JASC 2782
Service difficulty reports · 1,225
Reports filed under 2782 · Leading Edge Slat Actuator, newest first.
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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 SIMA200300818Actuator · failedDFW - FLT 3902 - CREW REPORTED A SLATS FAULT CAUTION ON EICAS. MAINTENANCE REMOVED AND REPLACED THE LEFT (S/N 0164) AND RIGHT OUTBOARD SLAT ACTUATORS IAW CRJ MM. AIRCRAFT WAS RELEASED FOR A FUNCTIONAL CHECK FLIGHT. CHECK FLIGHT WAS SATISFACTORY AND AIRCRAFTSDR CA030121003Bearing · loose(CAN) ON 9 JAN 2003 IT WAS FOUND THAT THE ROLLER BEARING ON THE NR 5 SLAT OUTBOARD TRACK HAD BECOME DETACHED AND THE CONTROL ARM HAD WORN THROUGH THE TOP WING SKIN FORWARD OF THE FRONT SPAR. UPON REMOVAL OF THE ACCESS PANEL ALL THE PARTS WERE FOUND INSIDE INCLSDR USAASB02245Rod End · failedORD - FLT 1472 - WHILE CONFIGURING FOR LANDING AT ORD, CAPTAIN REPORTED THE LEADING EDGE TRANSIT LIGHT ILLUMINATED AND REMAINED ON DURING SECLECTION OF FLAPS 1, 5, 10, AND 15. CREW COMPLETED QUICK REFERENCE HANDBOOK PROCEDURES AND ACCOMPLISHED A 15 DEGREE FLAPSDR SIMA200235104Actuator · inoperativeBOI - FLT 3903 - DURING DESCENT WHEN FLAPS WERE LOWERED CREW RECEIVED A SLATS FAIL MESSAGE ON EICAS. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE RIGHT SLAT ACTUATOR IAW CRJ MM. OSDR QXEA0202153Actuator · failedPDX - CREW REPORTED A INTERMITTENT SLAT FAULT MESSAGE DURING DESCENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE RIGHT NR 6 SLAT ACTUATOR. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR AWXA200201181Actuator · bindingEMERGENCY LANDING - FLT 0571 - ON LANDING, RECEIVED CLASS 1 SLAT FAULT, EMERGENCY DECLARED, LANDED WITHOUT SLATS. MAINTENANCE INSPECTED SLAT SYSTEM AND FOUND THE TORQUE LIMITER INDICATOR VISIBLE ON THE NR 2 SLAT ROTARY ACTUATOR. REMOVED AND REPLACED THE NR 2 SDR CA021203009Actuator · leaking(CAN) AFTER LANDING, FLIGHT CREW REPORTED THE AIRCRAFT LOST ALL SYSTEM "A" HYDRAULIC PRESSURE AND THE FLUID QUANTITY INDICATION READ ZERO.MAINTENANCE INSPECTION REFEALED THE NR 1 GROUND SPOILER OUTBOARD ACTUATOR ASSEMBLY WAS LEAKING - ACTUATOR CASING CRACKED. SDR DL72S021391Actuator · failedAFTER T/O AMBER LED LIGHT REMAINED ILLUMINATED AT FLAPS 2. POSITION TEST SHOWED NR 4 L/E DEVICE NOT RETRACTED. REPLACED NR 4 SLAT ACTUATOR.SDR SWAA022761Actuator · leakingON TAXI OUT, LOSS OF HYDRAULIC 'A' SYSTEM, ZERO QUANITY AND ZERO PRESS. REMOVED AND REPLACED NR 6 SPOILER ACTUATOR AND CASE DRAIN FILTER PER MM.SDR SWAA022760Actuator · leakingLEFT INBD GROUND SPOILER ACTUATOR LEAKING HYDRAULIC FLUID. REMOVED AND REPLACED LEFT INBD GROUND SPOILER ACTUATOR PER MM.SDR AALA20021684Actuator · inoperativeLEADING EDGE SLAT WOULD NOT RETRACT. AIRCRAFT LANDED PHL WITHOUT INCIDENT. REPLACED NR 6 LEADING EDGE SLAT ACTUATOR. ACCOMPLISHED THERMO CHECKS OF ALL SLAT FLAP ACTUATORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR CA021115012Actuator · failed(CAN) ON APPROACH YVR WHEN FLAP SELECTED 'F/CTL SLAT FAULT' MASSAGE APPEARING AND SLATS FAILED TO OPERATE.LT NR 2 SLAT ACTUATOR TORQUE LIMITER INDICATOR FOUND POPPED. R/H OUTBD. SLAT ACTUATOR 6029 CM REPLACED AS PER AMM 27-84-49 AND SLAT FUNCTION CHECKED SERVISDR GAIA02155OPActuator · crackedDURING CLIMB-OUT OF SCHEDULE FLIGHT NR 705 FROM IAH-FWA, THE CREW NOTICED THE LOSS OF SYSTEM 'A' HYDRAULIC QUANTITY, AND PRESSURE WENT TO ZERO. THE CREW DECLARED AND EMERGENCY AND RETURNED IAH. THE AIRCRAFT LANDED WITHOUT ANY INCIDENT. MAINTENANCE FOUND THESDR 02FDEA00802Actuator · leakingAFTER T/O, LOST A SYSTEM HYDRAULICS. PERFORMED CHECKLISTS AND RED TAB PROCEDURES. DECLARED EMERGENCY, CALLED MOCC. AFTER SLAT ACTUATOR CHANGE PER 27-80-6282 SERVICED HYD SYS PER MM 12-12-000-3. OPS CHECK GOOD.SDR AALA20021538Actuator · failedMIA - FLT 971 - EN ROUTE DFW-MIA, ON APPROACH TO MIA, RECEIVED LEADING SLAT ASYMMETRY EICAS MESSAGE WHEN EXTENDING FLAPS FROM 1 DEGREE. DECLARED EMERGENCY AND LANDED AT MIA WITHOUT INCIDENT. TROUBLESHOT AND REPLACED NR 7 SLAT OUTBOARD ROTARY SLAT ACTUATOR. SDR 0203479938Actuator · leakingDURING APPROACH FOR LANDING WHEN CREW SELECTED SLAT DEPLOYMENT, THE AIRCRAFT HAD AN UNCOMMANDED ROLL TO THE LEFT ACCOMPANIED BY SLAT DISAGREEMENT LIGHT. COMPLIED WITH COM PROCEDURES, THE SLATS WERE RETRACTED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE RIGHSDR 02FDEA00703Actuator · failedDURING FLAP RETRACTION NR 2 SLAT ON RIGHT WING REMAINED EXTENDED WITH FLAP LEVER IN UP POSITION. QRH PROCEDURES WERE FOLLOWED AND FLAPS WERE CYCLED BACK TO 5 ON SCHEDULE FLAPS RETRACTED AGAIN AND PROBLEM CONTINUED. REMOVED AND REPLACED NR 2 SLAT ACTUATOR AS SDR AUS20021240Piston · broken(AUS) NO1 LEADING EDGE FLAP ACTUATOR PISTON SHEARED IN HALF. RETAINER PITTED, KEY CHROME CHIPPED AND RODEND REQUIRED REPLACEMENT.SDR 02FDEA00688Actuator · failedAFTER FLAP RETRACTION, WITH FLAPS UP AND LED LIGHT GREEN, "A" SYSTEM QUANTITY DECREASED TO ZERO. WITH LOSS OF "A" SYSTEM PRESSURE RAN APPROPRIATE EMERGENCY CHECKLISTS. FOUND NR 4 SLAT ACTUATOR BODY FAILED AT ENDCAP WHERE ROD EXITS THE HOUSING. REMOVED AND RSDR DL72E021126Actuator · leakingTOTAL LOSS OF A SYSTEM HYDRAULICS. FOUND NR 5 LDG EDGE FLAP ACTUATOR LEAKING AT SHUTTLE VLV, REMOVED NR 5 LDG EDGE FLAP ACUATOR. REPLACED NR 5 L/E FLAP ACTUATOR AND SHUTTLE VALVE PER JIC. A SYS HYD READS 1.5 GALLON. SERVICED SAME TO FULL RAN ALL PUMPS AND SDR DL72E021115Actuator · leakingSHORTLY AFTER T/O A SYS HYD QUANTITY WENT TO ZERO AND LOST PRESSURE. ATB BACK TO BWI. FOUND NBR 5 KRUEGER FLAP ACTUATOR HAD FAILED AND WAS LOSING FLUID, REPLACED SAME.SDR C7WA200200028Actuator · brokenLOST ALL OF "A" SYSTEM HYDRAULIC WHEN CLIMBING OUT OF 15,000 FEET.RETURNED TO TUS WITHOUT FURTHER INCIDENT. 2 GALLONS REMAINING AFTER TAXI-IN.FOUND BROKEN #4 KRUEGER FLAP ACTUATOR. REMOVED AND REPLACED.OPS CHECK OK I/A/W M.M. 27-00-81SDR SWAA022018Actuator · failedNR 3 KRUEGER FLAP WILL NOT RETRACT. REMOVED AND REPLACED NR 3 KRUEGER FLAP ACTUATOR PER MM.SDR SWAA021951Actuator · failedAIR TURNBACK, DURING FLAP RETRACTION AFTER TAKEOFF, NR 3 L/E SLAT FAILED TO RETRACT. REMOVED AND REPLACED NR 3 L/E SLAT ACTUATOR PER MM.SDR SWAA021879Actuator · failedNR 3 L/E SLAT TRANSIT LIGHT ILLUMINATED. REMOVED AND REPLACED NR 3 SLAT ACTUATOR PER MM.SDR CA020731016Actuator · failed(CAN) L/E FLAP TRANSIT ON AFTER T/O. NR 5 RT WING SLAT FULLY EXTENDED FOR APPROX 2 MIN. WHEN IT RETRACTED AND BEFORE WE RECYCLED THE FLAPS. REPLACED NR 5 SLAT ACTUATOR AS PER AMM. SYSTEM CHECKED SERVICEABLE AND CERTIFIED.SDR SWAA021488Actuator · failedAIR TURNBACK, AFTER TAKEOFF NR 2 KRUEGER FLAP WOULD NOT RETRACT. REMOVED AND REPLACED NR 2 KRUEGER FLAP ACTUATOR PER MM.SDR SWAA021287Actuator · failedAIR TURNBACK, L/E FLAP TRANSIT LIGHT REMAINED ON WITH ALL L/E DEVICES EXTENDED. REMOVED AND REPLACED NR 1, 6, 7 AND 8 L/E SLAT ACTUATORS PER MM.SDR SWAA021235Actuator · failedAIR TURNBACK, DURING FLAP RETRACTION, THE L/E AMBER LIGHT AND NR 4 KRUEGER FLAP GREEN LIGHT SHOWED FULL EXTEND. RECYCLED FLAPS, NO HELP. VISUAL INSPECTION SHOWED NR 4 KRUEGER FLAP WAS STUCK FULL DOWN. REMOVED AND REPLACED NR 4 KRUEGER FLAP ACTUATOR PER MM.SDR SWAA021211Actuator · failedAIR TURNBACK, AFTER TAKEOFF L/E TRANSIT LIGHT ILLUMINATED, L/E DEVICES WOULD NOT FULLY RETRACT. REMOVED AND REPLACED NR 5, NR 7 AND NR 8 L/E SLAT ACTUATORS PER MM, ( S/N'S D00518, 2176 AND 5025 ).SDR DHL2002753004Actuator · failedNR 6 L/E SLAT FAILED TO RETRACT AFTER T/O. FOLLOWED ABNORMAL PROC, STILL DID NOT SHOW RETRACTED. R&R NR 6 L/E SLAT ACTUATOR IAW DHL B727A MM 27-81-32. OPS CHECK NORMAL.SDR 2002F00628Actuator · leakingON DEPARTURE FROM DAY TO ICT, 'A' SYSTEM HYDRAULIC QUANTITY WENT TO ZERO. ALL APPLICABLE CHECKLISTS WERE ACCOMPLISHED AND EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO DAY AND LANDED WITHOUT INCIDENT. (M)SDR UPS02238314Bracket · crackedINSPECTION TYPE:C, SUSPECT CRACKS ON NR 6 L/E FLAP ACTUATOR I/B & O/B ATTACH BRACKETS LWR FWD CORNERS. ATTACH BRACKETS FABRICATED IAW SRM 51-20-1 FIG 7, HEAT TREATMENT REF HT 02-27-03. BRACKETS INSTALLED IAW SRM 51-30-2 & DRAWING 65-16275.SDR AUS20020358Actuator · failed(AUS) INBOARD LEADING EDGE SLAT DRIVE ACTUATOR FAILED.SDR CA020412001Actuator · failed(CAN) "FLAP FAIL" WHEN FLAPS WERE SELECTED TO 8 DEG DURING APPROACH. EMERGENCY DECLARED AND LANDED. SYSTEM WOULD NOT RESET. FERRIED A/C , R&R'D LT INBD FLAP NR 1 AND 2 ACTUATORS FOR FAILING THEIR TORQUE CHECK. "FLAP FAIL" AT ZERO DEG AT 205 KNOTS ON DESCENSDR SWAA020688Actuator · failedDIVERSION, AT FL 350 L/E FLAP TRANSIT LIGHT ILLUMINATED, NR 2 L/E FLAP LIGHT ON OVERHEAD ILLUMINATED. REMOVED AND REPLACED NR 2 L/E FLAP ACTUATOR PER MM.SDR DL764020360Pdu · faultyALTERNATE SLAT INBOARD ELECTRIC ACTUATOR POPPED C/B. REPLACED SLAT PDU INBD ELECT MOTOR. OPS CHECK NORMAL.SDR DL764020313Actuator · malfunctionedRECEIVED ACARS FOR A FLAP DISAGREE ON CLIMBOUT FROM HNL, QRHB FOLLOWED AND WILL CONTINUE TO LAX. ON APPROACH IN LAX, FLAPS/SLATS EXTENDED, FLAPS OK BUT HAD NO INDICATION THAT THE LEADING EDGE HAD EXTENDED. CREW CALLED FAA FOR EMERGENCY EQUIPMENT. NORMAL LANSDR 2002UALA00501Pdu · failedLEADING EDGE DISAGREE EICAS MESSAGE AND LIGHT ILLUMINATED. FAILURE OF THE LEADING EDGE SLAT POWER DRIVE UNIT, (PDU), CAUSED THE LEADING EDGE SLAT AND TRAILING EDGE FLAP SYSTEMS TO SHUTDOWN AND PRODUCE THE LEADING EDGE DISAGREE EICAS MESSAGE. REPLACED THE LEASDR DL757020296Nut · looseRT AND LT WINGS L/E ROTARY ACTUATORS, TORQUE TUBE SPLINE RETAINING NUTS LOOSE. TORQUED RETAINING NUTS AS PER M/M 27-81-18-4.SDR 02FDEA00134Bearing · out of positionRT WING O/B SLAT DRIVE MECHANISM FWD BEARING MIGRATED. REMOVED AND REPLACED WING OUTBOARD SLAT DRIVE MECH PER EA 1-2780-60721.SDR 02FDEA00169Bearing · out of positionRT WING O/B SLAT DRIVE MECHANISM FWD BEARING MIGRATED.SDR 2002UALA00200Actuator · failedLEADING EDGE SLAT DISAGREE MESSAGE DISPLAYED. THE NUMBER 6 LEADING EDGE SLAT ROTARY ACTUATOR FAILED AND CAUSED SOME BINDING IN THE SLAT. THE BINDING WAS DETECTED BY THE FLAP/SLAT ELECTRONIC UNIT WHICH SUBSEQUENTLY SHUT DOWN THE SYSTEM AS FAILURE PROTECTION. SDR 2002UALA00199Actuator · failedLEADING EDGE SLAT DISAGREE MESSAGE DISPLAYED. THE NUMBER 6 LEADING EDGE SLAT ROTARY ACTUATOR FAILED AND CAUSED SOME BINDING IN THE SLAT. THE BINDING WAS DETECTED BY THE FLAP/SLAT ELECTRONIC UNIT WHICH SUBSEQUENTLY SHUT DOWN THE SYSTEM AS FAILURE PROTECTION. SDR 2002F00154Actuator · leakingFLT 8001 - DURING CRUISE 'A' SYSTEM HYDRAULIC QUANTITY DECREASED TO ZERO, FOLLOWED BY NR 1 'A' SYSTEM PUMP LOW PRESSURE LIGHT. FLIGHT CREW FOLLOWED AOM PROCEDURE. AIRCRAFT LANDED AT MMUN WITHOUT INCIDENT. MAINTENANCE FOUND 'A' SYSTEM RESERVOIR WITH 1 GALLONSDR 02FDEA00033Actuator · failedAFTER RETRACT FLAPS AND SLATS 5-6 MIN LATER AMBER LIGHT ILLUMINATED. REMOVED AND REPLACED NR 3 L/E FLAP SWITCH AND ACTUATOR PER MM 27-82-001-4, 27-81-022-4.SDR 0200199876Rod · brokenWHEN SLATS WERE EXTENDED, THE AIRCRAFT ROLLED TO THE RIGHT. SLAT DISAGREEMENT LIGHT ILLUMINATED AND BLUE SLAT EXTEND LIGHT DID NOT ILLUMINATE. COMPLIED WITH COM PROCEDURES AND AIRCRAFT LANDED UNEVENTFULLY WITH SLATS RETRACTED AND FLAPS EXTENDED. MAINTENANCE RESDR 2002F00233Spring · failedLE SLAT DISAGREE EICAS MESSAGE BETWEEN FLAPS 1 AND 0 ON RETRACTION. AIRCRAFT RETURNED TO DEPARTURE STATION. SLATS FOUND TO BE BINDING, LUBED AND OPERATIONAL CHECK PER AMM. ON NEXT DEPARTURE DISCREPANCY REPEATED. AIRCRAFT RETURNED TO DEPARTURE STATION. FURSDR 01FDEA01098Actuator · failedDURING T/O, NR 7 LEADING EDGE FAILED TO RETRACT. REMOVED AND REPLACED SLAT ACT PER MM 27-81-032-4.SDR ABXA010653Motor · leakingAN OIL ODOR WAS DETECTED IN THE AIR CONDITIONING SYSTEM DURING TAKEOFF. RAN UP PACKS WITH APU. SUSPECT ODOR FROM THE RIGHT PACK. FOUND EVIDENCE OF HYDRAULIC LEAK. SKYDROL AROUND THE PNEUMATIC DUCT CONNECTION IN THE KEEL AREA, RIGHT SIDE OF AIRCRAFT. REPLA
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