Fokker F.28 MK 0100
Service difficulty reports · 1,581
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = 'F28MK0100' 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 aircraft_model_key = 'F28MK0100' 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 CA070608008Control Cable · broken(CAN) FLIGHT CREW REPORTED DURING HEAD START CHECKS THAT THE FLIGHT CONTROL LOCK WOULD NOT LOCK THE ELEVATOR CONTROLS AND WAS VERY STIFF WHEN MOVING CONTROL LOCK TO FREE POSITION. RECERTIFICATION, FOUND THE FLIGHT CONTROL LOCK CABLE FCL1 SNAPPED AT AILERON FSDR CA070109005Valve · malfunctioned(CAN) DATE OF DELAY NOV 8, 2006 CADORS NR: 2006C2915. THE FLIGHT CREW WAS NOTIFIED THAT DURING TAXI FOR DEPARTURE FUEL WAS LEAKING FROM LT WING. AIRCRAFT TAXIED OFF RUNWAY BY WHICH TIME THE LEAK HAD STOPPED. FLIGHT CREW IN CONTACT WITH MAINTENANCE CONTROL SDR CA070110005Warning System · malfunctioned(CAN) THE REFERENCED AIRCRAFT AN EVENT INVOLVING THE AUTOMATIC SILENCING OF CABIN CHIMES. NORMALLY THE FLIGHT CREW WILL ADVISE THE FLIGHT ATTENDANTS TO TAKE THEIR POSITIONS FOR LANDING WITH 3 CHIMES SELECTED MANUALLY IN THE COCKPIT. IT APPEARS HOWEVER IN LASDR CA060919005Actuator · malfunctioned(CAN) FLIGHT CREW REPORTED THAT THE SPEED BRAKE WOULD NOT RETRACT UPON SELECTION TO DO SO. FOLLOWING LANDING. BOTH PADDLES CONFIRMED OPEN. AIRCRAFT WAS FERRIED TO BASE, WHERE THE SPEED BRAKE ACTUATOR WAS REPLACED. SYSTEM TESTED SERVICEABLE AFTER REPLACEMENT. SDR 2006F00020Arm · crackedCENTER ARMREST CRACKED AT ATTACH BRACKET TO SEAT FRAME, HAVE SEEN OTHER SEATS WITH SAME CONDITION, FLIGHTLINE IN TULSA IS WORKING WITH FSDO IN CALIFORNIA AND FLIGHTLINE ENGINEERING. AMERICAN AIRLINES HAS A REPAIR PROCEDURE FOR THIS PART.SDR AU510002130Oxygen Bottle · leakingCOCKPIT OXYGEN BOTTLE LEAKING FROM VALVE.SDR AU510002116Control Panel · faultyNR 2 ATC TRANSPONDER SYSTEM CONTROL PANEL DISPLAY DIGITS NOT VISIBLE.SDR AU510002112Transponder · failedNR 2 ATC TRANSPONDER FAILED. INVESTIGATION CONTINUING.SDR AU510002107Shutoff Valve · faultyRT BLEED AIR PRESSURE REGULATING AND SHUTOFF VALVE (PRSOV) FAULTY.SDR AU510002024Fairing · crackedENGINE EXHAUST SPOKE FAIRING CRACKED IN TWO PLACES AT THE 7:30 O`CLOCK AND 9 O`CLOCK POSITIONS.SDR AU510002019Solenoid · faultyNR 2 ENGINE THRUST REVERSER INTERMITTENT WARNING. INVESTIGATION FOUND THE SECONDARY LOCK SOLENOID HAD A FAULTY INTERNAL SWITCH.SDR AU510002018Igniter · wornNR 2 ENGINE IGNITER WORN.SDR AU510001949Skin · lightning strikeEVIDENCE OF LIGHTNING STRIKE ON FUSELAGE AT STN 9305, STN 9805 AND STN 10253. INVESTIGATION CONTINUING.SDR AU510001948Motor · faultyFUEL SYSTEM RT CROSS FLOW VALVE MOTOR FAULTY. VALVE STUCK IN CLOSED POSITION.SDR AU510001947Shutoff Valve · failedLT ENGINE ANTI-ICE PRESSURE REGULATING AND SHUTOFF VALVE (PRSOV) FAILED.SDR AU510001935Stringer · corrodedNR 3 LT STRINGER LOCATED AT STN 13851 IN THE FORWARD CARGO COMPARTMENT CORRODED.SDR AU510001923Cooling Fan · faulty(AUS) AVIONICS COOLING FAN NOISY IN OPERATION.SDR AU510001915Control Cable · misrigged(AUS) CONTROL CABLES FOR FLAPS ( F1 AND F2) WERE FOUND TO BE 43LB LOW IN TENSION. THE LT AILERON WING CABLE WAS 30LB LOW. THE LT AND RT AILERON UPFLOAT CABLES WERE 45LB LOW. (CASA NR 510001915)SDR AU510001914Bolt · loose(AUS) LT AILERON TAB OB HINGE BRACKET ATTACHMENT BOLTS LOOSE. BOLTS WERE THREADBOUND IN ANCHOR NUTS. INVESTIGATION FOUND INCORRECT BOLTS WERE FITTED BY A PREVIOUS OPERATOR IN THE US. (CASA NR 510001914)SDR AU510001903Drive Shaft · sheared(AUS) APU STARTER MOTOR DRIVESHAFT SHEARED. INVESTIGATION FOUND THAT THE BROKEN END WAS JAMMED IN THE CLUTCH ASSEMBLY. (CASA NR 510001903)SDR AU510001887Switch · faultyNR 1 ENGINE ANTI-ICE SWITCH FAULTY.SDR AU510001866Bolt · looseNR 1 LT LIFT DUMPER SYSTEM BELLCRANK SPIGOT ATTACHMENT BOLTS LOOSE.SDR AU510001805Iru · failedNR 2 INERTIAL REFERENCE UNIT (IRU) INTERMITTENTLY FAILS CODE 2. INVESTIGATION CONTINUING.SDR AU510001804Bolt · brokenNR 2 MAIN WHEEL TIE BOLT BROKEN. BOLT HEAD MISSING. INVESTIGATION CONTINUING.SDR AU510001802Motor · shearedAPU STARTER MOTOR DRIVE SHAFT SHEARED.SDR AU510001751Fuel Control · failed(AUS) APU AUTO-SHUTDOWN IN FLIGHT. INVESTIGATION FOUND A FAULTY FUEL CONTROL UNIT. (CASA NR 510001751)SDR AU510001740Exciter · faultyAPU IGNITION EXCITER UNIT FAULTY.SDR AU510001726Pipe · fracturedHYDRAULIC PIPE LOCATED ON THE FORWARD WALL OF THE REAR CARGO HOLD LEAKING. INVESTIGATION FOUND A FRACTURED FLARE. PIPE WAS A -4 STAINLESS STEEL TYPE.SDR AU510001721Hose · failedLT TOILET SMOKE DETECTOR TO AIR EJECTOR HOSE SPLIT AT EJECTOR END. RT SMOKE DETECTOR TO AIR EJECTOR TUBE SIDEWALL COLLAPSED. HOSES ALLOW FOR AIRFLOW THROUGH SMOKE DETECTORS.SDR AU510001667Smoke Detector · faultyREPORT OF CIGARETTE SMOKE SMELL IN CABIN. TOILET SMOKE DETECTOR DID NOT ACTIVATE ALARM. INVESTIGATION CONTINUING.SDR AU510001655Connector · leakingCREW OXYGEN MASK BOX ASSEMBLY CONNECTOR LEAKING. LOSS OF OXYGEN.SDR AU510001654Bearing · wornLT ENGINE INLET GUIDE VANE BEARINGS PNO UP60336 (1OFF) AND PNO EU61711 (2OFF) WORN. FOUND DURING INSPECTION IAW SB TAY-75-1655.SDR AU510001648Pitot Head · faultyNR 3 PITOT HEAD HEATING SYSTEM FAILED.SDR AU510001540Pressure Switch · faultyRT ENGINE LP FUEL PRESSURE SWITCH FAULTY.SDR AU510001534Connector · looseENGINE INDICATION SYSTEM PRESSURE BULKHEAD CONNECTOR P2874 LOOSE.SDR AU510001521Igniter · failedAPU IGNITER PLUG FAILED. WORKSHOP INVESTIGATION FOUND THAT ONLY APPARENT FAULT WAS SLIGHT SOILING ON THE CERAMIC INSIDE OF THE CONNECTOR END OF THE IGNITER. THERE WAS NO OBVIOUS SIGN OF ARCING ACROSS THE CERAMIC SURFACE. WHEN THE IGNITER WAS CLEANED, THERE WSDR AU510001498Strut · crackedRT MAIN LANDING GEAR STRUT BLEED PORT CRACKED, FOUND DURING INSPECTION IAW AD/F100/64.SDR AU510001497Strut · faultyLT MAIN LANDING GEAR STRUT INTERNAL SLEEVE MIGRATED OUT OF POSITION AND BLOCKED BLEED PLUG HOLE, FOUND DURING INSPECTION IAW AD/F100/64.SDR AU510001481Nipple · missing(AUS) FLAP BALL NUT GREASE NIPPLE MISSING.(OTHER CAUSE: UNKNOWN ) (CASA# 510001481)SDR AU510001439Microphone · faulty(AUS) HAND MICROPHONE SWITCH STICKING.(OTHER CAUSE: STICKY SWITCH - MATERIAL ) (CASA# 510001439)SDR AU510001988Apu · failedAPU AUTO SHUTDOWN. INVESTIGATION COULD FIND NO FAULTS. DURING TEST FLIGHT THE APU AGAIN SHUT DOWN. INVESTIGATION CONTINUING.SDR AU510001987Igniter · failedNR 1 ENGINE IGNITER PLUG FAILED.SDR AU510001868Bearing · wornRT WING FLAP TRACK BEAM ASSEMBLY FORWARD SUPPORT BEARING WORN.SDR AU510001867Bearing · wornLT WING TRAILING EDGE FLAP TRACK FORWARD SUPPORT BEARING WORN.SDR AU510001864Rod · crackedRH LIFT DUMPER SYSTEM VERTICAL ROD CRACKED.SDR AU510001862Bearing · looseRT LIFT DUMPER NR 3 BELLCRANK HORIZONTAL ROD ATTACHMENT BEARING MIGRATED OF POSITION.SDR AU510001861Bolt · shearedRT LIFT DUMPER SYSTEM NR 1 BELLCRANK INBOARD UPPER ATTACHMENT BOLT SHEARED.SDR AU510001708Apu · inoperativeAPU FAILED TO START. INVESTIGATION CONTINUING.SDR AU510001588Slide · faulty(AUS) RT ESCAPE SLIDE FAILED TO DEPLOY CORRECTLY. FOLLOWING MANUAL OPERATION THE SLIDE INFLATED BUT WAS NOT CORRECTLY ORIENTATED TO THE DOOR OPENING. SUSPECT CAUSED BY FAULTY PACKING OF THE SLIDE AT THE LAST OVERHAUL. (CASA NR 510001588)SDR AU510001587Computer · faulty(AUS) AUTOPILOT COMPUTER SUSPECT FAULTY. (CASA NR 510001587)
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