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 COMA0460171Warning Light · illuminatedFLIGHT 5745 FLAPS FAILED CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.SDR SWIA200412942Control Unit · malfunctionedWHEN FIRST POWER UP A/C RECEIVED A CONTROL FAULT ON FLAP. REPLACED FLAP CONTROL UNIT PER MM 27-50-00. OPS CHECK OK.SDR CA040225017Sensor · malfunctioned(CAN) AFTER TAKE OFF ABOUT 100 FOOT ABOVE GROUND LEVEL FLAPS LOCK ECAM MESSAGES, TRIED RESET , NIL FIX, RETURN TO GATE. RESET OF THE COMPUTER SLAT FLAP COMPUTERS ON GROUND FIXED THE PROBLEM BUT SAME THING HAPPENNED ON THE SECOND ATTEMPT. AIRCRAFT UNDER INVESTISDR MALA040224Control Valve · failedLANDING IN DTW CREW REPORTED FLAPS WOULD NOT EXTEND. COMPLETED ALL FLAPS LANDING. FLAPS WILL NOT EXTEND DN FLAPS 0 AT DTW ALL CB IN. REMOVED AND REPLACED FLAP CONTROL VALVE S/N ON 1168, S/N OFF 1588 IAW SAAB MM CHAP 27 SEE 409 CARD FOR DEATILS, ALL CHECKS GSDR CA040225014Control Cable · frayed(CAN) FLAP CABLES REMOVED FOR INSPECTION, REFERENCE SD ALERT AL-2003-05 IB FLAP CABLE, RT SIDE, PART NR 1460100-7 FRAYED APPROX 50 PERCENT AT IB BELLCRANK. 1 INCH FROM SWAGGED TERMINAL. ALSO BOTH OB CABLES PN 1460100-8 FRAYED AT IB BELLCRANK, APPROX. 1 INCH FRSDR CA040225011Control Cable · frayed(CAN) FLAP CABLES REMOVED FOR INSPECTION DUE TO SERVICE DIFFICULTY ALERT AL-2003-05. LT AND RT OUTBOARD FLAP CABLES FOUND TO BE FREYED AT THE INBOARD BELLCRANK, APPROXIMATELY 1 INCH FROM THE SWAGGED TERMINAL. BOTH CABLES ARE ORIGINAL CESSNA FLAP CABLES AND WERSDR COMA0460173Warning Light · illuminatedFLIGHT 5718 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.SDR 04054651Control Unit · malfunctionedDURING APPROACH OF FLIGHT 7522 CREW REPORTED A FLAP SYSTEM FAILURE WITH FLAPS A 8 DEGREES. FLIGHT LANDED UNEVENTFULLY. A SYSTEM OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE.SDR COMA0460160Bpsu · malfunctionedFLIGHT 5700 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU.SDR SWIA200412937Pdu · malfunctionedFLAP HALFSPEED MESSAGE DURING FLAP EXTENSION. REMOVED AND REPLACED FLAP PDU IAW 27-52-01. OPS CHECK GOOD.SDR COMA0460159Flap · malfunctionedFLIGHT 5706 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.SDR COMA0460157Pdu · malfunctionedFLIGHT 5108 FLAPS FAIL MESSAGE DURING TAXI. REPLACED THE PDU.SDR COMA0460156Flap · malfunctionedFLIGHT 5159 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.SDR 04049710AEcu · false activationDURING APPROACH THE CREW REPORTED A FLAP FAIL MESSAGE AT 30 DEGREES. FLIGHT LANDED WITHOUT INCIDENT AND PASSENGERS DEPLANED NORMALLY. A SATISFACTORY OPERATIONAL CHECK OF THE FLAP SYSTEM WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE.SDR DL78K040164Transmitter · inoperativeON FLAP EXTENSION THRU 2 DEG FLAPS SPLIT AND LOCKED OUT. DIVERTED TO ORD FOR A 2 DEG FLAP LANDING. REPLACED LEFT FLAP POSITION TRANSMITTER.SDR COMA0460155Control Unit · malfunctionedFLIGHT 5784 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU.SDR DBC2004F00000Fuse · failedON APPROACH, FLAPS WOULD NOT EXTEND, LANDED UNEVENTFULLY. TROUBLESHOT AND FOUND FUSE F23 IN FLAP CONTROL SYSTEM BLOWN. APPARENT CAUSE WAS MOISTURE CONTAMINATION OF FLAP CONTROLLER CONNECTOR. REPLACED FUSE F23, OPERATIONS CHECKED GOOD.SDR QXEA200400154Control Unit · failedON TAKEOFF THE CREW RECEIVED A FLAP POWER CAUTION LIGHT WHEN THE FLAPS WERE SELECTED UP. THE CREW RESET THE C/B AS PER THE ABNORMAL CHECK LIST AND THE CAUTION LIGHT EXTINGUISHED. MAINTENANCE INSPECTED THE AIRCRAFT FLAP SYSTEMS AND REPLACE THE FLAP POWER CONTSDR COMA0460149Bpsu · malfunctionedFLIGHT 5389 FLAPS FAIL CAUTION MESSAGE. REPLACED THE LT BPSU.SDR COMA0460151Control Handle · malfunctionedFLIGHT 5257 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FLAP CONTROL LEVER.SDR COMA0460145Control Handle · malfunctionedFLIGHT 5110 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FLAP SELECTOR UNIT.SDR CA040217008Control Cable · frayed(CAN) DURING SCHEDULED MAINTENANCE, IT WAS OBSERVED THAT THE LT IB FLAP ASSY WAS DROOPING. UPON FURTHER INVESTIGATION, THE CABLE ASSY WAS FOUND FRAYED AND BROKEN. A NEW CABLE ASSY WAS INSTALLED IAW MM 27-51-5 AND FUNCTIONED SERVICEABLE IAW MM 27-51-0. NO FURTSDR QXEA200400136Fcu · malfunctionedYYC FLIGHT 2329 AFTER DEPARTURE AIRCRAFT HAD FLAP POWER CAUTION MESSAGE. RAN CHECKLIST, LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED FCU. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR 04FDEA00399Control Valve · malfunctionedDURING FLAP RETRACTION AFTER TAKEOFF GOT FLAP DISAGREE ALERT. INBOARD FLAPS DID NOT RETRACT, STAYED AT 11; OUTBOARD LEFT INDICATED 5 AND OUTBOARD RIGHT INDICATED 6. QRH PROCEDURE ACCOMPLISHED. NOTE: TAKEOFF FLAP SETTING WAS 10.9. REMOVED AND REPLACED INBOSDR 58728Switch · stuckAFTER TAKEOFF FLAPS STUCK AT A PLACE IN BETWEEN 17 DEGREES & 34 DEGREES. CREW THEN DECIDED TO RETURN TO FIELD AND LANDED SAFELY WITH NO FURTHER INCIDENTS. CLEANED LT / RT SPLIT FLAP SWITCHES OPS CK NORMAL.SDR SWIA200412887Selector · malfunctionedRECEIVED A CONTROL FAULT WHEN SELECTING FLAPS FROM 15 TO 25. RESET IAW QRH. REPLACED FLAP SELECTOR SWITCH WITH SERVICEABLE UNIT. OPERATED FLAPS NUMEROUS TIMES, OPS CHECKS GOOD.SDR C1HA200478001Motor · inoperativeINBOARD TRAILING EDGE FLAPS WOULD NOT EXTEND HYDROLICLY OR ELECTRICALLY ON LANDING. FOUND INBOARD ALTERNATE FLAP MOTOR BINDING INSTALLED SERVICEABLE ALTERNATE FLAP MOTOR REF MM 27-51-141 PG 401-402. OPS CHECKED GOOD.SDR SWIA200412885Pdu · malfunctionedON APPROACH INTO DEN FLAPS FAIL CAUTION MESSAGE WHEN FLAPS ARE SELECTED FROM 0 TO 8 DEGREES. COMPLIED WITH QRH. REMOVED AND REPLACED POWER DRIVE UNIT. OPS CHECK GOOD. ALL WORK DONE IAW CRJ MM 27-52-01.SDR COMA0460127Fcu · malfunctionedFLIGHT 5131 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU.SDR A6WA200440020Drive Assy · failedFOUND FLAPS FAIL ON APPROACH FLAPS AT 30 DEGREES. REMOVED AND REPLACED 1 FLEX DRIVE CABLE AND 2 BPSU IAW MM 27-51-10. PERFORMED RIGGING AND OPS CHECK. OPS CHECK GOOD, S/N 5310, 0857.SDR A6WA20040020Controller · malfunctionedFLAPS FAIL ON APPROACH FLAPS AT 30 DEGREES. (M)SDR COMA0460126Warning Light · illuminatedFLIGHT 5027 FLAPS FAIL MESSAGE AFTER LANDING. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.SDR NACA20040010Bearing · seizedOUTBOARD FLAPS STUCK AT 3.5 DEGREES DURING FLAP RETRACTION. REPLACED BEARINGS IN RIGHT HAND OUTBOARD SEQUENCING CARRIAGE, SEQUENCING TOGGLES.SDR COMA0470019Control Unit · malfunctionedFLIGHT 5476 FLAPS HALF SPEED MESSAGE. REPLACED THE SFECU.SDR 04FDEA00313Motor · leakingDURING CLIMBOUT FROM EWR AT 25,000 FT CREW NOTICED A RAPID LOSS OF HYDRAULIC SYSTEM-A FLUID FOLLOWED PROPER CHECKLISTS AND RETURNED TO BASE. EVENTUALLY LOST ALL SYSTEM-A FLUID. FOUND HYDRAULIC FLUID POURING OUT OF CASE DRAIN OVERFLOW LINE FROM FLAP DRIVE MOTSDR A6WA200440018Bpsu · failedFLAP FAIL MESSAGE, PERFORMED ZERO FLAP LANDING, LANDED 165 KNOTS OW 45, 350 VSI 150 FPM FLAPS FAILED AS SOON AS HANDLE MOVED. REMOVED AND REPLACED LEFT BPSU AND FECU. (M)SDR 04035628Control Unit · faultyDURING APPROACH THE CREW REPORTED A FLAP SYSTEM FAILURE WITH FLAPS AT 0 DEGREE POSITION. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE FLAP ELECTRONIC CONTROL UNIT WAS FOUND FAULTY AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORSDR 04FDEA00296Rod End · corrodedFOUND OB FLAP, IB AFT HINGE ACTUATOR ROD END. HOLE IB (1) SPOT FACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75246. TRAILING EDGE & TRAILING EDGE DEVICES. RT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.SDR SWIA200412855Pdu · malfunctionedFLAPS 1/2 SPEED MESSAGE. REPLACED FLAP POWER DRIVER UNIT IAW MM 27-52-01-000-801. OPS CHECK GOOD.SDR COMA0470014Warning Light · illuminatedFLIGHT 5077 SLATS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE, FOUND NO FAULT CODES IN COMPUTER. SYSTEM OPERATION NORMAL.SDR COMA0460099Warning Light · illuminatedFLIGHT 5868 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.SDR A6WA200440015Flap · stuckON TAKEOFF, FLAPS STUCK AT 20 DEGREES. FECU INTERROGEAED NIL FAULTS FOUND. AIRCRAFT HANGARED 4.5 HOURS. FECU SYSTEM TESTED AS PER 27-51-05-946-009 JOB TASK. FLAPS CYCLED ALL POSITIONS, CHECKED SERVICEABLE. (M)SDR SWIA200412831Selector · malfunctionedON TOUCHDOWN, FLAPS 45 LANDING AND RECEIVED A CONTROL FAULT ALL LIGHT BARS FLASHING 0, QRH PROCEDURE DID NOT FIX. REPLACED FLAP SELECTOR LEVER ASSEMBLY WITH SERVICEABLE UNIT. FLAPS OPS CHECK GOOD.SDR COMA0460098Flap · failedFLIGHT 5712 FLAPS FAILED ON FINAL. C/W INSPECTION OF FLAP SYSTEM PER EO 27-046 AND AD 98-20-01.SDR SWIA200412823Flap · out of rigFLAPS FAIL AT 20 DEGREES AFTER TAKE-OFF. RIGGED FLAPS IAW 27-54-00. OPS. CHECK GOOD.SDR SWIA200412821Bpsu · malfunctionedFLAPS FAIL AT -0- WHEN SELECTED. REMOVED AND REPLACED RIGHT AND LEFT FLAP BPSU, LEFT FLAP ACTUATOR IN THE NUMBER 3 POSITION AND THE RIGHT NR 3 FLAP ACTUATOR. RIGHT BPSU S/N OFF: 0801, ACTUATOR P/N: 853D100-19, LEFT S/N OFF: 1945. RIGHT S/N OFF: 1941. OPS SDR SWIA200412828Fcu · out of rigAFTER TAKEOFF, SELECTED FLAP FROM 20 DEGREES TO 8 DEGREES AND GOT A FLAPS FAIL MESSAGE. RETURNED TO FAT. RE-RIGGED FECU IAW 27-51-10. OPS CHECK GOOD ON GROUND.SDR ANCF200400002Spring · brokenDURING APROACH WHEN EXTENDING SLATS, THE LEVER CAN NOT BE MOVED FROM UP/ RET POSITION. LANDING WAS MADE WITH FLAPS / SLATS RETRACTED AND 1.25 VS SPEED. SPRING DETENT HELICAL EXT WAS FOUND BROKEN IN CRANK OF THE FLAP LEVER. IT WAS REPLACED IAW AMM 27-50-00 PSDR DHL2004363002Gearbox · malfunctionedON APPROACH, FLAPS DID NOT EXTEND WITH FL 8 SELECTED. PERFORMED ABNORMAL PROCEDURE LANDED SL16/FL 0. ON TOUCHDOWN, FLAPS EXTENDED TO 8 DEGREES. CHECKED SERVICING ON THE FLAP CONTROL UNIT, DUPLEX AND SIMPLEX BEVEL GEARBOXES, TORQUE LIMITERS, DOWN DRIVE GEARBSDR SWIA200412815Pdu · malfunctionedON TAXI OUT, RECEIVED FLAPS HALFSPEED STATUS MESSAGE. REMOVED AND REPLACED FLAP PDU IAW MM 27-52-01. OPS CHECK GOOD. P/N 865D100-7, S/N ON 0831, S/N OFF 1036.
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