# N763CX: 1983 Boeing 767-232, registration cancelled 2024-08-05

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 5, 2024
- Status when cancelled: Valid registration
- Airframe: [Boeing 767-232](https://openairdocs.org/model/boeing-767-232) (registry code 1385132)
- Engine: [GE CF6-80A2](https://openairdocs.org/engine/ge-cf6-80a2) (registry code 30095)
- Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM), [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (OpenAirDocs)
- Serial number: 22223
- Year built: 1983
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 1, 2010
- Certificate issued: April 13, 2010
- Last registry action: September 29, 2023
- Mode S code: AA4CF5
- Owner when cancelled: [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC)
- Location: [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.4607° N, 83.8443° W: Placed by OpenAirDocs at the center of ZIP code 45177, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N763CX
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=763CX
- Page: https://openairdocs.org/deregistered/N763CX-2024-08-05

From the FAA registry file of November 5, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Boeing 767-232: https://openairdocs.org/model/boeing-767-232.md

## Service difficulty reports (131, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR IXXA20220922134](https://openairdocs.org/sdr/IXXA20220922134), Sep 18, 2022: BATTERY. INOPERATIVE. PRE-DEPARTURE, EMERGENCY FLASH LIGHT INOP. SYSTEM DEFERRED-34747 MEL CAT C. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-64-02. NO ADDITIONAL FA
- [SDR IXXA20220615118](https://openairdocs.org/sdr/IXXA20220615118), Jun 11, 2022: FLASHLIGHT. INOPERATIVE. DURING ROUTINE MAINTENANCE, EMERGENCY FLASHLIGHT OPERATIVE. REMOVED AND REPLACED EMERGENCY FLASHLIGHT ASSEMBLY IAW B767 AMM 26-64-02. OPERATIONAL CHECK GOOD.
- [SDR IXXA202204117107](https://openairdocs.org/sdr/IXXA202204117107), Apr 7, 2022: CONTROLLER. ARCED. ENROUTE FROM KRIV TO KIAH, CREW REPORTED A STRONG ELECTRICAL ODOR EMITTING FROM THE LEFT NUMBER 1 WINDOW ASSEMBLY ELECTRICAL CONNECTION. AIRCRAFT DIVERTED TO KP
- [SDR IXXA202202127009](https://openairdocs.org/sdr/IXXA202202127009), Feb 8, 2022: NONE. NONE. ENROUTE FROM KRFD TO KCLT AND CLIMBING THROUGH 12,000 WITH AUTOPILOT AND AUTOTHROTTLES ENGAGED, LEFT ENGINE CONTINUOUSLY STEADY STATE SURGE STALLED. EGT MAX IND
- [SDR IXXA2022012605](https://openairdocs.org/sdr/IXXA2022012605), Jan 26, 2022: SKIN PANEL. CORRODED. SKIN CORRODED BEYOND LIMITS
- [SDR IXXA2022012013](https://openairdocs.org/sdr/IXXA2022012013), Jan 20, 2022: STRINGER. CORRODED. STRINGER CORRODED BEYOND LIMITS.
- [SDR IXXA2022012012](https://openairdocs.org/sdr/IXXA2022012012), Jan 20, 2022: SHEAR TIE. CORRODED. SHEAR TIE CORRODED BEYOND LIMITS
- [SDR IXXA2022012011](https://openairdocs.org/sdr/IXXA2022012011), Jan 20, 2022: SHEAR TIE. CORRODED. SHEAR TIE CORRODED OUT OF LIMITS
- [SDR IXXA2022010703](https://openairdocs.org/sdr/IXXA2022010703), Jan 7, 2022: SHEAR TIE. CORRODED. SHEAR TIE CORRODED BEYOND LIMITS
- [SDR IXXA2021122303](https://openairdocs.org/sdr/IXXA2021122303), Dec 23, 2021: STRINGER. CORRODED. CORRODED STRINGER 36L
- [SDR IXXA20211115070](https://openairdocs.org/sdr/IXXA20211115070), Nov 14, 2021: PRESSURE SWITCH. FAULTED. ON FINAL APPROACH LEADING EDGE SLAT DISAGREE EICAS MESSAGE ANNUNICATED, LANDING ABORTED. CREW PERFORMED GO AROUND AND LEADING EDGE SLAT DISAGREE MESSAGE NO LONG
- [SDR IXXA20210516036](https://openairdocs.org/sdr/IXXA20210516036), May 5, 2021: SKIN. DAMAGED. AIRCRAFT GROUNDED FOR C-23 CHECK. DAMAGE TO FUSELAGE SKIN SECTION 43 BETWEEN STA 522 AND STA 566, BETWEEN STR 28R TO 34R . ACCOMPLISHED PERMANENT REPAIR AT FUSE
- [SDR IXXA20210516034](https://openairdocs.org/sdr/IXXA20210516034), May 5, 2021: STRINGER. CORRODED. AIRCRAFT GROUNDED FOR C-23 CHECK. IN ACCOMPLISHMENT OF TASK CARD ATI-53-552-01-01 STRINGER REPAIR DISCOVERED ADDITIONAL CORROSION TO STRINGER 36L 1361 TO 1336. 
- [SDR IXXA20210516033](https://openairdocs.org/sdr/IXXA20210516033), May 5, 2021: STRINGER. CORRODED. AIRCRAFT GROUNDED FOR C-23 CHECK. IN ACCOMPLISHMENT OF TASK CARD ATI-53-552-01-01 DOT 14 DOT 045 UNDERNEATH WASTE TANK VAVLE AT FS 1540-1582 BETWEEN STRINGER 37
- [SDR IXXA20210516032](https://openairdocs.org/sdr/IXXA20210516032), May 5, 2021: SKIN. SCRATCHED. AIRCRAFT GROUNDED FOR C-23 CHECK. IN ACCOMPLISHMENT OF TASK CARD ATI-53-552-01-01 MAINTENANCE IDENTIFIED D-15 DOT 163 AFT CARGO FUSELAGE SKIN SCRATCHED BETWEEN 
- [SDR IXXA20210516031](https://openairdocs.org/sdr/IXXA20210516031), May 3, 2021: PLENUM. CRACKED. AIRCRAFT GROUNDED FOR C-23 CHECK. IN ACCOMPLISHMENT OF TASK CARD ATI-24-031-01-01, MAINTENANCE IDENTIFIED SEVERAL CRACKS IN SUPPORT PLATFORM. REMOVED AND REPLAC
- [SDR IXXA20210516030](https://openairdocs.org/sdr/IXXA20210516030), May 3, 2021: STRINGER. CRACKED. AIRCRAFT GROUNDED FOR C-23 CHECK. IN ACCOMPLISHMENT OF TASK CARD 53-552-0101, MAINTENANCE IDENTIFIED D-15 DOT 162 AFT CARGO HAS TWO STRINGERS WITH MARKS AT STAT
- [SDR IXXA20190804013](https://openairdocs.org/sdr/IXXA20190804013), Jul 31, 2019: STRUCTURE. PUNCTURED. PRE DEPARTURE-PUNCTURE AFT OF LOWER CARGO DOOR BETWEEN S28R-S29R. AOG. COMPLIED WITH CONDITIONAL INSPECTION IAW B767 AMM 05-51-59/ NO FURTHER DEFECTS NOTED. TEM
- [SDR IXXA20190529008](https://openairdocs.org/sdr/IXXA20190529008), May 17, 2019: SUPPORT. CORRODED. AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE VISIT. THE FOLLOWING FINDING WAS NOTED FOR TASK CARD, 57-564-00-02- RIGHT WING TRAILING EDGE PANEL SUPPORT CORRODED AT S
- [SDR IXXA20190529009](https://openairdocs.org/sdr/IXXA20190529009), May 15, 2019: RETAINER. CORRODED. AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE VISIT. THE FOLLOWING FINDING WAS NOTED FOR TASK CARD 57-572-00-01, LOWER WING TRAILING EDGE LOWER PANEL NEAR O/B FLAP O/
- [SDR IXXA20190529011](https://openairdocs.org/sdr/IXXA20190529011), May 13, 2019: SKIN. CORRODED. AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE VISIT. THE FOLLOWING FINDING WAS NOTED FOR TASK CARD, 55-434-00-01. BLENDED CORROSION OUT OF LIMITS. NOMINAL T=.140" REM
- [SDR IXXA20190529010](https://openairdocs.org/sdr/IXXA20190529010), May 13, 2019: TRACK. CRACKED. AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE VISIT. THE FOLLOWING FINDING WAS NOTED FOR TASK CARD 71-828-00-01-O/B T/R UPPER SLIDE TRACK FAIRING IS BENT AND CHAFFED.
- [SDR IXXA20190529007](https://openairdocs.org/sdr/IXXA20190529007), May 8, 2019: SKIN. CORRODED. AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE VIST. FINDING: TASK CARD 57-572-00-02-RIGHT WING TRAILING EDGE BONDED PANEL LEADING EDGE IS BULGING WS 1050. REMOVED UPP
- [SDR IXXA20170513999](https://openairdocs.org/sdr/IXXA20170513999), May 9, 2017: ENGINE. MAKING METAL. FLIGHT ATN3706 EN ROUTE FROM DEPARTURE STATION KABE TO DESTINATION STATION KONT EICAS MESSAGE DISPLAYED "R OIL FILTER". AS DIRECTED BY QRH, THE RIGHT ENGINE WAS
- [SDR IXXA20170414238](https://openairdocs.org/sdr/IXXA20170414238), Mar 28, 2017: SHEAR TIE. CORRODED. AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. AFT SIDE OF FRAME AT STATION 742 OUTBOARD STRINGER 39R IS CORRODED. REMOVED AND REPLACED SHEAR TIE AND CLIP FROM FORWAR
- [SDR IXXA20170414236](https://openairdocs.org/sdr/IXXA20170414236), Mar 17, 2017: KEELBEAM. CORRODED. AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. UPPER KEEL WEB IN THE RIGHT MAIN LANDING GEAR WHEEL WELL HAS AREAS OF CORROSION IN THE FORWARD PASS THROUGH LOCATION. B
- [SDR IXXA20170414237](https://openairdocs.org/sdr/IXXA20170414237), Mar 16, 2017: FRAME. CRACKED. AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. STATION 859.5 LEFT BUTT LINE 89 BELOW WATER LINE 200, FRAME INNER CHORD TRANSITION RADIUS CRACKED .25" APPROXIMATELY. R
- [SDR IXXA20160429018](https://openairdocs.org/sdr/IXXA20160429018), Apr 9, 2016: SHEAR TIE. CRACKED. DURING MX VISIT ACCOMPLISHED PERMANENT REPAIR FOR THE SHEAR TIE ATTACHED TO THE LT LONGERON LOCATED AT STATION 1746.25 & WL 258.44. WORK WAS ACCOMPLISHED IAW EN
- [SDR IXXA20151107118](https://openairdocs.org/sdr/IXXA20151107118), Nov 7, 2015: SKIN. CRACKED. SKIN CRACK & PROBABLE CORROSION AT APPROX FS 1339, LONGERON 35L. REMOVED DAMAGED AREA, FABRICATED FILLER & DOUBLER, INSTALLED REPAIRED PARTS IAW SRM 51-30-01. C
- [SDR IXXA20150320050](https://openairdocs.org/sdr/IXXA20150320050), Mar 20, 2015: SPAR CAP. CORRODED. AIRCRAFT GNDED FOR HEAVY MX. WING LE FRONT SPAR UPPER CAP CORRODED AT WING LES 579. R & R SPAR CAP IAW REA 47089REA19.
- [SDR IXXA20150320049](https://openairdocs.org/sdr/IXXA20150320049), Mar 20, 2015: CAP. CORRODED. AIRCRAFT GNDED FOR HVY MX. UPPER CAP ON LE RIB AT LES 261 CORRODED 4 INCHES FROM FRONT SPAR ON INBD SIDE. REMOVED, REPAIRED & INSTALLED UPPER RIB CAP LES 261 IA
- [SDR IXXA20150320048](https://openairdocs.org/sdr/IXXA20150320048), Mar 20, 2015: SPAR CAP. CORRODED. WING LE FRONT SPAR UPPER CAP CORRODED AT LES 472. R & R SECTION OF UPPER SPAR CAP FROM LES 450 - 506 IAW EO 47089REA18.
- [SDR IXXA20150330071](https://openairdocs.org/sdr/IXXA20150330071), Mar 15, 2015: SKIN PANEL. CORRODED. AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. UPPER WING SURFACE AT STATION 187 REAR SPAR AREA PANEL IS BULGED UP. POSSIBLE SIGNS OF CORROSION UNDER PANEL.
- [SDR IXXA20150331084](https://openairdocs.org/sdr/IXXA20150331084), Feb 16, 2015: HINGE FITTING. CRACKED. AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. FWD FITTING AT BODY DOOR CTR HINGE BEAM CRACKED. R & R RT MLG DOOR HINGE FITTING AT CTR BEAM TO DOOR CTR IAW 
- [SDR IXXA20150406118](https://openairdocs.org/sdr/IXXA20150406118), Feb 13, 2015: SKIN. DAMAGED. AOG FOR HVY MX, FAILSAFE INSPECTION. AFT LOWER CARGO COMPARTMENT DOOR CUT OUT FOR PANEL 822D HAS A DAMAGED COUNTER SINK. REPAIRED DAMAGED SCREW HOLE IAW ENGINEE
- [SDR IXXA20150322061](https://openairdocs.org/sdr/IXXA20150322061), Feb 12, 2015: FITTING. CORRODED. AIRCRAFT GNDED FOR HEAVY MX. CORROSION ON LOWER PORTION OF BODY FITTING AT STATION 933 RT SIDE IN UPPER CARGO. INSTALLED NEW STUB FITTING AT RT STATION 933 IAW 
- [SDR IXXA20150322066](https://openairdocs.org/sdr/IXXA20150322066), Feb 10, 2015: STRINGER. CORRODED. AIRCRAFT GNDED FOR HEAVY MX. CORROSION ON STRINGER 36R AT STATION 445. R & R STRINGER 36R STATION 434 - 466 IAW REA 47089REA08.
- [SDR IXXA20150322060](https://openairdocs.org/sdr/IXXA20150322060), Feb 10, 2015: FLOORBEAM. CORRODED. AIRCRAFT GNDED FOR HEAVY MX. FLOOR FRAME UPPER CHORD HAS CORROSION UNDER NUTPLATES AT STATION 676, RBL 17 TO 19 LOWER SURFACE. FABRICATED, R & R FLOOR FRAME UPP
- [SDR IXXA20150322059](https://openairdocs.org/sdr/IXXA20150322059), Feb 10, 2015: FLOORBEAM. CORRODED. AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. FLOORBEAM UPPER TEE CORRODED AT BS 478, RBL 5 TO 9 AROUND NUTPLATES ON LOWER SURFACE. R & R FLOORBEAM UPPER TEE IAW DWG
- [SDR IXXA20150406114](https://openairdocs.org/sdr/IXXA20150406114), Dec 26, 2014: STRINGER. CRACKED. AOG FOR HVY MX, FAILSAFE INSPECTION. UPPER CARGO STATION 676 AFT OF SPLICE ON STRINGER 11L IS CRACKED. REMOVED, FABRICATED & INSTALLED NEW STRINGER IAW ENGINEER
- [SDR IXXA20150406116](https://openairdocs.org/sdr/IXXA20150406116), Dec 23, 2014: FLOORBEAM. CRACKED. AOG FOR HVY MX, FAILSAFE INSPECTION. STATION 1021 CTR FLOORBEAM FITTING CRACKED. R & R FLOORBEAM ATTACH FITTING IAW SRM 51-40-02.
- [SDR IXXA20150406115](https://openairdocs.org/sdr/IXXA20150406115), Dec 23, 2014: ATTACH FITTING. CRACKED. AOG FOR HVY MX, FAILSAFE INSPECTION. STATION 1043 CTR FLOORBEAM ATTACH FITTING CRACKED. R & R FLOORBEAM ATTACH FITTING IAW SRM 51-40-02.
- [SDR IXXA20150406112](https://openairdocs.org/sdr/IXXA20150406112), Dec 23, 2014: SKIN. GOUGED. AOG FOR HVY MX, FAILSAFE INSPECTION. FUSELAGE SKIN GOUGED IN TWO PLACES AT AFT END OF UPPER HORSE COLLAR FS 1804 - 1815. REPAIRED DAMAGED FWD SKIN IAW ENGINEERI
- [SDR IXXA20150403106](https://openairdocs.org/sdr/IXXA20150403106), Dec 23, 2014: FITTING. CORRODED. AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. RT 1809.5 OUTER CHORD LOWER TENSION FITTING, TENSION BOLT HOLE ELONGATED. REPLACED RT LOWER FWD STATION 1809.
- [SDR IXXA20150403105](https://openairdocs.org/sdr/IXXA20150403105), Dec 23, 2014: STRUCTURE. CORRODED. AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. RT 1809.5 FWD OUTER CHORD SKIN HAS HFEC OPEN HOLE DEFECT INDICATION AT FWD LOWER HOLE, COMMON TO CHORD, SPLIC
- [SDR IXXA20150403104](https://openairdocs.org/sdr/IXXA20150403104), Dec 23, 2014: FITTING. CORRODED. AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. RT 1809.5 FWD OUTER CHORD UPPER TENSION FITTING HAS DAMAGED HOLE, COMMON TO SPLICE FITTING & SKIN. RT UPPER F
- [SDR IXXA20150403103](https://openairdocs.org/sdr/IXXA20150403103), Dec 23, 2014: FITTING. CORRODED. AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. RT 1809.5 FWD OUTER CHORD SPLICE FITTING LOWER TENSION BOLT HOLE HAS HFEC OPEN HOLE DEFECT INDICATION. R & R 
- [SDR IXXA20150330070](https://openairdocs.org/sdr/IXXA20150330070), Dec 23, 2014: SPLICE PLATE. CORRODED. AIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. WING LE FRONT SPAR UPPER SPAR CAP CORRODED AT LES 472. R & R SECTION OF UPPER SPAR CAP, UPPER SPLICE PLATE, F
- [SDR IXXA201503220053](https://openairdocs.org/sdr/IXXA201503220053), Dec 19, 2014: PLATE. CORRODED. AIRCRAFT GNDED FOR HEAVY MX. STRUCTURE BEHIND LT PICKLE FORK SHOWS SIGNS OF CORROSION. R & R CORRODED BEARING PLATE IAW SRM 51-40-02 & EO 47008ORD11.
- [SDR IXXA20150406107](https://openairdocs.org/sdr/IXXA20150406107), Dec 17, 2014: FRAME. CORRODED. AOG FOR HVY MX, FAILSAFE INSPECTION. FLC FUSELAGE STATION 368, RBL 23 UNDERSIDE OF UPPER CHORD IS CORRODED AT NUTPLATE LOCATION. R & R UPPER CHORD IAW BDWG 143T

All 131: https://openairdocs.org/deregistered/N763CX-2024-08-05/reports.md

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