N160MC
Service difficulty reports not matched to an aircraft · 28
They name N160MC, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N160MC' AND registry_match IS NULL 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 = 'N160MC' AND registry_match IS NULL 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 2003F00628Water Injection · malfunctionedCAWI DID NOT FIRE. INSUFFICIENT AWI FLOW, HOT WEATHER OPS, OAT WAS APPROXIMATELY 100 DEGREES FARENHEIT. ADJUSTED CAWI FLOW VALVE OUT ONE FULL TURN. GROUND RUN CHECK GOOD WITH 30 PERCENT RISE IN TORQUE. (M)SDR BSA2002F00001Handle · out of adjustDURING CRUISE THE ANNUNCIATOR PANEL WARNING LIGHT CAME ON. CREW FOLLOWED EMERGENCY PROCEDURES, DEPRESSURIZED THE A/C AND CONTINUED TO DESTINATION AT A LOWER ALTITUDE. THE DESTINATION CITY WAS THE CLOSEST AIRPORT. THE CARGO DOOR WARNING LIGHT WENT OUT AFTER SDR 2002F00335Latch · misinstalledMWH - FLT 6006 - CARGO DOOR WARNING LIGHT CAME ON DURING CRUISE FLIGHT. WHEN AIRCRAFT WAS DEPRESSURIZED THE LIGHT WENT OUT. CREW CONTINUED TO NEXT STATION AS IT WAS CLOSER. THE LOWER EDGE FORWARD CLICK-CLACK JAWS WERE NOT EXTENDING CORRECTLY. THE LOWER EDGSDR 2002F00521Warning System · false activationMSO - FLT 2583 - CARGO DOOR WARNING LIGHT CAME ON DURING CLIMB 20 MILES NORTH OF THE STATION. CREW RETURNED TO THE STATION. NO APPARENT PROBLEM WAS FOUND. CARGO DOOR SWITCHES AND CLICK CLACKS WERE INSPECTED, THE SWITCHES WERE CLEANED. NO DEFECTS WERE REPORSDR 2002F00354Line · rupturedTHE RT HYD PRESS LIGHT CAME ON DURING CRUISE AND THE LT HYD PRESS LIGHT CAME ON DURING DESCENT. THE FLAPS EXTENDED SLOWLY, CREW DECLARED EMERGENCY, USED THE GEAR EMERGENCY EXTEND SYS. LANDING WAS COMPLETED WITHOUT INCIDENT. RT ENG HYD PUMP PRESSURE LINE HADSDR 2002F00357Seal · damagedFLT 2588 - HLN - DURING CLIMB-OUT, CABIN PRESSURE WAS LOST. CREW AND PASSENGERS UTILIZED OXYGEN MASKS AND FLIGHT CONTINUED TO DESTINATION. CABIN DOOR SEAL HAD A HOLE IN IT. INITIALLY WAS DEFERRED PER MEL. FOUND HOLE POKED IN PASSENGER DOOR SEAL, REPLACED DSDR 20010515SG001Handle · out of positionDURING CLIMB-OUT, CREW FOUND AIRCRAFT WOULDN''T PRESSURIZE IN EITHER MAN OR AUTO MODE. SUCTION GAUGE SHOWED IN NORMAL RANGE. RECYCLED CARGO DOOR HANDLE, PRESSURIZATION OPS CHECKED GOOD. (M)SDR 2002F00520Mechanism · damagedBIL - FLT 1315 - CARGO DOOR WARNING LIGHT CAME ON DURING CRUISE AT FL190. THE CREW DECREASED CABIN PRESSURE AS THEY RETURNED TO STATION. THE WARNING LIGHT WENT ABOUT THE TIME THE PRESSURE DIFFERENTIAL WAS REDUCED TO 0. INITIAL INSPECTION FOUND THE UPPER FORSDR 20010206SG004Warning Light · illuminatedHOB - FLT 1331 - LEFT WING OVERHEAT LIGHT CAME STEADY ON DURING CRUISE. CREW FOLLOWED CHECKLIST PROCEDURES, EXTENDED GEAR AND TURNED OFF LEFT BLEED. LIGHT WENT OUT AFTER ONE MINUTE. CREW RETURNED TO STATION WITH NO FURTHER PROBLEMS. NO APPARENT MECHANICAL SDR 20000810SH010Connector · damagedDFW - FLT 1325 - BATTERY OVERHEAT LIGHTS CAME ON IN-FLIGHT. WHEN BATTERY WAS SHUT OFF BY CREW USING EMERGENCY CHECKLIST PROCEDURES, LIGHTS WENT OFF AND BATTERY TEMPERATURE INDICATOR RETURNED TO GREEN RANGE. AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENASDR 20001005AP030Line · leakingFLT 1321 - DFW - DURING CRUISE FLIGHT, THE CREW NOTICED THE HYD PRESS LOW LIGHTS CAME ON . HYDRAULIC PRESSURE GAGES WERE CHEKED AND THE LACK OF HYD PRESS WAS CONFIRMED. THE FLIGHT CONTINUED NORMALLY. THE CREW PERFORMED AN EMERGENCY GEAR EXTENSION AND A FLAPSDR 20000816AP005Line · brokenDFW - FLT 1321 - DURING CRUISE FLIGHT, THE CREW NOTICED THE HYD PRESSURE LOW LIGHTS CAME ON. HYDRAULIC PRESSURE GAUGES WERE CHECKED AND THE LACK OF HYD PRESSURE WAS CONFIRMED. THE FLIGHT CONTINUED NORMALLY. THE CREW PERFORMED AN EMERGENCY GEAR EXTENSION ANDSDR MALA975388Radar · failedDURING CRUISE FLIGHT, CREW REPORTED WEATHER RADAR INOP. AIR TURN BACK TO MSP. MAINTENANCE REMOVED AND REPLACED WEATHER RADAR. OPS CHECK GOOD. (M)SDR MALA965209Switch · failedFLT 3365 - ON APROACH TO DTW, THE GEAR HAD TO BE CYCLED TWO TIMES BEFORE A NOSE GEAR DOWN INDICATION WAS RECEIVED. MAINTENANCE REPLACED THE DOWN AND LOCKED SWITCHES ON THE RIGHT SIDE OF THE NOSE GEAR. ALL CHECKS SATISFACTORY. (X)SDR MALA965079Switches · lack of lubeFLT 3397 - ON APPROACH TO DTW, THE NOSE GEAR GREEN LIGHT FAILED TO ILLUMINATE. THE CREW CYCLED THE GEAR AND THE LIGHT ILLUMINATED AFTER 15 SECONDS. MAINTENANCE CLEANED AND LUBED THE NOSE LANDING GEAR MICROSWITCHES. THE GEAR WAS SWUNG SEVERAL TIMES. ALL CHESDR MALA965001Connector · water contamFLT NR 3467 - ON CLIMB-OUT FROM YXU, THE LEFT BATTERY AMBER AND RED LIGHTS ILLUMINATED AND THE BATTERY TEMP INDICATION WAS HIGH. THE CREW TURNED OFF THE BATTERY AND RETURNED TO YXU. MAINTENANCE REPLACED THE BATTERY TEMP SENSOR CANNON PLUG. ALL CHECKS SATISFSDR MALA954695Starter/Gen · failedDURING A TRAINING FLIGHT IN FAR, THE LEFT ESSENTIAL BUS AND LEFT GENERATOR FAILED. THE AIRCRAFT RETUREND TO FAR WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LEFT STARTER GENERATOR AND A P/N ANL 325 CURRENT LIMITER. ALL SYSTEMS OPERATED SATISFACTORILSDR MALA954663Rib · crackedDURING A SCHEDULED INSPECTION IN MSP, THE LEFT FLAP INBOARD ACTUATOR RIB WAS FOUND TO BE CRACKED. REPAIRS WERE COMPLETED BY INSTALLING DOUBLER IAW FAC SRM 51-00-00, 57-90-10, REPAIR NR 11, AND LAR 95-MALA-254. (M)SDR MALA954612Door Frame · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE CARGO DOOR AFT FUSELAGE FRAME AT FS 438.060 TO BE CRACKED AT THE MOUNT POST HOLE. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR ANGLE IAW FAC ARP 53-20-9503. (M)SDR MALA954611Door Frame · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE CARGO DOOR AFT FUSELAGE FRAME AT FS 491 TO BE CRACKED AT THE GAS STRUT MOUNT POST HOLE. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR ANGLE IAW FAC ARP 53-20-9503. (M)SDR MALA954438Stiffener · crackedDURING BLOCK CHECK IN MSP, MAINTENANCE FOUND CENTER STIFFENER ASSY P/N 27-31110 AT BL 0.00 AND FS 254.52 CRACKED. REPAIRED BY REPLACING CENTER STIFFENER ASSY WITH NEW P/N STIFFENERS 27-31110-031, 032 AND CLIP P/N 27-31110-017, 027. ALSO, INSTALLED STIFFENER SDR MALA954437Frame · crackedDURING BLOCK CHECK INSPECTION MSP, MAINTENANCE FOUND A CRACK IN LOWER RT BELT FRAME RELIEF RADIUS AT FS 144.24 AND WL 80.39 RIGHT BELOW STRINGER NR 11A. REPAIRS WERE COMPLETED BY STOP DRILLING AND FABRICATING REPAIR DOUBLER IAW FAIRCHILD SRM NR 19 53-90-20, PSDR MALA954414Bleed Air · odorMSP - FLT 3235 - EN ROUTE, CREW NOTED A HOT SMELL FROM THE RIGHT BLEED SYSTEM. THE CREW SHUT OFF THE RIGHT BLEED SYSTEM AND THE SMELL DISSIPATED. THE AIRCRAFT CONTINUED TO MSP. THE SYSTEM IS CURRENTLY DEFERRED UNDER MEL 21-9C. (X)SDR MALA954402Angle · crackedDURING SCHEDULED MAINTENANCE IN MSP, THE RIGHT WING TO NACELLE UPPER INBOARD ATTACH ANGLE WAS FOUND TO BE CRACKED. REPAIRS WERE COMPLETED BY STOP DRILLING THE CRACK AND INSTALLING A REPAIR ANGLE AS PER ARP 54-20-9101 REVISION B. (W)SDR MALA954395Dnlock Spring · brokenFLT NR 3074 - ON APPROACH TO MSP, THE NOSE GEAR REMAINED UP AND LOCKED AFTER GEAR EXTENSION. THE CREW CYCLED THE GEAR UNTIL THE NOSE GEAR EXTENDED NORMALLY. THE AIRCRAFT LANDED IN MSP WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT DOWN LOCK SPRING MISSDR MALA954387Hsi · failedFLT 3211 - ON CLIMB-OUT FROM MSP, THE CAPTAINS HSI FAILED. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE NR 1 HSI. SYSTEM OPERATED SATISFACTORILY. (W)SDR MALA954384Frame · crackedMSP - DURING ROUTINE MAINTENANCE, LEFT FUSELAGE CONSTANT SECTION LOWER BELT FRAME AT FS 174.06 WAS FOUND CRACKED. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A DOUBLER IAW FAC ARP 53-20-9148. (X)SDR MALA954250Torque Tube · bentMSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND RUDDER TORQUE TUBE BENT. REPAIRS COMPLETED BY REPLACING TORQUE TUBE IAW FAC 27-20-20, 27-00-00, AND SRM 51-00-00, PAGE 3. (X)
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