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 CA141030010Control Cable · broken(CAN) PILOTS REPORTED A FLAP ASSYMETRY MESSAGE ON THE IIDS AFTER LANDING , AT THE SAME TIME THE MESSAGE APPEARED , THE FLAP SYSTEM JAMMED. DURING MAINTENANCE CREW INVESTIGATION/INSPECTION , IT WAS FOUND OUT THAT THE AFT FLAP CONTROL CABLE ON THE R/H SIDE WAS LSDR SWIA201439643Control Unit · failedRETURNED TO THE FIELD WITH A FLAP CONTROL FAULT. REPLACED THE FCU, OPS CHECKED GOOD.SDR SIMA20141019011Brake · failedFLAP LOW SPEED ADVISORY MSG ON EICAS AFTER LANDING. ITEM DEFERRED IAW MEL 27-9. FLAP LT MOTOR BRAKE FAIL M PROCEDURE COMPLIED WITH.SDR YENA20141017219Pickup · failedDURING APPROACH AND SELECTING FLAPS TO 2 DEGREES WITH SPEED BRAKES OUT, RECEIVED F/CTL FLAPS LOCKED WING TIP ON ECAM. COMPLETED ECAM ACTION AND LANDED UNEVENTUALLY. R & R ASYMMETRY POSITION PICK OFF UNIT ON THE LT SIDE, IAW AMM 27-51-18. OPS CHECK, FLAPS GOOSDR CA141017010Shaft · broken(CAN) THE PILOT REPORTED A FLAP SPLIT ASYMMETRY OCCURRED DURING FLIGHT. MAINTENANCE FOUND THAT THE RT INBD FLAP FLEX SHAFT WAS BROKEN. A HEAVY AMOUNT OF CORROSION WAS NOTICED AT THE BREAK LOCATION.SDR CA141006018Shaft · sheared(CAN) CREW REPORTED FLAP CAWS WHEN SELECTING FLAPS FROM 0 DEGREES TO 15 DEGREES. THE CREW WAS UNABLE TO RESET THE THE FLAP CAWS. FLAP FAULT ISOLATION PROCEDURE CARRIED OUT AND FOUND THE RT FLAP WOULD NOT MOVE WHEN USING THE FLAP MAINTENANCE SWITCH. THE RT FLSDR CA141015003Motor · malfunctioned(CAN) MOTOR WAS IDENTIFIED AND CERTIFIED AS PN 1202-00-1 SN 4556, , FAILED SHORTLY AFTER INSTALLATION. MOTOR MAY HAVE BEEN SETUP AT OVERHAUL AS A 12 VOLT UNIT PN 1202-20-1, BOTH PART NUMBERS WERE INDICATED ON UNIT? MOTOR FAILED AFTER APPROXIMATELY 45 COMPLETE SDR AALA20141005001Indicator · trippedTRAILING EDGE FLAP DISAGREE EICAS INDICATION. EMER DECLARED FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND LT WING INBD TE FLAP INBD FLAP TRANSMISSION OVERLOAD INDICATOR TRIPPED. RESET INDICATOR. SYS GND CHECKED NORMAL OPERATION CLOSED.SDR HNAA2014100300279Indicator · malfunctionedTAKEOFF WARNING HORN SOUNDED DURING TAKEOFF ROLL WHEN POWER LEVERS ADVANCED. TAKEOFF ABORTED. R & R FLAP POSITION INDICATOR AND PERFORMED OPS CHECK IAW MM 27-53-05. OPS CHECKED GOOD. PERFORMED TAKEOFF WARNING SYS CHECK, OPS CHECKED GOOD.SDR YENA20140930209Computer · failedFLIGHT CONTROL FLAPS LOCKED WING TIP BRAKE ON DESCENT. R & R APU AND PERFORMED CHECKS IAW AMM 27-51-00, OPS CHECKED NORMAL.SDR S9BA201409290013Circuit Breaker · trippedFLAPS LIGHT ILLUMINATED DURING FLIGHT, NO FLAP LANDING PERFORMED AFTER THE QRH COMPLETED. EMERGENCY DECLARED. PERFORMED A DETAIL VISUAL INSPECTION OF FLAPS AND FLAP SYSTEM. FOUND CIRCUIT BREAKER, FLAP CONTROL, TRIPPED OUT. PERFORMED OPT CHECK OF FLAP SYSTSDR AWKA20141001001Unknown · malfunctionedWHILE ON APPROACH, FLIGHT CREW RECEIVED AN AMBER FLAPS FAIL CAS MSG WHEN THE FLAP HANDLE WAS SELECTED TO THE 15 DEGREE POSITION. THE FLAPS STAYED AT THE 5 DEGREE POSITION & CREW REJECTED THE APPROACH SINCE THEY DID NOT MEET THE WET PERFORMANCE LANDING NUMBERSSDR CALA2014092601284Unknown · malfunctionedON LANDING TE STUCK AT 5 DEG. ACCOMPLISHED QRH FOR A FLAPS 15 LANDING PERFORMED FSEU BITE GOT 27-51351. FOLLOWED FIM & RESET FSEU RAN BITE GOT NO FAULTS. PERFORMED TE FLAP LOAD RELIEF BITE TEST. TEST PASSED IAW TASKS 27-51-00-810-830 + 27-51-00-810-803.SDR SIMA20140922003Motor-Brake Unit · faultedFLAP LOW SPEED ON EICAS 678 MEL DEFERRAL 67827051D. FLAP CHANNELS FLAP LOW SPEED ADV ON FLAP LOW SPEED CHANNEL 2 INOPERATIVE. RESTORATION OF MEL PLANE ACFT PN SN EMB145 14500813. TROUBLE SHOT FOUND FLAP LT MOTOR BRAKE FAIL & FLAP LT WING BRAKE FAIL ON CMC. SDR AWKA20140923001Fcu · malfunctionedWHILE EN ROUTE, THE FLIGHT CREW REPORTED A CYAN FLAPS FAULT MSG. AFTER CHECKLIST REVIEW & UPON ARRIVAL, FLIGHT CREW EXTENDED THE FLAPS EARLY AT WHICH THEY FAILED. DID ONE FLAP RESET & TRIED A COUPLE DIFFERENT FLAP POSITION SETTINGS. FLAPS WOULD EITHER TRAVESDR IPXA2014091984363Electronic Unit · inoperativeT/E FLAP DISAGREE MESSAGE ON APPROACH. EMERGENCY DECLARED. PERFORMED FSEU BITE PROCEDURE REF AMM 27-51-00-815. R & R FSEU AND OPS CHECKED GOOD IAW AMM 27-51-01 P201.SDR SWAA2014091732058Electronic Unit · failedDECLARED EMER FLAPS WOULD NOT DEPLOY ON APPROACH. R & R FLAP SLAT ELEC UNIT IAW MM.SDR FDEA201409112566Gearbox · lowON APPROACH TE FLAP DISAGREE EICAS WARNING WHEN SELECTING FLAPS 25. FLAPS REMAINED AT 20 RAN QRH PROCEDURE, LANDED UNEVENTFULLY AT FLAPS 20. AMM SMP FOUND FAULT MSG FLAP DISAGREE 305 IN NR 1 FSEU. PROCEEDED TO TROUBLESHOOT IAW FIM 27-5 1 FT 808 FOUND OVERLOSDR YENA20140910186Flap System · malfunctionedDURING FINAL APPROACH, SELECTED FLAPS 2 AND RECEIVED A F/CTRL FLAPS LOCKED WING TIP BRAKE ON ECAM. ACCOMPLISHED FLAPS/SLATS SYS RESET IAW AMM 27-50-00. NO FAULTS NOTED ON FLAP/SLATS, OPS CHECK NORMAL.SDR REXA2014090900886Bpsu · failedFLAPS FAIL CAUTION MSG. PERFORMED TROUBLESHOOTING IAW FIM CHAPTER 27-580-00 REV 47 IAW AD 2009-06-12 PARAGRAPH H 6 I AMOC DATED APRIL 22,2014 & TS001100-2014 FIM TECHNICAL SUPPLEMENT. TROUBLE SHOT WRING IAW FIM, CHANGED RT BPSU IAW 27-51-10. FLAP FAIL CODESSDR UHLA2014090600612Rod · out of rigFLAP FAIL DURING RETRACTION, ACFT DIVERTED. NO EMERGENCY DECLARED. FOUND RT INBD TRAILING FLAP OUT OF RIG. RIGGED RIGHT INBD FLAP AND R & R RODS. R & R RT INBD CANOE FAIRING REF MM 52-54-30.SDR SWIA201439249Flap System · false indicationFLAP ASYMETRY, CONTROL FAULT, DISAGREEMENT. FLAPS INDICATE 45A DEGREES, FLAPS SELECTED TO AND ACTUALLY AT 0A DEGREES. REPLACED FLAP ANNUNCIATOR IAW AMM, FLAPS OPS CHECKED GOOD, PN SN ON 0056, SN OFFSDR CA151220001Cam · worn(CAN) AFTER TAKE OFF IN FLAPS WERE CALLED TO BE RETRACTED FROM FLAPS APPROACH POSITION TO FLAPS ZERO. WHEN SELECTED THEY DID NOT MOVE AND WERE STUCK IN POSITION. AFTER GOING THROUGH THE APPROPRIATE CHECKLIST, IT WAS DECIDED THAT THE FLIGHT WAS OK TO CONTINUE TSDR SWIA201439289Flap System · failedFLAPS FAILED AT 20, RETURN TO FIELD. RAN QRH. RESET FLAPS IAW FIM. RAN FLAPS FIVE FULL CYCLES. OK TO CONTINUE IN SERVICE FOR 10 FLIGHT CYCLES IAW AD.SDR SWIA201439218Power Supply · failedRETURNED TO FIELD FLAP FAIL AT 0 AFTER FLAP RETRACTION. REMOVED AND REPLACED RT BPSU, OPS CHECKED GOOD IAW AMM.SDR CA140825002Drive Unit · failed(CAN) FLAPS HALF SPEED STATUS AFTER LANDING, 1 FLAP PDU INOPERATIVE WITH NO SKEW DETECT DEFERRAL M. SKEW DETECTION DUMMY BOX REMOVED AND ORIGINAL SKEW DETECTOR REINSTALLED. PDU FOUND U/S AND REPLACED WITH NEW UNIT, INSTALLED IAW AMM 27-52-01. FLAP SYS FUNCTISDR P5CA2014082500032Torque Tube · shearedFLAP DRIVE EICAS WITH OTBD T/E FLAPS SHOW ASSYMETRY AT 20 DEGREES, FOUND TORQUE TUBE COUPLING ON OTBD SIDE OF NR 2 FLAP TRANSMISSION SHEARED, REPLACED ASSOCIATED TORQUE TUBE AND TRANSMISSION.SDR P5CA2014082100031Warning Message · illuminatedFLAPS DRIVE EICAS WITH OTBD T/E FLAPS SHOW ASYMETRY AT 20 DEGREE. OPENSDR P5CA2014082100030Transformer · failedFLAPS DRIVE, R & R 1 OTBD T/E FLAP RVDT IAW AMM 27-58-01, OPS CHECK NORMAL.SDR CA140820003Control Lever · failed(CAN) ON APPROACH TO RUNWAY 22, WHEN SELECTED, THE FLAPS WOULD NOT MOVE FROM THE FLAPS 3 POSITION TO FULL FLAP. GO-AROUND WAS INITIATED DUE TO UNSTABLE APPROACH. ON SECOND ATTEMPT FLAPS MOVED TO THE CORRECT POSITION WHEN COMMANDED. TROUBLESHOT FLAP SLAT DISDR CA140819002Flap System · malfunctioned(CAN) FLAP CONTROL ISSUE IN DESCENT. GO-AROUND INITIATED, PERFORMED QRH PROCEDURE, SUBSEQUENT LANDING WITHOUT ISSUE. NO CURRENT/ACTIVE CMC MESSAGES.SDR RAIA201408180001Velocity Sensor · inoperativeFLAP FAIL AT ZERO DEGREES DURING APPROACH. MAINTENANCE INSPECTED AND REPLACED LT VELOCITY SENSOR, OPS CHECKED GOOD.SDR 9JLA201409111698Switch · failedON APPROACH THE FLAPS FAILED TO EXTEND PAST 12 DEGREES. THE CREW ABORTED THE LANDING & DIVERTED TO AN AIRPORT WITH A LONGER RUNWAY. TROUBLESHOOTING FOUND THE RT FLAP FOLLOW UP SWITCH PN 45AS61015-23 DEFECTIVE. THE SWITCH WAS REPLACED WITH AN OVERHAULED UNIT SDR SWIA201439170Computer · failedAFTER TAKEOFF, WHEN SELECTING FLAPS TO 0 DEGREE RECEIVED "FLAP DISAGREEMENT" OTBD FLAP COLUMNS DISPLAYING TWO ROWS OF LIGHTS, ALL OTHER COLUMNS SHOWED NO LIGHTS. SELECTED FLAPS 15A IAW QRH AND LANDED. CLEANED AND INSPECTED OTBD FLAP ROLLERS AND REPLACED FLAP SDR CA140811011Clutch · undertorqued(CAN) ON FLAP EXTENSION TO 15 UNITS AND BEYOND, THE AIRCRAFT EXPERIENCES A ROLL THAT REQUIRES A TRIM INPUT. WHEN THE FLAPS ARE AT 15, 1.5 UNITS LT ROLL TRIM REQUIRED TO KEEP AIRCRAFT LEVEL. WHEN THE FLAPS ARE AT 30, 2.5 UNITS OF LT ROLL TRIM TO KEEP AIRCRAFT LSDR FDEA201408082118Gimbal Joint · contaminatedON FINAL SELECTED FLAPS 20 & IMMEDIATELY GOT 2 FLAP SYS 1 & 2 FAULT LIGHTS. ELECTED TO GO AROUND & FOLLOWED ECAM & QRH PROCEDURES. AFTER LANDING, FLAP HANDLE SELECTED UP & THEY RETRACTED NORMALLY. FOUND TRACK 1 AND 2 GIMBLES ON BOTH WINGS WITH WATER UNDER SDR 9JLA201408131696Flap · malfunctionedTHE TE FLAPS FAILED TO EXTEND PAST 10 DEGREES ON APPROACH. ONCE ON THE GND THE FLAPS OPERATED CORRECTLY. THEN FLAP SYS WAS INSPECTED FOR DAMAGE & CLEARANCES AT THE UP POSITION, PERFORMED FUNCTIONAL TEST & OPERATIONAL TESTS, FLAP ASYMMETRY TESTS & LT & RT DEFSDR AWKA20140821784Controller · faultyDURING CLIMB OUT FLIGHT CREW RECEIVED A FLAPS FAIL CAS MSG WHILE THE FLAPS WERE IN THE UP POSITION, REPEAT ISSUE. THE DECISION WAS MADE TO DIVERT & AN EMER LANDING WAS DECLARED. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. A FAULTY RT FLAP POSITION RESOLVER PN 9SDR P5CA2014080500024Ball Screw · nickedDURING NR 5 BALLSCREW LUBRICATION, FOUND A NICK ON NR 5 BALLSCREW. REPLACED NR 5 BALLSCREW ASSY AND OPS CHECK NORMAL IAW AMM 27-51-41.SDR E4EB2014073112892Flap System · unknownNR 1 L/E FLAP INDICATION GREEN LIGHTS DO NOT ILLUMINATE WHEN FLAPS SELECTED TO FULL DOWN.SDR CA140728022Shaft · cracked(CAN) DURING AN A, B, C STRUCTURAL INSPECTION CHECK MAINTENANCE NOTICED THAT THE LT INBD FLAP ACTUATOR SHAFT ASSY PN 101-380000-1 WAS PULLED AWAY FROM THE "B" NUT SECURING IT TO THE FLAP GEARBOX. THE SHAFT ASSLY WAS R & R WITH A NEW UNIT. THE SYS WAS FUNCTIOSDR SWIA201438825Flap System · malfunctionedFLAP MESSAGE MAP CONTROL FAULT ON MAP WHEN HANDLE WAS SELECTED BETWEEN 0 AND 15 DEGREES. RESET FLAP SYSTEM AND PERFORMED FULL EXTENDS AND RETRACTS IAW AMM.SDR CA140717011Bushing · loose(CAN) DURING SCHEDULED INSPECTION THE FLAP ACTUATOR SHAFT GUIDE BUSHING WAS FOUND LOOSE & SLIDING BACK & FORTH WITH THE ACTUATOR SHAFT. ASSEMBLY CLEANED & INSPECTED, NO FAULT FOUND, BUSING RE-INSTALLED WITH LOCTITE RETAINING COMPOUND.SDR USAA2014071500008Computer · faultyAFTER TAKEOFF CREW RECEIVED A CAUTION FLIGHT CONTROL FLAPS LOCKED, WING TIP BRAKE ON SLAT SYS 1 FAULT. THE CAPTAIN ELECTED TO RETURN & THE FLIGHT DECLARED AN EMER LANDED WITHOUT FULL FLAPS & TAXIED TO THE GATE. CFR EQUIPMENT DID RESPOND. REPLACED SFCC NR 1SDR 2014FA0000418Cable · failedFLAP FAILURE OCCURRED WHILE PRACTICING POWER OFF STALLS. LT FLAP FAILED TO RETRACT DUE TO THE FLAP CABLE SWAGED BALL PULLED THROUGH THE FLAP DRIVE PULLEY GROOVE. THE LOAD BEARING WASHER WAS NOT POSITIONED BETWEEN THE SWAGGED BALL ON THE END OF THE CABLE AND SDR A6WA201441737Flap · malfunctionedFLAPS FAILED ON APPROACH AT 4000 FT WITH NO FLAP SELECTION. PERFORMED FLAP RESET PROCEDURE IAW SUP 98-18F BOX 12. FLAPS RESET, PLACARDED & PLACED ON MEL.SDR VNAA2014070500004Control Unit · failedCREW REPORTED FLAPS FAIL AMBER MESSAGE AT FLAPS 8 DEGREES AFTER TAKEOFF. FLAPS WOULD NOT RETRACT TO ZERO DEGREES. CREW DECLARED EMERGENCY, RETURNED TO FIELD AND LANDED SAFELY. MAINTENANCE TROUBLESHOT FLAP SYS, R & R FLAP ELECTRONIC CONTROL UNIT, FECU, AND PERSDR FDEA201407031618Jackscrew · contaminatedON APPROACH TO MEM FLAPS STUCK AT 15 DEG. PER A300-600 TSM 27-50-00, BITE CHECK OF SFCC 1 AND 2 SHOW FAULT FOR BOTH SFCC. RESET BOTH SFCC. FOUND LEFT WING TORQUE LIMITER POPPED. LUBED ALL BALL NUTS FOR SCREWJACKS ON LEFT WING. FOUND WATER IN NR 2 BALL NUTSDR A6WA201441730Flap · failedFLAPS FAIL CAUTION MSG ON APPROACH. FAILED AT 20 DEGREE DETENT. COMPLIED WITH QRH.SDR SWIA201438589Flap System · failedFLAPS FAIL AT 8, RETRACTED FROM 8 TO 0. RESET FLAPS IAW FIM. RAN FLAPS 5 FULL CYCLES.
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