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 CALA2013111893018Actuator · faultyHYD LEAK ON RT WING FLAP AREA. FOUND RT SPOILER ACTUATOR LEAKING 13 DROPS PER MIN. SEE 0266010 FOR RT WING NR 4 SPOILER ACTUATOR REPLACEMENT. OPERATIONS & LEAK CHECKED GOOD IAW AMM.SDR CALA2013111893016Actuator · unknownR & R NR 4 SPOILER ACTUATOR IAW AMM27-64-44. ADJUSTED RT NR 4 SPOILER ACTUATOR IAW AMM 27-64-00. OPERATIONS & LEAK CHECKED GOOD.SDR CALA2013110792727Actuator · leakingHYD LEAK RT ENG PYLON. REPLACED NR 10 SPOILER PCA.SDR CA131105009Housing · cracked(CAN) SPOILER SERVO ACTUATOR ASSY ARRIVED AT OUR REPAIR FACILITY DISASSEMBLED. UPON INVESTIGATION IT WAS NOTICED THE MAIN HSG ASSY WAS CRACKED AT THE GLAND END OF THE PISTON BORE. VISUAL INSPECTION UNDER MICROSCOPE OF THE FRACTURED AREA SHOWED BEACH MARKS WHSDR CA140715008Manifold · mismanufactured(CAN) IN FATIGUE FAILURE TESTING AT THE MANUFACTURER, TWO MANIFOLDS FAILED BY AXIAL CRACKING ALONG THE ACTUATOR CENTERLINE. THE ROOT CAUSE OF THE FAILURE WAS TRACED TO BATCHES FROM A PARTICULAR SUPPLIER THAT PARKER USES. PART WAS NOT ON AN AIRCRAFT IN SERVISDR SWAA2013110521953Actuator · crackedDECLARED EMERGENCY HYDRAULIC A FAILURE. FOUND LT OTBD GROUND SPOILER ACTUATOR CRACKED. R & R BOTH FILTERS & SPOILER ACTUATOR IAW AMM.SDR OZCA20131031001Housing · crackedWARNING INDICATION ON EICAS, HYD SYSTEM NR 1 LOW. MX INSPECTED THE ACFT AND FOUND THE RT INBD GROUND SPOILER ACTUATOR HOUSING WAS CRACKED. UNIT REPLACED WITH REPAIRED UNIT AND ACFT RELEASED TO SERVICE.SDR CALA2013103092521O-Ring · damagedLT OTBD FLAP LEAKING FLUID FROM FOUR DRAIN HOLES UNDER WING. REPLACED LEAKING O-RING MOST OTBD SPOILER ACTUATOR LT WING, LEAKS CHECKED GOOD.SDR CALA2013101592072Servo Valve · leakingFLUID APPEARS TO BE LEAKING FROM THE SPOILER ACTUATOR ON THE 3RD ONE IN FROM THE LT WINGTIP. REPLACED ELECTROHYDRAULIC SERVOVALVE ON NR 3 SPOILER PCA IAW MM. OPERATIONS & LEAK CHECKED GOOD.SDR FDEA201310102466O-Ring · leakingTHREE HRS INTO FLT, STARTED LOSING HYD FLUID, SHOWED 1.4 GALLONS AFTER LANDING AT SHUTDOWN. FOUND O-RINGS LEAKING AT RT SPOILER SERVO ACTUATOR. REPLACED O-RINGS IAW SMP AND OPS LEAK CHECK IAW MM 27-01-20-04. ALL FAULTS, ALERTS EXTINGUSED. ACFT OK FOR SESDR CALA2013100991886Plug · looseHYD FLUID LEAKING FROM LT WING OTBD SPOILER ACTUATOR. FOUND UPPER PLUG ON ACTUATOR LOOSE. SECURED & LEAK CHECKED. NO LEAKS NOTED.SDR CA131008004Actuator · cracked(CAN) DURING TRANSIT CHECK, HYDRAULIC LEAK FOUND DRIPPING FROM LT WING INBD AND OTBD CANOE FAIRINGS. LEAK WAS TRACED TO THE RT OTBD SPOILER ACTUATOR FROM THE PISTON SEAL. ACTUATOR WAS REPLACED AND SYSTEM BLED IAW AMM 27-14-05 AND 27-14-00. LEAK CHECKS WERE CSDR CA131002002Actuator · fractured(CAN) TAXING FOR TAKEOFF AND WHILE PERFORMING FLIGHT CONTROL CHECKS, FLIGHT CREW NOTICED THAT THEY HAD LOST THE NR 1 HYD SYS. ACFT TAXIED BACK TO THE GATE WHERE A HYDRAULIC LEAK WAS NOTICED UNDER THE RT WING. A MAINTENANCE TEAM TRAVELED TO THE OUTSTATION ANDSDR CA130927002Actuator · fractured(CAN) THE FLIGHT CREW REJECTED TAKEOFF AT 30 KNOTS WHEN THEY LOST NR 1 HYDRAULIC SYSTEM PRESSURE, THE RUD ISO CAUTION LIGHT ALSO ILLUMINATED. THE NR 1 HYDRAULIC RESERVOIR QTY WAS NEAR ZERO. MAINTENANCE INVESTIGATION FOUND THE RT INBD ROLL SPOILER ACTUATOR HOSDR CA130920005Actuator · leaking(CAN) AN ACFT HAD A HYDRAULIC FLUID LOSS WHILE TAXIING OUT FROM AIRPORT. THE CREW REPORTED IT WAS THROUGH LT OTBD SPOILER ACTUATOR. ACFT RTS- SPOILER ACTUATOR REPLACED.SDR CALA2013090490979Warning System · false activationEICAS MESSAGE SPOILERS DISPLAYED. SPOILER LIGHT ILLUMINATED WITH SPOILERS SELECTED UP. LIGHT STAYS ON WITH SPEED BRAKE STOWED. ACP TEST OF SCM 1R MODULE FAULTED PCA XDR 1 OR 12 INT CRUISE. ACP TEST OF SPOILERS ALL OPERATIONS & INDICATIONS NORMAL. TESTED ACPSDR SWAA2013090519876Actuator · faultyAFTER TO FROM SAT MOST INBD FLIGHT RT WING SPOILER REMAINED UP 4-5 INCHES, REMAINED SO REST OF FLIGHT. R&R NR 6 SPOILER ACTUATOR IAW MM.SDR CA130903004Actuator · fractured(CAN) DURING MAINTENANCE, IT WAS NOTICED THAT THE LT OTBD ROLL SPOILER ACTUATOR WAS BADLY LEAKING. FURTHER INVESTIGATION REVEALED THE ACTUATOR CASING WAS FRACTURED. THE ACTUATOR WAS REPLACED, TESTED AND THE ACFT RELEASED FOR SERVICE.SDR COZA20130830031Actuator · leakingDURING INSPECTION, THE NR 10 FLIGHT SPOILER ACTUATOR WAS FOUND STATICALLY LEAKING FROM THE INPUT LINKAGE ASSEMBLY. OPERATING THE FLIGHT SPOILER WITH HYD POWER DID NOT CHANGE THE LEAK RATE. REPLACED ACTUATOR AND OPERATIONALLY CHECKED WITH NO LEAKS FOUND.SDR CALA2013081690480Packing · leakingNR 10 SERVO VALVE ON SPEED BRAKE ACTUATOR LEAKING. FOUND PACKING LEAKING FROM PLUG PORT. REPLACED PACKING, NO LEAKS NOTED.SDR HNAA2013062600369Actuator · failedIN FLIGHT, LEFT TURNS ARE EXTREMELY DIFFICULT, FOUR TIMES MORE FORCE TO TURN LT THAN TO TURN RIGHT. R & R LT INBD SPOILER ACTUATOR. OPS CHECKED GOOD.SDR HNAA2013062600361Actuator · inoperativeTAXIING ON BOTH ENGINES, FLIGHT/TAXI SWITCH SELECTED TO FLIGHT, ROLL SPOILER INBD CAUTION LIGHT ILLUMINATED, FOLLOWED BY NR 1 ISOLATION VALVE CAUTION LIGHT ILLUMINATED WITH HYD QTY OF .7. R & R INBD ROLL SPOILER ACTUATOR IAW MM 27-14-05. OPS AND LEAKED CHECKSDR UALA2013062504414Actuator · leakingSPOILER NR 11, SMALL HYD LEAK ON EXTENSION CHECK AND THERMAL RELIEF VALVE, 2 DROPS. REMOVED AND REPLACED NR 11 SPOILER ACTUATOR PER AMM, OPS AND LEAK CHECKED GOOD,SDR CA130625002Case · fractured(CAN) TAXING FOR TAKEOFF, FLIGHT CREW NOTICED THEY HAD LOST NR 1 HYD SYSTEM PRESSURE. DECISION WAS TAKEN TO SHUTDOWN THE LT ENGINE AND TO RETURN TO GATE. MAINTENANCE FOUND THE RT INBD ROLL SPOILER ACTUATOR CASING FRACTURED. THE ACTUATOR WAS REPLACED, TESTED SDR CA130617003Actuator · cracked(CAN) THE LT OTBD SPOILER ACTUATOR HAD BEEN REPLACED. DURING A MAINTENANCE FUNCTIONAL CHECK AFTER INSTALLATION, THE LT OTBD SPOILER ACTUATOR MADE A VERY LOUD NOISE DURING EXTENSION AND WOULD NOT RETRACT. VISUAL INSPECTION REVEALED THAT THE ACTUATOR HSG HAD FSDR SWAA2013062017448Actuator · shearedLT WING I/B SPOILER O/B ACTUATOR ROD END SHEARED. R&R ACTUATOR IAW MM.SDR SWAA2013061016930Actuator · shearedRIGHT WING NR 5 GROUND SPOILER INBD ACTUATOR ROD END SHEARED. R & R ACTUATOR IAW MM.SDR CA130606002Actuator · failed(CAN) IMMEDIATELY AFTER TAKEOFF THE ACFT ROLLED TO THE RT, UNCOMMANDED ROLL. THE FLIGHT CREW WERE ABLE TO LEVEL THE ACFT AND RETURNED TO THE DEPARTURE AIRPORT. FROM THE FDR READOUT IT IS CLEAR THAT THE RT OTBD ROLL SPOILER DID NOT RETRACT ON TAKEOFF. THE SPOISDR AALA20130606002Actuator · damagedLEFT WING SPOILER KNOCK DOWN ACTUATOR SQUIB PINS BENT. REPLACED LT WING SPOILER KNOCK DOWN ACTUATOR ASSY.SDR AALA20130531019O-Ring · damagedCREW REPORTED CENTER HYD QTY LOSS FOLLOWED BY CENTER HYD SYS PRESSURE EICAS MESSAGES. EMERGENCY DECLARED, FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND NR 4 SPOILER ACTUATOR FILTER PLUG LEAKING. REPLACED O-RING. SYS GROUND CHECK NORMAL SDR SWAA2013060316663Actuator · shearedLEFT WING INBD GROUND SPOILER OTBD ACTUATOR ROD END SHEARED. R & R ACTUATOR IAW MM.SDR SWAA2013052816491Actuator · brokenRIGHT WING NR 5 SPOILER INBD ACTUATOR BOTTOM MOUNTING LUG BROKEN. R & R ACTUATOR IAW AMM.SDR SWAA2013052816489Actuator · brokenRT WING NR 5 SPOILER OTBD ACTUATOR BOTTOM MOUNTING LUG BROKEN. R & R ACTUATOR IAW AMM.SDR SWAA2013062017438Actuator · brokenRT WING GROUND SPOILER OUTBOARD ACTUATOR BROKEN. R & R ACTUATOR IAW AMM.SDR UALA2013052403604Actuator · faultyREF CF0669, R & R NR 2 SPOILER PCA. SUP: R & R NR 2 SPOILER PCA REF AMM. NO LEAKS NOTED.SDR UALA2013052403603Actuator · leakingLT WING NR 3 SPOILER LEAKING. SUP: REF CF0668 NR 3 SPOILER PCA NEEDS TO BE REPLACED DUE TO LEAKAGE. NR 3 SPOILER ACT LEAKING 1 DROP PER MIN FROM SWIVEL FITTING. LEAK WITHIN LIMITS, REMOVED AND INSTALLED NR 3 SPOILER PCA. NO LEAKS NOTED NEED TO CONTINUE FROSDR SWAA2013052816495Actuator · leakingRIGHT WING NR 6 SPOILER ACTUATOR LEAKED. R & R NR 6 SPOILER IAW AMM.SDR SWAA2013052016214Actuator · leakingRIGHT WING T/E INBD GROUND SPOILER OTBD SPOILER ACTUATOR LEAKED. R & R ACTUATOR IAW AMM.SDR SWAA2013051516060Actuator · brokenLEFT WING INBOARD NR 4 GROUND SPOILER INBOARD ACTUATOR FWD ATTACH FITTING BROKEN. REMOVED AND REPLACED ACTUATOR PER M/M.SDR CA130508010Actuator · cracked(CAN) DURING TAXI FOR FLIGHT, THE CREW RECEIVED THE NR 1 ISO CAUTION LIGHT, ROLL INBD HYD CAUTION LIGHT RESULTING IN FLUID QUANTITY AT .5. ACFT RETURNED. MAINTENANCE ACTION FOUND THAT THE RT OTBD, SPOILER ACTUATOR LEAKING HEAVILY AND FOUND TO BE CRACKED. THSDR USAA2013052000032Eyebolt · corroded2S CHECK, FRETTING CORROSION ON NR 4 SPOILER BOLT ACTUATOR EYE-END BETWEEN WS874 TO WS1020 & BETWEEN RIB 16 TO RIB 19. REPLACED NR 4 SPOILER BOLT ACTUATOR EYE-END BOLT IAW SRM 57-70-00.SDR AALA20130423005Pca · leakingGYE - INFIGHT LIM-MIA CREW REPORTED CENTER HYDRAULIC SYSTEM FLUID LOSS. EMERGENCY DECLARED FLIGTH DIVERTED GYE LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER FOUR SPOILER POWER CONTROL ACTUATOR. SYSTEM GROUND CHECK NORMAL OPERATIOSDR SIMA20130417004Pcu · jammedON FLIGHT 4581 THE CREW REPORTED THAT DESCENDING THOUGH FLIGHT LEVEL 285 THE FLIGHT SPOILERS WERE EXTENDED AND THEY RECEIVED AN O/B FLT SPOILER CAUTION MESSAGE. VISUAL INSPECTION BY THE FLIGHT ATTENDANT VERIFIED THAT THE LEFT OPB SPOILERON WAS NOT FLUSH WITH SDR UALA2013041602605Packing · leakingEVIDENCE OF HYDRAULIC LEAK AT THE RIGHT WING FLAP WELL AREA. FOUND NR 10 SPOILER PCU LEAK COMING FROM SMALL PLUG. FOUND LEAKING HYD PORT CAP, REPLACED PACKING.SDR CA130424005Pcu · failed(CAN) CREW REPORTED SPOILERONS FAULT. ACFT ROLLED HARD RT 20 BANK, FOLLOWED BY A HARD LT 20 BANK THEN MODULATED LT AND RT WITH F/O STRUGGLING TO MAINTAIN STRAIGHT AND LEVEL FOR ABOUT 10 SECONDS. CREW DISENGAGED THE AUTOPILOT AND PROBLEM WENT AWAY FOR ANOTHERSDR UALA2013041502576Actuator · leakingCENTER HYD LEAK ON RIGHT WING SPOILER. FOUND NR 10 SPOILER PCA LEAKING FROM FILTER CASE. REPLACED PCA AS PER MM 27-61-02 ALL OPS AND INDICATIONS NORMAL NO LEAKS AFTER FUNCTIONAL TEST.SDR UALA2013041202522Actuator · leakingNR 10 SPOILER ACTUATOR LEAKING HYDRAULIC FLUID FROM ACTUATOR FILTER CAP. NR 10 SPOILER FILTER CAP FITTED WITH NEW SEALS FILTER CAP TIGHTENED AND WIRE LOCKED PER AMM. ACP FUNCTIONAL CHECKED, NO LEAKS DETECTED.SDR SWAA2013041214771Actuator · leakingRIGHT WING INBOARD GROUND SPOILER LEAKED. REMOVED AND REPLACED GROUND SPOILER ACTUATOR PER MM.SDR SIMA20130409006Actuator · defectiveON FLIGHT 4333 THE CREW REPORTED THAT DURING CLIMB ACCELERATING FROM 270KTS TO 300 KTS, A STRONG VIBRATION FELT THROUGH AIRFRAME, W COCKPIT AND THROUGH CONTROL WHEEL. AS A/C CLIMBED THROUGH APPROX 17,000 VIBRATION SLOWLY DECREASE TO MINIMAL VIBRATION AT CRUISSDR UALA2013040802354Actuator · failedREF CH5479, T-S PER FIM.27-09-00 PG126 FIG 105 FAILED BLOCK 14. RESISTANCE CHECK. NEED TO REPLACE 6 & 7 PCA. REMOVED AND REPLACED 6 & 7 PCA PER MM, OP'S CHECK'S GOOD.
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