# N319UP: 1997 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: 27758 - Year built: 1997 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 9, 1997 - Certificate issued: September 12, 1997 - Expires: May 31, 2028 - Mode S code: A36A10 - 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=319UP - Page: https://openairdocs.org/aircraft/N319UP 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/N319UP/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 DFW06IA025](https://openairdocs.org/ntsb/DFW06IA025), Dec 16, 2005: Boeing 767-300ER (N319UP), Houston, TX, incident, minor damage. Probable cause: The captain's failure to maintain clearance from a parked airplane awaiting for a gate. A contributing factor was that taxi procedures were not issued by ground control to advise the captain that the… ## 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. - [Incident 20051215029949I](https://openairdocs.org/incident/20051215029949I), Dec 15, 2005: Boeing 76734AF (N319UP), Houston, TX, Minor damage. (-23) On December 15, 2005, at 1805 central standard time (CST), a Boeing 767-34AF cargo-configured airplane, N319UP, operated by united parcel service (ups)… ## Service difficulty reports (169, 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 IPXA2026040709874](https://openairdocs.org/sdr/IPXA2026040709874), Apr 2, 2026: DOOR. OUT OF ADJUST. LEFT FWD ENT DOOR AFTER PUSHBACK T/S PERFORMED. MAIN CREW DOOR SENSOR NOTED TO BE OUT OF ADJUSTMENT. ADJUSTED AS PER AMM 52-71-01-964-211. OPS CHECK GOOD. - [SDR IPXA2026040209874](https://openairdocs.org/sdr/IPXA2026040209874), Apr 2, 2026: WARNING LIGHT. FALSE ACTIVATION. LEFT FWD ENT DOOR AFTER PUSHBACK DEFERRED INDICATION OF LEFT FWD CREW ENTRY DOOR IAW MEL 52-71-1-1A. DMP CW. PLACARD INSTALLED. DOOR CLOSED AND LOCKED. - [SDR IPXA2024102874483](https://openairdocs.org/sdr/IPXA2024102874483), Oct 26, 2024: DRAIN. INOPERATIVE. FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R). ACCOMPLISHED EO-82173-JIC001. - [SDR IPXA2024102139954](https://openairdocs.org/sdr/IPXA2024102139954), Oct 20, 2024: DRAIN. NONE. (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R). C/W EO-82173. - [SDR IPXA2024102854364](https://openairdocs.org/sdr/IPXA2024102854364), Oct 16, 2024: FLOOR PANEL. BROKEN. BROKEN AND DENT - FOUND M/D FLOOR PNL BROKEN AND DENT AT STA 830 TO STA 933 LBL-58 P/N:145T5876-57 (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 - [SDR IPXA2024102850376](https://openairdocs.org/sdr/IPXA2024102850376), Oct 16, 2024: BUMPER. DAMAGED. FOUND THE CREW ENTRY DOOR FORWARD DOORWAY LINING BUMPER WITH BROKEN DAMAGE. (REPLACE). REPLACE DOORWAY LINING BUMPER I.A.W AMM 52-12-02-004-001 REV.143 AND AMM - [SDR IPXA2024102850625](https://openairdocs.org/sdr/IPXA2024102850625), Oct 16, 2024: BEAR STRAP. CRACKED. FOUND CRACK ON THE NO.1 FORWARD ENTRY DOOR AFT LOWER CORNER BEAR STRIP. (REPAIR). REMOVE ADJACENT FASTENERS AROUND CRACKED HOLE TO SEPARATE STRUCTURE I.A.W SRM - [SDR IPXA2024101848858](https://openairdocs.org/sdr/IPXA2024101848858), Oct 16, 2024: SKIN. DEBONDED. FOUND DISBOND AT NO.10 SPOILER UPPER SURFACE. (REPAIR). I.A.W AMM 20-11-00-910-802 REV.143 INSTALLED THE #10 SPOILER INBOARD SEAL. - [SDR IPXA2024102453236](https://openairdocs.org/sdr/IPXA2024102453236), Oct 16, 2024: ANGLE. CRACKED. THE ANGLE OF BULK CARGO COMPARTMENT RIGHT AREA WITH CRACK AT STA 1578 RBL 60. (REPLACE). I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.143 INSTALLED M - [SDR IPXA2024102453299](https://openairdocs.org/sdr/IPXA2024102453299), Oct 16, 2024: ANGLE. CRACKED. THE ANGLE OF BULK CARGO COMPARTMENT LEFT AREA WITH CRACK AT STA 1578 LBL 60. (REPLACE). I.A.W AMM 25-59-01-404-019 REV.143 INSTALL MAIN DECK CARGO DADO PANEL AN - [SDR IPXA2024102453912](https://openairdocs.org/sdr/IPXA2024102453912), Oct 16, 2024: DOUBLER. CRACKED. CRACK ON DOUBLER COMMON TO BULKHEAD FWD SIDE AT STA 1809, LBL 28.5. (EVALUATE). I.A.W AMM 20-10-09-404-007 REV 143 DO A LEAK CHECK TEST FOR THE HYDRAULIC TUBE, - [SDR IPXA2024101753946](https://openairdocs.org/sdr/IPXA2024101753946), Oct 16, 2024: FLOOR PANEL. DAMAGED. BROKEN AND DENT - FOUND M/D FLOOR PNL BROKEN AND DENT AT STA-930 TO STA 973 LBL-65 (P/N: 145T5876-79) (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ - [SDR IPXA2024101754022](https://openairdocs.org/sdr/IPXA2024101754022), Oct 16, 2024: FLOOR PANEL. DAMAGED. BROKEN AND DENT - FOUND M/D FLOOR PNL BROKEN AND DENT AT STA 930 TO STA 973 LBL-44 (P/N: 145T5876-80) (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ - [SDR IPXA2024101754094](https://openairdocs.org/sdr/IPXA2024101754094), Oct 16, 2024: FLOOR PANEL. DAMAGED. BROKEN AND DENT - FOUND FLOOR PNL BROKEN AND DENT AT STA 930 STA 973 LBL-33 (P/N: 145T5876-81) (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV - [SDR IPXA2024101754323](https://openairdocs.org/sdr/IPXA2024101754323), Oct 16, 2024: FLOOR PANEL. DAMAGED. BROKEN AND DENT - FOUND FLOOR PNL BROKEN AND DENT AT STA 977 TO STA 1107 LBL 11 TO RBL-11 P/N:145T5876-73 (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693 - [SDR IPXA2024101753124](https://openairdocs.org/sdr/IPXA2024101753124), Oct 16, 2024: FLOOR PANEL. DAMAGED. FOUND THE MAIN DECK CARGO FLOOR PANEL DENT AND BROKEN, P/N: 141T5856-3. (REPAIR). I.A.W AMM 53-01-06-400-801 REV.143 INSTALL MAIN DECK CARGO FLOOR PANEL AND CON - [SDR IPXA2024101753985](https://openairdocs.org/sdr/IPXA2024101753985), Oct 16, 2024: FLOOR PANEL. DAMAGED. DENT AND BROKEN - FOUND M/D FLOOR PNL DENT AND BROKEN AT STA 742 TO STA 830 LBL-11 TO RBL-11, 145T5876-68. (REPAIR). .FABRICATE A NEW FLOOR PANEL I.A.W. SREO-96 - [SDR IPXA2024101753968](https://openairdocs.org/sdr/IPXA2024101753968), Oct 16, 2024: FLOOR PANEL. DAMAGED. BROKEN AND DENT - FOUND M/D FLOOR PNL BROKEN AND DENT AT STA 933 TO STA 984 LBL-85 (P/N: 145T5876-78) (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ - [SDR IPXA2024101754052](https://openairdocs.org/sdr/IPXA2024101754052), Oct 16, 2024: FLOOR PANEL. DAMAGED. DENT AND BROKEN - FOUND M/D FLOOR PNL DENT AND BROKEN AT STA 977 TO STA 1087 LBL 81 P/N: 145T5876-22. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ - [SDR IPXA2024101754018](https://openairdocs.org/sdr/IPXA2024101754018), Oct 16, 2024: FLOOR PANEL. DAMAGED. DENT AND BROKEN - FOUND M/D FLOOR PNL DENT AND BROKEN AT STA 742 TO STA 830, LBL-65 P/N: 145T5876-63 (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ0 - [SDR IPXA2024101754133](https://openairdocs.org/sdr/IPXA2024101754133), Oct 16, 2024: FLOOR PANEL. DAMAGED. BROKEN AND DEND - FOUND M/D FLOOR PNL DENT AND BROKEN AT STA 977 TO STA 1107 LBL-22 P/N: 145T5876-72. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ - [SDR IPXA2024101754163](https://openairdocs.org/sdr/IPXA2024101754163), Oct 16, 2024: FLOOR PANEL. DAMAGED. DENT AND BROKEN - FOUND M/D FLOOR PNL BROKEN AND DENT AT STA 977 TO STA 1043 RBL-45 (P/N: 145T5876-75) (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-RE - [SDR IPXA2024101754176](https://openairdocs.org/sdr/IPXA2024101754176), Oct 16, 2024: FLOOR PANEL. DAMAGED. BROKEN AND DENT - FOUND M/D FLOOR PNL BROKEN AND DENT AT STA 977 TO STA 1043 LBL-45 (P/N: 145T5876-71) (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-RE - [SDR IPXA2024101754263](https://openairdocs.org/sdr/IPXA2024101754263), Oct 16, 2024: FLOOR PANEL. DAMAGED. BROKEN AND DENT - FOUND M/D FLOOR PNL BROKEN AND DENT AT STA 977 TO STA 1109 RBL-22 P/N: 145T5876-74. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ - [SDR IPXA2024101754332](https://openairdocs.org/sdr/IPXA2024101754332), Oct 16, 2024: FLOOR PANEL. DAMAGED. BROKEN AND DENT - FOUND M/D FLOOR PNL BROKEN AND DENT AT STA 930 TO STA 977 RBL-81 P/N:145T5876-84 (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 - [SDR IPXA2024101754364](https://openairdocs.org/sdr/IPXA2024101754364), Oct 16, 2024: FLOOR PANEL. DAMAGED. FAULT - BROKEN AND DENT - FOUND M/D FLOOR PNL BROKEN AND DENT AT STA 830 TO STA 933 LBL-58. (REPAIR) OK TO WORK - [SDR IPXA2024101650376](https://openairdocs.org/sdr/IPXA2024101650376), Oct 16, 2024: BUMPER. DAMAGED. FOUND THE CREW ENTRY DOOR FORWARD DOORWAY LINING BUMPER WITH BROKEN DAMAGE. (REPLACE) OK TO WORK. - [SDR IPXA2024102428366](https://openairdocs.org/sdr/IPXA2024102428366), Oct 15, 2024: HINGE FITTING. CRACKED. CRACKED SUPPORT RIB RIGHT WING NO : 10 SPOILER INBOARD SUPPORT RIB (REPLACE). I.A.W AMM 27-61-02-424-023 REV.143 AND AMM 27-61-00-825-072 REV.143 ADJUST THE NO. - [SDR IPXA2024101727357](https://openairdocs.org/sdr/IPXA2024101727357), Oct 15, 2024: FLOOR PANEL. DENTED. FOUND MAIN DECK CARGO FLOOR PANEL DENT, P/N:453T7025-12 (REPAIR). .I.A.W AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 AND AMM 25-58-04-404-015 AND AMM 25-58-05 - [SDR IPXA2024091627017](https://openairdocs.org/sdr/IPXA2024091627017), Aug 18, 2024: SEAL DEPRESSOR. DAMAGED. FWD CARGO DOOR SEAL DEPRESSOR UPPER AFTER WITH DAMAGE, DENT, SCRATCH AND HOLE. MATCH DRILLED SEAL DEPRESSOR PER EXAMPLE & INSTALLED SEAL DEPRESSOR IAW SRM-51-40 - [SDR IPXA2024081827017](https://openairdocs.org/sdr/IPXA2024081827017), Aug 18, 2024: SEAL DEPRESSOR. DAMAGED. FWD CARGO DOOR SEAL DEPRESSOR UPPER AFTER WITH DAMAGE, DENT, SCRATCH AND HOLE SREO-8088-REQ001 ((APPX A) INTERIM REPAIR: B767: CARGO DOOR SEAL DEPRESSORS AND AD - [SDR IPXA2024021835530](https://openairdocs.org/sdr/IPXA2024021835530), Feb 18, 2024: FLOOR PANEL. DAMAGED. *MAJOR REPAIR* ( SHEET -METAL EVAL ) - POSITION 7C - MCD FLOOR BOARD ( DAMAGED UPON REMOVAL REMOVAL. AFT LH FASTENER INSERT ( MARKED WITH TAPE. UNDERSIDE FWD PA - [SDR IPXA2024021862362](https://openairdocs.org/sdr/IPXA2024021862362), Nov 1, 2023: FLOOR PANEL. DAMAGED. *MAJOR REPAIR* MAIN CARGO DECK FLOOR PANEL DAMAGED AT POS 2R. DAMAGE AT AFT END OF PANEL WHERE LONG GUIDE ASSY ATTACHES.***SM13/LMX8*** INSTALLED MCD FLOOR BOAR - [SDR IPXA2023103026500](https://openairdocs.org/sdr/IPXA2023103026500), Oct 30, 2023: FLOOR PANEL. UNKNOWN. MAIN CARGO DECK CENTER FLOOR PANEL BETWEEN POSITION 10 AND 11 DAMAGED INSTALLED FLOOR PANEL IAW AMM 53€“01-06 - [SDR IPXA2023112923402](https://openairdocs.org/sdr/IPXA2023112923402), Oct 29, 2023: PANEL. DAMAGED. **SUPPLEMENTAL SDR**LH SIDE OF FUSELAGE AFT OF ADP EXHAUST PANEL 195PL DAMAGED***SM40/LMX10***AWP REQ#471333*** COMPLIED WITH EO. 88576 REQ 2, REFERENCE BARCODE - [SDR IPXA2023110621193](https://openairdocs.org/sdr/IPXA2023110621193), Oct 29, 2023: UNKNOWN. DAMAGED. *** SUPPLEMENTAL SDR *** MAIN DECK CARGO COMPARTMENT FLOOR FITTING SEAT TRACK CROWN LIP DAMAGE POS 7C C/W SREO-44173-REQ001 FOR LOCK.213 POS 7C REF. (T3F18E0037 - [SDR IPXA2023110618262](https://openairdocs.org/sdr/IPXA2023110618262), Oct 29, 2023: UNKNOWN. DAMAGED. *** SUPPLEMENTAL SDR *** MAIN DECK CARGO COMPARTMENT FLOOR FITTING SEAT TRACK CROWN LIP DAMAGE POS 11L/11R INSTALLED NEW FITTINGVAT POSITION 11L/11R IAW AMM 20- - [SDR IPXA2023103021193](https://openairdocs.org/sdr/IPXA2023103021193), Oct 29, 2023: UNKNOWN. UNKNOWN. MAIN DECK CARGO COMPARTMENT FLOOR FITTING SEAT TRACK CROWN LIP DAMAGE POS 7C. OPEN - [SDR IPXA2023103018262](https://openairdocs.org/sdr/IPXA2023103018262), Oct 29, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* MAIN DECK CARGO COMPARTMENT FLOOR FITTING SEAT TRACK CROWN LIP DAMAGE POS 11L/11R INSTALLED NEW FITTINGVAT POSITION 11L/11R IAW AMM 20-11-00 - [SDR IPXA2023103000402](https://openairdocs.org/sdr/IPXA2023103000402), Oct 29, 2023: UNKNOWN. UNKNOWN. LH SIDE OF FUSELAGE AFT OF ADP EXHAUST PANEL 195PL DAMAGED ASSIGNED EO-88576-REQ1 FOR TEMPORARY REPAIR. OPEN - [SDR IPXA2023100256128](https://openairdocs.org/sdr/IPXA2023100256128), Sep 6, 2023: SKIN. DAMAGED. SKIN BUBBLING L SIDE OF FUSELAGE AFT OF ADP EXHAUST. DRILLED, TRIMMED AND COUNTERSUNK NEW PANEL PER SRM 51-40-02-0G-0. STARTED INSTALLATION PER AMM 53-52-01. CO - [SDR IPXA2023090656128](https://openairdocs.org/sdr/IPXA2023090656128), Sep 6, 2023: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** SKIN BUBBLING L SIDE OF FUSELAGE AFT OF ADP EXHAUST REMOVED AFT LOWER FUSELAGE PANEL 195PL REF B767 AMM 53-52-01 AND ROUTED TO SHEETMETAL - [SDR IPXA2023081564054](https://openairdocs.org/sdr/IPXA2023081564054), Aug 11, 2023: ENGINE. SURGES. AIR TURNBACK L ENG SURGING AIRCRAFT YAWING N2 SURGING. CONTINUED WITH ENG RUNNING. LANDED ONT (+/- 10% N2 REPEATEDLY ON CLIMBOUT ) COMPLETED MPA TEST PER TASK 7 - [SDR IPXA20230811054](https://openairdocs.org/sdr/IPXA20230811054), Aug 11, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* AIR TURNBACK L ENG SURGING AIRCRAFT YAWING N2 SURGING. CONTINUED WITH ENG RUNNING. LANDED ONT (+/- 10% N2 REPEATEDLY ON CLIMBOUT ) - [SDR IPXA2023082356388](https://openairdocs.org/sdr/IPXA2023082356388), Jun 29, 2023: DOOR. FAILED. RIGHT NOSE GEAR DOOR FAILED TO RETRACT. INSTALLED NLG DOOR STRUT ASSEMBLY WRT AMM 32-22-02. RIGGED AS REQD AND PERFORMED FUNCTIONAL CHECK WRT 32-22-02. NO DEFEC - [SDR IPXA2023042216071](https://openairdocs.org/sdr/IPXA2023042216071), Apr 18, 2023: SHEAR WEB. CORRODED. FAULT - SHEAR WEB CORR FRS 470/510 & LBL 11.0/33.0 DISPLACED 2 CEILING PANELS IN FWD CARGO PIT LOWER FRS 470 AND FRS 510 FOR ACCESS IAW SRM 51-40-02. REMOVED SH - [SDR IPXA2023042263672](https://openairdocs.org/sdr/IPXA2023042263672), Apr 15, 2023: SHEAR WEB. CORRODED. FAULT - SHEAR WEB CORROSION STA 280, RBL 18- RBL 28 REMOVED FASTENERS (50EA) AT MAIN CARGO FWD FLOOR PAN SHEAR WEB STA 280 BETWEEN RBL 18 TO RBL 28 IAW B767 SRM - [SDR IPXA2023021691040](https://openairdocs.org/sdr/IPXA2023021691040), Feb 15, 2023: DOOR. NONE. L FWD ENTRY DOOR EICAS ILLUMINATED FOR 3 SECONDS THE EXTINGUISHED DURING PUSHBACK. EACH FLT REINSPECT- CREW ENTRY DOOR INDICATING SYSTEM - ALL DOOR EXCEPT MAIN - [SDR IPXA2023013190452](https://openairdocs.org/sdr/IPXA2023013190452), Jan 27, 2023: FLOOR PANEL. NONE. INSPECTION TYPE:C13*MAJOR REPAIR* BROKEN DAMAGE ON MAIN DECK FLOOR PANEL (PANEL NO.:231KFF, PN:143T5876-89) BETWEEN STA 554 AND 654+22 AND BETWEEN LBL 77 AND 88 - [SDR IPXA2023020390561](https://openairdocs.org/sdr/IPXA2023020390561), Jan 19, 2023: SKIN. CRACKED. INSPECTION TYPE:C13*MAJOR REPAIR* CRACK ON NOSE SKIN (P/N:114T4104-4) OF NO.9 SLAT AT OSS 572.55REPAIR I.A.W 767-300F SRM 57-43-01-2R-2 REV.85.01. All 169: https://openairdocs.org/aircraft/N319UP/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.