# N203CM: 1991 Boeing 767-375, registration cancelled 2024-10-31 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 31, 2024 - Exported to: Poland - Status when cancelled: Valid registration - Airframe: [Boeing 767-375](https://openairdocs.org/model/boeing-767-375) (registry code 1385217) - Engine: [GE CF6-80C2B6F](https://openairdocs.org/engine/ge-cf6-80c2b6f) (registry code 30109) - Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM), [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (OpenAirDocs) - Serial number: 25121 - Year built: 1991 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 4, 2022 - Certificate issued: June 1, 2021 - Last registry action: June 26, 2024 - Mode S code: A19D66 - 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/N203CM - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=203CM - Page: https://openairdocs.org/deregistered/N203CM-2024-10-31 From the FAA registry file of November 3, 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 767-375: https://openairdocs.org/model/boeing-767-375.md ## Service difficulty reports (19) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 2024FA0000569](https://openairdocs.org/sdr/2024FA0000569), Aug 6, 2024: SKIN. DENTED. REWPAIR - SECTION 41 - DENT - RH FUSELAGE SKIN BETWEEN STA 303 AND 325 AND BETWEEN STR 35R-36R. - [SDR MK1Y202207060018](https://openairdocs.org/sdr/MK1Y202207060018), Jul 6, 2022: HOUSING. CORRODED. L/H WING - MAIN FUEL TANK FUEL BOOST PUMP HOUSING REPAIRS - DURING MAINTENANCE INSPECTION AT IAI' CORROSIN WAS FOUND ON THE INNER FACE OF THE FUEL BOOST PUMP HO - [SDR MK1Y20220706017](https://openairdocs.org/sdr/MK1Y20220706017), Jul 6, 2022: REPAIR. DISCOVERED. ENG@ 2 - STRUT FAIRING - OUTBRD SIDE - NAC STA 304.5 - NAC STA 307.9 - - DURRING MAINTENANCE AT IAI - EXISTING UNDOCUMENTED REPAIR WAS FOUND ON STRUT OF ENGINE - [SDR MK1Y20220706016](https://openairdocs.org/sdr/MK1Y20220706016), Jul 6, 2022: HOUSING. CORRODED. L/H WING - MAIN FUEL TANK FUEL BOOST PUMP HOSING REPAIRS - DURING MAINTENANCE INSPECTION AT IAI, CORROSION WAS FOUND ON THE INNER FACE OF THE FUEL BOOST PUMP HO - [SDR MK1Y20220706015](https://openairdocs.org/sdr/MK1Y20220706015), Jul 6, 2022: SKIN PANEL. CRACKED. PROBLEM DESCRIPTION: PYLON #1, STRUT SIDE SKIN PANEL, PANEL 432AL, NAC 233,WL 143: FOUND EXTENDED CRACK BEYOND RIVET AT OUTER SKIN OF THE PYLON BY 1.8” IN LENGT - [SDR MK1Y20220706014](https://openairdocs.org/sdr/MK1Y20220706014), Jul 6, 2022: SKIN PANEL. CRACKED. PYLON # 2, OUTER SKIN PANEL 432AL, NAC 233, WL 143: FOUND EXTENDED CRACK BEYOND RIVET AT OUTER SKIN OF THE PYLON BY 2.5” IN LENGTH FROM THE CUTOUT OF PANEL 432A - [SDR MK1Y20220706013](https://openairdocs.org/sdr/MK1Y20220706013), Jul 6, 2022: SKIN. OUT OF LIMITS. EXTERNAL FUSELAGE SKIN, STA 226 – STA 347, STR-28L – STR-29L: NRC M0143-EXTERNAL FUSELAGE SKIN BS 226.5 AND 2.2” BELOW STR 29L: SKIN THICKNESS: 0.080”. REMOVED - [SDR MK1Y20220706012](https://openairdocs.org/sdr/MK1Y20220706012), Jul 6, 2022: REPAIR. DISCOVERED. R/H HORIZONTAL STABILIZER – UPPER SKIN: DURING MAINTENANCE PRACTICES AT IAI IN TLV, AN EXISTING UNDOCUMENTED REPAIR WAS FOUND ON R/H HORIZONTAL STABILIZER UPPER - [SDR MK1Y20220706011](https://openairdocs.org/sdr/MK1Y20220706011), Jul 6, 2022: REPAIR. DISCOVERED. R/H MLG SHOCK STRUT DOOR:DURING MAINTENANCE INSPECTION AT IAI, EXISTING UNDOCUMENTED REPAIR WAS FOUND ON R/H MLG SHOCK STRUT DOOR - [SDR MK1Y20220706010](https://openairdocs.org/sdr/MK1Y20220706010), Jul 6, 2022: REPAIR. DISCOVERED. STRUT # 2, INBD SIDE, SKIN 313T3310: DURING MAINTENANCE PRACTICES AT IAI IN TLV, AN EXISTING UNDOCUMENTED DOUBLER REPAIR WAS FOUND ON STRUT # 2 INBD SIDE, ON SK - [SDR MK1Y20220706009](https://openairdocs.org/sdr/MK1Y20220706009), Jul 6, 2022: SKIN. DAMAGED. DURING MAINTENANCE INSPECTION LIGHTNING STRIKES WERE DISCOVERED ON THE EXTERNAL FUSELAGE SKIN BETWEEN STA 212 AND STA 303, STR-29L – STR-30L. THE LIGHTNING STRI - [SDR MK1Y20220706008](https://openairdocs.org/sdr/MK1Y20220706008), Jul 6, 2022: SKIN PANEL. CORRODED. CENTER WING SECTION, UPPER CHORD AREA, STA 955, RBL 11.00: DURING CONVERSION WORK AT IAI, A CORROSION WAS FOUND AT DATUM LOCATION ON SKIN PANEL NO.1 OF CENTER W - [SDR MK1Y20220706007](https://openairdocs.org/sdr/MK1Y20220706007), Jul 6, 2022: REPAIR. DISCOVERED. : ENGINE #1, STRUT FAIRING, INBD SIDE, NAC STA 304.1 – NAC STA 311.1: DURING MAINTENANCE INSPECTION AT IAI, THE EXISTING UNDOCUMENTED REPAIR WAS FOUND ON THE ST - [SDR MK1Y20220706006](https://openairdocs.org/sdr/MK1Y20220706006), Jul 6, 2022: SKIN. DAMAGED. DURING MAINTENANCE INSPECTION LIGHTNING STRIKES WERE DISCOVERED ON THE EXTERNAL FUSELAGE SKIN BETWEEN STA 368 AND STA 412, STR-28L – STR-30L. THE LIGHTNING STRI - [SDR MK1Y20220706005](https://openairdocs.org/sdr/MK1Y20220706005), Jul 6, 2022: SKIN. SCRATCHED. : EXTERNAL FUSELAGE SKIN, STA 1487, STR-22L – STR-23L: DURING MAINTENANCE INSPECTION AT IAI, SCRATCHES WERE FOUND AT DATUM LOCATION. THE DAMAGE WAS BLENDED OUT - [SDR MK1Y20220706004](https://openairdocs.org/sdr/MK1Y20220706004), Jul 6, 2022: REPAIR. DISCOVERED. ENGINE #2, STRUT ACCESS PANEL 446BR, NAC STA 249 – NAC STA 253: DURING MAINTENANCE INSPECTION AT IAI, EXISTING UNDOCUMENTED REPAIR WAS FOUND ON ENGINE #2, STRUT - [SDR MK1Y20220706003](https://openairdocs.org/sdr/MK1Y20220706003), Jul 6, 2022: STUB FRAME. CRACKED. THE CRACK FOUND IN THE TRANSITION RADIUS OF THE RIGHT FUSELAGE FRAME STUB BEAM LOCATED STA 883.5 AND RBL 89. THE CRACK WAS FOUND DURING A REPETITIVE HFEC SURFAC - [SDR MK1Y20220706002](https://openairdocs.org/sdr/MK1Y20220706002), Jul 6, 2022: STUB FRAME. CRACKED. THE CRACK FOUND IN THE TRANSITION RADIUS OF THE LEFT FUSELAGE FRAME STUB BEAM LOCATED STA 859.5 AND LBL 89. THE CRACK WAS FOUND DURING A REPETITIVE HFEC SURFACE - [SDR MK1Y20220706001](https://openairdocs.org/sdr/MK1Y20220706001), Jul 6, 2022: SKIN PANEL. CORRODED. CENTER WING, UPPER SKIN, PANEL NO. 1, STA 955, LBL 74.00: DURING MAINTENANCE INSPECTION AT IAI, CORROSION WAS FOUND AT DATUM LOCATION. THE DAMAGE WAS BLENDED OU ## Other aircraft with N203CM - [Cancelled 2014-12-22](https://openairdocs.org/deregistered/N203CM-2014-12-22): Douglas DC-6, S/N 44627. Registration expired, pending cancellation. Owner: [Circle M Aviation Ltd](https://openairdocs.org/faa-owner/CIRCLE%20M%20AVIATION%20LTD), [Hockessin, DE](https://openairdocs.org/faa-place/DE/Hockessin) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.