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 98ZZZX4442Body Assy · crackedCRACKED AND FLAKING CHROME.SDR DL72S981931Angle · crackedFOUND ON A1 LETTER CK, NR 3 SLAT I/B ACTUATOR ATTACH ANGLE CRACKED. REPAIRED PER MM 57-54-0.SDR DHL98724002Actuator · failedWITH FLAP RETRACTED NR 7 SLAT LIGHT REMAINED ON BOTH ON THE FWD AND SECOND OFFICER PANEL. REPLACED NR 7 SLAT ACTUATOR AND SWITCH.SDR DL72W981904Actuator · failedAFTER T/O, LOST 'A' SYS HYD QTY AND PRESS IND ZERO. PROCEDURES COMPLIED WITH ALT FLAP SW USED GPWS INHIBITED. GEAR PIN INSTALLED BY MTC. REMOVED AND REPLACED NR 1 SLAT ACT. OPS AND LEAK CKS GOOD.SDR CALA9801704Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN BRACKET WHERE RT WING NR 6 LEADING EDGE FLAP ACTUATOR MOUNTS. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-40-3, 51-30-2, AND 51-10-2.SDR CALA9801578Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN SUPPORT BRACKET FOR LT WING NR 2 LEADING EDGE FLAP ACTUATOR. A NEW BRACKET WAS INSTALLED IAW SRM 51-30-2.SDR DL72L981890Stiffener · crackedA .625 INCH CRACK IN SPAR STIFFENER AT NR 5 SLAT ACTUATOR INBD ATTACH FITTING. REMOVED OLD STIFFENER. DRILLED UP STIFFENER PER M/M 57-20-21 PG 813.SDR DL72S981765Bracket · crackedNR 1 L/E FLAP ACTUATOR ATTACH BRACKET CRACKED O/B LOWER END. FOUND ON D1 LETTER CK. REPAIRED PER MM 57-20-21.SDR 98UAL900408Actuator · failedRETURNED TO ORD DUE TO A LEADING EDGE FLAP PROBLEM. *S/D* POSITION NUMBER 15 LEADING EDGE SLAT ACTUATOR WAS FOUND WITH AN INTERMITTENT PROBLEM CAUSING THE EICAS MESSAGE AND LOCKOUT OF THE LEADING EDGE SLATS. REPLACED NUMBER 15 LEADING EDGE SLAT ACTUATOR ANDSDR RAAA98B2040Actuator · failedDURING CLIMBOUT, LE FLAP STATUS DISAGREEMENT LIGHT ON AFTER FLAPS RETRACTED. RETURNED TO UUS AND LANDED WITHOUT INCIDENT. FOUND NR 5 LE FLAP WOULD NOT RETRACT. CHANGED NR 5 LE FLAP ACTUATOR AND SHUTTLE VALVE DUE ACTUATOR FAILED IN EXTENDED POSITION.SDR DL72S981671Support · crackedNR 8 SLAT ACTUATOR SUPPORT CRACKED I/B SIDE. REPAIRED PER MM 57-20-21.SDR AU981336Rod · fractured(AUS) NR 1 LEADING EDGE SLAT ACTUATOR EYE END FRACTURED. DAMAGE CAUSED TO NR 1 SLAT. INVESTIGATION FOUND THAT THE FAILURE WAS INITIATED BY STRESS CORROSION CRACKING AT AN AREA OF FRETTING AND CORROSION ON BORE SURFACE. PART TC: 28,098.SDR SCNA98085Actuator · failedDURING CLIMB, THE NUMBER FIVE LEADING EDGE SLAT AND THE NUMBER SIX LEADING EDGE FLAP WOULD NOT RETRACT. REMOVED AND REPLACED THE NUMBER FIVE LEADING EDGE SLAT ACTUATOR PER MAINTENANCE MANUAL 278132 AND INSTALLED A NUMBER SIX LEADING EDGE FLAP INDICATION EMERGSDR UPS98227520Mount · wornINSPECTION TYPE-D, NR 2 LE SLAT ACTUATOR VERY LOOSE IN MOUNTING STRUCTURE. REPLACED MOUNTING IAW SRM 51-30-02.SDR DHL98707003Actuator · leakingAFTER TAKEOFF WITH GEAR AND FLAPS UP, THE A- SYSTEM QUANTITY DECREASED TO ZERO. CRANKED GEAR DOWN, EXTENDED FLAPS AND LED WITH ALTERNATE SYSTEM. A-SYSTEM SHUT OFF 7 MINUTES. ABNORMAL PROCEDURES COMPLIED WITH. FOUND NR 1 LEADING EDGE FLAP ACTUATOR LEAKING.SDR UPS98227577Mounting · wornINSPECTION TYPE:D NR 2 L/E SLAT ACTUATOR VERY LOOSE IN MOUNTING STRUCTURE. MOUNTING REPLACED IAW EO B727-5720-1058.SDR SWAA981331Actuator · failedAFTER DEPARTURE CREW GOT INDICATIONS OF NR 5 SLAT ACTUATOR REMAINS EXTENDED, VISUALLY CONFIRMED. AIR TURNBACK TO NASHVILLE. AIRCRAFT MADE AN UNEVENTFUL LANDING. REPLACED SLAT ACTUATOR PER BOEING MM.SDR AU981256Actuator · leaking(AUS) RIGHT KRUEGER FLAP ACTUATOR LEAKING DUE TO EXCESS SEALANT ON THE SEAL PLATE BETWEEN THE ACTUATOR VALVE AND THE BLOCKING VALVE. LOSS OF HYDRAULIC FLUID. PART TC: 23,138.SDR DL72W981411Actuator · leakingNR 2 SLAT ACTUATOR LEAKING, LOST HYDAULICS ON FINAL. REPLACED ACTUATOR.SDR UPS98227230Angle · crackedINSPECTION TYPE-C, SUSPECT CRACK IN NR 2 KRUEGER FLAP ACTUATOR MOUNT SUPPORT STRUCTURE. REPLACED PART WITH NEWLY FABRICATED ANGLE IAW SRM 51-10-10, ANGLE INSTALLED IAW SRM 51-30-2.SDR TAOA079802Actuator · leakingBOS/LGA - FLT 6101 - LOST HYDRAULIC FLUID A-SYSTEM ON TAXI OUT. REPLACED NR 3 SLT ACTUATOR PER MM 27-81-32. LEAK CHECK AND OPERATIONAL CHECK NORMAL. (X)SDR SCNA98064Actuator · failedON CLIMB, THE NUMBER EIGHT LEADING EDGE SLAT WOULD NOT RETRACT ON SCHEDULE. TWO ATTEMPTS WERE MADE TO RECYCLE FLAPS AS PER COM PROCEDURE BUT THE NUMBER EIGHT SLAT REMAINED FULLY EXTENDED AS CONFIRMED BY VISUAL INSPECTION. FOUND THE LEADING EDGE NUMBER EIGHT SDR EISA98139Actuator · malfunctionedAFTER TAKEOFF FROM DFW DURING FLAP/SLAT RETRACTION, NR 5 SLAT FAILED TO RETRACT. RECYCLED NR 5 SLAT, STILL DID NOT RETRACT. RETURNED TO DFW. GENERATED FROM PILOT REPORT. REMOVED AND REPLACED NR 5 SLAT ACTUATOR WITH SERVICEABLE PART. GROUND OPS CHECK GOOD.SDR UPS98227021Slat · damagedINSPECTION TYPE:C, NR 5 SLAT O/B ACTUATOR RIB DAMAGED. REPAIR CARRIED OUT IAW SRM 51-40-2.SDR DL72L981264Support · crackedNR 6 L/E FLAP ACTUATOR SUPPORT BRACKET CRACKED AT RADIUS I/B UPPER END AND O/B LOWER END. INSTALLED DOUBLERS PER M/M 57-20-21.SDR DL72L981262Angle · crackedFOUND ON F1 LETTER CK, NR 2 LE FLAP ACTUATOR SUPPORT BOX CRACKED O/B SIDE. REPAIRED PER MM 57-20-21.SDR DL72W981231Fitting · crackedNR 4 SPOILER O/B ACT SUPPORT FITTING CRACKED. REPAIRED PER MM 57-42-0.SDR DL72S981183Actuactor · leakingIN CRUISE FLIGHT LEVEL 310 A SYSTEM QTY RAPIDLY DECREASED TO ZERO FOLLOWED BY A SYSTEM PRESSURE DECREASING TO ZERO. WHILE RUNNING POM OUTBOARD FLAPS FAILED TO ALT EXTEND. REPLACED NR 3 LED FLAP ACUTATOR. REPLACED NR 1 AND NR 2 HYD CASE DRAIN FILTERS. LEAK SDR DL72L981187Mount · crackedNR 1 LE FLAP ACTUATOR MOUNT CRACKED UPPER O/B CORNER. REPAIR PER M/M 57-20-21.SDR AU980675Pdu · faulty(AUS) GROUP 1 LEADING EDGE FLAP POWER DRIVE UNIT (PDU) FAULTY.SDR CALA9800927Bracket · crackedINSPECTION FOUND A 1 INCH CRACK IN LT WING NR 2 LEADING EDGE FLAP ACTUATOR ATTACH BRACKET AT LOWER INBOARD CORNER INSIDE LEADING EDGE AREA. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-1, AND 51-10-2.SDR CALA9800926Bracket · crackedINSPECTION FOUND A 1 INCH CRACK AT LOWER INBOARD AND OUTBOARD CORNERS OF LT WING NR 1 LEADING EDGE FLAP ACTUATOR ATTACH BRACKET. THE BRACKETS WERE REMOVED AND NEW BRACKETS WERE FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-10-6.SDR MZZA98160Actuator · rupturedMNL - FLT 876/27 - AIRCRAFT AIR RETURNED DUE TO LOSS OF A-SYSTEM HYDRAULIC FLUID. FOUND NR 1 LE FLAP ACT RUPTURED. LOG PAGE REMAINS OPEN AND NOT ENTERED, AWAITING SPARES. FLIGHT CONTINUED USING AIRCRAFT 435. (X)SDR CA980602080Actuator · cracked(CAN) AFTER DEPARTURE, THE AIRCRAFT EXPERIENCED A 'B' SYS FAILURE AND RETURNED TO BLOCKS. DURING FLAP AND GEAR SELECTION, THE AIRCRAFT ENTERED AN UNCOMMANDED RIGHT ROLL WHICH THE CREW WAS ABLE TO COMPENSATE FOR. THE OUTBOARD FLIGHT SPOILER WAS PARTIALLY DEPLSDR AU980984Stud · fractured(AUS) LT OUTBOARD NR 1 LEADING EDGE SLAT ACTUATOR STUD LOCKING ASSEMBLY END FITTING FRACTURED AND JAMMED UNDER THE HEAD OF THE INNER PISTON P\N 65-44757-1 AND THE END OF THE TRANSFER TUBE P\N 65-44768-1 PREVENTING CORRECT OPERATION OF THE ACTUATOR. PART TC: SDR CALA9800892Bracket · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 5 LEADING EDGE FLAP AFT INBOARD ACTUATOR MOUNT BRACKET BELOW ACTUATOR TRUNNION. THE MOUNT BRACKET WAS REMOVED, A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR 98FDEA00354Actuator · failedAFTER T/O, DURING FLAP RETRACTION FROM 2 DEG TO UP, AMBER LEADING FLAPS LIGHT REMAINED ON, NR 3 SLAT AMBER LIGHT IND INTERMEDIATE POS, A-SYS HYD QTY OBSERVED AT ZERO. RED TAB CKLT ACCOMPLISHED. SAFETY WIRE BROKEN ON A FLUID S/O VALVES AND GPWS FLAP. UNEVENTSDR DHL9870608CAngle · damagedAT C-CHECK, RIGHT WING NR 6 KRUEGER FLAP ACTUATOR CHECK PREV REPAIR, AT INBD VERTICAL SUPPORT ANGLE AT LOWER FWD END. REMOVED AND REPLACED SUPPORT ANGLE PER SRM 57-10-1, 8 X 4. N/R 2023.SDR DL72L980976Actuator · failedLOST ALL A-SYSTEM HYDRAULIC FLUID. REPLACED NR 4 SLAT ACTUATOR.SDR DL72E980980Bracket · crackedNR 1 SLAT ACTUATOR MOUNT BRACKET CRACKED 1.5 INCH VISIBLE O/B END. REPAIRED PER M/M 57-20-21.SDR 9808049931Rod End · brokenDURING APPROACH, SLAT DISAGREEMENT LIGHT ILLUMINATED WITH AIRCRAFT ROLL OF APPROXIMATELY 20 DEGREES ON SLAT EXTENSION. MAINTENANCE FOUND LEFT LOWER SLAT DRIVE CYLINDER ROD END BROKEN. REPLACED ROD END, OPERATIONAL CHECK NORMAL.SDR DL72S980966Bracket · crackedAT HMV, FOUND RW ACTUATOR BRACKET CRACKED NR 6 KRUEGER FLAP ACTUATOR BRACKET LOWER O/B FWD CORNER. REMOVED ACT AND BEAM PER MM 57-20-21, STOP DRILLED CRACK, INSTALLED PER MM 57-20-21.SDR DL72K980900Bracket · crackedFOUND ON MV2 CORROSION VISIT, NR 2 L/E FLAP ACTUATOR O/B ATTACH BRACKET CRACKED, LOWER END. REPAIRED PER 57-20-21.SDR DL72K980899Bracket · crackedFOUND ON MV2 CORROSION VISIT, NR 2 L/E FLAP I/B ACTUATOR ATTACH BRACKET CRACKED. REPAIRED PER M/M 57-20-21.SDR DL72K980898Bracket · crackedFOUND ON MV2 CORROSION VISIT, NR 1 L/E FLAP ACTUATOR INBD ATTACH BRACKET CRACKED, UPPER AND LOWER CORNERS. REPAIRED PER M/M 57-20-21.SDR 9806816611Actuator · malfunctionedDURING CLIMB, THE NR 3 LEADING EDGE FLAP WOULD NOT RETRACT. AIRCRAFT RETURNED TO NRT AND LANDED WITHOUT INCIDENT. REPLACED THE NR 3 LEADING EDGE FLAP ACTUATOR, OPERATIONAL CHECK GOOD.SDR DL72W980827Bracket · crackedFOUND ON C-2 LETTER CHECK, INBD ATTACH BRACKET CRACKED NR 1 L/E FLAP ACTUATOR. REPAIR PER MM 57-20-21.SDR DL72W980973Bracket · crackedBRACKET CRACKED NR 1 KRUEGER ACTUATOR SUPPORT BRACKET AT I/B LOWER CORNER. REMOVED FASTENERS TO FACILITATE DOUBLER AND STOP DRILLED CRACK PER M/M 57-20-21 PG 811. FABRICATED DOUBLER PER M/M 57-20-21 PG 811. INSTALLED DOUBLER PER MM 57-20-21 FIG 807.SDR K3HA980048Actuator · leakingLOSS A SYSTEM HYDRAULIC FLUID, RETURNED TO BLOCK. TROUBLESHOT NR 6 SLAT ACTUATOR, INSTALLED NR 6 SLAT ACTUATOR IAWMM 27-81-32 OPS CHECK OK. ALSO, CHECK A AND B SYSTEM CASE DRAIN FILTERS NO DEFECTS NOTED. REF MM 29-11-0 AND 29-12-0.SDR DL72W980768Bracket · crackedFOUND ON E1 LETTER CK, NR 8 SLAT ACTUATOR I/B MOUNT BRACKET IS CRACKED. REPAIR PER MM 57-20-21.
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