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 0500189947Line · leakingDURING FLIGHT, THE AIRCRAFT LOST PRESSURE AND A TOTAL LOSS OF FLUID FROM THE RIGHT HYDRAULIC SYSTEM. COMPLIED WITH COM PROCEDURES AND AIRCRAFT CONTINUED TO ORIGINAL DESTINATION. THE LANDING AT BTR WAS UNEVENTFUL. MAINTENANCE FOUND A LINE COMING FROM THE ELESDR CA050217005Selector Valve · intermittent(CAN) YAW DAMPER KICKED OFF UNCOMMANDED, GEAR SELECTED DOWN WITH NO FUNCTION, IT WAS NOTICED THAT L/G CNTRL C/B WAS TRIPPED, RESET, LANDING WAS UNEVENTFUL. PILOTS CONTINUED, C/B WAS TRIPPED WITH YAW DAMP ON. YAW DAMPER WAS DISENGAGED, C/B RESET, GEAR SELECTSDR 2005FA0000342Powerpack · failedAC DEPARTED, DIVERTED, PILOT THOUGHT THAT HIS LANDING GEAR WAS NOT FULLY IN THE UP AND LOCK POSITION (UNKNOWN IF GEAR UNSAFE LIGHT WAS ON). PILOT SELECTED GEAR DOWN, NOTHING HAPPENED, PULLED EMERGENCY GEAR EXTENSION AND LANDED WITH NO FURTHER INCIDENT. MAINTSDR SWAA050370B-Nut · looseA-SYSTEM HYDRAULICS FAILED. RECONNECTED NR 1 ENGINE HYDRAULIC SUPPLY LINE B-NUT PER MM.SDR HALA0500175Fuse · failedFLT 113 - HNL - AT PUSHBACK, WHEN STARTING LEFT ENGINE, GOT LEFT HYD PRESSURE AND QUANTITY TO '0' LINE SERVICE CONFIRMED LEFT HYD FLUID ON RAMP. FOUND LT LOWER FORWARD QTY LIMITER FUSE HOUSING CRACK. REMOVED AND REPLACED QTY LIMITER FUSE PER MM 32-44-10-4. SDR CA050208006Tube · leaking(CAN) DURING CLIMB THROUGH 10,000 FEET, THE NR 2 HYD QUANTITY GAUGE DECREASED, NR 2 HYD ISO VALVE CAUTION LIGHTS ILLUMINATED. AIRCRAFT ELECTED TO RETURN TO DEPARTURE AIRPORT, ALTERNATE GEAR EXTENSION SYSTEM USED. NORMAL LANDING. MAINTENANCE INSPECTION FOUNDSDR CA050207004Hydraulic System · failed(CAN) THE HELICOPTER WAS ON A INTERNATIONAL JOB. THE INITIAL REPORT FROM FLIGHT OPERATIONS IS HYDRAULIC FAILURE. THE AIRCRAFT WAS IN A HOVER WHEN IT YAWED TO THE RT. THE AIRCRAFT LANDED HARD ENOUGH TO DAMAGE ONE ARM OF THE MAIN ROTOR STAR AND THE TAILBOOM HSDR ASMF200502003Valve · leakingDURING TRANSIT CHECK WERE DETECTED HYDRAULIC LEAK AT RIGHT MAIN LANDING GEAR IN VALVE LOCKOUT. THE VALVE LOCKOUT WAS REPLACED IAW MM 32-42-06, TESTED CORRECT. CORRECT, DEFERRED REPORT WAS CLOSEDSDR DXTA200500665Manifold · bypassingON DESCENT THROUGH 17,000 AND 330 KTS IAS, GEAR UNLOCK LIGHT ILLUMINATED FOLLOWED BY THE GREEN NOSE GEAR LIGHT THEN BOTH EXTINGUISHED. THUD WAS FELT AND HEARD BY CREW. TROUBLESHOT DISCREPANCY TO A INTERMITTENLY FAILING LANDING GEAR CONTROL VALVE. REMOVED VASDR DXTA200500579Line · chafedFL 200 ON CLIMBOUT LOST LEFT HYDRAULIC SYSTEM FOLLOWED BY THE PTU. TURNED ON "A" PUMP LOST THAT ALSO. ON DESCENT LOST RIGHT SYSTEM. BLEW DOWN THE GEAR, USED EMERGENCY BRAKES. SIGNIFICANT SMOKE IN THE COCKPIT. CLEANED ALL HYDRAULIC FLUID. REPLACED HYDRAULSDR P5CA0501314Line · crackedLOSS OF NR 3 HYDRAULIC FLUID. TROUBLESHOT AND FOUND NR 3 EDP PRESSURE LINE UNDER THE GAP PANEL CRACKED. REPLACED LINE WITH FLEX LINE PER GMM 3-17-1, COI 450-017. OPS & LEAK CHECK OK PER 20-11-18.SDR 05FDEA00242Line · leakingHYDRAULIC GREEN SYSTEM FAILURE (LOW FLUID), FOLLOWED ECAM AND QRH. EXTENDED LANDING GEAR MANUALLY. DECLARED EMERGENCY LANDED MANILA. REPLACED HYDRAULIC LINE WITH TEMPORARY FLEX LINE AND SERVICE WITH HYDRAULIC FLUID. REPLACED TEMPORARY FLEX LINE P/N A292192SDR 2005F00020Fitting · crackedDURING GEAR RETRACTION, GREEN PUMP LOW PRESSURE AND LOW LEVEL LIGHTS ILLUMINATED. USED EMERGENCY GEAR EXTENSION SYSTEM. REPLACED SWIVEL FITTING AT LEFT GEAR ASSEMBLY. (M)SDR ASMF200502001Relief Valve · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING PUSH BACK, CAPTAIN REPORTED LOST OF HYDRAULIC PRESSURE AND QUANTITY. DURING CHECK WAS DETECTED A LEAK FROM THE LEFT HYDRAULIC RELIEF VALVE, IT WAS REPLACED IAW MM 29-10-12, TESTED CORRECT.SDR DL767050080Line · leakingRT HYD SYS FAILURE. RT HYD SYS QTY DROPPED QUICKLY SUGGESTING A LEAK. FOUND RT ENGINE PRESSURE LINE CHAFED THROUGH, REPLACED SAME.SDR C8GA20050006Line · rupturedFLT 721 FROM FLL TO RDU, AFTER TAKEOFF, BOTH "A" HYDRAULIC PRESSURE LOW LIGHTS ILLUMINATED FOLLOWED BY LOSS OF SYSTEM PRESSURE AND QUANTITY. AIRCRAFT RETURNED TO FLL AND LANDED WITHOUT FURTHER INCIDENT. FOUND RUPTURED FLEXIBLE HYDRAULIC LINE TO NOSE GEAR ACTSDR DL75K050071Line · leakingAIR TURN BACK RT GEAR WOULD NOT RETRACT AFTER TAKEOFF. REPLACED HYDRAULIC LINE TO TRUCK POSITION ACTUATOR.SDR MASA205500076Line · crackedASH 6318 SBA - LAX, PILOT DIVERTED INTO LAX EN ROUTE TO PHX DUE TO NR 1 HYD QUANTITY AND PRESSURE LOW. MAINTENANCE FOUND A CRACKED LINE AT THE NR 1 CASE DRAIN FILTER. 1/31/05 MAINTENANCE INSTALLED A TEMP HYD LINE, SERVICED HYD SYSTEM OPS CHECKED GOOD. LATERSDR COMA0560103Line · leakingFLT 5885 NR 1 HYDRAULIC SYSTEM LOW PRESSURE WARNING. REPLACED LEAKING HYDRAULIC LINE.SDR ASAA0510001Hydraulic Line · crackedSEA - WHILE EXTENDING FLAPS TO NR5 POSITION, HYDRAULIC LOW-PRESSURE LIGHTS ILLUMINATED. QUANTITY WENT TO ZERO. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED (A) SYSTEM HYDRAULIC PRESSURE LINE. ACCOMPLISHED CONDITIONAL INSPECTIONS. RETURNED TO SERVICE. (KSDR CA050211004Hose · ruptured(CAN) AFTER TAKE-OFF AND ON GEAR UP SELECTION, THE NOSE GEAR FAILED TO RETRACT AND IT WAS OBSERVED BY THE CREW THAT THE NR 2 HYDRAULIC SYSTEM WAS ALMOST DEPLETED OF OIL. AIRCRAFT WAS MAINTAINED VISUALLY IN THE CIRCUIT WHILE ALL RELEVANT QRH PROCEDURES WERE COMSDR CA050127007Line · unserviceable(CAN) HYDRAULIC FLUID LEAKING OUT OF THE LT IB L/E. L/E REMOVED AND FOUND RIGID HYDRAULIC BRAKE LINE CHAFFED THROUGH BY ENGINE CONTROL CABLES ABOVE HEAT EXCHANGER. REPLACED LINE. ALL COMPANY AIRCRAFT USING THIS HYDRAULIC LINE VISUALLY INSPECTED AND FOUND DAMASDR CA050126002Pump · failed(CAN) FOR THE RELIGHT PROCEDURES FOR THE RT ENGINE, THE RT HYD DCMP HAD BEEN TURNED ON PRIOR SHUTDOWN. AFTER 5 MINUTES OF DRIFT DOWN AT 185 KTS, AROUND 40000 FT, AP SYNC WAS PRESSED AND ACCELERATED TO 250. SOMEWHERE AROUND THAT TIME, THE LT GEN DROPPED OFF LSDR 2006FA0000179Line · chafedWHILE COMPLYING WITH SB, FOUND 2 HYDRAULIC LINES PN MY20751107 AND MY20751207 CHAFED 20 PERCENT OF WALL THICHNESS LINES REPLACED. (K)SDR 2006FA0000178Line · chafedWHILE COMPLAYING WITH SB, FOUND 2 HYDRAULIC LINES PN MY20751107 AND MY20751207 CHAFED 20 PERCENT OF WALL THICKNESS LINES REPLACED. (K)SDR 2005FA0001402Control Valve · shortedFLAP CONTROL VALVE PN 2710970 TO BE MAKING CONTACT WITH DUMP VALVE PN OA55319-1 CAUSING WAS SUBSTIALLY DAMAGE. BY SHORTING THE STAND OFF ON THE BOTTOM SIDE OF THE DUMP VALVE BY APROX .1250 OF AN INCH A CLEARANCE OF APROX .0625 OF AN INCH WAS OBTAINED. (K)SDR 2005FA0001401Line · damagedHYDRAULIC LINE, PN 6556000-20, ON LT ENGINE IS MAKING CONTACT WITH FUEL LINE PN 3042937-01. THIS CAUSED CHAFFING IN EXCESS OF 20 PERCENT OF THE WALL THICKNESS ON THE HYDRAULIC LINE AND 10 PERCENT TO 15 PERCENT WALL THICKNESS ON THE FUEL LINE. BOTH LINES WERESDR HSY2005F00002Hose · leaking(MRR NR 02-012405) LOSS OF HYDRAULIC PRESSURE AND QUANTITY LED TO THE INABILITY TO OPERATE THE LANDING GEAR WITH NORMAL PROCEDURES. LANDING GEAR HAD TO BE EXTENDED MANUALLY WITH THE HAND PUMP. NOTE: THIS WAS A PILOT TRAINING FLIGHT ONLY. FAILED LANDING GEARSDR DXTA200500555Line · leakingUPON LOWERING GEAR HANDLE A/C LOST ALL -A- SYSTEM FLUID. FOLLOWED EMERGENCY CHECKLIST, POST FLIGHT DISCOVERED FLUID IN NOSE WHEEL WELL. ITEM IS UNDER INVESTIGATION.SDR COMA0560072Hydraulic System · lowFLIGHT 5045 - DURING APPROACH TO BOS, RECEIVED A GEAR DISAGREE FOLLOWED BY A HYDRAULIC NR 3 LOW PRESSURE CAUTION, CREW DECLARED AN EMERGENCY, FOLLOWED QRH AND LANDED WITHOUT INCIDENT. SERVICED THE NR 3 HYDRAULIC SYSTEM.SDR SWAA050167Module · leakingDECLARED EMERGENCY, A-SYSTEM HYDRAULIC FAILURE, QUANTITY LOSS. REMOVED AND REPLACED A-SYSTEM FILTER MODULE O-RING PER MM.SDR ASOA05049Hydraulic Line · leakingDURING APPROACH, AT APPROXIMATELY 300 FT CREW RECEIVED A MASTER CAUTION SINGLE CHIME. EICAS SHOWED HYDRAULIC 2 LOW PRESSURE. PARKING BRAKE-BRAKE PRESSURE. RT THRUST REVERSER INOP, ALONG WITH FLIGHT SPOILER DEPLOY ADVISORY MESSAGES. HYDRAULIC SYNOPTIC PAGE SDR GTIA050013Hydraulic Line · leakingFLL - FOUND EVIDENCE OF A HYDRAULIC LEAK IN LEFT MLG WHEEL WELL, AIRCRAFT TAIL SWAP. FOUND LEFT GROUND SPOILER UP PRESSURE LINE LEAKING. INSTALLED FLEX LINE, TRANSFERRED TO CARRYOVER, NO LEAKS NOTED. (M)SDR SWAA050119Valve · leakingAIR TURNBACK, DURING CLIMB NR 2 ENGINE DRIVEN HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED, WITH LOSS OF SYSTEM-B HYDRAULIC FLUID. REMOVED AND REPLACED NR 2 T/R SHUTTLE VALVE PER MM.SDR 47518011705Line · rupturedTHE NR 1 HYD SYSTEM CAUTION LIGHT CAME ON. PRESSURE CHECKED AND WAS CONFIRMED TO BE AT ZERO. CYCLED SWITCH, MOVED PEDALS AND VERIFIED ACTUAL FAILURE, SO TURNED HYD SYSTEM #1 OFF, PROCEEDED TO FULLERTON AIRPORT AND MADE LANDING FROM A HOVER TO HELIPAD, NO PROBLSDR DLM88050039Line · failedRIGHT HYDRAULIC PRESSURE WENT TO ZERO IN FLIGHT. QTY WENT TO 6, THEN 2, THEN 7. USED ALT GEAR EXTENSION. LANDED SAFELY. FOUND HYD PRESSURE LINE IN PYLON FAILED. REPLACED SAME.SDR MASA200500041Hydraulic Line · leakingASH 6347 HMO PHX RETURNED TO THE FIELD DUE TO THE NR 2 HYD SYSTEM FAILED ON GEAR RETRACT. MAINTENANCE ARE IN THE PROCESS OF TROUBLESHOOTING. MAINTENANCE INSTALLED A TEMP FLEX LINE ON NR 2 HYD PRESS TRANSDUCER TO FLY THE AIRCRAFT BACK TO PHX. LATER THE FLEX SDR DL757050037Control Valve · ingestedRIGHT HYD QTY DROPPED TO .43 WITH RT AUTOPILOT TRIP. FOUND RT SYS QTY AT .43 WITH LT HYD QTY AT 1.33. REPLACED PARKING BRAKE VALVE AND ANTI-SKID SHUTTLE VALVES.SDR 2005UALA00065Hydraulic System · failedRETURNED TO LAX DUE TO RIGHT HYDRAULIC SYSTEM FAILURE. LOSS OF FLUID DUE TO FAILED O-RING ON CASE DRAIN MODULE DIFFERENTIAL PRESSURE INDICATOR BOSS. REPLACED O-RING AND RESERVICED HYDRAULIC SYSTEM.SDR ASMF200501009Selector Valve · leakingDURING TRANSIT CHECK WAS DETECTED AN HYDRAULIC LEAK ON RT MAIN LANDING GEAR WELL. WELL WAS CLEANED AND SYSTEM WAS PRESSURIZED AND NO LEAK WAS DETECTED, HYDRAULIC SYSTEM WAS RECHARGED WITH 4 QUARTERS, ALL CORRECT. AT AGU, HYDRAULIC LEAK WAS DETECTED ON RIGHT SSDR SWIA200514491Line · leakingAFTER GEAR EXTENSION, GREEN HYDRAULIC LOW LEVEL LIGHT, THE GUAGE CONFIRMED ZERO QUANTITY. REPLACED GEAR DOWN HYDRAULIC FLEXIBLE LINE ON RIGHT MAIN GEAR. SERVICED HYDRAULICS TO PROPER LEVEL. OPERATIONAL CHECK GOOD.SDR CA050215009Switch · defective(CAN) PILOT COULD NOT TURN HYD OFF DURING FLIGHT BY PRESSING BUTTON ON COLLECTIVE STICK. TROUBLESHOOTING DETERMINE THE SWITCH WAS DEFECTIVE AND NOT SUPPLYING VOLTAGE TO SOLENOIDS. NEW SWITCH INSTALLED.SDR C8GA20050001Line · splitAFTER TAKE OFF FROM SAN, "A" HYDRAULIC SYSTEM LOW LEVEL LIGHT ILLUMINATED FOLLOWED BY RAPID QUANTITY DEPLETION. TURNED OFF BOTH THE NR 1 AND 2 HYDRAULIC PUMPS AND RETURNED TO SAN. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. FOUND PRESSURE LINE SPLIT OPEN BETWSDR CA050113004Union · fractured(CAN) DURING CRUISE, THE NR 1 HYDRAULIC SYSTEM SUFFERED A TOTAL HYDRAULIC SYSTEM FLUID LOSS. A FULL EMERGENCY LANDING WAS DECLARED INTO BASE, WHICH WAS CARRIED OUT WITHOUT FURTHER INCIDENT. UPON INSPECTION BY ENGINEERING IT WAS DISCOVERED THAT THE NR 1 HYDRASDR CA050114003Motor · leaking(CAN) A/C DEPARTED AND TURNED AROUND AFTER NOTICING SLOW STEADY DECLINE IN CENTER SYSTEM QUANTITY. MAINTENANCE FOUND FLUID LEAKING FROM FUSELAGE DRAIN HOLES IN THS COMPARTMENT. UPON INVESTIGATION MAINTENANCE FOUND CENTER SYSTEM HYD MOTOR ON THIS GEARBOX LEAKINSDR DXTA200500530Warning Light · illuminatedON APPROACH WHEN FLAPS WERE SELECTED TO 15 DEG LOW HYD FLOW LT & RT CAUTION LIGHTS ILLUMINATED. THAT WAS FOLLOWED BY LOW HYD LEVEL AT AROUND THE SAME TIME THE FLAPS REACHED 15 DEG BECAUSE OF THE POTENTIAL FOR HYDRAULIC FLUID LOSS, AND EMERGENCY GEAR EXTENSIONSDR GNB2005F00003Line · corrodedFAILED HYDRAULIC PRESSURE CHECK. LINE LAYING ON DUCTING FOR HEATING CAUSING CORROSION TO FORM. (SW01200502894) (K)SDR CA050120006Line · cracked(CAN) AIRCRAFT DEPARTED. AS THE AIRCRAFT ACCELERATED THE CREW BECAME CONCERNED DUE TO A VIBRATION. THE AIRCRAFT WAS DIVERTED TO INTERNATIONAL AIRPORT. INVESTIGATION FOUND A CRACK IN THE HYDRAULIC LINE FROM THE LT ENGINE DRIVEN HYDRAULIC PUMP WHERE IT CONNECTSDR AU510001684Hose · failedRT HYDRAULIC PUMP PRESSURE LINE FAILED. LOSS OF HYDRAULIC FLUID. SUSPECT CAUSED BY FATIGUE TO TO PRESSURE SPIKES CAUSED BY PUMP ACTIVATION.SDR DXTA200500515Line · unknownON LANDING ROLL OUT,THE LEFT BRAKE PEDAL WENT TO THE STOP WITHOUT ANY BRAKING OCCURRING ON THE LEFT MAINS. TAXI CHECK A/C COULD NOT DUPLICATE. HOOKED UP PRESS GAUGES TO LT BRAKE ASSY APPLY HYD PRESS + GET 2000 PSI OUT OF BOTH BRAKE ASSY. BLED BRAKES. TAXI
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