# N334UP: 2001 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: 32844 - Year built: 2001 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 12, 2001 - Certificate issued: November 14, 2019 - Expires: November 30, 2029 - Mode S code: A3A67B - 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=334UP - Page: https://openairdocs.org/aircraft/N334UP 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/N334UP/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 N334UP. ## FAA accident and incident reports None matched to N334UP. ## Service difficulty reports (126, 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 IPXA2026062204155](https://openairdocs.org/sdr/IPXA2026062204155), Jun 17, 2026: NOSE COWL. DENTED. DENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 7:00 POS. (REPAIR) CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 11" FROM AFT EDGE AND 27" F - [SDR IPXA2026062204145](https://openairdocs.org/sdr/IPXA2026062204145), Jun 17, 2026: NOSE COWL. DENTED. DENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 1:00 POS. (REPAIR) CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 21" FROM FWD EDGE, 18" FROM - [SDR IPXA2026062204122](https://openairdocs.org/sdr/IPXA2026062204122), Jun 17, 2026: NOSE COWL. DENTED. DENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 11:00 POS. (REPAIR) CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 18.5" FROM AFT EDGE, 24" F - [SDR IPXA2026062204106](https://openairdocs.org/sdr/IPXA2026062204106), Jun 17, 2026: NOSE COWL. DENTED. DENTED SKIN, NR 1 ENG NOSE COWL BARREL NEAR 4:00 POS. (REPAIR) CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 20" FROM FWD EDGE, 4" FROM LOWER - [SDR IPXA2026062203995](https://openairdocs.org/sdr/IPXA2026062203995), Jun 17, 2026: NOSE COWL. DENTED. DENTED SKIN, NR 1 ENG NOSE COWL INNER BARRER NEAR 9:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 4.75" FROM AFT EDGE, 33" FROM LOWER - [SDR IPXA2026062203992](https://openairdocs.org/sdr/IPXA2026062203992), Jun 17, 2026: NOSE COWL. DENTED. DENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 6:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 10.5" FROM AFT EDGE AND 45" FROM OUT - [SDR IPXA2026062203971](https://openairdocs.org/sdr/IPXA2026062203971), Jun 17, 2026: NOSE COWL. DENTED. DENTED SKIN, NR 1 ENG NOSE COWL INNER BARRER NEAR 9:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 7" FROM AFT EDGE AND 24" FROM LOWER - [SDR IPXA2026062203947](https://openairdocs.org/sdr/IPXA2026062203947), Jun 17, 2026: NOSE COWL. DENTED. DENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 5:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 19.5" FROM UPPER EDGE AND 11.5" FROM - [SDR IPXA2026062203822](https://openairdocs.org/sdr/IPXA2026062203822), Jun 17, 2026: NOSE COWL. DENTED. DENT - SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 4:00 POS. (REPAIR) CONFIRM THAT THE ENGINE NACELLE IS ACOUSTICALLY COMPLIANT IAW SRM 54-00-00-2R-0 REV. 95. - [SDR IPXA2026062203799](https://openairdocs.org/sdr/IPXA2026062203799), Jun 17, 2026: NOSE COWL. DENTED. DENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 1:00 POS. (REPAIR) CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.7", 15.5" FROM AFT EDGE , 29" F - [SDR IPXA2026062203788](https://openairdocs.org/sdr/IPXA2026062203788), Jun 17, 2026: NOSE COWL. DENTED. DENTED SKIN, NR 1 ENG NOSE COWL INNER BARREL NEAR 6:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 11" FROM AFT EDGE AND 50.5" FROM OUT - [SDR IPXA2026062102849](https://openairdocs.org/sdr/IPXA2026062102849), Jun 17, 2026: SKIN. CRACKED. CRACKED SKIN, LT WING T/E NR 3 FLAP AFT FAIRING INBD. (REPAIR) IAW NDT MANUAL PART 1, 51-01-01 & PART 4, 51-00-03, REV.143 TO PERFORM NDT/UT FOR THE POST REPAIR - [SDR IPXA2026061903308](https://openairdocs.org/sdr/IPXA2026061903308), Jun 17, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 2 ENG RT T/R CLOSURE DOOR T/E AREA. (REPLACE). INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND ST ENGINEERING IPC 78-32-22 REV.96 C/W - [SDR IPXA2026061903879](https://openairdocs.org/sdr/IPXA2026061903879), Jun 17, 2026: SUPPORT ANGLE. CRACKED. CRACKED SUPPORT ANGLE, NR 2 PYLON AFT FAIRING INNER AFT FRAME INBD SIDE SUPPORT CLIP. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 313T23 - [SDR IPXA2026061903908](https://openairdocs.org/sdr/IPXA2026061903908), Jun 17, 2026: BRACKET. CRACKED. CRACKED BRACKET, RT WING INBD L/E CAVITY TORQUE TUBE SUPPORT BRACKET. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 114T1240 SH 4 REV: D. - [SDR IPXA2026061903869](https://openairdocs.org/sdr/IPXA2026061903869), Jun 17, 2026: SUPPORT ANGLE. CRACKED. CRACKED ANGLE, NR 2 PYLON AFT FAIRING INNER AFT FRAME OUTBD SIDE SUPPORT ANGLE. INSTALL NEW CLIP I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 313T2303 SH 74 - [SDR IPXA2026061904932](https://openairdocs.org/sdr/IPXA2026061904932), Jun 17, 2026: BRACKET. CRACKED. CRACKED BRACKET, LT WING L/E INBD PANEL 511KB TORQUE TUBE SUPPORT LES 281. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 114T1240 SH 4 REV - [SDR IPXA2026062585393](https://openairdocs.org/sdr/IPXA2026062585393), Jun 16, 2026: TORQUE BOX. DENTED. MANY DENTS & DISBOND - L/H V.S.T LOWER FWD TORQUE BOX UPPER PANEL. INSTALL NEW TORQUE BOX PANEL I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 175T0000 SH 1 RE - [SDR IPXA2026062485353](https://openairdocs.org/sdr/IPXA2026062485353), Jun 16, 2026: LONGERON FITTING. CRACKED. LEFT UNDERWING LONGERON FITTING HAS CRACK DURING PERFORMED J/C: EO-48156-JIC001. ACCOMPLISHED JOB I.A.W UPS EO-48156-JIC003 REV2 AND UPS EO-97843-REQ1 REV1 (EGA - [SDR IPXA2026061989107](https://openairdocs.org/sdr/IPXA2026061989107), Jun 16, 2026: ADAPTER. CHAFED. CHAFED BRACKET, NR 2 ENG RT CORE COWL INNER OPEN ROD STOW BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND CMM IPL 71-13-24, REV 50. - [SDR IPXA2026061989218](https://openairdocs.org/sdr/IPXA2026061989218), Jun 16, 2026: SEAL. CRACKED. CRACKED SEAL, NR 2 ENG RT CORE COWL FLIPPER DOOR. REMOVED DAMAGE SEAL IAW SRM 51-40-02-0G REV.95. INSTALLED A NEW SEAL IAW SRM 51-40-02-0G, REV.95, & CMM IPL 71 - [SDR IPXA2026061990900](https://openairdocs.org/sdr/IPXA2026061990900), Jun 16, 2026: ADAPTER. CHAFED. CHAFED BRACKET, NR 1 ENG LT CORE COWL INNER HOLD OPEN ROD SUPPORT BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 95, & CMM IPL 71-13-23 REV. 47. - [SDR IPXA2026061989175](https://openairdocs.org/sdr/IPXA2026061989175), Jun 16, 2026: ADAPTER. CHAFED. CHAFED BRACKET, NR 2 ENG LT CORE COWL INNER OPEN ROD STOW BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 95, & CMM IPL 71-13-23 REV. 47. - [SDR IPXA2026061988855](https://openairdocs.org/sdr/IPXA2026061988855), Jun 16, 2026: ADAPTER. CHAFED. CHAFED BRACKET, NR 1 ENG RT CORE COWL INNER HOLD OPEN ROD SUPPORT BRACKET. INSTALL NEW BRACKET IAW SRM 51-40-02-0G, REV 95 AND CMM IPL 71-13-24 REV. 50. - [SDR IPXA2026062287436](https://openairdocs.org/sdr/IPXA2026062287436), Jun 16, 2026: NOSE COWL. DENTED. DENTED SKIN, NR 2 ENG INLET COWL INNER BARREL NEAR 3:00 POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.7", 15.5" FROM AFT EDGE AND 25.5" - [SDR IPXA2026062287408](https://openairdocs.org/sdr/IPXA2026062287408), Jun 16, 2026: NOSE COWL. DENTED. DENTED SKIN, NR 2 ENG INLET COWL INNER BARREL NEAR 8:00 POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 7.5" FROM AFT EDGE AND 16.5" F - [SDR IPXA2026062287404](https://openairdocs.org/sdr/IPXA2026062287404), Jun 16, 2026: NOSE COWL. DENTED. DENTED SKIN, NR 2 ENG INLET COWL INNER BARREL NEAR 5:30 POSITION. (REPAIR). CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 14.75" FROM AFT EDGE - [SDR IPXA2026062286352](https://openairdocs.org/sdr/IPXA2026062286352), Jun 16, 2026: SKIN. DENTED. DENTED SKIN, NR 2 ENG INLET COWL INNER BARREL NEAR 6:00 POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 14.25" FROM FWD EDGE AND 38.5" - [SDR IPXA2026061989062](https://openairdocs.org/sdr/IPXA2026061989062), Jun 16, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 1 ENG RT T/R FWD LWR CLOSURE DOOR T/E AREA. (REPLACE). INSTALL NEW BRACKET IAW SRM 51-40-02-0G REV.95 AND ST ENGINEERING IPC 78-32-22 REV.96. - [SDR IPXA2026062572828](https://openairdocs.org/sdr/IPXA2026062572828), Jun 15, 2026: TORQUE BOX. DEBONDED. MANY DENTS & DISBOND - L/H V.S.T LOWER FWD TORQUE BOX LWR PANEL. INSTALL NEW TORQUE BOX PANEL I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 175T0000 SH 1 REV: - [SDR IPXA2026062173665](https://openairdocs.org/sdr/IPXA2026062173665), Jun 15, 2026: SKIN. CRACKED. CRACKED SKIN, LT WING T/E OTBD FLAP INBD END CAP (REPAIR) IAW NDT MANUAL PART 1, 51-01-01 & PART 4, 51-00-03, REV.143 TO PERFORM NDT/UT FOR THE POST REPAIRED AR - [SDR IPXA2026062158828](https://openairdocs.org/sdr/IPXA2026062158828), Jun 14, 2026: ANTENNA. ERODED. FOUND VST HF ANTENNA (321E) ERODED. IAW NDT MANUAL PART 1, 51-01-01 & PART 4, 51-00-03, REV.143 TO PERFORM NDT/UT FOR THE POST REPAIRED AREA INCLUDED THE AREA W - [SDR IPXA2026061860062](https://openairdocs.org/sdr/IPXA2026061860062), Jun 14, 2026: FLAP TRACK. CRACKED. CRACK - SKIN, R/H WING NO.6 FLAP TRACK MID FAIRING INBD SIDE T/E SKIN. (REPAIR) I.A.W. B767 NDT MANUAL PART 1, 51-01-01 AND PART 4, 51-00-03, REV.143 TO PERFORM - [SDR IPXA2026062542487](https://openairdocs.org/sdr/IPXA2026062542487), Jun 6, 2026: SEAL DEPRESSOR. DAMAGED. ROUND CREW REPORTED DAMAGE ON AFT MCD DOOR CUTOUT .INSTALLED MAIN DECK CARGO DOOR DEPRESSOR SEAL AT AFT SIDE I.A.W AMM 20-11-00-910-802 REV.148 AND TORQUE BOLTS - [SDR IPXA2024070337674](https://openairdocs.org/sdr/IPXA2024070337674), Jul 3, 2024: DRAIN. NONE. FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. EO-82173-JIC001 WAS ACCOMPLISHED. - [SDR IPXA2024062856854](https://openairdocs.org/sdr/IPXA2024062856854), Jun 28, 2024: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL DENT. PANEL NO. : 251AGF, P/N : 146T5869-91 (REPAIR) I.A.W AMM 25-57-02-404-016, AMM 25-58-01-404-005, AMM 25-57-05-404-006 AND AMM - [SDR IPXA2024062856740](https://openairdocs.org/sdr/IPXA2024062856740), Jun 28, 2024: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL 251AFF DENTED. OPEN - [SDR IPXA2024062856846](https://openairdocs.org/sdr/IPXA2024062856846), Jun 28, 2024: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL DENT. PANEL NO. : 222BFF, P/N : 141T5856-49 (REPAIR) I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404-005 AND AMM 25-58-05-404-052 REV.1 - [SDR IPXA2024062858148](https://openairdocs.org/sdr/IPXA2024062858148), Jun 28, 2024: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL DENT. PANEL NO. : 251LFF, P/N : 146T5869-78 (REPAIR) I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404-005 AND AMM 25-58-03-404-004 REV.1 - [SDR IPXA2024062856784](https://openairdocs.org/sdr/IPXA2024062856784), Jun 28, 2024: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL DENT. PANEL NO. : 231LFF, P/N : 143T5876-87 I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404-005, AMM 25-57-02-404-016 AND AMM 25-58-03- - [SDR IPXA2024062856822](https://openairdocs.org/sdr/IPXA2024062856822), Jun 28, 2024: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL 252BFF DENTED. FOUND MAIN DECK FLOOR PANEL DENT. PANEL NO. : 252BFF, P/N : 146T5869-62 (REPAIR) I.A.W AMM 25-57-05-404-006, AMM 25-5 - [SDR IPXA2024062857620](https://openairdocs.org/sdr/IPXA2024062857620), Jun 28, 2024: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL DENT. PANEL NO. : 232NFF, P/N : 143T5876-20 (REPAIR) I.A.W AMM 25-58-04-404-015, AMM 25-57-05-404-006, AMM 25-57-02-404-016 AND AMM - [SDR IPXA2024062857602](https://openairdocs.org/sdr/IPXA2024062857602), Jun 28, 2024: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL DENT. PANEL NO. : 231FFF, P/N : 143T5876-49 (REPAIR) I.A.W AMM 25-57-03-404-005, AMM 25-58-03-404-017, AMM 25-57-02-404-016 AND AMM - [SDR IPXA2024070906655](https://openairdocs.org/sdr/IPXA2024070906655), Jun 25, 2024: FITTING. BROKEN. FOUND MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING BROKEN AT STA 1175 BL00.0 AND STA 1197 BL00.0 TTL : 2EA (REPLACE). INSTALLED NEW PART I.A.W SRM 51-40-02-0 - [SDR IPXA2024070876655](https://openairdocs.org/sdr/IPXA2024070876655), Jun 25, 2024: FITTING. BROKEN. **SDR FILED OPEN**FAULT - FOUND MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING BROKEN AT STA 1175 BL00.0 AND STA 1197 BL00.0 TTL : 2EA (REPLACE) 1. REMOVED DAM - [SDR IPXA2024070791131](https://openairdocs.org/sdr/IPXA2024070791131), Jun 24, 2024: ANGLE. CRACKED. FOUND BULK CARGO COMPARTMENT RIGHT AREA ANGLE CRACK AT STA 1578. INSTALLED NEW PARTS I.A.W SRM 51-40-02-0G REV.89 AND BOEING DWG NO:146T5650 SHEET 5 REV.C. JOB - [SDR IPXA2024070791142](https://openairdocs.org/sdr/IPXA2024070791142), Jun 24, 2024: ANGLE. CRACKED. FOUND BULK CARGO COMPARTMENT LEFT AREA ANGLE CRACK AT STA 1578 LBL 80 INBOARD (REPLACE). INSTALLED NEW PARTS I.A.W SRM 51-40-02-0G REV.89 AND BOEING DWG NO:146T - [SDR IPXA2024071179048](https://openairdocs.org/sdr/IPXA2024071179048), Jun 24, 2024: ANGLE. CRACKED. FOUND BULK CARGO COMPARTMENT RIGHT AREA ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD. INSTALLED NEW PARTS I.A.W SRM 51-40-02-0G REV.89 AND BOEING DWG NO:146T5650 SHE - [SDR IPXA2024070871131](https://openairdocs.org/sdr/IPXA2024070871131), Jun 24, 2024: ANGLE. CRACKED. OPEN, FOUND BULK CARGO COMPARTMENT RIGHT AREA ANGLE CRACK AT STA 1578 (REPLACE) ATTACHEMENTS ARE UPLOADED. - [SDR IPXA2024070871142](https://openairdocs.org/sdr/IPXA2024070871142), Jun 24, 2024: ANGLE. CRACKED. OPEN, FOUND BULK CARGO COMPARTMENT LEFT AREA ANGLE CRACK AT STA 1578 LBL 80 INBOARD. All 126: https://openairdocs.org/aircraft/N334UP/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.