JASC 2782
Service difficulty reports · 1,225
Reports filed under 2782 · Leading Edge Slat Actuator, 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 = '2782' 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 = '2782' 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 0104905520Actuator · failedDURING APPROACH, UPON SELECTION OF FLAPS 1, THE LEADING EDGE SLAT DISAGREE WARNING LIGHT ILLUMINATED. AN EMERGENCY WAS DECLARED, THE FLIGHT CONTINUED THE APPROACH, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 20 LEADING EDGE ACTUATOR. SUBSEQUENTSDR RRX2001F00000Actuator · leakingLOST (A) SYSTEM HYDRAULIC PRESSURE DURING CLIMB OUT FROM MSY. ACCOMPLISHED EMERGENCY CHECKLIST RELATING TO LOSS OF (A) SYSTEM HYDRAULICS. EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED NR 3 SLAT ACTUATOR ASSEMBLY AND OPERATIONAL CHECK SYSTSDR 01FDEA00974Actuator · failedON DEPARTURE RETRACTING FLAPS ON RIGHT WOULD NOT RETRACT. REMOVED AND REPLACED NR 6 KRUEGER FLAP ACTUATOR PER MM 27-81-022-4.SDR IU62001F00012Actuator · flakingCHROME PLATING IS FLAKING OFF INSIDE THE BORE.SDR SWAA012914Actuator · failed(AIR TURNBACK ) AFTER TAKEOFF L/E FLAP TRANSIT LIGHT ILLUMINATED AFTER FLAP RETRACTION. RIGHT OUTBOARD SLAT CONFIRMED PARTIALLY EXTENDED. REMOVED AND REPLACED NR 6 L/E SLAT ACTUATOR PER MM.SDR DL72S011655Actuator · malfunctionedUPON FLAP RETRACTION FROM 2 TO 0, NR 7 L/E SLAT STAYED FULLY EXTENDED WITH FLAPS UP. VERIFIED AT S/O PANEL. APPROX 45 SECS LATER, NR 7 L/E SLAT RETRACTED ON ITS OWN. NO HYD PRESSURE OR QUANTITY FLUCTUATIONS NOTED. AIRCRAFT DID HAVE A ROLLING TENDENCY (ATLMSDR SWAA012764Actuator · failedAIR TURNBACK, NR 6 L/E SLAT WOULD NOT RETRACT, ALL FLAPS AND SLATS EXTENDED. REMOVED AND REPLACED NR 6 L/E SLAT ACTUATOR ASSY PER MM.SDR DHL2001742545Attach Fitting · crackedAT C-CHECK, LT WING L/E NR 4 SLAT ACTUATOR FRONT SPAR ATTACH I/B FITTING CRACKED 2 PLACES. REMOVED AND INSTALLED NEW I/B FITTING AT LT WING NR 4 SLAT ACTUATOR SUPPORT.SDR AWXA200100450Actuator · failedPHX - AIR TURNBACK - FLT 416 - "C" - DURING CLIMB OUT OF PHX ENROUTE TO COS, WHEN THE FLAPS WERE RETRACTED THE NR 2 L/E SLAT TRANSIT LIGHT STAYED ILLUMINATED. PERFORMED THE QRH PROCEDURES AND LIGHTS REMAINED ON, VISUALLY CONFIRMED THE NR 2 SLAT NOT COMPLETELY SDR 01FDEA00835Actuator · failedLEADING EDGE FLAP LIGHT CAME ON AT 10L FT WITH FLAPS UP. REMOVED AND REPLACED NR 2 & 6 SLAT ACTUATORS PER MM 27-81-032-4.SDR GAIA01305OPActuator · failedFLT - 1843 - PHL-FWA - ON APPROACH TO FWA, THE FLIGHT CREW NOTICED THAT THE NR 8 SLAT DID NOT INDICATE EXTENDED WHEN THE FLAP HANDLE WAS MOVED FROM 2 DEGREES TO THE 5 DEGREE POSITION. AN EMERGENCY WAS DECLARED AND A UNEVENTFUL LANDING WAS MADE AT FWA. REMOVESDR AWXA0002209Actuator · failedLAX - AIR TURNBACK - FLT 115 - DURING DEPARTURE CLIMB THE NR 6 LEADING EDGE SLAT WAS EXTENDED WITH FLAPS SELECTED UP. THE AIRCRAFT ENCOUNTERED A ROLL TO THE LEFT, MAX SPEED WAS 250 KTS. THE AIRCRAFT RETURNED TO LAX AND MADE AN UNEVENTFUL LANDING. IN LAX MAISDR SWAA012416Actuator · failed(AIR TURNBACK) NR 4 L/E SLAT WOULD NOT RETRACT. REMOVED AND REPLACED NR 4 SLAT ACTUATOR PER MM.SDR SWAA012382Actuator · failed(AIR TURNBACK) AFTER TAKEOFF, L/E TRANSIT LIGHT STAYED ILLUMINATED. REMOVED AND REPLACED NR 4 & 7 L/E SLAT ACTUATORS PER MM.SDR SWAA012364Actuator · failedAIR TURNBACK, AFTER TAKEOFF L/E EDGE TRANSIT LIGHT STAYED ILLUMINATED. REMOVED AND REPLACED NR 2 L/E SLAT ACTUATOR PER MM.SDR AUS20010911Pdu · faulty(AUS) NR 3 LT LEADING EDGE FLAP PNEUMATIC DRIVE UNIT FAULTY.SDR SWAA012351Actuator · failedAIR TURNBACK, AFTER TAKEOFF THE RT INBOARD L/E FLAP WOULD NOT RETRACT. REMOVED AND REPLACED NR 3 KRUEGER FLAP ACTUATOR PER MM.SDR DHL2001727536Mount · crackedLT WING NR 3 SLAT ACTUATOR FWD MOUNT INSP HOLE HAS 2 CRACKS AT I/B SIDE OF ACCESS PANEL. STOP DRILLED CRACKS PER SRM 51-10-1. INSTALLED DOUBLER REPAIR PER SRM 51-30-2.SDR DL72S011307Actuator · leakingON FINAL APPROACH PRIOR TO GEAR EXT WITH FLAPS 5 DEG AND HAD INDICATION OF A LOSS OF A SYSTEM HYD. REPLACED A SYSTEM FILTERS. REPLACED LEADING EDGE FLAP ACTUATOR FOR LEAKINGSDR SWAA012218Actuator · failedAIR TURNBACK, RT WING L/E FLAP TRANSIT AND NR 3 L/E DEVICE LIGHTS ILLUMINATED. REMOVED AND REPLACED NR 3 L/E FLAP ACTUATOR PER MM.SDR SWAA012217Actuator · failedAIR TURNBACK, RT WING L/E FLAP TRANSIT LIGHT ILLUMINATED. REMOVED AND REPLACED NR 3 L/E FLAP ACTUATOR PER MM.SDR XNA01015Jackscrew · lack of lubeDURING TAXI, NO SLATS INDICATION ON THE FCPI. SERVICED SLAT JACKSCREW AT LEFT WING ROOT. OPS CHECK GOOD IAW A300 MM 27-80.SDR 01FDEA00577Fitting · crackedDURING ROUTINE INSP FOUND SUPPORT FITTING NR 2 KRUEGER FLAP ACTUATOR SUPPORT FITTING AT FRONT SPAR CRACKED. *S/D* REMOVED AND REPLACED PER IAW SRM 57-20-1.SDR ABXA010401Rod End · brokenRIGHT WING LEADING EDGE SLAT ACTUATOR ROD END BROKEN. REPLACED THE RIGHT WING LOWER SLAT ACTUATOR ROD END IAW DC-9 MM 27-80-05-2-10. OPS CHECKED GOOD.SDR 2001UALA01354Slat · malfunctionedNR 1 SLAT WOULD NOT RETRACT FROM FLAPS 1 TO FLAPS 0.SDR DL72S011144Actuator · leakingHYD A SYST QUANTITY AND PRESSURE LOSS WELL AFTER GEAR AND FLAP RETRACTION. COMPLETED POM. FOUND NR 6 KRUEGER FLAP ACTUATOR LEAKING, REPLACED SAME. REMOVED AND REPLACED BOTH A SYS HYD PUMP CASE DRAIN FILTERS, NO CONTAMINATION FOUND. SERVICED HYD SYS, LEAK CSDR 01FDEA00527Actuator · failedWHEN RETRACT FLAPS FROM 2 DEG TO 0 NR 7 LED FAILED TO RETRACT. REMOVED AND REPLACED RIGHT WING NR 7 SLAT ACTUATOR PER MM 27-81-032-4. OPS AND LEAK CK GOOD.SDR DL72S011139Actuator · defectiveON FLAP RETRACTION AFTER T/O AMBER L/E FLAP LIGHT ON FWD PANEL REMAINED ILLUMINATED. NR 1 SLAT LIGHT ON S/O PANEL REMAINED ILLUMINATED. FLAPS 5 AND LOWER SHOWED NORMAL IND. REPLACED NR 1 SLAT ACTUATOR. FLAP/SLAT INDICATION OPS, CHECKS OK.SDR F3LA200100091Actuator · leakingAIR TURN BACK. FLIGHT CREW REPORTED "B" SYSTEM ENGINE DRIVEN HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED AND LOSS OF "B" SYSTEM HYDRAULIC FLUID. MAINTENANCE REPLACED NO. 2 ENGINE DRIVEN HYDRAULIC PUMP AND NO. 5 LEADING EDGE SLAT ACTUATOR.SDR 2001UALA01025Actuator · failedNR 6 SLAT WILL NOT RETRACT. *S/D* REPLACED NR 6 SLAT ACTUATOR.SDR 2001UALA00883Actuator · leakingRETURNED TO IAH DUE TO LOSS OF 'A' SYSTEM HYDRAULICS, FOUND NR 2 LEADING EDGE FLAP ACTUATOR LEAKING. REPLACED NR 2 FLAP ACTUATOR PER 727 MM, REPLACED NR 1, AND NR 3 ENGINE DRIVEN HYDRAULIC PUMPS PER 727 MM.SDR AWXA0001727Actuator · failedPHX - AIR TURNBACK, AFTER TAKEOFF THE FLAPS WERE RETRACTED BUT L/E FLAPS TRANSIT LIGHT ON FORWARD PANEL AND NR 1 SLAT INDICATOR ON THE OVERHEAD PANEL REMAINED ILLUMINATED. FLAPS WERE CYCLED BACK TO 1 & THEN UP SEVERAL TIMES. PILOT VISUALLY CONFIRMED THAT NR SDR AWXA0001718Rod End · damagedPHX - AIR TURNBACK, AT ROTATION THE LEADING EDGE INTRANSIT LIGHT ILLUMINATED AND THEN EXTINGUISHED AS THE CLIMB WAS INITIATED AND ALL SLATS WERE IN EXTENDED POSITION. WHEN FLAPS WERE RETRACTED A LOUD SOUND WAS HEARD AND THE NR 1 SLAT WAS AT FULL EXTEND WITH OSDR 2001UALA00658Actuator · failedLEADING EDGE LIGHT ON AND EICAS L/E SLAT DISAGREE MESSAGE. *S/D* LEADING EDGE SLAT ROTARY ACTUATOR NR 2 FAILED, WHICH CAUSED THE SLAT SYSTEM TO LOCKOUT AND ILLUMINATE THE DISAGREE LIGHT AND MESSAGE. REPLACED ACTUATOR NR 2, 3 AND 10 DUE TO OVERLOAD INDICATORSDR GAIA01161STAttach Fitting · crackedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE NR 4 SLAT ACTUATOR ATTACH FITTING PREVIOUS REPAIR IS CRACKED, INSIDE SLAT. ACCOMPLISHED NR 4 SLAT ACTUATOR RIB REPAIR IAW B727 SRM 57-50-3 FIG 9. (M)SDR 2001UALA00655Actuator · leakingDURING TAXI LOST HYDRAULIC SYSTEM-A. *S/D* LT NR 3 SLAT ACTUATOR WAS LEAKING. REMOVED AND REPLACED LT NR 3 SLAT ACTUATOR IN ACCORDANCE WITH MAINTENANCE MANUAL. OPERATIONAL CHECKS NORMAL.SDR 20010605CW005Sleeve · crackedSLEEVE (145) IS CRACKED. PROBABLE CAUSE: FATIGUE.SDR 20010605CW004Sleeve · crackedSLEEVE (145) IS CRACKED. PROBABLE CAUSE: FATIGUE.SDR 20010605CW003Sleeve · crackedSLEEVE (31) IS CRACKED. PROBABLE CAUSE: FATIGUE.SDR CA010510006Sleeve · worn(CAN) SLATS WOULD NOT EXTEND DUE TO HIGH TORQUE REQUIRED TO ACTIVATE THE BALL SCREW.PROBABLY CAUSED BY POOR LUBRICATION LEADING TO WORN SLEEVE.SDR CA010706003Actuator · worn(CAN) DURING TAKEOFF LEADING EDGE SLAT TRANSIT LIGHT CAME ILLUMINATED ON FLAP/SLAT INDICTOR WHEN A/C REACHED 80 KTS, REJECTED TAKEOFF OCCURRED. AFTER INVESTIGATION BY MAINTENANCE, NR 1 SLAT ACTUATOR FOUND WITH EXCESSIVE RADIAL PLAY AT JACKSCREW. ACTUATOR REPLASDR ABXA010209Rod End · brokenDURING A SERVICE CHECK, MAINTENANCE FOUND THE UPPER LEFT OUTBOARD SLAT ACTUATOR ROD END TO BE BROKEN. DAMAGE WAS ALSO NOTED UNDER THE LEFT INBOARD SLAT AND UPPER WING PANEL 1142A. MAINTENANCE REPLACED THE SLAT ACTUATOR ROD END ASSY IAW DC-9 MM 27-80-05. THESDR CA010507017Actuator · fractured(CAN) ON APPROACH TO WHEN FLAP 2 SELECTED THE CREW OBSERVED RAPID DECREASE IN A HYDRAULIC SYSTEM. HYDRAULIC LEAK/LOSS OK. LIST CARRIED OUT. MANUAL GEAR EXTENSION PERFORMED, AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS TOWED FROM THE RUNWAY TO THE HANGAR SDR SWAA011043Actuator · failedAIR TURNBACK, NR 4 L/E SLAT WOULD NOT RETRACT. VISUALLY VERIFIED SLAT NOT RETRACTED. R&R SLAT ACTUATOR PER MM. OPS & LEAK CHECK GOOD.SDR DL72E010484Actuator · jammedAFTER TAKEOFF NR 3 KRUEGER FLAP DID NOT RETRACT. REPLACED KRUEGER FLAP ACTUATOR AND SHUTTLE VALVE LEAK AND OPS CHECK OK PER OPN 7054.RIISDR AWXA0001532Actuator · failedIAH - EMERGENCY LANDING - 3/18/01 - EN ROUTE FROM PHX TO IAH PRIOR TO DESCENT THE L/E FLAP TRANSIT AMBER LIGHT CAME ON AND REMAINED ILLUMINATED; THE CREW LANDED IN IAH W/ FLAPS 15 PER THE QRH. MAINTENANCE FOUND THE SLAT CONTROL VALVE CABLE TENSIONS HIGH AND ASDR 2001UALA00256Actuator · failedLEADING EDGE FLAP EXTENSION PROBLEM. SUPPLEMENTAL DATA UPDATE REPLACED THE NR 3 LEADING EDGE FLAP ACTUATOR. OPS CHECKED NORMAL.SDR 20010417CW002Sleeve · crackedSLEEVE 145 IS CRACKED. FATIGUE IS PROBABLE CAUSE.SDR 20010417CW001Sleeve · crackedSLEEVE 145 IS CRACKED. FATIGUE AS PROBABLE CAUSE.SDR 20010417CW003Block · crackedSLEEVE 145 IS CRACKED AND APPEARS TO BE OCCURRING UNDER NORMAL USE.
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