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 9709742712Actuator · failedDURING CRUISE FLIGHT, AIRCRAFT LOST A-SYSTEM HYDRAULIC PRESSURE AND QUANTITY. BOTH ENGINE DRIVEN PUMPS RAN DRY. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED NR 3 LEADING EDGE KRUEGER FLAP ACTUATOR AND BOTH ENGINE DRIVEN HYDRAULIC PUMPS. PSDR DL72S970912Mount · crackedNR 5 K FLAP ACTUATOR MOUNT CRACKED. REMOVED ACTUATOR MOUNT AND STARTED REPAIR PER M/M 57-20-21 FIG 807. REPAIRED PER DAL M/M 57-20-21 FIG 807. INSTALLED ACTUATOR MOUNT.SDR 97ZZZX2629Actuator · mismodifiedSLAT ACTUATOR FAILED TO OPERATE PROPERLY UPON INSTALLATION. INITIAL INSPECTION AND TESTING REVEALED COMPONENT TO BE THE DASH 12 CONFIGURATION RATHER THAN DASH 15 CONFIGURATION. THE CURRENT CONFIGURATION WAS DETERMINED BY THE LENGTH OF STROKE AND A BEARING PASDR SCNA97135Bracket · brokenDURING HEAVY MAINTENANCE VISIT, RIGHT WING NUMBER 7 SLAT ACTUATOR MOUNT BRACKET INBOARD EAR WAS FOUND BROKEN. INSTALLED BRACKET AND DOUBLER IAW B727 SRM 51-10-01, 51-10-02, AND 51-10-03.SDR CALA9700889Bracket · crackedINSPECTION FOUND A 1 INCH CRACK AT INBOARD AND OUTBOARD ENDS OF NR 2 LEADING EDGE FLAP ACTUATOR ATTACH BRACKET. THE BRACKET WAS REMOVED, A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.SDR DL72W970793Actuator · destroyedON CLIMBOUT THROUGH 7,000 FEET, THE A-SYSTEM HYDRAULIC QUANTITY WENT TO ZERO AND THE PRESSURE WENT TO ZERO, FOLLOWED POM. FOUND THE NR 4 SLAT ACTUATOR CASTING END BLOWN OUT. REPLACED ACTUATOR.SDR DHL9770164CBrackets · crackedAT C-CHECK, L/E FLAP NR 6 ACTUATOR BRACKETS CRACKED AT I/B AND O/B SIDES UPPER AND LOWER ATTACH LUGS. REMOVED BRACKETS, INSTALLED BRACKETS PER SRM 51-40-3 .SDR SWAA970410Actuator · inopAFTER TAKEOFF, RT O/B L/E SLAT WOULD NOT RETRACT. AIRCRAFT RETURNED TO SMF AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED RT O/B L/E SLAT ACTUATOR AND OP CHECKED PER BOEING M/M.SDR AU970422Actuator · failed(AUS) NO5 LEADING EDGE SLAT ACTUATOR EYE END BROKEN - SUSPECT CAUSED BY CORROSION PITTINGSDR DHL9770519CMount · crackedAT C CHECK, NR 6 LEADING EDGE FLAP ACTUATOR MOUNT IS CRACKED AT LOWER OUTBOARD CORNER. REMOVED ACTUATOR, REPLACED MOUNT ACTUATOR PER SRM 51-30-2. REINSTALLED ACTUATOR. N/R 2432.SDR 97UAL900283Actuator · failedON APPROACH LEADING EDGE SLAT DISAGREE MESSAGE WITH AMBER LEADING EDGE LIGHT BETWEEN POSITION 1 AND 5 CAME ON. *S/D* LEADING EDGE SLAT ROTARY ACTUATOR FAILED. REPLACED POSITION NR 11 SLAT ROTARY ACTUATOR AND RETURNED TO SERVICE WITHOUT ANY FURTHER PROBLEMS.SDR 9707083236Actuator · lockedDURING APPROACH, THE LEADING EDGE SLATS REMAINED IN THE RETRACTED POSITION AFTER SELECTING FLAPS POSITON ONE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND SELECTED FLAPS POSITION THREE. TRAILING EDGE FLAPS EXTENDED NORMALLY. DECLARED AN EMERGENCY AND LANSDR DL72S970553Angle · crackedFOUND ON D1 LETTER CK, NR 8 SLAT ACTUATOR INBD AND OUTBD ATTACH ANGLES CRACKED. REPAIRED PER MM 57-20-21.SDR DHL9771294DActuator Mount · crackedDURING D-CHECK, THE NR 6 LEADING EDGE FLAP ACTUATOR MOUNT WAS FOUND CRACKED AT BOTH LOWER CORNERS. REMOVED AND REPLACED THE NR 6 L/E FLAP ACTUATOR MOUNT PER BOEING SRM 51-40-3.SDR DHL9771293DActuator Mount · crackedDURING D-CHECK, THE NR 5 LEADING EDGE FLAP ACTUATOR MOUNT BRACKET WAS FOUND CRACKED. REMOVED AND REPLACED INBOARD CORNER MOUNT BRACKET PER BOEING SRM 51-30-2.SDR DHL9771292DActuator Mount · crackedDURING D-CHECK, THE NR 2 LEADING EDGE FLAP ACTUATOR MOUNT WAS FOUND CRACKED AT THE OUTBOARD TOP CORNER AND INBOARD BOTTOM CORNER. REMOVED AND REPLACED ACTUATOR MOUNTS PER BOEING SRM 51-30-2.SDR EISA97075Actuator · failedNR 3 SLAT FAILED TO RETREAT. REMOVED AND REPLACED SLAT ACTUATOR AND SWITCH. (M)SDR DL72W970510Angle · crackedNR 8 SLAT ACTUATOR I/B AND O/B MOUNT ANGLES CRACKED. REPAIRED PER MM 57-20-21 FIG 808.SDR DL72W970506Angle · crackedOUTBOARD MOUNT ANGLE CRACKED NR 8 SLAT ACTUATOR. INBOARD MOUNT ANGLE CRACKED NR 8 SLAT ACTUATOR. REPAIRED PER MM 57-20-21 FIG 808.SDR DL72W970504Angle · crackedONE INCH VISIBLE CRACK AT INBD ATTACH ANGLE FOR NR 1 SLAT ACT. INSTALLED DOUBLER PER MM 57020-21 FIG 808.SDR CALA9700343Actuator · leakingAIRCRAFT LOST A-HYDRAULIC SYSTEM FLUID AFTER TAKEOFF. THE LOSS WAS ACCOMPANIED BY ILLUMINATION OF RUDDER SYSTEM A CAUTION LIGHT. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 KREUGER FLAP ACTUATOR LEAKING. THSDR DHL9771291DActuator Mount · crackedDURING D-CHECK, THE NR 1 SLAT ACTUATOR, INBOARD AND OUTBOARD MOUNTS WERE FOUND CRACKED. REPLACED MOUNTS PER BOEING S/B 727-57-130.SDR DL72W970464Angle · crackedFOUND DURING A-1 LETTER CHECK - 1 INCH VISIBLE CRACK NR 1 SLAT ACTUATOR INBOARD ATTACH BRACKET. REPAIRED PER M/M 57-20-21.SDR DL72S970522Mount Bracket · crackedFOUND DURING MV2F1, TOP I/B CORNER CRACKED ON NR 5 L/E FLAP ACTUATOR MOUNT BRACKET. FABRICATED REPAIR PER M/M 57-20-21 AND LEAK CHECKED.SDR DL72S970469Bracket · crackedDURING THE ACCOMPLISHMENT OF S.I. 4-57271-12 (S/B 727-57-0130, REV 2.) GAPS WERE DETECTED AT THE NR 1, NR 2, AND NR 7 SLAT ACTUATORS. THE WIDTHS OF THE GAPS ARE NR 1: 0.044 INCH; NR 2: 0.056 INCH; NR 7: 0.035 INCH. SHIMS WERE INSTALLED IN ACCORDANCE WITH BACSDR CALA9700347Angle · crackedINSPECTION FOUND A .75 INCH CRACK AT UPPER MOUNT BOLT OF NR 1 KREUGER FLAP ACTUATOR OUTBOARD UPPER SUPPORT ANGLE. A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR CA970314007Actuator · req adjustment(CAN) ON TAKEOFF SLAT AMBER LIGHT CAME ON AND #1 RH GREEN LOCK LIGHT WENT OUT FOLLOWED BY THE UNSAFE TAKEOFF WARNING HORN. TAKEOFF REJECTED. #1 SLAT ACTUATOR ADJUSTED.SDR HALA9717Actuator · slowFLT 1913 - HNL - A/C ROLLS WITH SLATS EXTENDED, AT 200 KIAS APPROXIMATELY ONE UNIT OF AILERON LEFT WING DOWN IS REQUIRED FOR NEUTRAL LOAD FEEL, WITH FLAPS EXTENDED SLIGHTLY LESS ROLL NOTICED. INSPECTED BOTH SLAT ASSEMBLY AND FOUND RIGHT SLAT SLOW TO EXTEND. SDR CA970318018Rotary Actuator · inoperative(CAN) LEADING EDGE SLAT LOCKED OUT. FOUND TORQUE LIMITER POPPED ON #5 AND #6 SLAT ACTUATORS ON LEFT HAND WING. ROTARY ACTUATOR REPLACED. OPERATION OF FLAPS CHECKED SERVICEABLE.SDR ABXA9700521Actuator Ftg · crackedDURING C-CHECK, THE RIGHT WING SLAT ACTUATOR INBOARD ATTACH FITTING WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 SRM 51-30-5.SDR 97UAL900159Actuator · failedLEADING EDGE SLAT DISAGREE MESSAGE AND LIGHT DURING CLIMB. RESET FLAP/SLAT ELECTRONIC UNIT (FSEU) BUT FAILURE OCCURRED AGAIN WHEN FLAPS MOVED. AIRCRAFT RETURNED TO FIELD. LEADING EDGE SLAT ROTARY ACTUATOR FAILED CAUSING THE EICAS MESSAGE. REPLACED ROTARY ACSDR DL72S970351Actuator · failedHYD SYS 'A' LOSS, CLIMBING THROUGH 8000 FT. OVERWEIGHT LANDING AT SEA 159,000 LBS, SMOOTH LANDING. FOUND NR 2 SLAT ACTUATOR END CAP BLEW OFF CAUSING LOSS OF 'A' SYS HYD FLUID. REPLACED SLAT ACTUATOR. PERFORMED OVERWEIGHT LANDING INSP PER M/M. REPLACED CASSDR CA970306009Actuator · tripped(CAN) ON APPROACH NO SLATS ON SELECTION, NO SLAT LANDING. 'A' AND 'C' SYSTEM FILTERS CLEANED. FOUND #3 AND #7 ACTUATORS TRIPPED, REPLACED.SDR TWAA9805602Bracket · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND NR 1 L/E SLAT ACTUATOR BRACKET CRACKED. INSTALLED DOUBLER PER SRM 51-10-01. (X)SDR TWAA9726003Bracket · crackedMCI - DURING OP-16, FOUND CRACKED LE SLAT ACTUATOR BRACKET, NR 1 SLAT. INSTALLED DOUBLER PER SRM 51-10-01. (M)SDR DL72W970263Actuator · failedLOST ALL HYD SYS A-PRESS AND FLUID 90 MILES FROM AIRPORT. USED ABNORMAL CHECKLIST. REPLACED RUPTURED NUMBER 3 SLAT ACTUATOR.SDR CA970306010Actuator · tripped(CAN) SLATS DID NOT EXTEND WHEN SELECTED. FOUND #6 ACTUATOR TRIPPED. REPLACED #6 SLAT ACTUATOR.SDR 9702843202Actuator · lockedDURING APPROACH WHILE SELECTING FLAPS 1, RECEIVED F/CTL SLATS LOCKED MESSAGE WITH THE WING TIP BRAKE ACTIVATED. COMPLIED WITH COCKPIT OPERATING PROCEDURES. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT WITH SLATS RETRACTED AND FLAPS 3. MAINTENANCE FOUNDSDR CA970306011Switch · intermittent(CAN) ON APPROACH WHEN FLAPS SELECTED SLATS DID NOT EXTEND. REPLACED SLAT POSITION INDICATION SWITCH.SDR DHL9774115CMount · crackedAT C-CHECK, NR 1 LEADING EDGE ACTUATOR MOUNT INBOARD CORNERS CRACKED AND OUTBOARD BOLTS PULLING THROUGH STIFFENER. REMOVED ACTUATOR, REMOVED DAMAGED MOUNT AND STIFFENER, FABRICATED MOUNT, 8 BY 6, INSTALLED SAME AND INSTALLED STIFFENER PER SRM 51-20-1 AND 51-3SDR DHL9774114CAngles · crackedAT C-CHECK, NR 3 SLAT ACTUATOR ATTACH ANGLES CRACKED AT FWD END. REMOVED AND REPLACED 2 ANGLES PER SRM 51-20-1 AND 51-30-2.SDR HALA97198Actuator · leakingHNL - FLT 158 - SLAT DISAGREEMENT LIGHT CAME ON UPON FLAP SELECTION FOR LANDING IN KOA. RECYCLED SLATS AND FLAPS. LIGHT CAME BACK ON AGAIN WITH SLAT EXTENTION. REPLACED LEFT WING SLAT EXTEND SWITCH AND LEFT WING TOP SLAT ACT CYL PER MM 27-80-5. LEAK CHECK SDR DL72S970045Actuator · failedSYSTEM-A QTY WENT TO 0, SYS-A HYD PUMPS WERE TURNED OFF PRIOR TO LOSING PRESS. TOWED FROM TAXIWAY. NR 5 LE FLAP ACT FAILED. REPLACED LE ACT, CHECK CASE DRAIN FILTERS OK.SDR EISA97001Actuator · inoperativeAFTER TAKEOFF WITH FLAPS RETRACTED NR 2 SLAT UNSAFE LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED SLAT ACTUATOR, OPS CHECK GOOD. (M)SDR WTAA970004Connector · moisture contamFAT - FLAP CONTROL FAULT ON CLIMB-OUT REPORTED. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE CLEANED WATER FROM OUTBOARD FLAP ACTUATOR CANNON PLUGS. OPERATIONAL CHECK AND TEST FLIGHT SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)SDR DHL9774006CActuator Mount · crackedAT C-CHECK, NR 5 LEADING EDGE FLAP ACTUATOR MOUNT IS CRACKED AT INBOARD CORNERS. REMOVED AND REPLACED ACTUATOR MOUNT AT L/E FLAP PER SRM 51-10-1, REPAIR 6.5 BY 8.SDR 96FDEA01708Actuators · iced upN 3 AND NR 4 LEADING EDGE FLAPS FAILED TO RETRACT FROM 2 DEGREES TO UP ON TAKEOFF. EXTENDED TO 5 DEGREES OK. LATER RETRACTION TO UP OK, THEN WENT INTERMITTENT WITH AIR SPEED INCREASE. DE-ICED LEADING EDGE ACTUATORS. OPERATIONAL CHECK OK.SDR DHL96705002Actuator · crackedSYSTEM-A HYDRAULICS SYSTEM FAILED ON DEPARTURE, QUANTITY WAS ZERO. FOUND NR 3 L/E SLAT ACTUATOR HOUSING CRACKED. REPLACED SAME.SDR 96UAL900959Bolt · shearedHYDRAULIC FLUID STREAMING FROM NR 5 SPOILER ACTUATOR. IT APPEARS THAT ONE OF THREE BOLTS HAS SHEARED FROM THE ACTUATOR CONTROL VALVE COVER ON THE LOWER AFT PART OF THE ACTUATOR. *S/D* BOLT FAILURE AT CONTROL VALVE COVER RESULTED IN SEAL DAMAGE AND LEAKAGE. SDR CALA9601860Actuator · leakingTHE A-HYDRAULIC SYSTEM WAS LOST WHILE EN ROUTE FROM IAH TO AUS. THE LOSS WAS ACCOMPANIED BY ILLUMINATION OF PUMP LOW PRESSURE LIGHTS 1 AND 2. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 5 L/E FLAP ACTUATOR SEAL
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