# N764CK: 1994 Boeing 767-3P6

- Status: Valid registration
- Airframe: [Boeing 767-3P6](https://openairdocs.org/model/boeing-767-3p6) (registry code 1385105, 290 seats)
- Engine: [GE CF6-80C2B6](https://openairdocs.org/engine/ge-cf6-80c2b6) (registry code 30103)
- Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (General Electric Company GE Aerospace) (OpenAirDocs)
- Serial number: 26234
- Year built: 1994
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 5, 2018
- Certificate issued: January 10, 2017
- Expires: January 31, 2030
- Mode S code: AA50A0
- Registered owner: [Kalitta Air LLC](https://openairdocs.org/faa-owner/KALITTA%20AIR%20LLC)
- Location: [Ypsilanti, MI](https://openairdocs.org/faa-place/MI/Ypsilanti)
- Owner type: LLC
- Owner's area on the map: 42.2751° N, 83.5863° W: Placed by OpenAirDocs at the center of ZIP code 48198, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=764CK
- Page: https://openairdocs.org/aircraft/N764CK

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): 31 in force

### Matched by airframe (Boeing 767-3P6)

None in force.

### Matched by engine (GE CF6-80C2B6)

- [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 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 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 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) (5 in force)

- [SAIB 2023-15](https://openairdocs.org/saib/2023-15): Falsified Forms from AOG Technics. Issued Dec 19, 2023
- [SAIB NE-11-27](https://openairdocs.org/saib/NE-11-27): Fuel Injector Nozzle - CF6-80 Improperly Welded Fuel Nozzles. Issued Apr 5, 2011
- [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 N764CK.

## FAA accident and incident reports

None matched to N764CK.

## Service difficulty reports (135, newest 50)

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 ABXA20261022478](https://openairdocs.org/sdr/ABXA20261022478), Oct 22, 2026: STATUS MESSAGE. ILLUMINATED. LT ENG FIRE LP1 STATUS MSG VISIBLE AFTER LANDING ON TAXI IN. DEFERRED L ENG FIRE LP 1 IAW MEL 26-11-1-1. PLACARDS INSTALLED. MBCB 11/01/26. NO MX PROCEDURES APP
- [SDR ABXA20261007460](https://openairdocs.org/sdr/ABXA20261007460), Oct 7, 2026: FLAP SYSTEM. MALFUNCTIONED. ON APPROACH SELECTING FLAPS TO 25, THE CREW GOT THE TRAILING EDGE FLAPS DISAGREE LIGHT AND EICAS, MSG TRAILING EDGE FLAP DISAGREE ACCOMPLISHED QRH AND LANDED FL
- [SDR ABXA20261002455](https://openairdocs.org/sdr/ABXA20261002455), Oct 2, 2026: BRACKET. DAMAGED. ENTRY DOOR LIGHT NOT EXTINGUISHING WHEN SHUTTING L1 DOOR. REMOVED AND REPLACED ENTRY DOOR SENSOR BRACKET IAW B767 AMM 52-71-01. OPS CHECK GOOD. A/C RETURNED TO 
- [SDR ABXA20260929440](https://openairdocs.org/sdr/ABXA20260929440), Sep 29, 2026: DOOR. UNLOCKED. MAIN CARGO DOOR LIGHT ON WHILE STARTING ENGINES ON PUSHBACK MTX ENTERED A/C AND FOUND MAIN CARGO DOOR NOT FULLY LOCKED, VENT DOORS WIDE OPEN. CLOSED AND LOCKED 
- [SDR ABXA20260903395](https://openairdocs.org/sdr/ABXA20260903395), Sep 3, 2026: PRIORITY VALVE. FAULTED. LEFT ENG PRV VALVE EICAS MESSAGE ON TAKE OFF. CREW ABORTED TAKEOFF (ATO) AND RETURNED TO THE GATE (BTB). PLACED ON DI IAW MEL 36-11-8-1-1A-1 MBCB 9.13.26 PLACAR
- [SDR ABXA20260825374](https://openairdocs.org/sdr/ABXA20260825374), Aug 25, 2026: FIRE LOOP. FAULT MESSAGE. R ENG FIRELOOP 2 STATUS MSG. DEFERRED PER MEL ABX-26-11-1-1. A/C RETURNED TO SERVICE.
- [SDR ABXA20260815367](https://openairdocs.org/sdr/ABXA20260815367), Aug 15, 2026: CIRCUIT CARD. TRIPPED. DURING POWER TRANSFER APU TO GPU, LT ENG FIRE LOOP 1 MESSAGE. RESET BOTH FUSE CARDS M681 (LOOP1) M683(LOOP 2) PERFORMED OPS TEST ON SYSTEM ALL CHECKED GOOD IAW 
- [SDR ABXA20260727337](https://openairdocs.org/sdr/ABXA20260727337), Jul 27, 2026: GENERATOR. FAULT MESSAGE. AFTER TAKEOFF CLEARANCE WAS RECEIVED PILOT REQUESTED THRUST/N1 TO BE SET. AT APPROXIMATELY 35 KIAS THE CREW RECEIVED THE R GEN OFF AND BOTH AUX BUS EICAS MESSAG
- [SDR ABXA20260724334](https://openairdocs.org/sdr/ABXA20260724334), Jul 24, 2026: WARNING MESSAGE. FALSE ACTIVATION. RIGHT ENG FIRE LOOP 2 STATUS MESSAGE. MTC PERFORMED STATIC FIRE LOOP TEST OPS CHECK MSG CLEARED IAW AMM 26-11-00. A/C RETURNED TO SERVICE.
- [SDR ABXA20260712318](https://openairdocs.org/sdr/ABXA20260712318), Jul 12, 2026: CIRCUIT CARD. DEFECTIVE. LEFT ENG FIRE LOOP NR 2 STATUS MSG. DUE TO PREVIOUS T/S HISTORY SUSPECTED AFOLTS CARD M-681 BAD. REMOVED OLD THEN INSTALLED NEW M682 AFOLTS CARD PER AMM 26-10-0
- [SDR ABXA20260711316](https://openairdocs.org/sdr/ABXA20260711316), Jul 11, 2026: CIRCUIT CARD. UNKNOWN. L ENG FIRE LOOP 1 STATUS MESSAGE AC GROUNDED ,CONDUCTED T/S PER FIM 26-11 FT 804, CONTINUITY CHECK PASS. INTEGRITY RESISTANCE FROM AFOLTS CARD M681 PINS 20 & 21
- [SDR ABXA20260711315](https://openairdocs.org/sdr/ABXA20260711315), Jul 11, 2026: TEST PANEL. MALFUNCTIONED. F/U-CHECK CONNECTORS & WIRING AT FIRE-OVHT TEST PANEL FOR HISTORY OF FIRE/OVHT SYS MESSAGES. IF NFF, REPLACE FIRE/OVHT TEST PANEL. PERFORMED GVI OF FIRE OVHT TE
- [SDR ABXA20260710314](https://openairdocs.org/sdr/ABXA20260710314), Jul 10, 2026: WARNING MESSAGE. FALSE ACTIVATION. "FIRE/OVHT SYS" EICAS CAUTION MESSAGE AFTER ENGINE NR 1 STARTED. ACCOMPLISHED QRH PROCEDURE AND MESSAGE DISAPPEARED PERFORMED ENGINE FIRE DETECTION SYSTEM TEST 
- [SDR ABXA20260630298](https://openairdocs.org/sdr/ABXA20260630298), Jun 30, 2026: WARNING MESSAGE. ILLUMINATED. LEFT ENG FIRE LP1 STATUS MESSAGE INTERMITTENTLY. ITEM PLACED ON MEL 26-11-1-1 PLACARD INSTALLED MBCB 07/10/2026 A/C REMAINS NO ETOPS. A/C RETURNED TO SERVICE.
- [SDR ABXA20260629291](https://openairdocs.org/sdr/ABXA20260629291), Jun 29, 2026: FIRE LOOP. FAULT MESSAGE. DURING CREW PREFLIGHT, L ENG FIRE LP 2 STATUS MESSAGE ILLUMINATED. MTX DEFERRED IAW ABX B767 MEL 26-11-1-1. PLACARDS INSTALLED. MX PROCEDURES C/W. MBCB 07/09/26
- [SDR ABXA20260621272](https://openairdocs.org/sdr/ABXA20260621272), Jun 21, 2026: WARNING MESSAGE. FALSE ACTIVATION. ON PREFLIGHT HAD A STATUS LEVEL L ENG FIRE LP1 THRT WOULD NOT CLEAR. MTX GROUNDED A/C AND PERFORMED OPS CHECK OF FIRE OVHT. MSG CLEARED. AIRCRAFT REMAINS NO ETO
- [SDR ABXA20260604245](https://openairdocs.org/sdr/ABXA20260604245), Jun 4, 2026: FIRE LOOP. WARNING MESSAGE. LEFT ENG FIRE LOOP LP1 STATUS MSG MTX GROUNDED AC AND DEFERRED LH ENGINE LOOP LP1 FOR DEPARTURE IAW MEL ABX-26-11-1-1. AND RETURNED ACFT TO SERVICE .
- [SDR ABXA20260529236](https://openairdocs.org/sdr/ABXA20260529236), May 29, 2026: CIRCUIT CARD. MALFUNCTIONED. INTERMITTENT ENG #1 LP1 STATUS MESSAGE MTX REMOVED AND REPLACED M681 FIRE DET CARD PER AMM 26-10-01. OPS CK GOOD NO DEFECTS NOTED. ACFT REMAINS NO ETOPS. RETURN
- [SDR ABXA20260527228](https://openairdocs.org/sdr/ABXA20260527228), May 27, 2026: FIRE LOOP. FAULTED. DURING CREW PREFLIGHT, STATUS MSG LEFT ENG FIRE LP 2. MTC DEFERRED STATUS MSG L ENG FIRE LP 2 IAW MEL 26-11-1-1, MBCB 06/06/26, PLACARD INSTALLED, NO DEACTIVATI
- [SDR ABXA20260525226](https://openairdocs.org/sdr/ABXA20260525226), May 25, 2026: THERMOCOUPLE. DEFECTIVE. AFTER ENG STARTS AND TAXI OUT, NOTICED LEFT ENGINE EGT INOP. NOTE: EGT LEFT ENGINE 72C RH 369C. CREW RETURNED TO THE GATE (BTB). MTC REMOVED AND REPLACED THERMO
- [SDR ABXA20260520216](https://openairdocs.org/sdr/ABXA20260520216), May 20, 2026: CIRCUIT CARD. FAULTED. DURING PUSHBACK, FIRE/OVHT SYS EICAS MSG. CREW ACCOMPLISHED QRH 8.35. MSG CLEARED THEN REAPPEARED ON FINAL. MTC SWAPPED LT ENG LP2 FIRE DETECTION CARD (M682) AN
- [SDR ABXA20260518214](https://openairdocs.org/sdr/ABXA20260518214), May 18, 2026: FIRE LOOP. INOPERATIVE. DURING INSP/MTC, L ENGINE FIRE LOOP 1 INOPERATIVE. DEFERRED L ENGINE FIRE LP 1 INOP IAW MEL 26-11-1-1. ALL MX PROCDURES CW PLACARD INSTALLED. MBCB 05/28/26 AC R
- [SDR ABXA20260518209](https://openairdocs.org/sdr/ABXA20260518209), May 18, 2026: CIRCUIT CARD. FAULTED. DURING APPROACH, CREW RECEIVED FIRE/OVHT STS EICAS MESSSAGE ON FINAL UNTIL ENGINE SHUTDOWN. MTC PERFORMED GVI OF LH ENG DUCTING -IAW B767 AMM 71-00-00 AND B767 
- [SDR ABXA20260324129](https://openairdocs.org/sdr/ABXA20260324129), Mar 24, 2026: WARNING MESSAGE. FALSE ACTIVATION. DURING MAINTENANCE INSPECTION, L ENG FIRE LP 2 STATUS MSG. MAINTENANCE PERFORMED FIRE DET TEST IAS AMM 26-11-00. TESTED GOOD. MESSAGE CLEARED. AIRCRAFT RETURNED
- [SDR ABXA20260323123](https://openairdocs.org/sdr/ABXA20260323123), Mar 23, 2026: FIRE LOOP. FAULTED. CREW REPORTED L ENG FIRE LP 2 STATUS MSG. MAINTENANCE PERFORMED AFOLTS TEST IAW AMM 26-10-00. OPS CHECK PASSED MESSAGE CLEARED. PERFORMED ENGINE FIRE DETECTION 
- [SDR ABXA20260307089](https://openairdocs.org/sdr/ABXA20260307089), Mar 7, 2026: FIRE LOOP. FALSE INDICATION. ON CPF L ENG FIRE LP1 STAUS MSG ON MTX PERFORMED A RESET OF LH FIRE LOOP 1 ON THE MTP-OPS NORMAL IAW AMM 26-11-0 AIRCRAFT NO ETOPS AND RETURNED AC TO SERVICE .
- [SDR ABXA20260128031](https://openairdocs.org/sdr/ABXA20260128031), Jan 28, 2026: WARNING MESSAGE. ILLUMINATED. ON TAXI OUT, AFTER CROSS BLEED ENGINE START, HAD LEFT BLEED INOP AND LEFT PACK INOP INDICATIONS. AIRCRAFT RETURNED TO BLOCKS (BTB). PERFORMED OPS CHECK OF LT EN
- [SDR ABXA20260121024](https://openairdocs.org/sdr/ABXA20260121024), Jan 21, 2026: APU. AUTO SHUTDOWN. DURING TAXI OUT, APU SHUT ITSELF DOWN ATTEMPTED RESTART AND FAULTED AGAIN. AIRCRAFT RETURNED TO BLOCKS (BTB). DEFERRED IAW MEL 29-11-1A CAT I PLAC INSTALLED MAI
- [SDR ABXA20260120021](https://openairdocs.org/sdr/ABXA20260120021), Jan 20, 2026: TARGET. OUT OF ADJUST. DURING TAXI OUT, LE SLAT ASYM EICAS MESSAGE ILLUMINATED. A/C RETURNED TO BLOCKS (BTB). MEG CHECKED AND VERIFIED INDUCTANCE OF PROX SWITCH S305.. ADUSTED GAP TO 
- [SDR ABXA20251231366](https://openairdocs.org/sdr/ABXA20251231366), Dec 31, 2025: WIRE. DAMAGED. FOUND LT ENG FIRE LOOP 1 ON EICAS DURING S/C MTX GROUNDED A/C AND TROUBLSHOT PER W.D. 26-11-11 FOUND RESISTANCE FLUCTUATION DURING WIRE SHAKE INSPECTION ON TS68
- [SDR ABXA20251225360](https://openairdocs.org/sdr/ABXA20251225360), Dec 25, 2025: TRANSMITTER. EXPIRED. DURING MAINTENANCE CHECK PORTABLE ELT FAIL OPERATIONAL TEST CODE FAULTED 3+2 FLASHES INDICATING LOW RF POWER .MTX REPLACED KANNARD ELT. PERFORMED OPS CHECK PER 
- [SDR ABXA202512109325](https://openairdocs.org/sdr/ABXA202512109325), Dec 9, 2025: BRAKE. OVERHEATED. WHILE TAXING IN AT DFW, RIGHT SIDE INBOARD AFT BRAKE OVERHEAT, TEMP AT '7". WHEN BRAKE ROSE TO UNAFE LIMIT DISCONTINUED TAXI. REFERRED TO QRH AND CALLED OPS. CR
- [SDR ABXA20251022276](https://openairdocs.org/sdr/ABXA20251022276), Oct 22, 2025: FIRE WARNING. FALSE ACTIVATION. EICAS FIRE / OVRHT SYS LIGHT ILLUMINATED WHILE TURNING FINAL UNTIL BOTH ENGINES SHUT DOWN.. MAINTENANCE PERFORMED FIRE / OVHT SYSTEM 6 TC CHECK IAW FIM 26-11 FT
- [SDR ABXA20251018273](https://openairdocs.org/sdr/ABXA20251018273), Oct 18, 2025: WARNING MESSAGE. ILLUMINATED. MAIN DECK CARGO DOOR WARNING ON DEPARTURE .ACFT RETURNED TO FIELD (ATB) AND MTX GROUNDED AC, MTX THEN DEFERRED MAIN DECK CARGO DOOR INDICATION IAW MEL ABX52-71-
- [SDR ABXA20251005257](https://openairdocs.org/sdr/ABXA20251005257), Oct 5, 2025: FRAME. DAMAGED. DURING AIRCRAFT N764CK C4-CHECK IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE DISCOVERED AFT CARGO FRAME WEB AT STA 1395 RBL 5 DAMAGED ,BLENDED AND FOUND TO BE 
- [SDR ABXA20251005256](https://openairdocs.org/sdr/ABXA20251005256), Oct 5, 2025: SKIN. DAMAGED. "DURING AIRCRAFT N764CK C4-CHECK IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE DISCOVERED FUSELAGE SKIN CORROSION UNDER STRINGER S-38L AT STA 1395 WHILE PERFORM
- [SDR ABXA20251005255](https://openairdocs.org/sdr/ABXA20251005255), Oct 5, 2025: STRINGER. CORRODED. DURING AIRCRAFT N764CK C4-CHECK IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE DISCOVERED ,EVIDENCE OF CORROSION FOUND ON STRINGER 32 AT STA. 697 AND REPAIRED ST
- [SDR ABXA20251005254](https://openairdocs.org/sdr/ABXA20251005254), Oct 5, 2025: DOOR SILL. CORRODED. DURING AIRCRAFT N764CK C4-CHECK IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE DISCOVERED CORROSION DAMAGE AT APPROXIMATELY STA 555 AND STA 610 ON THE OUTER CHOR
- [SDR ABXA20251005253](https://openairdocs.org/sdr/ABXA20251005253), Oct 5, 2025: DOOR SILL. CORRODED. DURING AIRCRAFT N764CK C4-CHECK IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE DISCOVERED CORROSION DAMAGE AT APPROXIMATELY STA 555 AND STA 610 ON THE OUTER CHOR
- [SDR ABXA20251005252](https://openairdocs.org/sdr/ABXA20251005252), Oct 5, 2025: WEB. CORRODED. DURING 4C IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE FOUND FWD CARGO COMPARTMENT R/H AT APPROX STA 610-544 RBL 36.70 WEB IN FRONT OF DOOR CORRODED TB76. FOUN
- [SDR ABXA20251005251](https://openairdocs.org/sdr/ABXA20251005251), Oct 5, 2025: SKIN. CORRODED. WHILE 764CK WAS UNDERGOING C 4 -CHECK IN OSC, CORROSION WAS FOUND ON THE INNER SURFACE OF THE INNER SKIN AT STA 1177 ALONG THE S-36L LAP JOINT. SEE FIGURE 1. TH
- [SDR ABXA20251000525](https://openairdocs.org/sdr/ABXA20251000525), Oct 5, 2025: STRUCTURE. CORRODED. DURING C 4 IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE FOUND EVIDENCE OF CORROSION ON UPPER CHORD IN AFT CARGO COMPARTMENT AT BS 1373 RBL 8 JM-44..FOUND TO BE
- [SDR ABXA20251005249](https://openairdocs.org/sdr/ABXA20251005249), Oct 5, 2025: DOOR FRAME. CRACKED. DURING C 4 CHECK IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE FOUND CRACK INDICATION FOUND DURING HFEC INSPECTION OF R1 LOWER DOOR CUTOUT. INDICATION IS LOCATE
- [SDR ABXA20251005248](https://openairdocs.org/sdr/ABXA20251005248), Oct 5, 2025: STRINGER. CORRODED. DURING C 4 CHECK IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE FOUND AFT CARGO COMPARTMENT HAS EVIDENCE OF CORROSION BETWEEN STATION 1351-1395 AT STRINGER L39. 
- [SDR ABXA20251005247](https://openairdocs.org/sdr/ABXA20251005247), Oct 5, 2025: STRINGER. CORRODED. DURING C 4 CHECK IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE FOUND AFT LWR CARGO COMPARTMENT HAS EVIDENCE OF CORROSION AT STRINGER 39R AT STA 1307. GB5.FOUND 
- [SDR ABXA20251005246](https://openairdocs.org/sdr/ABXA20251005246), Oct 5, 2025: SKIN. DELAMINATED. DURING C 4 CHECK IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE FOUND R/H HORZ STAB LOWER SKIN HAS AREA OF DELAMINATION AT AUX SPAR STA 243 JM-30.FOUND TO BE OUT
- [SDR ABXA20251005245](https://openairdocs.org/sdr/ABXA20251005245), Oct 5, 2025: NUT PLATE. CORRODED. DURING C 4 CKECK IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE FOUND FWD CARGO AT APPROX STA 654+44 ON INNER CHORD NUT PLATE HAS EVIDENCE OF CORROSION TB56 FOUN
- [SDR ABXA20251005244](https://openairdocs.org/sdr/ABXA20251005244), Oct 5, 2025: STRUCTURE. CRACKED. DURING C4 CHECK .IN OSCODA MICHIGAN (OSC), KALITTA MAINTENANCE FOUND CRACK WITH EDDY CURRENT INSPECTION AS MARKED ON INNER CHORED STA 903.5, LBL89. REPAIRED IAW
- [SDR ABXA20250928242](https://openairdocs.org/sdr/ABXA20250928242), Sep 28, 2025: SMOKE DETECTOR. NO TEST. DURING C-4 CHECK IN OSCALA, MI., MAINTENANCE FOUND AFT LOWER CARGO SMOKE DETECTOR ZONE FIALED LEAK CHECK. REMOVED AND REPLACED TUBE ASSY, TEE HOSE, AND SILICON 
- [SDR ABXA202506174127](https://openairdocs.org/sdr/ABXA202506174127), Jun 14, 2025: WIRE. SHORTED. STATUS MSG: L ENG FIRE LP 2. MAINTENANCE DEFERRED IAW MEL C ABX-26-11-1-1. REFERENCE B767 WDM 26-11-11. FOUND WIRE W53/6-002 R-16 SHORTED TO PNEUMATIC DUCT. TEM

All 135: https://openairdocs.org/aircraft/N764CK/reports.md

## STCs that may be installed (OpenAirDocs) (6)

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 CF6-80C2B6)

- [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 SE00969CH](https://openairdocs.org/stc/SE00969CH): Install AeroControlex P/N 2605290-001 variable stator feedback control cable. AeroControlex Group TransDigm Inc
- [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 767-3P6 aircraft: https://openairdocs.org/model/boeing-767-3p6/aircraft.md
- The GE CF6-80C2B6 engine: https://openairdocs.org/engine/ge-cf6-80c2b6.md

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