# Service difficulty reports: N203CM, cancelled Oct 31, 2024 A list on [N203CM, cancelled Oct 31, 2024](https://openairdocs.org/deregistered/N203CM-2024-10-31.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 2024FA0000569](https://openairdocs.org/sdr/2024FA0000569.md): Skin · dented · Aug 6, 2024 · N203CM · Boeing 767375 · Fuselage Main, Plate/Skin > REWPAIR - SECTION 41 - DENT - RH FUSELAGE SKIN BETWEEN STA 303 AND 325 AND BETWEEN STR 35R-36R. - [SDR MK1Y202207060018](https://openairdocs.org/sdr/MK1Y202207060018.md): Housing · corroded · Jul 6, 2022 · N203CM · Boeing 767323 · Fuel Boost Pump > 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 HOUSING ATTER REMOVING THE FWD FUEL BOOST PUMP SHUTOFF SLEEVE - [SDR MK1Y20220706017](https://openairdocs.org/sdr/MK1Y20220706017.md): Repair · discovered · Jul 6, 2022 · N203CM · Boeing 767323 · Nacelle/Pylon Structure > 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 #2, OUTBRD SIDE FAIRUNG SKIN. - [SDR MK1Y20220706016](https://openairdocs.org/sdr/MK1Y20220706016.md): Housing · corroded · Jul 6, 2022 · N203CM · Boeing 767323 · Fuel Boost Pump > 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 HOUSING AFTER REMOVING THE AFT FUEL BOOST PUMP SHUTOFF SLEEVE. - [SDR MK1Y20220706015](https://openairdocs.org/sdr/MK1Y20220706015.md): Skin Panel · cracked · Jul 6, 2022 · N203CM · Boeing 767323 · Nacelle/Pylon, Plate/Skin > 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 LENGTH FROM THE CUTOUT OF PANEL 432AL. - [SDR MK1Y20220706014](https://openairdocs.org/sdr/MK1Y20220706014.md): Skin Panel · cracked · Jul 6, 2022 · N203CM · Boeing 767323 · Nacelle/Pylon, Plate/Skin > 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 432AL. - [SDR MK1Y20220706013](https://openairdocs.org/sdr/MK1Y20220706013.md): Skin · out of limits · Jul 6, 2022 · N203CM · Boeing 767323 · Fuselage Main, Plate/Skin > 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 FASTENER: JO-BOLT 0.185” DIA.OS-1 EXISTING REPAIR WASHER: DIAMETR: 0.580”, THICKNESS: 0.065”. NRC M - [SDR MK1Y20220706012](https://openairdocs.org/sdr/MK1Y20220706012.md): Repair · discovered · Jul 6, 2022 · N203CM · Boeing 767323 · Empennage Structure > 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 SKIN. THE SKIN IS MADE FROM ALCLAD 7075-T6 1.100” IN THICK. THE REPAIR FOUND CONSISTS IN ONE DOUBLE - [SDR MK1Y20220706011](https://openairdocs.org/sdr/MK1Y20220706011.md): Repair · discovered · Jul 6, 2022 · N203CM · Boeing 767323 · Doors > 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.md): Repair · discovered · Jul 6, 2022 · N203CM · Boeing 767323 · Nacelle/Pylon Structure > 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 SKIN 313T3310. THE SKIN IS MADE FROM TWO BONDED SKINS OF ALCLAD 2024-T3 0.063” AND 0.040” IN THICKNESS - [SDR MK1Y20220706009](https://openairdocs.org/sdr/MK1Y20220706009.md): Skin · damaged · Jul 6, 2022 · N203CM · Boeing 767323 · Fuselage Main, Plate/Skin > DURING MAINTENANCE INSPECTION LIGHTNING STRIKES WERE DISCOVERED ON THE EXTERNAL FUSELAGE SKIN BETWEEN STA 212 AND STA 303, STR-29L – STR-30L. THE LIGHTNING STRIKES WERE BLENDED OUT. THE BLEND OUT AREA IS LOCATED COMMON TO THE EXISTING FASTENERS. AFTER INSPECTI - [SDR MK1Y20220706008](https://openairdocs.org/sdr/MK1Y20220706008.md): Skin Panel · corroded · Jul 6, 2022 · N203CM · Boeing 767323 · Fuselage Structure (General) > 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 WING, PRESSURE DECK WEB, AND UPPER CHORD OF REAR SPAR OF CENTER WING. THE SKIN AND WEB WERE BLENDED A - [SDR MK1Y20220706007](https://openairdocs.org/sdr/MK1Y20220706007.md): Repair · discovered · Jul 6, 2022 · N203CM · Boeing 767323 · Nacelle/Pylon Structure > : 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 STRUT FAIRING AT DATUM LOCATION. - [SDR MK1Y20220706006](https://openairdocs.org/sdr/MK1Y20220706006.md): Skin · damaged · Jul 6, 2022 · N203CM · Boeing 767323 · Fuselage Structure (General) > DURING MAINTENANCE INSPECTION LIGHTNING STRIKES WERE DISCOVERED ON THE EXTERNAL FUSELAGE SKIN BETWEEN STA 368 AND STA 412, STR-28L – STR-30L. THE LIGHTNING STRIKES WERE BLENDED OUT. THE BLEND OUT ARE LOCATED COMMON TO THE EXISTING FASTENERS. AFT - [SDR MK1Y20220706005](https://openairdocs.org/sdr/MK1Y20220706005.md): Skin · scratched · Jul 6, 2022 · N203CM · Boeing 767323 · Fuselage Main, Plate/Skin > : 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 AND FOUND WITHIN LIMITS, HOWEVER, THE BLEND OUT IS AMONG THE FASTENERS THAT PROHIBITED PER SRM 53-0 - [SDR MK1Y20220706004](https://openairdocs.org/sdr/MK1Y20220706004.md): Repair · discovered · Jul 6, 2022 · N203CM · Boeing 767323 · Nacelle/Pylon Structure > 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, ACCESS PANEL NO. 446BR. - [SDR MK1Y20220706003](https://openairdocs.org/sdr/MK1Y20220706003.md): Stub Frame · cracked · Jul 6, 2022 · N203CM · Boeing 767323 · Fuselage Main, Frame > 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 SURFACE INSPECTION IAW BOEING SERVICE BULLETIN 767-53A0209, AS MANDATED BY AIRWORTHINESS DIRECTIVE 2012-22 - [SDR MK1Y20220706002](https://openairdocs.org/sdr/MK1Y20220706002.md): Stub Frame · cracked · Jul 6, 2022 · N203CM · Boeing 767323 · Fuselage Main, Frame > 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 INSPECTION IAW BOEING SERVICE BULLETIN 767-53A0209, AS MANDATED BY AIRWORTHINESS DIRECTIVE 2012-22- - [SDR MK1Y20220706001](https://openairdocs.org/sdr/MK1Y20220706001.md): Skin Panel · corroded · Jul 6, 2022 · N203CM · Boeing 767323 · Wing, Plate/Skin > 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 OUT AND FOUND WITHIN LIMITS, HOWEVER, THE BLEND OUT IS AMONG THE FASTENERS THAT PROHIBITED PER SRM 53- ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N203CM' AND deregistration_id = 'N203CM-2024-10-31' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N203CM-2024-10-31/reports --- 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.