# N317UP: 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: 27745
- Year built: 1997
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 8, 1997
- Certificate issued: July 10, 1997
- Expires: November 30, 2027
- Mode S code: A362A2
- 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=317UP
- Page: https://openairdocs.org/aircraft/N317UP

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/N317UP/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 N317UP.

## FAA accident and incident reports

None matched to N317UP.

## Service difficulty reports (152, 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 IPXA2026070872957](https://openairdocs.org/sdr/IPXA2026070872957), Jun 26, 2026: SUPPORT BEAM. CORRODED. LEFT MLG SUPPORT BEAM ASSY OUTER BUSHING OF AFT TRUNNION BEARING HAS CORROSION ON LOWER EDGE. INSTALLED OUTER BUSHING P/N 113T1108-33SAAU AT LH MLG BEAM ASSY IA
- [SDR IPXA2026070774298](https://openairdocs.org/sdr/IPXA2026070774298), Jun 26, 2026: FITTING. CORRODED. RIGHT WING REAR SPAR, OUTBOARD SUPPORT OF TRUNNION BEARING HAS CORROSION ON O/B AND LOWER SPOT FACE, FLL-003, ACCOMPLISHED INSTRUCTIONS PER EO-97989-REQ1 AND EA
- [SDR IPXA2026033071018](https://openairdocs.org/sdr/IPXA2026033071018), Mar 20, 2026: WEB. CORRODED. CORROSION, AFT CARGO BALL PANEL AND FLOOR STRUCTURE FAYING SURFACE STA 1197+132 ~ 1219 RBL 40 ~ 50. (AGING A/C INSPECTION) (NO. 2868) (EVALUATE) INSTALL FAB WEB
- [SDR IPXA2026032975575](https://openairdocs.org/sdr/IPXA2026032975575), Mar 20, 2026: PLATE. CRACKED. FOUND THE PLATE ON SIDE GUIDE RAIL WITH CRACK DAMAGE AT BS 1219, LEFT SIDE IN AFT CARGO COMPARTMENT. INSTALLED NEW TIE PLATE IAW SRM 51-40-02-0G, REV 94, & AIPC
- [SDR IPXA2026032776354](https://openairdocs.org/sdr/IPXA2026032776354), Mar 20, 2026: RECEPTACLE. WORN. WORN RECEPTACLE, NR 2 ENGINE NOSE COWL EXTERNAL MID LOWER OUTER SKIN AT 6 O'CLOCK. INSTALLED A NEW RECEPTACLE IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-11-16 
- [SDR IPXA2026032978429](https://openairdocs.org/sdr/IPXA2026032978429), Mar 20, 2026: DEPRESSOR. CHAFED. CHAFING & DEFORM - FRAME , MAIN DECK CARGO DOOR CUTOUT AREA & AFT SIDE. INSTALL NUTPLATES ON NEW DEPRESSOR IAW SRM 51-40-02-0G REV. 94 AND DWG 143T1008, SHT, 11
- [SDR IPXA2026032675990](https://openairdocs.org/sdr/IPXA2026032675990), Mar 20, 2026: SKIN. CRACKED. CRACKED SKIN, LT WING FLAP FAIRING NR 3 AFT EDGE. PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2" HEATED AREA, PER NDT MANUAL PART 1 51-01-01 REV:143. NO DEFEC
- [SDR IPXA2026033051174](https://openairdocs.org/sdr/IPXA2026033051174), Mar 19, 2026: BRACKET. CORRODED. GOUGED BRACKET, LT WING T/E LOWER SURFACE WBL 289. ACCOMPLISHED GOUGE AND CORROSION DAMAGE REPAIR IAW EO-96933-REQ1, REV 1, & SRM 51-40-02-0G, REV 94, DWG 113T1
- [SDR IPXA2026032052387](https://openairdocs.org/sdr/IPXA2026032052387), Mar 19, 2026: REPAIR. DEBONDED. MAJOR REPAIR, DEBONDED, PREVIOUS REPAIR, L/H WING NO.5 SLAT UPPER SURFACE LES 440. CUT OUT THE DAMAGE MATERIALS AND CLEAN, MEASURE THE CUTOUT SIZE (L:5.75", W:5
- [SDR IPXA2026033158453](https://openairdocs.org/sdr/IPXA2026033158453), Mar 19, 2026: DOOR. DAMAGED. THE DESCENT DEVICE CONTAINER DOOR IS CRACKED. REPAIRED THE LID ASSY IAW EO-96902-REQ1, REV 2.
- [SDR IPXA2026032252574](https://openairdocs.org/sdr/IPXA2026032252574), Mar 19, 2026: REPAIR. DEBONDED. DEBONDED PREVIOUS REPAIR, LT WING NR 5 SLAT UPPER SURFACE LES 500. INSTALL THE EXTERNAL DOUBLER WITH FILM ADHESIVE IAW SRM 51-70-10-2R-0 PARAGRAPH 10 & 18 REV. 
- [SDR IPXA2026032456367](https://openairdocs.org/sdr/IPXA2026032456367), Mar 19, 2026: ANGLE. CRACKED. FOUND ANGLE CRACK AT ENTRY DOOR SCUFF PLATE. INSTALLED NEW CLIP ASSY I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO. 141T8310 SH. 4 REV. H.
- [SDR IPXA2026032053114](https://openairdocs.org/sdr/IPXA2026032053114), Mar 19, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 1 ENG RT THRUST REVERSER FWD LWR CLOSURE DOOR T/E AREA. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND IPC 78-32-22, REV 94.
- [SDR IPXA2026032056184](https://openairdocs.org/sdr/IPXA2026032056184), Mar 19, 2026: BRACKET. CHAFED. CHAFED BRACKET, NR 2 ENGINE RT THRUST REVERSER FWD LOWER CLOSEOUT INNER TRAILING EDGE. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV. 94 AND IPC 78-32-22 REV. 9
- [SDR IPXA2026032057534](https://openairdocs.org/sdr/IPXA2026032057534), Mar 19, 2026: BRACKET. CRACKED. CRACKED SUPPORT, RT WING L/E INBD PANEL 611KB, TORQUE SUPPORT LES 281. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 94, AND DWG 114T1240, SH 4, REV D.
- [SDR IPXA2026032058453](https://openairdocs.org/sdr/IPXA2026032058453), Mar 19, 2026: DOOR. CRACKED. THE DESCENT DEVICE CONTAINER DOOR IS CRACKED. (REPLACE) OK TO WORK.
- [SDR IPXA2026032831078](https://openairdocs.org/sdr/IPXA2026032831078), Mar 18, 2026: ANGLE. DAMAGED. DAMAGED ANGLE, NR 2 NACELLE AFT SKIRT FAIRING INNER RT, 4TH HINGE FITTING.. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 94, & DWG 313T3310, SHEET 1, REV L.
- [SDR IPXA2026032331814](https://openairdocs.org/sdr/IPXA2026032331814), Mar 18, 2026: CLAMP. BROKEN. BROKEN CLAMP , NR 1 PYLON AFT FAIRING INNER HOLD OPEN ROD SUPPORT BRACKET AREA. INSTALLED A NEW CLAMP IAW SRM 51-40-02-0G, REV 94, & DWG 313T3349, SH 2, REV B.
- [SDR IPXA2026032332844](https://openairdocs.org/sdr/IPXA2026032332844), Mar 18, 2026: BEAM. CRACKED. CRACKED BEAM , NR 2 NACELLE AFT LOWER FAIRING RT UPPER UNDER THE 4TH LATCH FITTING AT NAC STA 373. INSTALLED A NEW BEAM IAW SRM 51-40-02-0G, REV 94 AND DWG 313T
- [SDR IPXA2026032331943](https://openairdocs.org/sdr/IPXA2026032331943), Mar 18, 2026: ANGLE. CRACKED. CRACKED ANGLE, NR 2 PYLON AFT LOWER FAIRING INNER FWD BULKHEAD LT REAR MID. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 94, & DWG 313T3380, SH 3, REV F.
- [SDR IPXA2026032010352](https://openairdocs.org/sdr/IPXA2026032010352), Mar 17, 2026: HINGE FITTING. CRACKED. CRACKED SKIN, RT WING T/E NR 10 SPOILER INBD LWR FITTING. REPLACED DAMAGED FITTING IAW SRM 51-40-02-0G, REV 94, & DWG 112T1000, SH 14, REV B, 113T1422, SH 1, RE
- [SDR IPXA2026082593903](https://openairdocs.org/sdr/IPXA2026082593903), Mar 16, 2026: PAWL. WORN. HE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. (REPLACE) REPLACED THE PAWL I.A.W AMM 52-11-26-004-001 REV.147 AND AMM 52-11-26-404-003 REV.147.TORQ
- [SDR IPXA2026032591928](https://openairdocs.org/sdr/IPXA2026032591928), Mar 16, 2026: SKIN. CRACKED. CRACKED FWD ENTRY DOOR LT AFT LOWER CORNER SKIN. ACCOMPLISH THE REPAIR IAW EO-87307-REQ7, REV 2, & SRM 53-10-01-2R-1, REV 130, AND EGAT WORK SHEET 60160.
- [SDR IPXA2026031793903](https://openairdocs.org/sdr/IPXA2026031793903), Mar 16, 2026: PAWL. WORN. THE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. OPEN
- [SDR IPXA2026020667134](https://openairdocs.org/sdr/IPXA2026020667134), Jan 31, 2026: LANDING GEAR. FAULTED. EMERGENCY DECLARED, NOSE GEAR WOULD NOT COME DOWN AFTER !0 MIN WITH GEAR HANDLE IN THE DOWN POSITION MANUALLY DEPLOYED GEAR EXT PER QRH. CENTER HYD SYSTEM ADP F
- [SDR IPXA2026020558217](https://openairdocs.org/sdr/IPXA2026020558217), Jan 30, 2026: WIRE. CHAFED. LEFT FWD ENTRY DOOR EICAS MSG ON PUSHBACK FOUND WIRE ON SWITCH S194 CHAFED. REMOVED AND REPLACED CREW ENTRY DOOR SWITCH S194 IAW B767 AMM 52-71-01 AND SWPM 20-3
- [SDR IPXA2026013058217](https://openairdocs.org/sdr/IPXA2026013058217), Jan 30, 2026: WARNING MESSAGE. ILLUMINATED. LEFT FWD ENTRY DOOR EICAS MESSAGE ON PUSH BACK, DMP C/W IAW MEL 52-71-1-1A.
- [SDR IPXA2025073083108](https://openairdocs.org/sdr/IPXA2025073083108), Jul 29, 2025: WINDOW. CRACKED. DIVERSION, L1 WINDOW CRACKED. REPLACED WINDSHIELD IAW AMM 56-11-01-404-017 REV 145. LEAK AND OPS CHECKED SATIS.
- [SDR IPXA2025032162167](https://openairdocs.org/sdr/IPXA2025032162167), Mar 20, 2025: LIGHT. INOPERATIVE. FOUND EMERGENCY LIGHT INOP. FOUND BATTERY PACK DRAINED, R/R EMERGENCY EXIT LIGHT BATTERY PACK IAW AMM 33-51-07/201. OPS TEST SATIS.
- [SDR IPXA2025031479934](https://openairdocs.org/sdr/IPXA2025031479934), Mar 11, 2025: WARNING MESSAGE. FALSE ACTIVATION. EICAS L SIDE WINDOW. PERFORMED QRH PROCEDURE AND LIGHT EXTINGUISHED OPS CONT'D NORMAL PERFORMED BITE TEST PER FIM 30-41 FAULT TREE 804, NO FAULT NOTED. AIRCRAFT
- [SDR IPXA2024040886820](https://openairdocs.org/sdr/IPXA2024040886820), Mar 27, 2024: HINGE. DEFORMED. FOUND MAIN ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY DEFORM I.A.W AMM 52-12-02-404-025 REV.141 INSTALL DOORWAY LINING. I.A.W AMM 20-10-13-964-001 REV.141 REPLA
- [SDR IPXA2024040287451](https://openairdocs.org/sdr/IPXA2024040287451), Mar 27, 2024: ANGLE. CRACKED. CRACK - ANGLE BULK CARGO COMPARTMENT NEAR STA 1578 LBL 60 (REPLACE) 1.I.A.W AMM 53-01-06-400-801 REV.141 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK
- [SDR IPXA2024032786820](https://openairdocs.org/sdr/IPXA2024032786820), Mar 27, 2024: HINGE. DEFORMED. FOUND MAIN ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY DEFORM (REPLACE) OKAY TO WORK
- [SDR IPXA2024032853897](https://openairdocs.org/sdr/IPXA2024032853897), Mar 25, 2024: NONE. NONE. FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. ACCOMPLISHED SDR.
- [SDR IPXA2024032653856](https://openairdocs.org/sdr/IPXA2024032653856), Mar 25, 2024: STIFFENER. CRACKED. STIFFENER CENTER WING FRONT SPAR CRACK IN STIFFENER AT STA 785.9 LBL55(REPAIR) ACCOMPLISHED REPAIR I.A.W SRM 57-10-10-2R-2 REV.88 AND EGAT WORK SHEET NO.40286 A
- [SDR IPXA2024032653897](https://openairdocs.org/sdr/IPXA2024032653897), Mar 25, 2024: NONE. NONE. FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R.
- [SDR IPXA2024032653813](https://openairdocs.org/sdr/IPXA2024032653813), Mar 25, 2024: SKIN. CRACKED. CRACK - SKIN, FWD LOWER FACE OF L/H WING NO.5 SLAT L/E NOSE SKIN, NEAR OUTBD TRACK AREA OSS 492.953.(REPAIR) REPAIR DAMAGE AREA I.A.W SRM 57-43-01-2R-2 REPAIR 2
- [SDR IPXA2024022287752](https://openairdocs.org/sdr/IPXA2024022287752), Feb 21, 2024: WINDOW. CRACKED. L2 WINDOW HAS CRACK IN LOWER AFT CORNER. FLIGHT CREW FOUND PRIOR TO PRE FLIGHT. C/W REMAINING STEPS OF #2 L/H SLIDING WINDOW INSTALL MM 56-11-02.
- [SDR IPXA2022040380794](https://openairdocs.org/sdr/IPXA2022040380794), Apr 3, 2022: NONE. FAILED. INSPECTION TYPE:NA**ATB** LEFT AFT FUEL PUMP FAILED 50 MINS AFTER TAKEOFF. CB POPPED. LEFT FORWARD FUEL PUMP FAILED 1:30 AFTER TAKEOFF. CB POPPED.LEFT AFT FUEL 
- [SDR IPXA2022032280362](https://openairdocs.org/sdr/IPXA2022032280362), Mar 14, 2022: SKIN. CORRODED. INSPECTION TYPE:C13CORROSION ON INNER SKIN OF BULK CARGO DOOR AFT LOWER CORNER AREA AT STA 1457.REPAIR I.A.W 767-300F SRM 52-30-01-1A DETAIL VII,REV.82.01.
- [SDR IPXA2022030979915](https://openairdocs.org/sdr/IPXA2022030979915), Mar 8, 2022: DOOR. NONE. INSPECTION TYPE:NAENTRY DOOR CAPTURE LEVER CAN NOT BE CLOSED FROM INSIDE CABIN, ONLY FROMEXTERIOR BY MECHANIC-WX WERE ABLE TO CLOSE IT FROM INSIDE W/MUCH DIFFIC
- [SDR IPXA2021050268878](https://openairdocs.org/sdr/IPXA2021050268878), May 2, 2021: LAMP. INOPERATIVE. INSPECTION TYPE:N/AOUTSIDE EMERGENCY LIGHT INOPERATIVE. RELAMPED OUTSIDE EMERGENCY LIGHT I/A/W AMM 33-51-16 OPS CHECK GOOD
- [SDR IPXA2021021165580](https://openairdocs.org/sdr/IPXA2021021165580), Feb 11, 2021: PROXIMITY SWITCH. MALFUNCTIONED. INSPECTION TYPE:N/A**ATB - SUPPLEMENTAL SDR - NO EMERG DECLARED - NO EMERG EQUIP USED - LANDED W/OUT INCIDENT** STATUS MESSAGE LANDING GEAR MONITOR. FOUND RT NO
- [SDR IPXA2020122963918](https://openairdocs.org/sdr/IPXA2020122963918), Dec 28, 2020: WARNING MESSAGE. FALSE ACTIVATION. INSPECTION TYPE: N/A, DIVERSION, NO EMERGENCY DECLARED. DURING ARRIVAL BOTH "LT & RT ENGINE AI VALVE" MESSAGES OCCURED. MESSAGES CLEARED BY THEMSELVES BUT RE-AP
- [SDR IPXA2020080328542](https://openairdocs.org/sdr/IPXA2020080328542), Aug 2, 2020: SKIN. DAMAGED. LEFT OTBD ELEVATOR UPPER SKIN DAMAGED 25.25", OTBD AND 10.25" FWD OF T/E. REPAIRED IAW B767-5520-77296.
- [SDR IPXA2020031853259](https://openairdocs.org/sdr/IPXA2020031853259), Mar 6, 2020: SKIN. CRACKED. INSPECTION TYPE:C12CRACK ON L/E SKIN OF #8 SLAT NEAR OSS 592.95.REPAIR I.A.W 767-300F SRM 57-43-01-2R-2 REV.76.01
- [SDR IPXA2020031853258](https://openairdocs.org/sdr/IPXA2020031853258), Mar 6, 2020: SKIN. CRACKED. INSPECTION TYPE:C12CRACK ON L/E SKIN OF #4 SLAT NEAR OSS 607.REPAIR I.A.W 767-300F SRM 57-43-01-2R-2 REV.76.01
- [SDR IPXA2020031853257](https://openairdocs.org/sdr/IPXA2020031853257), Mar 6, 2020: SKIN. CRACKED. INSPECTION TYPE:C12CRACK ON L/E SKIN OF #9 SLAT NEAR OSS 572.55.REPAIR I.A.W 767-300F SRM 57-43-01-2R-2 REV.76.01
- [SDR IPXA2020031853291](https://openairdocs.org/sdr/IPXA2020031853291), Mar 6, 2020: STIFFENER. CRACKED. INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER (P/N : 111T2008-12) ON STA 785.9 , RBL 33REPAIR I.A.W 767-300F SRM 5710-10-2R-2 REPAIR 2 REV.76.01 , UPS 
- [SDR IPXA2020031853290](https://openairdocs.org/sdr/IPXA2020031853290), Mar 6, 2020: STIFFENER. CRACKED. INSPECTION TYPE:C12CRACK ON CENTER WING TANK STIFFENER (P/N : 111T2008-11) ON STA 785.9 , LBL 33REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.76.01 , UPS

All 152: https://openairdocs.org/aircraft/N317UP/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

## Earlier aircraft with N317UP

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N317UP before.

- [Cancelled 1974-04-19](https://openairdocs.org/deregistered/N317UP-1974-04-19): Cessna 182L, S/N 18259297. Exported to Canada. Owner: [Kerrville Flying Service Inc](https://openairdocs.org/faa-owner/KERRVILLE%20FLYING%20SERVICE%20INC), [Kerrville, TX](https://openairdocs.org/faa-place/TX/Kerrville)

## Related

- Other Boeing 767-34AF aircraft: https://openairdocs.org/model/boeing-767-34af/aircraft.md
- The GE CF6-80 series engine: https://openairdocs.org/engine/ge-cf6-80-series.md

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