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 SWAA2014012324453Flap · out of adjustRT WING INBD AFT FLAP OUT OF ADJUSTMENT. ADJUSTED AFT FLAP IAW AMM.SDR REXA2014011900123Flap · failedFLAP FAILED DURING RETRACTION. PERFORMED TROUBLESHOOTING IAW FIM REV 45 IAW AD 2009-06-12 PARAGRAPH H 6 I, AMOC DATED JULY 22, 2013 & PA AD 27-052N. ALS 2576584-2 FOR REMOVAL & INSTALLATION OF FECU.SDR CALA2014012090179Yoke · wornLT FLAPERON REPLACEMENT OTBD ACTUATOR YOKE ASSEMBLY HAS INTERNAL COATING WORN AND MISSING CAUSING EXCESSIVE PLAY IN YOKE. INSTALLED YOKE ASSEMBLY INTO SUPPORT STRUCTURE IAW AMM 27-11-12.SDR FDEA201401150106Fseu · malfunctionedLEADING EDGE SLAT ASYM ON TAKEOFF, OCCURRED AT WEIGHT OFF WHEELS ON TAKEOFF ROTATION. IAW AML 1565931 REPLACED NR 1 FSEU IAW MM 27-51-01-2. REPLACED RT INBD SLAT LOSS SWITCH IAW MM 27-81- 41-4. OPERATIONS CHECKED BAD, SUSPECT OUT OF ADJUSTMENT.SDR REXA2014011400120Shaft · malfunctionedFLAPS FAILED AT 30 WITH HANDLE AT 45. INSPECTED FLAPS, RESET & DEFERRED. PREFORMED TROUBLESHOOTING IAW FIM REV 45 IAW AD2009-06-12 PARAGRAPH H G I AMBC DATED JULY 22, 2013 & PA AD27-05-052N. PREFORMED LUBE OF RT FLAP SYS IAW CHECKLIST. R & R NR 3 & NR 5 RT SDR SWIA201435975Flap · dirtyAFTER SELECTING FLAPS 45 & AN INDICATION OF FLAPS 45 IS SEEN, A BUMP COULD BE BARELY FELT IN THE YOKE ALONG WITH A SUBSEQUENT ROLL TO THE RIGHT. AIRCRAFT REQUIRES 50% LT AILERON TRIM TO MAINTAIN WINGS LEVEL ATTITUDE AT APPROACH SPEED. FLT 1300 THOROUGHLY CLESDR SWIA201435974Flap · contaminatedSIGNIFICANT LT WING DOWN ROLL AFTER SELECTING FLAPS 45, REQUIRES AT LEAST 1/2 OF LT WING DOWN AILERON TRIM. FLT 4820 FOUND SIGNIFICANT SAND & GREASE ON LT & RT FLAPS, MORE SO ON LT FLAP LE. CLEANED BOTH FLAPS,SDR UHLA2014010700004Flap System · failedFLAP FAILED ON APPROACH, SLATS -3, FLAPS -0. UNABLE TO GET FLAPS/SLATS RESET WITH QRH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. INSPECTED FLAPS/SLATS ROLLERS, TRIP INDICATORS, SKEW SENSORS, LINKAGES. PERFORMED MULTIPLE OPS CHECKS, NO DEFECTS OR MESSAGESDR REXA2014010600110Torque Shaft · faultyAFTER LANDING DURING FLAP RETRACTION WE GOT A FLAPS FAIL AMBER EICAS MESSAGE. FLAPS REMAINED AT 45, AIR TEMP WAS -28 C, AIRSPEED WAS 0, TIME INTO FLIGHT WHEN FAILURE HAPPENED WAS 1:16. TROUBLE SHOT IAW BOMB FIM REV 45 IAW AD 2009-06-12 PARA H 6I, AMOC DATED SDR A6WA201401074053Flap · failed4097 ON APPROACH, FLAP FAILED AT ZERO, OAT 27. PERFORMED FLAP RESET PROCEDURE IAW AMM SUPP 98-18F, BOX 12. FLAPS RESET, PLACARD PLACE DON MEL.SDR SIMA20140104005Control Unit · faultyFLAP LOW SPEED EIAC DURING APPROACH. R & R FECU IAW AMM 27-53-07, OPERATIONS CHECKED GOOD.SDR SIMA20140104003Flap · malfunctionedNUMBER 1 FLAP FAIL CAUTION MESSAGE ON APPROACH FLAPS. CAME IN AT 0 AFTER SETTING FLAPS 9. ACFT REQUIRES INSPECTION FOR FERRY FLIGHT. THIS ACFT HAS BEEN INSPECTED TO THE EXTENT NECESSARY FOR A FERRY FLIGHT & FOUND TO BE IN A SAFE CONDITION FOR A FERRY FLIGHTSDR USAA2014010600045Unknown · malfunctionedPHL - FLT 1804 EN-ROUTE PHX TO PHL. FLAPS FAILED TO MOVE. TE LIGHT ON & EICAS MESSAGE TE FLAP DISAGREE DISPLAYED. FLAPS ALSO INOPERATIVE ON TE ALTN SYS. ACCOMPLISHED OPERATIONAL TEST OF THE TE EDGE FLAPS, COULD NOT DUPLICATE, INSPECTED FLAPS & NO FAULTS FOSDR CA140103003Flap System · failedFLAP FAIL CAS MESSAGE POSTED ON TAKEOFF ROLL AROUND 80 KNOTS. TAKEOFF WAS ABORTED AND ACFT TAXI BACK TO FBO. COULD NOT RESET FLAPS WITH THE FLAP RESET SWITCH. POWER DOWN ACFT AND BACK UP. FLAPS STILL WOULD NOT RESET.SDR WAIA2014010700036Flap System · frozenDURING APPROACH, CALLED FOR "FLAPS 8". "FLAPS FAIL" EICAS CAUTION MESSAGE DISPLAYED. APPROACH ABANDONED AND CREW RAN CHECKLIST. AN EMERGENCY WAS DECLARED AND FLIGHT PROCEEDED. LANDING WAS UNEVENTFUL. MFG HAS BEEN AWARE OF FLAP MALFUNCTION DURING COLD WSDR SIMA20140101003Flap · malfunctionedON FLIGHT 3578 DURING NR 1 ON APPROACH CREW REPORTED FLAP FAIL MESSAGE ON EICAS. DECLARED EMERGENCY & RAN AOM VOL 1 PROCEDURE LANDED FLAP 0. ACFT REQUIRES INSPECTION FOR FERRY FLIGHT. ACFT HAS BEEN INSPECTED TO THE EXTENT NECESSARY FOR A FERRY FLIGHT & FOUNSDR CALA2014010290016Fseu · malfunctionedFLAP SLAT SENSOR CB POPPED. REPLACED FSEU 1 IAW AMM 2 7-51-01. ALL TESTS PASSED.SDR AMPA2014F00019Control Unit · defective"FLAP LOW SPEED" EICAS MESSAGE DISPLAYED DURING CLIMBOUT AT APPROXIAMTELY 1,000' AGL FOLLOWED BY "FLAP FAIL" EICAS MESSAGE. FLAP SYSTEM OPERATION COMPLETELY INHIBITED. ACFT DIVERTED AND LANDED WITHOUT INCIDENT. FAULTY FECU, PN 363100-1011, SN 5282 WAS CONFISDR DXTA2013122702609Flap System · malfunctionedAFTER TAKEOFF, WHEN FLAPS WERE SELECTED TO 0, FLAPS STUCK AT 7 DEGREES. ON GROUND FLAP HANDLE SELECTED TO 35 DEGREES & STUCK AT 35 DEGREES. REPLACED THE LT FLAP ACTUATOR ASSEMBLY, LT FLAP OUTBOARD BELLCRANK ASSEMBLY AND LT FLAP OUTBOARD BELLCRANK BOLT. SYSTSDR CALA2013122693948Flap · vibrationPER FLIGHT CREW VIBRATION FELT WHEN FLAP SELECTED TO POSITION 3, WITH GEAR DOWN FOR LANDING. LOWER FLAPS & CAREFULLY INSPECT THE TOP & BOTTOM OF FLAP CUSHIONS & SEALS BETWEEN INNER & OUTER FLAPS IAW TSM 27-54-00-810-801.SDR UHLA2013122300694Warning Message · false activationFLAP FAIL MESSAGE ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOLLOWED FIM TASK 27-53-00-810-813A, CLEARED INHIBITS, MESSAGE CLEARED. FLAPS OPERATIONAL AT THIS TIME. INSPECTED FLAP ACTUATORS, NO DEFECTS NOTED AT THIS TIME.SDR CALA2013122393891Fseu · malfunctionedSTATUS MESSAGE FLAP SLAT ELECTRICAL. STAB POSITION CARD M838 & FLAP SLAT ELECTRICAL UNIT AT FAULT. R & R STAB MODULE & FLAP SLAT MODULE IAW 27-51-01, 27-58-01. SYS OPERATIONS CHECKED GOOD. ALSO PERFORMED TEST 30 ALL SYS PASSED.SDR CA131223006Arm · cracked(CAN) FLAP ARM FOUND CRACKED DURING ROUTINE MAINTENANCE.SDR CA131223008Arm · cracked(CAN) FLAP ARM FOUND CRACKED DURING ROUTINE MAINTENANCE.SDR CA131223007Arm · cracked(CAN) FLAP ARM FOUND CRACKED DURING ROUTINE MAINTENANCE.SDR CALA2013122393871Warning System · false activationTE FLAP DISAGREE EICAS ILLUMINATED WHEN FLAP LEVER MOVED FROM 20 TO 25 FLAPS. TROUBLE SHOT IAW FIM 27-51 PG 135 & FOUND A RT FLAP TRANSMITTER WIRE FAULT ON THE 2 FSCU. SWAPPED THE 2 & 3 FSCU. PERFORMED BITE TEST & HAVE NO MORE FAULTS. DID CHECK THE CP ON TSDR SWIA201335716Fcu · failedRECEIVED CONTROL FAULT WHEN SELECTING FLAPS 25. RAN QRH PROCEDURE, LANDED FLAPS 15. FLT 6359 REPLACED FCU IAW AMM PN 347200-1001, SN ON 0253 & SN OFF 0140.SDR CHQA20131219456Transmission · faultyCREW REPORTED THAT THEY RECEIVED A FLAP FAIL MESSAGE ON APPROACH. THE CREW FOLLOWED THE QRH & DECLARED AN EMERGENCY. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE ACFT WAS FOUND SAFE FOR FERRY FLIGHT TO KSDF. SDF MX REPLACED THE LT & RT FLAP TRANSMISSION SDR CHQA20131219455Transmission · faultyCREW REPORTED THAT THEY RECEIVED A FLAP FAIL MESSAGE ON APPROACH. THE CREW FOLLOWED THE QRH & DECLARED AN EMERGENCY. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE ACFT WAS FOUND SAFE FOR FERRY FLIGHT TO KSDF. SDF MX REPLACED THE LT & RT FLAP TRANSMISSION SDR CA131223010Arm · cracked(CAN) WHILE COMPLETING AN ANNUAL INSPECTION OF THE ACFT AND INSPECTING THE FLAP SYSTEM GENERAL INSPECTION A CRACK WAS NOTED ON THE LT INBD FLAP DRIVE ARM IN THE WEB RADIUS. THE CRACK WAS CLEARLY VISIBLE WITHOUT THE NEED FOR NDT. THE DRIVE ARM WAS R & R WITH ASDR CA131219011Torque Tube · misinstalled(CAN) THE FLAP TORQUE TUBE WAS FOUND NOT PROPERLY CONNECTED TO THE POWER DRIVE UNIT (PDU) SPLINE SHAFT HOLE.SDR CALA2013122393869Circuit Breaker · faultyALT FLAP POWER CB AT D24ON P6 PANEL POPPED. REPLACED CB P6D24 IAW MM STANDARD PRACTICE 20-60-00 SATIS. PN OUT BACC18AE15, PN IN BACC18AE15. FSEU BITE TEST PERFORMED IAW MM 27-51-00-735- 080 WITHOUT REMARKS, OK. FSPM BITE TEST PERFORMED IAW MM 27-51-00 -73SDR CALA2013121993795Fseu · failedSLAT PRIMARY FAIL EICAS ADVISORY MESSAGE, CYCLED FLAPS & MESSAGE RETURNED. SLATS RETRACTED IN THE SECONDARY MODE. REPLACED NR 2 FSEU IAW AMM, OPERATIONS CHECKED NORMAL. NO FAULTS OR EICAS MESSAGES.SDR CA131218025Flap System · failed(CAN) CREW EXPERIENCED A FLAP FAIL AT 0 DEGREES WHEN SELECTING 8 DEGREES. THE CREW DECLARED AN EMERGENCY AND REQUESTED PRIORITY FOR LANDING. THE ACFT LANDED SAFELY. THE FLAP SYS WAS RESET IAW AD 2009-06-12.SDR CA131218008Circuit Breaker · melted(CAN) AFTER TAKEOFF, 10 MINUTES INTO FLIGHT SMOKE IN COCKPIT. RETURNED TO DESTINATION OF TAKEOFF. UPON MAINTENANCE INVESTIGATION FOUND SEVERAL WIRES MELTED FROM THE FLAP MOTOR SYSTEM. FURTHER INVESTIGATION REQUIRED, WILL UPDATE AT A LATER DATE. INITIAL INVESDR CA131216014Flap System · malfunctioned(CAN) ON APPROACH, CREW REPORTED A FLIGHT CONTROL FLAP LOCKED. CREW DECLARED AN EMERGENCY WITH ATC. PERFORMED TSM TASK 27-51-00-810-818A. OPS CK OK, NO FAULTS FOUND. OPS TEST OF FLAP SYS IAW AMM 27-54-00-710-001A. TEST OK.SDR FDEA201312142981Jackscrew · lack of lubeON APPROACH, FLAPS DID NOT EXTEND. FLAPS SYS 1 & SYS 2 FAULT LIGHTS ILLUMINATED UPON MOVING FLAP HANDLE TO ANY EXTENDED POSITION. ALTITUDE 6200 FEET AT KGTF, TEMP -5C. RELIEVED LOAD ON LT FLAPS THEN RESET LT FLAP TO LIMITER. RT LIMITER OK IAW A310-300 AMMSDR 2013FA0000748Bracket · crackedFOUND THREE CRACKED BRACKETS.SDR REXA2013121302402Flap · failedFLAPS FAIL CAUTION MESSAGE. DEFERRED, PERFORMED TROUBLESHOOTING IAW FIM REV 45, IAW AD 2009-06-12 PARAGRAPH H 6 I AMOC DATED JULY 22, 2013 & PA AD 27-052N. SEE CORRECTIVE ACTION FOR LOG PAGE 2537736-2. THIS CLEARS DMI 020289 PLACARD REMOVED.SDR AALA20131211010Control Rod · bentDFW CREW REPORTED FLAP ASYMMETRY. FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND RT TE CONTROL ROD BENT. REPLACED DRIVE ROD ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.SDR REXA2013121102297Flap · failedFLAPS FAILED AT 2 DEG ON APPROACH. PERFORMED RESET & OPERATIONS CHECKED IAW AD 2009-06-12 PARA H-6 SEE DISC NR 2 FOR MEL DEFERRAL.SDR SIMA20131211003Shroud · defectiveON FLIGHT 3398 CREW REPORTED AFTER TAKEOFF RETRACTING FLAP FROM 18 TO 9, RECEIVED A FLAP FAIL MESSAGE WITH FLAP STUCK AT 11. THE CREW DECLARED EMERGENCY & THE ACFT WAS REMOVED FROM SERVICE. AFTER REPLACEMENT OF LT INBD FLAP EXTERNAL SHROUD DRIVER ON NRWC 819SDR FWTA201312110006Unknown · malfunctionedTRAILING EDGE FLAP SYS EICAS MESSAGE, TE FLAP DISAGREE, DISPLAYED, TE LIGHT ON. WHEN ANY TE FLAP POSITION SELECTED, FLAPS FAIL TO MOVE TO SELECTED POSITION. TE FLAP SYSTEM EICAS MESSAGE, TE FLAP SHUT DOWN, DISPLAYED. DECLARED EMERGENCY, FOLLOWED NO NORMAL LSDR CALA2013121793763Flap System · malfunctionedDIVERSION DUE TO LE SYMMETRY ISSUE COUPLED WITH MAIN FLAPS UNABLE TO ADVANCE BEYOND 20 DEGREES. IN THIS CONDITION AIRCRAFT IS UNABLE TO EXECUTE A AUTO LAND AS REQUIRED IAW FOM FOR CONDITIONS AT ETA.SDR CALA2013120993544Fseu · faultyTE FLAP DISAGREE TROUBLESHOOT DUE TO RECENT REPORTS OF TE FLAP DISAGREE EICAS MESSAGE. REPLACED FSEU WITH A 285T0049-63 IAW AMM 27-51-01.SDR CA131206002Flap System · inoperative(CAN) FLAP SYSTEM INOPERATIVE, FOUND ON MORNING WALK AROUND. PILOT CYCLED FLAPS AND WHEN FLAPS WHERE RETURNED TO ZERO, THE FLAP PRIMARY MOTOR COULD BE HEARD RUNNING. FLAP SYSTEM WOULD NOT FUNCTION IN EITHER PRIMARY OR STANDBY SYSTEM.SDR CALA2013120693516Fseu · faultyWITH FLAP HANDLE AT 5R FLAP IND 1 & LT FLAP IND 5. R & R FLAP SLAT ELECTRONIC UNIT IAW MM. PERFORMED BITE TEST IAW FIM 27-51-00 FIG 104, ALL SYSTEMS CHECKED GOOD. CYCLED FLAPS SEVERAL TIMES. NO DEFECTS NOTED AT THIS TIME, OPERATIONS CHECKED GOOD.SDR CALA2013120693507Strut · defectiveFLAPS LOCKED ALIGNMENT FAULT DISPLAYED ON UPPER ECAM SCREEN. ECAM AFTER LANDING WHEN FLAPS SELECTED UP, WAS ABLE TO DUPLICATE FLAP LOCKOUT PROBLEM. HAD FLIGHT CONTROL FLAPS LOCKED ECAM MESSAGE WITH AMBER INDICATION ON FLAPS. IAW TSM 27-51-00-810-818 SUSPECTSDR QMLA2013120413172Flap · malfunctionedON APPROACH TO LANDING BELOW 163 KIAS SELECTED FLAP POSITION TO 15 DEGREES. FLAPS FAILED TO MOVE, MASTER CAUTION & AMBER FLAP CAWS LIGHT ILLUMINATED. COMPLETED NO FLAP LANDING WITHOUT FURTHER INCIDENT.SDR UHLA2013113000616Control Unit · out of rigFLAP FAIL MESSAGE ON APPROACH, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. TROUBLESHOT IAW FIM 27-51-00-810-804. PERFORMED FLAP ELECTRONIC RIGGING IAW AMM 27-50-00, MESSAGE CLEARED, OPS CHECK GOOD.
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