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 DXTA2010082504206Circuit Board · inoperativeFLAPS INOPERATIVE. CLICKING SOUND HEARD ON TAKEOFF, COMING FROM LT SIDE OF COCKPIT. PLANNED A RETURN TO DEPARTURE; SELECTED FLAPS 15. FLAP HANDLE STOPPED AT THE FLAPS 7 POSITION. R & R HYD, PCB NZ014 IAW WDM 20-10-00. OPS CHECK THE FLAPS, SPEED BRAKES, AND LSDR UALA2010082303112Computer · failedUPON APPROACH FLAPS DOWN, SLATS STUCK AT 1 POSITION. RE-CYC FLAPS STILL NO HELP. GOT MESSAGE F-CTL SLATS LOCKED. WING TIP BRK. REPLACED THE 22CV SFCC2 COMPUTER. OPS CHECK GOOD.SDR COMA2010082450179Bpsu · faultyON APPROACH INTO CVG RECEIVED FLAPS FAIL CAUTION MSG. EMERGENCY DECLARED, A/C LANDED SAFELY. REMOVED AND REPLACED LEFT BPSU.SDR DXTA2010082004198Knob · looseAFTER TAKEOFF, FLAP LEVER WOULD NOT MOVE OUT OF TAKEOFF FLAP POSITION. RETURNED FOR LANDING. FOUND KNOB LOOSE UPON ARRIVAL TO ACFT. RESECURED FLAP LEVER KNOB AS REQ'D IAW 20-00-00, OPS TEST GOOD.SDR UALA2010081903044Circuit Card · faultyFLAP DISAGREE MSG. CONFIG LGT ON & EICAS MSG FLAPS DISPLAY WITH FLAP IN TAKE OFF POSITION, ABORTED TAKEOFF AT 20 KNOTS IAW CREW. PERFORMED FIM TASK 31-51-00 VERIFIED WIRING FROM WEU TAKEOFF CONFIG CARD PIN 44 TO FSEU AND CHECKED DIODE R607. WIRING CHECKED GOOSDR REXA201000104Ecu · failedFLAPS FAIL CAUTION AT FL210 FLAPS AT 0 DEGREES, LANDING WITH 0 DEGREE FLAPS. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH(H)(6)(I), AMOC DATED MARCH 27, 2009, TR# 27-012 PER AMOC DATED DECEMBER 18, 2009 AND PA AD27-052G. RESDR SIMA201023001Control Unit · failedON FLIGHT 3286 THE CREW REPORTED A FLAP FAIL ON APPROACH AND DECLARED AN EMERGENCY. A ZERO FLAP LANDING WAS PERFORMED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT. THE ESDR AALA20100815TUL04Relay · defectiveMIA - CREW REPORTED TRAILING EDGE FLAP DISAGREE AND FLAP ISOLATION VALVE STATUS MESSAGE. EMERGENCY DECLARED LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED FIM 25-51-00, NO FAULTS NOTED. REPLACED DEPRESSURIZATION RELAY AS A PRECAUTSDR AALA20100814LAX01Transmission · failedLAX - INFLIGHT ORD-SNA. CREW REPORTED TRAILING EDGE FLAP DISAGREE EICAS MESSAGE. EMERGENCY DECLARED, DIVERTED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT INBOARD FLAP TRANSMISSION. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR REXA201000103Bpsu · failedFLAPS FAIL AT 11 DEGREES CLIMBING OUT OFF DTW 170 KNOTS 2000FT. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I), AMOC DATED MARCH 27, 2009, TR 27-012 PER AMOC DATED DECEMBER 18, 2009 AND PA AD 27-052G. REMOVED AND RESDR UALA2010081202952Switch · out of positionFLAP ISSUE, RTFL. CHECKED VMO-MMO SWITCH IAW MM. RETURNED VMO-MMO SWITCH ON 188VU PANEL TO NORM POSITION. PERFORMED AFCS 1-2 GND SCAN AND AFS FAC TEST ALL CHECKED GOOD.SDR IPXA10561723Flap System · malfunctionedAS FLAPS WERE IN TRANSIT FROM 1 TO UP SAW MOMENTARY INCREASE IN AIRSPEED TO 250 KNOTS. AFTER FLAPS UP AIRSPEED RAPIDLY DECREASED TO 235 KNOTS TS. FLAP INDICATOR WAS AT .5 POSITION. NR 431740 ASSIGNED. C/W PHASE 1 OVERSPEED INSP L/E FLAPS IAW AMM 05-51-08-2. SDR AALA20100805ORD01Transmission · lowORD - CREW REPORTED TRAILING EDGE FLAP DISAGREE EICAS MESSAGE DURING DESCENT. FLIGHT LANDED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. SERVICED LEFT WING INBOARD FLAP TRANSMISSIONS AND RESET INDICATOR. SYSTEM GROUND CHECK NORMAL OPERATION.SDR WAIA2010F00188Motor · failedAFTER LANDING, THE SIC EXITED THE ACFT AND NOTICED THAT THE FLAPS WHERE STILL IN THE FULL DOWN POSITION. THE SIC NOTIFIED THE PIC OF THE DISCREPANCY. PIC THEN APPLIED POWER AND TRIED TO CYCLE THE FLAPS UP. AGAIN THE FLAPS DID NOT MOVE. THE CREW CHECKED ALL CIRSDR CA100802001Fcu · malfunctioned(CAN) FLIGHT CREW RECEIVED AN ENGINE INDICATION AND CREW ALERTING SYS (EICAS) FLAPS FAIL CAUTION MESSAGE DURING CLIMB OUT. DECISION WAS MADE TO CONTINUE TO DESTINATION WHERE AN UNEVENTFUL FLAP ZERO LANDING WAS CONDUCTED. THE ACFT WAS REMOVED FROM SERVICE, THSDR UHLA2010072700081Control Unit · unserviceableIN CRUISE FLIGHT AT FL350 NUMEROUS MASTER CAUTIONS APPEARED: AOA LIMIT FAIL, SHAKER ANTICIPATED, FLAP FAIL, GRND PROX FAIL, WINDSHEAR FAIL, AT FAIL, AP FAIL, AND THERE WAS NO LONGER A FLAP POSITION INDICATOR. RAN THE APPROPRIATE CHECK LISTS AND LANDED WITH NSDR N6WA20100717Flap System · malfunctionedFLAP FAIL ENROUTE, PERFORMED QRH PROCEDURE, LANDED FLAPS 1 PHL. PERFORMED OPS CHECK OF FLAPS AND SLATS IAW AMM 27-51-05. SELECTED FLAPS 8. ACFT SAFE FOR (1) TIME FERRY.SDR RAIA201007250001Flap · malfunctionedON APPROACH THE FLAPS FAILED TO EXTEND. AIRCRAFT MADE AN EMERGENCY LANDING. MAINTENANCE INSPECTED THE FLAP SYSTEM AND RESET THE FLAPS. PERFORMED SEVERAL OPS CHECKS. FLAPS OPS CHECKED GOOD.SDR N6WA20100715Flap System · warning lightFLAPS FAIL CAUTION MSG IN FLIGHT. CLEARED INHIBITS OF SFECU 1 AND 2 PERFORMED FIM TASK 27-52-00. FLAP FAIL MESSAGE IS NOT NOTED AT THIS TIME.SDR C2XA10CL118Control Unit · faultyCLE FLT 2730 THE CREW REPORTED A FLAP LOW SPEED MESSAGE ON TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD.SDR COMA2010072050148Control Handle · failedON APPROACH INTO CVG RECEIVED FLAPS FAIL CAUTION MSG. EMERGENCY DECLARED, A/C LANDED SAFELY. REMOVED AND REPLACED FLAP CONTROL LEVER. NO FURTHER DEFECTS NOTED.SDR ASAA1048087Flap System · malfunctionedDURING APPROACH, FLAPS SELECTED NO LE OR TE FLAP INDICATED. ACCOMPLISHED QRH FOR INDICATION & ALTERNATE FLAP EXTENSION. FULL EXTENSION ON LE BUT NO INDICATION ON TE FLAPS CONFIRMED VISUALLY. LANDED WITH FLAP HANDLE IN 1 DEGREE POSITION. AFTER LANDING, SELESDR TRBA2010078Valve · inoperativeDURING APPROACH, FLAP MOVE VERY SLOW FROM 15 DEGREES TO 30 DEGREES, EXT FLAG STAYED ON. FEW SECONDS AFTER REACHING 30 DEGREES, RECEIVED WARNING FLAP UNLOCK ON CAP EXECUTED GO AROUND FOLLOWED AOM PROCEDURES AND LANDED WITH FLAPS 15 DEGREES. "EMERGENCY DECLARESDR TRBA2010077Flap System · malfunctionedDURING FINAL APPROACH, WHEN SELECTING FLAP 30 EXT FLAG STAY ON THEN FLAP UNLOCK ON CCAS, EXCUTED GO AROUND "DECLARED EMERGENCY" ABLE TO LAND FLAP 15. MX INSPECTED FLAP SYS, PERFORMED OPS CK OF FLAPS 10 TO 15 TIMES, COULD NOT DUPLICATE PROBLEM IAW JIC 27-50-00.SDR DALA1151350676Gear · unknownT/E FLAP TRANSMISSION GEAR REPLACED IAW EA 06-097281-03, ME04.SDR GTIA1000033Flap System · faultedACFT DECLARED EMERGENCY ON APPROACH, RETRACTION FCTL FLAP SYS2 FAULT ONECAM. ON LAND FLAPS WOULD NOT EXTEND BEYOND FLAP-2 POS. PERF ECAM AND COM PROCEDURES.SDR CA100719007Seal · failed(CAN) DURING INITIAL CRUISE AND SELECTING FLAPS, FLAP SELECTOR VALVE FAILED IN FLIGHT RESULTING IN TOTAL LOSS OF HYDRAULIC FLUID AND PRESSURE. AIRCRAFT RETURNED TO AIRPORT AND FLIGHT CREW USED "EMERGENCY GEAR DOWN` SELECTION TO LAND SAFELY. MAINTENANCE CREW SDR TRBA2010073Valve · inoperativeDURING APPROACH AT EIS WHEN SELECT THE FLAPS TO 30 DEG. NEVER WENT DOWN, THE FLAPS WITH WENT AROUND, CAME BACK TO SJU AND THE FLAPS NEVER WENT DOWN TO FLAPS 15 OR 30 DEGREES, WITH MAKE A LANDING WITH FLAPS 0 DEG, FLAP 0 DEG LANDING PROCEDURES. R & R BOTH FLAPSDR C2XA10SH228Control Unit · malfunctionedXNA - TAKEOFF CONFIGURATION MALFUNCTION. REMOVED AND REPLACED FECU IAW EMB 145 XR AMM 27-53-02. OPS CHECK GOOD. NO FAULTS FOUND AT THIS TIME.SDR AALA20100703LGA01Computer · failedLGA - ON FINAL APPROACH CREW REPORTED TRAILING EDGE LIGHT ILLUMINATED, FLAP DISAGREE ON EICAS. FOLLOWED PROCEDURES AND CHECKLIST AND LANDED WITH NORMAL FLAPS 30 DEGREES. CYCLED FLAP/SLATS WITH BOTH HYDRAULICS AND ELECTRICAL. VERIFIED FLAP OVERLOAD INDICATORSSDR FDEA201007032339Flap System · malfunctionedON TAKEOFF PASSING 9,000 FT T/E FLAP DISAGREE EICAS ANNUNCIATED INTERMITTENTLY. ATB BACK TO KFSD, RAN T/E FLAP DISAGREE CHECKLIST, LANDED WITHOUT INCIDENT. T/E FLAP DISAGREE EICAS MSG WAS INTERMITTENT ON AND OFF THROUGH OUT THE FLIGHT.SDR CA100805012Relay · burned(CAN) FLAP CIRCUIT BREAKER POP OUT, DURING TESTING FLAP OPERATION ON THE GROUND. DEFECT FOUND WAS BURNED CONTACT IN FLAP RELAY LOCATED UNDER ACFT BELLY RT SIDE.SDR CALA2010063000315Flap System · malfunctionedEXTENDED FLAPS BUT NO FLAPS EXTENDED, HAD TO DO FLAP 15 LDG USING ALTERNATE FLAP SW. PERF FSEU BITE PROCEDURE AS PER FIM 27-51 TSK801, NO EXISTING FAULTS FOUND. PERF FLAP SKEW DETECT SYS TEST AS PER AMM 27-59- 00-730-801, SYS FUNCTION TEST OPS CHECK GOOD. PSDR DALA1142800694Gear · damagedTRAILING EDGE FLAP TRANSMISSION GEAR REPLACED IAW EA 06-097281-03, ME02, ME04.SDR A6WA201040461Flap System · out of rigA/C REQUIRES 1 FULL INDEX MARK LT WING DOWN AILERON TRIM TO MAINTAIN LEVEL FLIGHT WITH GEAR DOWN AND FLAPS AT 45 DEGREES. REF WO 156897 FOR WORK ACCOMPLISHED, TE FLAP RIGGING AND PAINT.SDR UALA2010062302209Valve · faultyFLAPS PRIMARY FAIL EICAS. PERFORMED FIM 21-52 TASKS 801 AND 843, FOUND FLAPS PRIMARY CONTROL VALVE LOW SPEED SOLENOID RESISTANCE OUT OF LIMITS, REPLACED FLAP PRIMARY CONTROL VALVE PER MM. ACCOMPLISHED FLAP PRIMARY CONTROL VALVE TEST PER AMM, FLAPS ARE OPERATINSDR FDEA201006222112Switch · misalignedDURING FLAP RETRACT ON TAKEOFF GOT FLAPS SYS 2 JAM AND FLAP VANE JAM FAULTS. CYCLED FLAPS WITH NO CHANGE. FLAPS WOULD LOWER, BUT NOT RAISE ABOVE 10 DEGREES. DURING TROUBLE SHOOTING FOUND THE RT WING INBD FLAP VANE EXTEND JAMMING SWITCH 42CV OUT OF ADJUSTMESDR 2010FA0000626Rvdt · faultyFLAPS FAIL AMBER CAS INFLIGHT.SDR NSVA2010101Flap · malfunctionedAFTER TAKEOFF CREW EXPERIENCED FLAP POWER FAIL. DECLARED EMERGENCY AND RETURNED TO BOS. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. DUTY OFFICER HAS CONTACTED FAA REGARDING THIS FLIGHT. CLEARED ECU CONTINUES BIT FAULT FROM CDS IAW Q400 MM 15-00-27. PERFORSDR 2010FA0000625Control Box · inoperativeFLAPS FAIL CAS MESSAGE IN FLIGHT.SDR AALA20100618MIA01Unknown · malfunctionedMIA - TRAILING EDGE FLAP DISAGREE LIGHT ON FINAL WHEN SELECTING 25 DEGREE FLAPS. FLAP INDICATOR STUCK AT 20 DEGREE FLAPS. ACCOMPLISHED QUICK REFERENCE HANDBOOK CHECKLIST. EMERGENCY DECLARED ACCOMPLISHED GO AROUND LANDED MIA WITH 20 DEGREE FLAPS WITHOUT INCISDR 2010FA0000623Flap · out of rigFLAPS FAIL AMBER CAS MESSAGE CAME ON IN LEVEL FLIGHT. CREW COULD NOT RESET.SDR 2010FA0000601Relay · intermittentOWNER REPORTED THE FLAP SYS TO BE INTERMITTENT WHEN THE FLAPS SELECTED TO DOWN POSITION. OPERATED THE FLAP SYS IN THE HANGER AND VERIFIED THE INTERMITTENT FLAPS. FOUND THE FLAP MOTOR CONTROL RELAY TO BE CAUSING THE INTERMITTENT PROBLEM. AFTER REMOVAL OF THE FLSDR ASOA201000922Flap System · failedFLAPS FAIL CAUTION IN CRUISE FLIGHT. (EMERGENCY TRUCKS REQUESTED AS A PRECAUTION - EMERGENCY DECLARED BY TOWER) T/S IAW FIM 27-52-45. PERFORMED CLEAR INHIBITS AND LRU TEST. FLAP FAIL MSG CLEARED. FLAPS AND SLATS OPS CHECK GOOD. (CLOSED)SDR CHQA201000119Flap · malfunctionedWHILE ON DESCENT INTO DCA WHEN THE CREW ATTEMPTED DEPLOY THE FLAPS TO 9 DEGREE POSITION, A FLAP LOW RATE MESSAGE WAS DISPLAYED FOLLOWED BY A FLAP FAIL MESSAGE AND THE FLAPS CONTINUED TO INDICATE ZERO. THE QRH WAS FOLLOWED AND THE AIRCRAFT DIVERTED TO IAD, LANSDR IPXA10M60394Control Valve · unserviceableINSPECTION TYPE:AS-E, AFTER T/O AT 400FT GOT A LEVEL 2 FLAP DISAGREE, BY THE TIME WE FINISHED CHECKLIST THE FLAPS HAD BLOWNBACK TO ZERO DEGREES. DURING BLOWBACK THE RT SIDE FLAPS BOTH INNER AND OUTER RETRACTED SUBSTAINTALLY FASTER THAN LT SIDE. BASED ON THE FESDR DXTA2010060904118Selector Valve · leakingAFTER TAKEOFF AND ON INITIAL GEAR RETRACTION, RT HYD PUMP PRESS LOW, AUX HYD PUMP ON, AND RT HYD LOW LEVEL CAUTION MESSAGES ILLUMINATED. FLUID QTY LEVEL WAS AT 24 ON RT HYD SYS. RAN QRH PROCEDURES AND LANDED SJC. ON POSTFLIGHT, HYD FLUID NOTED ON BOTTOM ON PLASDR CA100607004Bpsu · failedON APPROACH THE FLAPS FAILED AT ZERO DEGREES. AN EMERGENCY WAS DECLARED AND THE ACFT CARRIED OUT AN UNEVENTFUL FLAP ZERO LANDING. FECU CODES 12 & 13 WERE POSTED FOR THE LT BPSU. THE LT BPSU WAS REPLACED, MANUAL TORQUE TEST WAS CARRIED OUT WITH NO FAULTS, SOMSDR AALA20100605DFW03Fseu · inoperativeDFW - CREW REPORTED FLAPS WOULD NOT RETRACT AFTER TAKEOFF. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLAP SLAT ELECTRONIC UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.SDR FDEA201006021779Control Valve · failedON FLAP RETRACT AFTER TAKEOFF. WITH FLAPS 0 SLAT EXT GOT FLAP DISAG ALERT. ATTEMPTED TO EXTEND FLAPS BACK TO 15 & FLAPS WOULD NOT MOVE. FLAPS INDICATED EXT/0. DUMPED 20,000 LBS OF FUEL & MADE 0/EXT LANDING. TOUCHDOWN AT 174 KTS. WEIGHT 362,000. T/S FLAP S
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