JASC 2751
Service difficulty reports · 3,085
Reports filed under 2751 · Trailing Flap Position Indicating 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 = '2751' 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 = '2751' 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 CALA2009091700555Transmitter · faultyON EXTENDING THE FLAPS TO FIVE, THE FLAPS STOPPED AT ONE WITH LEADING EDGE FLAPS TRANSIT LIGHT ILLUMINATED. NO ASYMMETRY. ACCOMPLISHED THE FLAPS, TRAILING EDGE FLAP DISAGREE CHECKLIST. PER FAULT ISOLATION REMOVED AND REPLACED LEFT FLAP TRANSMITTER REF AMM 2SDR HNAA20090910001Indicator · false indicationTAKE OFF WARNING SOUNDED ON TAKE OFF ROLL. FOUND FLAP INDICATOR DEFECTIVE, REMOVED AND REPLACED FLAP INDICATOR REF M/M 27-53-05 AND COMPLIED WITH T/O WARNING HORN, OPS CHECKS PER CARD 31-50-00QSDR CA090902004Indicator · damagedWHEN LIGHTED POINTER ASSY WAS INSPECTED PRIOR TO FLAP POSITION INDICATOR ASSY, TECH NOTED THAT LIGHT ASSY WAS HANGING LOOSE OUTSIDE THE PLASTIC SLIDE AS OPPOSED TO BEING IMBEDDED IN THE PLASTIC SLIDE. ASSEMBLING THE POINTER TO THE INDICATOR SCALE WOULD RENDER SDR IPXA09557260Transmitter · faultyINSPECTION TYPE:N/A DIVERSION - ON APPROACH RECEIVED T/E FLAP DISAGREE GOING FROM FLAPS 15 TO 20. T/S SYSTEM USING FIM 27-51-00. RT FLAP TRANSMITTER WAS HUMMING AND BUZZING. REPLACED RIGHT FLAP TRANSMITTER. OPS CHECK GOOD.SDR SIMA200924501Velocity Sensor · failedON FLIGHT 3924 DURING THE CLIMBOUT THE CREW DISCOVERED FAILURE OF FLAPS. THE CREW REPORTED THAT THE FLAPS WOULD NOT RETRACT FROM 9 DEGREES. AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED ANDSDR HNAA2009090200026Indicator · false indicationSTICK SHAKER ATTIVATED IN FLIGHT AT ABOUT 220 KNOTS FOR ABOUT 10 MINUTES WHILE DECENDING UNTIL 15 MILES OUT. BOTH STALL SYSTEMS TEST NORMAL ON THE GROUND. R/R FLAP POSITION INDICATOR, PERFORMED FUNCTIONAL TEST OF STALL WARN SYS. CALIBRATED NR 1 AND 2 STALL WSDR YENA20090901102Position Sensor · failedFLT 185 JFK-SAN FLIGHT CREW REPORTED TRAILING EDGE FLAP WOULD NOT EXTEND. FAILURE APPEARS TO BE RIGHT TRAILING EDGE. CHECKED AND ADJUSTED RIGGING AFTER REPLACEMENT OF LT AND RT PPU. RESET WTB AND OPS CHECK OK AS PER AMM 27-81-51, 27-54-00-05, 27-51-19.SDR SAJFCALS098031Transmitter · failedCREW VHF INFORM DURING APPROACH T/E FLAPS STUCK APPROX 10.5, IND L-15 R-10. FLAP POSITION TRANSMITTER FAIL. EO 738-24-00-0017 WAS ISSUED TO INSP/PROTECT FLAP POS TX TER. EO 738-27-51-0006 WAS ISSUED TO RECORD FAULT HISTORY FROM FSEU AT EVERY RE-CHK. (B-1860SDR SWAA095630Indicator · faultyDECLARED EMERGENCY. SELECTED FLAPS 5 AND GOT RIGHT FLAPS 1, LEFT FLAPS BETWEEN 5 AND 10. ALSO L/E FLAP TRANSIT LIGHT ILLUMINATED. REMOVED AND REPLACED FLAP POSITION INDICATOR AND REPAIRED POSITION TRANSMITTER WIRING.SDR QXEA2009083100647Warning System · malfunctionedLAX - FLAP POWER CAUTION ILLUMINATES UPON SELECTION OF FLAPS 35- FLAPS REMAINED AT 15. AFTER LANDING, FLAPS CONT CB(L7) CYCLED PER CHECKLIST. FLAP POWER CAUTION WENT OUT. UPON SELECTION OF HANDLE TO FLAPS 0, BOTH FLAP POWER AND FLAP DRIVE CAUTIONS ILLUMINATESDR MASA2009082400271Transmitter · faultyASH FLT 7110 ORD-CAK. CREW DECLARED AN EMERGENCY AND LANDED NORMALLY. CREW REPORTED EXPERIENCING THE AIRCRAFT PITCHING NOSE DOWN AS DESCENT WAS STARTED. AS THIS OCCURRED CREW REPORTED GETTING HYDRAULIC 2B AND 3B PUMP CAUTION MESSAGES INTERMITTENTLY. AT THISDR SWAA095086Attach Fitting · corrodedDURING SCHEDULED 24Y CHECK, FOUND LT WING NR 2 FLAP TRACK CARRIAGE FORE FLAP ATTACH FITTING CORRODED. REMOVED AND REPLACED FITTING PER OHM.SDR SWAA094936Sensor · faultyDECLARED EMERGENCY, ON APPROACH TO AIRPORT THE LT FLAP INDICATOR INDICATED POSITION ZERO AND RT FLAP INDICATED POSITION 1, SPLIT FLAP INDICATION ON PANEL. REMOVED AND REPLACED LT FLAP POSITION TRANSMITTER & NR 4 SKEW SENSOR PER MM.SDR USAA20090803SB128Indicator · faultyEWR - CREW DECLARED AN EMERGENCY INBOUND TO EWR FOR A FLAP FAIL MESSAGE. WHEN FLAPS WERE EXTENDED FOR LANDING, A SPLIT WAS NOTED IN THE POSITION INDICATION. CREW EXECUTED A GO-AROUND. FLAPS WERE THEN RETRACTED, AND THEN EXTENDED TO 15 WITH NORMAL INDICATION.SDR QXEA2009080300564Warning System · activatedGEG - FLAP POWER CAUTION LIGHT ILLUMINATED SHORTLY AFTER SELECTING FLAPS FROM 5 DEG TO 15 DEG, ATTEMPTED RESET PER E&A CHECKLIST. FLAPS REMAINED AT 12 DEG. LANDED WITHOUT INCIDENT. PERFORMED FIM TASK 27-50-00-810-802. FAULTS CLEARED, PERFORMED SEVERAL OPS SDR QXEA2009080300563Transducer · malfunctionedGEG - FLAP POWER CAUTION MESSAGE WHEN FLAPS SET TO 35 DEGREES. FLAPS STUCK AT ZERO (0). LANDED UNEVENTFUL. REMOVED AND REPLACED LT FLAP POSITION TRANSDUCER IAW Q400 AMM TASK 27-53-06-960-801-STEPS AS REQUIRED PERFORMED FUNCTIONAL TEST OF FLAP CONTROL SYS IASDR CA090729003Bpsu · malfunctioned(CAN) ON SHORT FINAL, FLT CREW RECEIVED A FLAP FAILURE CAUTION MESSAGE WITH THE FLAPS TRAVEL STOPPING AT30 DEGREES. ACFT HAD POST MOD ACTUATORS INSTALLED AT THE LAST FLAP FAIL EVENT, BACK AT FEB 08,2008. THE FECU (52B AND 25C)CODES WERE RETRIEVED BY MAINT. SDR A6WA200940421Detector · malfunctionedUPON CLIMBOUT FLAP FAIL AT 20 DEGREES WHEN HANDLE SELECTED TO 8 DEGREES. RESET IAW SUPP 98-018C. REF 190586/2 - TROUBLESHOT TO SKEW DETECTION UNIT, REMOVED AND REPLACED SKEW DETECTION UNIT IAW AMM 27-51-15, CYCLED FLAPS 8 CYCLES. OPS CHECK GOOD. REMOVED FRSDR USAA20090721SB119Indication Sys · malfunctionedON APPROACH TO ORD, CAPTAIN REPORTED THE FLAPS WOULD NOT EXTEND PAST 1 DEGREE. FLAP POSITION INDICATOR SHOWED ASYMMETRY BUT AIRCRAFT DID NOT EXHIBIT SIGNS OF CONDITION. FLIGHT ACCOMPLISHED A GO-AROUND AND FLAPS WERE EXTENDED TO 15 DEGREES USING ALTERNATE EXTSDR AALA20090719RNO01Transmitter · faultedRNO - ON APPROACH FLIGHT RECEIVED INDICATION OF TRAILING EDGE FLAP ASYMMETRY PROBLEM. ACCOMPLISHED A GO AROUND. LANDED RNO WITHOUT INCIDENT. REPLACED NUMBER ONE SLAT TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR ZZDA2009200Sensor · inoperativeDURING APPROACH AFTER CALLING FOR FLAPS 5, REALIZED THE FLAPS WERE STUCK IN THE 1 POSITION WITH AN ASYMMETRICAL INDICATION. RAN THE QRH PROCEDURES, FLAPS WOULD NOT COME UP OR DOWN. SWAPPED NR 4 AND NR 5 SKEW SENSORS AND PROBLEM FOLLOWED. REPLACED NR 4 SKEW SDR ASOA200900776Warning System · activatedFLAPS FAIL CAUTION MSG IN FLT. FLT 5013, 5020, 5626 CX, EMERGENCY DECLARED.SDR ASOA200900763Warning System · activatedAFTER TAKEOFF, FLAPS FAIL CAUTION MSG IN FLIGHT. COMPLIED WITH QRH AND CONNECTED MTC CONTROL. DECISION WAS MADE TO RETURN TO ATLANTA, EMERGENCY DECLARED. LANDING UNEVENTFUL.SDR CA090708008Indicator · malfunctioned(CAN) CREW SELECTED FLAP LEVER TO 8 DEGREES AND RECEIVED A FLAP FAIL CAUTION MESSAGE. MULTIFUNCTION DISPLAY (MFD) WAS INDICATING FLAP AT ZERO DEGREE. THERE WAS NO EMERGENCY DECLARED AND ACFT LANDED WITHOUT FURTHER INCIDENT. FLAP ELECTRONIC CONTROL UNIT (FECSDR ASOA200900740Detection Sys · defectiveFLAPS FAIL AT 0 WHILE CLIMBING OUT AT FLT LEVEL 230, EMERGENCY DECLARED. SKEW DETECTION SYSTEM.SDR DXTA2009062503703Transmitter · erraticREPLACED LT ENTRATIC FLAP POSITION TRANMITTER WITH OVERHAULED UNIT. OPS CHECKED GOOD IAW MM 27-50-00.SDR DXTA2009062903703Indicator · inaccurateWHEN FLAPS WERE SELECTED TO 15 THE INDICATOR BOUNCED AROUND AND WENT BACK TO 0. FLAPS WERE CHECKED ON THE GROUND AND WHILE AT 45 THE INDICATOR READ 25.SDR COMA2009061590011Warning System · activatedON FINAL APPROACH INTO CVG RECEIVED FLAPS FAIL CAUTION MSG. EMERGENCY DECLARED, A/C LANDED SAFELY. CLEARED INHIBITS PER FIM 27-50-00, MSG CLEARED. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED.SDR ASOA200900574Warning System · activatedFLAP FAIL CAUTION MSG ON CLIMB OF ATL AT 18800' AND LANDED AT 300FPM, EMERGENCY DECLARED. FLT 5563 DEL 32 MINSSDR CALA2009042300212Transmitter · inoperativeTRAILING EDGE FLAP LIGHT ON AT FLAPS 5 DURING APPROACH. RAN CHECKLIST LANDED AT FLAPS 5, TROUBLESHOT PER FIM 27-51-00, FIG 104, FOUND MESSAGE NUMBER 27-51080. REMOVED AND REPLACED NR 5 TRAILING EDGE FLAP SKEW TRANSMITTER IAW AMM 27-51-45. OPERATIONAL CHECKSSDR ASOA200900468Warning System · activatedFLAPS FAIL CAUTION MSG, EMERGENCY DECLARED. SKEW DETECTION SYSTEM.SDR UHLA2009041100033Sensor · inoperativeFLAP FAIL EICAS MESSAGE SHORTLY AFTER REACHING CRUISE ALTITUDE. DECLARED AN EMERGENCY, LANDED ZERO FLAPS OR SLATS WITHOUT INCIDENT. MAINTENANCE REPLACED THE SF-ACE NR 1 AND T3 AND T4 LT O/B SKEW SENSORS. THERE HAVE BEEN NO WRITE UPS SINCE.SDR USAA20090410SB054Indicator · faultyON APPROACH TO DEN, CREW ENCOUNTERED A FLAP PROBLEM. THERE WAS ALSO LOW LEVEL TURBULENCE REPORTED IN THE AREA WITH GUSTY SURFACE WINDS. AT FIRST THE FLAPS WERE SLIGHTLY SPLIT AND STUCK IN THE FLAPS 1 POSITION. CREW INITIATED A GO-AROUND. AS CREW PROCEEDED SDR ASOA200900368Sensor · failedFLAP FAIL ON TAKEOFF FLAPS STUCK ON 8FT. EMERGENCY DECLARED, A/C RETURNED TO ATL AFTER T/O. THIS SDR WILL REMAIN OPEN PENDING MTC DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. FLT 5108 DEL 38 MINS. SKEW DETECTION SYSTEM. REMOVED AND REPLACED LT NR 3 SDR 1PC2009F00000Warning System · malfunctionedFLAP AND PUSHER CAWS LIGHT ILLUMINATED AFTER TAKEOFF. PAGE 3-32 (A) OF PC12/45 POH REV 11 DATED MARCH 1ST, 2003 INDICATES POSSIBLE FLAP ASYMMETRY PAGE 7-5 OF PC12/45 POH REV 11 DATED MARCH 1ST 2003, THE ASYMMETRY MAY BE IN EXCESS OF 2 DEGREES. RESET FLAP CONSDR ASOA200900309Warning System · activatedFLAPS FAIL CAUTION MSG ILLUM IN FLT AT 0 AT 17000. EMERGENCY DECLARED. A/C RETURNED TO ATL AFTER T/O. FLT 5399 DEL 156 MINS.SDR CALA2009031700143Transmitter · failedON APPROACH WHILE SETTING THE FLAPS TO 30, GOT A SPLIT FLAPS 17 TO 24. ON G/A PLACED FLAPS TO 15 DEGREES AND FLAPS STAYED AT 17 AND 24, ON DOWNWIND FLAPS CAME UP TO BETWEEN 10 AND 15. PUT FLAPS TO 10 WITH NORMAL INDICATIONS. QAR SHOWED A DELAY FROM FLAP XMTSDR DALA1217570635Gear · unknownTRAILING EDGE FLAP TRANSMISSION GEAR - REPLACEMENT IAW 06-097281-03 REV A ME04.SDR ASOA200900286Detection Sys · failedFLT 5609, FLAPS FAIL AT 0 WHEN SELECTED TO 8. EMERGENCY DECLARED. SKEW DETECTION SYSTEM. INSTALLED SKEW DETECTION PANEL IAW AMM 27-51-15 OPS CHECK GOOD DEFER CLEARED PLACARD REMOVED.SDR UALA200903100074AIndicator · malfunctionedFLAP PROBLEM. RTFL. REMOVED AND REPLACED TRAILING EDGE FLAP POSITION INDICATOR. PERFORMED THE TEST OF THE TRAILING EDGE FLAP POSITION INDICATOR SYSTEM. TESTS OK. RAN FLAPS FULL UP AND DOWN SEVERAL TIMES, FLAPS ARE WORKING NORMALLY.SDR UALA2009031000627Rotary Actuator · trippedT/E FLAP DISAGREE INDICATION, WHEN CREW WENT TO FLAPS 5. LOWERED FLAPS WITH ALT SWITCH PER CL. FOUND LT WING INBOARD FLAP OUTBOARD ROTARY ACT TRIPPED; RESET. ALSO FOUND RT WING OUTBOARD FLAP OUTBOARD FLAP ROTARY ACT TRIPPED; RESET. OPERATED FLAPS ONE CYCLESDR DXTA2009022303521Sensor · malfunctionedON APPROCH THE FLAPS FAIL CAS MESSAGE CAME ON WITH THE SLATS EXTENDED AND THE FLAPS AT 3DEG. REPLACED LT AND RT RESOLVER. GAINED ACCESS TO AND REMOVED LT AND RT RESOLVERS. REPLACED WITH OVERHAULED RESOLVERS. IAW MM 27-52-00 ADJUSTED RESOLVERS AND OPS CHECKED SDR ASOA200900207Warning System · activatedTHE "FLAPS FAIL" MSG IN CRUISE FLIGHT DESCENDING THROUGH 19,000FT AT 290 KIAS WITH LIGHT TO MODERATE TURBULENCE.SDR SAJFCALS098005Transmitter · malfunctionedDURING CLIMB, EICAS MSG "TE FALPS", "FLAPS DRIVE" IN VIEW. CREW SATCOM INFORM MOC AND PERFORM QRH THEN ACFT TURN BACK. CMC DOWNLINK FOUND OB TE FLAPS IND SHOW ASYMMETRY. REPLACED RT OTBD T/E FLAPS POS X’MIT AND OPERATION CHECK NML. PARTS SHIPPED FROM CI SPSDR AALA2009020301017Transmitter · out of positionDEN - INFLIGHT DFW-EGE. CREW REPORTED, HAD A TRAILING EDGE FLAP DISAGREEMENT AND PROCEEDED TO DEN, DECLARED AN EMERGENCY. LANDED IN DEN WITHOUT INCIDENT. ADJUSTED POSITION TRANSMITTER FOR TRAILING EDGE FLAP POWER DRIVE UNIT. SYSTEM GROUND CHECK NORMAL.SDR YENA20090204011Warning System · activatedFLT 1417 - MCO-AUS - FLAPS FAIL. INTERROGATED CMC. RETRIEVED FAULT CODE 27512009ACE. PERFORMED FIM TASK 27-51-00-810-804-A. CLEARED INHIBITS. FLAP TEST OK. FLAP LO RATE MESSAGE ON EICAS ON MEL.SDR CALA2009020200075Sensor · corrodedWHILE ON APPROACH DURING FLAP EXTENSION THE FLAPS STOPPED AT AROUND 1 WITH A SLIGHT ASYMMETRY AND WOULD NOT EXTEND FURTHER. FOLLOWED PROCEDURES WHICH CALLED FOR USE OF ALTERNATE FLAP EXTENSION TO 15. REMOVED AND REPLACED NR 3 SKEW SENSOR AND CONNECTOR PER MMSDR COMA2009020350076Warning System · activatedON APPROACH INTO JFK RECEIVED FLAPS FAIL CAUTION MSG AT 0 DEG. EMERGENCY DECLARED, A/C LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I0002, FLAPS FAIL CAUTION MESSAGE FOLLOW UP MAINTENANCE ACTION.SDR SWIA200920932Bpsu · failedFLT 5951 - FLAPS FAIL AT 20 DEGREE POSITION. REPLACED RIGHT BPSU, PN 855D100-15 SN OFF 2192.SDR AALA2009011300158Transmitter · failedLAX INFLIGHT - FLAP POSITION TRANSMITTER WOULD NOT HOLD POSITION. CREW REPORTED ASYMMETRY WARNING. LANDED LAX WITHOUT INCIDENT. REPLACED TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION.
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