JASC 2750
Service difficulty reports · 10,201
Reports filed under 2750 · Trailing Edge Flap Control System, 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 jasc_code = '2750' 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 jasc_code = '2750' 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 COMA60454ABpsu · malfunctionedFLIGHT 5144 - FLAPS FAIL CAUTION. REPLACED THE LT BPSU.SDR SWIA200515466Detector · malfunctionedFLAPS HALFSPEED STATUS MESSAGE DURING TAXI. REPLACED RIGHT WING OUTBOARD FLAP SKEW DETECTOR FOR NR 1 SFCU IAW MM 27-52-45. OPERATIONAL CHECK GOOD.SDR REX2005F00009Fcu · failed(REF NR: 05-098) FLAP FAILURE AT 0, QRH FOLLOWED UNEVENTFUL LANDING. REMOVED AND REPLACED FLAP ELECTRONIC UNIT (FECU) IAW AMM. (K)SDR REX2005F00008Control System · failed( REF NR 05-099) UPON CLIMBOUT, FLAPS FAIL WHEN SELECTED UP. DECLARED EMERGENCY, DIVERTED. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)SDR DLM90050464Control Unit · failedELEVATOR SPLIT MSG AND PYLON FLAP FAULT MSG ILLUM IN FLT. REPLACED ACU, ALL DIAGNOSTIC TESTS PASSED.SDR VNAA0508011Flap System · malfunctionedTHE FLAPS FAIL CAUTION MESSAGE ILLUMINATED ON APPROACH. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE CYCLED AIRCRAFT POWER. THE FLAP SYSTEM OPERATIONALLY CHECKED GOOD IAW CRJ200 AMM 27-54-00-710-801. THE AIRCRAFT WAS RELEASED FOR SERVSDR 08182005AValve · malfunctionedFLAPS DEPLOY VIOLENTLY FROM 0 TO 15 DEGREES. REMOVED AND REPLACED FLAP VALVE.SDR COMA0560450Bpsu · malfunctionedFLIGHT 5637 - FLAPS FAIL CAUTION. REPLACED THE LT BPSU.SDR SWIA200515433Control Unit · malfunctionedFLAP CONTROL FAULT ON CLIMB-OUT. REPLACED THE FLAP CONTROL UNIT. OPERATIONAL CHECK GOOD IAW MM 27-50-00.SDR SWAA052460Pushrod · brokenDURING SCHEDULED RON CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DRIVE PUSHROD BROKEN. REMOVED AND REPLACED PUSHROD PER MM.SDR ASOA05667Bpsu · malfunctionedFLT 4386 - DURING APPROACH INTO CVG FROM MHT, THE CREW RECEIVED A FLAPS FAIL MESSAGE WITH THE FLAPS SELECTED TO EIGHT DEGREES. EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS A PRECAUTION. THE AIRCRAFT LANDED SAFELY IN CVG. MAINTENANCE REMOVED AND REPSDR CA050824010Drive Assy · sheared(CAN) AC HAD JUST LANDED, SELECTED FLAPS UP, STOPPED BETWEEN APPROACH AND ZERO (FULL UP). PILOT CALLED MAINT, WAS INSTRUCTED TO TRY SPLIT FLAP BYPASS SYS, INFORMED MAINT THAT ALL FLAPS WENT UP EXCLUDING THE RT OB. ASSUMED THAT FLAP DRIVE CABLE WAS SHEARED. SDR C1HA200597002Transmission · inoperativeAFTER LANDING FLAP INDICATOR FLAPS STUCK ON 8 DEG (INBOARD) C/B`S CLOSED. PERFORMED ADJUSTMENT, FOUND SHEERED PIN ON OUTPUT DRIVE GEAR OF NR 5 FLAP TRANSMISSION R@RED NR 5 FLAP TRANSMISSION PER MM 27-51-41.SDR DL764050458Transmitter · out of adjustT/E FLAP ASYM EICAS MSG, LT FLAP READS 4 RT FLAP READS UP. ADJUSTED NR 5 POSITION TRANSMITTER PER MM.SDR SWIA200515419Sensor · malfunctionedFLAPS FAIL MSG DURING AFTER LANDING. REPLACED RT FLAP BPSU. OPERATIONAL CHECK GOOD IAW CRJ 200 AMM 27-51-10.SDR SWAA052422Torque Tube · wornDURING SCHEDULED SERVICE CHECK, FOUND NR 5 T/E FLAP TRANSMISSION TORQUE TUBES WORN. REMOVED AND REPLACED TORQUE TUBES PER MM.SDR SWAA052421Torque Tube · wornDURING SCHEDULED SERVICE CHECK, FOUND NR 4 T/E FLAP TRANSMISSION TORQUE TUBES WORN. REMOVED AND REPLACED TORQUE TUBES PER MM.SDR COMA0560441Bpsu · out of rigFLIGHT 5207 - FLAPS FAIL CAUTION. RE-RIGGED LT AND RT BPSU. SYSTEM CHECKS NORMAL.SDR 2005UALA01181Flap System · malfunctionedDIVERTED TO SFO DUE TO FLAP RETRACTION PROBLEM.SDR 2005FA0001210Motor · failedFLAP CIRCUIT BREAKER POPS WHEN RETRACTING FLAPS. FOUND FLAPS GOING OVER TRAVEL IN DOWN DIRECTION, PROBABLY OVERLOADING CAUSING OVERLOADING OF FLAP MOTOR. FOUND MOTOR COILS SHOW SIGNS OF OVERHEATING. MFG HAS SUPERSEDED MOTOR TO NEW MOTOR. (K)SDR COMA0560440Bpsu · unreliableFLIGHT 5208 - FLAPS FAIL CAUTION. REPLACED THE LT BPSU.SDR REX2005F00011Control System · failed(REF NR: 05-096) FLAPS FAILED AT 20 WHEN SELECTED TO 30 ON APPROACH. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)SDR SWIA200515431Flap System · out of rigFLAPS FAIL MESSAGE ON CLIMB-OUT. CLEARED INHIBITS. ELECTRICALLY RIGGED FLAPS. OPERATIONAL CHECK GOOD.SDR 05FDEA02381Motor · malfunctionedO/B T/E FLAPS WOULD NOT POSITION WITH FLAP HANDLE. FLT CREW C/W QRH PROCEDURES AND HAVE A C/B PULLED. INSPECTED O/B FLAPS FOR POSSIBLE JAM AND NONE NOTED. WITH HYD ON, THE O/B FLAP CONTROL VALVE IS BYPASSING FLUID. REMOVED AND REPLACED O/B FLAP HYD MOTOR SDR SWIA200515403Control Unit · malfunctionedFLAP 1/2 SPEED MESSAGE AND FLAP FAIL. REPLACED FECU IAW AMM TASK 27-51-05. OPERATIONAL CHECK GOOD. FLAPS HALFSPEED.SDR COMA0560434Control System · malfunctionedFLIGHT 5178 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR SWIA200515429Sensor · malfunctioned"FLAPS FAIL" CAUTION MSG. REMOVED AND REPLACED RT BPSU IAW CRJ MM 27-51-10 AND READJUSTED LT AND RT BPSU IAW M/M 27-51-10. READJUSTEMENT OF FECU POTENTIOMETER NR 5 AND NR 8. OPERATIONAL CHECK GOOD IAW CRJ M/M 27-51-10.SDR YENA200545Computer · malfunctionedECAM MSG FLAPS LOCKED FLT CNTRL - ALIGNMENT FAULT. DURING FINAL APP TO BUR, FLAP HANDLE MOVED TO FLAP 2 POSITION. FLAPS LOCKED BETWEEN POS 1 AND POS 2. SLATS EXTENDED NORMALLY: DIVERTED TO LAX. PERFORMED WTB RESET OF FLAP SYS PER AMM 27-50-00-02. REMOVED SDR COMA0560432Control System · failedFLIGHT 5660 - FLAPS FAIL. INSPECTED FLAPS IAW AD 98-20-01.SDR MASA200500613Fcu · malfunctionedASH 2664 PHL. FLAPS FAILING AT ZERO DETENT. MX REMOVED AND REPLACED THE FECU.SDR QXEA200501149Torque Sensor · malfunctionedSEA FLIGHT NR 2078 - RECEIVED FLAP DRIVE CAUTION LIGHT WHEN SELECTING FLAPS TO 5 DEGREES ON AFTER START PRIOR TO TAXI. MAINTENANCE REPLACED TORQUE SENSOR UNIT IAW DHC-8-200 AMM TASK 27-52-51-000-801 AND 27-52-51-400-801. FUNCTIONAL TEST GOOD. AIRCRAFT RETURSDR MASA200500612Flap System · failedASH 2751 PHL. FLAPS FAILED AT ZERO. MAINTENANCE RESET PER PART A OF AD.SDR SWIA200515359Fcu · malfunctionedFLAPS FAIL IN FLIGHT. REPLACED AND RERIGGED LEFT AND RIGHT BPSU AND FECU IAW 27-50-00. OPERATIONAL CHECK GOOD.SDR REX2005F00001Control System · malfunctioned(REF NR: 05-093) FLAPS FAIL AT 20 WHEN SELECTED ON TAXI. RESET SYSTEM AND PLACED 72 HOUR WATCH IAW AD 98-20-01. (K)SDR COMA0560423Coupling · malfunctionedFLIGHT 5454 - FLAP FAIL CAUTION. REPLACED THE LT NR 1 FLEY DRIVE SHAFT.SDR SWIA200515355Lever · malfunctioned"FLAP FAIL" CAUTION MESSAGE. REPLACED FLAP SELECTOR LEVER IAW MM 27-50-00. OPERATIONAL CHECK GOOD, PN 7-45500-1, SN/OFF 764.SDR SWIA200515408Controller · malfunctionedFLAPS HALFSPEED STATUS MSG. REPLACED SLAT/FLAP CONTROLLER. OPERATIONAL CHECK GOOD IAW MM 27-52-00.SDR COMA0560417Fcu · malfunctionedFLAPS FAIL CAUTION. REPLACED THE FECU.SDR 05FDEA02127Bracket · brokenCOMPLY WITH EA 8-2750-82100A FLIGHT CONTROL-FLAP-REPLACMENT OF FLAP CONTROL BRACKET. COMPLIED WITH EA 8-2750-82100A. FLIGHT CONTROL FLAP REPLACMENT OF LWR CONTROL BRACKET.SDR CA050804009Torque Tube · worn(CAN) DURING ROUTINE INSPECTION THE NR 2 TRANSMISSION TORQUE TUBE, A DEEP 'V' GOUGE .016 INCH DEEP WAS FOUND. A FLEET CAMPAIGN WAS INITIATED TO CHECK ALL TRAILING EDGE FLAP TORQUE TUBES.SDR REX2005F00012Control System · failed(REF NR: 05-091) FLAPS FAIL AT 30 DEGREES ON APPROACH, QRH FOLLOWED. LANDING UNEVENTFUL. FOUND FCL NOT IN 30 DETENT. RESET FLAPS AND COMPLIED WITH AD-98-20-01. MONITORING FLAPS FOR 72 HOURS. (K)SDR SWIA200515338Control Unit · malfunctionedFLAPS HALFSPEED STATUS MSG IN FLIGHT. REPLACED FECU IAW CRJ 200 MM 27-50-00. OPERATIONAL CHECK GOOD, PN 860D100-18 SNOFF 251.SDR CA050804008Control Cable · frayed(CAN) DURING A 100 HR INSPECTION THE CENTER FLAP CABLE WAS FOUND TO BE FRAYED AT THE PULLEY AREA. THE CABLE WAS REPLACED NEW. THIS IS A COMMON AREA FOR WEAR ON THESE CABLES.SDR COMA0560411Flap System · malfunctionedFLIGHT 5043- FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR COMA0560408Flap System · malfunctionedFLIGHT 5137- RECEIVED A FLAP FAIL CAUTION DURING CVG APPROACH. AIRCRAFT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST ENVENT MAINTENANCE ACTION PARAGRAPH (B) 1,2,3, (A,B,C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CASDR 07252005AFlap System · lack of lubeWITH AUTOPILOT ENGAGED THE FLAPS DO NOT MOVE. FOUND MINOR STICKING BETWEEN FLAP AND COVE WHERE FRESHLY PAINTED. SMOOTHED SURFACE AND LUBRICATED.SDR COMA0560406Flap System · malfunctionedFLIGHT 5497- FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR 07232005AFlap System · malfunctionedNO MOVEMENTS WHEN FLAPS SELECTED TO 15 DEGREESSDR QXEA20051138Flap System · malfunctionedDEN- ON FLIGHT 4277, DURING TAXI OUT, THE FLAP FAULT STATUS MESSAGE ILLUMINATED. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE RESET THE SYSTEM PER THE PROCEDURES IN THE AMM. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED.SDR QXEA200501132Flap System · inoperativeSEA-ON FLIGHT 2348, RETURNED TO GATE, WHEN SETTING FLAPS FOR TAKEOFF, THE FLAP POWER CAUTION LIGHT ILLUMINATED AND THE FLAPS DID NOT MOVE. NO FAULTS FOUND IN CDS. CLEARED NVM IN CDS, RESET FLAP CONTROL CIRCUIT BREAKER. RAN FLAPS UP AND DOWN TO 35 DEGREES. FLAP
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