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 J7SA2026010600466Fce · faultedDURING CRUISE, CREW RECEIVED SWPS FAULT, FLAPS FAIL, PTRIM BKP FAIL AND SPOILER FAULT. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED FCE 1 IAW EMB 505 AMM 27-03-01. FCE 1 RIGGING / OPS CHECK GOOD AND NO CAS MESSAGE ILLUMINATED.SDR AALA202512237111Strut · fault messageAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INTO DFW DUE TO THE FLIGHT CREW REPORTING THAT ON APPROACH A FLIGHT CONTROL FLAPS LOCKED / ALIGNMENT FAULT DISPLAYED. THE FLIGHT CREW ACCOMPLISHED QRH PROCEDURES AND LANDED SAFELY AT DFW WHERE IT TAXIED TO THE GSDR YENA2025122201243Flap System · faultedFLT # 771 BOS- CUN (AIRCRAFT DIVERTED TO MCO)"DEPARTURE OUT OF BOSTON AT 1500' ENCOUNTERED MODERATE TO BORDELINE SEVERE TURB AIRSPEED +/- 25 KTS EXCEDED FLAP OVERSPEED FOR + 2 SECS AT THRUST REDUCTION ALTITUDE LEFT PWE AT TOGA FOR POSSIBLE WINDSHEAR @ 1500 AFTSDR IXXA2025121901Retainer · crackedRIGHT WING INBOARD AFT FLAP OUTBOARD EDGE SEAL RETAINER IS DAMAGED AND BULB SEAL IS MISSING.SDR J7SA2026010600465Fce · faultedDURING CRUISE, CREW RECEIVED SWPS FAULT, FLAP FAIL, PTRIM BKP FAIL AND SPOILER FAULT. THE FLAPS WERE RETRACTED AT THE 0 POSITION. CAS MESSAGES REMAINED ON FROM CRUISE, LANDING AND SHUTDOWN. REPLACED FCE #1 AND OPS/RIGGED TESTED WITH NO FURTHER DEFECTS IAW PHENSDR SIMA20251214002Seal · failedFLAP FAIL OCCURRED UPON RETRACTING FLAPS FROM POSITION 1 TO POSITION 0. EMERGENCY DECLARED. PERFORMED FLAP SYSTEM OPS TEST IAW AMM 27-50-00-710-801. REINSTALLED LT INBD FLAP OTBD AERODYNAMIC SEAL IAW 57-51-02 OPS CHECK GOOD.SDR AALA202512151041Flap System · splitAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: ENROUTE SHORTLY AFTER TRIMMING THE AIRCRAFT, THE YOKE WAS TILTED RIGHT AND REQUIRED RETRIMMING AGAIN. SHORTLY AFTER THIS THE CREW NOTICED A FLAP ASYMMETRY. FLAP HANDLE UP, FLAP INDICATOR WAS SPLIT BETWESDR SIMA20251211001Warning Message · false activationFLAP FAIL AT 13000' MSL SPEED 280 IMMEDIATELY UPON SPEED BRAKE LEVER ACTUATION. NO FLAP LEVER ACTUATION. RAN QRH, MESSAGE REMAINED ANNUNCIATED. EMERGENCY LANDING EXECUTED WITH SLAT(3) FLAP(0). PERFORMED FLAP FAIL PER FIM TASK 27-51-00-810-805-A. MESS CLEARED ASDR SIMA20251210001Warning Message · false activationINFO TO MTX HAD A FLAP FAIL MESSAGE ON EICAS PERFORMED QRH RESET PROCEDURE MESSAGE CLEARED ON EICAS. EMERGENCY DECLARED. NO INJURIES. PERFORMED OPERATIONAL CHECK OF FLAP SYSTEM.OPC GOOD FOR NO FLAP FAIL MESSAGE ON EICAS IAW ERJ AMM 27-50-00.SDR DALA2025121109056Handle · stuckATB, DUE TO THE FLAP/SLAT CONTROL UNIT HANDLE STUCK AT POSITION 2. FOUND HANDLE TRIGGER SECURING PIN BROKEN. CORRECTIVE ACTION: REPLACED FLAP/SLAT COMMAND SENSE UNIT. (LP 7796736)SDR VNAA2025120411101Bpsu · unserviceableFLAPS FAIL AT 20 DURING APPROACH. REMOVED AND REPLACED LT BPSU UP TO CLOSE OUT 5.C. IAW AMM 27-52-03-000/400-801. ELECTRICAL RIGGING OF FLAP BPSU PASSED. SELF TEST OF SFECUS GOOD, OPS CHECKED GOOD.SDR SWI2025F01792Pdu · faultedFLAPS FAIL CAUTION MESSAGE ON APPROACH WHEN SELECTING FLAPS 20 TO 30. RAN QRH & FLAPS STAYED IN FLAPS 20 DETENT AFTER RESELECTING FLAPS 20 FROM FLAPS 30 DETENT IAW PROCEDURE. (FLIGHT 4808) REF CP 31297248 & CP 31297331 FOR TROUBLESHOOTING. REF CP 31297272 FOSDR DALA2025121008995Flap System · lockedATB DUE TO FLT CTL FLAPS LOCKED MESSAGE. REPLACED RT APPU, SFCC 1, SFCC 2, PROX SENSOR 40CV, AND PROX SENSOR 38CV. ADJUSTED INTERCONNECTING STRUT DUE TO OUT OF RIG. (LP 8049502)SDR DXTA2025120105887Flap System · faultedWHEN ON APPROACH, SELECTED FLAPS 20 AND RECEIVED A FLAP FAIL EICAS AND FLAPS STOP MOVE AT 3. PLACED THE FAIL HANDLE BACK TO 0 IAW QRC AND THE FLAP INDICATOR REMAINED AT 3. REMOVED DEFECTIVE RT FLAP RDU. INSTALLED REPAIRED UNIT WITH GOOD OPS CHECKS IAW AMM 2SDR CALA2025120111600Flap System · no discrepancyTE FLAP DISAGREE CAUTION AND INDICATION. REF FIM 27-51 FAULT TREE 808, FLAPS ARRIVED IN POS 20, BROUGHT FLAPS BACK UP ELECTRICALLY AND OPERATED HYDRAULICALLY SEVERAL TIMES. OBSERVED NO TRIPS ON TRANSMISSIONS. FSEU NO EXISTIMG FAULTS.SDR F2PA202512030279Pdu · failedON APPROACH TO LAND AT KAPA PILOTS SELECTED FLAPS DOWN, AND FLAP SYSTEM DID NOT RESPOND. PILOTS RECEIVED A CAS MASSAGE "FLAP FAIL". CREW FOLLOWED FOM AND PROCEEDED TO MAKE AN UNEVENTFUL NO FLAPS LANDING. AN EMBRAER AOG MAINTENANCE TEAM WAS DISPATCHED TO TROUBLSDR IPXA2025112636097Flap System · inoperativeTE FLAPS DISAGREE POSITIONING FLAPS 1 ON LANDING C/W FIM 27-51 FT 814. MSG CLEARED NO FUALTS NOTED. OPS CK REF AMM 27-51-00. NO MSG. OK TO CONTINUE.SDR DALA2025112408544Bearing · excess playLEFT WING INTERCONNECT STRUT, FWD ROD BEARING WITH PLAY AND NUT WITH RUST. CORRECTIVE ACTION: REPLACED ROD END AND NUT PER A319 CMM TASK 57-52-17-000-801-A01. (1317794)SDR DALA2025112408543Rod · excess playRT WING INTERCONNECT STRUT, FWD ROD BEARING WITH PLAY. REPLACED ROD END IAW A319 CMM TASK 57-52-17. OK FOR SERVICE. (1317780)SDR FDEA202511222200Transmitter · faultedTE FLAP DISAGREE EICAS ON APPROACH FLAPS 5. EMERGENCY DECLARED. AMM 27-51-45-2 FOUND THE NR 3 FLAP TRANSMITTER JUST AT LOWER LIMIT DEG. PER MM 27-51-45-2. PERFORMED ADJUSTMENT ON THE NR 3 TRANSMITTER AND NOW WITHIN LOWER AND UPPER LIMITS. CYCLED FLAPS 4 TSDR CALA2025111311179Indicator · faultedFLAPS STUCK BETWEEN 5 AND 10 DEGREES AND WOULD NOT MOVE WITH FLAP HANDLE MOVEMENT. PSEU LIGHT ON. BITE CHECKED PSEU AND FOUND LDG FLAP A FAULT MESSAGE 32-62009 AND LDG FLAP B FAULT WITH MESSAGE 32-62010. AND NO DISPATCH. PERFORMED FSEU BITE. FOUND PROBLEM WITSDR DALA2025111208296Flap System · malfunctioned-FCNT- CREW ELECTED DE DUE TO TE ASSYM INDICATION DURING APPROACH. CREW PERFORMED A GO AROUND AND LANDED WITHOUT INCIDENT. CYCLED TE ALT SWITCH AND OPERATED FLAP SYSTEM NORMALLY. NO FSEU FAULTS NOTED.(7657358)SDR FDEA202511112158Flap System · faultedAT APPROX 80 KTS ON TAKEOFF GOT EICAS FLAPS AND CONIF. REJECTED THE TAKEOFF RUNWAY 02R AT BKK AT 303 TOGW AND 31C TEMP. RAN CHECKLISTS, RETURNED TO THE GATE LEAVING FLAPS AT 5. PERFORMED T/S AS PER FIM 31-51 FT 808, NO FAULT FOUND. PERFORMED BITE PROCEDURSDR CVGA20251114002Switch · faultyFLAP ASYM LIGHT CAME ON AFTER SELECTING FLAPS 20 POSITION. FAULT COULD NOT BE DUPLICATED UPON ARRIVAL TO AIRCRAFT. MCC ELECTED TO REPLACE THE FLAP FOLLOW UP SWITCH. REMOVED FLAP FOLLOW UP SWITCH P/N 45AS61015-23 S/N 08A432AND INSTALLED AN OVERHAULED FLAP FOLLOSDR R61A2025111000490Flap System · faultedSLAT FLAP FAIL IN FLIGHT. SLATS 3 FLAPS 0. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND TO BE A TRANSITORY CONDITION OF THE FLAP CONTROL SYSTEM.SDR SWAA2025111033390Fseu · faultedSELECTED FLAPS 30 WITH NO LE LIGHTS INDICATION BY FLAP INDICATOR AND OVERHEAD PANEL. PSEU LIGHT ILLUMINATED ON LANDING. R & R FSEU REF AMM 27-51-01SDR CALA2025111011030Flap System · malfunctionedFLAP LOCK OUT ON 1ST TICK. ATTEMPTED RESEAT OF LEVER, NO HELP. ALTN EXTENSION REQUIRED. PERFORMED OPS CHECK OF NORMAL AND ALTN FLAP CONTROL SYSTEMS IAW AMM 27-51-00-710-801. OPS CHECK GOOD. PERFORMED BITE TEST OF FSEU IAW FIM 27-51 TASK 801. INTERMITTENT INACTSDR SWAA2025111031874Transmitter · faultySELECTED FLAP 5 . FLAPS; TRAILING EDGE; STOPPED PRIOR TO 1 AND LE FLAPS TRANSIT AMBER LIGHT ILLUMINATED AND STAYED ON.<[01] FOUND FAULT CODE 27-52259 IN FAULT HISTORY T/S PER FIM 27-51 TASK 813. R&R LH FLAP POSITION TRANSMITTER PER AMM 27-58-01. OPS TESTS GOODSDR AALA202511093574Actuator · faultedAIRCRAFT WAS GROUNDED: F/CLT FLAPS FAULT. ECAM ON ARRIVAL. FLAPS STUCK IN THE UP POSITION. RECYCLE PER ECAM. FAULT REMAINED. EMERGENCY DECLARED AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED FLAP ACTUATOR.SDR AALA202511066130Flap System · malfunctionedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO FLAPS DID NOT LOWER DURING APPROACH. EMERGENCY LANDED SAFELY AT CLT. ACCOMPLISHED FIM 27-59-00. PERFORMED FSEU BITE CHECK IAW AMM 27-51-00, BITE CHECK SHOWS NO EXISTING FAULTS. PERFORMED OPS CHECK OF FSDR SWAA2025110530978Flap System · lockedFLAP GAUGE DID NOT MATCH COMMANDED POSITION. FLAPS WOULD NOT RETRACT PAST FLAPS 2. PERFORMED FSEU BITE PER FIM 27-51 TASK 801; NO FAULTS NOTED. PERFORMED TRAILING EDGE FLAP SYSTEM OPS TEST PER AMM 27-51-00. ALL OPS NORMAL. A/C OK FOR SERVICE.SDR CVGA20251103001Flap System · failedFLAPS FAILED AT 5° ON APPROACH INTO KLAS. DECLARED EMERGENCY. REMOVED FAILED FLAP CONTROLLER AND INSTALLED A TESTED FLAP CONTROLLER IAW CE-750 AMM 27-51-00. OPS CHECK GOOD. NO DEFECTS NOTED. PN OFF/ON 6718328-1 SN OFF: 301 SN ON 117.SDR CALA2025110310835Limiter · brokenHYD SYS B FAILURE, T/S SYSTEM B FAILURE. FOUND TRAILING EDGE FLAP FLOW LIMITER BROKEN. REMOVED AND REPLACED TRAILING EDGE FLAP FLOW LIMITER REF MM 27-51-61-000-801. PERFORMED FLAP OPERATIONAL TEST, TEST PASSED. SERVICED SYSTEM B HYD. TO FULL. OPS AND LEAKCHESDR F2PA202511040256Control Lever · faultedON APPROACH TO LAND AT KAPF THE FLAPS FAILED TO LOWER. AIRCRAFT MADE AN UN-EVENTFUL LANDING W/O FLAP USE. FLAP SYSTEM WAS TROUBLESHOT AND THE FLAP HANDLE CONTROL ASSEMBLY WAS DETERMINED TO BE FAULTY. THE FLAP HANDLE CONTROL ASSEMBLY WAS REPLACED AND THE AIRCRASDR CALA2025102810670Adm · faultyFLAP FAIL AT 25 AND FLAP OVERSPEED 210 KTS DUE TO WINDSHEAR PERFORMED PHASE 1 INSPECTION OF FLAP SYS IAW AMM 05-51-08. NO ISSUES FOUND DURING INSP. PERFORMED BITE OF FSEU & FOUND FAULT CODE 27-51351 FROM INBOUND LEG. T/S IAW FIM 27-51 TASK 830 THRU STEP D.(8).SDR DALA2025102707837Flap System · false indicationSHIP 3714 FCNT/DE DECLARED EMERGENCY DUE TO FLAP LOCKOUT ON APPROACH MEX. PERFORMED FSEU BITE CHECK. NO FAULTS. OPERATED FLAPS SEVERAL CYCLES. OPS CHECK GOOD.SDR DXTA2025102705415Fce · faultedUPON DESCENT RECEIVED A FLAP FAIL CAS ALONG WITH SWPS FAULT, PTRIM BACKUP FAIL, SPOILER FAULT, LOSS OF FLAP INDICATION ON EICAS, ALONG WITH PTRIM INDICATION. ALSO RECEIVED GTC MESSAGE WITH DATA FAILURE. RESULTED IN A NO FLAP LANDING. OF NOTE AUTOPILOT APPEARESDR DXTA2025102705410Flap System · out of rigON APPROACH, GOT A FLAPS FAIL AMBER CAS, WHEN SELECTING FLAPS 1. RAN QRC AND CAS EXTINGUISHED. SELECTED FLAPS 1 AND GOT THE FLAPS FAIL AMBER CAS AGAIN. DISCONNECTED FLAP POWER BOX CONNECTOR, DISCONNECTED LT & RT INBOARD FLEX SHAFTS FROM PCU'S, DISCONNECTED OBSDR AALA202510230129Torque Tube · damagedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: DURING APPROACH FLAP INDICATION WERE SPLIT CONDUCTED A GO AROUND. AIRCRAFT EMERGENCY LANDED SAFELY AT DFW. **SUPPLEMENTAL REPORT FOR (AALA202510210129): FOUND RIGHT WING OUTBOARD TORQUE TUBE SPRT INBOARDSDR AALA202510210129Flap System · faultedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: DURING APPROACH FLAP INDICATION WERE SPLIT CONDUCTED A GO AROUND. AIRCRAFT EMERGENCY LANDED SAFELY AT DFW. (OPEN).SDR DALA2025102007653Motor · faultedCREW ELECTED DE DUE TO TE DISAGREE INDICATION DURING CRUISE. C/W QRH AND LANDED UNEVENTFULLY. LUBRICATED FLAP SYSTEM AND REPLACED TE ALT PDU MOTOR. FLAPS OPS GOOD IN HYD AND ALT ELEC.(7086116)SDR DXTA2025102105348Control Unit · faultyAFTER TAKEOFF, WE SELECTED THE FLAP HANDLE TO FLAPS 0. IMMEDIATELY AFTER THAT, WE GOT A FLAPS FAIL AMBER CAS. FLAPS DID NOT MOVE AND REMAINED AT 20 DEGREES. NEAR FREEZING TEMPS ON RON. REMOVED FAULTY FLAP CONTROL UNIT. P/N: 600-93000-121, S/N: 431 INSTALLESDR AALA202510209177Flap System · warning messageAIRCRAFT WAS GROUNDED: AFTER TAKEOFF WHEN RAISING THE FLAPS TO UP POSITION, F/CTL FLAPSFAULT CAUTION MESSAGE APPEARED. ECAM ACTIONS DID NOT RECTIFY SITUATION. AFTER TROUBLESHOOTING AND QRH PROCEDURES, IT WAS DETERMINED THAT FLAPS TWO AND THREE POSITIONS CLEASDR IPXA2025102008002Flap System · faultedON APPROACH RECEIVED FLAPS SYS 1&2 FAULT. FLAPS WOULD GO TO 20 THEN COMEBACK UP A FEW DEGREES AND THEN GIVE A JAM INDICATION OF FLAP SYS 1&2 FAULT. ++REPLACED #4 JACKSCREW PER AMM 27-54-24-401. OPS CHECK GOOD. VERIFIED AND WITNESSED #4 JACKSCREW INSTALLATION RSDR DXTA2025102005325Control Unit · defectiveON APPROACH SELECTED FLAPS 10. FLAPS TRACKED ONLY TO 2 DEGREES AND FLAP FAULT AMBER CAS APPEARED. COMPLIED WITH QRH SELECTED FLAPS BACK TO ZERO AND FLAPS FAIL AMBER CAS APPEARED. COMPLIED WITH QRH FOR ZERO FLAP LANDING. LANDED UNEVENTFULLY. B3 CODE #006786 FPSDR DALA2025100707278Rod · corrodedCORROSION ON ACTUATING ROD OF FLAP INTERCONNECTING STRUT LH WING. REMOVED INTERCONNECTING STRUT LH WING IAW AMDS CARD 2750-1010-LT. (1237667).SDR DALA2025100707277Rod · corrodedCORROSION ON ACTUATING ROD OF FLAP INTERCONNECTING STRUT RT WING. REMOVED INTERCONNECTING STRUT RH WING IAW AMDS CARD 2750-1010-RT. (1237680).SDR JR2R20251006311Bellcrank · chafedLEFT MAIN, NR 1 FLAP CARRIAGE ASSEMBLY, BELL CRANK ASSEMBLY. CHAFED OUT OF LIMITS. REPAIRED.SDR JR2R20251006312Bellcrank · chafedRIGHT MAIN, NR 1 FLAP CARRIAGE ASSEMBLY, BELL CRANK ASSEMBLY. CHAFED OUT OF LIMITS. REPAIRED.SDR JR2R2025100600268Bellcrank · chafedR/H MAIN, #1 FLAP CARRIAGE ASSEMBLY, BELL CRANK ASSEMBLY. CHAFED OUT OF LIMITS. REPAIRED
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