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 COMA0260085Bpsu · malfunctionedFLIGHT 5525 FLAPS FAIL CAUTION MESSAGE.REPLACED THE R/H BPSU.SDR COMA0260084Bpsu · malfunctionedFLIGHT 5518 FLAPS FAIL CAUTION MESSAGE.REPLACED THE LEFT BPSU.SDR COMA0260082FlapFLIGHT 5477 FLAPS FAILED DURING APPROACH.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR COMA0260079FlapFLIGHT 5957 FLAPS FAIL CAUTION MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR 02FDEA00084Transmitter · inoperative02-35 REPEAT AFTER T/O HAD IND OF ASYMMETRICAL OUTBOARD FLAPS LOCKED OUT. R&R OUTBOARD POS TRANSMITTER PER MM 27-52-013-4.SDR 02FDEA00078Motor · leakingHYDRAULIC SYS "A" QUANTITY LOSS IN FLIGHT. R&R OUTBOARD FLAP HYDRAULIC DRIVE MOTOR PER MM 27-51-062-4.SDR 02FDEA00077Control Unit · malfunctionedDURING CLIMBOUT FLAPS WOULD NOT RETRACT. R&R NR 1 & 2 SFCC PER MM 27-51-18.4.SDR 2002F00203Bpsu · malfunctionedFLT 6505 - FLAP FAIL MESSAGE DURING LANDING ROLLOUT IN PHL, WHEN FLAPS WERE RETRACTED. MAINTENANCE COMPLIED WITH PART A/B. MAINTENANCE REPLACED THE BPSU, AND THE OUTBOARD FLEX SHAFT. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR ABXA010694Link · brokenRIGHT INBOARD FLAP DRIVE LINK BROKEN. REPLACED RIGHT STATION 98 FLAP DRIVE LINK ASSEMBLY IAW DC8 MM 27-51-04-3-0001. OPS CHECKED GOOD.SDR SWIA200210590Connector · contaminatedON TAKEOFF, DURING FLAP RETRACTION, RECEIVED A FLAP DISAGREEMENT. FOLLOWED QRH AND FLAPS RETRACTED NORMALLY. COULD NOT DUPLICATE ON GROUND. INSPECTED FLAPS, TRACKS, ACTUATORS AND FOUND LEFT OUTBOARD FLAP CANNON PLUG WET. CLEANED AND RESECURED. OPS CHECKS SDR 2002F00250Switch · defectiveINT - WHEN FLAPS SELECT FROM 1-5 UNITS AUTO PILOT KICKS OFF. REMOVED AND REPLACED FLAPS UP SWITCH AND RIGGED PER MM 27-51-291. (M)SDR AUS20020043Bearing · failed(AUS) LT OUTBOARD FLAP INBOARD BELLCRANK BEARING HAD EXCESSIVE PLAY. SUSPECT CAUSED BY WATER INGRESS.SDR SWIA200210572Control Unit · malfunctionedAFTER TAKEOFF DURING FLAP RETRACTION, FLAP LIGHT ON MAP WITH DISAGREEMENT ON OUTBOARD PAIR. APPLIED QRH PROCEDURE, NO HELP. RETURNED TO SLC. CLEANED GLYCOL FROM ACTUATOR CANNON PLUGS, REPLACED FLAP CONTROL UNIT AND REPLACED RIGHT OUTBOARD FLAP ROLLERS (4). SDR AUS20020045Computer · faulty(AUS) FLAP SYSTEM INOPERATIVE. NO CAUSE COULD BE FOUND AND INVESTIGATION IS CONTINUING. FLAP COMPUTER PNO 676801007 CHANGED.SDR COMA0260057Bpsu · malfunctionedFLIGHT 5450 FLAPS FAILED AT 28 DEGREES DURING LANDING ROLL.REPLACED THE L/H BPSU.SDR CA020117013Torque Tube · chafed(CAN) CHAFING DAMAGE FOUND ON LT & RT FLAP INBD TORQUE TUBES & HYD LINES. THIS PROBLEM WAS FOUND ON INSPECTION OF UPPER FUSELAGE AREA BEHIND WING CENTRE SECTION LT & RT STA: YW42.000.SDR 2002UALA00064Flap · malfunctionedTAKEOFF ROLL 120 KTS TRAIL EDGE DISAGREE LIGHT ON EICAS AND FWD PANEL. USING NORMAL FLAP LEVER WOULD NOT MOVE. TRAILING EDGE ALTN SWITCH CLEARED DISAGREE LIGHT. USING ALTN METHOD LOWERED FLAPS TO 20. ACP CK OF FLAP SYSTEM. RAN FLAPS UP ELECTRIC AND FULL USDR SWIA200210567Bpsu · failedPRIOR TO FAF AT IDA, WHEN F/O CALLED FLAPS 8 RECEIVED A (FLAP FAIL) AMBER MESSAGE. CONSULTED QRH. FLAPS WERE STUCK AT 8 DEGREES. RETURNED TO SLC. LEFT BPSU FAILED BRAKE CHECK. REMOVED AND REPLACED LEFT BPSU. PERFORMED OPERATIONAL CHECKS, NO FAULTS NOTED.SDR MALA020127Hinge FittingDuring 4K-Check in CWA, LH Flap Hinge WS 123.38 has play at Flap Attach points. Maintenance installed new fitting PN 7257800-582 RHOB and new hardware IAW SB57-038. Removed and installed new fitting assembly. Re-installed Hinge with new Hardware.Re-installed SDR ABXA010676Control Cable · lack of lubeFINAL APPROACH, AIRCRAFT IN A TRIMMED DESCENT ON GLIDESLOPE, FLAPS 30, N1-60 PERCENT ON BOTH ENGINES, SPEED 10 + OVER TARGET 139. WENT TO FLAP 40, AIRCRAFT ROLLED RIGHT NOTICEABLE, 1 1/2 UNITS LEFT TO TRIM. INSPECTED AILERON AND FLAP CABLE SYSTEM. ALSO INSPSDR SWIA200210560Bpsu · malfunctionedON APPROACH FLAPS FAILED WHEN FLAPS SELECTED 8 DEGREES. FLAPS FAILED AT 0 DEGREES. RAN QRH. REPLACED LEFT BPSU AND PERFORMED RIGGING PER CRJ MM 27-51-10 AND CYCLED FLAPS SEVERAL TIMES. OPS CHECK GOOD. S/N OFF: 1241BSDR 2002FA0000122Bushing · missingFLAPS FAILED TO RETRACT DURING TOUCH AND GO TRAINING. INSPECTION BY MAINTENANCE FOUND BUSHING (P/N 1512280-24) HAD NOT BEEN INSTALLED AT THE FACTORY. THIS ALLOWED THE FLAP ARM ASSEMBLY (P/N 0560022-8) TO MOVE AWAY FROM FLAP LEVER ASSEMBLY (P/N 0560021-1) PRSDR COMA0260044FlapFLIGHT 5553 FLAPS FAILED AT 30 DEGREES DURING APPROACH.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01.SDR 02FDEA00052Flap · malfunctionedON LANDING APPROACH FLAPS STUCK AT LESS THAN 15 DEG SLATS NORMAL BOTH OVERHEAD EAD FLAP LIGHTS & FLAPS ON SFPI PANEL ON.SDR C2XA02IA009Roller · damagedIAH- FLIGHT 3664DURING TAKEOFF THE CREW NOTED A FLAP CONTROL FAULT,AND, ABORTED THE TAKEOFF. IAH-MAINTENANCE INSPECTEDTHE FLAPS,AND, FOUND THE BEARING ON THE RIGHT INBOARD FLAP, INBOARD END TO BE DAMAGED. MAINTENANCE REMOVED and REOPLACEDTHE BEARING,PERFORMSDR 2002F00100Flap · malfunctionedFLT 6071 - PHX-EUG - THE CREW DECLARED AN EMERGENCY DUE TO A FLAP FAIL CAUTION MESSAGE. THE AIRCRAFT RETURNED TO THE FIELD WHERE MAINTENANCE WERE ABLE TO RESET THE FLAP SYSTEM AND COMPLIED WITH PART 'A' OF THE AD. (M)SDR SWIA200210546Flap · malfunctionedUPON SELECTING FLAPS TO 45 DEGREES, THE OUTBOARD FLAPS WENT TO 25 DEGREES ONLY. RECEIVED A FLAP DISAGREEMENT. FOLLOWED QRH PROCEDURE AGAIN, FLAP DISAGREEMENT. DIVERTED FROM SBP TO SMX. RESET FLAP ANNUNCIATOR. INSPECTED FLAPS, ROLLERS AND TRACKS, FOUND TO SDR U30A200200004Computer · faultyDURING CRUISE, FLT/CTL WING TIP BRK FAULT ILLUMINATED. TROUBLESHOOTING REVEALED THE NR 2 SLAT FLAP CONTROL COMPUTER (SFCC) FAULTED. R&R WITH A SERVICEABLE UNIT AND OPERATIONALLY CHECKED WITH NO FAULTS FOUND.SDR C2XA02IA002Control Handle · faultyIAH- FLIGHT 3998 IN FLIGHT AFTER DEPARTURE A LANDING GEAR AURAL WARNING INDICATION CONTINUALLY SOUNDING. RECYCLED THE GEAR AND CONTINUED TO GET THE AURAL WARNING. RETURNED TO IAH WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED AND REPLACED THE FLAP SELECTOR LESDR COMA0260027FlapFLIGHT 5598 - FLAPS FAILED AT 28 DEGREES AFTER LANDING.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.SDR U30A200200002Computer · malfunctionedDURING CRUISE, FLT/CTL FLAP TIP BRK FAULT INDICATION ON ECAM. PERFORMED TROUBLESHOOTING IAW AMM 27-51-00-810-837 FOR LT WTB, NO FAULT FOUND. SWAPPED NR 1 & 2 SFCC'S TO THE FOLLOWING POSITIONS; NR 1 POS P/N 49-170-07, S/N 2007, NR 2 POS P/N 49-170-11, S/N 418SDR U30A200200001Solenoid · intermittentDURING CRUISE, FLT/CTL FLAP TIP BRK FAULT INDICATION ON ECAM. REPLACED BOTH SOLENOIDS ON LT WING TIP BRAKE. OPS CHECK OK.SDR 2002F00102Flap · malfunctionedFLT 6451 - PHX-COS - INBOUND TO COS, THE CREW REPORTED A FLAP FAIL CAUTION MESSAGE AND DECLARED AN EMERGENCY. THE MESSAGE APPEARED WITH THE FLAPS AT ZERO AND SELECTED DOWN. THE AIRCRAFT LANDED UNEVENTFULLY AND ON CALL MAINTENANCE PERFORMED PART A/B OF THE ADSDR SWIA200210503Fcu · faultyWHILE EN ROUTE GOT FLAP WARNING ASYMMETRY ASSOCIATED WITH CONTROL FAULT AND ADVANCED SWS. FLAP PAIR LIGHT BARS ON OUTBOARD PAIR SHOW ASYMMETRY WARNING, ONLY ONE LIGHT SEGMENT. THERE WERE NO CONTROL PROBLEMS OR ROLL TENDENCIES. PERFORMED SYSTEM SELF-DIAG TESSDR LR7A02001Brake Assy · leakingDURING CLIMB OUT OF OKO FLIGHT CREW REPORTED LOSS OF UTILITY HYDRAULIC SYSTEM PRESSURE. ACCOMPLISHED LANDING GEAR MANUAL EXTENSION AND MANUAL FLAP SETTING. FLIGHT DIVERTED TO NJA AND LANDED WITHOUT INCIDENT.FOUND FLAP DRIVE BRAKE ASSY LEAKING. REPLACED BRAKSDR U30A200100004Computer · faultyTROUBLESHOOTING REVEALED NR 2 SLAT FLAP CONTROL COMPUTER (SFCC) FAULTED. REPLACED NR 2 SFCC PER AMM 27-51-34-401 AND PERFORMED TEST PER AMM 27-54-00-210, OPS CHECK OK.SDR COMA0260019Motor · failedFLIGHT 5106 FLAPS FAILED WHEN SELECTED DURING TAXI.REPLACED THE FLAP PDU.SDR AUS20011401Control Unit · faulty(AUS) TRAILING EDGE FLAP CONTROL UNIT FAULTY.SDR 0105105642Mechanism · lack of lubeAFTER TAKEOFF UPON SELECTING FLAPS 1, THE TRAILING EDGE FLAP DISAGREE WARNING ILLUMINATED AND THERE WAS NO CHANGE IN THE INDICATED FLAP POSITION. THE FLIGHT DECLARED AN EMERGENCY, RETURNED TO MSP, AND ACCOMPLISHED AN OVERWEIGHT LANDING WITHOUT INCIDENT. MAINSDR COMA0260021Switch · malfunctionedFLIGHT 5949 FLAPS FAIL CAUTION MESSAGE.REPLACED THE FLAP CONTROL LEVER ASSY.SDR COMA0260011FlapFLIGHT 5400 FLAPS FAILED AT 26 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.SDR COMA0260014Fcu · malfunctionedFLIGHT 5764 FLAPS FAILED AT 30 DEGREES DURING LANDING.REPLACED THE FECU.SDR 2002F00101Flap · malfunctionedFLT 5629 - PHX-COS - INBOUND TO COS, THE CREW REPORTED A FLAP FAIL CAUTION MESSAGE. THE CREW DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. ON CALL, MAINTENANCE PERFORMED PART 'A' OF THE AD, RESET THE SYSTEM AND THERE WERE NO FURTHER MESSAGES OF DEFECTS NOTESDR SWIA200110491Power Unit · malfunctionedAFTER SETTING FLAPS 45 DEGREES, FLAPS FAIL CAUTION MESSAGE CAME ON. FLAPS FAILED AGAIN IN SLC. REMOVED AND REPLACED ELECTRONIC FLAP COMPUTER, OPS CHECK GOOD. REMOVED AND REPLACED PDU IAW CRJ MM 27-52-01, RIGGED BPSU IAW CRJ MM 27-51-10, REMOVED AND REPLACEDSDR SWIA200110468Control Unit · failedAFTER LEVELING OFF AT FL330, FLAPS FAIL CAUTION MESSAGE ILLUMINATED. REPLACED FECU PER MM 27-51-05. OPS CHECK OF SYSTEM GOOD.SDR SWIA200110467Bpsu · malfunctionedFLAPS FAILED AT 11 DEGREES DURING FLAP RETRACTION. REMOVED AND REPLACED LEFT BPSU IAW 27-51-10. ADJUSTED POTENTIOMETERS 6 AND 7 (6 FROM -0.019 TO 0.011; 7 FROM -0.013 TO 0.011). OPS CHECK GOOD.SDR COMA0160981Bpsu · malfunctionedFLIGHT 5296 - FLAPS FAILED AT 30 DEGREES.REPALCED THE R/H BPSU.SDR COMA0160987Actuator · malfunctionedFLIGHT 5957 FLAPS FAILED WHEN SELECTED FOR APPROACH.COULD NOT DUPLICATE DISCREPANCY; ALL 8 FLAP ACTUATORS REPLACED.SDR COMA0110165Roller · wornFLIGHT 5061 - FLAP DISAGREEMENT WARNING WHEN FLAPS SELECTED UP.REPLACED THE R/H OUTBD FLAP SECTION ROLLERS.SDR 2002F00099Ecu · failedFLT 5864 - HSV-CLT - IN CRUISE FLIGHT, THE CREW REPORTED A FLAP FAIL CAUTION MESSAGE. THE CREW DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED UNEVENTFULLY WITH FLAPS UP. MAINTENANCE REMOVED AND REPLACED THE FECU AND OPS CHECK GOOD. (M)
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