# Service difficulty reports: N395CM A list on [N395CM](https://openairdocs.org/aircraft/N395CM.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR IXXA202603192023](https://openairdocs.org/sdr/IXXA202603192023.md): Circuit Breaker · burned · Mar 12, 2026 · N395CM · Boeing 767323 · Electrical Power System Wiring > AFTER PUSHBACK AND CONFIGURED FOR DE-ICING A STRONG ELECTRICAL / PLASTIC BURNING SMELL WAS NOTICED. CREW ELECTED TO RETURN TO BLOCKS. AIRCRAFT IS GROUNDED FOR INSPECTION AND MAINTENANCE. SUPPLEMENTAL TO FIRST REPORT IXXA20260312023 DATED 12 MARCH 2026 IN KILN. - [SDR IXXA202603132023](https://openairdocs.org/sdr/IXXA202603132023.md): Unknown · odor · Mar 12, 2026 · N395CM · Boeing 767323 · Air Distribution System > AFTER PUSHBACK AND CONFIGURED FOR DE-ICING A STRONG ELECTRICAL PLASTIC BURNING SMELL WAS NOTICED. CREW ELECTED TO RETURN TO BLOCKS. AIRCRAFT IS GROUNDED FOR INSPECTION AND MAINTENANCE. OPEN - [SDR IXXA20251124078](https://openairdocs.org/sdr/IXXA20251124078.md): Cooling Fan · odor · Nov 21, 2025 · N395CM · Boeing 767323 · Air Distribution Fan > AFTER ENGINE START, CREW REPORTED ELECTRICAL BURNING SMELL WITH FAN EICAS MESSAGE DISPLAYED. BLOCK RETURN FOR INSPECTIONS AND MAINTENANCE. FOLLOWING FWD LOWER CARGO OFF LOAD, LINE MAINTENANCE ISOLATED FAULT TO FWD PRIMARY SUPPLY FAN. ADDITIONAL INSPECTIONS OF - [SDR IXXA20251013007](https://openairdocs.org/sdr/IXXA20251013007.md): Door Frame · cracked · Oct 13, 2025 · N395CM · Boeing 767323 · Fuselage Main, Structure > DAMAGE FOUND ON FORWARD LOWER CARGO DOOR CHORD - [SDR IXXA20251009002](https://openairdocs.org/sdr/IXXA20251009002.md): Floor Support · cracked · Oct 9, 2025 · N395CM · Boeing 767323 · Fuselage Miscellaneous Structure > FLOOR SUPPORT CRACKED AT STA 1480 RBL10. - [SDR IXXA20251009003](https://openairdocs.org/sdr/IXXA20251009003.md): Skin · corroded · Oct 9, 2025 · N395CM · Boeing 767323 · Fuselage Main, Plate/Skin > AFT CARGO COMPARTMENT AFT OF BULHEAD STA 1087-1109 STRINGER SKIN FOUND CORROSION - [SDR IXXA20251009001](https://openairdocs.org/sdr/IXXA20251009001.md): Web · damaged · Oct 9, 2025 · N395CM · Boeing 767323 · Fuselage Miscellaneous Structure > ALC WEBBING UPPER SURFACE HAS WEAR AND DAMAGE STA 1293, RBL10 - [SDR IXXA20251006002](https://openairdocs.org/sdr/IXXA20251006002.md): Floorbeam · cracked · Oct 6, 2025 · N395CM · Boeing 767323 · Fuselage Main, Floor Beam > BULK CARGO FLOOR SUPPORT BEAM CRACKED @ STA1480, RBL14 - [SDR IXXA20251006001](https://openairdocs.org/sdr/IXXA20251006001.md): Attach Bracket · broken · Oct 6, 2025 · N395CM · Boeing 767323 · Fuselage Main, Attach Fittings > SMALL FLOOR SUPPORT ATTACH BRACKET IS BROKEN ON AFT OF CABIN FLOOR BEAM STA 1562,. LBL82 - [SDR IXXA20251005007](https://openairdocs.org/sdr/IXXA20251005007.md): Stringer · corroded · Oct 5, 2025 · N395CM · Boeing 767323 · Fuselage Main, Longeron/Stringer > FUSELAGE STRINGER 37L CORROSION STA 742 - [SDR IXXA20251005006](https://openairdocs.org/sdr/IXXA20251005006.md): Skin · dented · Oct 5, 2025 · N395CM · Boeing 767323 · Fuselage Main, Plate/Skin > DENT IN FUSELAGE SKIN BETWEEN 1562 AND 1582,STR 15L - 16L. - [SDR IXXA20251005005](https://openairdocs.org/sdr/IXXA20251005005.md): Skin · dented · Oct 5, 2025 · N395CM · Boeing 767323 · Fuselage Main, Plate/Skin > RIGHT FUSELAGE SKIN DENTED AT STA 1582-1605 STR 16R. - [SDR IXXA20251005004](https://openairdocs.org/sdr/IXXA20251005004.md): Web · corroded · Oct 5, 2025 · N395CM · Boeing 767323 · Fuselage Miscellaneous Structure > STA 522 RBL5 CORROSION AROUND GROUND STUD AND WEB. - [SDR IXXA20251005003](https://openairdocs.org/sdr/IXXA20251005003.md): Stiffener · bent · Oct 5, 2025 · N395CM · Boeing 767323 · Fuselage Main, Bulkhead > ALC FLOORBEAM WEB BULKHEAD VERTICAL STIFFNER STA 1461 RBL 9, RBL 15 IS BENT. - [SDR IXXA20251005002](https://openairdocs.org/sdr/IXXA20251005002.md): Bulkhead Web · bent · Oct 5, 2025 · N395CM · Boeing 767323 · Fuselage Main, Bulkhead > ALC FLOORBEAM WEB BULKHEAD VERICAL STIFFNER STA 1439 RBL15 AND RBL9 IS BENT - [SDR IXXA20251005001](https://openairdocs.org/sdr/IXXA20251005001.md): Shear Tie · corroded · Oct 5, 2025 · N395CM · Boeing 767323 · Fuselage Internal Mounting Structure > FLC SHEAR TIE AT BS 742 STR 37L-38L CORRODED - [SDR IXXA20251002002](https://openairdocs.org/sdr/IXXA20251002002.md): Bracket · broken · Oct 2, 2025 · N395CM · Boeing 767323 · Fuselage Miscellaneous Structure > REMOVED AND REPLACED BRACKET P/N 368-53-16-94490-206 IAW B767-300 SRM 51-40-05 AND 51-40-02 PAR 7. AFT SIDE OF FLOOR BEAM STA1562 RBL 82 - [SDR IXXA20251002001](https://openairdocs.org/sdr/IXXA20251002001.md): Tube · dented · Oct 2, 2025 · N395CM · Boeing 767323 · Aircraft Fuel Distribution System > FUEL TUBE DENTED INSIDE THE LEFT FUEL TANK BEEN RIBS 20 AND 21, ACCESS PNL 541LB - [SDR IXXA20250907001](https://openairdocs.org/sdr/IXXA20250907001.md): Shear Tie · corroded · Sep 7, 2025 · N395CM · Boeing 767323 · Fuselage Internal Mounting Structure > CORROSION WAS FOUND DURING C-CHECK MAINTENANCE VISIT ON SHEAR TIE THAT WAS BLENDED WITH REMAINING MATERIAL THICKNESS OF.028" IN.. DAMAGE WAS DETERMINED TO BE OUT OF MANUFACTURE LIMITS IAW B767 SRM 53-00-07. SHEAR TIE WAS REPLACED DURING THE MAINTENANCE VISIT. - [SDR IXXA20240408021](https://openairdocs.org/sdr/IXXA20240408021.md): Window · detached · Apr 4, 2024 · N395CM · Boeing 767323 · Escape Slide > POST FLIGHT CREW REPORTED AN APPEARANCE OF LONGITUDINAL CRACK IN LEFT SLIDING WINDOW CARRIAGE. LINE MAINTENANCE REMOVED CARRIAGE AND VERIFIED FAULT IS ISOLATED TO CARRIAGE ONLY. AIRCRAFT GROUNDED FOR CORRECTIVE ACTION. LEFT CARRIAGE TRACK BRACKET REMOVED AND - [SDR IXXA2023081001](https://openairdocs.org/sdr/IXXA2023081001.md): Duct · cracked · Aug 10, 2023 · N395CM · Boeing 767323 · Air Intake Anti/De-Ice System > #2 PYLON ACCESS 441AT AFT T.A.I. DUCT SUPPORT COLLAR CRACKED AT BULKHEAD PASS THRU. - [SDR IXXA2023080801](https://openairdocs.org/sdr/IXXA2023080801.md): Fairing · cracked · Aug 8, 2023 · N395CM · Boeing 767323 · Nacelle/Pylon Miscellaneous Structure > PER DMI 27063 PER EO 54-767-8055 PERM REPAIR DUE WITHIN 300 FLIGHT HOURS. #1 PYLON PANEL UNDERWING FAIRING SKIN. - [SDR IXXA2023080103](https://openairdocs.org/sdr/IXXA2023080103.md): Acoustic Panel · delaminated · Aug 1, 2023 · N395CM · Boeing 767300 · Nacelle/Pylon Structure > #2 PYLON O/B STRUT FAIRING SKIN ( ARROWHEAD PANEL) DELAMINATED - [SDR IXXA2023080102](https://openairdocs.org/sdr/IXXA2023080102.md): Skin Panel · bulged · Aug 1, 2023 · N395CM · Boeing 767300 · Nacelle/Pylon, Plate/Skin > #1 PYLON I/B STRUT FAIRING SKIN/ ARROWHEAD PANEL BULGED - [SDR IXXA2023080101](https://openairdocs.org/sdr/IXXA2023080101.md): Acoustic Panel · delaminated · Aug 1, 2023 · N395CM · Boeing 767300 · Nacelle/Pylon, Main Frame > #1 PYLON PANEL 436CR SEPARATED BETWEEN THE METAL BACKING AND OUTER SKIN - [SDR IXXA2023080404](https://openairdocs.org/sdr/IXXA2023080404.md): Skin · cracked · Jun 4, 2022 · N395CM · Boeing 767323 · Fuselage Main, Plate/Skin > FWD ENTRY DOOR CUTOUT AFT LWR CORNER FASTENER HOLE IS CRACKED ALONG THE SKIN SIDE AT LFS 337 BETWEEN S-19L AND LWR MAIN SILL CHORD - [SDR IXXA2023080402](https://openairdocs.org/sdr/IXXA2023080402.md): Skin · cracked · Jun 4, 2022 · N395CM · Boeing 767323 · Fuselage Main, Plate/Skin > FWD SERVICE DOOR SKIN CUTOUT AFT LOWER CORNER IS CRACKED. - [SDR IXXA2023080401](https://openairdocs.org/sdr/IXXA2023080401.md): Panel · delaminated · Jun 4, 2022 · N395CM · Boeing 767323 · Nacelle/Pylon Miscellaneous Structure > #1 PYLON OUTBOARD ARROW HEAD PANEL DELAMINATED 4.5 INCHES.. - [SDR IXXA202108040047](https://openairdocs.org/sdr/IXXA202108040047.md): Web · cracked · Jul 15, 2021 · N395CM · Boeing 767323 · Fuselage Miscellaneous Structure > IN COMPLIANCE OF TASK CARD 53-767-07531 " INSPECTION/DETAILED VISUAL INSPECTION OF LFEC AND HFEC FUSELAGE SECTION 41 B.S 246 FLOOR BEAM" THE FOLLOWING FINDINGS WERE NOTED: CRACK AT WEB STA 246.LBLB 9 ALONG STIFFENER. - [SDR IXXA2021080400047](https://openairdocs.org/sdr/IXXA2021080400047.md): Fitting · corroded · Jul 3, 2021 · N395CM · Boeing 767323 · Fuselage Main, Structure > IN COMPLIANCE OF TASK CARD 51-041-02 " RESTORATION OF CANTED PRESSURE CAVITY CLEANING" THE FOLLOWING FINDINGS WERE NOTED: LEFT REAR SPAR FITTING STATION 955.6 INCHES FROM FITTING INBOARD ON UPPER CENTER WING SKIN CORROSION FOUND. WORK IN PROGRESS - [SDR IXXA20210804044](https://openairdocs.org/sdr/IXXA20210804044.md): Skin · cracked · Jun 8, 2021 · N395CM · Boeing 767323 · Fuselage Main, Plate/Skin > IN COMPLIANCE OF TASK CARD 53-73-00-02 "GENERAL VISUAL INSPECTION OF EXTERNAL EXTERIOR SECTION 48 RIGHT SIDE" THE FOLLOWING FINDINGS WERE NOTED: AFT RIGHT FUSELAGE SKIN SECTION 48 STATION 1654.5 ABOVE STRINGER 8R IS CRACKED. WORK IN PROGRESS - [SDR IXXA20200323008](https://openairdocs.org/sdr/IXXA20200323008.md): Battery · discharged · Mar 21, 2020 · N395CM · Boeing 767323 · Emergency Equipment > SERVICE CHECK FINDING: EMERGENCY FLASHLIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY IAW B767 AMM 25-05-03. OPS CHECK GOOD AT THIS TIME - [SDR IXXA20191031020](https://openairdocs.org/sdr/IXXA20191031020.md): Access Panel · corroded · Sep 11, 2019 · N395CM · Boeing 767323 · Cargo/Baggage Doors > AIRCRAFT GROUNDED FOR SCHEDULED MAINTENANCE. IN ACCOMPLISHMENT OF TASK CARD 53-002-02-IAI, THE FOLLOWING DISCREPANCY WAS NOTED: PAINT BUBBLED UP AND CORROSION ON MAIN CARGO DOOR EXTERNAL ACCESS PANELS 838I, 838H,838G, 838F, AND 838E. PANELS 838I AND 838H FOUND - [SDR MK1Y20170828001](https://openairdocs.org/sdr/MK1Y20170828001.md): Slat System · malfunctioned · Aug 18, 2017 · N395CM · Boeing 767323 · Leading Edge Slat Control System > DURING TEST FLIGHT AFTER BDSF CONVERSION, AT CRUISE ALTITUDE 38,000 FEET, 0.80 MACH A "LE SLAT ASYM" MESSAGE CAME ON WITH FLAP INDICATOR NEEDLE FLUCTUATING BETWEEN 0 TO 1 (WITH LEADING EDGE LIGHT ON).THE MESSAGE CAME ON AND OFF DURING THE DECELERATION AND DECE - [SDR MK1Y20170828004](https://openairdocs.org/sdr/MK1Y20170828004.md): Skin · corroded · Aug 17, 2017 · N395CM · Boeing 767323 · Wing, Plate/Skin > CORROSION FOUND ON THE RT WING UPPER INNER SPAR SKIN PANEL NR 1 OVERWING FUEL FILL PORT ADAPTER AT WS 785.2, STRINGERS 15 TO 16. - [SDR MK1Y20170828003](https://openairdocs.org/sdr/MK1Y20170828003.md): Skin · corroded · Aug 17, 2017 · N395CM · Boeing 767323 · Wing, Plate/Skin > CORROSION DAMAGE FOUND ON THE LEFT WING UPPER INNER SPAR SKIN PANEL NR 1 OVERWING FUEL FILL PORT ADAPTER AT WS 785.2, STRINGER 15 TO 16. ## 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 = 'N395CM' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N395CM/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.