JASC 2910
Service difficulty reports · 11,292
Reports filed under 2910 · Hydraulic System, Main, 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 = '2910' 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 = '2910' 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 SWIA200211191Hydraulic Line · leakingON DESCENT INTO PHX, HYD PUMP 1B CAUTION ILLUMINATED. CHECKED HYD SYNOPTIC PAGE. RESERVOIR 1 SHOWED WHITE WITH NO DATA (DASHED AMBER LINES) & HYD 1B PUMP AMBER, 1B THEN CYCLED FROM GREEN TO AMBER INTERMITTENTLY ON OR IN AUTO. AFTER LANDING, RESERVOIR READINSDR QXEA0201308O-Ring · leakingPDX - UPON LOWERING THE GEAR FOR LANDING, THE CREW RECEIVED AN AMBER GEAR DOOR LIGHT AND HYDRAULIC FLUID LOSS AND PRESSURE FLUCTUATION. THE CREW COMPLIED WITH EMERGENCY PROCEDURES, SHUT DOWN AND WAS TOWED TO THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT AND FSDR CA020830024Line · leaking(CAN) PILOTS REPORTED HYDRAULIC LEAK FROM LT NACELLE.LEAK TRACED TO NR 2 SYSTEM FLIGHT SPOILER UNLOADING HYDRAULIC LINE ON LT SIDE UNDER WING AREA. LINE REPLACED.SDR QXEA0201278Hydraulic System · contaminatedPDX - AIRCRAFT RETURNED TO FIELD WHEN AFTER TAKEOFF THE CREW RECEIVED A RUDD FULL PRESS CAUTION LIGHT FOLLOWED BY A RUDD PRESS CAUTION LIGHT. BOTH LIGHTS WENT OUT WHEN FLAPS WERE AT 15 DEGREES PRIOR TO LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND AISDR 373PA0005Hydraulic LineAfter departure, A/C experienced total loss of "A" system hydraulics, both quantity and pressure. A/C diverted, normal landing. Found hydraulic line to uplock actuator on Lt. gear broken. R&R hydraulic line.SDR AUS20020966Fitting · sheared(AUS) BRAKE SYSTEM MANIFOLD FITTING SHEARED. LOSS OF YELLOW' HYDRAULIC SYSTEM FLUID.SDR CA020828001Line · cracked(CAN) LOSS OF PRESSURE ON HYDRAULIC SYSTEM NR 2. HYDRAULIC LEAK LOCATED IN AFT EQUIPMENT BAY ONE DP NR 2 PRESSURE LINE TO PRESSURE MANIFOLD. FOUND LINE CRACKED.SDR 2002FA0001026Line · failedWHEN PILOT SELECTED GEAR DOWN AND PRESSURE WAS APPLIED TO DOWN HOSE. THE HOSE FAILED AT THE SWAGED END BLOWING ALL HYDRAULIC FLUID OVERBOARD. RECOMMEND CLOSER INSPECTION OF HOSES AND A MANDATORY TIME CHANGE OR BOTH HOSES. (PN S217840102) DOWN AND (PN S21784SDR MALA020471Pressure SwitchDURING LANDING ROLLOUT ON FLIGHT #3526, LOSS OF GREEN HYDRAULIC SYSTEM UPON LANDING ROLLOUT AND TAXI INTO GATE. MAINTENANCE FOUND #3 ENGINE DRIVEN HYDRAULIC PUMP PRESSURE SWITCH PN HE15258-1, SN 3704, FAILED INTERNALLY AT CANNON PLUG ATTACHMENT POINT. NEW SWISDR CA020826001Line · cracked(CAN) DURNING FLIGHT, PILOT REPORTED A HYD. SYSTEM NR 1 FAILURE. FLUID AND PRESSURE WENT TO ZERO. AFTER FURTHER INVESTIGATION IT WAS DISCOVERED THAT THE PRESSURE LINE FROM THE EDP WAS THE CAUSE OF THE LOSS OF FLUID. A/C TAT IS 2,110.6 AND TAC IS 1,809.HYSDR CA020821004Shuttle Valve · stuck(CAN) DOUBLE HYDRAULIC FAILURE PRIOR TO LANDING. AIRCRAFT STOPPED USING PARKING BRAKE JUST OFF END OF RUNWAY, WITH NO DAMAGE OR INJURY. NR 1 BRAKE UNIT FOUND LEAKING. NR 1 HYDRAULIC SYSTEM SHUTTLE VALVE FOUND STUCK OPEN ALLOWING DOUBLE HYDRAULIC SYSTEM FAISDR CA020820011Tube · cracked(CAN) SHORTLY AFTER DEPARTURE THE CREW NOTED ILLUMINATION OF THE RT HYDRAULIC LIGHT. A FEW SECONDS LATER THE LEFT HYDRAULIC LIGHT ILLUMINATED FOLLOWED BY A LOSS OF PRESSURE ON THE HYDRAULIC PRESSURE GAUGE. THE AIRCRAFT RETURNED TO BASE AND LANDED UNEVENTFULLYSDR IXXA0200050OO-Ring · damagedAFTER TAKEOFF FROM COF, THE FLIGHT CREW NOTICED A DROP IN THE HYDRAULIC QUANTITY AND THE OIL LOW LIGHT ILLUMINATED. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND RETURNED TO COF FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND LOCATED A DASDR AUS20020959Valve · faulty(AUS) NO1 HYDRAULIC SYSTEM INTEGRATED VALVE ASSEMBLY FAULTY.SDR 2002FA0000983Line · chafedDURING LANDING THE PILOT SELECTED GEAR DOWN, WITH NO RESPONSE FROM SYSTEM. THE PILOT SUCCESSFULLY PUT GEAR DOWN WITH EMERGENCY BLOW DOWN SYSTEM AND A SAFE LANDING WAS MADE. MAINTENANCE FOUND LEFT INBOARD PORTION OF WING COVERED IN HYDRAULIC FLUID. UPON REMOSDR 0202626626Fitting · looseDURING CLIMB, LOST FLUID FROM THE NR 4 HYDRAULIC SYSTEM AND THE OUTBOARD FLAPS DID NOT RETRACT. DECLARED AN EMERGENCY AND THE AIRCRAFT RETURNED TO NRT AND LANDED WITHOUT INCIDENT. TIGHTENED A FLEXIBLE HYDRAULIC PRESSURE LINE FITTING ON AFT SIDE OF THE ENGINESDR 0202635527Hydraulic Line · leakingJUST AFTER DEPARTURE FROM MSP, THE AIRCRAFT EXPERIENCED A COMPLETE LOSS OF HYDRAULIC FLUID FROM THE LEFT HYDRAULIC SYSTEM. AN EMERGENCY WAS DECLARED WITH ATC AND THE AIRCRAFT LANDED UNEVENTFULLY AND WAS TOWED FROM THE RUNWAY. REPLACED THE HYDRAULIC LINE AT TSDR AUS20020893Valve · leaking(AUS) HYDRAULIC SYSTEM NON-RETURN VALVE LEAKING. SUSPECT LEAK EMANATING FROM ENGRAVED PART NUMBER IN CASE.SDR QXEA0201213Flex Line · leakingSEA- AFTER GEAR EXTENSION, LOST NO.2 HYDRAULIC WITH ASSOCIATED CAUTION LIGHTS ILLUMINATED. ZERO HYDRAULIC FLUID AND ZERO HYDRUALIC PRESSURE WERE NOTED 5 MINUTES PRIOR TO ENGINE SHUTDOWN. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED AND FOUND MAIN LANDING GEAR DSDR CA020809002Limiter · cracked(CAN) SYSTEM "A" HYDRAULIC FAILURE ON SHORT FINAL. MAINTENANCE FOUND OUTBOARD FLAP FLOW LIMITING VALVE CRACKED. REPLACED.SDR PCAA0208087Hydraulic Line · leakingROC-DCA FLIGHT#3950. CREW REPORTED THAT THEY HAD INDICATION THAT #2 HYDRAULIC SYSTEM HAD LOST ALL FLUID. EMERGENCY DECLARED, AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND HYDRAULIC LINE BY FLAP MOTOR LEAKING. LINE REPLACED WITH AN INTERIM FLEX LISDR DL73K020922Hydraulic Line · leakingNR 2 ENGINE HYD PUMP RUPTURED THE PRESS LINE AND LOST ALL HYD QTY. FOUND RIGHT ENGINE HYD PUMP PRESS LINE LEAKING. REPLACED LINE. PULLED AND INSPECTED ALL SYSTEM AND CASE DRAIN FILTERS, NO TROUBLE FOUND. SERVICED HYD TO FULL. RAN ENGINE AND ELEC PUMPS. CSDR 2003FA0000087Line · failedLANDING GEAR HYDRAULIC FLUID HARD LINE FAILED DUE TO CRACKED FLARE UNDER (B) NUT CAUSING HYDRAULIC FLUID TO BE PUMPED OVERBOARD. RIGHT MLG AND NLG FAILED TO DOWN AND LOCK WITH EMERGENCY CO2 BOTTLE DEPLOYMENT. AIRCRAFT LANDED WITH THE RT MLG AND NLG UNLOCKED.SDR YENA200219Hydraulic System · lack of lubeAT JFK FLT 17, JFK TO FLL, ON TAKEOFF, B-HYDRAULIC SYSTEM LOW ECAM MESSAGE. ABORTED TAKEOFF AT APPROX 75 KTS, RETURNED TO GATE. FOUND BLUE SYSTEM LOW, FOUND NO EVIDENCE OF LEAK. SERVICED TO FULL, OPERATED ALL FLIGHT CONTROLS, UNABLE TO FIND LEAK AS PER AMM SDR AWXA200200691Solenoid Valve · leakingPHX - AIR TURNBACK - FLT 0081 - AFTER TAKEOFF FROM PHX EN ROUTE TO BWI DURING CLIMB ECAM INDICATED LOSS OF YELLOW HYDRAULIC PRESSURE AND FLUID. AIRCRAFT TURNED BACK TO PHX. MAINTENANCE FOUND THE 3150GP HYDRAULIC SOLENOID VALVE LEAKING AND REPLACED VALVE IAW SDR CA020806004Tube · deformed(CAN) OPERATOR PURCHASED A/C FROM COMMERCIAL OPERATOR & INHERITED PERSISTENT & ELUSIVE HYD LEAK. AFTER TROUBLESHOOTING, SOURCE ISOLATED TO TWO B-NUTS NOT TIGHT. FITTINGS WERE NOT ACCESSIBLE. 5 CYCLES LATER NR 13 HYDRAULIC LINE FAILED ON GEAR RETRACTION EMPSDR DL777030715Flex Line · leakingATB CTR HYD SYS FAILED-MTC MSG 29-10150 CTR HYD QTY LOW FLEX LINE GOING TO THE RT MLG STEERING ACT LEAKING (P/N AS4568G0580SS)- REPLACED LINE.SDR QXEA0201104Hydraulic Line · leakingPDX- DURING TAXI, UPON TRANSFER OF HYDRAULIC FLUID FROM NR 2 SYSTEM TO NR 1 SYSTEM, LOST ALL FLUID FROM NR 1 NACELLE. REMOVED AND REPLACED BRAKE LINE AND RESERVICE BOTH HYDRAULIC SYSTEMS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR AWXA200200692Shuttle Valve · faultySLC - EMERGENCY LANDING - FLT 0454 - ON SHORT FINAL APPROACH AT SLC EN ROUTE FROM PHX LOST A-SYSTEM HYDRAULIC QUANTITY AND PRESSURE. AIRCRAFT SHUT DOWN AND TOWED TO GATE. MAINTENANCE FOUND THE NR 1 THRUST REVERSER SHUTTLE VALVE HAD A BLOWN PLUG, REMOVED AND SDR PCAA0208085Actuator · crackedPHL-FLIGHT#3686. CREW REPORTED LOSS OF #1 HYDRAULIC SYSTEM FLUID JUST AFTER TAKEOFF.EMERGENCY DECLARD, AND AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED AIRCRAFT AND FOUND INBOARD RIGHT ROLL SPOILER ACTUATOR CRACKED AND LEAKING. INBOARD RIGHT ROLL SPOILER SDR AUS20020811Line · failed(AUS) MAIN LANDING GEAR ACTUATOR HYDRAULIC LINE PN 65C26809-3172 RUBBING ON SPOILER HYDRAULIC LINE PN 65C26809-3072. SPOILER LINE LEAKING. LINES ARE LOCATED IN THE LT UNDERCARRIAGE BAY ABOVE THE MAIN LANDING GEAR.SDR 2002FA0000984Line · deterioratedTHE AIRCRAFTS NOSE GEAR FAILED TO EXTEND DURING ROUTINE TRAINING FLIGHT. A/C MADE LANDING WITHOUT NOSE GEAR EXTENDING. PILOT WAS ABLE TO FEATHER RIGHT ENGINE BUT LEFT SUFFERED A MINOR PROP STRIKE. INSPECTION OF A/C ON THE RUNWAY REVELED THAT GEAR WAS FREE TSDR ZW0A0208301Hydraulic System · leakingHYD FLUID LEAK INTO APU INLET RESULTING IN SMOKE IN THE CABIN. RETURNED AIRCRAFT TO THE GATE. CHANGED WATER SEPARATORS AND PERFORMED MD9-49-06. PAC BURNOUT OP CHECK.SDR IU62002F00025Housing · crackedACTUATOR HOUSING IS CRACKED UNDER THE RETRACT PORT.SDR PCAA0207083O-Ring · damagedPHL - FLIGHT 3957 CREW REPORTED NR 2 HYDRAULIC CONTENTS DROPPED TO ZERO AND NR 2 HYDRAULIC PRESSURE DROPPED TO ZERO AFTER 5 MINUTES IN FLIGHT. NO PRESSURE FOR 10 MINUTES. MAINTENANCE INSPECTED NR 2 HYDRAULIC PUMP AND FOUND O-RING ON PRESSURE UNION DAMAGED. SDR IU62002F00017Cover · crackedCOVER CRACKED.SDR HEEA080683Sleeve · leakingLEAKED EXTERNALLY APPROX. 1 EA. TEASPOON UNDER PROOF PRESSURE TEST AT INNER SPOOL WITHIN 3 MINUTES.SDR HEEA080645Hose · failedPRESSURE HOSE FROM THE HYD PUMP TO AN AIRFRAME HAND LINE FAILED INTERNALLY IN FLIGHT CAUSING LOSS OF HYD FLUID. SCRAPPED.SDR MEX2002248Line · damagedON DEPARTURE, CAPTAIN REPORTED THE PRESENCE OF SMOKE IN THE PASSENGER CABIN. THE HYDRAULIC SYSTEM WAS VERIFIED TO BE LEAKING AND THE APU WAS SHUTDOWN DUE TO HYDRAULIC FLUID IN IT, AND THE A/C PACK WAS CONTAMINATED. HYDRAULIC LINE OF THE RT REVERSE FILTER WASDR IU62002F00023Housing · crackedVALVE HOUSING CRACKED AT MOUNTING HOLE.SDR PCAA0207082O-Ring · cutMDT-FLIGHT 3963. CREW REPORTED LOSS OF HYDRAULIC SYSTEM AND NR 1 QUANTITY IN FLIGHT WITH RUDDER ISOLATION VALVE LIGHT, FOLLOWED SHORTLY AFTER NR 1 HYDRAULIC PUMP, NR 1 HYDRAULIC PRESSURE, RUDDER PRESSURE AND FULL RUDDER PRESSURE LIGHTS ILLUMINATED. ZERO QUANSDR PCAA0207081Hydraulic Line · leakingSYR-FLIGHT#3992. CREW REPORTED #2 HYDRAULIC ISOLATION VALVE CAUTION LIGHT ILLUMINATED IN FLIGHT, LANDING GEAR ALTERNATE EXTENSION PERFORMED. MAINTENANCE INSPECTED AND FOUND HYDRAULIC LINE FROM DOGBONE ON LEFT FORWARD GEAR LEAKING. INTERIM FLEX LINE INSTALLED. SDR SWAA021697Fuse · malfunctionedAIR TURN BACK, AFTER TAKEOFF, LEADING EDGE DEVICES FAILED TO RETRACT. RESET B-SYSTEM L/E DEVICE HYD FUSES PER MM. OPS CK GOOD PER MM.SDR 2002F00888B-Nut · looseDURING CRUISE SYSTEM 'A' HYDRAULICS FAILED, PRESSURE WENT TO ZERO. AIRCRAFT DIVERTED TO SAP AND LANDED SAFELY, FOUND SYSTEM 'A' PRESSURE LINE B-NUT LOOSE TIGHTENED SAME SERVICED HYD AND OPS CHECK GOOD PER MM 29-11. AIRCRAFT RETURNED TO SERVICE. (M)SDR AALA20021081Seal · leakingIN CRUISE, LEFT HYD QTY LOW ON EICAS FOLLOWED PROCEED TO DEPRESS SYSTEM EXTENDED GEAR AND FLAPS USING ALTERNATE SYSTEM. REPLACED WORN SEAL ON FLAP/SLAT DEPRESSURIZATION CONTROL MODULE SOLENOID. SERVICED HYDRAULIC LT SYSTEM TO NORMAL PRESS, LT HYDRAULIC SYSTESDR CA020726012Line · leaking(CAN) HYDRAULIC LEAK IN NOSE AREA.NOSE LANDING GEAR DOOR SOLENOID VALVE LINE FOUND LEAKING. LINE REPLACEDSDR DL73K020871Hydraulic Line · blownLOSS OF A-HYD SYS WHEN LANDING GEAR HANDLE WAS LOWERED. BOTH LOW PRESS A-SYS LIGHTS ILLUM AND HYD QTY GAUGE WENT TO ZERO. LOUD BANG WAS HEARD WHEN GEAR WAS LOWERED. FOUND NOSE GEAR MAIN ACTUATOR PRESS LINE BLOWN. INSTALLED REPLACEMENT HYD LINE PER MM, HYD SDR IU62002F00021Housing · crackedACTUATOR HOUSING IS CRACKED OUT, 2ND SHOULDER ON THE RETRACT SIDE.SDR PCAA0207080Actuator · cracked#1 HYDRALIC ISOLATION VALVE LIGHT ILLUMINATED PRYER TO FLIGHT, HYD RIGHT LEFT WING. INSPECTED AND FOUND RIGHT INBOARD ROLL SPOILER ACTUATOR BODY CRACKED AND LEAKING. REMOVED AND REPLACED ACTUATOR I.A.W. -8 MAINT MANUALL 27-14-05. OPPS AND LEAK CHECKS OK.SDR CHQ000182Pressure Switch · failedHYD 1 LO QTY AND ENG 1 HYD PUMP FAIL, THEN HYD FLUID WAS GONE AND ELECTRICAL PUMP MAKING TERRIBLE NOISE, THEN HYD 1 SYSTEM FAILED. REMOVED AND REPLACED BRAKE PRESSURE SWITCH. BLED HYD SYSTEM, OPS CHECK GOOD.
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