# N358UP: 2013 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: 37864
- Year built: 2013
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 7, 2013
- Certificate issued: June 24, 2013
- Expires: June 30, 2029
- Mode S code: A40455
- Registered owner: [C C & E I LLC](https://openairdocs.org/faa-owner/C%20C%20%26%20E%20I%20LLC)
- Location: [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville)
- Owner type: LLC
- Owner's area on the map: 38.2585° N, 85.5398° W: Placed by OpenAirDocs at the center of ZIP code 40223, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=358UP
- Page: https://openairdocs.org/aircraft/N358UP

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 N358UP.

## FAA accident and incident reports

None matched to N358UP.

## 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 IPXA2026081350986](https://openairdocs.org/sdr/IPXA2026081350986), Aug 12, 2026: HINGE PIN. MIGRATED. FLIGHT DECK. CREW ENTRY DOOR. DOOR HANDLE COVER PLATE, SPRING LOADED. HINGE PIN MIGRATED 1/4 OF WAY OUT. RE-ALIGNED HINGE PIN. OPS CK GOOD. OK TO CONTINUE. REF 
- [SDR IPXA2025091401260](https://openairdocs.org/sdr/IPXA2025091401260), Sep 14, 2025: PANEL. CRACKED. NUMBER 2 ENG BETWEEN 2 & 4 O CLOCK 2 PANEL CRACK OUTTER PANEL ABOVE IGNITER PLUG. DURING BORESCOPE INSPECTION, FOUND CRACKS ON PANELS 1 AND 2 AT THE 2/4 O'CLOCK
- [SDR IPXA2025091401257](https://openairdocs.org/sdr/IPXA2025091401257), Sep 14, 2025: PANEL. CRACKED. NUMBER 2 ENG BETWEEN 12 & 1 O CLOCK 2 PANEL CRACK OUTTER PANEL. DURING BORESCOPE INSPECTION, FOUND CRACK(S) ON PANELS 1 AND 2 AT THE 12/1 O'CLOCK POSITION ON TH
- [SDR IPXA2025091401263](https://openairdocs.org/sdr/IPXA2025091401263), Sep 14, 2025: PANEL. CRACKED. NUMBER 2 ENG BETWEEN 5 & 6 O CLOCK POS 2 PANEL CRACK OUTTER PANEL. DURING BORESCOPE INSPECTION, FOUND CRACKS ON PANELS 1 AND 2 AT THE 5/6 O'CLOCK POSITION ON TH
- [SDR IPXA2025091401278](https://openairdocs.org/sdr/IPXA2025091401278), Sep 14, 2025: PANEL. CRACKED. NUMBER 2 ENG BETWEEN 9 & 8 O CLOCK 2 PANEL CRACK OUTTER PANEL. DURING BORESCOPE INSPECTION, FOUND CRACKS ON PANELS 1 AND 2 AT THE 9/8 O'CLOCK POSITION ON THE CO
- [SDR IPXA2025091401250](https://openairdocs.org/sdr/IPXA2025091401250), Sep 14, 2025: PANEL. CRACKED. NUMBER 2 ENGINE BETWEEN 4 & 5 O`CLOCK, PANELS CRACKED OUTTER PANEL BY LWD IGNITER PLUG. DURING BORESCOPE INSPECTION, FOUND CRACKS ON PANELS 1 AND 2 AT THE 4/5 O
- [SDR IPXA2025022870306](https://openairdocs.org/sdr/IPXA2025022870306), Feb 27, 2025: FLOOR PANEL. DENTED. DENT - PANEL, MAIN DECK CARGO COMPARTMENT FLOOR PANEL NO. 242UFF BETWEEN STA 977 AND STA 1114, RBL 54.75 ~ RBL 77.5, P/N : 145T5876-76. (REPAIR). FABRICATE A NE
- [SDR IPXA2025022870256](https://openairdocs.org/sdr/IPXA2025022870256), Feb 27, 2025: FLOOR PANEL. DENTED. DENT - PANEL, MAIN DECK CARGO COMPARTMENT FLOOR PANEL NO. 241ZFF BETWEEN STA 977 AND STA 1114, LBL 54.75 ~ LBL 77.5, P/N : 145T5876-77 (REPAIR). FABRICATE A NEW
- [SDR IPXA2025032632339](https://openairdocs.org/sdr/IPXA2025032632339), Feb 25, 2025: SEAL. BROKEN. AERODYNAMIC SEAL BROKEN , FWD LH ENTRY DOOR. (REPLACE). INSTALL NEW PART I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO.141T6121 SH 13 REV: B. I.A.W AMM 52-12-0
- [SDR IPXA2025022733959](https://openairdocs.org/sdr/IPXA2025022733959), Feb 25, 2025: ANGLE. CRACKED. FOUND CRACK - ANGLE , BULK CGO COMPT CEILING AREA , STA 1577 LBL 74 INBD SIDE. (REPLACE). INSTALL NEW PART I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO.146T56
- [SDR IPXA2025022733920](https://openairdocs.org/sdr/IPXA2025022733920), Feb 25, 2025: ANGLE. CRACKED. FOUND CRACK - ANGLE , BULK CGO COMPT CEILING AREA , STA 1577 RBL 74 INBD SIDE. (REPLACE). INSTALL NEW PART I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO.146T56
- [SDR IPXA2025022732399](https://openairdocs.org/sdr/IPXA2025022732399), Feb 25, 2025: ANGLE. CRACKED. FOUND CRACK - ANGLE , BULK CGO COMPT CEILING AREA , STA 1577 LBL 74 OUTBD SIDE. (REPLACE). INSTALL NEW PART I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO:146T5
- [SDR IPXA2025022733933](https://openairdocs.org/sdr/IPXA2025022733933), Feb 25, 2025: ANGLE. CRACKED. FOUND CRACK - ANGLE , BULK CGO COMPT CEILING AREA , STA 1577 RBL 74 OUTBD SIDE. (REPLACE). REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV.91. INSTALL NEW PART I.
- [SDR IPXA2025022633150](https://openairdocs.org/sdr/IPXA2025022633150), Feb 25, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE , P/N : 143T5876-58 PANEL NO : 231RFF. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-0
- [SDR IPXA2025022632339](https://openairdocs.org/sdr/IPXA2025022632339), Feb 25, 2025: SEAL. BROKEN. AERODYNAMIC SEAL BROKEN , FWD LH ENTRY DOOR. (REPLACE) 1.REMOVED ENTRY DOOR LINER I.A.W AMM 52-12-01-004-001 REV.144 AND G.V.I CONDITION CHECK NORMAL.
- [SDR IPXA2025022529230](https://openairdocs.org/sdr/IPXA2025022529230), Feb 25, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-27 PANEL NO: 251VFF. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-05-4
- [SDR IPXA2025022529199](https://openairdocs.org/sdr/IPXA2025022529199), Feb 25, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 143T5876-109 PANEL NO: 232GFF. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-02-
- [SDR IPXA2025022529213](https://openairdocs.org/sdr/IPXA2025022529213), Feb 25, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-136 PANEL NO: 252WFF. (REPAIR). TO FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-
- [SDR IPXA2025022529216](https://openairdocs.org/sdr/IPXA2025022529216), Feb 25, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 146T5869-19 PANEL NO: 251QFF. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-05-4
- [SDR IPXA2025030115250](https://openairdocs.org/sdr/IPXA2025030115250), Feb 24, 2025: STIFFENER. CRACKED. FAULT - CRACK, CENTER WING FRONT SPAR STIFFENR AT STA 785.9 LBL 11 (REPAIR). REPAIR DAMAGE AREA I.A.W SRM 57-10-10-2R-2 REV.91 AND EGAT WORK SHEET NO. 50137, UP
- [SDR IPXA2025022516150](https://openairdocs.org/sdr/IPXA2025022516150), Feb 24, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 143T5876-63 PANEL NO : 231EFF (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 53-01-06-
- [SDR IPXA2025022516192](https://openairdocs.org/sdr/IPXA2025022516192), Feb 24, 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. I.A.W AMM 53-01-06
- [SDR IPXA2025022516176](https://openairdocs.org/sdr/IPXA2025022516176), Feb 24, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 146T5869-110 PANEL NO : 251TFF (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 53-01-06
- [SDR IPXA2025022516008](https://openairdocs.org/sdr/IPXA2025022516008), Feb 24, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 145T5876-59 PANEL NO : 242EFF (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 53-01-06-
- [SDR IPXA2025022516188](https://openairdocs.org/sdr/IPXA2025022516188), Feb 24, 2025: FLOOR PANEL. DAMAGED. FOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 146T5869-135 PANEL NO : 251XFF (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 25-57-02
- [SDR IPXA2024093014854](https://openairdocs.org/sdr/IPXA2024093014854), Sep 26, 2024: A/C PACK. ODOR. STRONG OIL FUME SMELLS WHEN RUNNING LEFT PACK. DISCONTINUED USING LEFT PACK ++ PERFORMED PACK OPS CHECK IAW AMM 21-32-00 NO DEFECT WAS NOTED. RUN LEFT PACK FOR 
- [SDR IPXA2022110287774](https://openairdocs.org/sdr/IPXA2022110287774), Nov 1, 2022: SEAL. LEAKING. ENTRY DOOR SEAL LEAKING AIR PRESSUREFOUND APPROX 10 INCHES OF SEAL PULLED OUT ON BOTTOM ENTRY DOOR. RE-SEATED SEAL IN REF TO AMM 52-09-01-424-019.
- [SDR IPXA2022083185773](https://openairdocs.org/sdr/IPXA2022083185773), Aug 30, 2022: NONE. NONE. INSPECTION TYPE:N/A**SDR FILED OPEN**ACRID "ELECTRICAL BURNING SMELL" IN OVERHEAD CB PANEL. ACCOMPLISHED SMOKE AND FUMES CONDITIONAL INSPECTION IAW AMM 05-51-56
- [SDR IPXA2022011877991](https://openairdocs.org/sdr/IPXA2022011877991), Jan 17, 2022: ENGINE. SURGES. INSPECTION TYPE:N/A**IFSD**DIVERSION**EMERG DECL'D* REQ'D RADAR VECTORS*SUPPLEMENTAL SDR** A/C LANDED W/OUT INCIDENT**A/C OOS**ABNORMAL ENGINE INDICATIONS DURIN
- [SDR IPXA2021052469738](https://openairdocs.org/sdr/IPXA2021052469738), May 18, 2021: SKIN. CRACKED. INSPECTION TYPE:C4CRACK ON LEADING EDGE SKIN OF NO.6 SLAT NEAR ISS 300.REPAIR I.A.W. BOEING SR:3-5034298589 AND UPS EO B767-5750-80466-A
- [SDR IPXA2020121463384](https://openairdocs.org/sdr/IPXA2020121463384), Dec 12, 2020: SWITCH. INTERMITTENT. INSPECTION TYPE: N/A P5 OVERHEAD EMERGENCY SIGN ARM SWITCH INTERMITTENT. R & R EMERGENCY LIGHTS PANEL AND OPERATIONS CHECK OK, IAW AMM 33-51-08 ESR: IPC 31-12-1
- [SDR IPXA2020011350817](https://openairdocs.org/sdr/IPXA2020011350817), Jan 11, 2020: WARNING SYSTEM. FALSE ACTIVATION. INSPECTION TYPE:N/A**DIVERSION** DURING APPROACH TO MMX UPON SELECTING FLAPS 25, EICAS ALERT "LEADING EDGE SLAT ASYMETRY" DISPLAYED.FSEU: T/S IAW FIM 27-51-00-8
- [SDR IPXA2019061072941](https://openairdocs.org/sdr/IPXA2019061072941), Jun 7, 2019: LIGHT. INOPERATIVE. INSPECTION TYPE:N/AEMERGENCY LIGHTS PANEL INTEGRAL LIGHTS INOPC/W E/O B767-3310-72533A
- [SDR IPXA2019020178349](https://openairdocs.org/sdr/IPXA2019020178349), Jan 27, 2019: FLOOR PANEL. DAMAGED. MAIN CARGO COMP FLOOR PANEL REPAIR POSITION 11L/12L. FABRICATED FLOOR PANEL IAW EO B767-5320-9696-I ** SUPPLEMENTAL SDR**REPAIR COMPLETED ON NON ROUTINE 591343.
- [SDR IPXA2018121766965](https://openairdocs.org/sdr/IPXA2018121766965), Dec 16, 2018: WINDOW. INOPERATIVE. LEFT SIDE WINDOW HEAT INOPERATIVE DURING FLIGHT. QRH PROCEDURE DID NOT RESOLVE THE PROBLEM. REPLACED THE L2 WINDOW ASSY IAW AMM 56-11-02-401.
- [SDR IPXA2018120536517](https://openairdocs.org/sdr/IPXA2018120536517), Dec 1, 2018: LAMP. INOPERATIVE. EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE LAMPS IAW M/M 33-51-16-962-001, OPS NORMAL.
- [SDR IPXA2018120396517](https://openairdocs.org/sdr/IPXA2018120396517), Dec 1, 2018: LAMP. INOPERATIVE. EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW MM 33-51-16-962-001, OPS NORMAL.
- [SDR IPXA2018092874471](https://openairdocs.org/sdr/IPXA2018092874471), Sep 25, 2018: CONTROL UNIT. MALFUNCTIONED. ANTI-SKID EICAS ENROUTE FOR 1-2 MINUTES, THEN CLEARED ITSELF. EMERGENCY DECLARED. ON TOUCHDOWN, DID NOT GET SPOILER DEPLOYMENT. MANUALLY DEPLOYED SPOILERS. R & 
- [SDR IPXA2018061230601](https://openairdocs.org/sdr/IPXA2018061230601), Jun 12, 2018: PROBE. FAULTY. ATB - CLIMBING ABOVE 12,000 FT TAT PROBE ECIAS MESSAGE WITH AN OVERHEAD TAT LIGHT ILLUMINATED AIRSPEED BUG FAILED ALONG WITH AUTOPILOT WE ALSO LOSS LNAV & VNAV 
- [SDR IPXA2014101584618](https://openairdocs.org/sdr/IPXA2014101584618), Oct 13, 2014: WARNING LIGHT. ILLUMINATED. CAPTAIN'S EVAS INOPERATIVE. R & R EVAS BOX IAW AMM 25-69-00-4, REV 112.01. OPS CHECKED OK. T

## 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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