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 SWAA2012081406685Sensor · corrodedDECLARED EMERGENCY -- FLAP INDICATION UP (WITH SPLIT) FLAPS DID NOT EXTEND FOR APPROACH OR LANDING. REMOVED AND REPLACED NR 3 SENSOR AND NR 2, 3, 4, 5, 6, 7 AND 8 SKEW SENSOR CONNECTORS PER MM.SDR VNAA2012080400001Warning System · false activationCREW REPORTED FLAPS FAIL CAS MESSAGE WHEN SELECTING FLAPS 20 DEGREES. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM AND PERFORMED CHECKS OF FLAP CONTROL LEVER USING AIRCRAFT FIM. NO DEFECTS NOTED. AIRCRAFT RELEASED FOR SERVICE.SDR R61A201207300387Warning System · false activationCREW DECLARED AN EMERGENCY FOR A FLAL FAIL MESSAGE DURING CRUISE. MX RESET PER FIM 27-51-00-810-805-A AND CLEARED INHIBITS, MSG CLEARED AND FLAPS OPS CHECKED GOOD SEVERAL TIMES.SDR CA120718002Sensor · malfunctioned(CAN) INBOUND FLIGHT EXPERIENCED A FLAP FAIL EICAS. QRH WAS FOLLOWED AND A PAN WAS DECLARED AS A PRECAUTION. THE FLIGHT LANDED WITHOUT FURTHER EVENT. SFACE 1 & 2 PUT TO THIER ORIGINAL POSITION. SFACE 2 REPLACED AND CHECKED SERV IAW AMM 27-53-02. FLAP SKEW SESDR VNAA2012071500010Bpsu · failedCREW REPORTED FLAPS FAIL CAUTION MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED LEFT BPSU (BRAKE AND POSITION SENSOR UNIT) AND PERFORMED CHECKS USING FIM. AIRCRAFT RELEASED FOSDR CA120716011Sensor · failed(CAN) DURING APPROACH, THE ACFT EXPERIENCED A FLAP FAILURE WHEN THE FLAPS WERE SELECTED TO 8 DEGREES. AS A RESULT, A FLAPLESS LANDING WAS ACCOMPLISHED. UPON ARRIVAL INTO NEXT STATION, A WIRING CHECK AND CONTINUITY/INSULATION CHECK WERE ACCOMPLISHED. HOWEVER,SDR ERAA20120051Switch · out of adjustANC - FLAPS STUCK AT TAKEOFF. ANC- INFLIGHT GEAR HANDLE LIGHT DOES NOT COME ON. WARNING HORN SOUNDS. ADJUSTED RIGHT FLAP SWITCH IAW B-1900 MM 27-50-06. OPS CHECKED GOOD. OPS CHECKED GEAR WARNING SYSTEM AFTER ADJUSTING SPLIT FLAP SWITCH IAW B-1900MM 32-60-SDR CA120712003Indication Sys · malfunctioned(CAN) ON APPROACH HAD TO DO A GO AROUND DUE FLAP INDICATION PROBLEM, NO ISSUES ON SECOND APPROACH, ALL SYSTEMS NORMAL. ON LANDING AFTER SELECTING FLAP 3 TO 5, EICAS MESSAGE GROUND PROXIMITY FAIL + TERRAIN INHIBIT AMBER FLAP + AMBER 3, AFTER GO AROUND AND FLAPSDR SWAA2012071605808Transmitter · malfunctionedDECLARED EMERGENCY -- ASSYMETRICAL FLAP LOCK OUT LEFT FLAP 1 RIGHT FLAP 2. REMOVED AND REPLACED LEFT FLAP POSITION TRANSMITTER PER MM.SDR DALA1240241811Transmitter · failedFIRST OFFICER MINIMUM SPEED (RED ZIPPER) EXTENDS FROM BOTTOM TO TOP OF SPEED TAPE DISPLAY. FIRST OFFICER PFD HAS CROWS FEET ILLUMINATED CONTINUOUSLY. INTERROGATED FSEU AND FOUND 0 VOLTS FROM RT FSPM. TRIED FSPM, NO HELP. REPLACED NR 5 FLAP POSITION TRANSMISDR YENA20120630547Proximity Sensor · out of adjustFLT 510 FLL-EWR, CREW DECLARED EMERGENCY DUE TO F/CTRL ECAM FLAPS LOCKED ALIGNMENT FAULT DURING APPROACH. FLAPS LOCKED JUST PRIOR TO THE FIRST SETTING AT APPROX 190 KIAS AS FLAPS 2 WERE SELECTED. FOUND FLAP RIGHT PROX SENSOR 38 CV MISADJUSTED. ADJUSTED PER SDR VNAA2012062900013Bpsu · failedCREW REPORTED FLAPS FAIL CAUTION MESSAGE WHILE CLIMBING THROUGH 11,000 FEET. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED LEFT BPSU (BRAKE AND POSITION SENSOR UNIT) AND PERFORMED CHECKS USING FIM. AIRCSDR VNAA2012062800012Bpsu · failedCREW RECEIVED FLAPS FAIL AMBER MESSAGE IN FLIGHT. CREW LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED LEFT BPSU (BRAKE AND POSITION SENSOR UNIT) AND PERFORMED CHECKS USING FIM. AIRCRAFT RELEASED FOR SERVICE.SDR VNAA2012062800011Warning System · false activationCREW RECEIVED FLAPS FAIL AMBER MESSAGE IN FLIGHT. CREW LANDED WITHOUT INCIDENT. SYSTEM RESET AND AIRCRAFT RELEASED FOR SERVICE USING AD PROCEDURE.SDR N6WA2012062702Detector · faultyFLAPS FAIL CAUTION MESSAGE IN FLIGHT. R & R SKEW DETECTOR IAW AMM 27-52-45. OPS CHECK GOOD.SDR UALA2012062203364Fseu · faultyFLAP - SLAT CONTROL NR 1 MSG WOULD NOT CLEAR. SEE HISTORY. REPLACED FSEU-1 AS PER MM 27-51-01, ACCOMPLISHED SYSTEM TEST OF BOTH PRIMARY AND SECONDARY SYSTEM.SDR AALA20120620019Indicator · trippedMIA (REPEAT ITEM) CREW REPORTED TRAILING EDGE FLAP DISAGREE MESSAGE AND THE TRAILING EDGE LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND RIGHT INBOARD FLAP OUTBOARD TRANSMISSION AND SDR VNAA2012061900004Bpsu · malfunctionedCREW REPORTED FLAPS FAIL CAS MESSAGE WHILE CLIMBING THROUGH FL220. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED RIGHT BPSU (BRAKE AND POSITION SENSOR UNIT) AND PERFORMED CHECKS USING AIRCRAFT MSDR AALA20120619025Transmitter · inoperativeMIA - CREW REPORTED TRAILING EDGE FLAP DISAGREE LIGHT ILLUMINATED. FLIGHT LANDED MIA WITHOUT INCIDENT. REPLACED FLAP PDU POSITION TRANSMITTER. SYSTEM GROUND CHECK NORMAL OPERATION.SDR CALA2012061900406Indicator · defectiveON LANDING CLE, FLAPS 5 SELECTED. FLAPS ONLY EXTENDED TO BETWEEN 1 AN 2, RAN QRH ALT EXTEND TO 15 OK. REMOVED AND REPLACED FLAP INDICATOR REF TASK 27-58-41 PG BLOCK 401. RESAFTIED ALT FLAPS SWITCH OPS CHECK GOOD FILED SDR ROTABLE PARTS CHANGE WAS INDICATED SDR CA120625003Sensor · failed(CAN) WHILE IN CRUISE FLIGHT AT FL390 THE FLAP FAIL CAUTION MESSAGE CAME ON. A FLAP ZERO LANDING WAS CARRIED OUT UNEVENTFULLY. ALTHOUGH THE FLIGHT CREW DID REQUEST EMER SERVICES ON STANDBY, NO EMER WAS DECLARED. INVESTIGATION FOUND THE LT INBD FLAP SKEW SENSDR USAA2012061400003Syncronizer · failedPHX - FLT 26 EN ROUTE OGG TO PHX. FLAPS FAILED TO MOVE, TRAILING EDGE LIGHT ON, AND EICAS MSG TRAILING EDGE DISAGREE DISPLAYED. FLAPS NORMAL ON ALTERNATE SYS. THE FLIGHT PERFORMED A GO-AROUND TO RUN THE CHECKLIST. ON THE SECOND APPROACH, THE FLIGHT LANDESDR USAA2012061100016Indicator · faultyON APPROACH, CREW REPORTED THE FLAP INDICATOR SHOWED A 1/2 NEEDLE SPLIT BETWEEN 10 & 15. CREW ACCOMPLISHED GO-AROUND. FLAPS WERE NOT MOVEABLE UNTIL AFTER LANDING. FLAPS RETRACTED AND WORKED NORMALLY AFTER LANDING. MAINTENANCE REMOVED AND REPLACED THE FLAP SDR AALA20120519017Sensor · failedIAD INFLIGHT MIA-DCA. CREW REPORTED FLAP ASYMMETRY MESSAGE. EMERGENCY DECLARED FLIGHT DIVERTED IAD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACE NUMBER 3 FLAP SKEW SENSOR. SYSTEM GROUND CHECK NORMAL OPERATION.SDR SIMA20120518003Sensor · inoperativeON FLIGHT 3525 THE CREW REPORTED THAT AFTER SELECTING FLAPS TO "9" ON APPROACH "FLAP FAIL" APPEARED ON EICAS- FLAPS NEVER EXTENDED. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LSDR USAA2012051800008Proximity Sensor · faultyPILOT REPORTED F/CTL FLAPS LOCKED - ALIGNMENT FAULT ON APPROACH INTO PHX. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RIGHT FLAP INTERCONNECT STRUT PROXIMITY SWITCH 38CV IAW AIRBUS MAINTENANCE MANUAL 27-51-44-400-002-ASDR REXA2012051500737Detector · defectiveFLAP FAIL ON RETRACTION. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD2009-06-12 PARAGRAPH (H),(6),(1).AMOC DATED MARCH 27-2009,TR #27-012 D PER AMOC DATED DECEMBER 18,2009 AND PAAD27-052G, REMOVED AND REPLACED SKEW DETECTION UNIT IAW AMM 27-51-0SDR COMA2012051590009Detector · failedON DESCENT INTO BOS RECEIVED FLAPS FAILED CAUTION MSG, FAILED AT 6 DEG. QRH FOLLOWED. EMERGENCY DECLARED, A/C LANDED SAFELY IN BOS. REMOVED AND REPLACED RIGHT FLAP I/B SKEW DETECTOR. OPS CHECK GOOD.SDR AALA20120511010Sensor · inoperativeMIA - CREW REPORTED AFTER TAKEOFF FLAPS WOULD NOT RETRACT. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED INTERLOCK SENSOR. SYSTEM GROUND CHECK NORMAL OPERATION.SDR AALA20120504018Sensor · inoperativeLAX - CREW REPORTED UPON EXTENDING FLAPS, HAD NO INDICATION THAT FLAPS WERE MOVING AND NO WARNING. EMERGENCY DECLARED FLIGHT LANDED LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 3 FLAP SKEW SENSOR THAT WAS INOPERATIVE. SYSTEM GROUND SDR REXA2012042700573Detector · defectiveFLAPS FAIL AT 20 ON APPROACH. FLAPS PDU1 CB BREAKER POPPED WHEN FLAPS 30 SELECTED AT 165 KNOTS AT 2500 FEET. REMOVED AND REPLACED SKEW DETECTION UNIT POWER SUPPLY IAW AMM 27-51-00. NO FIX.SDR SWAA2012043003543Power Unit · faultyDECLARED EMERGENCY -- NO FLAP EXTENSION WHEN FLAP HANDLE MOVED TO FLAPS 5. FOLLOWING QRH WHEN ALT FLAP SWITCH WAS MOVED TO DOWN POS THE "ALT T/E FLAP DRIVE AC" CIRCUIT BREAKER POPPED. REMOVED AND REPLACED FLAP MOTOR HYD POWER UNIT PER MM.SDR UALA2012042302413Transmitter · erraticFLAPS DRIVE EICAS, RTFL. FOUND LEFT OUTBOARD FLAP POSITION TRANSMITTER GIVING ERRATIC READINGS. REPLACED LEFT O/B FLAP RVDT TRANSMITTER REF MM27-58-01-401. OPS NORMAL, NO CMC OR STATUS MESSAGES THRU OUT FULL FLAP MOVEMENT. ALL POSITION RVDT'S READINGS WITHSDR REXA2012042300565Transmitter · faultySPLIT FLAP CONDITION. SELECTED FLAPS 8: LT FLAP DEPLOYED TO 8 DEG, RT FLAP DEPLOYED TO 2 DEG. RT FLAP POSITION SENSOR RIG CHECKS GOOD. BEGINNING OF THE NIGHT THE RT FLAP WAS 6 DEGREES HIGHER ON EACH FLAP DETENT. BEFORE DEFERRING FLAP POSITION SENSOR IT WASSDR REXA2012041700523Detection Sys · malfunctionedFLAP FAIL DUE TO SKEW DET BOX NOT RESET. PLACARD INSTALLED. PERFORMED T/S OF SKEW DETECTION FLAP FAIL IAW FIM 27-50-00 AND AMM 27-51-15 NOTED SKEW DETECTION WOULD NO RESET. R/R SKEW DETECTION UNIT IAW AMM 27-51-15 PERFORMED SEVERAL OPS CHECK IAW AMM 27-51-15SDR VNAA2012041600009Bpsu · failedCREW REPORTED FLAPS FAIL AT ZERO DEGREES IN FLIGHT AT 12,000 FEET. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED LEFT BPSU (BRAKE AND POSITION SENSOR UNIT) AND PERFORMED CHECKS USING AIRCRAFT FIM MANUAL. AIRSDR CALA2012041100254Transmitter · out of adjustFLAPS STUCK BELOW FLAPS 1. WOULD NOT MOVE USING ALTERNATE METHOD WITH QRH. TROUBLESHOT PER FIM 27-57-00-810-801, 27-51-00-810-823. R & R PSEU PER 27-51-01, ALSO REMOVED AND REPLACED RT ALP POSITION TRANSMITTER PER A MM 27-58-01. ADJUSTED AND TESTED PER AMMSDR CALA2012040600240Transmitter · inoperativeDURING TROUBLESHOOTING OF FLAPS LOCKOUT REF LG PG 7699577. FOUND LT FLAP POSITION TRANSMITTER OUT OF ADJUSTMENT IAW MM 27-58-01-820-801. ADJUSTED LT FLAP POSITION TRANSMITTER IAW MM 27-58-10-820-801. SYS GROUND CHECKED GOOD.SDR CA120409007Indicator · intermittent(CAN) RT STALL WARNING CAUTION LIGHT WOULD ILLUMINATE INTERMITTENTLY. TROUBLESHOT SYS TO FIND FAULTY FLAP POSITION INDICATOR GIVING INTERMITTENT OUTPUT TO BOTH LT AND RT CIRCUITS CAUSING FDR AND RT STALL WARN CAUTION LIGHTS TO ILLUMINATE INTERMITTENTLY. REPLASDR UALA2012033001997Indicator · faultedFLAP NEEDLE SPLIT WHEN FLAPS DROPPED FROM 5 THRU 25, NEEDLES ALIGNED AT 25, SPLIT AT 30. CYCLED FLAPS AND DUPLICATED SPLIT AGAIN WHEN FLAPS DROPPED THRU EACH POSITION. FLAPS DRIVE SMOOTH HYDRAULICALLY, SUSPECT FLAP POSITION INDICATOR SYSTEM. REPLACED MODULESDR CALA2012032200210Limit Switch · defectiveYAW DAMPER FAILED ON TAXI OUT, RAN QRH FOR RESET. YAW DAMPER FAILED AGAIN ON CLIMBOUT AS WELL AS DESCENT AND TAXI IN. REPEAT WRITE UP SEE LOG PAGE 7056503. REPLACED FLAP LIMIT SWITCH. PERFORMED SWITCH ADJUSTMENT AND FUNCTIONAL TEST PER AMM 27-51-63. NO DESDR USAA2012032000012Indicator · faultyON APPROACH TO CLT, FLAPS AT 5 - GREEN LIGHT. SELECTED FLAPS 15 - FLAPS DID NOT GO PAST 5, HAD TO CYCLE FLAPS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED FLAP INDICATOR PER AMM 27-58-41. SERVICED FLAP POWER UNIT GEARBOX PER AMSDR USAA2012032000011Indicator · stuckON APPROACH TO PHL, AS FLAP HANDLE WAS EXTENDED TO FLAPS 30, FLAP INDICATOR NEVER MOVED PAST FLAPS 5 INDICATED WITH GREEN LIGHT. RECYCLED FLAPS, NORMAL INDICATIONS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE OPERATED FLAPS TO 40 SEVERAL TIMES. NO SDR SWAA2012031902417Transmitter · failedDECLARED EMERGENCY - FLAPS FAILED TO EXTEND WITH FLAP HANDLE A POSITION. REMOVED AND REPLACED LT NR 1 FLAP POSITION TRANSMITTER ASSY AND CONNECTOR ASSY PER AMM.SDR KPVA201203Indicator · faultyFLAPS STUCK AT 5 DEGREES DURING TAKEOFF. DECLARED EMERGENCY. RETURNED TO HNL. REMOVED AND REPLACED FLAP POSITION INDICATOR. GROUND OPERATION CHECKED GOOD.SDR SWAA2012030601973Sensor · faultyDECLARED EMERGENCY - FLAPS WOULD NOT EXTEND USING NORMAL PROCEDURES. EXTENDED FLAPS USING ALT METHOD TO POS 15 AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 6 AND NR 8 FLAP SKEW DETECTION SENSORS PER M/M.SDR UALA2012030201295Transmitter · faultyT/E FLAP ASYM FSEU NR 1 SHOW LEFT FLAP TRANSMITTER WIRING FAULT. RPLC'D FLAP POSITION TRANSMITTER PER MM. TESTED TRANSMITTER PER MM. NO DISCREPANCIES NOTED. SECURED CANNON PLUG ON FLAP TRANSMITTER.SDR UIEA2012030100074Transmitter · malfunctionedT/E FLAPS DISAGREE EICAS MESSAGE RETRACTING FLAPS FROM 1 DEG TO UP. RAN ABNORMAL CHECK LIST EICAS/LIGHT EXTING. T/E DISAGREE EICAS CAME ON SECOND TIME. R & R FSEU FOR TROUBLESHOOTING IAW AMM 27-51-00 ADJUSTED TRANSMITTER M473, M492, M489, IAW AMM 27-51-45. SDR AALA20120228001Transmitter · inoperativeDEN - INFLIGHT JFK-EGE. CREW REPORTED FLAP SPLIT INDICATION. EMERGENCY DECLARED FLIGHT DIVERTED DEN LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT AND RIGHT TRAILING EDGE FLAP POSITION TRANSMITTERS. SYSTEM GROUND CHECK NORMAL OPERATSDR CA120227010Indicator · inoperative(CAN) AN ACFT ON APPROACH DECLARED AN EMERGENCY LANDING WHEN THE FLIGHT CREW EXPERIENCED A FLAP ASYMMETRY CONDITION WHICH LOCKED THE FLAPS BETWEEN 25 AND 30 UNITS. THE ACFT MADE AN UNEVENTFUL LANDING AND WAS THEN MET BY MAINTENANCE. MAINTENANCE CARRIED OUT FIM
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