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 REXA2013112702283Shaft · lack of lubeFLAP FAIL AT 20 DEGREES. PERFORMED TROUBLESHOOTING IAW FIM REV 45 IAW AD 2009-06-12 PARAGRAPH H 6 I IAW AMOC DATED JULY 22, 2013 & PA AD27-052N. PERFORMED FLEX SHAFT LUBE IAW CHECKLIST & AMM 27-53-10, OPERATIONS CHECKED GOOD.SDR UHLA2013112700615Psu · failedFLAP FAIL AT 2300 FT, GOING FROM FLAP 1 TO FLAP 2, FOLLOWED QRH, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED FIM, R & R RT PSU IAW AMM 27-53-04 (NO FIX, REINSTALLED ORIGINAL), REATTACHED TORQUE TUBE, ADJUSTED RT ACTUATOR, PERFORMED ELECTRICAL RIGGINSDR SWAA2013120222858Electronic Unit · faultyDECLARED EMERGENCY DURING LANDING TE FLAPS WOULD NOT EXCEED BEYOND 5. R & R FLAPS ELECTRONIC UNIT IAW MM.SDR IPXA2013112700955Shutoff Valve · inoperativeAIR TURNBACK DUE TO FLAPS WOULD NOT MOVE WHEN SELECTED FROM 5 TO 10 DEGREES. REPLACED FLAP/SLAT SHUTOFF VALVE IAW AMM 27-51-48-022-001.SDR IPXA2013112700969Flap System · inoperativeATB -DURING CLIMB FLAPS WOULD NOT RETRACT. EMERGENCY DECLARED PERFORMED FSEU BITE IAW FIM 27-51-00-815. NO FAULTS NOTED. CYCLED FLAPS SEVERAL TIMES. SYS WORKING OK.SDR SIMA20131123001Ecu · malfunctionedON FINAL APPROACH INTO AIRPORT FLAP FAIL MESSAGE ON EICAS RESULTING IN FLAPS FAILING AT 0. R & R FECU IAW EMB 145 AMM 27-53-02, OPERATIONS CHECKED GOOD.SDR R61A201311221261Torque Tube · corrodedDURING HEAVY CHECK, RT WING TORQUE TUBES F5, F6 ARE CORRODED. MX R & R TORQUE TUBES IAW AMM 27-51-03.SDR CALA2013112593212Lever · bindingIN FLIGHT ONLY FLAPS DIFFICULT TO RETRACT PAST 1 & TO EXTEND PAST 1 FLAP LEVER. FOUND FLAP HANDLE MECH BINDING. REPLACED FLAP & SLAT CONTROL LEVER, FLAP LEVER OPERATION NORMAL.SDR CALA2013112293202Fseu · faultyEICAS MSG TE FLAP DISAGREE & TE FLAP LIGHT ILLUMINATED, WHEN FLAP LEVER & INDICATOR IN SAME POSITION. INTERMEDIATE TE FLAP DISAGREE DURING TAXI WITH FLAPS SET TO 15, ITEM ROLLED FORWARD. ADJUSTED OTBD SLAT PDU SENSOR M548, CHECKED ADJUSTMENT OF FLAP LEVER POSDR REXA2013112002264Ecu · malfunctionedFLAPS FAILED MESSAGE ON ED1 WHEN FLAPS WERE ATTEMPTED TO BE MOVED FROM 0 TO 20. PERFORMED TROUBLESHOOTING IAW FIM REV 45 IAW AD 2009-06-12 PARAGRAPH H 6 I, AMOC DATED JULY 22, 2013 & PA AD 27-052N. REPLACED FECU IAW AMM 27-51-05-04, OPERATIONS CHECKED GOOD ISDR 2013FA0000643Control Rod · wornRT FLAP CONTROL ROD HAS EXCESSIVE PLAY CAUSED BY THE URETHANE INSULATOR THAT IS MOUNTED BETWEEN 2 METAL CONTROL ROD SECTIONS AND HELD TOGETHER BY MS27039-1-23 SCREWS. THE HOLES IN THIS ASSY ELONGATED BEYOND MFG LIMITS. THIS IS A CONTINUAL ISSUE WITH THESE LTSDR 2013FA0000642Control Rod · wornRIGHT FLAP CONTROL ROD HAS EXCESSIVE PLAY. THE ROD ASSY IS PN LA57266102 WHICH IS CONSTRUCTED BY PN'S 286102-8 FOR THE URETHANE INSULATOR AND PN'S 2562102-3 AND 2862102-1. THE URETHANE INSULATOR IS MOUNTED BETWEEN BOTH METAL CONTROL RODSECTIONS AND HELD TOGESDR 2013FA0000641Control Rod · wornLEFT FLAP CONTROL ROD HAS EXCESSIVE PLAY. THE ROD ASSEMBLY IS PN LA57263101 WHICH IS CONTRUCTED BY PN 286102-8 FOR THE URETHANE INSULATOR AND PN 2562102-3 AND 2862102-1. THE URETHANE INSULATOR IS MOUNTED IN BETWEEN BOTH METAL CONTROL ROD SECTIONS AND HELD TOGESDR WAIA2014F00049Flap System · malfunctionedDURING APPROACH, FLIGHT CREW REPORTED FLAPS WOULD NOT EXTEND. AN EMERGENCY WAS DECLEARED AND MADE AN UNEVENTFUL LANDING. PERFORMED BRAKE AND POSITION SENSOR UNIT (BPSU) TEST IAW MM 27-51-10, TASK 27-51-10-740-801 AND PERFORMED BITE TEST OF THE BRAKE AND POSDR USAA2013111800006Transmitter · out of adjustEN-ROUTE, FLAPS LOCKED OUT AT 20 DEGREE DURING APPROACH, AND WOULD NOT EXTEND OR RETRACT. DID NOT USE ALTERNATE FLAP EXTENSION. THE FLIGHT DID A GO AROUND WHILE THE FLIGHT CREW ATTEMPTED TO CORRECT THE PROBLEM. THE ISSUE COULD NOT BE RESOLVED, SO THE CREW DSDR CA131115001Drive Assy · failed(CAN) WHILE BACK TRACKING ON THE RUNWAY, FLAPS WE RETRACTED BY FLIGHT CREW AND SHORTLY AFTER A BURNING ODOR WAS NOTICED IN THE CABIN. THE ACFT RETURNED TO THE APRON AND PASSENGERS WERE DEPLANED. THE FLIGHT CREW VISUALLY NOTED THAT THE RT INBD FLAP WAS IN THESDR CHQA20131108409Velocity Sensor · out of toleranceCREW REPORTED A FLAP FAIL MESSAGE ON APPROACH. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT AT DESTINATION. MAINTENANCE RESET FLAP SYSTEM AND NO DEFECTS WERE NOTED. MAINTENANCE REPLACED THE RT VELOCITY SENSOR. OPS CHECKED GOOD WITH NO FURTHER DEFECTS SDR CA131108003Controller · failed(CAN) ENROUTE FLIGHT EXPERIENCED A "FLAP FAIL" ECAM MESSAGE. QRH WAS CARRIED OUT AND ATC WAS ADVISED WITH A PAN DECLARED. THE ACFT LANDED WITHOUT FURTHER INCIDENT. THE ACFT STOPPED ON THE RUNWAY FOR EMERGENCY RESPONSE SERVICES TO INSPECT THE ACFT BEFORE TAXISDR R61A201311071137Torque Tube · corrodedDURING HEAVY CHECK, LT WING F6 TORQUE TUBE HAS PITTING ON SPLINES AT MALE END. MX REMOVED F6 TORQUE TUBE REPLACED SPLINE END IAW SRM 51-40-02. RE-INSTALLED F6 TORQUE TUBE IAW AMM 27-51-03 SEE CONTINUATION CARD FOR WORK ACCOMPLISHED. PN 5913246 UNIVERSAL JOSDR R61A201311071136Joint · corrodedDURING HEAVY CHECK, LT WING FLAP TORQUE TUBE F5 HAS PITTING ON SPLINES AT MALE END. MX R & R LT WING F5 TORQUE TUBE MALE SPLINE END IAW SRM 51-40-02. RE-INSTALLED LT WING F5 TORQUE TUBE IAW AMM 27-51-03 SEE CONTINUATION CARD FOR WORK ACCOMPLISHED. PN 59132SDR USAA2013110800003Computer · faultyCREW RECEIVED A FLT CONTROL FLAP SYS 1 FAULT DURING CRUISE. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE R & R SFCC 1. CHECKED GOOD IAW AMM 27-51-34. ACFT OK FOR SERVICE.SDR VNAA2013110600004Position Sensor · failedCREW REPORTED FLAPS FAIL MESSAGE AT ZERO DEGREES DURING EXTENSION ON DESCENT. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MX TROUBLESHOT FLAP SYS IAW FAULT ISOLATION MANUAL. MX R & R RT BPSU AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.SDR 2013FA0000630Resolver · failedCREW PERFORMED "PRIOR TO TAXI" CHECKLIST AND DISCOVERED FLAPS WERE STUCK BETWEEN 15 - 20 DEGREES. SHUTDOWN ACFT. MAINTENANCE TROUBLESHOT DISCREPANCY TO A DEFECTIVE LT FLAP CONTROL POSITION RESOLVER. ABLE TO DRIVE THE FLAPS ALL THE WAY UP TO 0 DEGREES USING TSDR REXA2013110101794Flap System · malfunctionedFLAP FAILED AT 45 DEGREES ON GROUND, DURING FLAP RETRACTION FROM 45 DEGREES TO 0 DEGREES WITH OAT OF 20 DEGREES C. RESET FLAP SYSTEM AND PERFORMED FIVE CONSECUTIVE FLAP CYCLES, MAINTENANCE PERFORMED IAW FIM 27-50-00. PERFORMED TROUBLESHOOTING IAW FIM RESDR IPXA2013611010736Relay · inoperativeDURING CLIMBOUT, FLAP INDICATOR DISPLAYED POS 1 WITH THE FLAP LEVER IN THE UP OR ZERO POSITION. NO EICAS MESSAGE DISPLAYED. NO WARNINGS OR CAUTION LIGHTS ILLUMINATED. SPEED REMAINED WITHIN LIMITS. ACCOMPLISHED FIM27-58-00-815-803, UP TO BLK 36. PERFORMEDSDR CA131101004Shaft · sheared(CAN) ON CLIMBOUT, CREW SELECTED FLAPS UP AND NOTICED THAT THEY DID NOT RETRACT, FLIGHT SERVICES WERE NOTIFIED THAT THEY WERE RETURNING TO THE AIRPORT. MAINTENANCE INSPECTED THE SYS AND FOUND THAT THE SPLIT FLAP SYS HAD ACTIVATED. SPLIT FLAP BY PASS SWITCH WSDR A6WA201310294038Control Unit · malfunctionedTO SHORTLY AFTER FLAP RETRACTION, "STAB AND MACH TRIM CAUTION" MSGS APPEARED AND WOULD NOT CLEAR. DIVERTED, LDG WT 38000. INTERROGATED MDC HSTCU 270, BIT 14 SET FOR DISCONNECT SWITCH. CW FIM FAULT RESET PROCEEDURE-NO FIX. RERACKED HSTCU REF AMM 27-41-01. SDR SWIA201335127Computer · malfunctionedFLAPS DISAGREE DURING DESCENT. PERFORMED GO-ROUND. RECYCLED FLAPS SEVERAL TIMES & FINALLY ALL FLAP PAIRS CAME DOWN. FLT 5405 REPLACED FLAP CONTROL COMPUTER.SDR REXA2013102501779Bpsu · faultedFLAP FAIL EVENT. PERFORMED TROUBLESHOOTING IAW FIM REV 45 IAW AD2009-06-12, PARAGRAPH (H)(G)(I). AMOC DATED JULY 22, 2013 AND PA AD2727-052M. PERFORMED WIRE CHECKS IAW FIM 27-50-00, FOUND BPSU INTERNAL CIRCUIT FAULTY. R & R RT BPSU IAW AMM 27-51-10. ALL CSDR REXA2013102501777Detector · out of adjustFLAPS FAIL CAUTION MSG WHEN SELECTING FLAPS TO 20 ON THE AFTER START CHECK. ACFT WILL NEED A REPLACEMENT FLAP FAIL EVENT CARD. PERFORMED TROUBLESHOOTING IAW FIM, REV 44 IAW AD 2009-06-12, PARA H6I AMOL DATED DECEMBER 07.2012 AND PA AD 27-052L. FOUND SKEW DESDR R61A201310231066Torque Tube · corrodedDURING HEAVY CHECK, REPORTED RT WING NR 6 FLAP TORQUE TUBE INBD END CORRODED AT GEAR BOX. MX R & R NR 6 FLAP TORQUE TUBE IAW AMM 27-51-03.SDR R61A201310231060Torque Tube · corrodedDURING HEAVY CHECK, LT WING NR 5 FLAP TOQUE TUBE OTBD END CORRODED AT GEAR BOX. MX R & R NR 5 FLAP TORQUE TUBE IAW EMB 27-51-03, PN 5912949-2, FLAP TORQUE TUBE.SDR R61A201310231059Torque Tube · corrodedDURING HEAVY CHECK, LT WING FLAP TORQUE TUBE NR 6 INBD END CORRODED AT GEARBOX. MX R & R NR 6 FLAP TORQUE TUBE IAW AMM 27-51-03. PN 5912949-3 TORQUE TUBE. ACFT REMAINS UNTIL COMPLETION OF HEAVY CHECK.SDR R61A201310231058Torque Tube · corrodedDURING HEAVY CHECK, RT WING NR 5 FLAP TORQUE TUBE OTBD CORRODED AT GEARBOX. MX R & R NR 5 FLAP TORQUE TUBE IAW AMM 27-51-03. PN 5912949-2 TUBE NR 5. AIRCRAFT REMAINS UNTIL HEAVY CHECK IS COMPLETED.SDR A6WA201310244036Flap System · failedFLAPS FAIL AT 30 DEGREES. PERFORMED FLAP RESET PROCEDURE IAW SUPPLEMENT 98-018F BOX 12. FLAPS RESET.SDR R61A201310201040Torque Tube · corrodedDURING HEAVY CHECK, LT WING FLAP TORQUE TUBE F5 MALE SPLINES ARE CORRODED. MX R & R TORQUE TUBE IAW AMM 27-51-03,SDR CALA2013102292245Flap · damagedRT INBD FORE FLAP TE RT WING FOUND DAMAGE 6FT FROM WING ROOT. 47 INCHES OF DAMAGE FROM END TO END. REMOVED RT WING INBD FORE FLAP IAW AMM. ROUTED TO SHOP 321 FOR REPAIR. REPLACED & REPAIRED FOREFLAP & PERFORMED OPERATIONAL CHECK IAW AMM.SDR 2013FA0000603Resolver · intermittentCREW REPORT ON APPROACH AT 5000' SLAT/ FLAP ADVISORY CAS MESSAGE ILLUMINATED WHEN FLAPS SYS CONFIGURED TO 16 DEGREES, FLAP FAILED AT 15 DEGREES AND AMBER CAS "FLAP FAILED" ILLUMINATED. MAINTENANCE PERSON WITH PILOT PERFORMED THE SLAT/ FLAP SYSTEM RESET PROCEDSDR FDEA201310152506Limiter · trippedDURING FINAL, TRIED LOWERING FLAPS AND RECEIVED A FLAPS 1/2 SYS FAULT. CYCLED HANDLE NO FLAPS EXTENDED. FOUND WHEEL WELL TORQUE LIMITER FOR RT WING FLAP DRIVE TRIPPED. RESET LIMITER. INSPECTED RT WING FLAP TRANSMISSION TORQUE LIMITERS NOT TRIPPED. NR 1 SFSDR S9BA201300006Control Valve · failedFLAPS FAILED TO EXTEND ON APPROACH. R & R FLAP CONTROL VALVE IAW AMM 27-51.SDR 2014F00033Control Unit · malfunctionedDURING APPROACH, FLAPS WOULD NOT TRANSITION PAST 10 DEGREES WHEN SELECTED FROM 10 TO 20, FOLLOWED BY PRIMARY FLAPS FAIL AND FLAP COMMAND INVALID CAS MESSAGE. FOLLOWED PROCEDURE IN AFM IN BOTH NORMAL AND ALTERNATE MODES WITH NO RESOLUTION. ADVISED TO CONTINUSDR CA131010001Selector · leaking(CAN) DURING FLIGHT, THE CREW NOTICED THE HYDRAULIC SYS PRESSURE INDICATION WAS ZERO AND A LARGE QTY OF HYDRAULIC FLUID WAS VISIBLE IN THE CENTER CABIN AREA DRIPPING FROM THE CABIN CEILING. ACFT RETURNED TO BASE FOR MAINTENANCE. INVESTIGATION REVEALED THAT THSDR CALA2013100991921Handle · stiffFLAP HANDLE STIFF, STICKS WHEN EXTENDING & RETRACTING FLAPS. LUBE FLAP HANDLE, OPERATIONS CHECKED OK.SDR A6WA201310094034Flap System · malfunctionedDURING CLIMB OUT, AFTER FLAPS WERE RETRACTED TO ZERO FOR A FEW SECONDS, RECEIVED A FLAP FAIL CAUTION MESSAGE. RETURNED TO DEPARTURE, LANDED FLAPS 0, BRAKE TEMPS NORMAL, WT 46800.
SDR YENA20131006209Flap System · malfunctionedCREW DECLARED AN EMERGENCY AND ACFT DIVERTED DUE TO FCTL FLAPS LOCKED. ALIGNMENT FAULT ECAM ON LANDING. INSPECTED INTEGRITY OF LT FLAP MECHANISM IAW TSM 27-51-00. NO FAULTS NOTED. RESET SYS, ACCOMPLISHED TEST OF FLAPS IAW AMM 27-54-00. NO FAULTS NOTED. OK SDR CALA2013100791806Computer · malfunctionedFLIGHT CONTROL FLAP SYS 2 ECAM. PLACED SFCS 2 FLAP CHANNEL INOPERATIVE IAW 2751A COMPLIED WITH MX PROCEDURES. R & R NR 2 SFCC, OPERATIONS CHECKED GOOD.SDR SWAA2013101421128Jackscrew · corrodedLT WING NR 2 FLAP TRANSMISSION CORRODED AT JACKSCREW ATTACHMENTS TO GIMBAL. R & R JACK SCREW ASSEMBLY IAW AMM.SDR CALA2013100791783Computer · faultyF-CTL FLAP SYS 2 FAULT ECAM, REPEAT. DEFERRED ON DF 923 IAW MAINT PROCEDURE NO FAULTS NOTED ON MCDU TESTS & COLLARED CB FLIGHT CONTROL-FLP-CTL & MONG SYS 2 ON 121VU PNL. ALSO DEFERRED IAW MEL CARD 73167. REPLACED FLAP CSU IAW AMM, GROUND CHECKED NORMAL NO DESDR SWAA2013101121111Transmission · corrodedNR 2 FLAP TRANSMISSION CORRODED AT GIMBAL ATTACH AREAS. R & R NR 2 FLAP TRANSMISSION IAW AMM.SDR CALA2013092591436Module · faultyTE FLAP DISAGREE, DUE TO TE FLAP DISAGREE & FINDING OF TE FLAPS MOVE TO SELECTED POSITION AT A RATE FASTER THAN NORMAL. PER 27-FAULT CODE INDEX PG 9 27-51-06-00, 27-51-07-00. REPLACE THE FLAP SLAT DEPRESSURIZATION MODULE IAW MM27-51-29-201 PCN 643-9093 REF I
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