# N301UP: 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: 27239 - Year built: 1995 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 23, 1995 - Certificate issued: January 29, 2026 - Expires: January 31, 2033 - Mode S code: A324D9 - 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=301UP - Page: https://openairdocs.org/aircraft/N301UP 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/N301UP/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 N301UP. ## FAA accident and incident reports None matched to N301UP. ## Service difficulty reports (196, 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 IPXA2026051511092](https://openairdocs.org/sdr/IPXA2026051511092), May 10, 2026: BRACKET. CRACKED. CRACKED BRACKET, NR 1 PYLON AFT FAIRING INNER VENT TUBE SUPPORT BRACKET. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV. 95 AND DWG 272T0333 SH. 8 REV. -. - [SDR IPXA2026051412136](https://openairdocs.org/sdr/IPXA2026051412136), May 10, 2026: COVER. DAMAGED. FOUND RT WING NR 11 SLAT OTBD SIDE AND NR 12 SLAT BOTH SIDE ROTARY ACTUATOR END COVER DAMAGED. I.A.W AMM 27-81-20-422-077 REV.148 INSTALL RT WING NR 11 SLAT OTB - [SDR IPXA2026051311114](https://openairdocs.org/sdr/IPXA2026051311114), May 10, 2026: FAIRING. CRACKED. CRACKED SKIN, RT WING T/E NO.6 FLAP AFT FAIRING. PERFORMED NDT/UT FOR REWORKED AREA PLUS 6'' AROUND HEATED AREA IAW NTM PART1 51-01-01 REV:143. NO DEFECT FOUND. - [SDR IPXA2026051311262](https://openairdocs.org/sdr/IPXA2026051311262), May 10, 2026: BRACKET. CRACKED. CRACK-BRACKET, NR 2 PYLON AFT FAIRING INBD INNER VENT TUBE NO.3 BRACKET CRACK. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV. 95. INSTALLED NEW BRACKET I.A.W - [SDR IPXA2026051312172](https://openairdocs.org/sdr/IPXA2026051312172), May 10, 2026: SEAL. BROKEN. BROKEN-SEAL STRIP, NO.2 PYLON FAIRING PNL NO.446CL SPRING SEAL. REMOVED DAMAGE SEAL STRIP I.A.W SRM 51-40-02-0G REV. 95. INSTALLED NEW SEAL STRIP I.A.W SRM 51-4 - [SDR IPXA2026051111053](https://openairdocs.org/sdr/IPXA2026051111053), May 10, 2026: FLOOR PANEL. CRACKED. FOUND MAIN DECK FLOOR PANEL WITH EDGE CRACK DAMAGE, PANEL 252WFF. INSTALL THE REPLACEMENT FLOOR PANEL PER AMM 53-01-06. - [SDR IPXA2026051111049](https://openairdocs.org/sdr/IPXA2026051111049), May 10, 2026: FLOOR PANEL. CRACKED. FOUND MAIN DECK FLOOR PANEL WITH EDGE CRACK DAMAGE. PANEL .252YFF. INSTALL THE REPLACEMENT FLOOR PANEL PER AMM 53-01-06. - [SDR IPXA2026051111011](https://openairdocs.org/sdr/IPXA2026051111011), May 10, 2026: FLOOR PANEL. CRACKED. FOUND MAIN DECK FLOOR PANEL WITH EDGE CRACK DAMAGE, PANEL 251ZFF. INSTALL THE REPLACEMENT FLOOR PANEL PER AMM 53-01-06. - [SDR IPXA2026051698681](https://openairdocs.org/sdr/IPXA2026051698681), May 9, 2026: FRAME. CHAFED. CHAFED FRAME, NR 2 ENG LT CORE COWL INNER NR 4 FRAME AREA. ACCOMPLISHED ZEE FRAME REPAIR I.A.W SRM 54-45-01-2R-3 REV. 95 AND EGAT WORK SHEET NO.60388. - [SDR IPXA2026051598444](https://openairdocs.org/sdr/IPXA2026051598444), May 9, 2026: SPLICE. CORRODED. CORROSION - SPLICE TEE, KEEL BEAM FWD SECTION LOWER ACCESS PANEL 139BL INTERNAL FWD SUPPORT. (REPLACE) Â INSTALLED NEW SPLICE TEE I.A.W SRM 51-40-02-0G REV. 95 - [SDR IPXA2026051397715](https://openairdocs.org/sdr/IPXA2026051397715), May 9, 2026: DOUBLER. CRACKED. CRACK - DOUBLER , RT WING L/E PNL 621HB RIB OSS 514. - [SDR IPXA2026051302042](https://openairdocs.org/sdr/IPXA2026051302042), May 9, 2026: BRACKET. WORN. WORN - BRACKET, NO.1 ENG R/H CORE COWL INNER HOLD OPEN ROD SUPPORT BRACKET. - [SDR IPXA2026051201811](https://openairdocs.org/sdr/IPXA2026051201811), May 9, 2026: SUPPORT BRACKET. CHAFED. CHAFED BRACKET, NR 2 ENGING RT CORE COWL HOLD OPEN ROD SUPPORT BRACKET. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV. 95. INSTALLED NEW BRACKET I.A.W SRM 51 - [SDR IPXA2026052076475](https://openairdocs.org/sdr/IPXA2026052076475), May 8, 2026: FLOOR SUPPORT. CORRODED. FOUND FLOOR INTERCOSTAL CORROSION AT STA 1598 RBL 62 IN THE AREA AFT OF BULK CARGO COMPARTMENT. INSTALLED FABRICATED INTERCOSTAL I.A.W SRM 51-40-02-0G REV. 95 A - [SDR IPXA2026052075956](https://openairdocs.org/sdr/IPXA2026052075956), May 8, 2026: FLOOR SUPPORT. CORRODED. FOUND FLOOR INTERCOSTAL CORROSION AT STA 1602 LBL 66 IN THE AREA AFT OF BULK CARGO COMPARTMENT. INSTALLED FABRICATED INTERCOSTAL I.A.W SRM 51-40-02-0G REV. 95 A - [SDR IPXA2026052076486](https://openairdocs.org/sdr/IPXA2026052076486), May 8, 2026: FLOOR SUPPORT. CORRODED. FOUND FLOOR INTERCOSTAL CORROSION AT STA 1598 FROM RBL 33 TO RBL 54.75 IN THE AREA AFT OF BULK CARGO COMPARTMENT. INSTALLED FABRICATED INTERCOSTAL I.A.W SRM 51- - [SDR IPXA2026051576502](https://openairdocs.org/sdr/IPXA2026051576502), May 8, 2026: SEAL DEPRESSOR. DENTED. FAULT-DENT-DEPRESSOR, MAIN DECK CARGO DOOR CUTOUT AFT UPPER SIDE (REPLACE) INSTALLED THE MAIN DECK CARGO DOOR DEPRESSOR SEAL I.A.W AMM 20-11-00-910-802 REV.148, - [SDR IPXA2026051580840](https://openairdocs.org/sdr/IPXA2026051580840), May 8, 2026: RIB. CRACKED. CRACKED LWR CHORD, R/H WING L/E PNL 621HB RIB OSS 531, INSTALLED NEW CHORD I.A.W SRM 51-40-02-0G REV. 95 AND DWG 114T2206 SH. 1 REV. E. - [SDR IPXA2026051576475](https://openairdocs.org/sdr/IPXA2026051576475), May 8, 2026: FLOOR SUPPORT. CORRODED. FOUND FLOOR INTERCOSTAL CORROSION AT STA 1598 RBL 62 IN THE AREA AFT OF BULK CARGO COMPARTMENT. FABRICATE P/N: 146T5649-8 I.A.W DWG 146T5649, SH 1, REV- AND ORI - [SDR IPXA2026051575956](https://openairdocs.org/sdr/IPXA2026051575956), May 8, 2026: FLOOR SUPPORT. CORRODED. FOUND FLOOR INTERCOSTAL CORROSION AT STA 1602 LBL 66 IN THE AREA AFT OF BULK CARGO COMPARTMENT. FABRICATE P/N: 146T5649-7 I.A.W BOEING DWG 146T5649 SH 1 REV.- , - [SDR IPXA2026051576486](https://openairdocs.org/sdr/IPXA2026051576486), May 8, 2026: FLOOR SUPPORT. CORRODED. FOUND FLOOR INTERCOSTAL CORROSION AT STA 1598 FROM RBL 33 TO RBL 54.75 IN THE AREA AFT OF BULK CARGO COMPARTMENT. FABRICATE P/N: 146T5649-2 I.A.W DWG 146T5649 S - [SDR IPXA2026051175974](https://openairdocs.org/sdr/IPXA2026051175974), May 8, 2026: CONTROL PANEL. MALFUNCTIONED. COCKPIT OVHD EMER LIGHT PANEL, LIGHT PLATE NOT ILLUMINATED. - [SDR IPXA2026051459222](https://openairdocs.org/sdr/IPXA2026051459222), May 7, 2026: RING ASSEMBLY. CRACKED. FOUND CRACK EXIST ON THE AFTER CASCADE SUPPORT RING, POSITION CLOSE TO THE NO.1 CASCADE OF 1L T/R HALF. .INSTALLED NEW CASCADE SUPPORT RING I.A.W SRM 51-40-02-0 - [SDR IPXA2026051661700](https://openairdocs.org/sdr/IPXA2026051661700), May 7, 2026: ACTUATOR. LEAKING. FOUND LT OUTBOARD AILERON OUTBOARD SIDE ACTUATOR LEAK. AMM 27-11-49-422-028 REV.148 STEP 3A TO 3H(7) INSTALL LT WING OUTBOARD AILERON OUTBOARD SIDE PCA. - [SDR IPXA2026051959294](https://openairdocs.org/sdr/IPXA2026051959294), May 7, 2026: SKIN PANEL. CRACKED. MAJOR REPAIR. CRACKED FWD ENTRY DOOR AFT LOWER CORNER SKIN ACCOMPLISH THE REPAIR I.A.W EO-87307-REQ7 REV2 AND SRM 53-10-01-2R-1 REV.95 AND EGAT WORK SHEET NO.60 - [SDR IPXA2026052062655](https://openairdocs.org/sdr/IPXA2026052062655), May 7, 2026: PLATE. CORRODED. FOUND SIDE GUIDE RAIL PLATE CORROSION AT STA 1395 RIGHT SIDE IN AFT CARGO COMPARTMENT INSTALLED FABRICATED TIE PLATE I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DW - [SDR IPXA2026052062772](https://openairdocs.org/sdr/IPXA2026052062772), May 7, 2026: FLOOR SUPPORT. CORRODED. FOUND FLOOR INTERCOSTAL CORROSION AT STA 1598 FROM RBL 11 TO RBL 33 IN THE AREA AFT OF BULK CARGO COMPARTMENT. INSTALLED FABRICATED INTERCOSTAL I.A.W SRM 51-40- - [SDR IPXA2026052062801](https://openairdocs.org/sdr/IPXA2026052062801), May 7, 2026: FLOOR SUPPORT. CORRODED. FOUND FLOOR INTERCOSTAL CORROSION AT STA 1598 FROM LBL 33 TO LBL 54.75 IN THE AREA AFT OF BULK CARGO COMPARTMENT INSTALLED FABRICATED INTERCOSTAL I.A.W SRM 51-4 - [SDR IPXA2026052062821](https://openairdocs.org/sdr/IPXA2026052062821), May 7, 2026: FLOOR SUPPORT. CORRODED. FOUND FLOOR INTERCOSTAL CORROSION AT STA 1598 FROM LBL 11 TO RBL 11 IN THE ARA AFT OF BULK CARGO COMPARTMENT INSTALLED FABRICATED INTERCOSTAL I.A.W SRM 51-40-02 - [SDR IPXA2026051661667](https://openairdocs.org/sdr/IPXA2026051661667), May 7, 2026: PCA. LEAKING. FOUND LT INBD AILERON INBOARD SIDE ACTUATOR LEAK. IAW AMM 27-11-48-422-040 REV.148 STEP 3A TO 3H(7) INSTALLED LT WING INBOARD AILERON INBOARD SIDE PCA. - [SDR IPXA2026051562655](https://openairdocs.org/sdr/IPXA2026051562655), May 7, 2026: PLATE. CORRODED. FOUND SIDE GUIDE RAIL PLATE CORROSION AT STA 1395 RIGHT SIDE IN AFT CARGO COMPARTMENT. - [SDR IPXA2026051962742](https://openairdocs.org/sdr/IPXA2026051962742), May 7, 2026: ANGLE. CORRODED. FOUND FLOOR ANGLE CORROSION AT STA 1596 RBL 59 IN THE AREA AFT OF BULK CARGO COMPARTMENT. FABRICATE P/N: 146T5619-357 I.A.W BOEING DWG NO: 146T5619 SH 8 REV."-" - [SDR IPXA2026051962761](https://openairdocs.org/sdr/IPXA2026051962761), May 7, 2026: ANGLE. CORRODED. FOUND FLOOR ANGLE CORROSION AT STA 1589.5 LBL 54.75 IN THE AREA AFT OF BULK CARGO COMPARTMENT. FABRICATE P/N: 146T5619-357 I.A.W BOEING DWG NO: 146T5619 SH 8 RE - [SDR IPXA2026051562772](https://openairdocs.org/sdr/IPXA2026051562772), May 7, 2026: FLOOR SUPPORT. CORRODED. FOUND FLOOR INTERCOSTAL CORROSION AT STA 1598 FROM RBL 11 TO RBL 33 IN THE AREA AFT OF BULK CARGO COMPARTMENT. FABRICATE P/N: 146T5649-3 I.A.W DWG 146T5649 SH 1 - [SDR IPXA2026051962786](https://openairdocs.org/sdr/IPXA2026051962786), May 7, 2026: FLOOR SUPPORT. CORRODED. FOUND FLOOR INTERCOSTAL CORROSION AT STA 1598 FROM LBL 11 TO LBL 33 IN THE AREA AFT OF BULK CARGO COMPARTMENT. FABRICATE P/N: 146T5649-3 I.A.W BOEING DWG NO: 14 - [SDR IPXA2026051562801](https://openairdocs.org/sdr/IPXA2026051562801), May 7, 2026: FLOOR SUPPORT. CORRODED. FOUND FLOOR INTERCOSTAL CORROSION AT STA 1598 FROM LBL 33 TO LBL 54.75 IN THE AREA AFT OF BULK CARGO COMPARTMENT (REPLACE) CORRECT REFERENCE SHOULD BE:
1. FA - [SDR IPXA2026051562821](https://openairdocs.org/sdr/IPXA2026051562821), May 7, 2026: FLOOR SUPPORT. CORRODED. FOUND FLOOR INTERCOSTAL CORROSION AT BS 1598 FROM LBL 11 TO RBL 11 IN THE ARA AFT OF BULK CARGO COMPARTMENT. FABRICATE P/N: 146T5649-4 I.A.W DWG 146T5649 SH 1 , - [SDR IPXA2026051561342](https://openairdocs.org/sdr/IPXA2026051561342), May 7, 2026: ANGLE. CRACKED. THE BULK CARGO OUTBOARD ANGLE AT STA 1578 LBL 80 IS CRACKED. (REPLACE) INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 95. AND BOEING DWG NO.146T5650 SH. 5 REV. - [SDR IPXA2026051561635](https://openairdocs.org/sdr/IPXA2026051561635), May 7, 2026: ANGLE. CRACKED. THE BULK CARGO INBOARD ANGLE AT STA 1578 RBL 80 IS CRACKED. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 95. AND BOEING DWG NO.146T5650 SH. 5 REV. C. - [SDR IPXA2026051561640](https://openairdocs.org/sdr/IPXA2026051561640), May 7, 2026: ANGLE. CRACKED. THE BULK CARGO OUTBOARD ANGLE AT STA 1578 RBL 80 IS CRACKED. (REPLACE) INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 95. AND BOEING DWG NO.146T5650 SH. 5 REV. - [SDR IPXA2026051461283](https://openairdocs.org/sdr/IPXA2026051461283), May 7, 2026: BRACKET. CRACKED. CRACKED BRACKET, NR 1 PYLON AFT FAIRING INNER HOLD OPEN ROD SUPPORT BRACKET. NR 1 PYLON AFT FAIRING INNER HOLD OPEN ROD SUPPORT BRACKET. (REPLACE) ATTACHMENTS A - [SDR IPXA2026050758690](https://openairdocs.org/sdr/IPXA2026050758690), May 7, 2026: BUMPER. MISSING. THE BUMPER IS MISSING FROM THE CREW ENTRY DOORWAY LINING (REPLACE) - [SDR IPXA2026082541483](https://openairdocs.org/sdr/IPXA2026082541483), May 6, 2026: PAWL. WORN. THE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. (REPLACE) REPLACED THE PAWL. I.A.W AMM 52-11-26-004-001 REV.148 AND AMM 52-11-26-404-003 REV.148. T - [SDR IPXA2026050741483](https://openairdocs.org/sdr/IPXA2026050741483), May 6, 2026: PAWL. WORN. THE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. (REPLACE) - [SDR IPXA2026051023848](https://openairdocs.org/sdr/IPXA2026051023848), May 5, 2026: ACTUATOR. FAILED. NO BACK BRAKE FUNCTION FAIL AT AFT CARGO DOOR ROTARY ACTUATOR. I.A.W AMM 52-37-04-404-009 REV.148 TO DO AFT CARGO DOOR OPERATIONAL TEST. THE RESULT WAS SATISFIE - [SDR IPXA2026051023870](https://openairdocs.org/sdr/IPXA2026051023870), May 5, 2026: ACTUATOR. NOISY. NOISE DURING FWD CARGO DOOR OPERATION. (REPLACE) I.A.W AMM 52-33-04-404-028 REV.148 TO DO FWD CARGO DOOR OPERATIONAL TEST. THE RESULT WAS SATISFIED. - [SDR IPXA2026033017125](https://openairdocs.org/sdr/IPXA2026033017125), Mar 28, 2026: COVER. UNSECURE. ARMING LEVER COVER FOR CREW ENTRY DOOR DOES NOT STAY FLUSH WITH ARMING LEVER IN INBD POSITION. ARMING LEVER COVER STAYS FLUSH WHEN ARMING LEVER IS IN THE OUTBOA - [SDR IPXA2026012785488](https://openairdocs.org/sdr/IPXA2026012785488), Jan 27, 2026: POWER SUPPLY. INOPERATIVE. DURING PDC, FOUND EMERGENCY LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-07. OPS CHECK GOOD. - [SDR IPXA2025110352856](https://openairdocs.org/sdr/IPXA2025110352856), Oct 31, 2025: DOOR. INOPERATIVE. L FWD ENTRY DOOR INDICATED OPEN WHEN IT IS CLOSED AND LOCKED ENTRY DOOR CLOSED SENSOR AND VISUAL WIRING INSPECTED FOR DAMAGES. NO FINDINGS. ENTRY DOOR CLOSED SE - [SDR IPXA2024111731063](https://openairdocs.org/sdr/IPXA2024111731063), Nov 16, 2024: FLOOR PANEL. NOT REPORTED. REMOVED FLOOR PANEL AT CENTER MCD POSITION 2&3, ROUTED TO SHEET METAL INSTALLATION ALSO UNDER T3F18E005LAN1. REPAIR ACCOMPLISHED PER SREO-9963-REQ001 All 196: https://openairdocs.org/aircraft/N301UP/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 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.