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 CA130719001Gear · damaged(CAN) DURING FLAP MOTOR OPS CHECK, TASK 27-51-00-710 PART OF THE OPS 1-2 INSPECTION, WHERE BOTH CONTROL SIDE OF THE FLAP ARE TESTED INDEPENDENTLY, THE RIGHT FLAP GEARBOX WAS DRIVING THE FLAPS ERRATICALLY BY SEQUENCE MAKING BIG (BANG) NOISE. THE FLAP MOTOR AND SDR REXA2013071401361Pdu · failedFLAP FAILED IAW FECU READ OUT. FOUND LT INBOUND FLAPS JAMMING AT 8 DEG AND RT PDU MOTOR BRAKE FAILURE. ADJUSTED LEFT INBD FLAP ACTUATORS IAW AMM 27-53-00. ALSO FLAP PDU WAS REPLACED.SDR R61A201307130614Torque Tube · corrodedWHILE ACFT WAS IN FOR HEAVY CHECK FOUND RT FLAP TORQUE TUBE NR 6 HAS CORROSION TO MALE END. MX R & R RT FLAP TORQUE TUBE F6 IAW AMM 27-51-03, PN 5912949-3. ACFT WAS RETURNED TO SERVICE.SDR A6WA201307124024Control Unit · malfunctionedFLAP FAIL AT 20 DEGREES DURING APPROACH.. FLAPS WERE AT 20 FOR A COUPLE OF MINUTES, APPROACH WAS IN HEAVY RAIN. PERFORMED FLAP RESET PROCEDURE IAW SUPP 98-18F, BOX 12, FLAPS RESET. INTEREGATED FECU REF 27-51 AT SUPP 98-018F. R & R FECU IAW AMM 2751. OPS CSDR CA130722004Gear · damaged(CAN) DURING FLAP MOTOR OPS CHECK,TASK 27-51-00-710 PART OF THE OPS 1-2 INSPECTION, WHERE BOTH CONTROL SIDES OF THE FLAP ARE TESTED INDEPENDENTLY, THE RIGHT FLAP GEARBOX WAS DRIVING THE FLAPS ERRATICALLY BY SEQUENCE MAKING BIG (BANG) NOISES. THE FLAP MOTOR ANDSDR CA130708003Spacer · missing(CAN) IT WAS REPORTED TO MAINTENANCE THAT THE FLAPS HAD STUCK IN THE UP POSITION. MAINTENANCE FOUND THE PRELOAD SHIM MISSING FROM THE RT FLAP. THERE WAS ENOUGH GLUE ON THE FLAP AREA TO PARTIALLY ADHERE IT TO THE WING FAIRING. THIS CAUSED THE FLAP TO STICK WHSDR REXA2013070401333Unknown · unknownFLAPS FAIL CAUTION AT ZERO, NOTICED AFTER BLOCKING OUT. FLAPS NOT SELECTED OUT OF ZERO. MAY OR MAY NOT BE RELATED TO ACFT BEING POWERED OFF OF A GPU BEFORE BLOCKING OUT. FLAPS RESET SUCCESSFULLY.SDR REXA2013070401332Warning Message · illuminatedFLAPS FAIL CAUTION MESSAGE.SDR A6WA20130418003Control Lever · failedRECEIVED FLAPS FAIL CAUTION MSSG INFLT FLAPS ARE AT 30 DEGREES. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPP. 98-18F BOX 12. FLAPS RESET. PERFORMED TROUBLESHOOTING IAW FIM PROBABLE CAUSE IS FLAP CONTROL LEVER. R & R FLAP CONTROL LEVER IAW AMM 27-51-01 OPS CSDR REXA201306271217Flap System · failedFLAPS FAILED AT 17 DEGREES ON LANDING AT RETRACTION.SDR REXA2013006261214Flap System · malfunctionedFLAPS DEGRADED STATUS MESSAGE, COMPLETED OPS TEST OF SKEW DETECTION SYS (IBIT) AND RESET SYS MESSAGE WENT AWAY OPERATED FLAPS THROUGH MESSAGE DID NOT RETURN, WORK DONE IAW FIM 27-50-00 AND AMM 27-51-15.SDR REXA201306261213Flap System · malfunctionedFLAPS DEGRADED STATUS MESSAGE, COMPLETED OPS TEST OF SKEW DETECTION SYSTEM (IBIT) AND RESET SYS, MESSAGE WENT AWAY, OPERATED FLAPS THROUGH, MESSAGE DID NOT RETURN. WORK DONE IAW FIM 27-50-00 AND AMM 27-51-15SDR REXA2013006251216Control Unit · failedFLAPS FAILED AT ZERO AT GATE, AFTER PUSHBACK AND AFTER ENGINE START. FLAPS WERE NOT SELECTED OUT OF ZERO. R & R FECU IAW AMM 27-51-05. ACFT OK FOR SVC. PERFORMED TROUBLESHOOTING IAW FIM REV 44 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I), AMOC DATED DECEMBER 07,201SDR ERAA201306250040Drive Shaft · kinkedFLAP DRIVE CAUTION LIGHT ILLUMINATED. RETURNED TO GATE. REPLACED LT INBD SECONDARY FLAP DRIVE CABLE IAW MM 27-52-11. FLAP SYSTEM OPS CHECKED OK.SDR GLBA2013062400264Motor · odorPILOT REPORTED THAT THEY SMELLED ELECTRICAL SMOKE IN THE AFT CABIN DURING SHUTDOWN. REPLACED THE FLAP MOTOR, SYS OPS CHECKED GOOD, NO BURNING ODOR NOTED.SDR REXA2013062401207Control Unit · failedFLAPS FAIL AT ZERO ON ACFT POWER UP. REPLACED FECU IAW AMM 27-51-05, OPS CHECKED GOOD.SDR REXA2013062101209Drive Unit · malfunctionedFLAPS HALFSPEED STATUS MESSAGE. R & R FLAP POWER DRIVE UNIT IAW AMM 27-52-01. OPS CHECK OF FLAP IAW AMM 27-54-00. OPSS CHECK GOOD.SDR REXA2013062101208Sdu · abnormalFLAPS FAILED CAUTION MESSAGE WHEN SELECTING FLAPS 20 ON GROUND. PERFORMED TROUBLESHOOTING IAW FIM, REV 44 IAW AD 2009-06-12, PARA (H)(6)(I) AMOC AND PA AD 27-052L. FOUND TO BE CAUSED BY INCORRECTLY RESET SDU. COMPLETED RESET IAW AMM 27-51-15. FLAPS SYS OPS SDR SWAA2013062417486Flap · out of adjustRT WING INBOARD AFT FLAP OUT OF ADJUSTMENT. ADJUSTED AFT FLAP IAW MM.SDR CA130620007Rod · bent(CAN) FOUND LT INBD FLAP TRACK MECHANISM LOWER ROD BENT AND RT INBD FLAP TRACK NR 2 MECHANISM LOWER ROD BENT. FOUND BOTH INBD AFT FLAPS TO BE OUT OF RIG. MECHANICAL RIGGING OF LT AFT FLAP, FLAP TRACK 1 & 2, C/OUT IAW AMM 27-50-00-820-801-1. CHECKS SERVICEABSDR CA130620002Flap System · out of rig(CAN) LEFT INBD LOWER ROD ON NR 1 FLAP TRACK FOUND BENT ON ARRIVAL. AFTER MECHANICAL RIGGING COMPLETED FOUND INBD FLAP MECHANISM UPPER AND LOWER RODS AND FLAP MECHANISM NR 2 UPPER AND LOWER RODS NOT PROPERLY ADJUSTED. MECHANICAL RIGGING OF LT AFT FLAP, FLAP TRSDR USAA2013061900002Unknown · malfunctionedON DESCENT, CREW RECEIVED A F/CTL FLAP FAULT. T/E DID NOT EXTEND BUT L/E POSITION 2 WITH FLAPS 3 SELECTED. CREW PERFORMED ECAM/NON NORMAL PROCEDURE AND LANDED WITHOUT INCIDENT. MX ACCOMPLISHED TROUBLESHOOTING TASK 27-51-00-810-810-A. PERFORMED DETAILED VISSDR REXA2013061301182Flap System · unknownFLAPS HALF SPEED.SDR R61A201306110530Control Handle · brokenDURING APPROACH, CREW REPORTED THAT THE FLAPS WERE STUCK BETWEEN 3 AND 5. DECLARED AN EMERGENCY. ACFT LANDED WITHOUT INCIDENT. FOUND THE SLAT/FLAP CONTROL HANDLE BROKEN AND BINDING AT POSITION 4. REPLACED HANDLE IAW AMM AND OPS CHECKED GOOD.SDR SIMA20130610006Ecu · failedDURING CRUISE, RECEIVED AN EICAS FLAP LOW SPEED AND SPS ADVANCED MESSAGES. COMPLIED WITH AOM, VOL 1 PROCEDURES. ON APPROACH EICAS FLAP FAIL MESSAGE RECEIVED. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REMOVED AND REPLASDR USAA2013061300016Strut · wornDUE TO A FLAP ISSUE, F/CTRL FLAPS LOCKED, CREW DECLARED AN EMERGENCY INBOUND. FLIGHT LANDED AND TAXIED TO THE GATE WITHOUT INCIDENT. MX TROUBLESHOT IAW TSM AND FOUND LT AND RT FLAP INTERCONNECT STRUT WORN AND OUT OF RIG. R & R LT AND RT FLAP INTERCONNECT STSDR SIMA20130610002Ecu · malfunctionedTHE CREW REPORTED THEY RECEIVED A FLAP LOW SPEED EICAS MESSAGE DURING CRUISE FOLLOWED BY FLAP FAIL UPON FLAPS 9 SELECTION. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. R & R FLAP ELECTRONIC CONTROL UNIT IAW SDR UIEA2013061000323Control Unit · inoperativeDURING APPROACH, FLAPS WOULD NOT GO TO 20 OR 25 AND TURN GREEN. FLAPS 30 SELECTED AND TRAVELED TO 30 AND WENT GREEN (LEFT FCU STATUS MSG. LEFT FCU REPLACED IAW AMM)SDR UALA2013061304094Pushrod · wornLT INBD AFT FLAP, CENTER UPPER AND LOWER PUSH ROD ENDS WORN. REPLACED ROD AND HARDWARE. VERIFIED NEW ROD AND HARDWARE ARE IN PLACE IAW IPC 27-51-02-010C.SDR USAA2013061000014Transmission · trippedENROUTE, FLIGHT CREW OBSERVED A "T/E FLAP DISAGREE" MESSAGE WITH FLAP HANDLE AT 20. DECLARED AN EMERGENCY AND EXECUTED A MISSED APPROACH IN ORDER TO PERFORM THE ALTERNATE FLAPS PROCEDURE. ON SELECTING ALTERNATE FLAPS, "T/E FLAP DISAGREE" MESSAGE DISAPPEARED.SDR USAA2013061000042Warning Switch · activatedON APPROACH, FLAPS 2 SELECTED ECAM: F/CTL FLAPS FAULT. SLATS WERE AT POSITION 3, FLAPS 0. CREW DECLARED AN EMERGENCY AND PERFORMED LANDING DISTANCE CALCULATION IAW QRH. FLIGHT LANDED SAFELY WITH EMERGENCY EQUIPMENT MEETING THE FLIGHT. MX ACCOMPLISHED FLAPS JSDR CA130613009Rod · damaged(CAN) IT HAS BEEN FOUND THAT THE C6CW1083-1 FLAP ROD WAS FOUND SCUFFED AND FOULING ON ROOT RIB C6W1035-15/16. MFG IS CONTINUING TO INVESTIGATE.SDR ASOA20130607318Flap System · out of rigFLAP FAIL MESSAGE INFLIGHT. PERFORMED FLAP RIGGING. OPS CHECK GOOD, ACFT RELEASED AND RETURNED TO SERVICE.SDR FDEA201306051202Screw · brokenFLAP HANDLE WOULD NOT RETRACT AFTER TAKEOFF. FOUND FLAP HANDLE SCREW BROKEN REPLACE REF EO 6-2750-7-5006, PART 1.SDR REXA2013060401063Flap · failedFLAPS FAIL WHEN THEY REACHED 30 DEG ON APPROACH LEVEL AT 4000 FT., 175KTS, 21C - 70MIN IN TO FLIGHT.SDR CA130603010Flap System · failed(CAN) AT APPROX 10, 000FT CREW GOT AN EICAS MSG FOR FLAP/SLAT FAILURE. DECLARED A PAN PAN WITH ATC. ATC CHANGED ARRIVAL RWY TO 08R FOR AN INTO WIND APPROACH ON THE LONG RWY. EMERG TRUCKS WERE CALLED OUT AND WERE WAITING FOR AC565`S ARRIVAL. FLAPLESS LANDING WASDR REXA2013060201046Bpsu · failedFLAPS FAIL CAUTION MESSAGE WHEN SELECTING FLAPS FROM 0 TO 20 AFTER ENGINE START PERFORMED TROUBLESHOOTING IAW FIM REV 44 IAW AD 2009-06-12 PARA (H)(6)(I) AMOC DATED DECEMBER 07,2012,AND PA AD27-05 2L. R & R LT BPSU IAW AMM 27-51-10. OPC GOOD, COULD NOT DUPLICASDR REXA2013060201038Bpsu · failed"FLAPS FAIL" CAUTION MESSAGE WHEN SELECTING FLAPS FROM 0 TO 20 AFTER ENGINE START. PERFORMED TROUBLESHOOTING IAW FIM REV 44 IAW AD 2009-06-12, PARA H.6.I AMOC DATED DECEMBER 07,2012, AND AD27-05 2L. R & R LT BPSU IAW AMM 27-51-10. OPS CHECK GOOD, COULD NOT DSDR REXA2013053101043Flap · failedFLAPS FAIL WHEN THEY REACHED 30 DEG ON APPROACH LEVEL AT 4000FT. 175KTS -21C-70 MIN IN TO FLIGHT ACFT LANDED SAFELY , UNKNOWN IF EMERGENCY WAS DECLARED. COMPLIED WITH MEL 27-50-00, NO RECENT HISTORY OF ISSUES WITH THE FLAPS.SDR AALA20130531063Fseu · inoperativeCREW REPORTED FLAP ASYMMETRY DURING DESCENT. ACCOMPLISHED QRH PROCEDURES AND RAISED FLAPS. EMERGENCY DECLARED, FLIGHT LANDED WITHOUT INCIDENT. REPLACED FLAP SLAT ELECTRONICS UNIT. SYS GROUND CHECK NORMAL OPERATION.SDR CA130604007Rod End · corroded(CAN) DURING INSPECTION IT WAS FOUND THAT THE ROD ENDS THAT ATTACH TO THE FLAP WERE BOTH CORRODED TO THE POINT WHERE MOVEMENT OF THE ROD END BALL WAS DIFFICULT. THE DIAMOND MANUAL DOES NOT ALLOW FOR LUBRICATION OF THESE ROD ENDS AS THEY ARE TEFLON LINED. (TC# SDR CA130610010Control Unit · failed(CAN) THE FLIGHT CREW HAD A SLAT FLAP HALFSPEED MESSAGE WITH NR 2 SFCU POWER CB POPPED THAT WILL NOT RESET. TECH FOUND NR 2 SFCU WITH BURN MARKS ON COVER AND BURNED ELECTRONIC ODOR. THE FLIGHT CREW COULD SMELL THE SMOKE IN THE COCKPIT AND THE "SMOKE" EICAS WSDR REXA2013052801029Flap · malfunctionedFLAPS FAIL CAUTION MESSAGE DURING AFTER START CHECKLIST WHILE MOVING FLAPS FROM ZERO TO 20 DEGREES ON THE GROUND. FLAPS STOPPED AT ZERO, OAT 14 DEGREES FAILED DURING EXTENSION. PERFORMED SDU RESET PROCEDURES, OPS CHECK GOOD IAW MEL PROCEDURES 27-51-14.SDR CA130604011Relay · tripped(CAN) THE PILOTS WASHED THE AIRCRAFT AND THEN GOT A DISPATCH (THE FLAPS WHERE DOWN FOR WASHING). ON THE TAXI OUT THEY SELECTED FLAPS UP BUT DID NOT NOTICE THE FLAPS HAD ONLY CAME UP TO APPROACH BEFORE THE CIRCUIT BREAKER POPPED FROM THE FLAP SYSTEM. THEY TOOK SDR CA130528001Case · failed(CAN) AFTER LANDING WHEN THE CREW SELECTED FLAPS TO ZERO, THEY CAME UP TO 15 DEG AND STOPPED AND THE FLAP DRIVE CAUTION LIGHT CAME ON. MAINTENANCE INVESTIGATION FOUND THE SECONDARY DRIVE SYS SEIZED. FURTHER INVESTIGATION FOUND THE CENTER SECTION SECONDARY DRSDR UALA2013052903733Fseu · faultyFLAP SLAT CONTROL 1 AND PFCS INTERFACE MESSAGES DISPLAYED ON LOWER EICAS DISPLAY. REPLACED FSEU NR 1, MESSAGE CLEARED AND MAT GROUND TEST PASSED OK.SDR N6WA2013052501Warning Message · illuminatedFLAPS HALFSPEED STATUS MESSAGE. CLEARED INHIBITS AND PERFORMED OPS CHECK OF SFECU IAW AMM 27-51-05. OP'S CHECK GOOD AT THIS TIME.SDR SWAA2013052316421Roller · out of adjustLEFT WING INBD AFT FLAP LOOSE. ADJUSTED ROLLERS IAW AMM.SDR SWAA2013052316420Flap · looseRIGHT WING INBD AFT FLAP LOOSE. ADJUSTED AFT FLAP IAW AMM.SDR REXA2013052000897Ecu · failedFLAP FAIL ON GROUND SETTING FLAPS 20 FOR TAKEOFF LEFT FLAP INDICATING 0 DEGREES RIGHT FLAP INDICATING 2 DEGREES PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 44 IAW AD 2009-06-12 PARAGRAPH H.6.I, AMOC DATED DECEMBER 07,2012 AND PA AD27-052L. REMOVED AND RE
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