N362CM
Service difficulty reports · 97
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 = 'N362CM' 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 = 'N362CM' 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 ABXA2021118110Shutoff Valve · stuckON TAKE OFF, TRAILING EDGE FLAP DISAGREE EICAS MSG WHILE MOVING FLAPS FROM 5 TO 1. FOLLOWED QRH PROCEDURE. FLAP WORKED FINE ELECTRICALLY. AIR TURNBACK. LANDED WITHOUT FURTHER INCIDENCE. AIRCRAFT GROUNDED BY MAINTENANCE. MAINTENANCE FOUND THE FLAP/SLAT SHUTOFF SDR ABXA2021831084Circuit Breaker · trippedAUTO SPEED BRAKE CAUTION AFTER ENGINE START. C/B POPPED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED OPERATIONAL TEST OF THE AUTO-SPEED BRAKE SYSTEM IAW AMM 27-62-00, OPS NORMAL, AIRCRAFT RELEASED FOR FLIGHT.SDR ABXA2021417026Sensor · out of toleranceRIGHT PACK TEMP EICAS MESSAGE ILLUMINATED, AICRAFT BACK TO GATE AND TAKEN OUT OF SERVICE BY MAINTENANCE. REPLACED TEMP SENSOR TS199 IAW AMM 21-58-08 POST INSTALLATION TEST NORMAL R PACK TEMP CONTROL OPS CHECK OK IAW AMM 21-51-00/501 A/C UPGRADED TO ETOPS 180 PSDR ABXA202149024Module · intermittentAILERON LOCK-OUT EICAS MSG AFTER LEAVING BLOCKS. BACK TO BLOCK AND AIRCRAFT WAS GROUNDED. MAINTENANCE REMOVED AND REPLACED RH SAM.AIRCRAFT IAW B767 AMM 27-11-02 WAS RETURNED BACK TO SERVICE.SDR ABXA2021218014Bleed Valve · rupturedRIGHT ENGINE BLEED VALVE WON’T OPEN, NO AIRFLOW, "RT ENG BLEED" LIGHT ILLUMINATED, AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. FOUND RIGHT ENGINE PRV STUCK IN THE CLOSED POSITION, FAILED THUMB TEST. SWAPPED RT PRV AND HPSOV IAW B767 AMM 36-11-18. TRSDR ABXA2021212010Hydraulic Line · leakingUPON A CAT 3 LANDING , AT LEIPZIG, LOSS OF CENTER HYDRAULIC QUANTITY. ABLE TO EXIT AT A4. SLUGGISH RESPONSE TO BRAKES AND NOSE WHEEL STEERING ELECTED NOT TO FURTHER TAXI, HELD SHORT OF TAXIWAY C. AIRCRAFT TOWED BACK TO GATE. MAINTENANCE FOUND TAIL SKID HYDRAULSDR ABXA2021129005Pressure Switch · intermittentRUDDER RATIO LIGHT AND EICAS MESSAGE AFTER ENGINE START. BTB AND GROUNDED. RIGHT YAW DAMPER MODULE FAULTED LEFT HYD SWITCH. REMOVED AND REPLACED S27 HYD PRESS SWITCH, IAW B767 AMM 27-11-17. OPERATIONS AND LEAK CHECK GOOD. RAN ENGINE, IAW B767-10A. NO DEFSDR ABXA202112821Switch · stickingRUDDER RATIO EICAS MESSAGE AND LIGHT. AIRCRAFT BTB. AND GROUNDED. FOUND PCA FAULT ON BOTH MODULES. DISCOVERED TAIL HYDRAULIC CUT OFF SWITCH KORRY SWITCH UNLATCHED. REPLACED KORRY LENS MODULE, IAW B767 SWPM 20-84-14. RUDDER RATIO RESET AND PASSES TEST, AS SDR ABXA20200803230Skin · dentedNR 1 SLAT DAMAGED BY BOARDING STAND ON TAXI OUT. DAMAGE WAS OBSERVED BY GROUND CREW. THEY CALLED MANAGEMENT AND MANAGEMENT NOTIFIED TOWER. TOWER NOTIFIED FLIGHT CREW AND THE CREW PERFORMED AIR TURN BACK INTO CVG. MAINTENANCE OBSERVED DAMAGE TO NR 1 SLAT ANSDR ABXA20200803209Skin · gougedDURING AIRCRAFT C-CHECK AT TAMPA, MAINTENANCE DISCOVERED A GOUGE ON THE UPPER OUTER SKIN (P/N 113T3140-5) OF THE RT WING OUTBOARD FLAP AT OTEF STA 83.72. THE GOUGE WAS REMOVED BY LOCALIZED BLENDING, PER 767-300 SRM 57-53-01, EXCEEDING PUBLISH LIMITS. ALL FASDR ABXA2020080173164Warning Message · false activationSPOILER EICAS MESSAGE APPEARED AND SPOILER DISCREET LIGHT ILLUMINATED AIRCRAFT WAS GROUNDED. PERFORMED FIM TASK 27-09 FT 809. RESET SPOILER MODULE 1 LEFT AND MESSAGE AND LIGHT CLEARED. SPOILERS OPS CHECK OKAY.SDR ABXA2020050429054Warning System · activatedRIGHT SIDE BRACE EICAS. GEAR HANDLE DOWN, NO RIGHT GREEN LIGHT AND GEAR DISCREET LIGHT. CONFIGURATION AND GEAR NOT DOWN EICAS MESSAGE. AIRCRAFT WAS GROUNDED.SDR ABXA20200302035Unknown · odorSTRONG SMELL OF ELECTRICAL ODOR (SMOKE LIKE IN NATURE). THAT LASTED APPROX. 2 MINUTES AT THE TIME THE AUTO-PILOT DISCONNECTED. THE AIRPLANE WAS GROUNDED. CAUSE OF ODOR IS UNKNOWN.SDR ABXA20190716125Unknown · odorDURING THE DESCENT INTO HRL, THE CREW SMELLED A STRONG ELECTRICAL ODOR WHICH LASTED ABOUT FIVE MINUTES. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE MAIN EQUIPMENT CENTER, MAIN CARGO COMPARTMENT, FLIGHT DECK, AND GALLEY WERE INSPECTED. NO ABNORMALISDR ABXA201812031133Skin · corrodedCORROSION ON THE RIGHT WING NUMBER 9 SLAT LEADING EDGE SKIN. THE SKIN WAS REPAIRED.
THE AIRPLANE WAS GROUNDED.SDR ABXA201812031131Stiffener · corrodedCORROSION ON THE WHEEL WELL BULKHEAD HORIZONTAL STIFFENER NUMBER 7 AT FUSELAGE STATION 1065. THE STIFFENER WAS REPAIRED.
THE AIRPLANE WAS GROUNDED.SDR ABXA201812031130Skin · corrodedCORROSION ON THE FUSELAGE SKIN AT STATION 1490 UNDER THE BULK CARGO EXTERIOR FLOODLIGHT HOUSING. THE SKIN WAS REPAIRED.
THE AIRPLANE WAS GROUNDED.SDR ABXA201812031129Skin · dentedDENT ON THE RIGHT WING NUMBER 8 SPOILER, LOWER SURFACE SKIN. THE SKIN WAS REPAIRED.
THE AIRPLANE WAS GROUNDED.SDR ABXA201812031128Skin · crackedCRACK AND CORROSION ON THE LEFT WING NUMBER 2 LEADING EDGE SLAT, OUTBOARD LOWER SKIN. THE SKIN WAS REPAIRED.
THE AIRPLANE WAS GROUNDED.SDR ABXA201812031127Skin · crackedR1 DOOR SILL, FUSELAGE SKIN AT LOWER AFT EXTERIOR CORNER HAS CRACK INDICATION. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA2018082016094Module · odorDURING TAXI TO THE RUNWAY, THE CREW SMELLED A SULFUR/WOOD SMOKE IN THE FLIGHT DECK. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE MAINTENANCE TECHNICIAN NOTICED AN ODOR IN THE GALLEY. THE OVEN/HOT CUP MODULE WAS REPLACED. THE CAUSE FOR THE ODOR WAS SDR ABXA20161018149Unknown · odorTHE FLIGHT CREW REPORTED A STRONG HOT METAL TYPE OF ODOR DURING TAKEOFF AND CRUISE. THE ODOR WOULD LAST A MINUTE OR TWO, THEN DISSIPATE. NO SMOKE WAS OBSERVED. THE AIRPLANE WAS REMOVED FROM SERVICE AND THE MAIN EQUIPMENT CENTER WAS INSPECTED. THERE WAS NO SDR ABXA20160924147Bulkhead Web · crackedCANTED PRESSURE WEB IS CRACKED AT STATION 995 IN MAIN CABIN UNDER FLOOR. REPAIRED MAIN CABIN FLOOR PRESSURE WEB AT STATION 995 IN ACCORDANCE WITH REO G20250 REV 8 AND ABX REA B653-62043MR. SDR INFO: CRACKED, 11", PART NUMBER: 145T8755-19, SERIAL NUMBER: NSNSDR ABXA20160818133Transformer · defective5 OUT OF 6 FORWARD LOWER CARGO DOOR SILL AREA LIGHTS DO NOT ILLUMINATE DURING CARGO LOADING OPERATIONS. AT THE FORWARD UPPER SILL LIGHT POSITION, SMOKE WAS FOUND AT A BURNED WIRE. THE FORWARD UPPER LIGHT ASSEMBLY WAS REMOVED AND FOUND 4 WIRES BURNED, 2 SHORTESDR ABXA20160626105Skin · damagedLOWER HORIZONTAL STAB HAS SKIN DAMAGE. AIRCRAFT WAS GROUNDED. REMOVED DAMAGE AND REPAIRED AREA IAW SRM 51-70-10 & REA-8655-62114-MR.SDR ABXA20160626104Skin · damagedLOWER HORIZONTAL SKIN DAMAGED. AIRCRAFT WAS GROUNDED. REPAIRED AREA IAW SRM 51-70-10 AND REA-8655-62114-MR.SDR ABXA20160626103Skin · damagedLOWER HORIZONTAL SKIN DAMAGED. AIRCRAFT WAS GROUNDED. REPAIRED THE AREA IAW SRM 51-70-10 & REA-8655-62114-MR. RESTORED FINISH IAW AMM 51-21-10.SDR ABXA20150608078Support · corrodedDISCREPANT HOLE REAMED TO 0.499" FROM INITIAL 0.438", PERFORMED HFEC WITH NO FURTHER DEFECT INDICATIONS. REA NR C057-61570-MR ISSUED TO FABRICATION REPAIR OF BUSHING & WASHERS. WORK STEPS 1-11 OF REA COMPLIED WITH. FOR DETAILS REF SRM 51-40-05 FOR REAMING OSDR ABXA20150608077Support · corrodedNUMBER 7 FLAP SUPPORT 1-2-3 BEAM HAS 5 HOLES WITH DEFECT INDICATIONS & 1 HOLE WITH DEFECT INDICATION & IS OUT OF ROUND, FOUND ON HFEC ROTARY SCAN. REAMED DISCREPANT HOLES ROUND & TONE, PERFORMED HFEC WITH NO INDICATION. REA NR C057-61559-MR WAS ISSUED, ALL DSDR ABXA20150604076Support · corrodedNUMBER 2 FLAP SUPPORT 1-2-3 BEAM HAS 2 HOLES WITH DEFECT INDICATIONS WITH HFEC ROTARY SCAN. HOLES FOR NR 2 FLAP SUPPORT 1-2-3 BEAM REPAIRED IAW REA C057-61571-MR AS REQUIRED. SDR INFO, LEVEL 2, PN 113T1499-11, PART NAME NR 2 FLAP SUPPORT 1-2-3 BEAM, SN ABX V9SDR ABXA20150604075Support Rib · corrodedNUMBER 1 FLAP SUPPORT 1-2-3 BEAM HAS 7 HOLES WITH DEFECT INDICATIONS ON HFEC ROTARY SCAN. HOLES REPAIRED FOR REA C057-61565-MR. SDR INFO, LEVEL 2, PN 113T1498-7, PART NAME NR 1 FLAP SUPPORT 1-2-3 BEAM, SN ABX V965, WS LOCATION FROM WS 798 LT. ACFT WAS GNDEDSDR ABXA20150604072Skin · damagedFUSELAGE SKIN AT LOWER VHF ANTENNA LOCATION HAS A SCRIBE LINE THE ENTIRE PERIPHERY OF THE ANTENNA. REPAIRED FUSELAGE SKIN AT LOWER VHF ANTENNA IAW SRM 53-60-01 REPAIR & REA B-653-61554-MR. SDR INFO, PN 146T3261-1, PART NAME SKIN, SN NSN, FS LOCATION FROM 119SDR ABXA20150527074Support Rib · corrodedNUMBER 2 FLAP OTBD SUPPORT HAS 1 ROTARY ACTUATOR HOLE WITH A DEFECT INDICATION ON HFEC ROTARY SCAN, HOLE IS LOCATED AT 2:00 LOOKING OTBD. REA B657-61551 ISSUED, REMOVED DISCREPANT HOLE, RE-SCANNED, NO DEFECTS NOTED. INSTALLED FREEZE PLUG & REAMED TO 1.380" ISDR ABXA20150527073Support Rib · corrodedNUMBER 1 FLAP SUPPORT INBD FLANGE HAS 2 ROTARY ACTUATOR HOLES WITH DEFECT INDICATIONS ON HFEC ROTARY SCAN, HOLES ARE AT 10:00 AND 10:30 LOCATIONS LOOKING OTBD. AFTER CLEANING & RE-CANNING DISCREPANT HOLE AT 10:00 POSITION, NO FURTHER DEFECTS NOTED. REA B 657SDR ABXA20150524071Skin · crackedELT ANTENNA LOCATION, SKIN HAS HFEC CRACK INDICATION AT MID OTBD ANTENNA MOUNT HOLE. REPAIRED ELT ANTENNA SKIN AT MID OTBD ANTENNA MOUNT HOLE IAW EWO NR 57133-0000-0005 & SRM 53-00-01 REPAIR 14. SDR INFO, PN 146T1331-1, PART NAME SKIN, SN NSN, CRACKED .200, SDR ABXA20150521069Skin · chafedVERTICAL STABILIZER ACCESS 324AL FUSELAGE MOUNTED FWD & AFT FLANGE COMMON TO PANEL MATING SURFACE CHAFED. R & R SKIN FAIRING IAW SRM 51-40-05 & 51-40-02. APPLIED PROTECTIVE COATINGS IAW SRM 51-20-01. APPLIED TOP COAT IAW AMM 51-21-10. SDR INFO, CORRODED PNSDR ABXA20150507070Skin · crackedRIGHT FUSELAGE EXTERNAL SKIN CRACKED AROUND TWO FASTENERS IN SECTION 48B, STATION 654.5 BETWEEN STRINGER 3R & 4R. REPAIRED CRACKED SKIN ON EXTERNAL FUSELAGE AT STATION 1654 IAW SRM 53-00-01. SDR INFO, PN 148T3121, PART NAME FUSELAGE SKIN, SN NSN, CRACKED LENSDR ABXA2014051394Skin · puncturedTHREE INCH SQUARE PUNCTURE THROUGH FUSELAGE SKIN BETWEEN FUSELAGE STATIONS 1373 & 1395 BETWEEN STRINGERS 26R & 27R. REPAIRED IAW SRM 53-00-01, REPAIR 12 WITH SLIGHT DEVIATIONS DUE TO DAMAGE BEING NEAR AN EXTERNAL LIGHT & A BUTT JOINT. .
SDR ABXA2014031738Engine · bird ingestionON TAKEOFF, BIRD STRIKE TO THE RT ENG. HIGH EGT, 1025 DEGREES FOR 2 SECONDS. RT ENG SHUT DOWN, AIR TURN BACK.SDR ABXA20130924546Warning Message · false activationAFTER BLOCKOUT, EICAS MESSAGE RT ENGINE FIRE LP1. PERFORMED RT ENGINE FIRE LP1 OPS CHECKED IAW AMM 23-11-00. EICAS ERASE PROCEDURE IAW AMM 31-41-00-2. NO FURTHER FAULTS NOTED. OPS CHECKED NORMAL.SDR ABXA20130629476Skin · crackedDENT BS 500 S17-18L. SKIN DETERMINED CRACKED. REPAIRED SKIN IAW SRM 53-00-01. REMOVED AND REINSTALLED SIDEWALL PANELS AND KICK PANEL IAW AMM 75-27-09-4 AND REA B653-60595-MR, ACFT WAS GROUNDED.SDR ABXA20130625474Beam · chafedTHREE CHAFED AREAS ON LOWER BEAM AFT OF SECOND PANEL LATCH FOR 437BR. R & R HYD BAY ACCESS DOOR LOWER BEAM IAW SRM 51-40-02. PYLON BEAM INBD.SDR ABXA20130620475Attach Fitting · crackedVERTICAL STABILIZER TO FUSELAGE ATTACHMENT STRUCTURE BETWEEN STAB REAR SPAR AND T/E IS CRACKED ON FWD RT FLANGE ACCESS THROUGH PANEL 324CLX FS 1746. R & R ATTACHED STRUCTURE ANGLE IAW SRM-300 51-40-02. ACFT WAS GROUNDED.SDR ABXA20130416428Control Panel · faultyFLIGHT MANAGEMENT COMPUTER SYSTEMS "CDU" FIRST OFFICER, DISPLAY BLANK. SELECTING ALT FMC DID NOT CORRECT FAULT. FIRST OFFICERS FMCS CDU CIRCUIT BREAKER POPPED AND ELECTRIC BURNING SMELL ALSO NOTED. REMOVED AND REPLACED FLIGHT MANAGEMENT PANEL PER AMM 34-61-0SDR ABXA20130416425Pin · misinstalledLOSS OF NR 2 BRAKE ROD PIN ALLOWED BRAKE ROD TO ROTATE INTO A POSITION THAT PREVENTED LEFT MAIN LANDING GEAR FULL RETRACTION INTO WHEEL WELL. ON LANDING, BRAKE ROTATED WITH WHEEL ASSEMBLY CAUSING FIELD REPAIRABLE DAMAGE TO LEFT MAIN LANDING GEAR. BRAKE ROD PSDR ABXA20120909273Smoke Detector · defectiveNR 5A CARGO SMOKE DETECTOR LIGHT IS AMBER. REMOVED AND REPLACED NR 5A SMOKE DETECTOR IAW MM 26-14-01. OPS CHECK GOOD. OPS CHECK GOOD PER AMM 26-14-01, ACFT WAS GROUNDED.SDR ABXR2012022000027Wire · arcedDURING INSPECTION FOUND WIRE W9021-015-16 SHOWING SIGNS OF ARCING. R & R AFFECTED WIRE IAW SWPM.
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