JASC 2750
Service difficulty reports · 10,193
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 UIEA2024111701095Warning Light · abnormalLOW-SPEED RTO DUE TO CONFIG WARN FLASPS M/S SET WITH FLAPS RESET SYS OPS NORMAL(<P>PERFORMED FLAPS SYS TEST PER 767 AMM 27-51-00, OPS CKS NORMAL, NO FAULTS NOTED </P>)SDR DALA2024111811016Fseu · faultedSHIP 0654 -FCNT/DE- DUE TO TRAILING EDGE FLAP DISAGREE ON APPROACH. CORRECTIVE ACTION: REPLACED NUMBER 2 FSEU AND LEFT SLAT POSITION TRANSMITTER.SDR AALA202411182043Flap System · malfunctionedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: ON APPROACH THE FLAPS WOULD NOT EXTEND TO 30 BUT THEY DID EXTENDTO 25. AIRCRAFT ABORTED APPROACH AND LANDED SAFELY AT ORD. BITE CHECK OF FSEU NOTED NO FAULTS, PER FIM 27-51-00-810-801 VISUALLY CHECKED FLSDR SWAA2024111859868Computer · fault messageAT 500 FEET FLAPS BLEW BACK FROM 30 TO 25 DUE TO WINDSHEAR ; GOT FLAPS DISAGREE AND FLAPS STUCK AT 25<[01] FOUND FAULT CODE 27-81357. PERFORMED FIM 27-81 TASK 806 NO DEFECTS FOUND OK FOR SERVICE. PERFORMED CONDITIONAL INSP05-51-04 NO DEFECTS NOTED.SDR SWAA2024111959174Tab · crackedRIGHT WING INBOARD FIXED TRAILING EDGE DEFLECTION CONTROL RIB UPPER TAB CRACKED<[01] REMOVED RIGHT WING DEFLECTION CONTROL RIB REF SRM 51-40-02;[02] REMOVED AND REPLACE RH WING DEFLECTION CONTROL RIB IAW SRM 51-40-02; (VERY AFT ROLLER NEEDS TO BE INSTALLED);[0SDR FDEA202411131675Flap System · faultedON FLAP EXTENSION JUST PRIOR TO FLAP 5 FULL EXTENSION THE AIRCRAFT ROLLED 5 DEGREES LEFT. AT FLAPS 5 FULL EXTENSION THE AIRCRAFT ROLLED WINGS LEVEL. ALTITUDE 3000FT SPEED 190 KNOTS. FULL SPOILERS WERE SELECTED AT THE TIME. LOWER THE FLAP TO 5 DEG AND VISDR SWAA2024111859368Transmitter · faultyON LANDING WE GOT A TOO LOW FLAPS WARNING & PERFORMED A GO-AROUND; RETRACTED FLAP ON SCHEDULE BUT FLAP STUCK AT 2 DEGREES. WE RAN THE TRAILING EDGE FLAP DISAGREE QRH AND LANDED FLAPS 15 DEGREES.<[01] FOUND FAULT CODE 27-51351 ON FSEU. PERFORMED FIM TASK 27-51 SDR DALA2024111210861Flap System · lockedSHIP 3812 -ATB- RETURNED TO SJU DUE TO FLAP LOCKOUT AFTER TAKEOFF. CORRECTIVE ACTION: FSEU FAULTS SL8/PROX INBD 27-81215. REPLACED #8 SLAT INBOARD PROX SENSOR AND FSEU AS PRECAUTION. FLAP/SLAT OPS CHECKS GOOD.SDR HALA20241119074Cable · damagedRH INBD FLAP TRACK PULLEY AFT CABLE NYLON TORN. COMPLETED REPLACING 4EA FLAP BUS CABLES 33A, 33B, 34A, AND 34B. PER B717 DRAWING # 5940898 REV5.SDR SWAA2024111157562Flap System · lockedNO FLAP RESPONSE WHEN FLAP HANDLE SET TO 5. ALTERNATE EXTENSION WORKED PROPERLY. FLAPS 15 LANDING.<[01] CHECKED FSEU FOR LOGGED FAULTS. NONE FOUND. OPERATED FLAPS REF. AMM 27-51-00 USING PRIMARY HYDRAULIC POWER. FLAPS WORKED NORMALLY. UNABLE TO VERIFY FAILED CSDR SWAA2024110856878Flap System · lockedFLAPS WOULD NOT GO DOWN PAST 5<[01] FOUND #1 FLAP TRANSMISSION TRIP INDICATOR TRIPPED. RESET PER FIM 27-51 TASK 849.;[02] REPLACED OIL FOR TRAILING EDGE FLAP TRANSMISSION?S 1-8 IAW AMM 12-22-51 (SEE TTG8Q00WV8DF FOR WORK PERFORMED) OPS CHECK GOODSDR SCNA20241028348Flap System · malfunctionedDEFECT 752974: SELECTED FLAPS 15 WITH A/S 210 KNOTS FLAPS LOCKED AT 15. - RESOLUTION: PERFORMED CONDITIONAL INSPECTION IAW AMM 05-51-08, NO DEFECTS NOTED.SDR A6WA202410268838Control Lever · faultedFLAPS FAIL CAUTION MSG AT 20* FLAPS ON APPROACH. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-18I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. ACARS: A/C FLT DEP DST TIME ALT N420AW 6068 LEX PHL 1642Z 1756 STATE MINS IAS OAT FLAPS FAILSDR DALA2024102810474Flap System · malfunctionedSHIP 187 ON APPROACH FINAL CONFIG FLAPS 25. FLAP INDICATOR SHOWED L AT 25 R AT 20. GO AROUND, LANDED WITH FLAP 25 RAN QRH. CORRECTIVE ACTION: DEFER FLAP INDICATION PER B767-300 MEL 27-08-02 (6538436)SDR DALA2024102110240Control Rod · disconnectedSHIP 3733 -ATB- RETURNED TO ATL DUE TO FLAP SKEW INDICATION AFTER TAKEOFF. CORRECTIVE ACTION: FSEU BITE SHOWS MSG 27-53254 (FLAP 5 SKEW). FOUND CONTROL ROD FOR #5 SKEW SENSOR DISCONNECTED. RE-CONNECTED ROD TO SENSOR AND OPS CHECK NORMAL PER B737 AMM.SDR VNAA202410163013Seat Track · chafedLH IB FLAP LOWER SKIN IS CHAFED AROUND IB HINGE FAIRING PERIMETER WS54.55SDR DXTA2024102200899Drive Unit · defectiveFLAP FAIL YELLOW CAS: FLAP FAIL YELLOW CAS DISPLAYED ON APPROACH AFTER SELECTING FLAPS 1 AT APPROXIMATELY 160KIAS. FLAPS FAILED AT THE "0" POSITION. REPEAT WRITE UP. CORRECTIVE ACTION; REPLACE SUSPECT FAULTY FLAP PDU IAW PHENOM 300 MM 27-51-07. REPLACED SUSPECSDR ABXA20241017190Warning Message · false indicationDURING TAXI OUT FLAP/SLAT ELEC. MSG. APPEARED, AC RETURNED TO THE GATE AND MTX GROUNDED THE AC . MTX PERFORMED BITE TEST OF FSEU IAW FIM 27-51-50-00, NO DEFECTS WERE FOUND . RAN BOTH ENGINES AND OPERATED FLAPS AND SLATS HYDRAULICALLY AND ELECTRICALLY NO MEASAGSDR AALA202410171627Flap System · warning messageAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT DUE TO THE FLIGHT CREW REPORTING A FLIGHT CONTROL FLAP SYSTEM 2 FAULT WHEN MOVING FLAPS FROM 2 TO 1 ON TAKEOFF. THE AIRCRAFT LANDED SAFELY AT CLT WITHOUT FURTHER INCIDENT. MAINTESDR SWAA2024111148205Bracket · crackedLEFT WING: OUTBOARD DEFLECTION ROLLER OUTBOARD MOUNT BRACKET CRACKED STREAMER ATTACHED.<[01] REMOVED AND REPLACED BRACKET PN#:5A6260-1 PO:1103180.1 IAW B737-800 SRM 51-40-02;[02] VERIFIED REMOVED AND REPLACED BRACKET PN#:5A6260-1 PO:1103180.1 IAW B737-800 SRM SDR DXTA2024101600849Flap System · faultedAFTER TAKEOFF WE RECEIVED FLAP FAIL CAS. FLAPS FAILED IN THE NUMBER 1 POSITION AND DID NOT RETRACT TO 0. WE ACCOMPLISHED THE QRH PROCEDURE AND CYCLED THE FLAPS AND THE FLAPS STAYED AT FLAPS 1. LANDED WITH FLAPS 1 IN TEB. CORRECTIVE ACTION: GAINED ACCESS TO SDR MASA2024101400026Warning Message · illuminatedFLAPS FAIL WHILE RETRACTING FLAPS (EMERGENCY DECLARED)----------CURRENTLY OOS AND BEING TROUBLESHOT.SDR A6WA202410108834Bpsu · failedWHILE EXTENDING FLAP TO 8 DEG ON APPROACH, RCVD "FLAP FAIL" CAUTION MESSAGE. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-18IBOX 12. FLAPS RESET. PLACARED AND PLACED ON MEL ***** AIRCRAFT REMOVED FROM SERVICE ***** R/R LFT BPSU OPS CHECK GOOD AT THISDR AALA202410109874Proximity Sensor · faultedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO BFL DUE TO THE FLIGHT CREW REPORTING A FLAPS LOCKED ECAM MESSAGE ON APPROACH. THE AIRCRAFT LANDED SAFELY AT BFL AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE FOUND LEFT FLASDR AALA202410108529Proximity Sensor · faultedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO BFL DUE TO THE FLIGHT CREW REPORTING A FLAPS LOCKED ECAM MESSAGE ON APPROACH. THE AIRCRAFT LANDED SAFELY AT BFL AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE FOUND LEFT FLASDR U5QA202410080140Flap System · stuckFLAPS STUCK AT 3 DEGREES WHILE IN FLIGHT. FLAPS RESET ON GROUND BUT NEEDS FUNCTIONAL CHECK BEFORE NEXT FLIGHT. MX C/A: C/W FLAPS FUNCTIONAL CHECK IN REF CH350 TASK 27-52-00-710-802 WITH NO DISCREPANCIES NOTED. NO RECURS TO DATE.SDR DALA2024100709749Rod End · disconnectedSHIP 3848 -MISC- AFTER TAKEOFF AND FLAP RETRACTION, FLAPS LOCKED OUT AT 5. FLIGHT CONTINUED AND CREW DECLARED EMERGENCY INTO ATL. CORRECTIVE ACTION: FOUND ROD END FOR #5 SKEW SENSOR DISCONNECTED AT SENSOR. REPLACED ROD END BOLT. OPS CHECK NORMAL.SDR AALA202410072075Flap System · fault messageAIRCRAFT WAS NOT GROUNDED: AN EMERGENCY WAS DECLARED ON ARRIVAL AT CLT DUE TO FLAPS SYSTEM 1 FAULT MESSAGE ON APPROACH. THE AIRCRAFT LANDED SAFELY AT CLT AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE NOTED NO ON THE POST FLIGHT, NO CLASS 3 FAULTS INSDR SCNA20240930322Flap System · malfunctionedDEFECT 777888: WHILE TURNING BASE WE SELECTED FLAPS 1. AFTER SELECTION OF THE FLAPS THE A/P DISCONNECTED AND THE FO PFD/ ND/ LOWER DU WENT BLACK. WE NOTICED WE HAD A TOTAL ELECTRIC FAILURE. WE THEN REALIZED WE HAD A #1 ENGINE FAILURE. AS WELL AS ALL HYDRAULICSSDR AALA202409299362Pressure Switch · inoperativeAIRCRAFT WAS GROUNDED: ON ROTATION FROM LAS, MASTER CAUTION FLT CONT ILLUMINATED. ON THE OVERHEAD PANEL NO FLT CONT LIGHTS ASSOCIATED WERE ILLUMINATED.WITH NO OTHER INFORMATION, QRH PROCEDURE WAS UNABLE TO BE USED. WITH A CALL TO MOC IT WAS DETERMINED THAT THESDR DALA2024092309322Transmission · trippedSHIP 5648 -FCNT/DE- TRAILING EDGE FLAP DISAGREE ON APPROACH. CORRECTIVE ACTION: REPLACED NUMBER 4 FLAP TRANSMISSION, SERVICED 5, 6, AND 8 TRANSMISSIONS. PERFORMED FLAP LUBE. REPLACED FLAP CONTROL VALVE MODULE.SDR J7SA2024093000417Fce · faultedFLAPS FAIL CAS AND INDICATION WHEN FLAPS 1 WAS SELECTED DURING THE AFTERSTART FLOW. THE CAS MESSAGE REMAINED AFTER AN ELECTRICAL RESET. REPLACED FAULTY FCE 1 WITH A REPAIRED UNIT IAW EMB 505 AMM 27-03-01. OPS CHECK GOOD WITH NO DEFECTS FOUND.SDR VNAA2024092311101Bpsu · faultedFLAPS FAIL CAUTION AFTER T/O. / UPON TROUBLESHOOTING FOUND LH FLAP BPSU DISCONNECTED. MANUALLY RIGGED LH BPSU IAW CRJ 700 AMM 27-52-03-801-A01. PRIOR TO CONNECTING OTBD FLAP TORQUE TUBE VERIFIED LH FLAP BPSU IS WITHIN RIG LIMITS. INSTALLED OTBD FLAP TORQUE TUBSDR 2024FA0000726Bpsu · failed"FLAP FAIL" MESSAGE AT CRUISE. FLAPS WERE STUCK AT 0 FOR LANDING. AIRCRAFT MODEL IS CL-600-2B19 IT WAS NOT LISTED ABOVE UNDER BOMBARDIERSDR 21GA20240917016Module · faultedON APPROACH TO CVG SELECTED FLAPS AND GOT TRAINING EDGE FLAP DISAGREEE MESSAGE. LANDED WITH FLAPS AT 20 DEGREES.SDR AALA202409175367Flap System · faultedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: ON APPROACH, A FLAP DISAGREEMENT OCCURRED WHEN FLAPS WERE SELECTED FROM 15 TO 25. NO MOVEMENT OCCURRED WHEN SELECTED. THE CREW EXECUTED A GO AROUND AND EXECUTED QRH PROCEDURES IN THE HOLDING PATTERN; AIRSDR DXTA2024091700552Control Handle · defectiveFLAPS FAIL AMBER CAS: DURING APPROACH TO KHND WE RECEIVED A FLAP FAIL AMBER CAS WHEN SELECTING FLAPS 15. RAN THE FLAP FAIL QRC. CORRECTIVE ACTION: REMOVED AND REPLACED THE FLAP HANDLE IAW CE 680 MM 27-51-00. OPS CHECK GOOD, NO DEFECTS NOTED. REMOVED PN: 696525SDR CALA2024091300630Warning Light · false activationON DESCENT LE FLAPS TRANSIT LIGHT ILLUMINATED. PERFORMED FIM 27-81 TASK 821. OPS CHECKED LE FLAPS. LE FLAPS TRANSIT LIGHT REMAINS EXTINGUISHED. NO PREVIOUS HISTORY. OK FOR SERVICE. PERFORMED FIM 27-81 TASK 821. OPS CHECKED LE FLAPS. LE FLAPS TRANSIT LIGHT RESDR L9QS2024091200711Pulley · damagedL/H FLAP BINDING, CAUSING DAMAGE TO L/H FLAP & L/H FLAP DRIVE PULLEY. REPLACED DAMAGED PARTSSDR IPXA2024091333751Torque Tube · faultedON APPROACH SELECTED FLAP 20 AND RECEIVED TE FLAP ASYM. EICAS PLUS TRAILING EDGE LIGHT. FLAPS ASYMETRY GREATHER THAN 5 AND LESS THAN 20. RII REMOVED AND REPLACED #3 TORQUE TUBE IAW AMM 27-51-25/201.SDR J6BA2024091000008Bpsu · failedON APPROACH TO RWY 22L, WE SELECTED FLAPS 45. WE RECEIVED FLAPS FAIL. WE EXECUTED A GO-AROUND. WE NEVER UTILIZED GO-AROUND THRUST SINCE IT WAS EXECUTED AT OVER 1000 FT. WE PERFORMED ALL CHECKLISTS TO INCLUDE QRH (FLAPS FAIL CHECKLIST) AND APPLICABLE DOCUMENTATSDR CALA2024090600592Flap System · malfunctionedON APP FLAP ASSYMETRY WHEN SEL F25. TURNED INTO A FLAP DISS F15- 25 AFTER LNDG FLAPS SHOW15 AHM UPDATE: CHIME ALERT FOR THE BYPASS. PERFORMED FSEU BITE. LAST LEG FAULT HISTORY SHOWED TE FLAPS SNSR DIS FAULT CODE 27-52261. CURRENT FAULTS SHOWED FLAP LEVER FASDR A6WA202409058806Control Unit · faultedFLAPS FAIL CAUT MESSAGE FLAPS FAILED AT 16K FT 250 KNOTS FAILED IN THE ZERO DEGREE POSITION. AIRCRAFT REMOVED FROM SERVICE R&R THE FECU IAW AMM 27-51-05. OPS CHECK GOOD. REMOVED PLACARD AND REMOVED FROM MEL. SDR A6WA202409058804Control Unit · failedFLAPS FAIL CAUT MESSAGE FLAPS FAILED AT 16K FT 250 KNOTS FAILED IN THE ZERO DEGREE POSITION. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-18I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL ***** AIRCRAFT REMOVED FROM SERVICE ***** R&R THE FECU IAW SDR CALA2024090502390Flap System · faultedON APP FLAP ASSYMETRY WHEN SEL F25. TURNED INTO A FLAP DISS F15- 25 AFTER LNDG FLAPS SHOW15 AHM UPDATE: CHIME ALERT FOR THE BYPASS. SEE ATTACHED REPORT. PERFORMED FSEU BITE. LAST LEG FAULT HISTORY SHOWED TE FLAPS SNSR FIM REF 27-51 TASK 819 RECOMMENDS CHANGINGSDR JJBA20240906003Control Unit · inoperativeFLAP FAIL MESSAGE WHEN PERFORMING CLIMB CHECK AT 1300 AFTER MOVING FLAP LEVER FROM 9 TO 0 DEGREES. ON POST WALK AROUND FLAPS ARE STILL AT 9 DEGREES, SPEED WHEN THE FLAP FAIL OCCURRED WAS AROUND 160 TO 170 KNOTS. FOUND RH TRANSMISSION FAIL ON CMC. PERFORMED FIMSDR SCNA20240903310Flap System · malfunctionedDEFECT : APON APPROCH AT FLAPS 30 AND THEN FLAPS 15 AIRSPEED LOW AURAL WARNING SOUNDED UNABLE TO CONFIGURE FOR NORMAL LANDING. (EMERGENCY DECLARED) - - RESOLUTION: AIRSPEED WARNING AND CONFIG PROBLEMS FOUND TO BE FROM DDG PROCEDURE NOT FOLLOWED CORRECTLY FOR SDR IPXA2024083095805Torque Tube · unserviceableFLAP ASSYMMETRY TRAILING EDGE DURING APPROACH WHEN FLAPS 20 SELECTED. ACCOMPANIED WITH CORRESPONDING EICAS MSG AND LIGHT. REPLACED TORQUE TUBES 251N4281-16,-17,-18 WITH 251N4281-26,-27,-28. REPLACED BEARING 251N4318-1 WITH 251N4381-6. ACCOMPLISHED PER AMM 27-SDR IPXA2024082995805Flap System · faultedEMERGENCY DECLARED, FLAP ASSYMMETRY TRAILING EDGE DURING APPROACH WHEN FLAPS 20 SELECTED. ACCOMPANIED WITH CORRESPONDING EICAS MSG AND LIGHT PER THE FIM 27-51 TREE 809 ,DID A FSEU BITE PER 27-51-00 FIG 104 . FOUND A RIGHT FLAP DRIVE FAULT. MORE TROUBLE SHOOTSDR DALA2024082908553Roller · excess playSHIP 3143 EXCESSIVE PLAY CRUISE ROLLER I/B FLAP ON RH WING. CORRECTIVE ACTION: REPLACED CRUISE ROLLER I/B FLAP ON RH WING AS PER AIRBUS CMM 57-52-21. (0526868)
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