# N345UP: 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: 37867
- Year built: 2011
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 28, 2011
- Certificate issued: July 8, 2011
- Expires: July 31, 2027
- Mode S code: A3D1B1
- 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=345UP
- Page: https://openairdocs.org/aircraft/N345UP

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 N345UP.

## FAA accident and incident reports

None matched to N345UP.

## Service difficulty reports (36)

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 IPXA2025021560262](https://openairdocs.org/sdr/IPXA2025021560262), Feb 15, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N:143T5876-88 PANEL NO.232KFF (REPAIR)I.A.W AMM 53-01-06-000-801 REV.144 REMOVED MAIN DECK CARGO FLOOR PANEL SEALANT AND C
- [SDR IPXA2025021547434](https://openairdocs.org/sdr/IPXA2025021547434), Feb 14, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 143T5876-86 PANEL NO : 232LFF (REPAIR)I.A.W AMM 53-01-06-000-801 REV.144 REMOVED MAIN DECK CARGO FLOOR PANEL SEALANT A
- [SDR IPXA2025021321473](https://openairdocs.org/sdr/IPXA2025021321473), Feb 13, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-19 PANEL NO: 251QFF. (REPAIR) I.A.W AMM 53-01-06-000-801 REV.144 REMOVED MAIN DECK CARGO FLOOR PANEL SEALANT A
- [SDR IPXA2025021321483](https://openairdocs.org/sdr/IPXA2025021321483), Feb 13, 2025: FLOOR PANEL. DAMAGED. FOUND AFT CARGO FLOOR PANEL DAMAGE, P/N: 453T1996113 AT DOORWAY FWD SIDE R/H. (REPAIR)CUT OUT THE DAMAGE AND CLEANED.MEASURED THE CUT OUT (LENGTH:9.5", WIDTH:0.
- [SDR IPXA2025021321528](https://openairdocs.org/sdr/IPXA2025021321528), Feb 13, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-134 PANEL NO: 252UFF. (REPAIR)I.A.W AMM 53-01-06-000-801 REV.144 REMOVED MAIN DECK CARGO FLOOR PANEL SEALANT A
- [SDR IPXA2025021304100](https://openairdocs.org/sdr/IPXA2025021304100), Feb 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 143T5876-112 PANEL NO: 231LFF. (REPAIR) I.A.W AMM 53-01-06-000-801 REV.144 REMOVED MAIN DECK CARGO FLOOR PANEL SEALANT 
- [SDR IPXA2025021304168](https://openairdocs.org/sdr/IPXA2025021304168), Feb 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 141T5856-102 PANEL NO: 221CFF. (REPAIR)I.A.W AMM 53-01-06-000-801 REV.144 REMOVED MAIN DECK CARGO FLOOR PANEL SEALANT A
- [SDR IPXA2025021304218](https://openairdocs.org/sdr/IPXA2025021304218), Feb 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-62 PANEL NO: 252BFF. (REPAIR)I.A.W AMM 53-01-06-000-801 REV.144 REMOVED MAIN DECK CARGO FLOOR PANEL SEALANT AN
- [SDR IPXA2025021302780](https://openairdocs.org/sdr/IPXA2025021302780), Feb 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE , P/N:146T5869-132 PANEL NO: 251AFF. (REPAIR)I.A.W AMM 53-01-06-000-801 REV.144 REMOVED MAIN DECK CARGO FLOOR PANEL SEALANT A
- [SDR IPXA2025021303987](https://openairdocs.org/sdr/IPXA2025021303987), Feb 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-135 PANEL NO: 251XFF. (REPAIR) I.A.W AMM 53-01-06-000-801 REV.144 REMOVE MAIN DECK CARGO FLOOR PANEL SEALANT A
- [SDR IPXA2025021304012](https://openairdocs.org/sdr/IPXA2025021304012), Feb 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-77 PANEL NO: 251MFF. (REPAIR)I.A.W AMM 53-01-06-000-801 REV.144 REMOVED MAIN DECK CARGO FLOOR PANEL SEALANT AN
- [SDR IPXA2025021304050](https://openairdocs.org/sdr/IPXA2025021304050), Feb 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 145T5876-63 PANEL NO: 241DFF. (REPAIR) I.A.W AMM 53-01-06-000-801 REV.144 REMOVED MAIN DECK CARGO FLOOR PANEL SEALANT A
- [SDR IPXA2025021304072](https://openairdocs.org/sdr/IPXA2025021304072), Feb 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 143T5876-20 PANEL NO: 232NFF. (REPAIR) I.A.W AMM 53-01-06-000-801 REV.144 REMOVED MAIN DECK CARGO FLOOR PANEL SEALANT A
- [SDR IPXA2025021303989](https://openairdocs.org/sdr/IPXA2025021303989), Feb 12, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N:146T5869-136 PANEL NO: 252WFF. (REPAIR)I.A.W AMM 53-01-06-000-801 REV.144 REMOVED MAIN DECK CARGO FLOOR PANEL SEALANT AN
- [SDR IPXA2023031291759](https://openairdocs.org/sdr/IPXA2023031291759), Mar 6, 2023: ANGLE. CRACKED. INSPECTION TYPE:C6CRACK ON ANGLE (P/N: 146T5651-8) OF BULK CGO COMPT NEAR STA 1577, RBL 80.INSTALL NEW PARTS I.A.W 767-300F SRM 51-40-02-0G REV. 85.01 AND BOEIN
- [SDR IPXA2023031191740](https://openairdocs.org/sdr/IPXA2023031191740), Mar 6, 2023: ANGLE. CRACKED. INSPECTION TYPE:C6CRACK ON ANGLE(P/N:146T5651-7)OF BULK CGO COMPT NEAR STA 1577,LBL 80.INSTALL NEW PARTS I.A.W 767-300F SRM 51-40-02-0G REV.85.01 AND BOEING DWG
- [SDR IPXA2023031291758](https://openairdocs.org/sdr/IPXA2023031291758), Mar 5, 2023: ANGLE. CRACKED. INSPECTION TYPE:C6CRACK ON ANGLE (P/N: 146T5651-6) OF BULK CGO COMPT NEAR STA 1577, RBL 80.INSTALL NEW PARTS I.A.W 767-300F SRM 51-40-02-0G REV. 85.01 AND BOEIN
- [SDR IPXA2023031191741](https://openairdocs.org/sdr/IPXA2023031191741), Mar 5, 2023: UNKNOWN. CRACKED. INSPECTION TYPE:C6CRACK ON CLIP(P/N:141T5146-16)OF M/D CGO FLOOR BEAM SUPPORT AT STA 246,LBL 49.INSTALL NEW PARTS I.A.W 767-300F SRM 51-40-02-0G REV.85.01 AND B
- [SDR IPXA2023031191739](https://openairdocs.org/sdr/IPXA2023031191739), Mar 5, 2023: ANGLE. CRACKED. INSPECTION TYPE:C6CRACK ON ANGLE(P/N:146T5651-5)OF BULK CGO COMPT NEAR STA 1577,LBL 79.INSTALL NEW PARTS I.A.W 767-300F SRM 51-40-02-0G REV.85.01 AND BOEING DWG
- [SDR IPXA2023031191738](https://openairdocs.org/sdr/IPXA2023031191738), Mar 5, 2023: UNKNOWN. CRACKED. INSPECTION TYPE:C6CRACK ON THE CLIP(P/N:140T0138-38)OF AFT CARGO COMPARTMENT STRUCTURE AT STA 1087,RBL 26.INSTALL NEW PART I.A.W 767-300F SRM 51-40-02-0G REV.85
- [SDR IPXA2023031191737](https://openairdocs.org/sdr/IPXA2023031191737), Mar 5, 2023: UNKNOWN. CRACKED. INSPECTION TYPE:C6CRACK ON THE CLIP(P/N:140T0130-39)OF AFT CARGO COMPARTMENT STRUCTURE AT STA 1087,LBL 26.INSTALL NEW PARTS I.A.W 767-300F SRM 51-40-02-0G REV.8
- [SDR IPXA2023031591848](https://openairdocs.org/sdr/IPXA2023031591848), Mar 4, 2023: SKIN. UNKNOWN. 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 Q9DY202201120001](https://openairdocs.org/sdr/Q9DY202201120001), Aug 6, 2021: WASHER. MISSING. L/H NOSE WHEEL WAS REPLACED IN CGN 08/05/21 AND LOG PAGE INDICATES THAT WASHER AND SPACER WERE VERIFIED (REF. LOG PAGE 938817/01). HOWEVER, AFTER THE NEXT FLIGH
- [SDR IPXA2021012064690](https://openairdocs.org/sdr/IPXA2021012064690), Jan 19, 2021: SEAL. OUT OF POSITION. INSPECTION TYPE: N/A VERY LOUD AIR LEAK COMING FROM CREW ENTRY DOOR LOWER RIGHT SIDE. FOUND LOWER DOOR SEAL PULLED OUT, REINSTALLED SEAL, OK FOR SERVICE. AMM 52
- [SDR IPXA2020111762494](https://openairdocs.org/sdr/IPXA2020111762494), Nov 17, 2020: STATUS MESSAGE. ILLUMINATED. INSPECTION TYPE: ETOP, ETOPS FILED OPEN. LEFT ENGINE FIRE LOOP 1 STATUS MESSAGE. DEFERRED IAW MEL 26-11-1-1B.
- [SDR IPXA2019081215532](https://openairdocs.org/sdr/IPXA2019081215532), Aug 11, 2019: PACKING. LEAKING. AIR TURN BACK. L HYD QTY EICAS MSG AND QTY LITE ILLUMINATED. RF DISPLAYED AT .45 LANDED WITH .12 QUANTITY AT 325.0 LANDING WEIGHT, R&R PACKING ON #12 SPOILER AC
- [SDR IPXA2018091433920](https://openairdocs.org/sdr/IPXA2018091433920), Sep 12, 2018: FAIRING. CRACKED. RIGHT ENGINE OUTBOARD C DUCT LOWER FAIRING CRACKED. THRUST REVERSER DEPLOYED FOR MAINT, STOWED THRUST REVERSER. MADE TEMP REPAIR AND DEFERRED IAW MX AC CMM 78-3
- [SDR IPXA2018012125717](https://openairdocs.org/sdr/IPXA2018012125717), Jan 20, 2018: COUPLING. BLOWN. INSPECTION TYPE:ETOPWHILE CHECKING APU OIL FOUND SURGE BLEED DUCT COUPLINGS BLOWN OUT.R&R'D SURGE VALVE DUCT COUPLINGS IN REFERENCE TO AMM 49-53-01. NO LEAKS NO
- [SDR IPXA2017122024688](https://openairdocs.org/sdr/IPXA2017122024688), Dec 19, 2017: WARNING MESSAGE. ILLUMINATED. INSPECTION TYPE: L, PIMU MAINTENANCE MESSAGE DISPLAYED ON EICAS.
- [SDR IPXA2017021213940](https://openairdocs.org/sdr/IPXA2017021213940), Feb 12, 2017: FLOOR PANEL. DAMAGED. FLOOR PANEL DAMAGE. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-I.
- [SDR IPXA2016091308228](https://openairdocs.org/sdr/IPXA2016091308228), Sep 10, 2016: DOOR. OUT OF SEQUENCE. CREW ENTRY DOOR WOULD NOT OPEN/CLOSE. FOUND, UPPER TRIM ON CREW ENTRY DOOR OUT OF SEQUENCE. REPOSITIONED TRIM AND CYCLED DOOR IAW AMM 52-12-00 PB 201
- [SDR IPXA2016091108093](https://openairdocs.org/sdr/IPXA2016091108093), Sep 10, 2016: STRUCTURE. OUT OF SEQUENCE. ENTRY DOOR WOULD NOT CLOSE. FOUND UPPER TRIM OUT OF SEQUENCE. REPOSITIONED TRIM AND CYCLED DOOR IAW AMM 52-12-00 PB 201.
- [SDR IPXA2016031800904](https://openairdocs.org/sdr/IPXA2016031800904), Mar 17, 2016: FLAP SYSTEM. FALSE INDICATION. EMERGENCY DECLARED, EICAS MSG T/E FLAP DISAGREE. RAN CHECKLIST AND LANDED, FLAPS 20' V, REF WAS 158 USED ALT FLAP SW. T/S IAW FIM 27-51-00-815-810. T/E FLAP OPS
- [SDR IPXA2015010985245](https://openairdocs.org/sdr/IPXA2015010985245), Jan 8, 2015: RECEPTACLE. DAMAGED. EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED DAMAGED EXTERIOR EMERGENCY BULB RECEPTACLE IAW CMM 33-51-52. REPLACED WITH NEW RECEPTACLE ASSY OPS CHECK GOOD IAW 
- [SDR IPXA2013122001089](https://openairdocs.org/sdr/IPXA2013122001089), Dec 18, 2013: LAMP. BURNED OUT. EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP, OP CHECKED NORMAL.
- [SDR IPXA1668985](https://openairdocs.org/sdr/IPXA1668985), Sep 1, 2011: SPRING. DAMAGED. EICAS MESSAGE EMERGENCY LIGHTS DISPLAYED & UNARMED LIGHT ILLUMINATED WITH EMERGENCY LIGHTS SWITCH ARMED. EMERGENCY LIGHT SWITCH GUARD SPRING CORRECTED AND EMERG

## 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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