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 COMA0460652Bpsu · malfunctionedFLIGHT 5841- FLAPS FAIL CAUTION MESSAGE DURING TAXI. REPLACED THE LEFT BPSU.SDR COMA0460650Bpsu · malfunctionedFLIGHT 5815 - FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU.SDR A6WA200440194Control System · malfunctionedON APPROACH TO LANDING FLAPS FAILED AT 0 DEGREES UPON FLAP SELECTION TO 8 DEGREES. PLACED ON 72 FLAP WATCH C/W AWAC SUPPLEMENT 01-05. RESET FLAPS. NO DAMAGE NOTED.SDR SWIA200414132Fcu · malfunctionedRECEIVED FLAP CONTROL FAULT MESSAGE WHEN SELECTING FLAPS 15. REMOVED AND REPLACED FCU AND LEFT NACELLE ACTUATOR. REFERENCES A/C MM (27-50-08) (27-50-06) OPERATIONAL CHECK GOOD. P/N 347200-1001, S/N OFF 3039, P/N 308200-1007, S/N OFF 016.SDR SWIA200414157Control Unit · malfunctionedIN FLIGHT HAD CONTROL FAULT FLAP WARNING INDICATION. REMOVED AND REPLACED FLAP CONTROL COMPUTER IAW MM 27-50-06. OPERATIONAL CHECK GOOD.SDR SWIA200414119Actuator · malfunctionedFLAPS FAIL CAUTION MESSAGE. REPLACED LEFT OUTBOARD FLAP OUTBOARD ACTUATOR IAW 27-53-05. OPERATIONAL CHECK GOOD.SDR DXTA200400453Warning System · activatedAFTER TAKEOFF, SELECTED FLAPS UP, FLAPS WERE AT ZERO. THE AMBER YD FAIL A-B, CAS MESSAGE ILLUMINATED ON THE CONTROL PAGE. IT SHOWED THE UPPER FAILED TO THE RIGHT OF THE AVAILABLE GREEN LIMIT. SELECTED THE UPPER BUTTON AND THE CAS WENT OUT, UPON LANDING DID SDR 04324648Fcu · malfunctionedEVENT SUMMARY ON 11/19 STATED FLAP FAIL AT 0 DEGREES, EMERGENCY DECLARED, LANDED WITHOUT COMPLICATIONS. INTEROGATED FECU FAULTS 1 JAM, 2 PDU DIFF, 3 UNSPECIFIED. CLEARED FAULTS. OPS CHECK GOOD AT THIS TIME REF 27-51-00.SDR REXA04034Flap · out of rigFLAPS FAIL ON LANDING. SYSTEM RE-RIGGED IAW AMM 27-54-00, OPERATIONALLY CHECKED GOOD.SDR COMA0460633Bpsu · faultyFLIGHT 5304 RECEIVED A FLAP FAIL CAUTION MESSAGE DURING TAXI OUT. AIRCRAFT RETURNED TO THE GATE. REPLACED THE LEFT BPSU.SDR COMA0460634Bpsu · faultyFLIGHT 5304 RECEIVED A FLAP FAIL CAUTION MESSGE DURING TAXI OUT. AIRCRAFT RETURNED TO THE GATE. REPLACED THE RIGHT BPSU.SDR A6WA200440192Flap · malfunctionedFLAPS FAIL CAS AND FLAPS STUCK AT 20 DEGREE ON APPROACH. RESET FLAP SYSTEM IAW AWAC SUPPLEMENT 98-18. NO FURTHER DISCREPANCIES.SDR A6WA200440187Flap · stuckFLAPS FAIL CAS AND FLAPS STUCK AT 20 DEGREES ON APPROACH. RESET FLAPS SYSTEM IAW SUPPLEMENT 98-18, NO FURTHER DISCREPANCIES.SDR ASAA0410535Jackscrew · chafedOKC - FOUND RIGHT WING OUTBOARD MID FLAP BEHIND OUTBOARD JACKSCREW IS CHAFED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLED BLENDED AREA IAW AS AND AAR EA. (M)SDR COMA0460627Bpsu · malfunctionedFLT 5497 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU.SDR REXA04032Control System · malfunctionedFLAPS FAILED AT ZERO ON APPROACH WHEN SELECTED TO THIRTY. QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01.SDR REXA04031Controller · malfunctionedFLAP FAILS AT ZERO WHEN SELECTED TO 20 ON APPROACH. QRH FOLLOWED EMERGENCY DECLARED, UNEVENTFUL LANDING. SYSTEM RESET, PLACED FLAPS ON 72 HOUR WATCH IAW AD 98-20-01.SDR COMA0460624Drive Shaft · malfunctionedFLIGHT 5488 FLAPS FAIL CAUTION MESSAGE. REPLACED THE NR 3 FLEX DRIVE SHAFT.SDR SWIA200414114Control Unit · malfunctionedAFTER TAKEOFF FLAPS OUTBOARD WOULD NOT RETRACT, RETURNED TO FIELD. REPLACED FLAP CONTROL UNIT IAW EMB 120 MM 27-50-60. OPERATIONAL CHECK GOOD.SDR COMA0460619Drive Shaft · malfunctionedFLIGHT 5606 FLAPS FAILED CAUTION MESSAGE. REPLACED THE NR 3 FLEX DRIVE SHAFT.SDR SWIA200414103Controller · malfunctionedSPLR/STAB FAULT, RUD LIMITER FAULT & PITCH FEEL FAULT DISPLAYED ON EICAS. REMOVED AND REPLACED SFECU NR 1 IAW CRJ MM 27-51-05. COMPLIED WITH SLAT/FLAP AUTO RIG AS REQUIRED. OPERATIONAL CHECK GOOD.SDR QXEA200400770Power Unit · failedPDX - FLIGHT 2309 - THE FLIGHT RETURNED TO FIELD AFTER THE CREW RECEIVED A FLAP DRIVE CAUTION DURING CLIMB. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE FLAP POWER UNIT. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR MALA040727Controller · malfunctionedFLAP FAULT CWP ILLUMINATES WHEN EXTENDING FLAPS UNTIL FLAPS REACH SELECTED POSITION. AIR RETURN TO MEM. MAINTENANCE REMOVED AND REPLACED FLAP CONTROLLER PN 8519M3, SN/OFF 555, SN/ON 057, IAW SMM CHAP 27-51-1.SDR COMA0460610Warning Light · illuminatedFLIGHT 5816 FLAPS FAILED CAUTION MESSAGE. COULD NOT DUPLICATE. INSPECTED FLAP SYSTEM IAW AD 98-20-01.SDR SIMA200431701Brake · malfunctionedDURING APPROACH TO LGA WHEN CREW SELECTED FLAPS THE FLAPS FROZE WOULD NOT MOVE FROM 0 DEGREES. MAINTENANCE REMOVED AND REPLACED THE LT AND RT FLAP TRANSMISSION BRAKES IAW MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RELEASED FOR A FUNCTIONAL CHECSDR ASOA04897Bpsu · malfunctionedDURING CLIMB-OUT, AT APPROXIMATELY 18,000 FEET, THE CREW RECEIVED A (FLAP FAIL) MESSAGE. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE RT BRAKE POSITION SENSOR UNIT (BPSU) AND ALSO SDR REXA04030Flap · malfunctionedFLAPS FAIL AT ZERO ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS, PLACED FLAPS ON 72 HOUR WATCH IAW AD 98-20-01. (NE02200500600)SDR REXA04029Flap · malfunctionedRECEIVED (FLAPS HALF-SPEED) MESSAGE ON BLOCK OUT. FLAP SYSTEM INSPECTED FECU CHECKED FOR CODES, NO CODES FOUND. SYSTEM RESET, PLACED FLAPS ON 72 HOUR WATCH IAW AD 98-20-01.SDR QXEA200400742Warning Light · illuminatedPDX - THE CREW REPORTED THAT THE FLAP POWER CAUTION LIGHT ILLUMINATED AND THAT THE CHECKLIST WAS RUN. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO CURRENT FAULTS IN THE CDS. THE FLAP CIRCUIT BREAKER WAS CYCLED AND THE CAUTION LIGHT EXTINGUISHED. OPERATIOSDR SWIA200414106Control Unit · malfunctionedAFTER T/O FROM LAX, FLAPS FAIL CAUTION MSG. FLAPS FAILED AT 6 DEGREES. RETURNED TO LAX. REPLACED FECU IAW MM 27-51-05. OPERATIONAL CHECK GOOD. P/N 860D100-18ABCD, S/N OFF 1413.SDR SWIA200414077Selector · malfunctionedON FINAL WHEN SELECTING FLAPS 25, CONTROL FAULT WITH ASSOCIATED LIGHTS. INSTALLED SERVICEABLE FLAP HANDLE IAW MM 27-50-00. OPERATIONAL CHECK GOOD.SDR SWIA200414073Control Lever · malfunctionedAFTER LANDING CHECK FLAPS FAIL CAUTION AFTER RETRACTING TO 30 DEGREES. REPLACED FLAP CONTROL LEVER, OPERATIONAL CHECKED GOOD. P/N OFF 292-65253-1, S/N OFF 592.SDR REXA04033Bpsu · failedFLAPS FAIL AT 32 DEGREES ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. REMOVED AND REPLACED LT BPSU (BRAKE POSITION SENSING UNIT) IAW 27 AMM. OPERATIONALLY TESTED GOOD.SDR REXA04028Potentiometer · out of rigFLAP FAILURE ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. PERFORMED RIGGING OF FLAP POTENTIOMETERS AND BPSU IAW AMM 27.SDR AMCR200400005Roller · out of positionAFTER LANDING, THE PILOT WAS NOT ABLE TO RAISE THE FLAPS FROM THE 39 DEGREE POSITION AND HAD ASSOCIATED CAS MESSAGES CONCERNING THE FLAP SYSTEM. VISUAL INSPECTION REVEALED THE FLAPS TO BE OVER-EXTENDED WHICH CAUSED EACH OB ROLLER TO BE OUT BEYOND THE FLAP TRASDR C2XA04RI012Control Unit · inoperativeCREW REPORTED FLAP FAIL AND SPS ADV FAIL MESSAGES ON EICAS DURING LANDING. CREW DECLARED EMERGENCY AND LANDED WITH OUT INCIDENT. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. AIRCRAFT RETURNED TO SERVICE.SDR COMA0460595Warning Light · illuminatedFLIGHT 5152 FLAPS FAILED CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.SDR SWIA200414080Drive Assy · corrodedLEFT WING NR 5 FLEX DRIVE CORRODED. ITEM FOUND AT C-CHECK INSPECTION. FLEX DRIVE REMOVED, SURFACE CORROSION ON HEX END REMOVED, POWER CORE LUBRICATED, NEW END SEAL INSTALLED, FLEX SHAFT REINSTALLED IAW 27-53-10-400-805.SDR SWIA200414048Controller · malfunctionedSPLR/STAB FAULT, PITCH FEEL AND RUDDER LIMIT STATUS MESSAGE. REMOVED AND REPLACED NR 1 SFECU PER CRJ 700 MM 27-50-00/27-51-05. OPERATIONAL CHECK GOOD.SDR SWAA043150Bearing · brokenSUSPECT SINGLE SPINDLE T/E FLAPS FAILURE, AT FLAPS 5 180 KNOTS HEARD LOUD POP, EXPERIENCED SLIGHT YAW AND SLIGHT ROLL, VERY CONTROLLABLE. NORMAL LANDING. REMOVED AND REPLACED RT INBOARD T/E FLAP BOOM CABLE DRUM BEARING PER MM.SDR 04304675Fcu · failedEVENT SUMMARY STATED THAT AFTER TAKEOFF FLAP FAIL INDICATION RTF. REMOVED AND REPLACED FECU MM 27-51-05.SDR 63710292004Control Unit · defectiveUNCOMMANDED STAB, FLAP/STAB SYS FAIL CH B, FLAP STAB MX REQ CAS MESSAGES.SDR COMA0460591Pdu · malfunctionedFLIGHT 5776 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FLAP PDU.SDR SWIA200414032Skin · crackedRIGHT NACELLE FLAP IS CRACKED ON BOTTOM SKIN. REPLACED RIGHT NACELLE FLAP, OPERATIONAL CHECK GOOD. WORK PERFORMED IAW MM 27-50-02.SDR 0401939153Pulley · wornON FINAL APPROACH FOR LANDING AFTER SELECTING FLAPS TO 30 DEGREES DOWN, THE CREW FELT A SLIGHT ROLL AND NOTICED THAT THE LT FLAP INDICATOR WAS AT 20 DEGREES AND THE RT FLAP INDICATOR WAS AT 30 DEGREES. CREW EXECUTED MISSED APPROACH PROCEDURES TO ALLOW TIME FOSDR 04299634Bpsu · failedEVENT SUMMARY STATES THAT FLAP FAIL AT 8 DEGREES. REMOVED AND REPLACED BPSU REF CRJMM 27-51-10. OPS CHECK GOOD.SDR SWIA200414025Control Unit · malfunctionedCONTROL FAULT WITH ASSOCIATED MAP WARNING LIGHTS CAME ON DURING TAXI AND ONCE DURING APPROACH. REPLACED FCU WITH A SERVICEABLE UNIT. OPERATIONAL CHECK GOOD.SDR 66078Switch · lack of lubeFLAPS WOULD NOT RETRACT AFTER TAKEOFF. A/C RETURNED TO THE FIELD. CLEANED AND LUBED FLAP SWITCH, REMOVED AND REPLACED RT SWITCH.SDR DL76L040987Shutoff Valve · failedFLAPS FAILED TO RETRACT PAST 5 AFTER T/O. ALSO RECEIVED A TRAILING EDGE DISAGREE LIGHT. REPLACED RELAY K351 AND SHUTOFF VALVE SOLENOID V1.SDR SWIA200414004Control Unit · contaminatedFLAP CONTROL FAULT ON TAXI OUT. RERACKED FLAP CONTROL UNIT IAW AMM 27-50-06 PAGE 401. CLEANED MOISTURE FROM LEFT AND RIGHT FLAP ACUTATOR CANNON PLUG. OPERATIONAL CHECK GOOD.
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