# N356UP: 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: 37869
- Year built: 2013
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 27, 2013
- Certificate issued: April 3, 2013
- Expires: April 30, 2029
- Mode S code: A3FCE7
- 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=356UP
- Page: https://openairdocs.org/aircraft/N356UP

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 N356UP.

## FAA accident and incident reports

None matched to N356UP.

## 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 IPXA2026031113913](https://openairdocs.org/sdr/IPXA2026031113913), Jan 21, 2026: ENGINE. SHUTDOWN. R STARTER CUTOUT (MOMENTARY) ENG FLUX OUT OF LIMITS SHUTDOWN AT FL370 DEIVERT TO CYYT STATUS MSGS RENG REV POS, RENG CONTROL, R ENG EEC C1 #2 ENGINE WAS R&R'D. 
- [SDR IPXA2026012213913](https://openairdocs.org/sdr/IPXA2026012213913), Jan 21, 2026: STARTER. FAULTED. DIVERTED RT STARTER CUTOUT (MOMENTARY) ENG FLUX OUT OF LIMITS SHUTDOWN AT FL370 DIVERT TO CYYT STATUS MSGS RENG REV POS, RENG CONTROL, R ENG EEC C1
- [SDR IPXA2025090263446](https://openairdocs.org/sdr/IPXA2025090263446), Sep 1, 2025: ANGLE. CRACKED. MEC BAY CEILING AREA LEFT HAND SIDE, BS 246, LBL40 ANGLE CRACK REPAIR CRACKED.
- [SDR IPXA2025012345579](https://openairdocs.org/sdr/IPXA2025012345579), Jan 17, 2025: CEILING PANEL. DAMAGED. FOUND THE CEILING PANEL WITH SCRATCH DAMAGE IN AFT CARGO COMPARTMENT, P/N: 453T1862-57. (REPAIR). I.A.W AMM 25-52-01-404-049-001 REV.144 INSTALL AFT CARGO CEILI
- [SDR IPXA2025012145579](https://openairdocs.org/sdr/IPXA2025012145579), Jan 17, 2025: CEILING PANEL. DAMAGED. FOUND THE CEILING PANEL WITH SCRATCH DAMAGE IN AFT CARGO COMPARTMENT, P/N: 453T1862-57. (REPAIR) I.A.W AMM 25-52-01-404-049-001 REV.144 INSTALL AFT CARGO CEILIN
- [SDR IPXA2025011728784](https://openairdocs.org/sdr/IPXA2025011728784), Jan 16, 2025: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578 LBL 80 INBOARD IN BULK CARGO COMPARTMENT LEFT AREA (REPLACE). INSTALL NEW PART I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO:
- [SDR IPXA2025011626595](https://openairdocs.org/sdr/IPXA2025011626595), Jan 16, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL DENT, P/N: 143T5876-99 (REPAIR). REQUEST PERFORM MAIN DECK CARGO FLOOR PANEL OK TO INSTALL CHECK. P/N:143T5876-99. THIS REPAIR IS CO
- [SDR IPXA2025011626558](https://openairdocs.org/sdr/IPXA2025011626558), Jan 16, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL DENT, P/N: 143T5876-75 (REPAIR). REQUEST PERFORM MAIN DECK CARGO FLOOR PANEL OK TO INSTALL CHECK. P/N:143T5876-75. THIS REPAIR IS CO
- [SDR IPXA2025011626521](https://openairdocs.org/sdr/IPXA2025011626521), Jan 16, 2025: FLOOR PANEL. BROKEN. BROKEN - FND M/D CGO FLOOR PANEL BROKEN AT STA 890, RBL 3 P/N:145T5876-85 (REPAIR). REQUEST PERFORM MAIN DECK CARGO FLOOR PANEL OK TO INSTALL CHECK. P/N:145T587
- [SDR IPXA2025011728641](https://openairdocs.org/sdr/IPXA2025011728641), Jan 16, 2025: SIDEWALL PANEL. CRACKED. CRACK - BOTTOM CHORDS, STA 1065, SUPPORT AFT CARGO COMPARTMENT FWD WALL PANEL, (RH) LOWER CORNER, ZONE : 152 (REPLACE). INSTALL NEW PARTS I.A.W SRM 51-40-02-0G 
- [SDR IPXA2025011728715](https://openairdocs.org/sdr/IPXA2025011728715), Jan 16, 2025: SIDEWALL PANEL. CRACKED. BOTTOM CHORDS, STA 1065, SUPPORT AFT CARGO COMPARTMENT FWD WALL PANEL (LH) LOWER CORNER ZONE: 151 (REPLACE). INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV.91 AND 
- [SDR IPXA2025011626627](https://openairdocs.org/sdr/IPXA2025011626627), Jan 16, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL DENT, P/N: 143T5876-109 (REPAIR). REQUEST PERFORM MAIN DECK CARGO FLOOR PANEL OK TO INSTALL CHECK. P/N:143T5876-109. THIS REPAIR IS 
- [SDR IPXA2025011626563](https://openairdocs.org/sdr/IPXA2025011626563), Jan 16, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL DENT, P/N : 143T5876-110 (REPAIR). REQUEST PERFORM MAIN DECK CARGO FLOOR PANEL OK TO INSTALL CHECK. P/N:143T5876-110. THIS REPAIR IS
- [SDR IPXA2025011626509](https://openairdocs.org/sdr/IPXA2025011626509), Jan 16, 2025: FLOOR PANEL. DENTED. FAULT - FOUND MAIN DECK FLOOR PANEL DENT, P/N:143T5876-114 (REPAIR). THIS REPAIR IS CONSIDERED MAJOR PER GMM 05.04.01.02 CLASSIFICATION OF REPAIRS. REPAIR PER S
- [SDR IPXA2025011626484](https://openairdocs.org/sdr/IPXA2025011626484), Jan 16, 2025: FLOOR PANEL. DENTED. FAULT - FOUND MAIN DECK FLOOR PANEL DENT, P/N: 143T5876-102 (REPAIR). THIS REPAIR IS CONSIDERED MAJOR PER GMM 05.04.01.02 CLASSIFICATION OF REPAIRS. REPAIR PER 
- [SDR IPXA2025011626464](https://openairdocs.org/sdr/IPXA2025011626464), Jan 16, 2025: FLOOR PANEL. DENTED. FAULT - FOUND MAIN DECK FLOOR PANEL DENT, P/N: 143T5876-104 (REPAIR). THIS REPAIR IS CONSIDERED MAJOR PER GMM 05.04.01.02 CLASSIFICATION OF REPAIRS. REPAIR PER 
- [SDR IPXA2025011626387](https://openairdocs.org/sdr/IPXA2025011626387), Jan 16, 2025: FLOOR PANEL. DENTED. FAULT - FOUND MAIN DECK FLOOR PANEL DENT, P/N: 143T5876-103 (REPAIR). THIS REPAIR IS CONSIDERED MAJOR PER GMM 05.04.01.02 CLASSIFICATION OF REPAIRS. REPAIR PER 
- [SDR IPXA2025011626438](https://openairdocs.org/sdr/IPXA2025011626438), Jan 16, 2025: FLOOR PANEL. DENTED. FAULT - FOUND MAIN DECK FLOOR PANEL DENT, P/N: 143T5876-106 (REPAIR). THIS REPAIR IS CONSIDERED MAJOR PER GMM 05.04.01.02 CLASSIFICATION OF REPAIRS. REPAIR PER 
- [SDR IPXA2025011626392](https://openairdocs.org/sdr/IPXA2025011626392), Jan 16, 2025: FLOOR PANEL. CRACKED. FAULT - FOUND MAIN DECK FLOOR PANEL WITH CRACK DAMAGE, P/N: 146T5869-135 PANEL NO.251XFF (REPAIR). I.A.W AMM 25-57-02-404-016, AMM 25-57-05-404-006, AMM 25-58-0
- [SDR IPXA2025011626505](https://openairdocs.org/sdr/IPXA2025011626505), Jan 16, 2025: FLOOR PANEL. DENTED. FAULT - FOUND MAIN DECK FLOOR PANEL DENT, P/N: 143T5876-101 (REPAIR). THIS REPAIR IS CONSIDERED MAJOR PER GMM 05.04.01.02 CLASSIFICATION OF REPAIRS. REPAIR PER 
- [SDR IPXA2025011626513](https://openairdocs.org/sdr/IPXA2025011626513), Jan 16, 2025: FLOOR PANEL. DENTED. FOUND MAIN DECK FLOOR PANEL DENT, P/N: 143T5876-111 (REPAIR) OK TO INSTALL (RII ITEM) CHECK OK. OPEN
- [SDR IPXA2025011779614](https://openairdocs.org/sdr/IPXA2025011779614), Jan 14, 2025: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578 LBL 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 
- [SDR IPXA2025011780088](https://openairdocs.org/sdr/IPXA2025011780088), Jan 14, 2025: ANGLE. CRACKED. FOUND THE ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. (REPLACE). INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG
- [SDR IPXA2023082826833](https://openairdocs.org/sdr/IPXA2023082826833), Aug 25, 2023: APU. UNKNOWN. *** SUPPLEMENTAL SDR *** APU GEN INTERMITTENTLY CUTS ON AND OFF*OII 2* PERFORMED APU BITE PROCEDURE IAW FIM TASK 49-11 FAULT TREE 803. T/S TO FIGURE 103 SH 7 TA
- [SDR IPXA2023082526833](https://openairdocs.org/sdr/IPXA2023082526833), Aug 25, 2023: UNKNOWN. UNKNOWN. *** SDR FILED OPEN *** APU GEN INTERMITTENTLY CUTS ON AND OFF*OII 2* DEFERRED APU GEN IAW MEL 22-00-2A. NON ETOPS. PLACARD INSTALLED. DMP C/W
- [SDR IPXA2023110861537](https://openairdocs.org/sdr/IPXA2023110861537), Aug 21, 2023: FLAP. DENTED. RIGHT WING OUTBOARD FLAP TRAILING EDGE WEDGE LOWER SKIN DENT. VERIFIED ALL LOTO HAS BEEN REVERSED I AM MM 27-51-00 AND 27-81-00
- [SDR IPXA2023082161537](https://openairdocs.org/sdr/IPXA2023082161537), Aug 21, 2023: UNKNOWN. UNKNOWN. RIGHT WING OUTBOARD FLAP TRAILING EDGE WEDGE LOWER SKIN DENT. APPLIED SKIM COAT AND EXTERIOR FINISH TO COMPLETE REPAIR. SRM 51-70-06. OPEN
- [SDR IPXA2023032992378](https://openairdocs.org/sdr/IPXA2023032992378), Mar 23, 2023: STIFFENER. CRACKED. INSPECTION TYPE:C5CRACK 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 REV 85.01.
- [SDR IPXA2023032992377](https://openairdocs.org/sdr/IPXA2023032992377), Mar 22, 2023: SUPPORT. CRACKED. INSPECTION TYPE:C5CRACK ON SUPPORT (P/N:141T5282-2) OF M/D CGO FLOOR BEAM SUPPORT AT STA 246, NEAR LBL 26.INSTALL NEW PARTS I.A.W 767-300F SRM 51-40-02-0G REV.8
- [SDR IPXA2023032992376](https://openairdocs.org/sdr/IPXA2023032992376), Mar 22, 2023: UNKNOWN. CRACKED. INSPECTION TYPE:C5CRACK 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
- [SDR IPXA2023033092423](https://openairdocs.org/sdr/IPXA2023033092423), Mar 21, 2023: BRACKET. CRACKED. INSPECTION TYPE:C5CRACK ON BRACKET (P/N:148T7312-43) OF STABILIZER SEAL SEAL FAIRING NEAR STA 1767.25.INSTALL NEW PART I.A.W 767-300F SRM 51-40-02-0G REV.85.01,
- [SDR IPXA2023032892337](https://openairdocs.org/sdr/IPXA2023032892337), Mar 20, 2023: SKIN. NONE. INSPECTION TYPE:C5FUSELAGE 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 IPXA2022041581183](https://openairdocs.org/sdr/IPXA2022041581183), Apr 14, 2022: ENGINE. NONE. INSPECTION TYPE:NA**SUPPLEMENTAL SDR**IFSD** DIVERSION**EMERGENCY DECL'D**DURING CRUISE FL370, LH ENG SURGE & LOST THRUST. THRUST LEVER MOVEMENT RESULTED IN NO 
- [SDR IPXA2021052469785](https://openairdocs.org/sdr/IPXA2021052469785), May 21, 2021: SENSOR. DIRTY. INSPECTION TYPE:NAL FWD ENT DOOR EICAS CAME ON AFTER LANDING AND WENT OUT JUST PRIOR TO BLOCK IN. THIS CAUSED THE ACARS TO SHOW US BLOCKED IN AS SOON AS THE LIG
- [SDR IPXA2021032467216](https://openairdocs.org/sdr/IPXA2021032467216), Mar 24, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C4DAMAGE ON M/D FLOOR PANEL AT STA 412 , RBL 11 - LBL 11.FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO. B767-5320-9693-I.
- [SDR IPXA2021032467215](https://openairdocs.org/sdr/IPXA2021032467215), Mar 23, 2021: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C4DAMAGE ON M/D FLOOR PANEL AT STA984, RBL 33 - RBL 54.FABRICATE THE REPLACEMENT PANEL PER EO NO. B767-5320-9693-I.
- [SDR IPXA2021032667283](https://openairdocs.org/sdr/IPXA2021032667283), Mar 17, 2021: SKIN. CRACKED. INSPECTION TYPE:C4CRACK ON THE NO.5 SLAT SKIN (P/N:114T4105-23) NEAR OSS 492.95.REPAIR I.A.W. 767-300F SRM 57-43-01-2R-2 REV.79.01
- [SDR IPXA2020102661691](https://openairdocs.org/sdr/IPXA2020102661691), Oct 26, 2020: SKIN. DAMAGED. DENT AND GOUGE ON RH SIDE OF FUSELAGE. REPAIRED, IAW EO B767-5330-78150. REPAIRED IAW EO B767-5330-78150.
- [SDR IPXA2020021765173](https://openairdocs.org/sdr/IPXA2020021765173), Feb 16, 2020: SKIN. PUNCTURED. INSPECTION TYPE:N/ALH INBD EVELVATOR HAS A SKIN PUNCTURE ON UPPER SURFACEREPAIRED IAW UPS E.O. B767-5520-75204 ON NRC 655755
- [SDR IPXA2019111348952](https://openairdocs.org/sdr/IPXA2019111348952), Nov 13, 2019: SEAL. LEAKING. INSPECTION TYPE:N/AMAIN ENTRY DOOR SIGNIFICANT SEAL LEAKING AT BOTTOM CABIN LEAKING AT BOTTOM CABIN ALTITUDE NORMAL AT FLY 200 LEAK STARTED GOING GOING THOUGH 8
- [SDR IPXA201906243587](https://openairdocs.org/sdr/IPXA201906243587), Jun 21, 2019: SEAL. OUT OF POSITION. LOUD AIR LEAK AT BOTTOM OF CREW ENTRY DOOR DURING CLIMB OUT. PRESSURIZATION WAS GOOD DOOR SEAL IS LOOSE AT BOTTOM. REINSTALLED SEAL INTO THE SEAL RETAINER ON TH
- [SDR IPXA2019031740128](https://openairdocs.org/sdr/IPXA2019031740128), Mar 5, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C3 DAMAGE ON M/D CARGO FLOOR PANEL AT STA 1114 - STA 1197 PLUS 22, LBL 55 - LBL 77, PNL NR 251DFF. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO 
- [SDR IPXA2019031740127](https://openairdocs.org/sdr/IPXA2019031740127), Mar 5, 2019: FLOOR PANEL. DAMAGED. INSPECTION TYPE:C3 DAMAGE ON M/D CARGO FLOOR PANEL AT STA 1114-STA 1197 PLUS 22, LBL 33 - LBL 55, PNL NO.251CFF. FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NR
- [SDR IPXA2019021549018](https://openairdocs.org/sdr/IPXA2019021549018), Feb 14, 2019: SEAL. DISLODGED. AFT PART CREW ENTRY DOOR LEAKS.NOISE HEARD AT 5500 .2 DIFFERENTIAL PRESSURE. ABOUT 1,000 CABIN ALTITUDEDOOR & FRAME INSPECTED. FOUND 3" SECTION OF LOWER DOOR SE
- [SDR IPXA2017120524215](https://openairdocs.org/sdr/IPXA2017120524215), Dec 4, 2017: FAN. MALFUNCTIONED. INSPECTION TYPE:FWD EQUIP EXH FAN STATUS MSG ON. FWD EQUIP COOLING EXHT FAN - ONE SUPPLY FAN INSTALL. AUTHORIZED BY 0557835. PLACARD INSTALLED. MEL/CDL 21-58-04
- [SDR IPXA2017072119602](https://openairdocs.org/sdr/IPXA2017072119602), Jul 21, 2017: SLEEVE. MISSING. RIGHT ENGINE INBD THRUST REVERSER COWL INNER TRANSLATING SLEEVE MISSING THE SURFACE FILLER MATERAL AT THE 9 O`CLOCK POSITION, TWO PLACES. REPAIRED IAW SREO M-78
- [SDR IPXA2016062004800](https://openairdocs.org/sdr/IPXA2016062004800), Jun 20, 2016: SKIN. DAMAGED. RUDDER UPPER T/E LIGHTNING STRIKE DAMAGED. REF LOG PAGE 238111, REPAIRED REF EO 5540-60426-B.
- [SDR IPXA2015072791637](https://openairdocs.org/sdr/IPXA2015072791637), Jul 27, 2015: EVAS UNIT. NO TEST. CAPTAIN`S EMERGENCY VISION ASSURANCE SYSTEM FAILED THE SYSTEM TEST IAW T/C 25-069-00, BLOWER DID NOT ACTUATE DURING TEST. REPLACED THE CAPTAIN'S EVAS UNIT IAW M

## 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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