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 CA190304013Control Unit · inoperative(CAN) DURING TAXI, A FLAPS FAIL MESSAGE APPEARED WITH THE FLAPS AT ZERO DEGREES. DURING A SUBSEQUENT TEST OF THE FLAP ELECTRONIC CONTROL UNIT (FECU), THE FECU WAS FOUND INOPERATIVE. THE FECU WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR CA190228001Position Unit · malfunctioned(CAN) FLAP POWER CAUTION IN FLIGHT AFTER TAKE OFF , AND FLAP STRUCK AT 10 , AIR TURN BACK PERFORMED , NORMAL LANDING , NO EMERGENCY DECLARED , FAULT CODE SHOWS UNCOMMANDED MOTION , FPU REPLACED AND AIRCRAFT RTS.SDR YENA201902250102Control Lever · failedFLT 2773, BOS-AUA. UPON EXTENSION OF FLAPS FOR LANDING DISCONNECT THE LOWER HANDLE ON FLAP HANDLE ITSELF WAS DISCONNECTED FLAPS FROZEN IN PLACE IN HOLDING COULD INSERT PEN TIP INTO JUNCTION OF UPPER AND LOWER FLAP HANDLE TO MOVE FLAP HANDLE TO USE. LANDED FLAPSDR UIEA2019022503375Warning Message · false activationTE FLAP DISAGREE DURING APPROACH. PERFORMED FSEU BITE TEST IAW FIM 24-51 FT 809, FOUND NO FAULTS, PERFORMED OPS TEST OF FLAP / SLAT SYSTEM IAW AMM 27-51-00. NO DEFETS NOTED. REMOVED AND REPLACED INBOARD SLAT NR 6 OUTBOARD PROXIMATELY SWITCH IAW AMM 27-8SDR A6WA2019022546411Warning Message · illuminatedDURING CRUISE FLIGHT, THE FLIGHT CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE. THE CREW DECLARED AN EMERGENCY AND CONTINUED TO DESTINATION. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT.SDR CA190221008Shaft · deformed(CAN) DURING MAINTENANCE TO RECTIFY A FLAP MEL, IT WAS DISCOVERED THAT THE #4 FLAP SHAFT ASSEMBLY HAD BEEN TWISTED AND DEFORMED. THE SHAFT ASSEMBLY WAS ULTIMATELY REPLACED IAW MANUFACTURER`S INSTRUCTIONS AND SYSTEM OPERATION WAS CARRIED OUT WITH NO OTHER FAULTSDR FDEA201902150419Warning Message · false activationTE FLAP DISAGREE EICAS MSG WHEN SELECTING FLAPS 25. COMPLIED WITH QRH AND LANDED WITH FLAPS 20. PERFORMED FSEU BITE CHECK IAW 757 FIM 27-51 FIG104B. NO EXISTING FAULTS AND BITE CHECK GOOD ON ALL 3 UNITS. CHECKED TRANSMISSIONS FOR TRIPED INDICATORS ANDSDR HALA2019021200056Vane · out of adjustATB / FCF FAILED = ACFT ROLLS RIGHT AT FLAP 40. ADJUSTED R/H MID FLAP FIX VANE PER AMM
24-20-02.SDR UIEA2019F00131Flap System · malfunctionedRH INBOARD FORE-FLAP FAIL TO PROPERLY DEPLOY DURING TEST FLIGHT. CAUSING EMERGENCY LANDING (POSSIBLE DUPLICATE ENTRY)SDR UIEA201902270133Flap System · damagedRIGHT HAND OUTBOARD FORE-FLAP FAIL TO FULLY EXTEND DURING TEST FLIGHT. PILOT REQUESTED EMERGENCY EQUIPMENT BE PRESENT DURING LANDING AFTER TEST FLIGHT.SDR 2019F00122Flap System · failedR/H INBOARD FORE-FLAP FAILED TO PROPERLY EXTEND DURING OPERATIONS OF FLAP SYSTEM WHILE PREFORMING TEST FLIGHT.SDR GTIA201902113151Flap System · malfunctionedF LOCKED FLAP-PERFORMED TROUBLE SHOOTING PER TSM 27-51-00-810-819-A FOUND L/H APPU SYNCHRO ANGLES IN EXCESS OF 5.2 PERFORMED VISUAL INSP OF TRANSMISSION ASSEMBLY PER AMM 27-54-00-200-001-A NO DEFECTS NOTED FOUND L/H APPU INSPECTION WINDOW FILLED WITH DEBRIS R/SDR DALA2019021300942Proximity Sensor · failedCREW REPORTED TO CONFIG FLAP WARNINGS DURING CLIMB OUT . ELECTED TO DIVERT. MTC FOUND FAILED K215 A/G RELAY AND S266 PROX SENSOR, AND HAS ALSO REPLACED TO CONFIG WARNING CARD. OPS CHECKS ARE NORMAL. NON-REV FCF SUCCESSFUL AND AIRCRAFT RTS.SDR GTIA2019020803147Flap System · malfunctionedON FINAL APPROACH WHEN FLAPS 2 SELECTED ECAM F/CTL FLAPS LOCKED WING TIP BRK ON LANDED WITH SLATS 2 AND FLAPS ZERO--SDR A6WA2019020846374Flap System · malfunctionedAT FLIGHT LEVEL 27,000 RECEIVE FLAP FAIL CAUTION WITH FLAPS AT ZERO DEGREES. NO FLAP SELECTIONS WERE MADE. CREW DECLARED AN EMERGENCY LANDING WITH IAD TOWER. ONCE AT THE GATE THE CREW CALLED MAINTENANCE CONTROL. THE FLAPS WERE SUCCESSFULLY RESET PER FIM SUPPLESDR R61A2019020510144Control Lever · faultyFLAP FAIL MESSAGE AT FL360 ENROUTE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R RHOB T3 SKEW SENSOR AND FLAP/SLAT CONTROL LEVER IAW AMM 27-53-01. OPS CHECK GOOD.
FLAP SKEW SENSOR P/N 5912843-7 S/N 9058 TSN 2267 CSN 1403SDR R61A2019020510143Warning Message · false activationFLAP FAIL AT CRUISE FL330. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED FIM TASK 27-51-00-810-802-A, CLEARED INHIBITS AND PERFORMED FLAPS ACE 1 AND ACE 2 MESSAGES. CLEARED ON EICAS AT THIS TIME, OPS CHECK GOOD IAW AMM 27-51-01.SDR SIMA2019020413004Flap System · malfunctionedFLAP FAIL ON FINAL-C/A-RAI LH FSA #1,#2 ,#3 IAW EMB 145 AMM 27-51-09 AND AMM 27-51-10 OPS TEST GOOD. REMOVED AND REPLACED LH FVS AIRFRAME CONNECTOR J1111 IAW EMB 145 SWPM 20-50-01. RECHECKED WIRING OF LH FVS FOR INSULATION AND CONTINUITY IAW 20-20-03. NO DEFSDR A6WA2019020546361Flap System · failedFLAPS FAIL AT 20 DEGREES ON APROACH PERFORMED FLAPS RESET PROSEDURE IAW AWAC SUP 98-018G FLAPS RESET PLACARDED AND PLACED ON MELSDR DJFA20190127001Trim System · malfunctionedIN FLIGHT WE HAD SWPS FAULT CAS AND SPOILER FAULT CAS ONLY. ON THE MFD IN YELLOW "X" FLAP POSITION, FLAP INDICATION AND PITCH TRIM FLAPS STAYED AT ZERO AND WOULD NOT EXTEND. PITCH TRIM WORKED/ BACKUP PITCH TRIM DIDN'T WORK. AIRCRAFT LANDED WITHOUT INCIDENT. COSDR SIMA20190125001Shaft · contaminatedFLAP FAIL ON APPROACH AFTER FCF, 30 MIN IN FLT A/C COLD SOAKED FLAP FAIL ON EICAS UPON SELECTING FLAPS 9 DEGREES. C/A-TROUBLE SHOT IAW FIM 27-51-00-810-804-A FOUND FLAP FLEXIBLE SHAFT SECTION 3 HAVING MOISTURE PENETRATION. REMOVED AND REPLACED CONTACTS 40, 41SDR A6WA2019012846331Flap · failedFLAPS FAILED AT ZERO DEGREES ON APPROACH.SDR HNAA2019012500028Flap · out of rigPDIS 638 27-50 2047071 23JAN19 PHL CLOSE FLAPS FAIL MSG IN FLT AFTER T/O WHEN SETTING FLAPS TO ZERO. FACT 24JAN19 22:25 PHL
FOUND FLAPS TO BE OUT OF RIG. PERFORMED FLAP ZERO-DEGREE RIGGING IAW AMM 27-53-04. OPS CHECK GOOD OK FOR SERVICE AT THIS TIME.SDR IPXA2019011737957Flap · lockedINSPECTION TYPE:N/A TE FLAP DISAGREE ON APPROACH. THE CREW DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. PERFORMED FIM 27-51-00-815-808 PER TECH SUPPORT AES DAA LAP HANDLE WAS AT 17DEGREES. PER BLOCK ONE THIS CONDITION WILL LOCK OUT FLAPS/SLATS. RESET SYSTEM SDR A6WA2019020546360Warning Message · illuminatedFLAP FAIL CAUTION MESSAGE WHEN FLAPS SELECTED TO 30 DEGREES, FLAPS REMAINED AT 20 DEGREES, C/W QRHSDR AWKA2019010702Current Limiter · failedWHILE CLIMBING OUT, THE FLAP SYSTEM FAILED AT 0. THE FLIGHT CREW ELECTED TO RETURN TO THE DEPARTURE FIELD. THE AIRCRAFT LANDED WITHOUT INCIDENT. TECHNICIANS INSPECTED THE AIRPLANE AND DETERMINED THE FLAP CONTROLLER TO BE FAULTY (P/N 6718328-1). THE UNIT WAS RESDR SWAA2019010428221Torque Tube · shearedDECLARED EMERGENCY, T/E FLAPS WOULD NOT FULLY EXTEND ALONG WITH A SPLIT POSITION INDICATION. R&R TE FLAP RT TORQUE TUBE PER MM.SDR QXEA2019010300001Bearing · defectiveON APPROACH WHEN SELECTING FLAPS FROM 15 TO 35, THE HANDLE REACHED 35 BUT FLAP DRIVE CAUTION LIGHT ILLUMINATED AT THE FLAPS STUCK AT ABOUT 20 DEGREES. FLAP DRIVE CHECKLIST DID NOT RESOLVE. RETURNED TO FIELD. LANDING UNEVENTFUL. REMOVED FROM SERVICE. REPLACEMENSDR AALA201901039014Not Reported · malfunctionedAIRCRAFT WAS GROUNDED: ON APPROACH FLAPS WOULD NOT EXTEND BEYOND 15 DEGREES WHEN FLAP HANDLE WAS MOVED TO 25 DEGREES. RETRACTED FLAG HANDLE TO 15 DEGREES POSITION AND LANDED WITH SELECTED FLAPS. EMERGENCY DECLARED, FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTSDR AALA201901029014Flap System · malfunctionedON APPROACH, THE FLAPS WOULD NOT EXTEND BEYOND 15 WHEN THE FLAP HANDLE WAS MOVED TO 25. RETURNED FLAP HANDLE 15 POSITION, AN EMERGENCY DECLARED AND DIVERTED, LANDED WITH SELECTED FLAPS WITHOUT FUTHER INCIDENT. THE AIRCRAFT WAS GROUNDED. MAINTENANCE PERFORSDR IPXA2018122937335Flap · lack of lubeINSPECTION TYPE:N/A TE FLAP DISAGREE WHEN TE FLAP POSITION SELECTED. FLAPS FAILED TO MOVE TO SELECTED POSITION. EMERGENCY DECLARED AND LANDED AT DESTINATION WITHOUT INCIDENT. T/S C/W IAW FIM 27-51-00-815-808, BLOCK 23 TO 59, FOUND NR 1 & NR 4 FLAP TRANSMISSIONSDR AWKA2018123101Controller · failedWHILE IN CRUISE FLIGHT AT FL470, THE FLIGHT CREW RECEIVED AN AMBER FLAPS FAIL CAS MESSAGE. FOLLOWING THE EMERGENCY CHECK LIST, THE CREW ATTEMPTED A FLAP RESET, BUT, THE CAS MESSAGE IMMEDIATELY RE-POSTED. DUE TO RUNWAY LENGTH AT DESTINATION AIRPORT, THE DECISIOSDR HYIA20181218001Rod · brokenPILOT REPORTED RIGHT OUTBOARD FLAP DID NOT EXTEND. INSPECTION FOUND THE RIGHT OUTBOARD FLAP ACTUATING ROD BROKEN AT THREADS. ROD WAS REPLACED WITH NO FURTHER DEFECTS NOTED.SDR SIMA20181213001Ecu · failedSUPPLEMENTAL FLAP FAIL EICAS MESSAGE. FLAPS FAILED AT 0 DEGREES ON APPROACH. C/A-CMC FAULT MSG RH FLAP SENSOR FAIL HAD TO RESTORE FCU TO RESET FLAPS IAW FIM 27-51-00-810-817-A STEP 1 ITEM 2. RESTORED FCU BACK TO ORIGINAL CONDITION FOR MEL 27-09. REMOVED AND RESDR DALA2018121437213Shaft · corroded(AIRCRAFT 692, L/P 5201369) FLAP DRIVE TORQUE TUBE SPLINED SHAFT CORRODED AT ATTACH POINT TO RH I/ B FLAP TRANSMISSION. INSTALLED NEW SHAFT INST NEW DRIVE SHAFT REF B757 M/M 27-51 ALL RII C/W.SDR IPXA2018120766655Control Lever · bindingDUE TO FLAP DISAGREE IAW FIM 27-51-00-815-808, FOUND FLAP CONTROL LEVER BINDING AT THE ZERO POSITION. LUBRICATED THE FLAP HANDLE IAW FIM 27-51-00/101. IAW AMM 27-51-00-715-001. OPS CHECKED GOOD.SDR IPXA2018120766643Fseu · inoperativeAFTER TAKEOFF, RECEIVED A TE FLAP DISAGREE. AIR TURN BACK. REMOVED AND REPLACED THE NR 1 FSEU IAW AMM 27-51-01-022-006, AND 27-51-01-422-011. NO FAULTS NOTED T/E FLAP SYSTEM OP CHECKED GOOD IAW AMM 27-51-00-715-001.SDR AALA201812049032Torque Tube · excess playLEFT WING FLAP TORQUE TUBE AT THE TRAILING EDGE REAR SPAR AREA, BELOW THE NR 5 SPOILER HAD EXCESSIVE PLAY. REPLACED THE TORQUE TUBE AND PERFORMED A SATISFACTORY OPERATIONAL CHECK IAW AMM 27-51-25.SDR AALA201811309001Fseu · faultedDURING APPROACH, THE TRAILING EDGE FLAPS DISAGREED AT ABOUT 17DEG, FLAP HANDLE AT 20DEG. ACCOMPLISHED QRH CHECKLIST. FLAP / SLAT ELECTRONIC UNIT DISPLAYED CODE 305. ACCOMPLISHED FAULT ISOLATION MANUAL 27, ALL TESTED NORMAL. OPS TESTED OK, FLAP SYSTEM NORMSDR AALA2018112969040Flap System · malfunctionedDURING APPROACH, DURING FLAP EXTENSION, FLAPS STOPPED AT ABOUT 13 DEG, USED ALTERNATE EXTENSION TO 15 DEG. DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. THE AIRCRAFT WAS GROUNDED. PERFORMED VISUAL INSPECTION OF FLAP SYSTEM IAW AMM 27-51-00-210-801. NO DEFECTSDR DALA2018112606798Fseu · faultedSHIP 3761 - ATO - DURING TAKEOFF ROLL AT 90 KNOTS THE T/O CONFIG LIGHT ILLUMINATED WITH AURAL WARNING. CREW ABORTED TAKEOFF. CORRECTIVE ACTION: MAINTENANCE FOUND FSEU FAULTED. REPLACED FSEU. OPS CHECKS GOOD, AIRCRAFT RETURNED TO SERVICE.SDR R61A2018112641175Warning Message · false activationFLAP FAIL EICAS IN FLIGHT. DECLARED EMERGENCY, DIVERTED TO IAD, LANDED WITHOUT INCIDENT. PERFORMED FIM IAW 25-51-00. OPS CHECK GOOD.SDR SIMA201811196001Warning Light · false activationFLAP LOW SPEED ADVISORYIN CRUISE AT FL 370 NO FLAPS SELECTED LEVER NOT MOVED MECH FLAP WARNING AT ALTITUDE AND POSS AIRSPEED UNRELIABLE EMERGENCY DECLARED.-C/A-CHECKED CMC MESSAGES. FOUND 1 OCCURANCE OF MESSAGE "FLAP FEEDBACK POS FAIL" T/SHOT PER FIM TASK 27-5SDR 2020FA0000075Tube · brokenON TAKEOFF FROM KEDC, SELECTED GEAR AND FLAPS UP. AIRCRAFT STARTED ROLLING TO THE LEFT HAVING TO USE FULL AILERON TO KEEP IT STRAIGHT, AT THIS POINT PILOT NOTICED RIGHT FLAP WAS DEPLOYED AND LEFT FLAP UP. SELECTED FLAPS DOWN AND WAS ABLE TO REGAIN CONTROL ONSDR DALA2018111436621Stop · obstructed(AIRCRAFT 5812, L/P 5155985) TE FLAP DISAGREE ON FINAL APP WHEN MOVING FLAPS FROM 15 TO 20. PERFORMED BITE OF FSEU 1+2 FSEU FAULTS MSG 30T FSEU FAULTING 327 FOUND LT OUTBOARD FLAP TORQUE LIMITER TRIPPED. TRIED TO CYCLE FLAPS SLATS WOULD NOT MOVE RAN UP ELEC RESDR AALA2018111659009Fseu · faultyDURING APPROACH, WHILE SELECTING FLAPS 15 TO FLAPS 20, ONE OF THE FLAP INDICATORS STAYED AT 15 FOR ABOUT 3 MINUTES AND THEN SNAPPED TO 20, NO ASSYMETRY FELT IN FLIGHT CONTROLS. DECLARED AN EMERGENCY AND DID A GO-AROUND. FLAP INDICATOR WORKED NORMALLY WHEN FSDR FDEA2018110213075Ball Screw · corrodedTE FLAP DISAGREE WHEN FLAP HANDLE WAS MOVED FROM 0 TO 1. RAN QRH AND LANDED. R & R THE LT INBD NR 4 FLAP TRANSMISSION ASSY IAW MM 27-51-06-4, UP TO UNIVERSAL JOINT DRIVE SHAFT. FOUND THE DRIVE SHAFT BEARINGS EXCESSIVELY CORRODED AND UNSERVICEABLE. R & R SDR AALA2018110231005Fseu · faultedDURING DECENT, FLAP DRIVE MESSAGE INDICATED. EMERGENCY DECLARED AND FLIGHT LANDED WITHOUT FUTHER INCIDIENT. THE AIRCRAFT WAS GROUNDED. MAINTENANCE PERFORMED TROUBLESHOOTING IAW FIM 27-59-00, NO FAULT FOUND AND ACCOMPLISHED GROUND TEST. MAINTENANCE REPLACESDR SWAA2018110126407Transmission · malfunctionedDECLARED EMERGENCY, ON APPROACH WHEN FLAPS SELECTED TO 15 THE FLAPS SPLIT AND STUCK. R&R NR 1 TRAILING EDGE FLAP TRANSMISSION PER AMM.SDR AALA201810299052Strut · excess playAIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON INTERCONNECTING STRUT ON RIGHT HAND WING. REPLACED INTERCONNECTING STRUT ON RIGHT HAND WING PER AMM 27-51-44 AND PERFORMED OPERATIONAL TEST OF THE FLAP SYSTEM PER AMM 27-54-00-710-001-A, TEST IS OK.
Back to JASC 2750