# N762CK: 1992 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: 26236
- Year built: 1992
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 30, 2017
- Certificate issued: January 10, 2017
- Expires: January 31, 2030
- Mode S code: AA4932
- 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=762CK
- Page: https://openairdocs.org/aircraft/N762CK

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 N762CK.

## FAA accident and incident reports

None matched to N762CK.

## Service difficulty reports (100, 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 ABXA20261015469](https://openairdocs.org/sdr/ABXA20261015469), Oct 15, 2026: FIRE LOOP. FAULTED. RIGHT ENG FIRE LOOP 1 STATUS MSG DISPLAYED. MX DEFFERED R ENG FIRE LOOP 1 IAW ABX AIR MEL 26-11-1-1 PLACARDS INSTALLED MX PROCEDURES ACCOMPLISHED MBCB 10-25-26-
- [SDR ABXA20261010465](https://openairdocs.org/sdr/ABXA20261010465), Oct 10, 2026: WARNING MESSAGE. FALSE ACTIVATION. AFTER BLOCK OUT FWD EQPT EICAS AND VALVE LIGHT ILLUMINTATED AND A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C. MTX PERFORMED OPS CHECK FOR FWD EQPT VALVE 
- [SDR ABXA20261009466](https://openairdocs.org/sdr/ABXA20261009466), Oct 9, 2026: WARNING MESSAGE. FALSE INDICATION. ON DEPARTURE AT ROTATION HAD A STATUS MSG L EMERG INST XFER BUS MSG AT AROUND 4000FT. MTC DID AN INSTRUMENT BUS VOLTAGE SENSING UNIT TEST FOR THE CAPT IBVSU NO 
- [SDR ABXA20261005454](https://openairdocs.org/sdr/ABXA20261005454), Oct 5, 2026: FIRE LOOP. WARNING MESSAGE. R ENG FIRE LP 1 EICAS MESSAGE. DEFERRED "R ENG FIRE LP1" EICAS MESSAGE IAW MEL 26-11-1-1. MX PROCEDURE COMPLIED WITH. MBCB 10/15/2026. PLACARD INSTALLED. NO ETO
- [SDR ABXA20260918426](https://openairdocs.org/sdr/ABXA20260918426), Sep 18, 2026: SKIN. DAMAGED. DURING AIRCRAFT C-5 CHECK, LT WING L/E JUST OTBD OF NR 1 ENG, APPROX 4 INCHES, L/E PANEL APPEARS DEFORMED ON UPPER AND LOWER SURFACE. MAINTENANCE FOUND A CRACK 
- [SDR ABXA20260918425](https://openairdocs.org/sdr/ABXA20260918425), Sep 18, 2026: FRAME. CRACKED. DURING AIRCRAFT C-5 CHECK, MAINTENANCE DISCOVERED A CRACK IN THE BS 1809.5 BULKHEAD AFT OUTER FRAME BETWEEN S-5L AND S-6L. THIS CRACK IS OUT OF LIMITS IAW SRM A
- [SDR ABXA20260918424](https://openairdocs.org/sdr/ABXA20260918424), Sep 18, 2026: WEB. CRACKED. CRACK INDICATION FOUND DURING LFEC INSPECTION AT FASTENER COMMON WITH L/H SIDE STA 1809 BULKHEAD WEB BELOW UPPER LONGERON LOWER TENSION FITTING .REAMED 1EA HOLE
- [SDR ABXA20260918423](https://openairdocs.org/sdr/ABXA20260918423), Sep 18, 2026: SKIN. CORRODED. DURING AIRCRAFT C5-CHECK , MAINTENANCE DISCOVERED CORROSION DAMAGE ON THE UPPER SKIN PANEL OF THE RIGHT HORIZONTAL STABILIZER BETWEEN FRONT SPAR HSS 157.439 AND
- [SDR ABXA20260918422](https://openairdocs.org/sdr/ABXA20260918422), Sep 18, 2026: SKIN. CORRODED. DURING AIRCRAFT C5 CHECK, MAINTENANCE DISCOVERED RT HORZ STAB UPPER SKIN HAS EVIDENCE OF CORROSION, 24 INCHES AFT OF THE LEADING EDGE AT AUX SPAR HSS 365 JM-1 C
- [SDR ABXA20260918421](https://openairdocs.org/sdr/ABXA20260918421), Sep 18, 2026: FRAME. CRACKED. DURING AIRCRAFT C5 CHECK, MAINTENANCE DISCOVERED CRACK INDICATIONS ON THE RT INNER FRAME AT STA 903.5 WHILE ACCOMPLISHING AN HFEC SURFACE SCAN IAW REF D. AN OPE
- [SDR ABXA20260918420](https://openairdocs.org/sdr/ABXA20260918420), Sep 18, 2026: INTERCOSTAL. CRACKED. L/H AFT CARGO INTERCOSTAL AT STA 1395 CRACKED ON FWD CORNER BETWEEN STRINGER S-29L AND S-30L. AR 29. REMOVED AND REPLACED 1 EA AFT CARGO INTERCOSTAL @ STA 1395 
- [SDR ABXA20260918419](https://openairdocs.org/sdr/ABXA20260918419), Sep 18, 2026: STRINGER. DAMAGED. (FORWARD PIT) DAMAGED STRINGER BETWEEN STA 522-544 STRINGER 33L ACCOMPLISHED REPAIR OF STRINGER 332 BETWEEN STA. 522-544 IAW B767-300 SRM 53-00-03 REPAIR 2.
- [SDR ABXA20260918418](https://openairdocs.org/sdr/ABXA20260918418), Sep 18, 2026: STRUCTURE. CRACKED. DURING C5 CHECK FOUND CRACK IN LH HORIZONATL STAB. INNER CORD ,STA 1809.5 ON INSPECTION CARD ABX-NEA-5330-0043-001. PERFORMED REPAIRED IAW ABX JOB CARD ABX-EA-5
- [SDR ABXA20260918417](https://openairdocs.org/sdr/ABXA20260918417), Sep 18, 2026: STRUCTURE. CRACKED. DURING C5 CHECK FOUND CRACK IN RH HORIZONTAL STAB. INNER CORD ,STA 1809.5 ON INSPECTION CARD ABX-NEA-5330-0042-001. PERFORMED REPAIRED IAW ABX JOB CARD ABX-EA-5
- [SDR ABXA20260508191](https://openairdocs.org/sdr/ABXA20260508191), May 8, 2026: ISOLATION VALVE. WARNING LIGHT. AFTER ENGINE START, L BLEED ISOLATION VALVE DISCRETE LIGHT AND YELLOW EICAS MESSAGE ON WHEN VALVE COMMANDED CLOSED. CREW RETURNED TO GATES (BTB). MTC SWAPPED L+
- [SDR ABXA202603108092](https://openairdocs.org/sdr/ABXA202603108092), Mar 8, 2026: BLOWER. INOPERATIVE. DURING MAINTENANCE INSPECTION, "AFT DET FAN" EICAS MESSAGE. MAINTENANCE REPLACED AFT CARGO SMOKE DET AIR FLOW BLOWER 1, M718 PER B767 AMM 26-16-02. SYSTEM CHECK
- [SDR ABXA20260205049](https://openairdocs.org/sdr/ABXA20260205049), Feb 5, 2026: PUMP. WARNING MESSAGE. DURING TAXI OUT, L FWD FUEL PUMP EICAS MESSAGE ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE DEFERRED IAW MEL 28-22-1 CAT "C" MX PROCEDURES CW. PL
- [SDR ABXA2026011109010](https://openairdocs.org/sdr/ABXA2026011109010), Jan 9, 2026: FIRE DETECTOR. FAULTED. DEFERRED RT ENG FIRE DETECTION SYSTEM LP1 DUE TO HISTORY. IAW MEL 26-11-1-1. MAINTENANCE PROCEDURES CW. PLACARD INSTALLED. AC REMAINS NO ETOPS. MBCB 01/29/2026 
- [SDR ABXA20260109009](https://openairdocs.org/sdr/ABXA20260109009), Jan 9, 2026: FIRE DETECTOR. FAULTED. DEFERRED LT ENG FIRE DETECTION SYSTEM LP1 IAW MEL 26-11-1-1. MAINTENANCE PROCEDURES CW. PLACARD INSTALLED. AC REMAINS NO ETOPS. MBCB 01/29/2026 AND RETURNED AC 
- [SDR ABXA20251211326](https://openairdocs.org/sdr/ABXA20251211326), Dec 11, 2025: FIRE LOOP. WARNING MESSAGE. DURING INSPECTION, RIGHT ENG FIRE LOOP 1 STATUS MESSAGE. DEFERRED R ENG FIRE LOOP 1 IAW MEL 26-11-1-1. MAINTENANCE PROCEDURES CW. PLACARD INSTALLED. AC REMAINS 
- [SDR ABXA20250912225](https://openairdocs.org/sdr/ABXA20250912225), Sep 12, 2025: WINDOW. CRACKED. DURING CLIMB, R1 WINDOW HEAT EICAS WITH WINDOW CRACKING.. AIRCRAFT RETURNED TO CVG. (ATB). MTX GROUNDED AC . REMOVED AND REPLACED R1 WINDOW AND WINDOW HEAT CONT
- [SDR ABXA20250802169](https://openairdocs.org/sdr/ABXA20250802169), Aug 2, 2025: START VALVE. INOPERATIVE. ON TAXI, RT ENGINE START VALVE INOP. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE DEFERRED IAW MEL C ABX-80-00-2-1. REMOVED AND REPLACED RT ENGINE START VALVE
- [SDR ABXA20250707142](https://openairdocs.org/sdr/ABXA20250707142), Jul 7, 2025: TRANSDUCER. FAULTED. ANTI-SKID MSG AFTER PUSHBACK AND ENGINE START. *#8 XCDR SYSTEM FAULT* AIRCRAFT RETURNED TO BLOCKS. (BTB) MAINTENANCE DEFERRED IAW MEL C ABX-32-42-1-1A. AIRCRAFT
- [SDR ABXA20250331067](https://openairdocs.org/sdr/ABXA20250331067), Mar 31, 2025: IDG. FAULTED. DURING TAXI OUT AFTER ENGINE START, EICAS MESSAGE APPEARED RT GENERATOR OFF. A/C RETURNED TO BLOCKS (BTB). DEFERRED RT ENGINE IDG IAW MEL ABX-24-00-1-1. MBCB 04
- [SDR ABXA20250314055](https://openairdocs.org/sdr/ABXA20250314055), Mar 14, 2025: ACTUATOR. LEAKING. DURING TAXI AFTER START RH HYDRAULIC QUANTITY EICAS MSG. QUANTITY ON STATUS PAGE 0.22. A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C. INSPECTED AND FOUND 
- [SDR ABXA20250219047](https://openairdocs.org/sdr/ABXA20250219047), Feb 19, 2025: SMOKE DETECTOR. MALFUNCTIONED. MAIN DECK FIRE INDICATION AND SMELL OF SMOKE ON FLT DECK DURING DE-ICING , CREW DECLARED EMERGENCY AND CALL FIRE RESCUE , AND (QRH) PERFORMED EVACUATION PROCEED
- [SDR ABXA20250217043](https://openairdocs.org/sdr/ABXA20250217043), Feb 17, 2025: ANTI-ICE VALVE. FAILED. ON BLOCK OUT L ENG A/I VALVE FAILED TO OPEN , A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C .MTX MANUALLY ACTUATED VALVE ,THEN OPS CHECKS WERE GOOD IAW B7
- [SDR ABXA20250206034](https://openairdocs.org/sdr/ABXA20250206034), Feb 6, 2025: BLEED AIR SYS. FAULTED. DURING TAXI WHILE STARTING ENGINE APU DOES NOT HAVE PNEUMATIC AIR FOR ENGINE START,A/C THEN RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C. MTX DEFERRED APU AI
- [SDR ABXA20250120017](https://openairdocs.org/sdr/ABXA20250120017), Jan 20, 2025: VALVE. WARNING MESSAGE. FWD EQPT VAL YELLOW MESSAGE APPEARED WHILE ENTERING RUNWAY FOR TAKEOFF. QRH PROCEDURES DID NOT REMEDY.AC RETURNED TO THE GATE (BTB) AND MTX GROUNDED ACFT , MTX 
- [SDR ABXA20250115010](https://openairdocs.org/sdr/ABXA20250115010), Jan 15, 2025: IRU. MALFUNCTIONED. DURING TAXI THE CTR IRU FAIL APPEARED , AC RETURNED TO THE GATE (BTB) MTX GROUNDED AC AND MTX REMOVED AND REPLACED CENTER IRU UNIT IAW AMM 34-21-00 OPS CHECK GO
- [SDR ABXA2025010503](https://openairdocs.org/sdr/ABXA2025010503), Jan 5, 2025: WARNING LIGHT. FALSE ACTIVATION. DUING TAXI AFTER ENGINE START L ENG.ANTI ICE AND VALVE LIGHT ILLUMINATED AC RETURNED TO GATE(BTB) MTX GROUNDED AC MTX MANUALLY ACTUATED VALVE AND PERFORMED OPS 
- [SDR ABXA20241219262](https://openairdocs.org/sdr/ABXA20241219262), Dec 19, 2024: WARNING MESSAGE. FALSE ACTIVATION. DURING CLIME OUT LE SLAT DISAGREE LIGHT CAME ON ,AC RETURNED TO FIELD (ATB) AND MAINTENACE GROUNDED AC , MTX T/S IAW KAC FIM 27-51 FT 809. FSEU SHOWS NO EXISITI
- [SDR ABXA20241003182](https://openairdocs.org/sdr/ABXA20241003182), Oct 3, 2024: WARNING MESSAGE. ILLUMINATED. DURING PUSHBACK FWD CABIN TEMP EICAS MSG AC RETURNED TO BLOCK AND MTX GROUNDED AC . DEFERRED FOR DEPARTURE IAW MEL ABX-21-61-6-2 . AND RETURNED AC TO SERVICE AN
- [SDR ABXA20240830167](https://openairdocs.org/sdr/ABXA20240830167), Aug 30, 2024: SWITCH. OUT OF POSITION. POST C-CHECK MAINTENANCE EVALUATION FLIGHT. CLIMBING THROUGH 10,000' VMO POINTER/BARBER POLE FAILED TO INCREASE SPEED TURNED OFF A/T TO CONTROL SPEED. AIRCRAFT 
- [SDR ABXA20240830164](https://openairdocs.org/sdr/ABXA20240830164), Aug 30, 2024: FRAME. CORRODED. "WHILE 762CK WAS UNDERGOING C-CHECK IN OSC, MAINTENANCE FOUND CORROSION ON THE FRAME WEB AT STA 1307, BETWEEN S-371 & S-381 ATLBL 11. CORROSION REMOVAL EXCEEDED
- [SDR ABXA20240830163](https://openairdocs.org/sdr/ABXA20240830163), Aug 30, 2024: KEELBEAM. DAMAGED. WHILE 762CK WAS UNDERGOING C-CHECK IN OSC, MAINTENANCE DISCOVERED DAMAGE TO THE KEEL BEAM HORIZONTAL WEB AT STA 860 AND BL 0. AFTER DAMAGE REMOVAL, THE REMAININ
- [SDR ABXA20240830162](https://openairdocs.org/sdr/ABXA20240830162), Aug 30, 2024: SKIN. CORRODED. WHILE 762CK WAS UNDERGOING C-CHECK IN OSC. MAINTENANCE DISCOVERED CORROSION ON THE L/H WING UPPER SKIN AT WING STA 1066, BETWEEN RIB 33 & 34, AT THE FWD SPAR. A
- [SDR ABXA20240830161](https://openairdocs.org/sdr/ABXA20240830161), Aug 30, 2024: SKIN. CORRODED. WHILE 762CK WAS UNDERGOING C-CHECK IN OSC. MAINTENANCE DISCOVERED CORROSION ON THE L/H WING UPPER SKIN AT WING STA 1066, BETWEEN RIB 33 & 34, AT THE FWD SPAR. A
- [SDR ABXA20240612110](https://openairdocs.org/sdr/ABXA20240612110), Jun 12, 2024: WARNING LIGHT. FALSE ACTIVATION. DURING TAXI BULK CARGO DOOR INDICATION UPON STARTING #2 ENGINE . AC RETURNED TO THE GATE AND MAINTENANCE GROUNDED AC. OPENED AND CLOSED BULK CARGO DOOR MULTIPLE
- [SDR ABXA2024032868](https://openairdocs.org/sdr/ABXA2024032868), Mar 28, 2024: HOSE. BROKEN. ON TAXI OUT GOT EICAS MESAGE L HYD QTY FOLLOWINED BY CAUTION BEEPER EICAS MESSAGE L HYD SYSTEM PRESS. STATUS PAGE SHOWED L HYD QTY 0.17 RF. FOUND BROKEN / DAMAG
- [SDR ABXA20230703140](https://openairdocs.org/sdr/ABXA20230703140), Jul 1, 2023: COMPUTER. MALFUNCTIONED. AFTER ENGINE START, WE HAD AN ELEV FEEL STATUS MESSAGE. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REPLACED ELEVATOR FEEL COMPUTER PER B767
- [SDR ABXA20230608115](https://openairdocs.org/sdr/ABXA20230608115), Jun 8, 2023: UNKNOWN. UNKNOWN. RUDDER TRIM INDICATOR INOPERATIVE ON TAXI OUT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE . MAINTENANCE DEFERRED IAW MEL 27-21-3. AIRCRAFT RETURNED TO S
- [SDR ABXA20230605114](https://openairdocs.org/sdr/ABXA20230605114), Jun 5, 2023: UNKNOWN. UNKNOWN. LT HYDRAULIC QUANTITY DROPPING DURING TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE INSPECTED AIRCRAFT FOR HYDRAULIC LEAKS. NO EXTERNAL 
- [SDR ABXA2023051297](https://openairdocs.org/sdr/ABXA2023051297), May 11, 2023: UNKNOWN. UNKNOWN. TE FLAP DISAGREE EICAS MESSAGE ILLUMINATED AFTER FLAPS 5 WERE SELECTED & INDICATED 5. MISSED THE APPROACH AND PERFORMED TROUBLESHOOTING & QRH PROCEDURES. DUE TO
- [SDR ABXA2023040550](https://openairdocs.org/sdr/ABXA2023040550), Apr 3, 2023: UNKNOWN. UNKNOWN. AUTO THROTTLES DISCONNECTED ON TAKE OFF ROLL. LOW SPEED ABORT. AIRCRAFT EXITED RUNWAY AND CONTACTED MAINTENANCE CONTROL. AUTO THROTTLE SYSTEM WAS DEFERRED BY TH
- [SDR ABXA2023020319](https://openairdocs.org/sdr/ABXA2023020319), Feb 2, 2023: NOT ENTERED. NOT ENTERED. AFT CABIN TEMP INOP LIGHT ON DURING TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE C/W CABIN TEMP SENSOR FILTER CLEANING PER AMM 21-51-00
- [SDR ABXA20221214151](https://openairdocs.org/sdr/ABXA20221214151), Dec 13, 2022: AUTOTHROTTLE SYS. FAULT MESSAGE. ON TAKEOFF ROLL AFTER (THR) SELECTED EICAS MSG AUTO THROTTLE DISC DISPLAYED. AIRCRAFT EXITED ON TO TAXI WAY AND AUTO THROTTLE SYSTEM WAS DEFFERED BY FLIGHT CREW
- [SDR ABXA20221210150](https://openairdocs.org/sdr/ABXA20221210150), Dec 8, 2022: AUTOTHROTTLE SYS. MALFUNCTIONED. LOW SPEED ABORT LESS THAN 70 KIAS AUTO THROT DISC ANNUCIATED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED AUTO THROTTLE SYSTEM IAW 
- [SDR ABXA2022122143](https://openairdocs.org/sdr/ABXA2022122143), Dec 1, 2022: WARNING MESSAGE. FALSE ACTIVATION. A/T DISC ON LOW SPEED TAKE OFF, TAKE OFF ABORTED. FLIGHT CREW DEFERRED 22-30-1A. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENCE. MAINTENANCE CHECKED MCDP FAILURES.
- [SDR ABXA20220930103](https://openairdocs.org/sdr/ABXA20220930103), Sep 30, 2022: PUMP. INOPERATIVE. C HYDRAULIC PRIMARY 2 PUMP DID NOT COME BACK ON AFTER ENG START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED THE C 2 HYDRAULIC PUMP

All 100: https://openairdocs.org/aircraft/N762CK/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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