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 MZZA96170Actuator · leakingFLT 959 - GUM - LOST SYSTEM 'A' HYDRAULIC PRESSURE WHILE LOWERING FLAPS, NR 4 LE SLAT DID NOT DEPLOY. COMPLIED WITH EMERGENCY PROCEDURES AS PER FLIGHT MANUAL. REMOVED AND REPLACED NR 4 LE SLAT ACTUATOR. CHECKED BOTH ENGINE CASE DRAIN FILTER MAGNETIC PLUGS, SDR 96UAL900953Actuator · malfunctionedWHEN SPEED BRAKES ARE EXTENDED, WITH TRIM AT ZERO, THE AIRCRAFT ROLLS TO THE RIGHT. *S/D* THE INBOARD LT FLIGHT SPOILER (A5) WAS NOT DEPLOYING FULLY BECAUSE OF A FAULTY ACTUATOR. ASYMMETRIC SPOILER DEPLOYMENT DURING SPEED BRAKE EXTENSION CAUSED THE ROLL. NSDR DL72W962705Bracket · crackedFOUND ON B1 LETTER CK, .5 INCH CRACK AT NR 1 L/E FLAP ACTUATOR MOUNT BRACKET UPPER INBD CORNER. REPAIRED PER MM 57-20-21.SDR UPS96221745Slat Actuator · inoperativeINSPECTION TYPE-N/A, NR 2 SLAT WOULD NOT RETRACT AFTER T/O. COMPLETED AOM PROCEDURES, DUMPED FUEL AND RETURNED TO OAK. REPLACED NR 2 SLAT ACT AS PER MM 27-81-32, SLAT OPS CHKS NORMAL ON GROUND (P/N 141095-9-2) (S/N 3997L) OFF, (S/N 01405BDJLMN) ON.SDR EIAA9694Actuator · seizedJFK - DURING MAINTENANCE OPERATIONAL CHECKS OF THE LEADING EDGE DEVICES, NR 16 RIGHT WING LEADING EDGE FLAP LOCKED UP CAUSING EXTENSIVE DAMAGE TO LEADING EDGE FLAP. FOUND OUTBOARD ACTUATOR SEIZED, NEXT INBOARD ACTUATOR BINDING, NR 16 TORQUE TUBE SHEARED AND SSDR 9625603219Actuator · malfunctionedEXPERIENCED F/CTL SLATS FAULT' ACCOMPANIED BY SLATS LOCKED DURING HEAVY ICING. AIRCRAFT DID NOT SWITCH TO ALTERNATE LAW. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BOTH LEFT AND RIGHT WING NR 2 SLAT ACTUATOR TORQUE LIMITERS POPPED. REPLACED BOTH SSDR DL72E962598Bracket · crackedFOUND ON A1 LETTER CK, NR 1 L/E FLAP ACTUATOR I/B ATTACH BRACKET CRACKED. REPAIRED PER MM 57-20-21.SDR DHL96703005Actuator · failedNR 1 L/E WOULD NOT RETRACT WHEN FLAPS SELECTED FROM ZERO. REMOVED AND REPLACED L/E SLAT ACTUATOR OPS AND LEAK CHECK OK.SDR DL72S962589Bracket · crackedFOUND ON E1 LETTER CK, NR 2 INBD AND OUTBD SLAT ACTUATOR ATTACH BRACKETS CRACKED. REPAIRED PER MM 57-40-0.SDR 9624636302Drive Unit · failedDURING CLIMB, THE NR 3 LEADING EDGE FLAP DID NOT RETRACT ACCOMPANIED BY A LEADING EDGE FLAP STATUS MESSAGE. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE NR 3 LEADING EDGE FLAP DRIVE UNIT AND FOUR RELAYS, OPERATIONAL CHECK GOOD.SDR DL72W962520Angle · crackedFOUND THE NR 1 SLAT ACTUATOR INBD ATTACH ANGLE CRACKED. REPAIRED PER MM 57-20-21.SDR DL72S962529Support · crackedFOUND CRACK ON THE NR 1 SLAT ACTUATOR SUPPORT STRUCTURE. REPLACED CRACKED WEB IAW DAL ER/A 304444-14AD.SDR 96ZZZX6077Seal Plate · deterioratedSLAT ACTUATOR HAS BEEN IN REPAIR TWICE ON WARRANTY. BOTH TIMES SEAL PLATES WERE CAUSING UNIT TO LEAK.SDR 96ZZZX6076Seal Plate · deterioratedSLAT ACTUATOR HAS BEEN IN REPAIR TWICE ON WARRANTY. BOTH TIMES SEAL PLATES WERE CA USING UNIT TO LEAK.SDR DL72K962569Actuator Bracket · crackedO/B ACTUATOR ATTACH BRACKET CRACKED AT UPPER CORNER NR 1 L/E FLAP. INSTALLED REPAIR DOUBLER PER M/M 57-20-21.SDR CKSA96195Drive Unit · wornUHHH-FLT NR 80738: WHEN RETRACTING FLAPS, NR 1 LEADING EDGE FLAP, LEFT SIDE WOULD NOT RETRACT. NR 1 REMAINED INTRANSIT DURING EXTENSION ALSO. REPLACED NR 1 LEFT LEADING EDGE FLAP DRIVE UNIT. OPS CHECKS NORMAL ON GROUND PER MM 27-81-03.SDR DL72S962437Bracket · crackedFOUND ON F1 LETTER CK, NR 1 SLAT ACTUATOR ATTACH BRACKETS CRACKED INBD AND OUTBD SIDES. REPAIRED PER MM 57-20-21.SDR DHL9672039CMount · crackedAT C-CHECK, NR 2 LEADING EDGE FLAP ACTUATOR MOUNT O/B SIDE BOTH CORNERS CRACKED. REPLACED BRACKET PER SRM 51-10-1 AND 51-30-2, REPAIR 6 BY 8 .SDR CALA9601686Actuator Mount · crackedINSPECTION FOUND A .5 INCH CRACK IN NR 2 KREUGER FLAP ACTUATOR MOUNT. THE CRACK WAS LOCATED BELOW AND FORWARD OF INBOARD AND OUTBOARD LOWER MOUNT BOLTS. THE CRACK WAS STOP DRILLED, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-10-1 AND 51-40-3.SDR 96ZZZX5797Pdu Motor · crackedA-HYD RESERVOIR QTY LOW AND LOW QTY LIGHT ON. TURNED OFF HYD PUMP - LEAK STOPPED. AIRCRAFT LANDED NORMAL. FOUND SLAT A-SYS PDU HYD MOTOR HOUSING CRACKED. REMOVED AND REPLACED MOTOR IAW MM 27-80-10. AIRCRAFT RETURNED TO SERVICE.SDR DHL9672029CAngle · crackedAT C-CHECK, NR 8 SLAT ACTUATOR TRUNNION, OUTBD VERTICAL SUPPORT ANGLE IS CRACKED JUST UNDER LOWER ATTACH BOLT TO TRUNNION. REMOVED AND REPLACED OUTBD VERTICAL SUPPORT ANGLE AT NR 8 SLAT ACTUATOR TRUNNION PER SRM 51-10-1, 9 BY 4.5.SDR DHL9672030CBracket · crackedAT C-CHECK, NR 1 SLAT ACTUATOR I/B MOUNT CRACKED. REMOVED AND REPLACED INBOARD MOUNT BRACKET PER SRM 51-10-1 AND 51-30-3, REPAIR 7.5 BY 5.SDR SWAA961074Actuator · failedRETURNED TO PHX DUE TO NR 5 L/E SLAT NOT FULLY RETRACTING. INSPECTED, REPLACED NR 5 SLAT ACTUATOR AND OP CHECKED PER BOEING M/M.SDR CALA9601385Actuator · inoperativeTHE NR 2 LEADING EDGE SLAT DID NOT RETRACT AFTER TAKEOFF. THE LEADING EDGE TRANSIT LIGHT WAS ON AFTER FLAP RETRACTION AND A VISUAL CHECK CONFIRMED THE NR 2 SLAT WAS STILL EXTENDED. A RECYCLE WAS PERFORMED, BUT THE SLAT REMAINED EXTENDED. THE AIRCRAFT WAS RESDR UPS96221316Act Bracket · crackedINSPECTION TYPE-C, RT WING L/E NR 5 K-FLAP ACTUATOR I/B SUPPORT BRACKET IS CRACKED UNDER MOUNT LUG. FABRICATED AND INSTALLED NEW BRACKET PER SRM 51-10-1, BOEING DRAWING 65-16269, SRM 51-30-2.SDR 96FDEA01534Act Mount · crackedNR 0219 AND 006. NR 3 SLAT ACTUATOR ROD END MOUNT I/B AND O/B RIBS ARE CRACKED. ***S/D***** REMOVED AND REPLACED NR 3 SLAT ACTUATOR ROD AND MOUNT I/B AND O/B RIBS ON SLAT.SDR UPS96221321Attach Rib · crackedINSPECTION TYPE-C, RT WING NR 7 SLAT ACTUATOR ROD END ATTACH O/B RIB IS CRACKED. REMOVED FASTENERS, STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE PER SRM 57-50-2, 51-40-3.SDR UPS96221319Act Bracket · crackedINSPECTION TYPE-C RT WING NR 6 K-FLAP ACTUATOR I/B SUPPORT BRACKET IS CRACKED AT LOWER MOUNT LUG. FABRICATED AND INSTALLED NEW BRACKET PER SRM 51-10-1, 51-30-1, BOEING DRAWING 65-16275.SDR UPS96221318Act Bracket · crackedINSPECTION TYPE-C, RT WING NR 6 K-FLAP ACTUATOR O/B SUPPORT BRACKET IS CRACKED AT LOWER MOUNT LUG. FABRICATED REPLACEMENT BRACKET AND INSTALLED PER SRM 51-10-1, 51-30- 1, BOEING DRAWING 65-16275.SDR DL72S962140Bracket · crackedFOUND DURING A-1 LETTER CHECK, NR 2 L/E FLAP ACTUATOR MOUNT BRACKET CRACKED AT LWR I/B RADIUS. REPAIRED PER M/M 57-20-21 PAR 12.SDR CA960923016Seal · worn(CAN) DURING WALKAROUND OBSERVED SEAPAGE AT #6 LEADING EDGE SLAT, BEYOND LIMITS ACTUATOR REPLACEDSDR 96ZZZX5078Body Assy · chrome flakeACTUATOR CHROME FLAKING FROM INSIDE MAIN CYLINDER BORE/POOR ADHESION UPON RECHROME.SDR EISA96249Angle · crackedNR 2 LE FLAP ACTUATOR MOUNT, INBOARD UPPER ANGLE CRACKED. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-10-0 AND 51-12-1. (M)SDR 96UAL900694Actuator · failedWHEN EXTENDING FLAPS TO 15, NR 2 SLAT DID NOT EXTEND. REPLACED NR 2 SLAT ACTUATOR. OPERATIONAL CHECK WAS NORMAL.SDR 96FDEA01474Connector · dirtyON FLAP RETRACTION FROM 2 DEGREES TO 0 DEGREES THE AMBER LEADING EDGE FLAP LIGHT REMAINED ON. SECOND OFFICER'S AUXILIARY PANEL POSITION INDICATOR SHOWED THAT THE NR 7 LEADING EDGE DEVICE WAS INTRANSIT. COMPLETED CHECKLIST FOR LEADING EDGE DEVICE FAILURE ON FSDR 9619892709Actuator · failedDURING TAKEOFF ON FLAP RETRACTION, THE NR 3 LEADING EDGE SLAT INDICATED DOWN. AIRCRAFT RETURNED TO MKE AND LANDED WITHOUT INCIDENT. REPLACED NR 3 LEADING EDGE FLAT ACTUATOR AND SLAT EXTEND SWITCH, OPERATIONAL CHECK OK.SDR DHL9672253CMount · crackedAT C-CHECK, NR 7 SLAT ACTUATOR O/B MOUNT REPAIR PLATE CRACKED. REMOVED AND REPLACED SUPPORT ANGLE PER S/B 57-130 AND REPLACED ATTACH DOUBLER PER S/B 57-0130.SDR DHL9670818CAngle · crackedAT C-CHECK, NR 7 SLAT ACTUATOR, INBD TRUNNION VERT ANGLE AT FWD SPAR, STAINLESS DOUBLER HAS CRACK BEYOND STOP DRILL. FABRICATED ANGLE 1 INCH BY 35 INCHES PER S/B 57-0130, FABRICATED DOUBLER PER S/B, 8 INCHES BY 3.5 INCHES AND INSTALLED PER SRM 51-30-2 AND S/SDR DHL9670827CMount · crackedAT C-CHECK, NR 2 LEADING EDGE FLAP ACTUATOR MOUNT CRACKED ON INBD SIDE TOP AND BOTTOM. REMOVED AND REPLACED ACTUATOR MOUNT PER SRM 51-10-1.SDR MZZA96069Actuator · crackedFLT NR 916 - SPN - MAINTENANCE FOUND NR 3 LEADING EDGE SLAT LEAKING HYDRAULIC FLUID ON GROUND. MAINTENANCE REMOVED AND REPLACED NR 3 SLAT ACTUATOR DUE TO CRACK IN THE ACTUATOR HOUSING SYSTEM LEAK CHECK AND OPERATION CHECK GOOD, MM REFERENCE 27-81-22. (M)SDR UPS96221038Actuator Rib · crackedINSPECTION TYPE-C, LT NR 2 SLAT ACTUATOR RIB MOUNT ON O/B SIDE IS CRACKED. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE PER SRM 57-50-2, 51-40-3, 51-30-1, 51-30-2, 51-10-1, 51-10-2.SDR 96ZZZX4710Fitting · corrodedDURING SB INSPECTION OF NR 1 AND NR 5 LEADING EDGE SLAT ACTUATOR SUPPORT FITTINGS, FITTINGS WERE REMOVED TO REPLACE ATTACH HARDWARE. CORROSION WAS FOUND AT BOTH POSITIONS SEVERE ENOUGH TO REQUIRE REPAIR. SUBSEQUENT INSPECTION UNDER REMAINING FITTINGS REVEALESDR CALA9601181Actuator · leakingTHE NR 7 LEADING EDGE SLAT WOULD NOT RETRACT AFTER TAKEOFF. THE FLAPS WERE CYCLED AND THE LEADING EDGE DEVICE RETRACTION FAILURE CHECKLIST WAS COMPLIED, BUT THE NR 7 SLAT WOULD NOT RETRACT. SOME LOSS OF THE A-SYSTEM HYDRAULIC QUANTITY WAS ALSO OBSERVED. THESDR IXKA9600068Actuator Switch · stuckEWR/BDA - FLT 2 - AFTER TAKEOFF DURING FLAP RETRACTION, THE L/E FLAPS LIGHT ON FORWARD PANEL REMAINED ON (AMBER). AS FLAP RETRACTED TO ZERO DEGREES ON SECOND OFFICER'S SLAT POSITION INDICATOR, NR 8 WAS ILLUMINATED AMBER. A/C RETURNED TO EWR. REMOVED AND REPSDR USAASB96154Actuator · internal leakageROA - FLT 2520 - THE NR 5 LEADING EDGE SLAT FAILED TO RETRACT AFTER TAKEOFF. FLIGHT RETURNED TO FIELD AT ROA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NR 5 LEADING EDGE SLAT ACTUATOR TO HAVE INTERNAL LEAKAGE. REPLACED ACTUATOR PER MM 27-81-SDR SWAA960735Actuator · malfunctionedON CLIMBOUT, NR 3 SLAT WOULD NOT FULLY RETRACT. AIRCRAFT RETURNED TO MAF AND MADE AN UNEVENTFUL LANDING. INSPECTED AND LUBED SLAT TRACKS, OPERATION CHECKED SLATS. MX FERRIED TO DAL. REMOVED AND REPLACED NR 3 SLAT ACTUATOR AND OP CHECKED PER BOEING M/M.SDR AALA961175Act Bracket · corrodedTUL - FOUND CORROSION VERTICAL BRACKET 11B NR 5 LSAT ACTUATOR BY NR 3 FUEL VALVE. REMOVED AND REPLACED BRACKET WITH NEW SERVICABLE BRACKET. (M)SDR 96UAL900585Actuator · brokenTHE LEADING EDGE FLAPS TRANSIT LIGHT IS ON AND THE NR 6 SLAT LIGHT IS ON STEADY. REPLACED SLAT ACTUATOR. SHOP FOUND THE ACTUATOR ROD END BROKEN. SENT ROD END TO BOEING FOR EVALUATION.SDR UPS96220741Support Channel · crackedINSPECTION TYPE-C, NR 3 SLAT ACTUATOR SUPPORT CHANNEL BETWEEN I/B AND O/B ACTUATOR. REMOVED, FABRICATED AND INSTALLED CHANNEL PER DWG 65-17294 AND SRM 51-30-2.SDR UPS96220740Actuator Ribs · crackedINSPECTION TYPE-C, NR 3 SLAT INBD AND OTBD ACTUATOR ATTACH RIBS ARE CRACKED. REMOVED, FABRICATED AND INSTALLED RIBS PER SRM 57-50-2, 51-30-2 AND BOEING DWG 65-17240.
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