N395CM
Service difficulty reports · 36
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "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"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR IXXA202603192023Circuit Breaker · burnedAFTER 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 IXXA202603132023Unknown · odorAFTER 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. OPENSDR IXXA20251124078Cooling Fan · odorAFTER 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 IXXA20251013007Door Frame · crackedDAMAGE FOUND ON FORWARD LOWER CARGO DOOR CHORDSDR IXXA20251009002Floor Support · crackedFLOOR SUPPORT CRACKED AT STA 1480 RBL10.SDR IXXA20251009003Skin · corrodedAFT CARGO COMPARTMENT AFT OF BULHEAD STA 1087-1109 STRINGER SKIN FOUND CORROSIONSDR IXXA20251009001Web · damagedALC WEBBING UPPER SURFACE HAS WEAR AND DAMAGE STA 1293, RBL10SDR IXXA20251006002Floorbeam · crackedBULK CARGO FLOOR SUPPORT BEAM CRACKED @ STA1480, RBL14SDR IXXA20251006001Attach Bracket · brokenSMALL FLOOR SUPPORT ATTACH BRACKET IS BROKEN ON AFT OF CABIN FLOOR BEAM STA 1562,. LBL82SDR IXXA20251005007Stringer · corrodedFUSELAGE STRINGER 37L CORROSION STA 742SDR IXXA20251005006Skin · dentedDENT IN FUSELAGE SKIN BETWEEN 1562 AND 1582,STR 15L - 16L.SDR IXXA20251005005Skin · dentedRIGHT FUSELAGE SKIN DENTED AT STA 1582-1605 STR 16R.SDR IXXA20251005004Web · corrodedSTA 522 RBL5 CORROSION AROUND GROUND STUD AND WEB.SDR IXXA20251005003Stiffener · bentALC FLOORBEAM WEB BULKHEAD VERTICAL STIFFNER STA 1461 RBL 9, RBL 15 IS BENT.SDR IXXA20251005002Bulkhead Web · bentALC FLOORBEAM WEB BULKHEAD VERICAL STIFFNER STA 1439 RBL15 AND RBL9 IS BENTSDR IXXA20251005001Shear Tie · corrodedFLC SHEAR TIE AT BS 742 STR 37L-38L CORRODEDSDR IXXA20251002002Bracket · brokenREMOVED 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 82SDR IXXA20251002001Tube · dentedFUEL TUBE DENTED INSIDE THE LEFT FUEL TANK BEEN RIBS 20 AND 21, ACCESS PNL 541LBSDR IXXA20250907001Shear Tie · corrodedCORROSION 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 IXXA20240408021Window · detachedPOST 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 IXXA2023081001Duct · cracked#2 PYLON ACCESS 441AT AFT T.A.I. DUCT SUPPORT COLLAR CRACKED AT BULKHEAD PASS THRU.SDR IXXA2023080801Fairing · crackedPER DMI 27063 PER EO 54-767-8055 PERM REPAIR DUE WITHIN 300 FLIGHT HOURS . #1 PYLON PANEL UNDERWING FAIRING SKIN.SDR IXXA2023080103Acoustic Panel · delaminated#2 PYLON O/B STRUT FAIRING SKIN ( ARROWHEAD PANEL ) DELAMINATEDSDR IXXA2023080102Skin Panel · bulged#1 PYLON I/B STRUT FAIRING SKIN/ ARROWHEAD PANEL BULGEDSDR IXXA2023080101Acoustic Panel · delaminated#1 PYLON PANEL 436CR SEPARATED BETWEEN THE METAL BACKING AND OUTER SKINSDR IXXA2023080404Skin · crackedFWD ENTRY DOOR CUTOUT AFT LWR CORNER FASTENER HOLE IS CRACKED ALONG THE SKIN SIDE AT LFS 337 BETWEEN S-19L AND LWR MAIN SILL CHORDSDR IXXA2023080402Skin · crackedFWD SERVICE DOOR SKIN CUTOUT AFT LOWER CORNER IS CRACKED.SDR IXXA2023080401Panel · delaminated#1 PYLON OUTBOARD ARROW HEAD PANEL DELAMINATED 4.5 INCHES..SDR IXXA202108040047Web · crackedIN 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 IXXA2021080400047Fitting · corrodedIN 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 PROGRESSSDR IXXA20210804044Skin · crackedIN 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 PROGRESSSDR IXXA20200323008Battery · dischargedSERVICE CHECK FINDING: EMERGENCY FLASHLIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY IAW B767 AMM 25-05-03. OPS CHECK GOOD AT THIS TIMESDR IXXA20191031020Access Panel · corrodedAIRCRAFT 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 FOUNDSDR MK1Y20170828001Slat System · malfunctionedDURING 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 DECESDR MK1Y20170828004Skin · corrodedCORROSION 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 MK1Y20170828003Skin · corrodedCORROSION 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.
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