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 96ZZZX4611Actuator · crackedSLAT ACTUATOR CRACKED INSIDE TRUNNION. SUBMITTER RECOMMENDS MANUFACTURING PROCESS TO SMOOTH OUT SHARP EDGES OF PORT.SDR 96ZZZX4610Restrictor Plug · debris pluggedRETRICTOR PLUGS (8) WERE PLUGGED UP WITH DEBRIS.SDR EISA96116Actuator Bracket · crackedRIGHT WING NR 5 SLAT ACTUATOR ATTACH RIB BRACKET CRACKED. FABRICATED AND INSTALLED REPAIR PER SRM 57-20-03. TT: 66,991:57 HOURS. TC: 45,084. (X)SDR IXKA9600057Actuator · failedON DEPARTURE FROM LAS TO MDW, FLT 88 RETURNED TO LAS, AFTER NR 5 LE SLAT FAILED TO PROPERLY STOW, LE AMBER LIGHT ILLUMINATED. CONFIRMED NOT STOWED. REMOVED AND REPLACED NR 5 LE ACTUATOR, OPS AND LEAK CHECK OK AS PER MM 27-81. (M)SDR UPS96220635Mount Angle · crackedINSPECTION TYPE-C, LT WING NR 4 SLAT ACTUATOR ROD END MOUNT ANGLE O/B AND I/B SIDES ARE CRACKED. REMOVED CRACKED FLANGE FROM I/B AND O/B RIBS, FAB'D AND INSTALLED REPAIR ANGLE IAW SRM 51-40-3.SDR 9614982276Actuator · failedDURING FLAP RETRACTION, THE NR 1 SLAT AMBER LIGHT ILLUMINATE ON SECOND OFFICER'S PANEL. VISUAL CHECK SHOWED NR 1 SLAT DID NOT RETRACT. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED NR 1 SLAT ACTUATOR, PERFORMED FLAP/SLAT LEAK AND OPERATIONASDR SWAA960647Actuator · failedAFTER TAKEOFF, NUMBER 1 L/E SLAT WOULD NOT RETRACT. AIRCRAFT RETURNED TO MCO AND MADE AN UNEVENTFUL LANDING. REPLACED SLAT ACTUATOR AND LEAK CHECKED PER BOEING M/M.SDR DL72K961716Bracket · crackedFOUND NR 7 SLAT ACTUATOR CRACKED I/B BRACKET UPPER LOBE. REPAIRED PER ERA 303841-14.SDR CALA9600970Actuator · leakingTHE A-SYSTEM HYDRAULIC QUANTITY WAS LOST DURING CLIMBOUT. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 LEADING EDGE FLAP ACTUATOR LEAKING. THE ACTUATOR WAS REMOVED AND REPLACED. IN ADDITISDR DL72W961599Bracket · crackedFOUND ON B1 LETTER CK, NR 1 SLAT ACT INBD MOUNT BRACKET CRACKED. REPAIRED PER MM 57-20-21.SDR DL72W961598Bracket · crackedFOUND ON B-1 LETTER CK, NR 2 L/E FLAP ACTUATOR I/B MOUNT BRACKET CRACKED AT THE UPPER CORNER. REPAIRED PER MM 57-20-21.SDR AWXA960322Actuator · damagedICT/PHX - FLT 1103 - LOSS OF A-SYSTEM HYDRAULIC FLUID. CONTRACT MAINTENANCE FOUND NR 2 LEADING EDGE SLAT ACTUATOR DAMAGED. REMOVED AND REPLACED ACTUATOR PER R3M27020. OP CHECK NORMAL. INSPECTED HYDRAULIC FILTERS PER MM 2911-0. NO CONTAMINATION FOUND. PHXSDR AWXA960295Actuator · malfunctionedTUS - FLT 2606 - UNCOMMMANDED ROLL EXPERIENCED ON CLIMB-OUT OF TUSCON, CAUSED BY YAW DAMPER. YAW DAMPER COUPLER FAILS STEP 4 OF BITE, NEW COUPLER NO HELP. INSTALLED MEL 22-03. YAW DAMPER BITE CHECK GOOD AT THIS TIME PER MM 22-11-00, PAGES 543, 544. MEL 22-SDR 96ZZZX3977Actuator · failedLOG REPORT: GL521 AT MIA - RETURN FROM FLIGHT. AFTER TAKEOFF WHILE RETRACTING THE FLAPS FROM THE 5-DEGREE TO THE 2-DEGREE POSITIONS, THE LE FLAP AMBER INTRANSIT LIGHT ILLUMINATED ON THE FORWARD AND FE'S PANELS FOR THE NR 8 POSITION. REPLACED NR 8 SLAT ACTUASDR AWXA960266Actuator · failedLAS/SNA - FLT 0806 - AIR TURNBACK. ON TAKEOFF FROM LAS AT 200 FEET, HAD A STICK SHAKER FOR 25 SECONDS AT 170 KIAS. LEADING EDGE FLAP ANNUNCIATOR LIGHTS FLASHING BETWEEN TRANSIT EXT. AND L/E DEVICES OVERHEAD ANNUNCIATOR PANEL SHOWED NR 5 SLAT GOING BETWEEN EXSDR DL73S961364Actuator · failedNR 4 SLAT ACTUATOR FAILED TO EXTEND ON APPROACH. REPLACED NR 4 SLAT ACTUATOR, CHECKS OK.SDR 9612852294Act Fitting · crackedDURING P-CHECK, FOUND A CRACK IN THE NR 4 SLAT ACTUATOR INBOARD MOUNT FITTING. REPLACED FITTING PER SRM 51-10-01, PG 4.SDR AWXA960258Actuator · failedPHX/OAK - FLT 0577 - AIR TURNBACK. NR 2 SLAT EXTENDED ABOUT 2 INCHES EN ROUTE. REMOVED AND REPLACED NR 2 ACTUATOR PER R3M27020. OPERATION AND LEAK CHECK GOOD. PART TOTAL CYCLES, 35,841. (X)SDR AU960980Piston · fractured(AUS) NO6 LEADING EDGE KRUEGER FLAP ACTUATOR PISTON PNO 1110-15 BROKEN IN TWO IN THE RADIUS OF THE EXTENDED LOCKING KEY GROOVESDR UPS96220416Act Support Web · crackedINSPECTION TYPE SI, NR 5 K-FLAP ACTUATOR O/B TRUNNION SUPPORT WEB IS CRACKED. REMOVED CRACKED SUPPORT WEB, FABRICATED NEW SUPPORT WEB AND INSTALLED ON A/C IAW SRM 51-30-2, SRM 51-10-2.SDR 96ZZZM1024Actuator · malfunctioningTHE NR 2 LEADING EDGE SLAT FAILED TO RETRACT AFTER TAKEOFF FROM IND. AIRCRAFT MADE AIR TURN BACK TO IND AND LANDED WITHOUT INCIDENT. REPLACED THE NR 2 SLAT ACTUATOR PER MM 27-81-32. OPS CHECK GOOD. (M)SDR 9611352294Actuator · malfunctionedDURING TAKEOFF CLIMB, THE NR 3 LEADING EDGE KRUEGER FLAP WOULD NOT RETRACT AND FUEL WAS DUMPED TO LANDING WEIGHT. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE NR 3 KRUEGER FLAP ACTUATOR, FUNCTIONAL CHECK OK.SDR 96UAL900347Actuator · inoperativeFLIGHT CREW VISUAL VERIFICATION THAT THE NUMBER TWO LEADING EDGE FLAP WAS HANGING UP IN THE EXTENDED POSITION. *S/D* NUMBER TWO LEADING EDGE FLAP ACTUATOR MALFUNCTIONED. REPLACED ACTUATOR AND SYSTEM CHECKED OK.SDR 9610752276Actuator · failedDURING CLIMB, NR 2 SLAT FAILED TO RETRACT. AIRCRAFT RETURNED TO ABQ AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NR 2 SLAT ACTUATOR, OPERATIONAL CHECK OK.SDR SWAA960377Actuator · failedAFTER TAKEOFF, NR 5 L/E SLAT WOULD NOT RETRACT. AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. REPLACED SLAT ACTUATOR PER BOEING M/M.SDR AU960988Actuator · faulty(AUS) WING LHS OUTBOARD NO2 AND NO5 SLAT ACTUATORS FAULTY - SUSPECT CAUSED BY INCREASED BREAKOUT TORQUE AT LOW TEMPERATURESSDR DL72P961094Bracket · crackedAPPROX 2 INCH CRACK IN NR 1 SLAT I/B AND O/B ACTUATOR MOUNT BRACKET'S. REPAIRED PER M/M 57-20-21 AND ERA DUE TO A/C EFFECTIVITY.SDR DL72P961093Bracket · crackedNR 1 L/E FLAP ACTUATOR MOUNT BRACKET CRACKED AT LOWER I/B CORNER. REPAIRED PER M/M 57-20-21 AND ERA DUE TO A/C EFFECTIVITY.SDR AU960888Actuator · faulty(AUS) NO2 SLAT RH OUTBOARD SLAT ACTUATOR FAULTY - SUSPECT MOISTURE INGRESS CAUSED FREEZING AT ALTITUDE PREVENTING SLAT ACTUATIONSDR DHL9670912CActuator Mount · crackedAT C-CHECK, FOUND NR 2 SLAT ACTUATOR MOUNT CRACKED. FABRICATED DOUBLER REPAIR PER S/B 57-130, DOUBLER 8 BY 3.SDR 96UAL900312Actuator · failedABORTED TAKEOFF SJC AT 115 KNOTS DUE TO THE LOSS OF 'A' HYDRAULIC SYSTEM. TOWED TO GATE. SUPPLEMENTAL DATA UPDATE: NR 1 LEADING EDGE SLAT ACTUATOR CRACKED AT HOUSING AFT END. REPLACED NR 1 LEADING EDGE SLAT ACTUATOR. SERVICED 'A' HYDRAULIC SYSTEM.SDR 96FDEA00897Act Bracket · crackedNR 0089 AND NR 002, NR 2 K-FLAP ACTUATOR AFT I/B MOUNT IS CRACKED AT UPPER FWD CORNER. ****S/D ****** COMING. REMOVED AND REPLACED NR 2 K-FLAP ACTUATOR APT I/B MOUNT IAW FEDEX SRM 51-10-1 AND 51-30-2.SDR SWAA960318Actuator · failedDURING CLIMBOUT, NUMBER 6 L/E SLAT WOULD NOT RETRACT. RECYCLED FLAPS, NO HELP. AIRCRAFT RETURNED TO ONT AND MADE AN UNEVENTFUL LANDING. REPLACED NR 6 SLAT ACTUATOR AND OPERATION CHECKED PER BOEING M/M.SDR 9610962295Actuator Fitting · crackedDURING H-CHECK, FOUND A CRACK AND CORROSION IN THE RIGHT WING NR 4 LEADING EDGE FLAP ACTUATOR FITTING. REPLACED FLAP (P/N 65-16225-6A) PER MM 27-81-01.SDR 96UAL900294Drive Unit · failedNR 1 LEADING EDGE FLAP FAILED TO RETRACT. *S/D* DRIVE UNIT FAILED TO RETRACT PNEUMATICALLY OR ALTERNATELY AFTER TAKEOFF. DISASSEMBLY OF THE FAILED UNIT REVEALED A FAILED AIR ROTOR BEARING. ADDITIONALLY THE ALTERNATE DRIVE MOTOR FAILED, PROBABLY DUE TO EXTSDR DL72S960995Actuator Bracket · crackedNR 8 SLAT ACTUATOR MOUNT BRACKETS CRACKED OUTBOARD AND INBOARD SIDES. REPAIRED PER M/M 57-20-21.SDR DL72S960985Actuator Bracket · crackedFOUND ON F1 LETTER CHECK, NR 5 LE FLAP ACTUATOR ATTACH ANGLE CRACKED. REPAIRED PER MM 57-20-21.SDR DL72S960983Actuator Bracket · crackedFOUND ON F1 LETTER CHECK, NR 1 SLAT ACTUATOR INBOARD MOUNT BRACKET CRACKED AT UPPER MOUNT BOLT. REPAIRED PER MM57-20-21.SDR DL72P960965Act Mount Brkt · crackedFOUND DURING C-CHECK - CRACK NR 8 SLAT ACTUATOR MOUNT BRACKETS, INBOARD AND OUTBOARD SIDES. REPAIRED PER M/M 57-20-21.SDR DL72W960930Act Angle · crackedNR 8 SLAT ACTUATOR INBOARD ATTACH ANGLE CRACKED. REPAIR PER M/M 57-20-21.SDR DL72W960929Act Support · crackedFOUND TWO-INCH CRACK IN NR 8 SLAT OUTBOARD ACTUATOR SUPPORT WHILE SHOWING MAINTENANCE LOCATION OF CRACK AT INBOARD SUPPORT. REPAIR PER M/M 57-20-21.SDR DL72S960885Act Mount Box · cracked angleFOUND ON B-1 LETTER CHECK, NR 5 L/E FLAP ACT MOUNT BOX I/B LWR ANGLE CRACKED. REPAIRED PER M/M 57-20-21 PG 811.SDR DL72S960883Act Attach Box · crackedFOUND ON B-1 LETTER CHECK, 1 INCH CRACK NR 2 L/E FLAP ACT ATTACH BOX O/B SIDE. REPAIRED PER M/M 57-20-21.SDR 96ZZZM903Actuator · failedFLT 680 - STL - DURING LANDING, 'A' SYSTEM HYDRAULIC QUANTITY WAS LOST. REMOVED AND REPLACED NR 6 LEADING EDGE SLAT ACTUATOR, MFG P/N 1U1095-9-2. OPERATIONAL CHECK NORMAL. (M)SDR DL72S960778Actuator · failedSLOW LEAK OF HYDRAULIC SYSTEM-A AT F310 AFTER 2 HRS AT CRUISE. POM PROCEDURES FOLLOWED FOR LOSS OF SYSTEM-A. RT SLAT NR 6 DID NOT EXTEND WITH ALTERNATE FLAPS EXTENSION SWITCH. FOUND NR 6 SLAT ACTUATOR LEAKING. REPLACED ACT SERVICED HYD SYSTEM, OPERATIOSDR MZZA96016Slat Actuator · crackedGUM - FLT 0956 - ON TAKEOFF CLIMB OUT OF TKK, NR 6 LEADING EDGE SLAT DID NOT RETRACT AND A HYDRAULIC SYSTEM HAD FLUID LOSS. ALL REQUIRED CHECK LISTS WERE COMPLETED AND AIRCRAFT DIVERTED TO GUM. MAINTENANCE FOUND THE NR 6 LEADING EDGE SLAT ACTUATOR FORWARD ENSDR 9607602286Actuator · failedDURING CLIMB, NR 2 LEADING EDGE FLAP INDICATED DOWN WITH FLAP HANDLE IN THE UP POSITION. AIRCRAFT HAD A 5 DEGREE ROLL ATTITUDE AT 2 DEGREES OF FLAPS. DUMPED FUEL, RETURNED TO MSP, AND LANDED WITHOUT INCIDENT. REPLACED THE NR 2 LEADING EDGE FLAP ACTUATOR. ASDR 9606782204Actuator · malfunctionedDURING DEPARTURE CLIMB UPON FLAP RETRACTION, THE NR 2 LEADING EDGE SLAT REMAINED EXTENDED WITH FLAPS UP SELECTED. NOTABLE VIBRATION WAS FELT. CREW JETTISONED 20,000 LBS OF FUEL AND RETURNED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 SLATSDR DL72L960640Attach Fitting · crackedA .5 INCH CRACK IN NR 1 SLAT ACTUATOR I/B ATTACH FITTING. FOUND DURING D-1 LETTER CHECK. REPAIRED PER MM 57-20-21.SDR DL72L960639Attach Fitting · crackedDURING D-1 LETTER CHECK, FOUND .5 INCH CRACK IN NR 1 SLAT ACTUATOR O/B ATTACH FITTING. REPAIRED PER MM 57-20-21.
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