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 DL72S010333Bracket · crackedNR 7 SLAT ACTUATOR INBD ATTACH BRACKET CRACKED. REPAIRED PER 57-42-000-8.SDR EISA20010031Connector · looseNR 8 LEADING EDGE SLAT HAD BOTH AMBER LIGHTS ON IN AGREEMENT, PILOT STATED THAT HE COULD FEEL VIBRATION. THE AIRCRAFT OVERFLEW DFW TO IND. INSPECTED NR 8 ACTUATOR AND FOUND LOOSE CONNECTOR. TIGHTENED CONNECTOR ON ACTUATOR, OPS CHECK GOOD.SDR AU010200Actuator · jammed(AUS) RH OUTBOARD LEADING EDGE FLAP DRIVE ACTUATOR JAMMED.SDR EISA20010030Actuator · malfunctionedON DEPARTURE WHEN RETRACTING FLAPS FROM 5 TO 2 DEGREES NR 8 SLAT WAS STUCK, IN THE EXTEND POSITION. AMBER L/E FLAP LIGHT ILLUMINATED AND NR 8 SLAT ILLUMINATED. CYCLED AGAIN SLAT RETRACTED. REMOVED AND REPLACED NR 8 SLAT ACTUATOR PER M/M 27-80-00, OPS CHECK SDR 01FDEA00160Support Bracket · crackedDURING ROUTINE INSP, NR 1 LEAD EDGE FLAP ACTUATOR, FWD OTBD UPPER FITTING SUPPORT BRACKET FOUND CRACKED.*S/D* REMOVED AND REPLACED BRACKET PER IAW BAC 727 MM 27-81-001-4 AND BAC 727 SRM 51-10-1.SDR AWXA0001374Actuator · contaminatedPHX - EMERGENCY LANDING - 2/12/01 - ON APPROACH, THE CREW GOT AN ECAM WARNING, F/CTL SLATS FAULT AND THE CREW DECLARED AN EMERGENCY; AN UNEVENTFUL LANDING WAS MADE IN PHX. MAINTENANCE TROUBLESHOT AND FOUND 1 LT AND 2 RT LEADING EDGE SLAT ROTARY ACTUATORS WITHSDR 01FDEA00136Actuator · failedREPEAT WRITE-UP NR 6 SLAT SHOW INTRANSIT AFT FLAPS WERE RAISED TO 0. RED TAB PROC FOLLOW WITH NO IMPROVEMENTS. CREW REPORTS A/C ROLLS TO THE LEFT WITH THE FLAPS SEL UP AND THE NR 6 L/E INTRANSIT LIGHT ON. REMOVED AND REPLACED SLAT ACTUATOR PER MM 27-81-03-4SDR SWAA010477Actuator · inoperativeAIR TURNBACK, RT KRUEGER FLAP WOULD NOT RETRACT. REMOVED AND REPLACED RT KRUEGER FLAP ACTUATOR. OPS CK GOOD PER MM.SDR DL72S020170Actuator · failedNR 4 SLAT LEFT WING REMAINED EXTENDED. REMOVED AND INSTALLED NR 4 SLAT ACTUATOR PER JIC OPN 7056.SDR 2001UALA00108Actuator · brokenHYDRAULIC SYSTEM-A FAILURE OCCURRED DURING FINAL APPROACH. LOST FLUID THEN PRESSURE. *S/D* FOUND NR 6 L/E SLAT ACT RETAINER CAP SEVERED FROM END OF THE ACTUATOR, WITH THE ACTUATOR IN THE FULLY EXTENDED AND LOCKED POSITION. REMOVED FAILED ACTUATOR, INSTALLESDR SWAA010369Actuator · failedAIR TURNBACK, 3 L/E FLAP FAILED TO RETRACT AFTER TAKEOFF. REMOVED AND REPLACED NR 3 L/E FLAP ACTUATOR PER MM.SDR EISA20010004Stiffener · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND CRACK AT NR 2 SLAT ACTUATOR STIFFENER. REMOVED CRACKED STIFFENER, FABRICATED STIFFENER, DOUBLER AND FILLER, ALODINED, PRIMED AND INSTALLED IAW SRM 51-30-2, 51-10-2, SB 57-0130, BSOPM 20-42-02.SDR DL72L010173Actuator · leakingSYSTEM A HYDRAULIC FLUID DECREASED BELOW 1 GALLON. TURNED OFF A-SYSTEM PUMPS AND COMPLIED WITH POM PROCEDURES FOR HYDRAULIC SYSTEM EMERGENCY. CRANKED GEAR AND FLAPS DOWN AND PERFORMED UNEVENTFUL LANDING AT 160000 LBS, RATE OF DESCENT AT TOUCHDOWN WAS 4SDR 20010125CW011Sleeve · fracturedSLEEVE /145/ OF BLOCKING VALVE ASSEMBLY IS FRACTURED. PROBABLE CAUSE/ FATIGUESDR 20010214SG001Mount Bracket · brokenON TAKEOFF FROM CAE SLAT INDICATION SHOWED RIGHT WING NR 3 SLAT EXTENDED. FLIGHT CREW RECYCLED THE FLAP SYSTEM AND SLAT REMAINED EXTENDED. CREW REPORTED HEARING A NOISE AND THEN LOSS OF THE ''''A'''' HYDRAULIC SYSTEM PRESSURE AND QT. THE CREW CONDUCTED A AISDR 2000UALA00813Actuator · leakingLEADING EDGE FLAP NR 5 WILL NOT RETRACT WITH FLAPS ALL THE WAY UP. *S/D* REPLACED NR 5 LEADING EDGE FLAP ACTUATOR PER MAINTENACE MANUAL. OPS CHECKS GOOD.SDR 20010126CW010Sleeve · crackedBLOCKING VALVE ASSEMBLY HAS A CRACKED SLEEVE 145.SDR 00FDEA00861Actuator · failed00-343 ON CLIMBOUT RETRACTED FLAPS FROM 5 DEG TO 2 DEG ON SCHELDULE NR 1 LEAD EDGE FLAP REMAIN IN TRANSIT. R&R PER 727-200 MM 27-81-22. OPS CK OK. AC OK FOR SERVICE.SDR 2000UALA00718Gear · wornL/E SLAT ASYM DURING FLAP EXTENTION ON APPROACH. *S/D* THE RIGHT WING SLATS DID NOT MOVE TO THE COMMANDED POSITION DUE TO A SEVERELY WORN OUTBOARD LEADING EDGE SLAT DRIVE TORQUE TUBE. WHEN THE LEFT WING L/E SLAT POSITION DOES NOT MATCH THE RIGHT WING L/E SLSDR GAIA00718Actuator · inoperativeFLT 3736 - BNA-FWA - NR 5 LEADING EDGE FLAP DID NOT FULLY EXTEND ON FLAP EXTENSION. HOWEVER, AT SLOW SPEED, FLAP FULLY EXTENDED. AIRCRAFT MADE AN UNEVENTFUL LANDING AT FWA. REMOVED AND REPLACED NR 5 KRUEGER FLAP ACTUATOR IAW 272 MM 27-81-22. OPS CHECK GOODSDR C1HA200097005Actuator · malfunctionedAFTER DEPARTURE UNABLE TO RETRACT NR 6 K-FLAP. COM CHECKLIST ACCOMPLISHED. REMOVED AND REPLACED NR 6 K-FLAP ACTUATOR, OPS CHECKED GOOD.SDR GAIA00690Actuator · inoperativeBNA/FWA - FLT 3735 - DURING LANDING, THE NR 5 LE KRUGER FLAP DID NOT FULLY EXTEND ON FLAP EXTENSION. THE CREW DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE NR 5 LE KRUGER FLAP ACTUATOR. OPS CHECK PERFORMED, AIRCRAFT RESDR DL72S002149Actuator · leakingON SLAT EXTENSION NR 6 SLAT NO INTRANSIT OR EXTEND LIGHT. CYCLED SLATS AND LOST A SYS HYD QTY. REPLACED NR 6 SLAT ACTUATOR FOR LEAKING.SDR 20001212SH016Locking Stud · chippedLOCKING STUD IS CHIPPING ON END THAT CONTACT WITH THE LOCKING SEGMENTS. (X)SDR 2000UALA00589Actuator · malfunctionedON DEPARTURE FROM PVD, NR 2 LEADING EDGE SLAT REMAINED IN THE EXTENDED POSITION. DIVERTED TO BOSTON. *S/D* FOUND FAILED TAI TELESCOPING DUCT AND RESULTING DAMAGE TO NR 2 L/E SLAT. REPLACED FAILED DUCT AND NR 2 L/E SLAT ASSY PER MAINTENANCE MANUAL. SYSTEMSDR DL73E001979Actuator · failedDURING APP WHEN FLAPS 2 SELECTED L/E FLAP TRANS LIGHT STAYED ILLUM AND 4 SLAT SHOWED UNSAFE YELLOW ON OVHD PANEL FLAPS WERE SELECTED TO 5 AND ALL WENT GREEN AND SHOWED SAFE. ABOUT 5 SECS LATER L/E FLAP TRANS LIGHT REILLUM AND 4 SLAT SHOWED UNSAFE AGAIN. FLASDR 20001102SH024Sleeve · crackedSLEEVE (145) OF THE BLOCKING VALVE ASSY WAS FOUND CRACKED DURING NDI. REMOVED AND REPLACD SLEEVE (145). (X)SDR DL72W001961Actuator · failedON TAKEOFF NR 2 SLAT ON LEFT WING DID NOT RETRACT. REPLACED NR 2 SLAT ACTUATOR, VISUALLY INSPECTED AND ALL CHECKS OK. SLAT ACTUATOR LEAK AND OPS CKS OK. NR 2 L/E SLAT ACTUATOR INSTALLATION, LEAK CK AND OPS CK OK PER M/M.SDR SWAA001948Actuator · inoperativeAIR TURNBACK, NR 1 L/E SLAT WOULD NOT RETRACT AFTER TAKEOFF, EXTENDED NORMALLY. REMOVED AND REPLACED NR 1 L/E SLAT ACTUATOR PER MM.SDR 20001102SH019Stud · chippedLOCKING STUD IS CHIPPING WHERE LOCKING SEGMENTS CONTACT. (X)SDR EISA20000153Actuator · inoperativeDURING CLIMBOUT AT FL 190, THE AMBER LEADING EDGE FLAP LIGHT ILLUMINATED. CONFIRMED WITH FE LED PANEL. RIGHT NR 6 SLAT INDICATOR SHOWED SLAT NOT RETRACTED. RETURNED TO (AUS) PER COMPANY REQUEST, EMERGENCY CHECKLIST COMPLIED WITH. REMOVED AND REPLACED NR 6 SDR 00FDEA00679Actuator · inoperativeON FLAP RETRACT, WHEN FLAPS RAISED THE LEAD EDGE DEVICE LIGHT REMAIN AMBER. *S/D* REMOVED AND REPLACED NR 1 SLAT ACTUATOR, OPS AND LEAK CK GOOD PER 727 MM 27-81-32.SDR CA001102014Actuator · cracked(CAN) ON LANDING DURING GROUND SPOILER DEPLOYMENT HYDRAULIC FLUID WAS OBSERVED LEAKING FROM THE NR 5 GROUND SPOILER NR 5 ACTUATOR. OBSERVATION REVEALED THAT UNDER PRESSURE A CRACK WOULD OPEN UP IN THE CASE. SPOILER ACTUATOR WAS REPLACED. CHECKED SERVICEABLE.SDR 2000UALA00557Actuator · leakingON TAKEOFF THE OUTBOARD FLAPS WOULD NOT RETRACT BEYOND POSITION 2. RETURNED TO ORD. ON APPROACH TO GATE SYSTEM A HYDRAULIC FLUID QUANTITY WENT TO ZERO. *S/D* REPLACED NR 5 RIGHT WING MIDDLE KRUEGER FLAP ACTUATOR PER MAINTENANCE MANUAL. SERVICED HYDRAULIC SDR CA001012007Actuator · failed(CAN) DURING APPROACH , GEAR DOWN, FLAPS 20, AUTOPILOT ON. VIBRATION, FELT LIKE SPOILERS UP. CONTROL WHEEL SHOWED 1/2 TO 3/4 (TOTAL) WHEEL MOVEMENT ROLL TO RIGHT. DISCONNECTED AUTOPILOT & AUTO THROTTLE, A AIRCRAFT, THEN ROLLED HARD TO LEFT, REQUIRED LARGE AMOSDR DHL2000740004Rod End · wornDURING T/O ROLL, LED ANNUNCIATOR WENT FROM GREEN TO AMBER. T/O REJECTED. CHRISTMAS TREE VERIFIED NR 3 FLAP. ABORT 80 KTS AND 152000 LBS. FOUND WORN ROD END ON NR 3 L/E FLAP ACTUATOR. REMOVED AND REPLACED ACTUATOR PER M/M 27-81-22, OPS CHK OK.SDR 20001102SH007Valve · crackedBLOCKING VALVE ASSY HAD A CRACKED SLEEVE. (X)SDR 00FDEA00620Actuator · failedON FLAP RETRACTION TO 2 DEGREES NR 1 LEAD EDGE FLAP STAY AMBER BOTH ON UP. REMOVED AND REPLACED SLAP IND SWITCH (S202) PER MM 27-81-000-5. REMOVED AND REPLACED ACTUATOR PER MM 27-81-22.SDR 20001102SH017Sleeve · crackedBLOCKING VALVE SLEEVES ITEMS 31 AND 32 ARE CRACKED. SUBMITTER STATED APPEARED CRACKS WERE OCCURRING UNDER NORMAL USE. (X)SDR 20001102SH016Sleeve · crackedBLOCKING VALVE SLEEVES ITEMS 31 AND 32 ARE CRACKED. SUBMITTER STATED APPEARED CRACKS WERE OCCURRING UNDER NORMAL USE. (X)SDR 20001102SH015Sleeve · crackedBLOCKING VALVE SLEEVES ITEMS 31 AND 32 ARE CRACKED. SUBMITTER STATED APPEARED CRACKS OCCURRING UNDER NORMAL USE. (X)SDR 20001102SH014Sleeve · crackedBLOCKING VALVE SLEEVES ITEMS 31 AND 32 ARE CRACKED. SUBMITTER STATED APPEARED CRACKS OCCURRING UNDER NORMAL USE. (X)SDR CA000907003Actuator · cracked(CAN) LOST " A" SYSTEM HYDRAULICS, PRESSUE AND QUANTITY READ ZERO. TROUBLESHOOTING CARRIED OUT FOUND NR 3 LEADING EDGE SLAT ACTUATOR HOUSING CRACKED. LEADING EDGE SLAT ACTUATOR REPLACED PER MM 27-81-22.SDR 20001102SH013Housing · crackedBODY HAD CRACKS IN BOTH THE EXTEND AND RETRACT PORTS. STRESS AND FATIGUE, TIME IN SERVICE UNKNOWN. (X)SDR DL72L001629Actuator · leakingA SYS HYD LOSS ON TAKEOFF, FOUND NR 7 LEADING EDGE SLAT ACTUATOR LEAKING FROM AFT SIDE. REPLACED NR 7 LEADING EDGE ACTUATOR.SDR C8GA200000009Actuator · rupturedFLIGHT EB513, FROM JAX TO BWI. ON TAXI OUT , LOST A SYSTEM HYDRAULICS. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENCE. FOUND NR 8 LEADING EDGE SLAT ACTUATOR HOUSING RUPTURED. REPLACED ACTUATOR. AIRCRAFT RETURNED TO SERVICE.SDR 2000UALA00494Actuator · splitON INITIAL MOVEMENT OF THE FLAP HANDLE TO 2 ON APPROACH, HYDRAULIC SYSTEM ''A'' QUANTITY AND PRESSURE WENT TO ZERO. *S/D* FOUND NR 6 SLAT ACTUATOR SPLIT AT AFT UPPER CYLINDER. REPLACED ACTUATOR PER MAINTENANCE MANUAL. SERVICED HYDRAULIC SYSTEM, OPERATIONASDR DL72S001560Actuator · failedSYSTEM A HYD LOSS IN FLIGHT WENT TO ZERO. FOUND NUMBER 6 LEADING EDGE KRUEGER FLAP ACTUATOR FAILED. REPLACED ACTUATOR.SDR USAA001186Bushing · corrodedPIT - FOUND CORROSION IN BOTH BUSHINGS .25 INCH BY .25 INCH AREA, FOR NR 2 KRUEGER FLAP ACTUATOR. CORROSION LEVEL 1, TASK NR C57-302-01. POLISHED AND BLENDED PER SRM 20-50-03. (M)SDR 2000UALA00422Actuator · bypassingNR 5 SLAT NOT RETRACTING TO FULL UP. *S/D* FOUND NR 5 SLAT ACTUATOR BYPASSING. REPLACED THE NUMBER 5 SLAT ACTUATOR.
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