# N763CK: 1993 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: 26233
- Year built: 1993
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 1, 2018
- Certificate issued: January 10, 2017
- Expires: January 31, 2030
- Mode S code: AA4CE9
- 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=763CK
- Page: https://openairdocs.org/aircraft/N763CK

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 N763CK.

## FAA accident and incident reports

None matched to N763CK.

## Service difficulty reports (94, 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 ABXA20261011467](https://openairdocs.org/sdr/ABXA20261011467), Oct 11, 2026: FIRE LOOP. FALSE INDICATION. AFTER BLOCK OUT STATUS MESSAGE R ENG FIRE LP2 APPEARED. DEFERRED R ENG FIRE LP 2 IAW MEL 26-11-1-1. NO MX ACTION REQUIRED. PLACARDS INSTALLED. MBCB 10/21/26. A/
- [SDR ABXA20261008462](https://openairdocs.org/sdr/ABXA20261008462), Oct 8, 2026: WARNING MESSAGE. FALSE ACTIVATION. RIGHT ENGINE FIRE LOOP 2 STATIC MSG. MTC PERFORMED OPS TEST OF RIGHT ENGINE FIRE LOOP IAW AMM 26-11-00, OPS TEST GOOD. ACFT REMAINS NO ETOPS. ACFT RETURNED TO S
- [SDR ABXA20261005446](https://openairdocs.org/sdr/ABXA20261005446), Oct 5, 2026: START VALVE. FAULTED. DURING TAXI, RIGHT ENG START VALVE. CREW RETURNED TO THE GATE (BTB). MTC DEFERRED R ENG START VALVE IAW B767 MEL 80-00-2-1. MX PROCEDURES C/W. PLACARDS INSTALLE
- [SDR ABXA20260809355](https://openairdocs.org/sdr/ABXA20260809355), Aug 9, 2026: INDICATOR. INOPERATIVE. APU BOTTLE DISCHARGE LIGHT INOPERATIVE. AIRCRAFT RELEASED WITH IAW MEL 26-22-1-2A. AND GMM 07.04 MBCB: AUG 18, 2026. APU BOTTLE DISCHARGE 2 LIGHT INOP. ACFT NO 
- [SDR ABXA20260717322](https://openairdocs.org/sdr/ABXA20260717322), Jul 17, 2026: UNKNOWN. ODOR. DURING CRUISE, STRONG SMELL OF SMOKE AT 25000' AND AT 8000'. MTC PERFORMED T/S IAW B767 AMM 05-51-56. DID NOT FIND EVIDENCE OF SMOKE, COULD NOT DUPLICATE. A/C R
- [SDR ABXA20260707308](https://openairdocs.org/sdr/ABXA20260707308), Jul 7, 2026: WARNING MESSAGE. FALSE ACTIVATION. RT WING HYD VALVE EICAS MSG DISPLAYED DURING TAXI. ACFT RETURNED TO THE GATE (BTB) AND MTX GROUNDED ACFT. MTX PERFORMED OPS CHECK OF RT WING HYD SHUTOFF VALVE I
- [SDR ABXA20260605246](https://openairdocs.org/sdr/ABXA20260605246), Jun 5, 2026: LIFE VEST. MISSING. FIRST OFFICER LIFE VEST IS MISSING, MTX DEFERRED FO'S LIFE VEST IAW ABX MEL 25-62-1A CAT D MBCB 10-02-26 MX PROCEDURES C/W PLACARDS INSTALLED . AND RETURNED ACF
- [SDR ABXA20260409154](https://openairdocs.org/sdr/ABXA20260409154), Apr 9, 2026: MODULE. NO TEST. DURING MTC PREFLIGHT, AFOTLS TEST IS INDICATING BUT NO AURAL WARNINGS. REPLACED MODULE ASSY, AURAL WARNING (M1000) IAW AMM 31-51-04 OPS CHECK GOOD. AIRCRAFT REM
- [SDR ABXA20260325131](https://openairdocs.org/sdr/ABXA20260325131), Mar 25, 2026: FUEL LINE. RUPTURED. RIGHT ENG FAILED DURING CLIMB HAD ROTATION - UNABLE TO RESTART. CREW COMPLETED AN IN FLIGHT SHUTDOWN (IFS), DECLARED AN EMERGENCY (EDC) AND DID AN AIR TURN BACK
- [SDR ABXA20260210064](https://openairdocs.org/sdr/ABXA20260210064), Feb 10, 2026: STARTER. DEFECTIVE. DURING TAXI OUT, AND DURING ENG START N2 STAGNATED AT ABOUT 26%. SHORTLY AFTER THE START WAS ABORTED. THE ABORTED START CHECKLIST WAS RUN, AND N2 WAS DECREASING
- [SDR ABXA20260124026](https://openairdocs.org/sdr/ABXA20260124026), Jan 24, 2026: SEQUENCE VALVE. MALFUNCTIONED. DEPARTING SJU, CREW REPORTED A GEAR DISAGREE & GEAR DOOR LIGHT MESSAGE WHEN GEAR IN UP POSITION. ALSO REPORTED GEAR INDICATION LIGHTS EXTINGUISHED. FOLLOWED QRH
- [SDR ABXA20251212335](https://openairdocs.org/sdr/ABXA20251212335), Dec 12, 2025: FIRE LOOP. FAULTED. CARGO FIRE B ROW YELLOW LIGHTS ON,MTX,DEFERRED FOR DEPARTURE IAW MEL 26-16-2-2 MX ACTIONS C/W PLACARDS INSTALLED. AC REMAINS NO ETOPS. REPETITIVE ITEM REQUIRES 
- [SDR ABXA202512062319](https://openairdocs.org/sdr/ABXA202512062319), Dec 2, 2025: AUTOTHROTTLE SYS. MALFUNCTIONED. THE AUTO-THROTTLE WOULD NOT ENGAGE DURING THE TAKEOFF ROLL. PERFORMED A LOW SPEED REJECTED TAKEOFF (<30 KNOTS). CLEARED RUNWAY TO TROUBLE SHOOT. FOLLOWED GUIDAN
- [SDR ABXA20250710156](https://openairdocs.org/sdr/ABXA20250710156), Jul 10, 2025: SEAT TRACK. DAMAGED. DURING 763CK'S C4 CHECK IN OSC, KALITTA MAINTENANCE FOUND SEAT TRACK HAS DAMAGE IN CENTER CHANNEL @ LBL 11, STA 1263-1274 TT41 .ACCOPLISHED REPAIR ON SEAT TRACK
- [SDR ABXA20250710154](https://openairdocs.org/sdr/ABXA20250710154), Jul 10, 2025: BEAM. CORRODED. DURING 763CK'S C4 CHECK IN OSC, KALITTA MAINTENANCE CORROSION FOUND NOSE WHEEL WELL BEAM STA: 266.5 RIGHT HAND E&E BAY TUNNEL REPAIRED DAMAGED BEAM IAW B767-300
- [SDR ABXA20250710153](https://openairdocs.org/sdr/ABXA20250710153), Jul 10, 2025: STRINGER. CORRODED. DURING 763CK'S C4 CHECK IN OSC, KALITTA MAINTENANCE CORROSION FOUND ON STRINGER 39L AT STA. 1285-1263.ACCOMPLISHED REPAIR OF STRINGER 39L IAW B767-300 SRM 53-00
- [SDR ABXA20250710152](https://openairdocs.org/sdr/ABXA20250710152), Jul 10, 2025: FRAME. CRACKED. DURING 763CK'S C4 CHECK IN OSC, KALITTA MAINTENANCE CRACK IN STA 903.5, RBL 89, FRAME INNER CHORD FOUND DURING ACCOMP OF ABX-NEA-5300-0050. RPR'D PER ABX-EA-530
- [SDR ABXA20250710151](https://openairdocs.org/sdr/ABXA20250710151), Jul 10, 2025: FRAME. CRACKED. DURING 763CK'S C4 CHECK IN OSC, KALITTA MAINTENANCE FOUND CRACK R1 DOOR THRESHOLD LOWER AFT CORNER MARKED CRACK ACCOMPLISHED REPAIR OF R1 DOOR AFT CORNER IAW B7
- [SDR ABXA20250710150](https://openairdocs.org/sdr/ABXA20250710150), Jul 10, 2025: STRINGER. CORRODED. DURING 763CK'S C4 CHECK IN OSC, KALITTA MAINTENANCE FOUND BULK CARGO STRINGER AT STA.1540 STR39R HAS EVIDENCE OF CORROSION .REPAIRED STRINGER AT STA 1540 SR39R 
- [SDR ABXA20250710149](https://openairdocs.org/sdr/ABXA20250710149), Jul 10, 2025: SKIN PANEL. CORRODED. DURING 763CK'S C4 CHECK IN OSC, KALITTA MAINTENANCE FOUND CORROSION ON THE UPPER SKIN PANEL #1 (P/N 112T3301-1) UNDER PANEL #9 (P/N 113T1609-1), AFT OF THE REAR
- [SDR ABXA20250710148](https://openairdocs.org/sdr/ABXA20250710148), Jul 10, 2025: FRAME. CORRODED. DURING 763CK'S C4 CHECK AT OSC KALITTA, CORROSION WAS FOUND ON THE STA 1153 FRAME ASSEMBLY INNER CHORD (P/N 146T1060-2) IN THE LOWER CARGO COMPARTMENT. THE CHOR
- [SDR ABXA20250710147](https://openairdocs.org/sdr/ABXA20250710147), Jul 10, 2025: SKIN PANEL. CORRODED. DURING 763CK'S C4 CHECK AT KALITTA, CORROSION WAS FOUND ON THE LH WING, LOWER SKIN PANEL #3 BETWEEN WING STATION 668.2 - 694.2, RIB 19 - 20 AND A BLENDOUT WAS A
- [SDR ABXA20250710146](https://openairdocs.org/sdr/ABXA20250710146), Jul 10, 2025: FLOORBEAM. CORRODED. WHILE 763CK WAS UNDERGOING C-CHECK IN OSC, CORROSION WAS FOUND ON THE UPPER CHORD OF THE STA 228.5 TRANSVERSAL FLOOR BEAM. (P/N 141T5810). THE CORROSION WAS REM
- [SDR ABXA20250710145](https://openairdocs.org/sdr/ABXA20250710145), Jul 10, 2025: SKIN PANEL. DAMAGED. WHILE 763CK WAS UNDERGOING C-CHECK IN OSC, DAMAGE WAS FOUND ON THE LH INBOARD ELEVATOR (P/N 183T2001-29; S/N 000518). THE DAMAGE WAS ON THE OUTBOARD EDGE NEAR T
- [SDR ABXA20250329066](https://openairdocs.org/sdr/ABXA20250329066), Mar 29, 2025: SHUTOFF VALVE. FROZEN. DURING TAXI OUT, RT ENG PRV ON TAKEOFF. ABORTED TAKEOFF ABOUT 120 KTS. RIGHT BRAKES UP TO 9 ON TEMP. REUTRNED TO BLOCKS (BTB). REMOVED AND REPLACED RT ENGINE PR
- [SDR ABXA20250206033](https://openairdocs.org/sdr/ABXA20250206033), Feb 6, 2025: WARNING LIGHT. FALSE ACTIVATION. DURING AFTER START CHECK LIST, C HYD SYS PRESS DISCRETE LIGHT AND EICAS MSG DISPLAYED. QRH PROCEDURE DID NOT FIX THE ISSUE.AC/ REURNED TO THE GATE (BTB) AND MTX
- [SDR ABXA20241231275](https://openairdocs.org/sdr/ABXA20241231275), Dec 31, 2024: START VALVE. MALFUNCTIONED. DURING TAXI OUT WHILE STARTING RH ENGINE ,RH ENGINE STARTER WILL NOT ENGAGE AFTER START SWITHCH TO GROUND VALVE LIGHT STAYS ON , AC RETURNED TO GATE (BTB) AND M
- [SDR ABXA20241220267](https://openairdocs.org/sdr/ABXA20241220267), Dec 20, 2024: START VALVE. FAULTED. DURING TAXI WHILE STARTING RH ENGINE ,RIGHT STARTER CUTOUT EICAS MESSAGE APPEARED AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC MTX DEFERRED RH START VALVE FOR 
- [SDR ABXA20241017190](https://openairdocs.org/sdr/ABXA20241017190), Oct 17, 2024: WARNING MESSAGE. FALSE INDICATION. DURING TAXI OUT FLAP/SLAT ELEC. MSG. APPEARED, AC RETURNED TO THE GATE AND MTX GROUNDED THE AC . MTX PERFORMED BITE TEST OF FSEU IAW FIM 27-51-50-00, NO DEFECTS
- [SDR ABXA20240608109](https://openairdocs.org/sdr/ABXA20240608109), Jun 8, 2024: WARNING MESSAGE. FALSE ACTIVATION. DURING TAXI AIR GROUND DISAGREE STATIS MEASEAGE APPEARED AC RETURNED TO GATE AND MAINTENANCE GROUNDED AC . VERIFIED SENSOR 244 CHECKS NORMAL IAW AMM 32-09-08 , 
- [SDR ABXA2024052092](https://openairdocs.org/sdr/ABXA2024052092), May 20, 2024: TRANSPONDER. MALFUNCTIONED. DURING TAXI OUT ATC NOT RECEIVING INFO FROM EITHER XPDR . NO EICAS MSG. AC RETURNED TO THE GATE AND MAINTENANCE GROUNDED AC AND PERFORMED OPS CHECK IAW B767 AMM
- [SDR ABXA2024050489](https://openairdocs.org/sdr/ABXA2024050489), May 4, 2024: SKIN. CRACKED. DURING ROUTINE LINE OPERATIONS IN MIA, MAINTENANCE DISCOVERED TWO CRACKS AT THE RH EMPENNAGE SECTION AT STA. 1654.5. AT APPROXIMATELY STRINGER 15R. BOTH CRACKS 
- [SDR ABXA2024041680](https://openairdocs.org/sdr/ABXA2024041680), Apr 16, 2024: ENGINE. UNKNOWN. ON TAXI OUT RT ENGINE DID NOT STABILIZE AFTER START ON 1ST ATTEMPT .AC RETURNED TO GATE AND MAINTENANCE GROUNDED AC . MAINTENANCE PERFORMED RH ENG RUN PER AMM 7
- [SDR ABXA202402270647](https://openairdocs.org/sdr/ABXA202402270647), Feb 26, 2024: PITOT HEAD. MALFUNCTIONED. DURING TAXI F/O PITOT FAILED AFTER ENGINE START . AC RETURNED TO GATE AND MAINTENACE GROUNDED AC . TROUBLE SHOT AND REMOVED AND REPLACED F/O PITOT-STATIC PROBE(
- [SDR ABXA2024020820](https://openairdocs.org/sdr/ABXA2024020820), Feb 8, 2024: CIRCUIT CARD. MALFUNCTIONED. AMENDED:.AFTER BOTH ENG'S STARTED ADP PRESS LGT ILLUMINATED PRESS LGT STAYS ILUMINATED WITH SELECTOR SWITCH IN ON POSTION .AC RETURNED TO THE GATE , MAINTENACE 
- [SDR ABXA20240209820](https://openairdocs.org/sdr/ABXA20240209820), Feb 8, 2024: WARNING LIGHT. ILLUMINATED. AFTER BOTH ENG'S STARTED ADP PRESS LGT ILLUMINATED PRESS LGT STAYS ILUMINATED WITH SELECTOR SWITCH IN ON POSTION .AC RETURNED TO THE GATE , MAINTENACE GROUNDED 
- [SDR ABXA20230912185](https://openairdocs.org/sdr/ABXA20230912185), Sep 11, 2023: UNKNOWN. UNKNOWN. AILERON LOCKOUT MESSAGE DISPLAYED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE DEFERRED AILERON LOCKOUT SYSTEM PER MEL 27-11-2. AIRCRAFT RET
- [SDR ABXA20230905183](https://openairdocs.org/sdr/ABXA20230905183), Sep 5, 2023: UNKNOWN. UNKNOWN. DURING PUSH BACK MAINTENANCE NOTED TOILET DOOR SERVICE SNAPPED. REALLIGHNMENT HINGE SPRINGS AND SECURED DOOR CLOSED IAW AMM 52-49-07
- [SDR ABXA20230705142](https://openairdocs.org/sdr/ABXA20230705142), Jul 3, 2023: STARTER. FAILED. #2 ENGINE DID NOT ROTATE WHEN SELECTED TO START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED RH STARTER, REF AMM 80-11-
- [SDR ABXA2023042865](https://openairdocs.org/sdr/ABXA2023042865), Apr 26, 2023: UNKNOWN. UNKNOWN. AFTER PUSHBACK NOSE A/G SYS EICAS ADVISORY AND NOSE A/G DISAGREE STATUS MESSAGE APPEARED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFOR
- [SDR ABXA2023041857](https://openairdocs.org/sdr/ABXA2023041857), Mar 9, 2023: RIB. GOUGED. WHILE IN C-CHECK AT KALITTA IN OSC. IT WAS FOUND THAT RIGHT WING LEADING EDGE BULL NOSE PANEL GOUGED AT APPROX LES 500.10, TD10. AFTER BLENDING IT WAS FOUND TO 
- [SDR ABXA2022125144](https://openairdocs.org/sdr/ABXA2022125144), Dec 2, 2022: THRUST REVERSER. NOT CLOSED. ON PUSH OUT, NOTICED R/H I/B TR NOT STOWED FULLY. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PROPERLY DEFERRED R/H T/R IAW ABX MEL 78-31-1A
- [SDR KCSA2022082019](https://openairdocs.org/sdr/KCSA2022082019), Aug 20, 2022: NONE. UNKNOWN. CAPTAIN'S SIDE EMERGENCY FLASHLIGHT INOP REMOVED AND REPALCED CAPTAIN'S SIDE EMERGENCY FLASHLIGHT BATTERY IAW B767-300 AMM 25-54-02 OPERATIONS CHECK GOOD NO DEF
- [SDR KCSA202103171022](https://openairdocs.org/sdr/KCSA202103171022), Mar 17, 2021: SEAT TRACK. CRACKED. FIRST OFFICERS AFT INBOARD SEAT TRACK P/N 1A097-0106 CRACKED
- [SDR KCSA202103171021](https://openairdocs.org/sdr/KCSA202103171021), Mar 17, 2021: SEAT TRACK. CRACKED. FIRST OFFICERS OUTBOARD AFT SEAT TRACK P/N 1A097-0508 CRACKED
- [SDR KCSA202103171020](https://openairdocs.org/sdr/KCSA202103171020), Mar 17, 2021: SEAT TRACK. CRACKED. FIRST OFFICERS FWD INBOARD SEAT TRACK P/N 1A098-0182 CRACKED
- [SDR KCSA202103171019](https://openairdocs.org/sdr/KCSA202103171019), Mar 17, 2021: SEAT TRACK. CRACKED. CAPTAINS INBOARD AFT SEAT TRACK P/N 1A097-0105 CRACKED
- [SDR KCSA202103171018](https://openairdocs.org/sdr/KCSA202103171018), Mar 17, 2021: SEAT TRACK. CRACKED. CAPTAINS OUTBOARD FWD SEAT TRACK P/N 1A098-0183 CRACKED
- [SDR KCSA202103171017](https://openairdocs.org/sdr/KCSA202103171017), Mar 17, 2021: SEAT TRACK. CRACKED. CAPTAINS INBOARD SEAT TRACK P/N 1A098-0181 CRACKED
- [SDR KCSA202103171016](https://openairdocs.org/sdr/KCSA202103171016), Mar 17, 2021: STRUCTURE. DAMAGED. R/H INBD AILERON OTBD FACE DAMAGED NEAR HINGE

All 94: https://openairdocs.org/aircraft/N763CK/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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