# N312UP: 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 CF6-80C2B6F](https://openairdocs.org/engine/ge-cf6-80c2b6f) (registry code 30109)
- Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs)
- Serial number: 27763
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 6, 1996
- Certificate issued: November 7, 1996
- Expires: November 30, 2028
- Mode S code: A3500F
- 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=312UP
- Page: https://openairdocs.org/aircraft/N312UP

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.

## ADs that may apply (OpenAirDocs): 34 in force

### Matched by airframe (Boeing 767-34AF)

None in force.

### Matched by engine (GE CF6-80C2B6F)

- [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 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 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 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 2009-07-03](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 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 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 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 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 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 95-10-11](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 94-06-03](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
- [AD 93-14-18](https://openairdocs.org/ad/93-14-18): High pressure turbine (HPT) thermal shields · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Oct 4, 1993
- [AD 91-15-25](https://openairdocs.org/ad/91-15-25): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Sep 6, 1991
- [AD 91-11-05](https://openairdocs.org/ad/91-11-05): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Jul 5, 1991
- [AD 91-05-21](https://openairdocs.org/ad/91-05-21): High Pressure Turbine · General Electric CF6-80C2A5, CF6-80C2B6, CF6-80C2B6F and 1 more. Effective Mar 27, 1991

### 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 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 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 2000-16-12](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 99-08-13](https://openairdocs.org/ad/99-08-13) (historical): General Electric CF6-80A, CF6-80A1, CF6-80A2 and 26 more. Effective May 13, 1999
- [AD 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

## Information bulletins (advisory) (4 in force)

- [SAIB 2023-15](https://openairdocs.org/saib/2023-15): Falsified Forms from AOG Technics. Issued Dec 19, 2023
- [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 N312UP.

## 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 20000620034529I](https://openairdocs.org/incident/20000620034529I), Jun 20, 2000: Boeing 76734AF (N312UP), Orlando, FL, Minor damage. (-23)While taxing left hand, main landing gear, strut dynamic seal failed. Hydraulic fluid sprayed on the hot brakes and ignited. Landing gear assembly, strut…

## Service difficulty reports (159, 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 IPXA2026092829503](https://openairdocs.org/sdr/IPXA2026092829503), Sep 25, 2026: HANDLE. BINDING. CREW ENTRY DOOR CAPTURE LEVER STICKS IN INBOARD POSITION. ++ FOUND DOOE CREW ENTRY DOOR INTERLOCK PAWL WORN, REMOVED AND REPLACED INTERLOCK PAWL REF 767 M/M 52-
- [SDR IPXA2026081809155](https://openairdocs.org/sdr/IPXA2026081809155), Aug 16, 2026: DISPLAY. INOPERATIVE. EMERGENCY DECLARED, CAPT / FO LOST ALL PFD/MAP EICAS ALL LARGE DISPLAY SCREENS WERE LOST FROM FL200 TO PARK SPOT STBY INSTRUMENTS WORKED. REPLACED LT, RT & CNTR
- [SDR IPXA202608179155](https://openairdocs.org/sdr/IPXA202608179155), Aug 16, 2026: DISPLAY. FAILED. EMERGENCY DECLARED, CAPT / FO LOST ALL PFD/MAP EICAS ALL LARGE DISPLAY SCREENS WERE LOST FROM FL200 TO PARK SPOT STBY INSTRUMENTS WORKED.
- [SDR IPXA2026061551590](https://openairdocs.org/sdr/IPXA2026061551590), Jun 13, 2026: PAWL. INOPERATIVE. YELLOW ARM HANDLE ON ENTRY DOOR DOES NOT WORK. REPLACED PAWL MECHANISM ON CREW ENTRY DOOR IAW AMM 52-11-26. OPS CHECKED OK.
- [SDR IPXA2025060622941](https://openairdocs.org/sdr/IPXA2025060622941), May 29, 2025: SPLICE. CORRODED. FAULT - CORROSION - SPLICE TEE , LOWER WING - TO - BODY FAIRING PANEL #149AL INTERNAL FORWARD SURFACE.REMOVED DAMAGE SPLICE TEE I.A.W SRM 51-40-02-0G REV.92.INS
- [SDR IPXA2025052891612](https://openairdocs.org/sdr/IPXA2025052891612), May 27, 2025: SKIN. DENTED. GOUGE-SKIN, R/H WING LEADING EDGE #12 SLAT UPPER EDGE AT MIDDLE SUPPORT ADJACENT AREA (AGING A/C NSPECTION) (REPAIR) PERFORMED NDT/ET FOR THE CUTOUT AREA I.A.W.
- [SDR IPXA2025060381793](https://openairdocs.org/sdr/IPXA2025060381793), May 26, 2025: FILLER. CORRODED. FILLER WITH SURFACE CORROSION AT STA 1601 IN THE AREA AFT BULK CARGO COMPARTMENT.REMOVED DAMAGE FILLER I.A.W SRM 51-40-02-0G REV.92.PERFORMED CHROMIC ACID ANODI
- [SDR IPXA2025060378665](https://openairdocs.org/sdr/IPXA2025060378665), May 26, 2025: FILLER. CORRODED. FOUND THE FILLER WITH CORROSION DAMAGE AT STA 1599 LBL 60 IN CEILING AREA OF BULK CARGO.REMOVED DAMAGE FILLER I.A.W SRM 51-40-02-0G REV.92. PERFORMED CHROMIC AC
- [SDR IPXA2025052778870](https://openairdocs.org/sdr/IPXA2025052778870), May 26, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-78 PANEL NO.231AFF.I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-01-004-001 REV.145
- [SDR IPXA2025052779608](https://openairdocs.org/sdr/IPXA2025052779608), May 26, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-89 PANEL NO.231KFF (REPAIR)I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-05-004-047
- [SDR IPXA2025052779630](https://openairdocs.org/sdr/IPXA2025052779630), May 26, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N : 143T5876-75 PANEL NO.231CFF (REPAIR)I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-05-004-04
- [SDR IPXA2025052779388](https://openairdocs.org/sdr/IPXA2025052779388), May 26, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR WITH DENT DAMAGE, P/N: 143T5876-90 PANEL NO.232JFF. I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-01-004-001 REV.145 REMO
- [SDR IPXA2025052779529](https://openairdocs.org/sdr/IPXA2025052779529), May 26, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-38 PANEL NO.232BFF.I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-01-004-001 REV.145
- [SDR IPXA2025052779313](https://openairdocs.org/sdr/IPXA2025052779313), May 26, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-80 PANEL NO.232HFF.I.A.W AMM 25-57-02-004-029 REV.145 REMOVED BALL TRAY ASSY.I.A.W AMM 53-01-06-000-
- [SDR IPXA2025052778917](https://openairdocs.org/sdr/IPXA2025052778917), May 26, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-10 PANEL NO.232EFF.I.A.W AMM 25-58-04-004-010 REV.145 REMOVED SIDE RESTRAINT ASSY.I.A.W AMM 53-01-06
- [SDR IPXA2025052779581](https://openairdocs.org/sdr/IPXA2025052779581), May 26, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-76 PANEL NO.232AFF.I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-01-004-001 REV.145
- [SDR IPXA2025052779634](https://openairdocs.org/sdr/IPXA2025052779634), May 26, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N : 143T5876-81 PANEL NO.231HFF (REPAIR)I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-05-004-04
- [SDR IPXA2025052779432](https://openairdocs.org/sdr/IPXA2025052779432), May 26, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-84 PANEL NO.232FFF.I.A.W AMM 25-57-02-004-029 REV.145 REMOVED BALL TRAY ASSY.I.A.W AMM 53-01-06-000-
- [SDR IPXA2025052778688](https://openairdocs.org/sdr/IPXA2025052778688), May 26, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE , P/N : 143T5876-77 PANEL NO. 231BFF.I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-01-004-001 REV.
- [SDR IPXA2025052779657](https://openairdocs.org/sdr/IPXA2025052779657), May 26, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-83 PANEL NO.231GFF (REPAIR)I.A.W AMM 25-57-02-004-029 REV.145 REMOVED BALL TRAY ASSY.I.A.W AMM 53-01
- [SDR IPXA2025052779404](https://openairdocs.org/sdr/IPXA2025052779404), May 26, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DAMAGE, P/N: 143T5876-72 PANEL NO.232CFF.I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-01-004-001 REV.145 REMO
- [SDR IPXA2025052779626](https://openairdocs.org/sdr/IPXA2025052779626), May 26, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-79 PANEL NO.231JFF (REPAIR)I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-05-004-047
- [SDR IPXA2025060670494](https://openairdocs.org/sdr/IPXA2025060670494), May 25, 2025: SEAT TRACK. CRACKED. FOUND MAIN DECK SEAT TRACK CRACK AT STA 522 LBL 88.I.A.W AMM 25-57-05-004-001 AND AMM 25-58-04-004-010 REV.145 REMOVED MAIN DECK CARGO HANDLING.I.A.W AMM 53-01-
- [SDR IPXA2025032656838](https://openairdocs.org/sdr/IPXA2025032656838), Mar 25, 2025: PAWL. BROKEN. FWD LH ENTRY/SERVICE DOOR EXTERNAL HANDLE PAWL BROKEN. REMOVED AND REPLACED FWD LH ENTRY DOOR EXTERNAL HANDLE PAWL IAW 767 AMM 52-12-00. DOOR AND HANDLE TEST GO
- [SDR IPXA2024040145516](https://openairdocs.org/sdr/IPXA2024040145516), Mar 30, 2024: FLAP SYSTEM. FAULTED. **EMERGENCY DECLARED**ON APPROACH WHEN FLAPS 20 SELECTED €Œ TE FLAP DISAGREE€? AOM PROCEDURE COMPLETED PERFORM FIM TASK 27-51 FAULT TREE 809.FAULT TE ON FSEU.
- [SDR IPXA2024011058596](https://openairdocs.org/sdr/IPXA2024011058596), Jan 10, 2024: UNKNOWN. WARNING MESSAGE. *** DIVERSION *** RUDDER RATIO ON EICAS C/W FIM 27-21-804 AND FIM 27-09-814 NO FAULTS AND RUDDER RATIO CHANGER PASSES BITE TEST A/C OKAY TO CONTINUE
- [SDR IPXA2023121115599](https://openairdocs.org/sdr/IPXA2023121115599), Dec 5, 2023: INLET. CRACKED. #1 ENGINE INLET COWL HAS APPROXIMATELY 3.0 INCH CRACK AT 12:00 POSITION ON AFT PORTION OF BULLNOSE LIP. MARKED. REMOVED AND REPLACED LH ENGINE INLET DURING ENGI
- [SDR IPXA2023080351495](https://openairdocs.org/sdr/IPXA2023080351495), Jul 25, 2023: SLAT. CRACKED. RH WING #12 SLAT CLOSURE PANEL SPLIT AND NOT FAIRED TO LOWER WING SKIN. PANEL IS SPLIT APPROX. 2 INCHES OUTBOARD TO INBOARD. 10 CYCLE LIMIT, SM20/LMX4. FABRICAT
- [SDR IPXA2023072551495](https://openairdocs.org/sdr/IPXA2023072551495), Jul 25, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* RH WING #12 SLAT CLOSURE PANEL SPLIT AND NOT FAIRED TO LOWER WING SKIN. PANEL IS SPLIT APPROX. 2 INCHES OUTBOARD TO INBOARD.**10 CYCLE LIMIT***
- [SDR IPXA2023061639500](https://openairdocs.org/sdr/IPXA2023061639500), May 29, 2023: FITTING. BROKEN. FAULT - FOUND MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING BROKEN, LOC: STA 764 BL0, STA 764 LBL 47.5, STA 942 BL0, STA 1021 LBL 47.5, STA 1043 RBL 47.5, STA
- [SDR IPXA2022100286786](https://openairdocs.org/sdr/IPXA2022100286786), Sep 30, 2022: WARNING MESSAGE. FALSE ACTIVATION. INSPECTION TYPE:N/A**ATB** - AT ATLITUDE RECEIVED "AILERON LOCKOUT" MSG PERFORMED QRH RESULTED IN ATBR&R L AND R ADC PER TECH REQ. PER AMM 32-12-01. OPS CHECK G
- [SDR IPXA2021061470590](https://openairdocs.org/sdr/IPXA2021061470590), Jun 14, 2021: FAN. OUT OF BALANCE. ATB NO EMERG DCLD-NO EMERG EQUIP USED-LANDED UNEVENTFLY-AC OOS** DURING CL/OUT VIB ON LH ENG IND FAN 3.3 & INCREASED TO 4.0 AVER 3.5 3.7 @ CRZ VIB STEADY @ 1.9-
- [SDR IPXA2021052569803](https://openairdocs.org/sdr/IPXA2021052569803), May 17, 2021: SEAT TRACK. BROKEN. INSPECTION TYPE:C13BROKEN ON SEAT TRACK ON MAIN DECK CGO COMPARTMENT BETWEEN STA 467.45-STA 511.45,LBL 88.5.REPAIR I.A.W BOEING SR:3-5033972797 AND UPS EO B767-
- [SDR IPXA2021052369717](https://openairdocs.org/sdr/IPXA2021052369717), May 17, 2021: SEAT TRACK. CORRODED. INSPECTION TYPE:C13CORROSION ON SEAT TRACK ON MAIN DECK CGO COMPARTMENT BETWEEN STA 610 AND STA 654, RBL88.5.REPAIR I.A.W. BOEING SR:3-5034191698 AND UPS EO B76
- [SDR IPXA2021052369716](https://openairdocs.org/sdr/IPXA2021052369716), May 17, 2021: STIFFENER. CRACKED. INSPECTION TYPE:C13CRACK ON CENTER WING TANK STIFFENER (P/N:111T2011-6) ON STA 785.9 , RBL 55.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR2 REV.80.01 AND UPS 
- [SDR IPXA2021052369715](https://openairdocs.org/sdr/IPXA2021052369715), May 17, 2021: STIFFENER. CRACKED. INSPECTION TYPE:C13CRACK ON CENTER WING TANK STIFFENER (P/N:111T2005-8) ON STA 785.9,RBL 11.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.80.01 AND UPS E
- [SDR IPXA2021052369714](https://openairdocs.org/sdr/IPXA2021052369714), May 17, 2021: STIFFENER. CRACKED. INSPECTION TYPE:C13CRACK ON CENTER WING TANK STIFFENER(P/N:111T2005-7) ON STA 785.9,LBL 11.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.80.01 AND UPS EO
- [SDR IPXA2020012951515](https://openairdocs.org/sdr/IPXA2020012951515), Jan 29, 2020: WARNING MESSAGE. ILLUMINATED. STATUS MESSAGE L ENG FIRE LP 1 APPEARED DURING CLIMB TO CRUISE ALTITUDE. DEFERRED IAW MEL 26-11-1-1
- [SDR IPXA2019061754291](https://openairdocs.org/sdr/IPXA2019061754291), Jun 2, 2019: PRESSURE DECK. CRACKED. INSPECTION TYPE:C12 CRACK ON WEB (P/N:145T8755-27) OF WHEEL WELL PRESSURE DECK BETWEEN STA 955 - STA 977, LBL 11.06 - LBL 33.06.REPAIR I.AW BOEING SRID :4-44919
- [SDR IPXA2019061243122](https://openairdocs.org/sdr/IPXA2019061243122), May 31, 2019: STIFFENER. CRACKED. INSPECTION TYPE:C12CRACK ON VERTICAL STIFFENER AT WHEEL WELL BULKHEAD AT STA 287, RBL 25.REPAIR I.A.W UPS EO B767-5310-20118-F AND 767-300F SRM 51-70-12 GENERAL
- [SDR IPXA2019061443263](https://openairdocs.org/sdr/IPXA2019061443263), May 30, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C12DAMAGE ON M/D CARGO FLOOR PANEL AT STA985 - STA 1087,RBL77 - RBL 88 , PNL NO.242VFF.FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO.B767-5320
- [SDR IPXA2019061443262](https://openairdocs.org/sdr/IPXA2019061443262), May 30, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C12DAMAGE ON M/D CARGO FLOOR PANEL AT STA 731-STA834,RBL 11 - RBL 33, PNL NO.242AFF.FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO.B767-5320-96
- [SDR IPXA2018121036759](https://openairdocs.org/sdr/IPXA2018121036759), Dec 9, 2018: BUMPER. MISSING. CREW ENTRY DOOR INTERIOR HANDLE BUMPER MISSING & PANEL DAMAGED.
- [SDR IPXA2018100394594](https://openairdocs.org/sdr/IPXA2018100394594), Sep 28, 2018: SEAL. TORN. ENTERY DOOR INSIDE SEAL WAS TORN. REPLACED TRIM SEAL AS REQUIRED IAW AMM 20-00-00.
- [SDR IPXA2018040928359](https://openairdocs.org/sdr/IPXA2018040928359), Apr 9, 2018: SKIN. DENTED. LEFT WING INBD AFT FLAP T/E WEDGE, LOWER SKIN DENTED. REPAIRED IAW EO B767-5750-67013-B.
- [SDR IPXA2017073119987](https://openairdocs.org/sdr/IPXA2017073119987), Jul 31, 2017: SEAL. MISSING. RUBBER SEAL ON FWD EDGE OF CREW DOOR MISSING. INSTALLED THE RUBBER SEAL IAW AMM 52-12-02.
- [SDR IPXA2017073119995](https://openairdocs.org/sdr/IPXA2017073119995), Jul 30, 2017: HANDLE. WORN. EXTERIOR CREW ENTRANCE DOOR HANDLE INTERNAL PANEL WORN. REMOVED AND REPLACED THE DOOR HANDLE IAW CMM 52-11-12, OPS CHECKED GOOD.
- [SDR IPXA2017051817262](https://openairdocs.org/sdr/IPXA2017051817262), May 16, 2017: SKIN. CRACKED. INSPECTION TYPE: C11, CRACK FOUND ON THE RT FUSELAGE SKIN AT BS 1725.5, STRINGER 7R. REPAIRED IAW EO B767-5330-24301-D, APPX. C AND SRM 53-80-01-2R-5, REPAIR 5,
- [SDR IPXA2017051717203](https://openairdocs.org/sdr/IPXA2017051717203), May 8, 2017: SKIN. CRACKED. INSPECTION TYPE: C11, CRACK WAS FOUND ON THE LEADING EDGE SKIN OF THE LT WING NR 4 SLAT AT INBD TRACK AREA REPAIRED IAW SRM 57-43-01-2R-2, REPAIR 2, REV 68.
- [SDR IPXA2017041216074](https://openairdocs.org/sdr/IPXA2017041216074), Apr 12, 2017: DOOR. LACK OF LUBE. MAIN CABIN DOOR TAB (YELLOW) VERY STIFF. HARD TO CLOSE. LUBED MAIN CABIN DOOR IAW 52-12-00. OPS CK OK.

All 159: https://openairdocs.org/aircraft/N312UP/reports.md

## STCs that may be installed (OpenAirDocs) (5)

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 CF6-80C2B6F)

- [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
- [STC SE01478CH](https://openairdocs.org/stc/SE01478CH): Installation of Cook Airtomic alignment joint p/n AIR 22912. Cook Airtomic
- [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
- [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. Lists CF6-80 Series

## Related

- Other Boeing 767-34AF aircraft: https://openairdocs.org/model/boeing-767-34af/aircraft.md
- The GE CF6-80C2B6F engine: https://openairdocs.org/engine/ge-cf6-80c2b6f.md

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