JASC 2761
Service difficulty reports · 1,071
Reports filed under 2761 · Drag Control 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 = '2761' 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 = '2761' 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 SWAA2015032637850Actuator · leakingRIGHT WING NR 5 FLIGHT SPOILER ACTUATOR LEAKED. R & R ACTUATOR IAW MM.SDR UIEA2015032100184Actuator · brokenBLOCK TURN BACK, LT SPOILER INDICATION DOES NOT MOVE FOR FLIGHT CONTROL CHECK. FOUND NR 4 SPOILER ACTUATOR ROD BROKEN. R & R NR 4 SPOILER ACTUATOR. OPERATIONAL & LEAK CHECKED OK IAW MM 27-61-05. LEFT SPOILER INDICATION OPERATES NORMAL.SDR ASMF201503019Actuator · failedAIRCRAFT RETURNED TO PLATFORM DUE TO TAKEOFF CONFIGURATION ALARM WAS ACTIVE. PERFORMED BITE TO FSEU IAW FIM 31-51 TASK 801, NO CONFIRMING FAILURE, TESTED CORRECT. THE ACFT WAS SENT TO THE HANGAR & AS PRECAUTIONARY ACTIONS, THE AUTO SPEED BRAKE ACTUATOR WAS RSDR SIMA20150220003Actuator · failedUPON DESCENT, THE SPEED BRAKES WERE OPENED WHEN COMMANDED TO CLOSE. THE ACFT EXHIBITED A PRONOUNCED BUT CONTROLLABLE ROLL TO THE RT, FOLLOWED BY SPOILER FAIL MSG ON EICAS. AFTER 15 - 20 SECS THE ACFT RETURNED TO NORMAL CONFIG & THE SPOILER FAIL MSG EXTINGUISSDR CA150204009Cylinder · leaking(CAN) THE MFS PCU GT411-6001-9 CYLINDER, PN 376340-7, BASE RADIUS WAS FOUND OUT OF SPEC, OVERSIZED RELIEF IN THE BOTTOM OF THE CYLINDER BORE, CAUSING PISTON SEAL DAMAGE. THIS DEFECT CREATES A HYD FLUID BYPASS CONDITION THAT COULD RESULT IN A REDUCTION IN HINGSDR A6WA201542324Warning System · activatedON DIVERSION RECEIVED GLD UNSAFE CAUTION. QRH PROCEDURE COMPLIED WITH. MSG CLEARED BUT FLIGHT SPOILERS GO INTERMITTENT DEPLOYMENT ON FLIGHT CONTROL PAGE WITH HYD SYS PRESSURIZED.SDR CA150113028Manifold · failed(CAN) CREW REPORTED ON TAXI CHECK OUT OF VANCOUVER GROUND SPOILERS WOULD NOT RETRACT - TROUBLESHOOTING CARRIED OUT USING CL605 WM 27-61-00 AND ROCKWELLCOLLINS PSEU SENSOR DISCRETE DATA LABEL 271-274, LABEL 274 BIT 28 FOUND AT 0 INDICATING NO RETURN HYDRAULIC PSDR AALA20141214003Actuator · defectiveAIR INTERRUPT, RETURNED & EMER DECLARED. LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB AN EICAS SPOILERS MSG WAS RECEIVED. DURING RETURN SPOILERS WERE ARMED FOR LANDING & DEPLOYED NORMALLY. BITE OF 2R MODULE INDICATES NR 3 PCA REQUIRES REPLACEMENTSDR USAA2014120800002Actuator · inoperativeDURING DECENT FROM FL 280, RECEIVED A FLIGHT CONTROL SPOILER FAULT ON ECAM. SPOILERS FELT EXTENDED. TROUBLESHOOTING IAW TSM 27-60-00-810-817A. SUSPECT RSPLR 1 SERVO 31CE2. REPLACED NR 1 RIGHT WING SPOILER ACTUATOR IAW AMM 27-64-51-400-004-A. OPS CHECKED SDR CA141031009Actuator · failed(CAN) ON APPROACH FLIGHT EXPERIENCED A SPOILER CONTROL FAULT. A RESET WAS ATTEMPTED BUT WAS UNSUCCESSFUL. WITH WET RUNWAYS, THE CREW ELECTED TO DECLARE A PAN WITH ATC. THE LANDING WAS UNEVENTFUL AND THE ACFT TAXIED TO THE GATE. THE CREW REPORTED THAT THERE WASDR CA141028004Actuator · fractured(CAN) THE NR 1 HYD ISO LIGHT ILLUMINATED DURING TAXI WITH ASSOCIATED LOSS OF NORMAL BRAKES AND LOSS OF NR 1 HYDRAULIC SYSTEM SERVICES DUE LOSS OF FLUID. THE LT INBOARD ROLL SPOILER ACTUATOR WAS FOUND LEAKING DUE TO A FRACTURE OF THE HOUSING. THE ACTUATOR WAS RSDR SIMA20140921006Actuator · malfunctionedDURING DESCENT WHILE USING SPEED BRAKE THE ACFT ROLLED LT FOLLOWED BY SPOILER FAIL EICAS MSG, THIS WAS MOMENTARY. R & R RT SPEED BRAKE ACTUATOR IAW AMM 27-62-02. OPERATIONS CHECKED GOOD. LEAK CHECKED GOOD.SDR AALA20140825002Actuator · leakingLEFT HYD QTY EICAS WITH RESERVOIR LIGHT. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED NR 8 SPOILER ACTUATOR. SYS GND CHECKED NORMAL OPERATION CLOSED.SDR CA140818019Actuator · failed(CAN) RT SCOOP ACTUATOR END CAP FAILED ACTUATOR REPLACED.SDR AALA20140811002Actuator · leakingLOSS OF CTR HYD QTY. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED NR 5 SPOILER ACTUATOR. SYS GND CHECKED NORMAL OPERATION CLOSED.SDR ERAA201408010047Actuator · crackedNUMBER 1 HYD ISO VLV, ROLL SPOILER INBD, FLAP POWER CAUTION LIGHTS WITH LESS THAN MIN NR 1 HYD FLUID. FLAPS REMAINED AT 5 DEGREES. FOUND RT INBD ROLL SPOILER ACTUATOR HOUSING CRACKED. R & R INBD ROLL SPOILER ACTUATOR IAW MM 27--14-05. RIGGING NOT AFFECTED,SDR SAJF2014072203024Actuator · malfunctionedAIRCRAFT RTO DUE TO SPEED BRAKE DO NOT ARM LIGHT ILLUMINATED AFTER TAKEOFF THRUST SET. CREW INFO RTO IAS 70 GROSS WEIGHT 148000 LBS WITHOUT USING REVERSE. LIGHT EXTINGUISHED DURING DECELERATION. PFM AACU BITE TEST NO FAULT FOUND. BITE TEST SMYD 2 FOUND FAUSDR AALA20140718010Actuator · leakingRT HYD QTY SYS LOSS FOLLOWED BY RT HYD QTY EICAS MSG & RESERVOIR LIGHT ON OVERHEAD ILLUMINATED. EMER DECLARED FLIGHT DIVERTED LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND HYD FLUID LEAKING FROM NR 2 SPOILER ACTUATOR. REPLACED NR 2 SPOILER POWSDR ERAA20140044Actuator · leakingHYDRAULIC FLUID LEAKING FROM DRAIN HOLES ON WING FLAP FAIRINGS WITH NR 2 ENG RUNNING. R & R LT OTBD ROLL SPOILER ACTUATOR IAW MM 27-14-05. RIGGED IAW 27-14-00. LEAK & OPS CHECKED GOOD.SDR SWAA2014062329303Actuator · out of adjustLEFT WING NR 4 GND SPOILER OTBD ACTUATOR OUT OF ADJUSTMENT. R & R ACTUATOR IAW AMM.SDR SWAA2014062329302Actuator · brokenLEFT WING NR 4 GND SPOILER INBD ACTUATOR BROKEN. R & R SPOILER IAW AMM.SDR CA140610006Pcu · failed(CAN) INBD SPOILER MESSAGE, REPEAT, DECLARED EMERGENCY.SDR ASMF2014061806015Linkage · out of adjustCAPTAIN REPORTED THAT DURING DESCENT TO EXTEND THE SPEED BRAKES, THE RT SPOILERS HIGHER THAN LT SPOILERS. ACFT WAS SENT TO THE HANGAR & PERFORMED ADJUSTMENT OF SPOILERS ACTUATORS SYS LINKAGES IAW AMM 27-61-00-820-801 & FLIGHT SPOILERS SYS TEST WAS PERFORMED IASDR SWAA2014051227880Casting · crackedNUMBER 5 GND SPOILER CASTING BROKEN AT OTBD ACTUATOR MOUNT. R & R SPOILER ASSEMBLY IAW MM.SDR SWAA2014051227879Casting · crackedRIGHT INBD GND SPOILER ACTUATOR CASTING CRACKED. REPAIRED CASTING IAW SRM.SDR CALA2014050690972Seal · damagedHYD CTR SYS LOSS OF QTY AT GR EXTENSION. REPLACED LEAKING NR 10 SPOILER ACTUATOR FILTER HOUSING SEAL MM27-61-01. LEAK CHECKED NORMAL & C SYS REPLENISHED.SDR CA140423008Actuator · cracked(CAN) DURING GROUND RUNS FOR UNRELATED MAINTENANCE WORK, IT WAS NOTED THAT THE LT OTBD SPOILER WAS NOT MOVING. MAINTENANCE DISCOVERED THAT THE LT OTBD ACTUATOR HOUSING HAD FRACTURED AT THE END CAP RESULTING IN A LEAK. THE ACTUATOR WAS REPLACED IAW THE AMM, PNSDR CA140429005Housing · cracked(CAN) TAXIING FOR TAKEOFF, GOING THROUGH THE TAKEOFF CHECKLIST AND SELECTING THE FLIGHT TAXI SWITCH TO FLIGHT, THE RT OTBD SPOILER WOULD NOT DEPLOY UPWARDS. CREW RETURNED TO TERMINAL AND CONTACTED MAINTENANCE. MAINTENANCE INSPECTED THE PLANE AND CONFIRMED THSDR CA140416003Pcu · failed(CAN) THE CAPTAIN NOTIFIED THEIR DISPATCHER THAT THEY DECLARED AN EMERGENCY DUE TO A RUDDER CONTROL MALFUNCTION AND THEY DIVERTED TO AN ALTERNATE AIRPORT. AFTER SPEAKING WITH THE CAPTAIN, HE MENTIONED THAT THE ACFT WAS UNCONTROLLABLE CAUSING THE LEFT WING TO SDR SIMA20140410001Warning System · false activationUPON SELECTING FLT SPOILER DURING DESCENT RECEIVED OTBD SPOILERON & OTBD FLT SPOILER CAUTION MSG. PERFORMED SPOST 1 & SPOST 2 TEST IAW MM 27-60-05, OPERATIONS CHECKED NORMAL.SDR SWAA2014032726566Actuator · leakingLEFT WING NR 2 FLIGHT SPOILER ACTUATOR LEAKED. R & R ACTUATOR IAW AMM.SDR SWAA2014032726565Actuator · leakingRIGHT WING NR 7 FLIGHT SPOILER ACTUATOR LEAKED. R & R ACTUATOR IAW AMM.SDR SWAA2014032626530Actuator · leakingLEFT WING NR 1 SPOILER HYD ACTUATOR LEAKED. R & R ACTUATOR IAW AMM.SDR CALA2014032490688Pca · malfunctionedSPOILERS EICAS MSG & OVERHEAD LIGHT ON. REPLACED NR 3 SPOILER PCA IAW AMM 27-61-02, OPERATIONS TESTED OK.SDR SWAA2014032026274Actuator · out of adjustRIGHT WING NR 5 GND SPOILER OTBD ACTUATOR ROD END OUT OF ADJUSTMENT. R & R ACTUATOR IAW AMM.SDR SWAA2014031025908Actuator · leakingRT WING NR 6 SPOILER ACTUATOR LEAKED. R & R ACTUATOR IAW AMM.SDR SWAA2014030425736Actuator · leakingLT WING NR 2 FLIGHT SPOILER LEAKED. R & R ACTUATOR IAW AMM.SDR SWAA2014031025917Actuator · leakingLT WING NR 2 SPOILER ACTUATOR LEAKED. R & R ACTUATOR IAW AMM.SDR SWAA2014012024266Actuator · faultyAIR TURN BACK DECLARED EMERGENCY LOST HYD SYSTEM A AT APPROXIMATELY 2000 FT AGL. LOW PRESS HYD ENG A ILLUMINATED & THEN A SYSTEM HYD, QUANTITY WENT TO ZERO. R & R NR 3 FLIGHT SPOILER ACTUATOR IAW MM.SDR GTIA201401131112Actuator · corrodedCORROSION FOUND AT WING OVERHANG LT NR 3 SPOILER ACTUATOR. WORK ACCOMPLISHED IN NON ROUTINE7281N00209 IAW EO 5750-1401.SDR CA140106004Housing · fractured(CAN) DURING THE FLIGHT CONTROL CHECK PRIOR TO TAKEOFF, THE CREW NOTED THAT THE LT OTBD ROLL SPOILER WAS NOT INDICATING ANY MOVEMENT ON THE PFCS INDICATOR. MAINTENANCE INVESTIGATION FOUND THE LT OTBD ROLL SPOILER ACTUATOR HOUSING FRACTURED AND LEAKING. THE ROSDR HNAA2013122600639Actuator · leakingDURING TAXI, HYDRAULIC FLUID LEAKING FROM RT WING. LOST NR 1 HYDRAULIC QTY AND ISOLATION LIGHT ILLUMINATED. R & R RT INBD ROLL SPOILER ACTUATOR IAW AMM 27-14-05. OPS CHECKED GOOD.SDR SWAA2013122323608Actuator · leakingHYD A SYS FAILURE. BOTH PUMPS LOW PRESSURE LIGHTS CAME ON & FLUID DRIPPING FROM APPROXIMATELY UNDER NR 2 SPOILER. R & R NR 1 GND SPOILER ACTUATOR IAW MM.SDR CA131219012Lock · cracked(CAN) DURING SCHEDULED INSPECTION, MAINTENANCE PERSONNEL NOTED THAT THE LOCKWIRE ATTACHMENT TABS ON BOTH RT WING GROUND SPOILER ACTUATORS WHICH SECURE THE LENGTH ADJUSTMENT JAM NUT WERE BROKEN OFF. THE LOCKING DEVICES WERE REPLACED WITH SERVICEABLE PARTS IAW SDR SWAA2013121823484Actuator · leakingLT WING GND SPOILER INBD ACTUATOR LEAKING. R & R ACTUATOR IAW MM.SDR CA131213004Actuator · cracked(CAN) PILOT REPORTED THAT LT OTBD ROLL SPOILER WILL NOT EXTEND BUT THE INBD IS OK. MAINTENANCE DISCOVERED THAT THE LT OTBD ACTUATOR HSG WAS CRACKED. THE ACTUATOR WAS REPLACED IAW THE AMM AND THE ACFT RETURNED TO SERVICE, PN A44700-009, SN 0186.SDR SWAA2013120322937Actuator · brokenNR 4 GROUND SPOILER INBD ACTUATOR ATTACH FITTING BROKEN. R & R ACTUATOR IAW MM.SDR CA131126009Actuator · fractured(CAN) CREW REPORTED LOSS OF BRAKE PRESSURE WITH THE SELECTION OF SPOILERS ALSO THE HYDRAULIC ISO VALVE LIGHT CAME ON. VISIBLE HYDRAULIC LEAK IN THE LT WING/NACELLE AREA. MAINTENANCE DISCOVERED THAT THE LT, INBD SPOILER ACTUATOR HOUSING WAS FRACTURED. THE ACTUSDR CALA2013112193160Actuator · faultyCREW REPORTS THAT DURING TEST FLT THE NR 1 SPOILER FLOATED APPROXIMATELY 6 INCHES WITH THE CTR HYD SYS DEPRESSURIZED. NR 1 SPOILER ACT CHANGED IAW PTT 4952017, OPERATIONS CHECKED NORMAL IAW MM.SDR CALA2013112293201Actuator · faultyNR 6 SPOILER FLOATED DURING TEST FLIGHT. R & R SPOILER ACTUATOR IAW AMM 27-61-02 ON NR 36598.
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