# N344UP: 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: 37866
- Year built: 2011
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 7, 2011
- Certificate issued: June 17, 2011
- Expires: June 30, 2027
- Mode S code: A3CDFA
- 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=344UP
- Page: https://openairdocs.org/aircraft/N344UP

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 N344UP.

## FAA accident and incident reports

None matched to N344UP.

## Service difficulty reports (40)

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 IPXA2026082611932](https://openairdocs.org/sdr/IPXA2026082611932), Aug 25, 2026: CONTROL PANEL. FAULTED. ON DEPARTURE FOUND EXTERIOR EMERGENCY LIGHTS ON WITH SWITCH IN THE ARMED POS. R&R EMERGENCY LIGHTS PANEL ASSY PER AMM 33-51-08/401
- [SDR IPXA2026062264476](https://openairdocs.org/sdr/IPXA2026062264476), Jun 20, 2026: BULB. INOPERATIVE. ENTRY DOOR EMERGENCY LIGHT(L313) INOPERATIVE. REMOVED AND REPLACED INOPERATIVE BULB IAW AMM 33-51-03. OPS CHECK OF EMERGENCY LIGHTS NORMAL.
- [SDR IPXA2026052141708](https://openairdocs.org/sdr/IPXA2026052141708), May 12, 2026: SENSOR. OUT OF LIMITS. AIR TURN BACK, FWD CARGO DOOR MESSAGE ILLUMINATED IN CLIMB OUT. INSPECTED AND MEASURED SENSORS S214, S215, S893 PER AMM 52-33-00/501. FOUND SENSOR S214 OUT OF L
- [SDR IPXA2026051241708](https://openairdocs.org/sdr/IPXA2026051241708), May 12, 2026: WARNING MESSAGE. ILLUMINATED. AIR TURN BACK, FWD CARGO DOOR MESSAGE ILLUMINATED IN CLIMB OUT. DEFERRED PER MEL 52-71-1-1B. PLACARD INSTALLED.
- [SDR IPXA2025022484603](https://openairdocs.org/sdr/IPXA2025022484603), Feb 11, 2025: WARNING MESSAGE. FALSE ACTIVATION. CLIMBING OUT OF APPROX 300 FT RECEIVED FWD CARGO DOOR MESSAGE AND ANNUNI. RAN CK LIST. LIGHT WENT OUT BUT CAME BACK ON AS SOON AS WE STARTED TO CLIMB AGAIN. PER
- [SDR IPXA2025021184603](https://openairdocs.org/sdr/IPXA2025021184603), Feb 11, 2025: WARNING MESSAGE. ILLUMINATED. *SDR FILED OPEN* *AIR TURN BACK* CLIMBING OUT OF APPROX 300 FT RECEIVED FWD CARGO DOOR MESSAGE AND ANNUNI. RAN CK LIST. LIGHT WENT OUT BUT CAME BACK ON AS SOON 
- [SDR IPXA2025011089555](https://openairdocs.org/sdr/IPXA2025011089555), Jan 2, 2025: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA (REPLACE). INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO
- [SDR IPXA2025011089611](https://openairdocs.org/sdr/IPXA2025011089611), Jan 2, 2025: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD IN BULK CARGO COMPARTMENT RIGHT AREA (REPLACE). INSTALL NEW PART I.A.W SRM 51-40-02-0G REV.91 AND BOEING NO.14
- [SDR IPXA2025010693036](https://openairdocs.org/sdr/IPXA2025010693036), Jan 2, 2025: FLOOR PANEL. DEBONDED. FOUND MAIN DECK CARGO FLOOR PANEL DISBOND P/N: 143T5876-112 (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. CONDITION CHECK IS SATISFACTORY.
- [SDR IPXA2025010183712](https://openairdocs.org/sdr/IPXA2025010183712), Jan 1, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 146T5869-134, PANEL NO : 252UFF (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. CONDITION CHECK I
- [SDR IPXA2025010183757](https://openairdocs.org/sdr/IPXA2025010183757), Jan 1, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 146T5869-137, PANEL NO : 251AGF (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. CONDITION CHECK I
- [SDR IPXA2025010183702](https://openairdocs.org/sdr/IPXA2025010183702), Jan 1, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 146T5869-10, PANEL NO : 252HFF (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. CONDITION CHECK IS
- [SDR IPXA2024072597199](https://openairdocs.org/sdr/IPXA2024072597199), Jul 25, 2024: WINGLET. GROUND DAMAGE. A/C STRUCK BY K-LOADER. DAMAGE TO R/H WINGLET TRAILING EDGE INSTALLED NEW WINGLET UP TO AND INCLUDING STEP 18 REFERENCE AMM 57-31-03-002-002. ALL OPS CHECKS GOO
- [SDR IPXA2023091227393](https://openairdocs.org/sdr/IPXA2023091227393), Sep 12, 2023: UNKNOWN. UNKNOWN. *SDR FILED OPEN* *ATB* N1 ENG VIB REACHED 5.0 DURING CLIMB - LEFT ENG REMOVED AND REINSTALLED FAN BLADES ALL IN SAME POSITION, FOUND DAMAGED SHIM AFT OF HUB, AB
- [SDR IPXA2023031791920](https://openairdocs.org/sdr/IPXA2023031791920), Mar 16, 2023: SKIN. NONE. INSPECTION TYPE:C6*MAJOR REPAIR* FUSELAGE DRAIN HOLES ADDITION AND INSPECTION AFT OF STA 1725.5 BETWEEN S-36L AND S-36R.PERFORM UPS EO B767-2740-82173-C APPX B
- [SDR IPXA2023031691889](https://openairdocs.org/sdr/IPXA2023031691889), Mar 11, 2023: STIFFENER. CRACKED. INSPECTION TYPE:C6*MAJOR REPAIR* CRACK ON THE STIFFENER (P/N: 141T5146-65) OF THE FLOOR BEAM ASSEMBLY AT STA 246, LBL 40.REPAIR I.A.W 767-300F SRM 53-10-51-2R-4
- [SDR IPXA2023031791928](https://openairdocs.org/sdr/IPXA2023031791928), Mar 9, 2023: UNKNOWN. CRACKED. INSPECTION TYPE:C6CRACK ON ANGLE OF AFT CARGO COMPARTMENT NEAR STA 1087, LBL 26.INSTALL NEW PART I.A.W BOEING DWG NO.:140T0130 SH 50, REV ''A'' AND 767-300F SRM
- [SDR IPXA2023031491829](https://openairdocs.org/sdr/IPXA2023031491829), Mar 9, 2023: ANGLE. CRACKED. INSPECTION TYPE:C6CRACK ON ANGLE (P/N:146T5651-6) OF BULK CGO COMPT NEAR STA 1578, RBL 78.INSTALL NEW PARTS I.A.W 767-300F SRM 51-40-02-0G REV. 85.01 AND BOEING
- [SDR IPXA2023031491828](https://openairdocs.org/sdr/IPXA2023031491828), Mar 9, 2023: ANGLE. CRACKED. INSPECTION TYPE:C6CRACK ON ANGLE (P/N:146T5651-5) OF BULK CGO COMPT NEAR STA 1578, LBL 78INSTALL NEW PARTS I.A.W 767-300F SRM 51-40-02-0G REV.85.01 AND BOEING D
- [SDR IPXA2022071584207](https://openairdocs.org/sdr/IPXA2022071584207), Jul 15, 2022: LIGHT. INOPERATIVE. INSPECTION TYPE:N/ADURING OPS CHECK OF INTERIOR EMERGENCY LIGHTS FOUND THAT ALL EMERGENCY LIGHTS FADE OFF AFTER APPROX 3 SECONDSR & R EMERGENCY LIGHTS BATTERY A
- [SDR IPXA2021100674671](https://openairdocs.org/sdr/IPXA2021100674671), Oct 5, 2021: NONE. NONE. INSPECTION TYPE:N/AENTRY DOOR PLUNGER WITH NOT LOCK/MOVE FORDAVEL FROM INSIDERESET ENTRY DOOR ENTRY/EXIT HANDLE. REF MM 52-12-00
- [SDR IPXA2021020165162](https://openairdocs.org/sdr/IPXA2021020165162), Feb 1, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE:N/ADAMAGE TO UPPER SKIN OF THE FLOOR PANELFABRICATE NEW FLOOR PANEL PER SREO B767-5320-9693.
- [SDR IPXA2019120439658](https://openairdocs.org/sdr/IPXA2019120439658), Dec 3, 2019: COVER. SHEARED. MAIN ENTRY DOOR ARMING LEVER HINGED COVER SHEARED OFF. REPLACED THE HINGE OPS CHECKED OK.
- [SDR IPXA2018070931446](https://openairdocs.org/sdr/IPXA2018070931446), Jul 6, 2018: TERMINAL. BROKEN. ON PUSHBACK STATUS MSG "R ENG FIRE LOOP2" WAS SHOWN. COULD NOT RESET. FOUND TS6582 TERMINAL LUG IS BROKEN AT LWR AFT FIRED DET ELEMENT. TERMINAL LUG REPLACED IA
- [SDR IPXA2018043029113](https://openairdocs.org/sdr/IPXA2018043029113), Apr 30, 2018: LIGHT. DETACHED. EMERGENCY EXIT LIGHT AT MAIN ENTRY DOOR BRACKET SECURING LIGHT IS DETACHED FROM WALL. REMOVED FWD ENTRY DOOR ASSY ROUTED TO SM SHOP. REATTACHED BRACKET IAW DRAW
- [SDR IPXA2018011925680](https://openairdocs.org/sdr/IPXA2018011925680), Jan 19, 2018: SWITCH. BROKEN. THE GUARDED SWITCH COVER ON THE EMERGENCY EXIT LIGHTS HAS A BROKEN PIECE. REMOVED & REPLACED EMERGENCY LIGHT CONTROL PANEL IAW MM 33-51-08-004-002, AND MM 33-51
- [SDR IPXA2017111523599](https://openairdocs.org/sdr/IPXA2017111523599), Nov 15, 2017: FIRE LOOP. INOPERATIVE. LEFT ENGINE FIRE LOOP 1 INOPERATIVE.
- [SDR IPXA2017071619341](https://openairdocs.org/sdr/IPXA2017071619341), Jul 16, 2017: ROLLER. INOPERATIVE. L1 DOOR HARD TO OPEN. REMOVED AND REPLACED THE L1 DOOR AFT SIDE ROLLER IAW MM 52-12-03. OPS CHECKED NORMAL.
- [SDR IPXA2016112110886](https://openairdocs.org/sdr/IPXA2016112110886), Nov 19, 2016: TRACK. OUT OF ADJUST. MAIN ENTRY DOOR IS HEAVY AND DIFFICULT TO OPEN. TROUBLESHOT IAW FIM 52-12-00 REV 119.00. FOUND MOVABLE CEILING PANEL NEED TUBE ADJUSTED & DOOR TRACK AND TROLLEY
- [SDR IPXA2016111110525](https://openairdocs.org/sdr/IPXA2016111110525), Nov 10, 2016: ESCAPE ROPE. LOOSE. ESCAPE ROPE ON CREW ENTRY DOOR FOUND LOOSE. R & R THE DOOR INGRESS COVER AND REINSTALLED ROPE IAW MM 25-61-04.
- [SDR IPXA2015101994939](https://openairdocs.org/sdr/IPXA2015101994939), Oct 18, 2015: D-RING. MISSING. DEMO EMERGENCY ESCAPE DESCENT HARNESS IS MISSING ITS D-RING. R & R DEMO EMERGENCY DESCENT HARNESS REF MM D25-61-03-252-023. PN ON & OFF 65B40289-12, SN ON TAG 0
- [SDR IPXA2015030286556](https://openairdocs.org/sdr/IPXA2015030286556), Mar 2, 2015: SKIN. DAMAGED. RIGHT SIDE FUSELAGE SKIN DAMAGED BETWEEN STA 228.5 AND 236.5. REMOVED DAMAGE BY BLENDING IAW SRM 53-00-01-1A-1. HFEC, NO CRACK. C/W EO 767-5330-49395A INTERIM R
- [SDR IPXA2014101384588](https://openairdocs.org/sdr/IPXA2014101384588), Oct 12, 2014: SKIN. DENTED. FUSELAGE SKIN DAMAGED AT BS 1461-1480 STRINGERS 31-32R. REPAIRED IAW EO B767-5330-54805-B.
- [SDR IPXA2014072183687](https://openairdocs.org/sdr/IPXA2014072183687), Jul 19, 2014: RETAINER. DAMAGED. FOUND EMERGENCY ESCAPE RETAINER DAMAGED. R & R EMERGENCY ESCAPE RETAINER IAW AMM 25-61-02, REV 112.00, 06-23-14.
- [SDR IPXA2014071883655](https://openairdocs.org/sdr/IPXA2014071883655), Jul 17, 2014: SLIDING WINDOW. NOISE. LOUD NOISE FROM CAPTAIN`S WINDOW, STARTED 25.500. REPLACED LT SLIDING WINDOW IAW AMM 56-11-02-004-039 AND 56-11-01 -404-026. ADJUSTED IAW 56-11-2-506.
- [SDR IPXA2014021781960](https://openairdocs.org/sdr/IPXA2014021781960), Feb 14, 2014: HMU. MALFUNCTIONED. ATB INSPECTION, NR 2 ENGINE POWER REDUCTION SHOWING 300 LBS AT CLIMB POWER, REMOVED RT THRUST LEVER, ENGINE DID NOT RESPOND, IAW AMM 73-21-14-401. REPLACED RT E
- [SDR IPXA2013110600767](https://openairdocs.org/sdr/IPXA2013110600767), Sep 28, 2013: SKIN. DAMAGED. NR 3 SLAT LOWER SKIN DAMAGED. REMOVED DAMAGE IAW SRM 57-43-02, FIG 201. OK TO INSTALL REPAIR C/W INSTALL PERMANENT REPAIR IAW B767 57-43-02, SEAL & PAINT IAW B7
- [SDR IPXA3679708](https://openairdocs.org/sdr/IPXA3679708), Aug 7, 2013: SWITCH. INOPERATIVE. FWD EQUIPWENT OVERHEAT ILLUMINATED, APROACHING 290. RAN ENTIRE CHECKLIST FOR FWD EQUIPMENT OVERHEAT WITH EQUIPMENT COOLING SWITCH PLACED TO OVERIDE IAW INSTRUCT
- [SDR IPXA3677449](https://openairdocs.org/sdr/IPXA3677449), Mar 10, 2013: FLOOR PANEL. DAMAGED. MAIN CARGO DECK FLOOR PANEL BETWEEN 8-9L HAS 2 INCH HOLE. FABRICATED FLOOR PANEL IAW EO B767-5320-9693-H AND REPLACED.
- [SDR IPXA2672830](https://openairdocs.org/sdr/IPXA2672830), Apr 9, 2012: WEDGE. DENTED. LEFT WING INBD FLAP T/E WEDGE DENTED UPPER AND LWR SURFACE. REPAIRED REF EO B767-5750-46365-B.

## 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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