdocs.org/sdr/IPXA2024071728851), Jul 16, 2024: FLOOR PANEL. DENTED. FOUND MAIN DECK CARGO FLOOR PANEL DENT, PANEL NO: 231DFF P/N: 143T5876-37.FLOOR PANEL SEALANT REMOVED AND OK TO INSTALL.FABRICATED A NEW FLOOR PANEL I.A.W. SREO
- [SDR IPXA2024071728936](https://openairdocs.org/sdr/IPXA2024071728936), Jul 16, 2024: FLOOR PANEL. DENTED. FOUND MAIN DECK CARGO FLOOR PANEL DENT, PANEL NO: 231EFF P/N: 143T5876-63.FLOOR PANEL SEALANT REMOVED AND OK TO INSTALL. FABRICATED A NEW FLOOR PANEL I.A.W. SRE
- [SDR IPXA2024071627695](https://openairdocs.org/sdr/IPXA2024071627695), Jul 16, 2024: WARNING SYSTEM. FAILED. DFDR REPORT FAR #30 MASTER WARNING CAPT FAIL. (TROUBLESHOOTING/REPAIR) OK TO WORK.
- [SDR IPXA2023110763529](https://openairdocs.org/sdr/IPXA2023110763529), Nov 1, 2023: COVER. BROKEN. *** SUPPLEMENTAL SDR *** CREW DOOR CLEAR PLASTIC COVER FOR LEVER LATCH STUCK IN THE OPEN POSITION R&R CREW DOOR CLEAR PLASTIC COVER HINGE PER IPC 52-11-02-10A I
- [SDR IPXA2023110163529](https://openairdocs.org/sdr/IPXA2023110163529), Nov 1, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* CREW DOOR CLEAR PLASTIC COVER FOR LEVER LATCH STUCK IN THE OPEN POSITION DEFERRED AS PAR MEL 52-11-2 PLACARDS INSTALLED

All 216: https://openairdocs.org/aircraft/N305UP/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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