# N343UP: 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: 37945
- Year built: 2011
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 27, 2011
- Certificate issued: May 6, 2011
- Expires: May 31, 2027
- Mode S code: A3CA43
- 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=343UP
- Page: https://openairdocs.org/aircraft/N343UP

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 N343UP.

## FAA accident and incident reports

None matched to N343UP.

## Service difficulty reports (48)

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 IPXA2025010869446](https://openairdocs.org/sdr/IPXA2025010869446), Jan 8, 2025: NONE. NONE. ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) ACCOMPLISHED.
- [SDR IPXA2025010856429](https://openairdocs.org/sdr/IPXA2025010856429), Jan 7, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-89. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. CONDITION CHECK IS SATISFACTORY. I.A.
- [SDR IPXA2025010856389](https://openairdocs.org/sdr/IPXA2025010856389), Jan 7, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 143T5876-109. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. CONDITION CHECK IS SATISFACTORY. I.A
- [SDR IPXA2025010856493](https://openairdocs.org/sdr/IPXA2025010856493), Jan 7, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-132. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. CONDITION CHECK IS SATISFACTORY. I.A
- [SDR IPXA2025010856464](https://openairdocs.org/sdr/IPXA2025010856464), Jan 7, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-134. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. CONDITION CHECK IS SATISFACTORY. I.A
- [SDR IPXA2025010856446](https://openairdocs.org/sdr/IPXA2025010856446), Jan 7, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-133. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. CONDITION CHECK IS SATISFACTORY. I.A
- [SDR IPXA2025010856415](https://openairdocs.org/sdr/IPXA2025010856415), Jan 7, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 145T5876-7. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. CONDITION CHECK IS SATISFACTORY. I.A.W
- [SDR IPXA2025011645897](https://openairdocs.org/sdr/IPXA2025011645897), Jan 6, 2025: BUMPER. MISSING. FOUND L1 ENTRY DOOR BUMPER MISSING (REPLACE). I.A.W AMM 52-12-02-404-025 REV.144 INSTALL BUMPER. CONDITION CHECK NORMAL. REVIEWED
- [SDR IPXA2025010645897](https://openairdocs.org/sdr/IPXA2025010645897), Jan 6, 2025: BUMPER. MISSING. FOUND L1 ENTRY DOOR BUMPER MISSING (REPLACE)
- [SDR IPXA2024071630231](https://openairdocs.org/sdr/IPXA2024071630231), Jul 16, 2024: COVER. OUT OF ALIGNMENT. MAIN ENTRY DOOR ARMING LEVER HINGED COVER WILL NOT LAY FLAT. DEFERRED MAIN ENTRY DOOR ARMING LEVER HINGED COVER PER MEL 52-11-2. PLACARD INSTALLED. NO DMP. INSU
- [SDR IPXA2024011161702](https://openairdocs.org/sdr/IPXA2024011161702), Jan 10, 2024: DOOR. LEAKING. *** SUPPLEMENTAL SDR *** AIR LEAK IN MAIN DOOR (CREW ENTRY DOOR) LEAKING DURING ENTIRE FLIGHT GOOD PRESSURIZATION REPAIRED CREW ENTRY DOOR LOWER SEAL PER AMM 52
- [SDR IPXA2024011061702](https://openairdocs.org/sdr/IPXA2024011061702), Jan 10, 2024: UNKNOWN. UNKNOWN. AIR LEAK IN MAIN DOOR (CREW ENTRY DOOR) LEAKING DURING ENTIRE FLIGHT GOOD PRESSURIZATION REPAIRED CREW ENTRY DOOR LOWER SEAL PER AMM 52-09-00.
- [SDR IPXA2023011890014](https://openairdocs.org/sdr/IPXA2023011890014), Jan 18, 2023: FLOORBEAM. DAMAGED. INSPECTION TYPE:C6, DAMAGE ON M/D CGO FLOOR BEAM SUPPORT AT STA 246, LBL 47FABRICAT THE REPLACEMENT CLIP PER BOEING DWG NO.:141T5146 SH 15 REV. ''B'', PL REV.''
- [SDR IPXA2023011648879](https://openairdocs.org/sdr/IPXA2023011648879), Jan 14, 2023: FLOOR PANEL. DAMAGED. INSPECTION TYPE: C6, MAJOR REPAIR, DAMAGE ON M/D CARGO FLOOR PANEL AT STA 412 - STA 544, RBL 11 - LBL 11.FABRICATE THE REPLACEMENT FLOOR PANEL PER NO. B767-5320
- [SDR IPXA2023011389857](https://openairdocs.org/sdr/IPXA2023011389857), Jan 13, 2023: THRUST REVERSER. INOPERATIVE. CRACK-SUPPORT FITTING, NR 1 ENGINE RT THRUST REVERSER FORWARD TORQUE BOX LOWER ACTUATOR REAR UPPER AND DOWNACCOMPLISHED NO.1 ENG R/H T/R REMOVE/INSTALL I.A.W UP
- [SDR IPXA2023011389856](https://openairdocs.org/sdr/IPXA2023011389856), Jan 13, 2023: THRUST REVERSER. INOPERATIVE. CRACK-J-RING, NR 1 ENG LT THRUST REVERSER J-RING UPPER SIDEACCOMPLISHED NO.1 ENG L/H T/R REMOVE/INSTALL I.A.W UPS EO B767-7830-52256-K STEP 48. ORIG SUBMISSION 
- [SDR IPXA2023011389844](https://openairdocs.org/sdr/IPXA2023011389844), Jan 4, 2023: STIFFENER. CRACKED. INSPECTION TYPE:06*MAJOR REPAIR* CRACK ON CENTER WING TANK STIFFENER (P/N:111T2008-12) ON STA 785.9, RBL 33.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV
- [SDR IPXA2022111488094](https://openairdocs.org/sdr/IPXA2022111488094), Nov 13, 2022: DOOR. UNSECURE. LOUD SQUEAL FROM SILL AREA OF MAIN ENTRANCE DOOR BEGINNING AT 6.5PSI DIFF AND REMAINS THROUGHOUT FLT SUSPECT AREA APPX 4IN FWD OF AFT DOOR GRASP HANDLE RESECURE
- [SDR IPXA2021092774333](https://openairdocs.org/sdr/IPXA2021092774333), Sep 25, 2021: DOOR. NONE. INSPECTION TYPE:NA** SUPPLEMENTAL SDR**FWD ENTRY DOOR MSG ON EICAS.ASSIGNED M757745 IN REF TO MEL 52-71-1-1 DMP C/W PLACARDS INSTALLEDT/S SYSTEM REF FIM 52-71-0
- [SDR IPXA2021083173380](https://openairdocs.org/sdr/IPXA2021083173380), Aug 31, 2021: UNKNOWN. NOISE. INSPECTION TYPE:N/ALOUD LOW FREQUENCY NOISE(SUSPECT AIR LEAK)COMINE FROM AREA BELOW FLT DECK.NOISE STARTED AT 12100FT AND THEN GRADUALLY WENT AWAY BETWEEN 20000
- [SDR IPXA2021021165551](https://openairdocs.org/sdr/IPXA2021021165551), Feb 11, 2021: INERTIA REEL. UNSECURE. INSPECTION TYPE:NAFLIGHT CREW NOTICED 4TH FROM THE FWD END OF EMERGENCY ESCAPE INERTIAL DESCENT DEVICE FALLEN DOWNR/R'D WITH NEW REEL (767) EMER ESCAPE INERTIAL
- [SDR IPXA2020022645418](https://openairdocs.org/sdr/IPXA2020022645418), Feb 22, 2020: SEAL. LEAKING. INSPECTION TYPE:N/ASIGNIFICANT PRESSURIZATION LEAK SOUNDS LIKE COMING FROM THE MAIN CABIN ENTRY DOOR AREAFOUND 14" SECTION OF LOWER MED SEAL PULLED OUT OF RETAI
- [SDR IPXA2020011750978](https://openairdocs.org/sdr/IPXA2020011750978), Jan 15, 2020: UNKNOWN. LEAKING. INSPECTION TYPE:N/A CREW ENTRY DOOR LEAKS. NOISE STARTED AROUND 5000FT DURING CLIMB OUT. A/C PRESSURIZATION IS NORMAL. CREW ENTRY DOOR INSPECTION AND LUBRICATIO
- [SDR IPXA2019082324912](https://openairdocs.org/sdr/IPXA2019082324912), Aug 20, 2019: SEAL. LEAKING. AIR LEAK SOUND CREW ENTRY DOOR. PRESSURIZATION OK, RESEATED LOOSE PRESSURE SEAL ON BOTTOM OF DOOR IAW B767 AMM 52-09-01-424-019. ACCOMPLISHED PRESSURE LEAKAGE T
- [SDR IPXA2019061243058](https://openairdocs.org/sdr/IPXA2019061243058), Jun 8, 2019: SEAL. DETACHED. LOUD AIR LEAK NOISE COMING FROM BOTTOM OF CREW ENTRY DOOR. FOUND LOWER DOOR SEAL OUT OF RETAINER REINSTALLED SEAL IN RETAINER PER MM 52-09-01-424-019 LEAK CHECK
- [SDR IPXA2019052442434](https://openairdocs.org/sdr/IPXA2019052442434), May 23, 2019: DOOR SEAL. OUT OF POSITION. INSPECTION TYPE:N/A CREW ENTRY DOOR HAS NOISE FROM AIRLEAK. NOISE SEEMS TO COME FROM LOWER AFT CORNER OF DOOR. CABIN ALT WAS NORMAL. AIR LEAK NOISE STARTED JUST
- [SDR IPXA2019051041964](https://openairdocs.org/sdr/IPXA2019051041964), May 9, 2019: DOOR SEAL. OUT OF POSITION. INSPECTION TYPE:SDR CREW ENTRY DOOR EXCESSIVE NOISE LVL-AIR LEAK APPEARS TO BE LOWER LEFT.INSPECTED DOOR SEAL/ENTRY FOUND LOWER SEAL OUT OF SEAL RETAINER. REINS
- [SDR IPXA2019040314688](https://openairdocs.org/sdr/IPXA2019040314688), Mar 31, 2019: SEAL. TORN. CREW ENTRY DOOR SEAL APPEARS TO BE TORN AT THE BOTTOM MIDDLE OF THE DOOR. LOUD HISSING NOISE.ENTRY DOOR SEAL INSTALLED ACCORDING TO AMM TASK 52-09-01-424-019. E
- [SDR IPXA2019030139600](https://openairdocs.org/sdr/IPXA2019030139600), Mar 1, 2019: DOOR SEAL. DISLODGED. INSPECTION TYPE:N/A PRESSURIZATION LEAK AT CABIN DOOR SEAL. ACCOMPLISHED GENERAL VISUAL INSPECTION PEROF CREW ENTRY DOOR IAW AMM TASK 52-05-02-212-812. FOUND LW
- [SDR IPXA2019011837986](https://openairdocs.org/sdr/IPXA2019011837986), Jan 10, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C4 DAMAGE ON M/D CARGO FLOOR PANEL AT STA 285- STA 412, RBL 77- RBL 88, PNL NR 222DFF. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR B767-5320
- [SDR IPXA2019011837985](https://openairdocs.org/sdr/IPXA2019011837985), Jan 10, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C4 DAMAGE ON M/D CARGO FLOOR PANEL AT STA 1353- STA 1480, LBL 11- RBL 11, PNL NR 251SFF. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR B767-53
- [SDR IPXA2019011837984](https://openairdocs.org/sdr/IPXA2019011837984), Jan 10, 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 IPXA2018112136189](https://openairdocs.org/sdr/IPXA2018112136189), Nov 21, 2018: SEAL. LOOSE. A LOUD HISS FROM THE BOTTOM OF ENTRY DOOR, LEFT SIDE. NOTICED DURING CLIMBOUT ABOVE 7000 FEET. THE SEAL WAS FOUND LOOSE AT THE BOTTOM OF ENTRY DOOR. SEAL FASTEN
- [SDR IPXA2018070931516](https://openairdocs.org/sdr/IPXA2018070931516), Jul 7, 2018: COVER. BROKEN. CREW ENTRY DOOR ARMING LEVER HINGE COVERS BROKEN. INSTALLED A NEW LINING PANEL. ARMING LEVER HINGED COVER INSTALLED IAW MM 52-12-02.
- [SDR IPXA2018010725176](https://openairdocs.org/sdr/IPXA2018010725176), Jan 5, 2018: FAN. VIBRATION. AIR TURNBACK, DURING CLIMB OUT, NR 1 ENGINE FAN VIBRATION REACHED 5.0 DURING CRUISE FLIGHT. WENT DOWN TO 1 DURING CRUISE. STEP CLIMB FROM FL 330 TO 370 THE NR 1
- [SDR IPXA2017022214330](https://openairdocs.org/sdr/IPXA2017022214330), Feb 22, 2017: STRUCTURE. CHAFED. INSPECTION TYPE : C, FOUND CHAFING ON THE NR 1 NACELLE CORE COWL EXTERNAL AFT UPPER CHAFED.
- [SDR IPXA2017011712842](https://openairdocs.org/sdr/IPXA2017011712842), Jan 16, 2017: START VALVE. STUCK. LT ENG START VALVE STUCK, MECHANIC WAS ABLE TO UNSTICK VALVE. NORMAL START ON NEXT ATTEMPT. LEFT ENGINE START VALVES PER MEL CDL 80-00-2-1 ***ETOPS REPORT FILED
- [SDR IPXA2017010512413](https://openairdocs.org/sdr/IPXA2017010512413), Jan 4, 2017: COWL DOOR. CRACKED. UPON WALKAROUND FOUND LT ENGINE INLET NOSE COWL CRACKED AT 12:00 POS. (APPROX 4: LONG) REMOVED & REPLACED LT ENG MAIN COWL REF MM 71-11-01-404-005-H00 EFF SOURC
- [SDR IPXA2016061904788](https://openairdocs.org/sdr/IPXA2016061904788), Jun 19, 2016: DOOR SEAL. DAMAGED. ATB-LOUD HISSING SOUND FROM CREW ENTRY DOOR PASSING 16000, NO CHANGE AT FL 230. UPON INVESTIGATION, SOUND WAS COMING FROM LOWER PART OF DOOR WITH DAYLIGHT VISIB
- [SDR IPXA2016052503854](https://openairdocs.org/sdr/IPXA2016052503854), May 25, 2016: GASKET. LEAKING. APU- FLOW SENSING MODULE PRESSURE SENSOR GASKET SHOWS SIGNS OF LEAKAGE. REF TC 49-100-00 REPLACED GASKET IAW AMM 49-53-08-4.
- [SDR IPXA2015052389350](https://openairdocs.org/sdr/IPXA2015052389350), May 22, 2015: FAN. FAILED. INSPECTION TYPE:ETOP, ELECTRICAL BURNING ODOR IN COCKPIT, NOT ABLE TO IDENTIFY, RAN ALL ELECTRICAL SYS, CHECKED EQUIP COOLING, IN ALL MODES, HYD-ELEC/RAN FOR 30
- [SDR IPXA2015010585201](https://openairdocs.org/sdr/IPXA2015010585201), Jan 1, 2015: FLOOR PANEL. DAMAGED. 1" X 1" HOLE IN FLOOR PANEL TOP SKIN AND CORE AND BOTTOM SKIN. FABRICATED NEW PANEL IAW EO B767-5320-9693-H.
- [SDR IPXA2014122285115](https://openairdocs.org/sdr/IPXA2014122285115), Dec 20, 2014: LAMP. INOPERATIVE. LOWER EXTERNAL EMERGENCY LIGHTS INOPERATIVE. REPLACED THE LAMP. OPS CHECKED NORMAL IAW AMM 33-51-16-201.
- [SDR IPXA2014062083360](https://openairdocs.org/sdr/IPXA2014062083360), Jun 19, 2014: RETAINER. DAMAGED. RETAINER FOR FLIGHT COMPARTMENT INGRESS ROPE AT AFT FRAME ON FWD ENTRY DO DOOR DAMAGED. R & R RETAINER FOR FLT COMPARTMENT INGRESS ROPE AT AFT FRAME OF FWD ENTR
- [SDR IPXA3677481](https://openairdocs.org/sdr/IPXA3677481), Mar 11, 2013: FLOOR PANEL. DENTED. INSPECTION TYPE:C01 2 DENTS ON M/D CARGO FLOOR PANEL 231FFF. REPAIRED IAW EO NR B767-5320-9693-H.
- [SDR IPXA12672518](https://openairdocs.org/sdr/IPXA12672518), Mar 22, 2012: AUTOTHROTTLE SYS. MALFUNCTIONED. DUE TO A BURNING ODOR IN COCKPIT, WITH AUTOPILOT ENGAGED THRUST LEVERS CAME BACK RAPIDLY AND SPEED DEGRADED 20KTS, HAD TO PUSH THRUST LEVERS UP AND THEN NOTICED
- [SDR IPXA1669548](https://openairdocs.org/sdr/IPXA1669548), Oct 2, 2011: FLOOR PANEL. DAMAGED. HOLE IN FLOOR PANEL AT POS 4 ON MCD. REPAIRED FLOOR PANEL IAW SRM 53-00-50.
- [SDR IPXA1666357](https://openairdocs.org/sdr/IPXA1666357), Apr 29, 2011: FLOORBOARD. PUNCTURED. INSPECTION TYPE:MOD, FLOORBOARD PUNCTURED AT STA 360, RBL 6. REMOVED, FABRICATED AND INSTALLED NEW FLOORBOARD IAW AMM 25-57-05-4, AMM 25-58-01-4, AMM 53-01-06-4

## 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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