# N314UP: 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: 27742
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 5, 1996
- Certificate issued: December 8, 2008
- Expires: February 28, 2029
- Mode S code: A3577D
- 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=314UP
- Page: https://openairdocs.org/aircraft/N314UP

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/N314UP/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 DCA26WA260](https://openairdocs.org/ntsb/DCA26WA260), Jul 1, 2026: Boeing 767-34AF (N314UP), Singapore, Singapore, incident, no damage

## 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 20040330004599I](https://openairdocs.org/incident/20040330004599I), Mar 30, 2004: Boeing 76734AF (N314UP), Oakland, CA. (-23) Crew reported a landing gear and flap problem prior to landing to ATC at Oakland international airport. The crew stated "c" hydraulic quantity decreased…

## Service difficulty reports (136, 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 IPXA2026092379070](https://openairdocs.org/sdr/IPXA2026092379070), Sep 22, 2026: ACCELEROMETER. OSCILLATES. DURING CLIMB EXPERIENCED NOTICABLE OSCILLATIONS COMING FROM THE TAIL THAT DISSIPATED AT CRUISE. ALL ENG INDICATIONS NORMAL VERTICAL STABILIZER ACCESS PANELS AND
- [SDR IPXA2026090220809](https://openairdocs.org/sdr/IPXA2026090220809), Aug 31, 2026: WINDOW. FAILED. DURING CRUISE, THE CAPTAIN`S FWD WINDOW BEGAN ARCING IN BOTTOM LEFT PART OF THE WINDOW. WINDOW HEAT WAS IMMEDIATELY TURNED OFF, AND A FEW SECONDS LATER, THE WIN
- [SDR IPXA2026090120809](https://openairdocs.org/sdr/IPXA2026090120809), Aug 31, 2026: WINDOW. ARCED. DURING CRUISE, THE CAPT`S FWD WINDOW BEGAN ARCING IN BOTTOM LT AREA OF WINDOW. THE WINDOW HEAT WAS IMMEDIATELY TURNED OFF, & A FEW SECONDS LATER, THE WINDOW SHA
- [SDR IPXA2026062631637](https://openairdocs.org/sdr/IPXA2026062631637), Jun 24, 2026: WINDOW. SCRATCHED. LEFT PILOTS DV WINDOW IS SCRATCHED. WHEN TURNING LEFT INTO PARKING SPOT & SUN HITTING DIRECTLY ON WINDOW MARSHALER COULD NOT BE SEEN. C/W RII IAW GMM 04-02 REMO
- [SDR IPXA2026062531637](https://openairdocs.org/sdr/IPXA2026062531637), Jun 24, 2026: WINDOW. SCRATCHED. LEFT PILOTS DV WINDOW IS SCRATCHED. WHEN TURNING LEFT INTO PARKING SPOT & SUN HITTING DIRECTLY ON WINDOW MARSHALER COULD NOT BE SEEN. REMOVED CAPTAINS L2 WINDOW
- [SDR IPXA2025100597605](https://openairdocs.org/sdr/IPXA2025100597605), Oct 5, 2025: BATTERY PACK. DISCHARGED. DURING PDC FOUND EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-07. OPS CHECK GOOD. A/C OK FOR SVC
- [SDR IPXA2025082200297](https://openairdocs.org/sdr/IPXA2025082200297), Aug 22, 2025: UNKNOWN. ODOR. AFTER AIR CART CONNECTED & PACKS TURNED ON STRONG FUMES ENTERED THE COCKPIT, FUMES REMAINED UNTIL PACKS WERE SELECTED OFF. ACCOMPLISHED REMOVAL OF OIL CONTAMINA
- [SDR IPXA2025061186460](https://openairdocs.org/sdr/IPXA2025061186460), Jun 1, 2025: SKIN. CORRODED. CORROSION-SKIN, AFT CGO COMPT FWD BULKHEAD LWR STRINGER AREA, NEAR STA 1083, S-39L.I.A.W AMM 53-66-01-004-002 REV.145 REMOVED FAIRING PANEL NO.197AL AND 197JL.R
- [SDR IPXA2025060974047](https://openairdocs.org/sdr/IPXA2025060974047), May 31, 2025: STRAP. CORRODED. CORROSION-U CHANNEL, FORWARD CARGO COMPARTMENT AROUND CEILING PANEL NUTPLATES AREA BETWEEN STA 566 AND STA 610, RBL 40.(REPLACE) 1. JOB COMPLETED.
- [SDR IPXA2025060971981](https://openairdocs.org/sdr/IPXA2025060971981), May 31, 2025: SKIN. CORRODED. RIGHT WING INBOARD MAIN FLAP TE LOWER SKIN INSIDE SUSPECT CORROSION, IFS 105.75. ACCOMPLETED REPAIR IAW EO-94005-REQ1 REV1.
- [SDR IPXA2025060944382](https://openairdocs.org/sdr/IPXA2025060944382), May 30, 2025: ANGLE. CRACKED. CRACKED ANGLE, L/H LOWER WING TO BODY AREA, STA 785. (AGING A/C INSPECTION).REMOVED DAMAGE ANGLE I.A. W SRM 51-40-02-0G REV. 92. INSTALLED NEW ANGLE I.A.W SRM 5
- [SDR IPXA2025052908018](https://openairdocs.org/sdr/IPXA2025052908018), May 28, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-89 PANEL NO: 251XFF. (REPAIR) I.A.W AMM 25-57-05-004-001, AMM 25-57-02-004-029, AMM 25-58-01-004-001 AND AMM 2
- [SDR IPXA2025052908016](https://openairdocs.org/sdr/IPXA2025052908016), May 28, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-134 PANEL NO: 252UFF. (REPAIR) I.A.W AMM 25-57-05-004-001, AMM 25-57-02-004-029, AMM 25-58-01-004-001 AND AMM 
- [SDR IPXA2025030451226](https://openairdocs.org/sdr/IPXA2025030451226), Feb 20, 2025: TRANSCEIVER. FAULTED. BOTH HF UNABLE TRANSMIT. OPS CHECK OK ON GND, SATCOM INOP ALSO. RESULTED IN ATB. ++ C/W FIM T/S 23-11-00. R&R HF TRANSCEIVER REF AMM 23-11-03-424-005. BOTH HFS 
- [SDR IPXA2025022051226](https://openairdocs.org/sdr/IPXA2025022051226), Feb 20, 2025: SATCOM. FAULTED. **ATB**BOTH HF UNABLE TRANSMIT. OPS CHECK OK ON GND, SATCOM INOP ALSO. RESULTED IN ATB. DEFERRED BOTH HF COMMUNICATION SYSTEMS REF MEL 23-11-1-2A-2, PLACARD INS
- [SDR IPXA2025010279317](https://openairdocs.org/sdr/IPXA2025010279317), Dec 31, 2024: DOOR. OBSTRUCTED. CREW ENTRY DOOR IS NOT CLOSING CORRECTLY FROM THE INSIDE UPON FURTHER INSP FOUND SMALL PIECE OF RUBBER TRIM WEDGED IN INSIDE HANDLE AREA, REMOVED TRIM PIECE ,OP
- [SDR IPXA2024121990371](https://openairdocs.org/sdr/IPXA2024121990371), Dec 19, 2024: SKIN. DAMAGED. L WING PANEL 561GB LEADING EDGE HAS SEPARATION WITH RIVETS PULLED THROUGH. MARKED WITH TAPE. REPLACED DAMAGED WIGGLE PLATES WITH 113T1663Y1013, 113T1663-1037 AN
- [SDR IPXA2025022632593](https://openairdocs.org/sdr/IPXA2025022632593), Nov 28, 2024: TORQUE TUBE. BENT. R/H AFT INBOARD FLAP TORQUE TUBE SLOT DOOR BENT/ DAMAGED INSTALLED NEW UPPER TORQUE TUBE / AFT SLOT DOOR ASSY IAW AMM 27-51-07. WILL REQUIRE ADJUSTMENTS AFTER T
- [SDR IPXA2024112832593](https://openairdocs.org/sdr/IPXA2024112832593), Nov 28, 2024: TORQUE TUBE. BENT. *** SDR FILED OPEN *** R/H AFT INBOARD FLAP TORQUE TUBE SLOT DOOR BENT/ DAMAGED WILL REQUIRE SM TO DRILL NEW PARTS AND FASTENER INSTALLATION 12 HOURS. MAINTENAN
- [SDR IPXA2023100914881](https://openairdocs.org/sdr/IPXA2023100914881), Oct 5, 2023: IRU. OUT OF ALIGNMENT. *** SUPPLEMENTAL SDR *** COULD NOT ALIGN IRU'S ATTEMPTED TWICE. FMC MESSAGE IRS MOTION. (CENTER NOT ALIGNING) **OII 2** R&R RIGHT IRU PER MM 34-21-01, OPS CHECK
- [SDR IPXA2023100514881](https://openairdocs.org/sdr/IPXA2023100514881), Oct 5, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* *DIV* COULD NOT ALIGN IRU'S ATTEMPTED TWICE. FMC MESSAGE IRS MOTION. (CENTER NOT ALIGNING) **OII 2** SWAPPED CENTER IRU(PART NUMBER HG1050AE15,
- [SDR IPXA2023082195742](https://openairdocs.org/sdr/IPXA2023082195742), Aug 5, 2023: HANDLE. UNKNOWN. *** SUPPLEMENTAL SDR *** FAULT - WORN - PAWL, CREW ENTRY DOOR HANDLE MECHANISM. (REPLACE) REVIEW COMPLETE
- [SDR IPXA2023080701](https://openairdocs.org/sdr/IPXA2023080701), Aug 5, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - WORN - PAWL, CREW ENTRY DOOR HANDLE MECHANISM. (REPLACE) OK TO WORK
- [SDR IPXA2023082162818](https://openairdocs.org/sdr/IPXA2023082162818), Aug 3, 2023: UNKNOWN. CRACKED. *** SUPPLEMENTAL SDR *** FAULT - FOUND MAIN DECK CARGO ZONE TEMP SENSOR COVER CRACK AT STA 1164 RIGHT SIDE (REPLACE) REVIEW COMPLETE
- [SDR IPXA2023082162263](https://openairdocs.org/sdr/IPXA2023082162263), Aug 3, 2023: UNKNOWN. UNKNOWN. *** SUPPLEMENTAL SDR *** FAULT - FOUND MAIN DECK CARGO ZONE TEMP SENSOR COVER CRACK AT STA 654+33 RIGHT SIDE (REPLACE) REVIEW COMPLETE
- [SDR IPXA202308030004](https://openairdocs.org/sdr/IPXA202308030004), Aug 3, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - FOUND MAIN DECK CARGO ZONE TEMP SENSOR COVER CRACK AT STA 654+33 RIGHT SIDE (REPLACE) OK TO WORK
- [SDR IPXA202308030001](https://openairdocs.org/sdr/IPXA202308030001), Aug 3, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* FAULT - FOUND MAIN DECK CARGO ZONE TEMP SENSOR COVER CRACK AT STA 1164 RIGHT SIDE (REPLACE) OK TO WORK
- [SDR IPXA2023081352701](https://openairdocs.org/sdr/IPXA2023081352701), Aug 2, 2023: FITTING. BROKEN. FAULT - FOUND MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING BROKEN AT STA ( 870 & 890 ) RBL47.5 & STA890 BL0 & STA ( 999 & 1087 & 1131 ) LBL47.5 TTL: 6EA(REPL
- [SDR IPXA2023080825567](https://openairdocs.org/sdr/IPXA2023080825567), Jul 31, 2023: STIFFENER. CRACKED. *SDR FILED OPEN* *MAJOR REPAIR* FAULT - CRACK CENTER WING FRONT SPAR CRACK IS STIFFENERS AT STA 785.9 RBL 55 (REPAIR) THE CENTER WING FRONT SPAR IS CLASSIFIED A
- [SDR IPXA2023080825558](https://openairdocs.org/sdr/IPXA2023080825558), Jul 31, 2023: STIFFENER. CRACKED. MAJOR REPAIR, FAULT - CRACK CENTER WING FRONT SPAR CRACK IS STIFFENERS AT STA 785.9 LBL 33 (REPAIR) THE CENTER WING FRONT SPAR IS CLASSIFIED AS PRIMARY STRUCTUR
- [SDR IPXA2023071641325](https://openairdocs.org/sdr/IPXA2023071641325), Jul 16, 2023: FLOOR PANEL. UNKNOWN. FLOOR PANEL IN POS 12L AND 12R HAS DAMAGE NEAR FASTENER. LABOR ROW NOT REQUIRED.
- [SDR IPXA2023020790745](https://openairdocs.org/sdr/IPXA2023020790745), Feb 7, 2023: SENSOR. NONE. INSPECTION TYPE:N/A**ATB** ON TAKEOFF, CREW HAD TO USE OVERRIDE SWITCH TO BRING UP GEAR . A/C NEVER RECOGNISED T/OFOUND RMLG TILT SENSOR BRACKET IMPROPERLY INST
- [SDR IPXA2022110687864](https://openairdocs.org/sdr/IPXA2022110687864), Nov 6, 2022: FLOORBOARD. DAMAGED. DAMAGE ON FLOORBOARD ON MCD CENTER 9R/9L.FABRICATED NEW FLOOR BOARD PER EO B767-5320-9693-I.
- [SDR IPXA2022072084364](https://openairdocs.org/sdr/IPXA2022072084364), Jul 19, 2022: EICAS. INOPERATIVE. INSPECTION TYPE:NA** ATB**SDR FILED OPEN**NO EMERG ACTION** A/C LANDED WITHOUT INCIDENT**DURING START L AOA PROBE EICAS DISPLAYED. LEFT ANGLE OF ATTACK SENOSR H
- [SDR IPXA2021071971817](https://openairdocs.org/sdr/IPXA2021071971817), Jul 19, 2021: SKIN. DENTED. INSPECTION TYPE:C13, DENT ON FUSELAGE SKIN (PN:146T3241-15) BETWEEN STA 1417 AND 1439, S-36L TO S-37L.REPAIR IAW SRM 53-00-01-2R-12, REV 20.03. REPAIRED I.A.W 7
- [SDR IPXA2021062570948](https://openairdocs.org/sdr/IPXA2021062570948), Jun 25, 2021: WARNING MESSAGE. FALSE INDICATION. INSPECTION TYPE:N/A** ATB **LANDED UNEVENTFULLY** GEAR DISAGREE WITH GEAR DOORS LIGHT ILLUMINATED AFTER TAKE OFF.VISUALLY INSPECTED ALL LANDING GEARS & GEAR DOO
- [SDR IPXA2019083046158](https://openairdocs.org/sdr/IPXA2019083046158), Aug 29, 2019: SKIN. DAMAGED. SKIN PUNCTURE AT FS 637 JUST AFT AND BELOW MAIN CARGO DOOR. DUE TO A1 CAN BEING BLOWN INTO FUSELAGE DURING WIND STORM. THIS IS A MAJOR REPAIR. CUTOUT DAMAGED SK
- [SDR IPXA2019083086114](https://openairdocs.org/sdr/IPXA2019083086114), Aug 28, 2019: SKIN. DAMAGED. FUSELAGE SKIN PUNCTURED AT BS 637, STRINGER 31L. TEAR STRAP DAMAGED. REPAIRED IAW EO B767-5330-73738-A AND SRM 53-00-01-2R.
- [SDR IPXA2019083086113](https://openairdocs.org/sdr/IPXA2019083086113), Aug 28, 2019: STRINGER. DAMAGED. STRINGER 31L DAMAGED AT BS 637. STRINGER SHEARED AT TEAR STRAP LOCATION. REPAIRED IAW EO B767-73734-A AND SRM 53-30-03-01.
- [SDR IPXA2019070444060](https://openairdocs.org/sdr/IPXA2019070444060), Jun 24, 2019: STIFFENER. CRACKED. INSPECTION TYPE:C12 CRACK ON VERTICAL STIFFENER AT WHEEL WELL BULKHEAD AT STA 287, LBL 25. REPAIR IAW EO B767-5310-20118-F AND SRM 51-70-12 GENERAL , FIGURE 1 ,
- [SDR IPXA2019070444059](https://openairdocs.org/sdr/IPXA2019070444059), Jun 24, 2019: STIFFENER. CRACKED. INSPECTION TYPE:C12 CRACK ON CENTER WING TANK STIFFENER(P/N:111T2008-12) ON STA 785.9,RBL33. REPAIR IAW SRM 57-10-10-2R-2 REPAIR 2 REV.74.00, EO B767-5740-58151
- [SDR IPXA2018070231299](https://openairdocs.org/sdr/IPXA2018070231299), Jul 2, 2018: SMOKE DETECTOR. FAULTY. MAIN CARGO SMOKE DETECT 2 MESSAGE. AFTER ARRIVAL FOUND SMOKE DETECTOR 2 EA FAULT LIGHT ILLUMINATED. REMOVED AND REPLACED SMOKE DETECTOR FOR MAIN CARGO IN POSITI
- [SDR IPXA2018043029097](https://openairdocs.org/sdr/IPXA2018043029097), Apr 29, 2018: ESCAPE REEL. UNSERVICEABLE. DECENT DEVICE S/N 14877 FOUND TO BE UNSERVICEABLE. REF PART REQ 228947A MOST FORWARD POSITION, EXP DATE JULY 6, 2020. REMOVED & REPLACED FWD DECENT DEVICE PER A
- [SDR IPXA2017121824613](https://openairdocs.org/sdr/IPXA2017121824613), Dec 16, 2017: LIFE VEST. OPEN. FIRST OFFICEER`S LIFE VEST OPENED. INSTALLED A NEW LIFE VEST.
- [SDR IPXA2017102322891](https://openairdocs.org/sdr/IPXA2017102322891), Oct 20, 2017: CONNECTOR. DIRTY. DURING START, THE LEFT ENGINE START VALVE DID NOT OPEN. CLEANED THE CONNECTOR ON LT ENGINE STARTER MOTOR AND PERFORMED AN OPS CHECK 3 TIMES ON GROUND. ALL CHECK
- [SDR IPXA2017091821834](https://openairdocs.org/sdr/IPXA2017091821834), Sep 16, 2017: LIGHT. INOPERATIVE. RT AFT FLIGHT DECK EMERGENCY EXIT LIGHT INOP. RELAMPED IN REFERENCE TO AMM 33-51-11, OPS NORMAL.
- [SDR IPXA2017072719833](https://openairdocs.org/sdr/IPXA2017072719833), Jul 27, 2017: WARNING MESSAGE. ILLUMINATED. STATUS MESSAGE FOR WEATHER RADAR SYS. OPEN
- [SDR IPXA2017061918346](https://openairdocs.org/sdr/IPXA2017061918346), Jun 18, 2017: SENSOR. OUT OF LIMITS. CLEARANCE OF ENTRY DOOR CLOSER SENSOR IS NOT WITHIN LIMITS IAW TC 52-000-100. ADJUSTED ENTRY DOOR CLOSED SENSOR IAW TC 52-000-100 AND AMM 52-12-00
- [SDR IPXA2017060417857](https://openairdocs.org/sdr/IPXA2017060417857), Jun 4, 2017: LAMP. INOPERATIVE. INSPECTION TYPE: C11, FOUND EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED EXTERIOR EMERGENCY LIGHT LAMP IAW AMM 33-51-16-962-001, REV 121. PERFORMED TEST OF TH
- [SDR IPXA2017051617193](https://openairdocs.org/sdr/IPXA2017051617193), May 16, 2017: FLOORBOARD. DAMAGED. FLOORBOARD AT POS 2/3 LBL 49 DAMAGED. REMOVED THE FLOORBOARD. MAJOR REPAIR. FABRICATED A NEW FLOORBOARD.

All 136: https://openairdocs.org/aircraft/N314UP/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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