# N342UP: 2011 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: 37865
- Year built: 2011
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 7, 2011
- Certificate issued: April 18, 2011
- Expires: April 30, 2030
- Mode S code: A3C68C
- 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=342UP
- Page: https://openairdocs.org/aircraft/N342UP

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 (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 OPS15IA017](https://openairdocs.org/ntsb/OPS15IA017), Apr 12, 2015: Boeing 767 34AF (N342UP), Miami, FL, incident, no damage. Probable cause: The controller's issuance of a landing clearance to an arriving aircraft while another aircraft was in position on the same runway. Contributing to the incident was the controller's non-compliance…

## FAA accident and incident reports

None matched to N342UP.

## Service difficulty reports (41)

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 IPXA2026091176660](https://openairdocs.org/sdr/IPXA2026091176660), Sep 10, 2026: SEAL. LEAKING. ENTRY DOOR POTENTIAL SEAL LEAK , LEAKING NOISE MOST OF THE FLIGHT ALL ALTITUDES, SOUND APPEARS TO COME FROM BOTTOM OF DOOR FOUND SEALANT MISSING FROM SEAMS IN S
- [SDR IPXA2026091076660](https://openairdocs.org/sdr/IPXA2026091076660), Sep 10, 2026: SEAL. LEAKING. ENTRY DOOR POTENTIAL SEAL LEAK , LEAKING NOISE MOST OF THE FLIGHT ALL ALTITUDES, SOUND APPEARS TO COME FROM BOTTOM OF DOOR PRESSURE CHECK ENTRY DOOR IAW AMM 05-
- [SDR IPXA2026060872758](https://openairdocs.org/sdr/IPXA2026060872758), Jun 8, 2026: TEST BUTTON. INOPERATIVE. WHEEL WELL FIRE DETECTION TEST DOESN'T WORK WHEN TEST BUTTON IN FLIGHTDECK PRESSED. T/S CARRIED OUT IAW FIM 26-17 FAULT TREE 803 REV. 148. FOUND WHEELWELL FIRE 
- [SDR IPXA2025102829407](https://openairdocs.org/sdr/IPXA2025102829407), Oct 24, 2025: FLAP. DAMAGED. BIRD STRIKE DAMAGE TO RIGHT WING OUTBOARD FLAP LEADING EDGE. COMPLETED REPAIR TO LEADING EDGE PANEL PER SRM 51-70-05-0G-0 ALL STEPS OF REPAIR COMPLETE. REPAIR P
- [SDR IPXA2025102429407](https://openairdocs.org/sdr/IPXA2025102429407), Oct 24, 2025: FLAP. DAMAGED. BIRD STRIKE DAMAGE TO RIGHT WING OUTBOARD FLAP LEADING EDGE. REMOVED PANEL 666AT AND ROUTED TO SHEET METAL SHOP FOR REPAIR.
- [SDR IPXA2025062264991](https://openairdocs.org/sdr/IPXA2025062264991), Jun 22, 2025: FMC. FAULTED. ATB FMC LOCKED UP WITH STBY ONE MSG PRESENT (FULL WRITEUP IN FAULT DESCRIPTION). + PERFORMED TROUBLE SHOOTING REF B767 FIM 34-61 FAULT TREE 854,NO FAULTS FOUND.
- [SDR IPXA2025020716359](https://openairdocs.org/sdr/IPXA2025020716359), Feb 7, 2025: NONE. NONE. ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF STA 1725.5 BETWEEN S-36L AND S-36R) [T3F18E0013XJ0] ACCOMPLISHED SDR. REVIE
- [SDR IPXA2025020220164](https://openairdocs.org/sdr/IPXA2025020220164), Feb 1, 2025: SKIN. DEBONDED. DISBOND PNL, RT WING NR 8 L/E SLAT INBD, SIDE INNER UPPER WEDGE. INST THE EXT DBLR WITH FILM ADHESIVE & CURE IAW SRM 51-70-10-2R-0 PARA 18 & 20. PERFORMED NDT/U
- [SDR IPXA2025020491420](https://openairdocs.org/sdr/IPXA2025020491420), Jan 26, 2025: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578 RBL 80 INBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. (REPLACE). REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.91. INSTALL NEW
- [SDR IPXA2025020491290](https://openairdocs.org/sdr/IPXA2025020491290), Jan 26, 2025: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. (REPLACE). REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.91. INSTALL NE
- [SDR IPXA2025020491462](https://openairdocs.org/sdr/IPXA2025020491462), Jan 26, 2025: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA. (REPLACE). REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.91 INSTALL NEW 
- [SDR IPXA2025013192484](https://openairdocs.org/sdr/IPXA2025013192484), Jan 26, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 146T5869-65 PANEL NO: 251JFF STA 1197+22~STA 1197+110 LBL 55~LBL 77. (REPAIR). FABRICATE A NEW FLOOR PANEL I.
- [SDR IPXA2025013192466](https://openairdocs.org/sdr/IPXA2025013192466), Jan 26, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 146T5869-9 PANEL NO: 241KFF STA 1197+22~STA 1197+110 LBL 77~LBL 88. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A
- [SDR IPXA2025013192454](https://openairdocs.org/sdr/IPXA2025013192454), Jan 26, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 145T5876-68 PANEL NO: 241AFF STA 731~STA 834 LBL 11~RBL 11. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO
- [SDR IPXA2025013192451](https://openairdocs.org/sdr/IPXA2025013192451), Jan 26, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 146T5869-135 PANEL NO: 251XFF STA 1440~STA 1540 LBL 77.5~LBL 54.75. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A
- [SDR IPXA202403040049](https://openairdocs.org/sdr/IPXA202403040049), Feb 21, 2024: PITOT HEAD. DAMAGED. LUZ DE CAPT PITOT ENCENDIDA DESPUES DEL ARRANQUE DE MOTORES, PROBETA DE TUBO PITOT DEL CAPITAN DAÑADA CAPT PITOT LIGHT ON AFTER STARTING, PITOT TUBE DAMAGED.
- [SDR IPXA2023012690278](https://openairdocs.org/sdr/IPXA2023012690278), Jan 13, 2023: FLOORBEAM. DAMAGED. INSPECTION TYPE:C6, DAMAGE ON M/D CARGO FLOORBEAM, BS 246, LBL 53. FABRICATED A REPLACEMENT IAW DWG 141T5146 SH 15 REV B, PL REV F AND PSDL REV-. REPLACED IAW S
- [SDR IPXA2022112888472](https://openairdocs.org/sdr/IPXA2022112888472), Nov 28, 2022: SEAL. DETACHED. INSPECTION TYPE:N/ACREW ENTRY DOOR SEAL MAKES VERY LOUD HISSING NOISE IN FLIGHT.PRESSURISATION OKAYFOUND CREW ENTRY DOOR BOTTOM SEAL DETACHED SECURED AND CLEANE
- [SDR IPXA2021121777022](https://openairdocs.org/sdr/IPXA2021121777022), Dec 16, 2021: APU. FAULTED. INSPECTION TYPE:N/ASUPPLEMENTAL SDR**DIVERSION**EMERG DECLARED**A/C LANDED W/OUT INCIDENT**APU FAULT AT FL 390 DIVERTED TO STL. DEFERRED PER MEL 49-11-1A ASSIGN
- [SDR IPXA2020051355257](https://openairdocs.org/sdr/IPXA2020051355257), May 12, 2020: TIRE. DAMAGED. INSPECTION TYPE:N/A** EMERGENCY DECLARED ** THE FIRE TRUCKS FOLOWED THE A/C TO THE RAMP & THE FIRE CHIEF DETERMINED IT WAS SAFE TO TAXI TO THE GATE & FOLLOWED T
- [SDR IPXA2020051155077](https://openairdocs.org/sdr/IPXA2020051155077), May 7, 2020: CONTROL MODULE. INOPERATIVE. INSPECTION TYPE:N/AHYDRAULIC POWER CAME ON PRIOR TO ENGINE START ON PUSHBACK, BOTH YOKES WENT 3/4 FULL LEFT TURN FOR NO REASON. A/P OFF.R/R AILERON RUDDER TRIM 
- [SDR IPXA2019091046567](https://openairdocs.org/sdr/IPXA2019091046567), Sep 10, 2019: BATTERY PACK. DISCHARGED. INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. R&R BATT PACK PER AMM 33-51-07 OPS CHK GOOD. ESR: IPC 33-51-07-32.
- [SDR IPXA2019040864843](https://openairdocs.org/sdr/IPXA2019040864843), Apr 6, 2019: BULB. INOPERATIVE. EXTERIOR EMERGENCY LIGHT INOP. REPLACED THE BULB IAW AMM 33-51-16-962-001 OPS CKS OK
- [SDR IPXA2019012338207](https://openairdocs.org/sdr/IPXA2019012338207), Jan 13, 2019: SKIN PANEL. BROKEN. INSPECTION TYPE:C4 BROKEN ON LOWER SKIN PANEL OF RT WING INBD AFT FLAP NEAR IFS 119.75. REPAIR IAW SRM 57-53-01 REPAIR 1, SRM 51-70-10 REPAIR 2, SRM 51-70-10 GE
- [SDR IPXA2019011837983](https://openairdocs.org/sdr/IPXA2019011837983), Jan 13, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C4 DAMAGE ON M/D CARGO FLOOR PANEL AT STA 834-STA 930, LBL 11 - RBL 11, PNL NR 241FFF. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR B767-5320
- [SDR IPXA2019010737587](https://openairdocs.org/sdr/IPXA2019010737587), Dec 8, 2018: LIGHT. INOPERATIVE. INSPECTION TYPE:N/A EXTERIOR EMERGENCY LIGHT INOP. R&R LAMP W/ REF TO AMM. 33-51-16. LIGHT OPERATES NORMAL P/N ON/OFF 767.
- [SDR IPXA2016062605049](https://openairdocs.org/sdr/IPXA2016062605049), Jun 26, 2016: FLOOR PANEL. PUNCTURED. MCD FLOOR PANEL PUNCTURED POSITION 2R, FABRICATED NEW PANEL IAW EO B767-5320-9693-I.
- [SDR IPXA2015120896506](https://openairdocs.org/sdr/IPXA2015120896506), Dec 7, 2015: FIRE LOOP. MALFUNCTIONED. RIGHT ENGINE FIRE LOOP 1 STATUS MESSAGE. REPLACED THE RT FWD LOWER FIRE LOOP DETECTOR IAW AMM 26-11-02 AND TESTED NORMAL.
- [SDR IPXA2015032287255](https://openairdocs.org/sdr/IPXA2015032287255), Mar 21, 2015: SKIN. DAMAGED. DURING MAJOR MAINTENANCE VISIT NR 6749, FOUND DENT ON SKIN, BULK CARGO DOOR OUTER SURFACE, STA 1447, BETWEEN S-23L AND S-24 L/E, EVALUATED DAMAGE IAW SRM 52-30-
- [SDR IPXA2014011001250](https://openairdocs.org/sdr/IPXA2014011001250), Jan 7, 2014: LAMP. INOPERATIVE. EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP.
- [SDR IPXA2014010201191](https://openairdocs.org/sdr/IPXA2014010201191), Dec 29, 2013: LATCH. BROKEN. CAPTAIN'S OVERHEAD ESCAPE ROPE DOOR LATCH INOPERATIVE. OVERHEAD PANEL ASSY R & R IAW AMM TASK 25-1 4-02. ROPE INSTALLED IAW AMM TASK 25-61-02-682-001, REV 110, 
- [SDR IPXA3680327](https://openairdocs.org/sdr/IPXA3680327), Sep 21, 2013: FLOOR PANEL. DAMAGED. FLOOR PANEL DAMAGED. REPAIRED IAW SRM 53-00-50.
- [SDR IPXA3677437](https://openairdocs.org/sdr/IPXA3677437), Mar 4, 2013: SKIN. DENTED. INSPECTION TYPE:C01, A DENT WAS FOUND ON LT WING NR 3 SLAT UPPER SURFACE OF WEDGE AREA. DAMAGE SIZE IS MEASURED AS 1.75"(LENGTH) X 1.5"(WIDTH) X 0.031"(DEPTH) A
- [SDR IPXA3677436](https://openairdocs.org/sdr/IPXA3677436), Mar 4, 2013: SKIN. DENTED. INSPECTION TYPE:C01, A DENT WAS FOUND ON LT WING NR 3 SLAT UPPER SURFACE OF WEDGE AREA. DAMAGE SIZE MEASURED AS 0.88" (LENGTH) X 0.62"(WIDTH) X 0.025" (DEPTH) A
- [SDR IPXA3677435](https://openairdocs.org/sdr/IPXA3677435), Mar 4, 2013: SKIN. DENTED. INSPECTION TYPE:C01, A DENT WAS FOUND ON LT WING NR 3 SLAT UPPER SURFACE OF WEDGE AREA. DAMAGE SIZE MEASURED AS 0.62" (LENGTH) X 0.55" (WIDTH) X 0.012"(DEPTH) A
- [SDR IPXA3677434](https://openairdocs.org/sdr/IPXA3677434), Mar 4, 2013: SKIN. DENTED. A DENT WAS FOUND ON LT WING NR 3 SLAT UPPER SURFACE OF WEDGE AREA. DAMAGE SIZE IS MEASURED AS 0.78" (LENGTH) X 0.55" (WIDTH) X 0.012" (DEPTH) AT OSS 801.5. REPA
- [SDR IPXA3677431](https://openairdocs.org/sdr/IPXA3677431), Mar 4, 2013: WEDGE. DENTED. INSPECTION TYPE:C01, LT WING NR 3 SLAT T/E WEDGE ASSY UPPER SKIN DENTED AT OSS 819. DAMAGE SIZE IS MEASURED AS 1.0" (LENGTH) X 0.66"(WIDTH) X 0.013"(DEPTH) AND 
- [SDR IPXA2676466](https://openairdocs.org/sdr/IPXA2676466), Dec 15, 2012: FLOOR PANEL. DENTED. MAIN CARGO DECK FLOOR PANEL POS NR 12L OTBD HAS DENT CENTER OF PANEL. REPAIRED IAW SRM 53-00-50-2R.
- [SDR IPXA2672017](https://openairdocs.org/sdr/IPXA2672017), Mar 4, 2012: FLOOR PANEL. DAMAGED. MAIN CARGO FLOOR PANEL HAS A 3" BY 1" HOLE AT POS 6/7 PANEL CENTER, IDENTIFIED PANEL FROM POS 6/7 CENTER AS PN 145T5876-60 IAW EO B767-5320-9693H. FABRICATED A 
- [SDR IPXA2672016](https://openairdocs.org/sdr/IPXA2672016), Mar 4, 2012: FLOOR PANEL. DAMAGED. MAIN CARGO COMPARTMENT FLOOR PANEL HAS A 3" BY 1" HOLE AT POSITION 4/5 CENTER PANEL 31" AFT OF POS 4. IDENTIFIED PANEL FROM POSITION 4/5 CENTER AS PN 143T5876-1
- [SDR IPXA2672015](https://openairdocs.org/sdr/IPXA2672015), Mar 4, 2012: FLOOR PANEL. DAMAGED. MAIN CARGO COMPARTMENT FLOOR PANEL HAS A .5" DIAMETER HOLE AT POSITION 4/5 CENTER PANEL, 59" FWD FROM POS 4. IDENTIFIED PANEL FROM POS 4/5 CENTER AS PN 143T5876

## 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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