# N313UP: 1996 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: 27764 - Year built: 1996 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 21, 1996 - Certificate issued: November 22, 1996 - Expires: November 30, 2028 - Mode S code: A353C6 - Registered owner: [C C & E I LLC](https://openairdocs.org/faa-owner/C%20C%20%26%20E%20I%20LLC) - Location: [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville) - Owner type: LLC - 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=313UP - Page: https://openairdocs.org/aircraft/N313UP 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/N313UP/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 N313UP. ## FAA accident and incident reports None matched to N313UP. ## Service difficulty reports (177, 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 IPXA2026041371289](https://openairdocs.org/sdr/IPXA2026041371289), Apr 13, 2026: FITTING. NONE. NR 2 WING STRUT SUPPORT CLEVIS FITTING FREEZE PLUG - PERMANENT REPAIR. CONDITION CHECK NORMAL. PAPER FINAL CHECK OK. - [SDR IPXA2026041575356](https://openairdocs.org/sdr/IPXA2026041575356), Apr 7, 2026: BUSHING. MIGRATED. MIGRATED BUSHING, RT WING T/E NR 8 SPOILER MID LWR. IAW CMM:57-70-11, REV 42, REPAIR 2-1, PAGE 601 - 602 STEP 3, COMPLETED THE REPLACEMENT OF BUSHING. - [SDR IPXA2026041070344](https://openairdocs.org/sdr/IPXA2026041070344), Apr 7, 2026: SEAL. CRACKED. NR 1 ENG FAIRING PANEL 436CR SPRING SEAL CRACKED. INSTALL NEW STRIP SEAL I.A.W SRM 51-40-02-0G REV.94 AND BOEING DWG NO:311T2570 SH 1 REV.N - [SDR IPXA2026041669415](https://openairdocs.org/sdr/IPXA2026041669415), Apr 7, 2026: DEPRESSOR. DEFORMED. DEFORMED DEPRESSOR SILL, FORWARD CARGO DOOR CUTOUT AREA AFTER SIDE. INSTALL NEW DEPRESSOR SEAL I.A.W SRM 51-40-02-0G REV.94 AND BOEING DWG NO:143T8540 SH1 REV.B - [SDR IPXA2026041172897](https://openairdocs.org/sdr/IPXA2026041172897), Apr 7, 2026: SKIN. BULGED. SKIN, R/H WING T/E OUTBD FLAP INBD LWR. PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2" HEATED AREA IAW NDT MANUAL PART 1 51-01-01 REV 143. - [SDR IPXA2026040958846](https://openairdocs.org/sdr/IPXA2026040958846), Apr 6, 2026: SEAL. BROKEN. NO.2 PYLON, RT FAIRING PANEL 446CR SEAL BROKEN INSTALLED NEW SEAL I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO. 311T2570 SH. 1 REV. N. - [SDR IPXA2026041159269](https://openairdocs.org/sdr/IPXA2026041159269), Apr 6, 2026: HINGE. WORN. NR 2 PYLON L/H PRSOV ACCESS DWR. INSTALLED NEW HINGE I.A.W SRM 51-40-02-0G REV. 94, BOEING DWG NO. 311T1064 SH. 1 REV. G AND BOEING DWG NO. 311T1064 SH. 2 REV. - [SDR IPXA2026041658143](https://openairdocs.org/sdr/IPXA2026041658143), Apr 6, 2026: FLOORBEAM. CRACKED. CRACK, ANGLE FLOORBEAM BS 246, RBL 38. ACCOMPLISHED REPAIR I.A.W UPS EO-97146-REQ1 REV1. - [SDR IPXA2026041458575](https://openairdocs.org/sdr/IPXA2026041458575), Apr 6, 2026: STRUT. CRACKED. CRACKED STRUT, RT WING L/E PANEL NR 621SB, OTBD, OSS 694.  INSTALLED NEW STRUT I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO. 114T2214 SH 1 REV. B, 112T2000 - [SDR IPXA2026041259154](https://openairdocs.org/sdr/IPXA2026041259154), Apr 6, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 1 ENG LT CORE COWL HOLD OPEN ROD SUPPORT BRACKET. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-13-23, REV 47. - [SDR IPXA2026041259005](https://openairdocs.org/sdr/IPXA2026041259005), Apr 6, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 1 ENGINE RT CORE COWL HOLD OPEN ROD SUPPORT BRACKET. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-13-24, REV 50. - [SDR IPXA2026041159001](https://openairdocs.org/sdr/IPXA2026041159001), Apr 6, 2026: STIFFENER. CRACKED. CRACKED STIFFENER, NR 1 ENG RT THRUST REVERSER FWD TORQUE BOX SUPPORT STIFFENER NEAR 2:00 POS. INSTALL A NEW STIFFENER IAW SRM 51-40-02-0G, REV 94, AND AIPC 78- - [SDR IPXA2026041158718](https://openairdocs.org/sdr/IPXA2026041158718), Apr 6, 2026: STIFFENER. CRACKED. CRACKED STIFFENER, NR 1 ENG RT THRUST REVERSER. FWD TORQUE BOX SUPPORT STIFFENER NEAR 1:00 POS. INSTALLED A NEW STIFFENER IAW SRM 51-40-02-0G, REV 94 & AIPC 78- - [SDR IPXA2026041058741](https://openairdocs.org/sdr/IPXA2026041058741), Apr 6, 2026: CHANNEL. CRACKED. CRACKED CHANNEL, NR 2 ENG AFT FAIRING PANEL 447DB INNER AREA. INSTALLED A NEW CHANNEL IAW SRM 51-40-02-0G REV.94, & DWG 313T3360, SH 42, REV E. - [SDR IPXA2026041059158](https://openairdocs.org/sdr/IPXA2026041059158), Apr 6, 2026: FLOOR PANEL. DELAMINATED. FLOOR PANEL IN THE AFT CARGO COMPARTMENT IS DELAMINATED. REPAIRED IAW SRM 53-00-50-2R-0, REV 94. CHECKED SATISFACTORY. - [SDR IPXA2026041346666](https://openairdocs.org/sdr/IPXA2026041346666), Apr 5, 2026: RUB STRIP. CRACKED. NR 2 ENG LT CORE COWL INNER T/E UPPER RUB STRIP. INSTALLED NEW STRIP IAW SRM 51-40-02-0G REV. 94 AND CMM IPL 71-13-23 REV. 47. - [SDR IPXA2026041447390](https://openairdocs.org/sdr/IPXA2026041447390), Apr 5, 2026: STRUCTURE. CRACKED. CRACKED CHORD, RT WING L/E PNL 621HB MID AREA OSS 531. INSTALLED NEW CHORD I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO: 114T2206 SH 1REV. B. - [SDR IPXA2026041047733](https://openairdocs.org/sdr/IPXA2026041047733), Apr 5, 2026: FLOOR PANEL. DELAMINATED. THE FLOOR PANEL IN THE AFT CARGO COMPARTMENT IS DELAMINATED. REPAIRED IAW SRM 53-00-50-2R-0, REV 94. - [SDR IPXA2026041047753](https://openairdocs.org/sdr/IPXA2026041047753), Apr 5, 2026: FLOOR PANEL. DELAMINATED. THE FLOOR PANEL IN THE AFT CARGO COMPARTMENT IS DELAMINATED. REPAIRED IAW SRM 53-00-50-2R-0 REV. 94. - [SDR IPXA2026041047769](https://openairdocs.org/sdr/IPXA2026041047769), Apr 5, 2026: FLOOR PANEL. DELAMINATED. THE FLOOR PANEL IN THE AFT CARGO COMPARTMENT IS DELAMINATED. IAW SRM 53-00-50-2R-0, REV 94, PERFORMED A BOND THE REPAIR OF PLIES WITH RESIN CURED AT 170°F FOR - [SDR IPXA2026041047239](https://openairdocs.org/sdr/IPXA2026041047239), Apr 5, 2026: FLOOR PANEL. DELAMINATED. THE FLOOR PANEL IN THE AFT CARGO COMPARTMENT IS DELAMINATED. REPAIRED IAW SRM 53-00-50-2R-0, REV 94. - [SDR IPXA2026040746687](https://openairdocs.org/sdr/IPXA2026040746687), Apr 5, 2026: BRACKET. CRACKED. L/H WING INBD L/E CAVITY TORQUE TUBE SUPPORT BRACKET CRACKED. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND DWG 114T1240, SHT 2, REV E. - [SDR IPXA2026040746494](https://openairdocs.org/sdr/IPXA2026040746494), Apr 5, 2026: ANGLE. CRACKED. CRACKED CLIP, NR 2 PYLON AFT LWR FAIRING INNER NUT FRAME OUTBD SIDE SUPPORT CLIP. INSTALLED NEW CLIP IAW SRM 51-40-02-0G, REV 94 AND DWG 313T3380, SHT 3, REV F. - [SDR IPXA2026040746727](https://openairdocs.org/sdr/IPXA2026040746727), Apr 5, 2026: CLAMP. CRACKED. CRACKED CLAMP, NR 2 ENG AFT FAIRING DOOR SUPPORT ROD STOW AREA. INSTALLED NEW CLAMP IAW SRM 51-40-02-0G REV. 94 AND DWG 313T3349, SH. 2 REV. B. - [SDR IPXA2026041535922](https://openairdocs.org/sdr/IPXA2026041535922), Apr 4, 2026: TEE FITTING. CRACKED. CRACKED TEE FITTING, NR 1 PYLON AFT FAIRING INNER OUTBD LWR TEE CRACK. INSTALLED NEW TEE IAW SRM 51-40-02-0G, REV 94, AND DWG 313T2380, SHT 7, REV H, AND EO NO: - [SDR IPXA2026041536044](https://openairdocs.org/sdr/IPXA2026041536044), Apr 4, 2026: SEAL. CRACKED. CRACKED ZEE, NR 2 PYLON RT FAIRING DOOR AFT LWR CUTOUT AREA. INSTALLED NEW ZEE IAW SRM 51-40-02-0G, REV.94, AND DWG 313T2380, SHT 10, REV K AND DWG 313T2380, SH - [SDR IPXA2026041635932](https://openairdocs.org/sdr/IPXA2026041635932), Apr 4, 2026: RUB STRIP. BROKEN. BROKEN STRIP, NR 1 ENG NOSE COWL T/E RT UPPER WEAR STRIP. INSTALLED NEW STRIP I.A.W SRM 51-40-02-0G REV. 94 AND GOODRICH CMM IPL 71-11-16 REV. 54. AND AMM INTRO - [SDR IPXA2026041637268](https://openairdocs.org/sdr/IPXA2026041637268), Apr 4, 2026: FLOORBEAM. CORRODED. CORROSION DAMAGE ON UPPER CHORD OF FLOOR BEAM AT STA 246 NEAR RBL 30 (EVALUATE) REVIEWED PER GMM-MTX 09.05.01.09. ACCOMPLISHED REPAIR I.A.W EO-97113-REQ1 REV1 A - [SDR IPXA2026041435847](https://openairdocs.org/sdr/IPXA2026041435847), Apr 4, 2026: PLATE. CRACKED. THE FORWARD CARGO SIDE GUIDE RAIL TIE PLATE AT LT BS 566 IS CRACKED. REPLACED. INSTALLED FABRICATE TIE PLATE IAW SRM 51-40-02-0G, REV 94, AND DWG 452T2003, SHT - [SDR IPXA2026041235947](https://openairdocs.org/sdr/IPXA2026041235947), Apr 4, 2026: BRACKET. CRACKED. CRACKED, NR 2 PYLON AFT LWR FAIRING INNER DRAIN TUBE SUPPORT BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, & DWG 272T0333, SHT 8, REV -. - [SDR IPXA2026041035897](https://openairdocs.org/sdr/IPXA2026041035897), Apr 4, 2026: CHANNEL. CRACKED. CRACKED, NR 1 PYLON AFT FAIRING PNL NR 437DB INNER CHANNEL AREA. INSTALLED A NEW CHANNEL IAW SRM 51-40-02-0G, REV 94, AND DWG 313T3360, SHT 42, REV E. - [SDR IPXA2026041035962](https://openairdocs.org/sdr/IPXA2026041035962), Apr 4, 2026: BULKHEAD. CRACKED. CRACKED BULKHEAD, NR 1 PYLON AFT FAIRING PANEL NR.437DB INNER NEW AREA. INSTALL NEW BULKHEAD IAW SRM 51-40-02-0G, REV 94, AND DWG 313T3360, SHT 42, REV E. - [SDR IPXA2026041518128](https://openairdocs.org/sdr/IPXA2026041518128), Apr 3, 2026: WINGLET. DAMAGED. R/H WING OUTBD AREA WINGLET. (REPAIR) REPAIR LIGHTNING STRIKE DAMAGE ON FASTENER HOLE OF RH WINGLET LOWER SKIN I.A.W. UPS EO-97110-REQ1 REV.1 AND EGAT EI NO. F2 - [SDR IPXA2026041517950](https://openairdocs.org/sdr/IPXA2026041517950), Apr 3, 2026: HANDLE. 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, - [SDR IPXA2026041317026](https://openairdocs.org/sdr/IPXA2026041317026), Apr 3, 2026: FLOORBEAM. CORRODED. FOUND MAIN DECK FLOOR BEAM FITTING CORROSION. INSTALLED FABRICATED FILLER IAW SRM 51-40-02-0G, REV 94, AND DWG 146T5650, SHEET 5, REV C. - [SDR IPXA2026040317950](https://openairdocs.org/sdr/IPXA2026040317950), Apr 3, 2026: PAWL. WORN. THE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. (REPLACE) - [SDR IPXA2026041091568](https://openairdocs.org/sdr/IPXA2026041091568), Apr 2, 2026: SEAT TRACK. WORN. FOUND SEAT TRACK ASSY INBOARD FWD OF CAPTAIN SEAT WORN. REPLACED THE SEAT TRACK ASSY IAW AMM 25-11-01-822-095-001, REV 147. - [SDR IPXA2026030586411](https://openairdocs.org/sdr/IPXA2026030586411), Jan 27, 2026: SENSOR. FALSE INDICATION. L1 DOOR EICAS MESSAGE CLIMBING THROUGH 5000 FT. PRESSURIZATION REMAINED NORMAL. REPLACED DOOR CLOSED SENSOR IAW AMM 52-71-01-964-211. DMP REVERSED. DEFERRAL CLE - [SDR IPXA2026012786411](https://openairdocs.org/sdr/IPXA2026012786411), Jan 27, 2026: WARNING MESSAGE. ILLUMINATED. LEFT FWD ENTRY DOOR EICAS MSG CLIMBING THROUGH 5000 FT. PRESSURIZATION REMAINED NORMAL. DEFERRED PER MEL 52-71-1-1A - [SDR IPXA2025092645526](https://openairdocs.org/sdr/IPXA2025092645526), Sep 25, 2025: LATCH. FAULTED. COVER FOR YELLOW ENTRY DOOR LATCH PROTRUDES OUT AND WILL NOT CLOSE. DEFERRED MAIN ENTRY/SERVICE DOOR ARMING LEVER HINGED COVERS IAW MEL 52-11-2. - [SDR IPXA2024070994662](https://openairdocs.org/sdr/IPXA2024070994662), Jun 30, 2024: HANDLE. DETACHED. CREW DOOR HANDLE FELL OFF. R&R DOOR HANDLE ESCUTCHEON DOOR ACCESS AND FWD ENTRY DOOR HINGE ASSY REF AMM 52-12-02/401. THIS CLEARS MEL 52-11-2. PLACARDS REMOVED. - [SDR IPXA2024063094662](https://openairdocs.org/sdr/IPXA2024063094662), Jun 30, 2024: HANDLE. DETACHED. CREW DOOR HANDLE FELL OFF. DEFERRING PER MEL 52-11-2 PLACARD INSTALLED. OPEN - [SDR IPXA2024032147565](https://openairdocs.org/sdr/IPXA2024032147565), Mar 19, 2024: SKIN. CORRODED. FAULT - CORROSION ON FUSELAGE SKIN BETWEEN STA 1395-STA 1417, S-38R-S-39R. (REPAIR). PERFORMED FPI INSPECTION AT TRIM AREA PER SOPM 20-20-02 TO CONFIRM CORROSIO - [SDR IPXA2024030138141](https://openairdocs.org/sdr/IPXA2024030138141), Mar 1, 2024: FLOOR PANEL. BROKEN. *MAJOR REPAIR* FAULT - FOUND MAIN DECK CARGO FLOOR PANEL BROKEN, PANEL NO.231AFF P/N: 143T5876-78 (REPLACE) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 - [SDR IPXA2024030138116](https://openairdocs.org/sdr/IPXA2024030138116), Mar 1, 2024: FLOOR PANEL. BROKEN. *MAJOR REPAIR* FAULT - FOUND MAIN DECK CARGO FLOOR PANEL BROKEN, PANEL NO.231FFF, P/N: 143T5876-85 (REPLACE) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 - [SDR IPXA2024031397889](https://openairdocs.org/sdr/IPXA2024031397889), Feb 28, 2024: STRAP. CRACKED. FOUND CRACK AT STA 1725.5 STR-7R BULKHEAD OUTER CHORD STRAP. ACCOMPLISHED REPAIR I.A.W EO-24301-REQ002 REV.5 AND EO-24301-JIC003 REV.3 AND EO-89771-REQ1 REV.1 A - [SDR IPXA2024031197280](https://openairdocs.org/sdr/IPXA2024031197280), Feb 28, 2024: ACCESS PANEL. CRACKED. FOUND RH WING LOWER OUTBOARD MAIN FUEL PUMP ACCESS CRACK (REPLACE) 1.I.A.W AMM 20-11-00-910-802 REV.141 REPLACED THE ACCESS PANEL. COND CHECK NORMAL. ATTACHMENT - [SDR IPXA2024030700729](https://openairdocs.org/sdr/IPXA2024030700729), Feb 28, 2024: ANGLE. LEAKING. ANGLE CRACKED BULK CARGO COMPARTMENT RIGHT AREA STA 1578 LBL 60 (REPLACE) ACCOMPLISHED MAIN DECK CARGO ACCESS DADO PANEL AND FLOOR PANEL OK TO INSTALL CHECK,AND - [SDR IPXA2024030700671](https://openairdocs.org/sdr/IPXA2024030700671), Feb 28, 2024: ANGLE. CRACKED. CRACKED ANGLE STA 246, LBL 49. FABRICATE P/N(141T5146-16) PER BOEING DWG NO.:141T5146 SH 15 REV."B";PL REV."F";PSDL REV."-" AND ORIGINAL PART AS A SAMPLE I.A.W. - [SDR IPXA2024030500756](https://openairdocs.org/sdr/IPXA2024030500756), Feb 28, 2024: ANGLE. CRACKED. CRACKED ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60 (REPAIR) 1. REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.88 2. INSTALLED NEW PARTS I.A.W SRM 5 All 177: https://openairdocs.org/aircraft/N313UP/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.