# N318UP: 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: 27746
- Year built: 1997
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 18, 1997
- Certificate issued: September 22, 1997
- Expires: May 31, 2028
- Mode S code: A36659
- 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=318UP
- Page: https://openairdocs.org/aircraft/N318UP

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/N318UP/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 N318UP.

## FAA accident and incident reports

None matched to N318UP.

## Service difficulty reports (125, 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 IPXA2026093083485](https://openairdocs.org/sdr/IPXA2026093083485), Aug 23, 2026: DRAG BRACE. CORRODED. AFTER OTBD BUSHING REMOVAL, FOUND PITTING CORROSION ON CHAMFER FACE OF RT MLG FORWARD DRAG BRACE FITTING, AT WS 240 REAR SPAR, INSTALL NEW SERVICABLE BUSHINGS A
- [SDR IPXA2026050999461](https://openairdocs.org/sdr/IPXA2026050999461), May 9, 2026: LENS. DETACHED. FLIGHT DECK EMERGENCY EXIT SIGN LENS DOES NOT REMAIN SECURED (FALLS OFF WHEN DOOR CLOSES/FOUND ON FLOOR WHEN ENTERING AIRCRAFT) REMOVED AND REPLACED EMERGENCY E
- [SDR IPXA2026032073759](https://openairdocs.org/sdr/IPXA2026032073759), Mar 20, 2026: ARMING LEVER. INOPERATIVE. MAIN ENTRY SERVICE DOOR (L1), DOOR ARMING LEVER WILL NOT ARM UNLESS DOOR IS SLAMMED CLOSED. PERFORMED CREW ENTRY DOOR SYSTEM TEST IAW AMM 52-12-00. COULD NOT DU
- [SDR IPXA2026031354595](https://openairdocs.org/sdr/IPXA2026031354595), Mar 13, 2026: DOOR. BINDING. MAIN ENTRY DOOR LEVER WILL NOT CLOSE WHEN DOOR IS SHUT. FOUND EXTERIOR DOOR HANDLE NOT FLUSH WHEN DOOR IS CLOSED. CLEANED DEBRIS FROM EXTERIOR DOOR HANDLE PAWL 
- [SDR IPXA2026030514435](https://openairdocs.org/sdr/IPXA2026030514435), Mar 4, 2026: DOOR. FOD. COULD NOT SECURE THE YELLOW DOOR ARMING LEVER. CLEANED DEBRI OPS CK NORM IAW 52-12-00 NO DEFECTS NOTED
- [SDR IPXA2025060250870](https://openairdocs.org/sdr/IPXA2025060250870), May 30, 2025: CONTROL HANDLE. INOPERATIVE. AFTER TAKEOFF THE GEAR LOCK OVRD HAD TO BE PUSHED TO RAISE THE GEAR. THE GEAR HANDLE WAS DIFFICULT TO MOVE FROM THE UP POSITION TO THE OFF POSITION ACCOMPLISHED
- [SDR IPXA2025042288075](https://openairdocs.org/sdr/IPXA2025042288075), Mar 27, 2025: SKIN. DEBONDED. RIGHT WING OUTBOARD FLAP, TOP PANEL 666KT SKIN DISBOND, 22 INCH TO INBOARD EDGE AREA (REPAIR). CLEAN, SEAL AND FINFISH AT REPAIR AREA I.A.W. 767-300F SRM 51-70-
- [SDR IPXA2025033188075](https://openairdocs.org/sdr/IPXA2025033188075), Mar 27, 2025: SKIN. DEBONDED. RIGHT WING OUTBOARD FLAP, TOP PANEL 666KT SKIN DISBOND, 22 INCH TO INBOARD EDGE AREA (REPAIR) CLEAN, SEAL AND FINFISH AT REPAIR AREA I.A.W. 767-300F SRM 51-70-1
- [SDR IPXA2025042260393](https://openairdocs.org/sdr/IPXA2025042260393), Mar 26, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE , P/N : 146T5869-10 PANEL NO : 252HFF STA 1197~STA1197+120 RBL77~RBL88. (REPAIR). .FABRICATE A NEW FLOOR PANEL I.A.
- [SDR IPXA2025032760393](https://openairdocs.org/sdr/IPXA2025032760393), Mar 26, 2025: FLOOR PANEL. DENTED. **SDR FILED OPEN** FAULT - FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE , P/N : 146T5869-10 PANEL NO : 252HFF STA 1197~STA1197+120 RBL77~RBL88. (REPAIR) I.A.W A
- [SDR IPXA2025062740712](https://openairdocs.org/sdr/IPXA2025062740712), Mar 25, 2025: SPAR. CRACKED. CRACK - HOLE , RIGHT WING FRONT SPAR LOWER CHORD SKIN PANEL CRACK AT RIB 32 ( WSTA 1018.2 ), 1 EA. (REPAIR) 1. ACCOMPLISHED JOB I.A.W UPS EO-93536-REQ1 REV1 2. 
- [SDR IPXA202504220161](https://openairdocs.org/sdr/IPXA202504220161), Mar 25, 2025: SKIN. CRACKED. DURING PERFORM T/C NO. EO-24301-JIC001 FOUND SKIN CRACK. (REPAIR). .REPAIR DAMAGE AREA I.A.W SRM 53-80-01-2R-5 REV.91 AND EGAT WORK SHEET NO. 50216 AND UPS EO-2
- [SDR IPXA2025041240712](https://openairdocs.org/sdr/IPXA2025041240712), Mar 25, 2025: SPAR. CRACKED. *** SDR FILED OPEN *** FAULT - CRACK - HOLE , RIGHT WING FRONT SPAR LOWER CHORD SKIN PANEL CRACK AT RIB 32 ( WSTA 1018.2 ), 1 EA. (REPAIR) I.A.W AMM 27-81-32-90
- [SDR IPXA2024090887761](https://openairdocs.org/sdr/IPXA2024090887761), Sep 8, 2024: LOCK ACTUATOR. BROKEN. **ATB**UPON GEAR RETRACTION ON INITIAL TAKEOFF WITH THE GEAR HANDLE IN THE UP POSITION WE HAD A €ŒGEAR DISAGREE AND GEAR DOORS€? ICAS MESSAGE AIR TURN BACK AN
- [SDR IPXA2023052512708](https://openairdocs.org/sdr/IPXA2023052512708), May 12, 2023: UNKNOWN. UNKNOWN. *SUPPLEMENTAL SDR * FAULT - WORN - PAWL, CREW ENTRY DOOR HANDLE MECHANISM (REPLACE) I.A.W AMM 52-11-26-004-001 REV. 139.00 AND AMM 52-11-26-404-003 REV. 139.00 
- [SDR IPXA2023051212708](https://openairdocs.org/sdr/IPXA2023051212708), May 12, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - WORN - PAWL, CREW ENTRY DOOR HANDLE MECHANISM (REPLACE) OK TO WORK
- [SDR IPXA2023051278793](https://openairdocs.org/sdr/IPXA2023051278793), May 10, 2023: FLOOR PANEL. DAMAGED. FAULT - FOUND MAIN DECK CARGO FLOOR PANEL DAMAGE LOCATION: STA 933 ~ STA 985 RBL 75 - RBL 88 (PANEL NO: 242MFF P/N: 145T5876-84) (REPAIR) REVIEWED
- [SDR IPXA2023052380501](https://openairdocs.org/sdr/IPXA2023052380501), May 10, 2023: GUARD. CRACKED. FAULT - CRACK - GUARD ASSY, MEC ACCESS DOOR R/H CUTOUT AREA. (REPLACE) PAPER REVIEW OK
- [SDR IPXA2023051344938](https://openairdocs.org/sdr/IPXA2023051344938), May 6, 2023: STIFFENER. CRACKED. FAULT - CRACK - STIFFENER, FORWARD CARGO COMPARTMENT, WING CENTER SECTION FRONT SPAR, STA 785.9, RBL 55. (REPAIR) REVIEWED
- [SDR IPXA2022101787179](https://openairdocs.org/sdr/IPXA2022101787179), Oct 17, 2022: SKIN. CHAFED. INSPECTION TYPE:N/ARIGHT WING NO. 8 SLAT TRAILING WEDGE LOWER SKIN CHAFE REPAIRREPAIRED IAW UPS E.O. B767-5750-84540-B ON NRC 684226
- [SDR IPXA2022100586864](https://openairdocs.org/sdr/IPXA2022100586864), Oct 3, 2022: INDICATOR. INOPERATIVE. INSPECTION TYPE:N/A**ATB - EMERGENCY DECLARED** IN CLIMB, CRUISE, DECENT WITH AUTOPILOT ONA ND OFF, RIGHT ELEVATOR INDICATOR OSCILLATING UP AND DOWN MORE PREVAL
- [SDR IPXA2022051482098](https://openairdocs.org/sdr/IPXA2022051482098), May 14, 2022: AUTOPILOT SYS. FAULT MESSAGE. INSPECTION TYPE:NACENTER AUTOPILOT ENGAGED - RCVD "AUTOPILOT" EICAS DURING CLIMB OUT. AUTOPILOT REMAINED ENGAGED. VNAV DISENGAGED. FMA DISPLAYED V/S W/ YELLOW L
- [SDR IPXA2022030779840](https://openairdocs.org/sdr/IPXA2022030779840), Mar 5, 2022: ENGINE. VIBRATION. INSPECTION TYPE:N/A***SUPPLEMENTAL SDR*** DIVERSION ** IFSD **EMERGENCY DECLARED ** AT ROTATION FROM ANCHORAGE, THERE WAS A VIOLENT BANG FOLLOWED BY #2 ENG FAIL
- [SDR IPXA2021081272684](https://openairdocs.org/sdr/IPXA2021081272684), Aug 12, 2021: IDG. FAULTED. DIVERSION, NO EMERG DECLARED, A/C LANDED WITHOUT INCIDENT* L GEN DRIVE EICAS ALERT IN CRUISE. FOLLOWED QRH PROCEDURE.DEFERRED IAW MEL 24-00-1-1.AIRCRAFT DID DIS
- [SDR IPXA2021051269314](https://openairdocs.org/sdr/IPXA2021051269314), May 2, 2021: SKIN. CRACKED. INSPECTION TYPE:C12CRACK DAMAGE WAS FOUND ON NO.1 PYLON OUTBD SKIN ASSEMBLY(P/N:311T2450-25) NEAR NAC STA 237.5PERFORM REPAIR I.A.W BOEING SR 4-5075409410 AND U
- [SDR IPXA2021051069171](https://openairdocs.org/sdr/IPXA2021051069171), May 2, 2021: SKIN. CRACKED. INSPECTION TYPE:C12CRACK ON THE NO.10 SLAT SKIN (P/N : 114T4103-4) NEAR OSS 792.537REPAIR I.A.W 767-300F SRM 57-43-01-2R-2 REV.80.00
- [SDR IPXA2020123063959](https://openairdocs.org/sdr/IPXA2020123063959), Dec 30, 2020: SHUTOFF VALVE. MALFUNCTIONED. INSPECTION TYPE: N/A ATB, LANDED UNEVENTFUL. NO EMEGENCY DECLARED. AFTER T/O THROUGH 5,000 LT ENGINE HPSOV EICAS L/BLEED LIGHT ILLUMINATED RAN QRH AIR TURNBACK 
- [SDR IPXA2020123063945](https://openairdocs.org/sdr/IPXA2020123063945), Dec 29, 2020: SHUTOFF VALVE. MALFUNCTIONED. INSPECTION TYPE: N/A ATB. LANDED UNEVENTFUL, NO EMERGENCY DECLARED. LT ENGINE HPSOV EICAS MESSAGE DISPLAYED AT B6000 FT BLEED LIGHT REILLUMINATED AFTER BLEED LI
- [SDR IPXA2020100661015](https://openairdocs.org/sdr/IPXA2020100661015), Oct 5, 2020: CIRCUIT CARD. FALSE ACTIVATION. INSPECTION TYPE: NA, DIVERSION, NO EMERGENCY DECLARED. SPD LIM ANNUNCIATED ON CAPT'S PFD BEFORE SPEED LIMIT IS APPROACHED. NO AIRSPEED LIMITS WERE APPROACHED OR
- [SDR IPXA2020081859189](https://openairdocs.org/sdr/IPXA2020081859189), Aug 17, 2020: ACTUATOR. DAMAGED. FOUND DAMAGE ON THE NR 1 ENGINE THRUST REVERSER UPPER ACTUATOR CLEVIS FITTING REF DEFERRAL M 716678. EO B767-7830-77544A C/W. PLACED ON DEFERRAL PER EO B767-783
- [SDR IPXA2019072344809](https://openairdocs.org/sdr/IPXA2019072344809), Jul 23, 2019: WINDOW. CRACKED. INSPECTION TYPE:IN DEFECT POSSIBLE CRACK IN LOWER RIGHT SIDE OF L1 WINDOW. REPLACED L1 WINDOW PER MM 56-11-01-004-039 & 56-11-01-404-017 PER STEP 32 CONNECTED E
- [SDR IPXA2019071944619](https://openairdocs.org/sdr/IPXA2019071944619), Jul 19, 2019: WARNING SYSTEM. FALSE ACTIVATION. INSPECTION TYPE:N/A AFT CARGO DET 2 STATUS MESSAGE DISPLAYED ON EICAS. **SUPPLEMENTAL ETOPS** SYS OPS CHECK OK PER FIM 26-16-00-615-829-000. THIS CLEARS M677264
- [SDR IPXA2019061743344](https://openairdocs.org/sdr/IPXA2019061743344), Jun 16, 2019: CONTROL PANEL. MALFUNCTIONED. FOUND "EMERGENCY LT " STILL ON EVEN SWITCH BEING IN "OFF" POSITION ON CTRL PANEL .R/R PILOT,S EMERGENCY LT CTRL PANEL AND OPS CHK OK IAW MM 53-51-08/401 IPC : 3
- [SDR IPXA2019042941540](https://openairdocs.org/sdr/IPXA2019042941540), Apr 29, 2019: SKIN. DENTED. RT WING #9 SLAT T/E WEDGE DENT ON UPPER SKIN SURFACEREPAIRED PER EO B767-5750-71556-B
- [SDR IPXA2019042974491](https://openairdocs.org/sdr/IPXA2019042974491), Apr 27, 2019: SKIN. NOT REPORTED. L/H I/B ELEVATOR HOLE IN UPPER SKINREPAIRED LH INBD UPPER ELEVATOR SKIN IAW UPS E.O. B767-5520-71458-A
- [SDR IPXA2018092134221](https://openairdocs.org/sdr/IPXA2018092134221), Sep 20, 2018: TRANSCEIVER. FAILED. AIR TURN BACK DUE TO THE WEATHER RADAR FAILED DURING CLIMBOUT. FLT CREW REPORTED NO LRU FAULTS ALONG WITH MX FAIL FAULT. SUSPECT THE R/T UNIT THAT WAS INSTALLED
- [SDR IPXA2017121124378](https://openairdocs.org/sdr/IPXA2017121124378), Dec 11, 2017: CIRCUIT BREAKER. TRIPPED. INSPECTION TYPE:ETOPDURING CRUISE EICAS STATUS LEFT ENG IGNITER 1.LEFT ENG IGNITION SYS 1 INOP. T/S AND FOUND L PIMU FAULTED W/NO 115 VOLT POWER TO ENG 1/IGN. F
- [SDR IPXA2017081720635](https://openairdocs.org/sdr/IPXA2017081720635), Aug 12, 2017: ACTUATOR. SHEARED. RIGHT MLG RETRACT ACTUATOR SHEARED. R & R THE RETRACT ACTUATOR IAW AMM 32-32-01-404-018, REV 121.02. OPS CHECKED GOOD.
- [SDR IPXA2017072119576](https://openairdocs.org/sdr/IPXA2017072119576), Jul 21, 2017: COVER. DETACHED. EMERGENCY EXIT SIGN COVER AT MAIN DOOR FELL OFF. SECURED THE SIGN COVER IAW AMM 33-51-01-201, OPS CHECKED OK
- [SDR IPXA2017072419682](https://openairdocs.org/sdr/IPXA2017072419682), Jul 20, 2017: LENS. UNSECURE. EMERGENCY EXIT LIGHT COVER NEXT TO CREW ENTRY DOOR FELL OFF. REINSTALLED THE COVER
- [SDR IPXA2017060717997](https://openairdocs.org/sdr/IPXA2017060717997), Jun 7, 2017: BATTERY PACK. FAILED. INSPECTION TYPE: C10, EMERGENCY LIGHT BATTERY PACK DEEP CYCLING FAILURE. REPLACED THE BATTERY PACK.
- [SDR IPXA2017060717996](https://openairdocs.org/sdr/IPXA2017060717996), May 31, 2017: SKIN. CRACKED. INSPECTION TYPE: C10, CRACK ON RIGHT FUSELAGE SKIN AT BS 1660, STRINGER 13AR, REPAIRED IAW SRM 53-80-01, REPAIR 7, REV 68.
- [SDR IPXA2017060717995](https://openairdocs.org/sdr/IPXA2017060717995), May 29, 2017: STIFFENER. CRACKED. INSPECTION TYPE: C10, CRACK ON STIFFENER UPPER SIDE AT BS 785.9, LBL 33. REPAIRED IAW SRM 57-10-10-2R-2, REPAIR 2, REV 68, AND EO B767-5740-58151-A.
- [SDR IPXA2017060717994](https://openairdocs.org/sdr/IPXA2017060717994), May 29, 2017: STIFFENER. CRACKED. INSPECTION TYPE: C10, CRACK ON STIFFENER UPPER SIDE AT BS 785.9 , LBL 11. REPAIRED IAW SRM 57-10-10-2R-R, REPAIR 2, REV 68, AND EO B767-5740-58151-A.
- [SDR IPXA2017022614426](https://openairdocs.org/sdr/IPXA2017022614426), Feb 26, 2017: FLOOR PANEL. DAMAGED. MCD FLOOR PANEL, POS 9 CNT, HAS 2 HOLES THROUGH SKIN AND INTO CORE. REMOVED DAMAGE, AND REPAIRED THE FLOOR PANEL IAW SRM 53-00-50-2R.
- [SDR IPXA2016122211996](https://openairdocs.org/sdr/IPXA2016122211996), Dec 22, 2016: LENS. DETACHED. EXIT SIGN LENS FELL OFF. INSTALLED THE LENS IAW MM 33-51-01-201 AND CHECKED OK
- [SDR IPXA2015122797104](https://openairdocs.org/sdr/IPXA2015122797104), Dec 27, 2015: FLOOR PANEL. DAMAGED. DECK FLOOR PANEL PN 143T5876-87 DAMAGED IN NUMEROUS AREAS. FABRICATED NEW FLOOR PANEL, REF EOB 767-5320-9693-H.
- [SDR IPXA2015092393866](https://openairdocs.org/sdr/IPXA2015092393866), Sep 21, 2015: BLADES. DAMAGED. INSPECTION TYPE:ETOP, ON T/O, APPROXIMATELY 400 FT AGL WE FLEW INTO SEVERAL BIRDS ON RT SIDE OF ACFT AND RT ENG VIBRATION WAS 5.0 ON INSTRUMENT AND NOTICEABLE I
- [SDR IPXA2015082892839](https://openairdocs.org/sdr/IPXA2015082892839), Aug 28, 2015: CONTAINER. TORN. CENTER SUPERNUMERY SEAT LIFE VEST BAG TORN. R & R ED CENTER SUPERNUMERY SEAT LIFE VEST LOCATED UNDER SEAT COMPARTMENT REF AMM 25-62-00 & IPC 25-64-55, EFF SOURC
- [SDR IPXA2015061290090](https://openairdocs.org/sdr/IPXA2015061290090), Jun 11, 2015: SLEEVE. DENTED. INSPECTION TYPE: C, DURING MAJOR MAINTENANCE VISIT, FOUND A DENT ON THE EXHAUST SLEEVE AT NAC STA 342.5 6 O'CLOCK POSITION OF THE NR 1 ENGINE.

All 125: https://openairdocs.org/aircraft/N318UP/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

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