JASC 2781
Service difficulty reports · 1,398
Reports filed under 2781 · Leading Edge Slat 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 = '2781' 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 = '2781' 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 R61A20100082Sensor · faultyCREW REPORTED, A SLAT FAIL DURING APPROACH INTO DCA. DECLARED AN EMERGENCY AND DIVERTED TO IAD AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT TO TROUBLESHOOT. MAINTENANCE REMOVED AND REPLACED THE LT 2/3 O/B SLAT SKEW SENSOR AND PERFSDR VNAA2010022600010Warning System · malfunctionedCREW REPORTED A SLAT FAIL MESSAGE AT 20° AFTER DEPARTURE FROM IND. AIRCRAFT RETURNED TO IND AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND INSPECTED THE AIRCRAFT AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. RESULTS OF THE CHECKS WERSDR REXA201000025Warning System · malfunctionedSLATS FAIL CAUTION MESSAGE. CLEARED INHIBITS FROM SFECU AND PERFORMED OPS CHECK OF SLAT/FLAP SYSTEM IAW AMM 27-51-05. OPS CHECK GOOD, OK FOR SERVICE. MX PERFORMED AT OUTSTATION: BUF.SDR UALA2010020900504Switch · failedL/E SLAT ASYM EICAS, RTFL. REPLACED LT INBD SLAT LOSS SENSING SWITCH S10589. CYCLED SLATS SEVERAL TIMES WITH NO ASYM MSGS.SDR USAA20100203EM002Sensor · faultyFLIGHT 9198, PHL-CLT - FLIGHT WAS A POSITION FERRY FLIGHT TO CLT. INBOUND THE CREW DECLARED AN EMERGENCY WHILE ON APPROACH TO LANDING FOR FLAPS 1, RECEIVED SLATS 0 FLAP 1 MESSAGE. THE CREW PERFORMED QRH PROCEDURE; LANDED WITH SLATS 0, FLAPS 2. BRAKES WERE USDR MYWA100017Warning System · false activationETOPS SIGNIFICANT SYSTEM - L/E SLAT IN TRANSIT LIGHT REMAINS ON.SDR SWIA201023512Warning System · malfunctionedSLATS FAIL CAUTION MESSAGE ON APPROACH. (FLT 6698) CLEARED INHIBITS, OPERATIONAL CHECKS NORMAL.SDR YENA20100112006Sensor · malfunctionedFLT JB907 JFK-ORD ON APPROACH TO ORD CREW DECLARED AN EMERGENCY FOR A "SLAT FAIL" CAS MESSAGE WHEN SELECTING FLAPS SLATS FROM ZERO TO 1. CREW ACCOMPLISHED QRH PROCEDURES AND LANDED UNEVENTFULLY. MX RETRIEVED CMC CODE 27811014ACE AND COMPLIED WITH AMM FIM 27-SDR UALA2010011100123Actuator · malfunctionedLE SLAT DISAGREE MSG, RTFL. SLAT-FLAP OPS STOPPED AT AN INDICATED POSITION JUST LESS THAN 1. ACCOMPLISHED REVIEW OF FSEU. LAST FLIGHT FAULT SHOWS L/E DISAGREE MSG NR 310. VISUALLY CHECKED L/E ROTARY ACTUATORS. NR 6 INBD ROTARY ACTUATOR WAS TRIPPED. ALL OTHERS SDR UAL2010F00000Actuator · trippedL/E SLAT DISAGREE MESSAGE, RTFL SLAT-FLAP OPS STOPPED AT AN INDICATED POSITION JUST LESS THAN 1. ACCOMPLISHED REVIEW OF FSEU LAST FLIGHT FAULT SHOWS L/E DISAGREE MSG NR 310. VISUALLY CHECK L/E ROTARY ACTUATORS. NR 6 INBD ROTARY ACTUATOR WAS TRIPPED. ALL OTHESDR R61A20090102Sensor · faultyCREW DECLARED EMERGENCY FOR SLAT FAIL INTO DEN, LANDED WITHOUT INCIDENT. MTX DISPATCHED TO A/C TO TROUBLESHOOT, AND FOUND FAULT CODE 27811014ACE. MTX REMOVED AND REPLACED THE RT OUTBOARD SKEW SENSOR PER EMB AMM, A/C WAS THEN RELEASED BACK INTO SERVICE.SDR YENA20091224182Sensor · failedFLT JB601 PWM-JFK UPON SELECTION OF FLAPS 5, SLATS EXTENDED, RECEIVED "SLAT FAIL" CAS MESSAGE. SLATS STILL INDICATE FULL, BUT IN AMBER. FOUND RT OUTBOARD 2/3 SKEW SENSOR AT FAULT. REMOVED AND REPLACED RT OUTBOARD 2/3 SKEW SENSOR IAW MM 27-83-01. OPS CHECK SDR YENA20091214173Sensor · failedFLT 130 JFK-BUF ON FINAL APPROACH INTO BUF "SLAT FAIL" EICAS MESSAGE WHEN SLAT/FLAPS SELECTED TO POS 1 LANDING UNEVENTFUL. BUF MX PERFORMED AMM FIM TASK 27-83-00-810-814A FOUND TO BE SF-ACE TRANSITORY CONDITION OPS CHECK GOOD. AFTER NEXT FLIGHT IN BOS, MX PESDR AALA20091210DFW01Sensor · faultyON APPROACH INTO DFW WHEN EXTENDING FLAPS FROM 15-20, SLAT ASYMMETRY MESSAGE DISPLAYED ON EICAS. LANDED WITHOUT INCIDENT AT 160 KNOTS AMD NORMAL SINK RATE. REPEAT. REPLACED SENSORS S285 AND S286.SDR R61A20090088Sensor · faultyCREW REPORTED FLAP/SLAT FAIL MSG WHILE ON APPROACH INTO LGA. CREW DECLARED AN EMERGENCY AND LANDED AT LGA WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT TO TROUBLESHOOT. MAINTENANCE REMOVED AND REPLACED THE RT O/B SKEW SENSORS PER EMB AMM. A/SDR VNAA2009113000006Warning System · malfunctionedCREW REPORTED A SLATS FAIL CAUTION MSG IN FLIGHT. CREW DECLARED AN EMERGENCY AND LANDED SAFELY IN LIT. MAINTENANCE RESET THE SLAT SYSTEM AND TESTED AIRCRAFT PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.SDR R61A20090081Sensor · malfunctionedCREW RECEIVED SLAT FAIL WHILE INBOUND TO BOI. EMERGENCY VEHICLES WERE DISPATCHED AND ROLLED, AIRCRAFT LANDED WITHOUT INCIDENT AT BOI. MAINTENANCE REMOVED AND REPLACED THE LT NR 3 SKEW SENSOR PER EMB AMM.SDR YENA20091105149Warning System · malfunctionedFLT JB1403 - AUS-SFO 'SLAT FAIL' MESSAGE WHEN SELECTING FLAPS 1. FLIGHT CREW FOLLOWED QRH ,LANDED SLATS 0 AND FLAPS 2 WITHOUT INCIDENT. MX ACCOMPLISHED AMM FIM TASK 27-11-00-810-802A FAULT CONSIDERED TRANSIENT, CYCLED SLATS & FLAPS 2 TIMES NO FAULTS NOTED. SDR AALA20091018ORD01Sensor · failedWHEN RETRACTING THE SLATS ON DEPARTURE THE SLAT DISAGREE LIGHT STAYED ILLUMINATED. THERE WAS NO ADVERSE YAW OR ROLL. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED RIGHT SLOT C SENSOR.SDR FDEA200909123288Warning Light · illuminatedSLAT DISAGREE LIGHT LEVEL 2 ON SHORT FINAL, 36R MEM NO CONTROL ISSUES, ACFT STABLE AND HAD BEEN CONFIGURED FOR LONG TIME ALREADY. PERFORMED GO AROUND, RAN QRH, RECONFIGURED, NO MORE LITES. UNEVENTFULL LANDING. PSEU HAD NO FAULTS STORED AND RTS OK. FCC'S HASDR C8GA20090183Switch · defectiveDURING CLIMB OPERATION, WHILE RETRACTING THE FLAP FROM FLAPS 5 TO FLAPS 2. THE L/E FLAP AMBER LIGHT ILLUMINATED, FLIGHT ENGINEERS FLAP DISPLAY INDICATED NR 6 FLAP OUT. ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMSDR USAA20090828SB143Warning System · malfunctionedPHX - DURING APPROACH, AS FLAPS WERE SELECTED FROM FLAPS 1 TO 5, CREW RECEIVED A LEADING EDGE FLAPS TRANSIT LIGHT ALONG WITH THE NR 2 SLAT. CREW EXECUTED A MISSED APPROACH AND ACCOMPLISHED A GO-AROUND. PRIOR TO LANDING WITH FLAPS AT 15, THE LEADING EDGE FLAPSDR AALA20090820JFK01Sensor · faultyJFK - CREW REPORTED LEADING EDGE SLAT ASYMMETRY LIGHT ILLUMINATED. RETURNED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER FOUR OUTBOARD SLAT SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR AALA20090813MIA01Sensor · inoperativeMIA - CREW REPORTED LEADING EDGE SLAT ASYMMETRY FAULT. EMERGENCY DECLARED RETURNED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR USAA20090814EM051Sensor · openFLIGHT 1944, ON APPROACH TO CLT THE FLAPS FAILED TO EXTEND WHEN COMMANDED. THE CAPTAIN DECLARED AN EMERGENCY, THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE RIGHT OUTBOARD SLAT SKEW SENSOR S0162 OPEN. MAINTENANCE REMOVED AND REPLACED THE SDR RYNA200908100012Proximity Sensor · out of adjustAT 120 KTS ABORTED TAKEOFF DUE TO FLAP TAKEOFF WARNING INDICATION CAUTION LIGHT ILLUMINATED ADDITIONALLY THE MASTER WARNING LED ASYMMETRY LIGHT BELOW 80KTS. PERFORMED B-767 FIM 27-81-00N FOUND THE RT NR 12 O/B PROXIMITY SENSOR FAIL. ADJUSTED THE NR 12 O/B LESDR UALA2009081002406Fseu · malfunctionedLEADING EDGE SLAT DISAGREE MSG. RTFL. ON FLAP RETRACTION LEADING EDGE SLAT DISAGREE MSG. VISUALLY VERIFIED FLAPS AND SLATS RETRACTED. SELECTED ALT SLATS AND FLAPS MSG CLEARED. USED ALT FLAPS TO RETURN TO DEN. CHECKED FSEUS, NO FAULTS, NO HISTORY. CHECKESDR USAA20090722EM046Sensor · faultySLAT FAIL ON FLAP EXTENSION, FAILED TO RESET WHEN CYCLED TO 0 THEN BACK TO 1. CREW DECLARED AN EMERGENCY LANDING. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED WIRING FROM BOTH RIGHT OUTBOARD SKEW SENSOR TO SF-ACE 1. REPLACED RT OUTBOARD SKEW SENSOR SDR R61A20090035Sensor · failedCREW REPORTED SLAT FAIL DURING SLAT EXTENSION WHILE ON FINAL. CREW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT INTO PIT. MAINTENANCE WAS DISPATCHED TO THE A/C TO TROUBLESHOOT. MAINTENANCE FOUND BOTH LT O/B SKEW SENSORS TO BE AT FAULT, AND REMOVED AND REPSDR YENA20090715075Sensor · failedFLT 1422 - LGB-PDX, "SLAT FAIL" UPON SELECTING FLAP 1 ON APPROACH. SLATS FAILED TO MOVE AND DISPLAYED AN AMBER "0" POSITION INDICATION. QRH PROCEDURE APPLIED AND FAILURE PERSISTED. REMOVED AND REPLACED LT OUTBOARD SCREW SENSOR 2 AND 3 PER 27-83-01. OPS CHESDR R61A20090033Sensor · failedCREW RECEIVED A SLAT FAIL MESSAGE DURING APPROACH, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT IN CLT. MAINTENANCE WAS DISPATCHED TO THE A/C TO TROUBLESHOOT, AND FOUND LT O/B SKEW SENSORS TO BE AT FAULT. MAINTENANCE REMOVED AND REPLACED BOTH LT O/B SKEW SSDR UHLA2009062100041Sensor · inoperativeON APPROACH AFTER SELECTING FLAPS 3 RECEIVED SLAT FAIL EICAS MESSAGE. EXECUTED GO AROUND. ONE LEVELED OFF, RAN QRH AND DECLARED EMERGENCY. LANDED WITH NO INCIDENT, SLATS AT 3 AND FLAPS AT 2. MAINTENANCE REMOVED AND REPLACED LHOB 3/4 SKEW SENSOR. SI 270826SDR R61A20090030Sensor · faultyCREW RECEIVED SLAT FAIL DURING APPROACH INTO SAT. CREW DECLARED EMERGENCY AND LANDED IN SAT WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO AIRCRAFT, TROUBLESHOT AND FOUND THE LT OUTBOARD SKEW SENSOR AT FAULT. MAINTENANCE REMOVED AND REPLACED THE LT OUTBOARSDR USAA20090527EM033Sensor · faultyFLIGHT 1845, PHL-FPO - THE CREW RECEIVED A SLAT FAIL WITH SLAT DEPLOYED TO UNKNOWN POSITION MESSAGE. THE CREW FOLLOWED THE QRH AND WAS UNABLE TO CLEAR THE ITEM. THE CREW DECIDED TO RETURN TO THE FIELD,PHL, AND CALLED EMERGENCY EQUIPMENT OUT AS A PRECAUTIONASDR YENA20090513048Sensor · failedFLT NR1310, ON APPROACH SLAT FAIL AT POSITION 3, REMOVED AND REPLACED RT WING SKEW SENSOR AT THE 2/3 POSITION. OPERATED SLATS SEVERAL TIMES. NO FAULTS NOTED.SDR YENA20090505044Sensor · defectiveFLT 1401, FLL-AUS, SLAT FAIL AFTER TAKEOFF, RETURN TO FLL. TROUBLESHOT PER FIM 27-81-00-810-807-A. FOUND DEFECTIVE AND REPLACED SLAT SKEW SENSORS, RT 2/3 & RT 3/4 OUTBOARDS PER AMM 27-83-01. CLEARED INHIBITS AND CYCLED FLAPS/SLATS NORMALLY. SLAT FAIL MESSASDR YENA20090505042Sensor · defectiveFLT 1401, FLL-AUS, SLAT FAIL AFTER TAKEOFF, RETURN TO FLL. TROUBLESHOT PER FIM 27-81-00-810-807-A, FOUND DEFECTIVE AND REPLACED SLAT SKEW SENSORS, RT 2/3 & RT 3/4 OUTBOARDS PER AMM 27-83-01. CLEARED INHIBITS AND CYCLED FLAPS/SLATS NORMALLY. SLAT FAIL MESSAGSDR R61A20090022Sensor · failedA/C RECEIVED A SLAT FAIL MESSAGE DURING APPROACH INTO PIT. CREW DECLARED AN EMERGENCY AND LANDED IN PIT WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT, AND TROUBLESHOT PROBLEM TO THE LT OUTBOARD SKEW SENSORS. MAINTENANCE REMOVED AND REPLACED BSDR UHLA2009043000035Sensor · out of rigAPPROXIMATELY 20 MINUTES AFTER TAKEOFF, CREW RECEIVED EICAS MESSAGE SLAT FAIL. DIVERTED TO IND, DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. MAINTENANCE RE-RIGGED THE SLAT SKEW SENSORS AND OPS CHECKED GOOD.SDR R61A20090019Sensor · failedCREW RECEIVED SLAT FAIL MESSAGE ON APPROACH INTO PHL. CREW DECLARED EMERGENCY INTO PHL, AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE A/C, TROUBLESHOT PROBLEM DOWN TO RT OUTBOARD SKEW SENSOR. MTX REMOVED AND REPLACED THE RT OUTBOARD 3/4 SKESDR R61A20090018Sensor · failedCREW RECEIVED SLAT FAIL MESSAGE ON APPROACH INTO CLT. CREW DECLARED EMERGENCY INTO CLT, AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE A/C, TROUBLESHOT PROBLEM DOWN TO LT OUTBOARD SKEW SENSORS. MTX REMOVED AND REPLACED BOTH LT OUTBOARD SLAT SDR UALA2009041501094Sensor · faultyLE SLAT ASSY MSG. FLIGHT DIVERTED. BITE CHK PROX SWITCH ELEX UNIT SHOW SENSOR 303 RT 9 INBD FAILED. RPLD SENSOR S303, OP CKD OKAY. BITE TEST OK.SDR R61A20090015Sensor · failedCREW REPORTED SLAT FAIL WHILE EN ROUTE TO DCA, DECLARED EMERGENCY AND DIVERTED TO IAD AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE A/C, TROUBLESHOT AND FOUND RT O/B NR 2 SKEW SENSOR AT FAULT. REPLACED THE RT O/B NR 2 SKEW SENSOR PER EMB AMMSDR USAA20090331EM018Sensor · inoperativeFLIGHT 1907 - PHL-DFW - THE FLIGHT CREW RECEIVED A SLAT FAIL EICAS MESSAGE EN ROUTE TO DFW. THE FLIGHT DIVERTED TO PIT FOR MAINTENANCE. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED THE LEFT SLAT 2/3 SKEW SENSDR QXEA2009032600197Detector · failedSEA - INTERMITTENT SLAT FAULT STATUS MSG. RETURNED TO FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. NO MX AVAILABLE IN YEG. PLACED ON MEL 27-51-4. RETURNED TO SERVICE. MEL CLEARED ON 3/25. REPLACED SKEW SENSOR ON LT INBD SLAT IAW CRJ AMM 27-81-39 PG 401-4SDR AALA2009032000003Sensor · faultySXM - ON APPROACH LEADING EDGE FLAPS TRANSIT LIGHT ILLUMINATED. EMERGENCY DECLARED LANDED SXM WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND NUMBER TWO LEADING EDGE SLAT RETRACT SENSOR FAULT. REPLACED NUMBER TWO LEADING EDGE FLAP PROXIMITY SENSOR. SDR R61A20090012Sensor · failedCREW REPORTED SLAT FAIL INTO MHT ON EICAS DURING APPROACH. CREW DECLARED EMERGENCY INTO MHT, AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO A/C. TROUBLESHOT AND FOUND RT OUTBOARD SKEW SENSOR AT FAULT. REPLACED RT OUTBOARD SKEW SENSOR PER EMB AMSDR YENA20090304022Warning System · false activationSLAT FAIL MESSAGE WHILE SELECTING LEVER FROM "0" TO THE "1" POSITION, DURING APPROACH. ACCOMP'D FIM TASK 27-81-00-810-805A. CLEARED INHIBITS FLIGHT CODE SLATS. NO FURTHER FAULTS NOTED.SDR IPXA09M54861Proximity Sensor · malfunctionedCREW DECLARED EMERGENCY DUE TO SLAT DISAGREE MESSAGE. ON APPROACH TO MSP BRAKING ACTION WAS CHANGED FROM GOOD TO POOR DUE TO SNOW AND THE CREW DECIDED TO DIVERT TO STL. LANDING WAS UNEVENTFUL. REF FIM 31-71-00-1, PSEU SHOWS LT SLAT NR 4A PROX SENSOR AT FAULSDR R61A20090006Sensor · brokenCREW REPORTED SLAT FAIL ON APPROACH TO MKE AND DIVERTED TO ORD. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. ORD MAINT CALLED TO AC, PERFORMED AC DOWNLOADS. MAINT FOUND LEFT O/B SLAT SKEW SENSOR 3/4 BROKE IN HALF. MAINT REPLACED SKEW SENSOR PER EMB AMM.
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