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 COMA0560578Pdu · malfunctionedFLIGHT 5013 - FLAPS FAIL CAUTION. REPLACED THE FLAP PDU.SDR ASOA05931Seal · leakingDURING APPROACH FROM PHF-ATL, THE FLAPS AT ZERO. THE CREW DECLARED AN EMERGENCY AND THE EMERGENCY VEHICLES WERE DISPATCHED. THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT IN ATL. MX REMOVED AND REPLACED THE FLEX SHAFT SEALS, LUBRICATED THE LEFT FLEX SHSDR 11022005ARelay · failedFLAPS STUCK AT 17 DEGREES. REMOVED AND REPLACED FLAP CONTROL RELAY OPS CHECK NORMAL, P/N SM50D7.SDR VNAA0510023Flap System · malfunctionedDURING APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WITH FLAPS AT 20 DEGREES SELECTED TO 30 DEGREES. THE CREW ABORTED THE APPROACH, RECONFIGURED THE AIRCRAFT, AND LANDED WITHOUT INCIDENT. MAINTENANCE RECORDED FECU LRU & FAULT LOG CONTENTS PER THE FIM.SDR SWIA200515769Fcu · malfunctionedFLAPS FAIL MESSAGE, AFTER TAKEOFF. RETURNED TO SLC. REPLACED FECU IAW MM 27-51-05. OPERATIONAL CHECK GOOD.SDR COMA0560577Flex Coupling · lack of lubeFLIGHT 4997 - FLAPS FAIL CAUTION. CLEANED AND LUBRICATED RT WING FLEX DRIVE CABLES.SDR SWIA200515764Pdu · malfunctionedFLAP DEGRADED MESSAGE, ON TAXI OUT. REPLACED FLAP PDU IAW MM 27-52-01, OPERATIONAL CHECK GOOD. P/N 865D100-7, S/N ON 0792, S/N OFF 1093.SDR COMA0560572Flap System · malfunctionedFLIGHT 5640 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR COMA0560570Bpsu · unreliableFLIGHT 5267 - FLAPS FAIL CAUTION. REPLACED THE RT BPSU.SDR SIMA200530108Flap System · stuckCREW REPORTED AFTER TAKEOFF DURING FLAP RETRACTION THEY RECEIVED A FLAP FAIL MESSAGE. REPLACED RT FLAP TRANSMISSION BRAKE. OPERATIONAL CHECK GOOD, AC RETURNED TO SERVICE. (K)SDR SWIA200515741Position Sensor · malfunctionedFLAPS FAIL CAUTION MSG. INSTALLED SERVICEABLE BPSU IAW 27-56-00. ALSO ADJUSTED FECU POTS, OPERATIONAL CHECK GOOD.SDR MASA200500869Bpsu · malfunctionedASH 6383 DSM - FLAP FAIL AT 8DEG. MAINTENANCE REPLACED THE BPSU.SDR COMA0560564Bpsu · failedFLAPS FAIL CAUTION. CND REPLACED THE RT BPSU.SDR MASA200500880Flap System · failedASH 6022 FAT - FLAP FAIL IN FLIGHT AT 0 DEGREES. MAINTENANCE RESET THE FLAP SYSTEM AND COMPLIED WITH PART A OF FLAP FAIL INSPECTION.SDR 05FDEA03476Flap System · malfunctionedUPON CONFIG, A/C ROLLED LEFT REQ 3/4 DEFLECTION TO RIGHT TO HOLD A/C LEVEL. A/C WAS CONTROLLABLE TO TOUCHDOWN. ON POST FLIGHT WALK AROUND, DISCOVERED THAT THE MIDDLE OF THE LEFT OUTBD FLAP VANE HAD DEPARTED THE A/C. REMOVED RT INBD FLAP SPRING CARTRIGDE. RESDR MASA200500817Control Unit · failedASH 7100 ORD, FLAPS FAILED AT 20 DEG. MX R2 FLAP CONTROL UNIT.SDR COMA0560562Pdu · malfunctionedFLIGHT 5582 - FLAPS FAIL CAUTION. CND REPLACED THE PDU FOR TROUBLESHOOTING.SDR UPS05845642Flap System · splitRIGHT HAND INBD FLAP OUTBD HINGE BRACKET COVER FWD PANEL CRACKED. INSTALLED INTERIM AIRWORTHY PANEL IAW EO DC8-5720-23117-A. DEFERRAL D312507 PER EO. REPLACED PANEL IAW MM 57-30. THIS CLEARS D312507.SDR VNAA0510013Flap System · malfunctionedON APPROACH WITH FLAPS AT 20 DEGREES, THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WHEN SELECTING FLAPS 30 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED SAFELY. MAINTENANCE RESET AND OPERATIONALLY CHECKED THE FLAP SYSTEM IAW CRJ200 AMM 27-54-00-710-801. OPS CSDR COMA0560559Drive Assy · dirtyFLAPS FAIL CAUTION. CND, FOUND NO DEFECTS IN FLAP SYSTEM, CLEANED AND GREASED FLEX DRIVE CABLES.SDR SWIA200515691Sensor · malfunctionedRECEIVED A -FLAP FAIL CAUTION MSG- WHEN FLAPS WERE SELECTED TO 30 DEG ON APPROACH. REPLACED RT BPSU IAW AMM 27-51-10. OPERATIONAL CHECK GOOD.SDR REXA200500133Flap System · failedFLAPS FAILED ON APPROACH, FOLLOWED QRH WITH UNEVENTFUL LANDING. SYSTEM RESET AND PLACED ON 72 HOUR MONITOR PER AD 98-20-01.SDR SWIA200515727Detector · malfunctionedRECEIVED FLAPS FAIL CAUTION MESSAGE ON TAXI OUT. REPLACED RIGHT FLAP PDU BRAKE MOTOR IAW AMM 27-52-00, OPERATIONAL CHECK GOOD. P/N ON 601R59014-1, S/N OFF A568.SDR COMA0560557Flap System · malfunctionedFLIGHT 5711- FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR DXTA200501029Warning Light · illuminatedWHILE DESCENDING TO LAND, WITH NO FLAPS OR SLATS EXTENDED, RECEIVED AN AMBER FLAP FAIL MESSAGE ALONG WITH THE FLAPS INDICATING FLAPS 15 DEGREES WHEN UP. FOLLOWED EMERGENCY CHECKLIST. LANDED WITH SLATS EXTENDED ONLY. COULDN'T RETRACT AFTER LANDING. ITEM IS SDR COMA0560555Pdu · malfunctionedFLIGHT 5876 - FLAPS FAIL. REPLACED THE PDU.SDR VNAA0510010Flap System · malfunctionedTHE FLAPS FAIL CAUTION MESSAGE ILLUMINATED ON APPROACH WITH FLAPS 20 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED SAFELY. MAINTENANCE INSPECTED THE FLAP SYSTEM AND RESET THE FECU IAW CRJ200 FIM 27-50-00. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELESDR QXEA200501353Warning Light · illuminatedSEA - FLIGHT 2390 FLAP POWER CAUTION LIGHT ILLUMINATED. MAINTENANCE COMPLIED WITH FIM TASK 27-50-00-810-802. RESET CONTINUOUS BIT FAULT, CYCLED FLAP C/B. COMPLIED WITH Q400 AMM TASK 27-50-00-710-801. OPERATIONAL TEST OF WING FLAPS. NO FURTHER FAULTS OR CASDR S2YA05066CFlex Drive · damagedSHORTLY AFTER TAKEOFF, THE CREW REPORTED THE FLAPS WERE AT 17 DEGREES AND WILL NOT RETRACT. THE AC CONTINUED WITH THE FLAPS AT 17. THE FLAPS WERE RAISED USING THE OVER RIDE SWITCH AND THE SYSTEM WAS PUT ON MEL. DISCOVERED THE FLAP MOTOR/GEAR BOX STRUGGLING SDR S2YA05066BFlex Drive · damagedSHORTLY AFTER TAKEOFF, THE CREW REPORTED THE FLAPS WERE AT 17 DEGREES AND WILL NOT RETRACT. THE AC CONTINUED WITH THE FLAPS AT 17. THE FLAPS WHERE RAISED USING THE OVER RIDE SWITCH AND THE SYSTEM WAS PUT ON MEL. DISCOVERED THE FLAP MOTOR/GEARBOX STRUGGLING SDR S2YA05066AGearbox · damagedSHORTLY AFTER TAKEOFF THE CREW REPORTED THE FLAPS WERE AT 17 DEGREES AND WILL NOT RETRACT. THE AC CONTINUED WITH THE FLAPS AT 17. THE FLAPS WHERE RAISED USING THE OVER RIDE SWITCH AND THE SYSTEM WAS PUT ON MEL. MX DISCOVERED THE FLAP MOTOR/GEAR BOX STRUGGLISDR S2YA05066Motor · damagedSHORTLY AFTER TAKEOFF, THE CREW REPORTED THE FLAPS WERE AT 17 DEGREES AND WILL NOT RETRACT. THE AC CONTINUED WITH THE FLAPS AT 17. THE FLAPS WERE RAISED USING THE OVERRIDE SWITCH AND THE SYSTEM WAS PUT ON MEL. DISCOVERED THE FLAP MOTOR/GEAR BOX STRUGGLING TSDR 2005UALA01138Flap System · malfunctionedLANDED ORD UNDER AMBER ALERT DUE TO TRAILING EDGE FLAP INDICATION PROBLEM.SDR COMA0560551Control Unit · malfunctionedFLIGHT 5033 - FLAPS FAIL CAUTION. REPLACED THE FECU.SDR COMA0560547Bpsu · unreliableFLIGHT 5074 - FLAPS FAIL CAUTION. REPLACED THE RIGHT BPSU.SDR 2005FA0001457Transmitter · out of adjustFLAP ASYMMETRY ANNUNCIATOR ILLUMINATED DURING APPROACH. FOUND MIDBOARD ASYMMETRY DETECTOR READING 5.7 VOLTS. FOUND IB ASYMMETRY DETECTOR READING 7.8 VOLTS. ADJUSTED LT AND RT FLAP POSITION TRANSMITTERS AS REQUIRED IAW MM TO BRING VOLTAGES TO 5.8 VOLTS +/- 0SDR COMA0560546Bpsu · malfunctionedFLIGHT 5505 - FLAPS FAIL CAUTION. REPLACED THE RIGHT BPSU.SDR COMA0560545Flap System · malfunctionedFLIGHT 5400 - FLAPS FAIL CAUTION. CND, INSPECTED FLAPS SYSTEM AND FOUND NO FAULTS.SDR COMA0560543Control Unit · malfunctionedFLIGHT 5682 - FLAPS FAIL CAUTION. REPLACED THE FECU.SDR COMA0560542Flap System · malfunctionedFLIGHT 5707 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR COMA0560541Warning Light · illuminatedFLIGHT 5093 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR SWIA200515682Fcu · malfunctionedFLAPS FAIL CAUTION MESSAGE WITH OVERSPEED CLACKER FLAPS WERE IN THE 0 DEGREE DETENT POSITION. REPLACED FECU IAW MM 27-51-05, OPERATIONAL CHECK GOOD.SDR COMA0560536Flap System · malfunctionedFLIGHT 5605 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR S2YA05065BRelay · failedFLAPS FAILED TO EXTEND, SYS WAS MEL`D. MEL WAS CLEARED WHEN MX INS SYS, OPS CHECKED, COULD NOT DUPLICATE DISCREPANCY. TROUBLESHOOTING REPLACED FLAP MOTOR AND FLAP POSITION RELAY (K105). SHORTLY AFTER TAKEOFF CREW REPORTED FLAPS WERE AT 17 DEGREES AND WILL NSDR S2YA05065AGearbox · failedFLAPS FIALED TO EXTEND, SYS WAS MEL`D. MEL WAS CLEARED WHEN MX INSP SYS, OPS CHECKED, COULD NOT DUPLICATE DISCREPANCY. TROUBLESHOOTING REPLACED FLAP MOTOR, FLAP POSITION RELAY (K105). SHORTLY AFTER TAKEOFF CRWE REPORTED FLAPS WERE A T 17 DEGREES AND WOULD NSDR S2YA05065Motor · malfunctionedFLAPS FAILED TO EXTEND, SYS WAS MEL`D. MEL WAS CLEARED WHEN MX INSP SYS, OPS CHECKED IT, COULD NOT DUPLICATE DISCREPANCY. TROUBLESHOOTING REPLACED FLAP MOTOR AND FLAP POSITION RELAY (K105). SHORTLY AFTER TAKEOFF CREW REPORTED FLAPS WERE A 17 DEGREES AND WILSDR CA051007003Bellcrank · corroded(CAN) DURING A ROUTINE DAILY CHECK,IT WAS NOTED THAT THE LT OB T/E FLAP HAD EXCESSIVE PLAY WHEN HAND FORCE WAS APPLIED TO THE TRAILING EDGE FLAP. UPON FURTHER INVESTIGATION IT WAS DISCOVERED THAT THE CLEVIS BOLT AND THE BELLCRANK WERE WORN AND CORRODED. BELLSDR COMA0560534Flap System · malfunctionedFLIGHT 5096 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR COMA0560532Flap System · malfunctionedFLIGHT 5093 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR SWAA053027Control Cable · brokenLT WING INBD T/E FLAP BOOM CABLE BROKEN. REMOVED AND REPLACED BOOM CABLES BC-3 AND BC-4 PER MM.
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