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 AU510001476Line · worn(AUS) LH ENGINE DRIVEN HYDRAULIC PUMP PRESSURE LINE CHAFED AND HOLED BY OIL TANK UNION. LOSS OF HYDRAULIC PRESSURE RESULTED IN AN EMERGENCY LANDING. DUE TO NO HYDRAULIC PRESSURE, THE ANTISKID WAS NOT AVAILABLE AND THE BRAKES LOCKED UP. NO1, NO2 AND NO3 TYRES WSDR MASA200500288Hydraulic Line · brokenCAPT RETURNED TO FIELD FOR HYDRAULIC SYSTEM NR 1 QUANTITY DROPPED TO 0 PERCENT. MAINTENANCE FOUND HYDRAULIC LINE BROKEN AND REPLACED IT.SDR HEEA107343Hose · leakingON FIRST FLIGHT OF DAY, IN CRUISE HYD SERVO ONE LIGHT FOLLOWED BY HYD PUMP ONE LIGHT AND ONE HYD PRESSURE WENT TO ZERO. FOUND PIN HOLE IN HOSE UNDER CLAMP. REPLACED HOSE AND CLAMP.SDR ARWA20050402Line · brokenDURING TAXI, TOTAL LOSS OF HYDRAULIC SYSTEM NR 3 FLUID. T/S FOUND BROKEN LINE FROM NR 3 SYSTEM IN CENTER WHEEL WELL. REPAIRED LINE IN ACCORDANCE WITH DC-10 M/M 20-10-01. SERVICED NR 3 HYDRAULIC SYSTEM IN ACCORDANCE WITH M/M 12-13-02. NO LEAKS NOTED.SDR HNAA050034Line · leakingON GEAR RETRACTION NOSE GEAR DID NOT RETRACT, NR 2 HYDRAULIC QUANTITY DROPPED TO .5 QUARTS. CREW PERFORMED EMERGENCY EXTENSION. FOUND PRESSURE LINE TO NOSE GEAR DRAG STRUT ACTUATOR LEAKING. REMOVED AND REPLACED LINE AND COMPLIED WITH GEAR SWINGS.SDR HEEA107350Tube · leakingAFTER TAKEOFF, THE ODOR OF HYDRAULIC OIL WAS NOTED IN THE COCKPIT, THE AIRCRAFT WAS TURNED AROUND AND LANDED. AFTER LANDING, THE NR 2 HYDRAULIC PRESSURE FLUCTUATED AND STARTED TO GO DOWN, THE AICRAFT WAS SHUTDOWN, AND MAINTENANCE FOUND PIN HOLE IN THE TUBE CASDR P9RA20050074Packing · splitCRUISE FLT FL390, EICAS MESSAGE FOR LEFT SYSTEM HYDRAULIC FLUID LOW. FOLLOWED QRH PROCEDURE BUT FLUID LEVEL CONTINUED TO DECREASE. ALTERNATE EXTEND ON GEAR AND FLAPS. EMERGENCY DECLARED ON APPROACH INTO ATL. NORMAL LANDING FOLLOWED BY FULL STOP ON TAXIWAY.SDR SWAA050991Line · chafedAIR TURNBACK, DECLARED EMERGENCY. LOST B-HYDRAULIC SYSTEM ON TAKEOFF. REMOVED AND REPLACED HYDRAULIC LINES FROM B-SYSTEM PUMP TO B-SYSTEM CONTROL MODULE & B-SYSTEM PUMP CASE DRAIN TO T-FITTING PER MM.SDR QXEA200500526Hydraulic Line · leakingYKM-ON FLIGHT NUMBER 2002, AFTER LANDING AND PARKING NOTICED A STRANGE ODOR AND BOTH PILOTS STARTED COUGHING, COULD SEE MIST/SMOKE IN THE COCKPIT. AFTER SHUTDOWN NOTICED FLUID LEAKING FROM BELLY OF AIRCRAFT UNDER COCKPIT. MAINTENANCE INSPECTED AND FOUND HYDRSDR 0500413218Fitting · brokenAFTER TAKEOFF FROM MEM PRIOR TO FLAP RETRACTION, RECEIVED ECAM CAUTION HYD Y RSVR LO LVL. FOLLOWED COM PROCEDURES, RETURNED TO MEM, AND LANDED UNEVENTFULLY. ENGINE DRIVEN PUMP CAVITATED FOR ABOUT 30 SECONDS. FOUND UNION FITTING BROKEN OFF OF BRAKE DUAL DISTSDR BSYA200500006Hose · leakingNR 3 BRAKE HOSE LEAKED DEPLEATING HYD RES. GEAR WOULD NOT CYCLE DOWN, DECLARED AN A EMERGENCY AT CMH, GEAR DID COME DOWN AND LOCK WITH AUX HYD PUMP. LANDED NO PROBLEMS. FOUND NR 3 BRAKE FLEX LINE LEAKING. REMOVED AND REPLACED LINE, CHANGED BOTH ENGINE DRIVSDR MR0510Line · crackedJUST BEFORE LANDING, HYDRAULIC VAPOR/SMOKE NOTED IN CABIN AND COCKPIT. AIRCRAFT LANDED WITHOUT INCIDENT, ENGINES SHUTDOWN AND PAX DEPLANED. MAINTENANCE FOUND FAILED HYDRAULIC LINE IN WING ROOT THAT SPRAYED FLUID INTO AIR CYCLE MACHINE INTAKE WHICH TRANSFERRESDR A6WA200540127Line · chafedHYDRAULIC NR 1 LOW PRESSURE MESSAGE INFLIGHT ON CLIMBOUT. QUANTITY INDICATES ZERO. REMOVED AND REPLACED HYDRAULIC SUPPLY LINE TO CASE DRAIN ASSY REF 29-11-02, RAN ENGINE LEAK CHECK. OPS CHECK GOOD. (K)SDR DLM88050191Hydraulic Line · wornLEFT HYD QTY DROPPED PRESSURE FAILED TO ZERO. REPLACED ENG HYD PRESSURE LINE IN TAIL COMPARTMENT.SDR 2005F00062Hose · rupturedWHILE EN ROUTE FROM SIOUX FALLS, SD TO RAPID CITY, SD THE PILOT NOTICED THE HYDRAULIC PRESSURE WAS FLUCTUATING ON THE LEFT HAND ENGINE. SHORTLY THEREAFTER THE RIGHT HAND PRESSURE BEGAN TO FLUCTUATE. THE PILOT REQUESTED CLEARANCE TO RETURN TO SIOUX FALLS WHICSDR MAC5302Hydraulic System · malfunctionedDURING CLIMB, THE A/C EXPERIENCED LIGHTNING AND A MOMENTARY LOSS OF BLUE SYSTEM HYDRAULICS. AN EMERGENCY WAS DECLARED AND THE A/C LANDED WITHOUT FURTHER INCIDENT. AN INSPECTION IAW ATR JIC 05-51-13OUI 1000 WAS PERFORMED AND AN OPERATIONAL TEST OF THE HYDRAULSDR 248232Swivel · crackedCOMPLETE LOSS OF HYDRAULIC PRESSURE AND FLUID AFTER GEAR RETRACTION, HAND PUMPED GEAR DOWN PER QRH. INSPECTED AND FOUND HYDRAULIC SWIVEL TO BE CRACKED. AIRCRAFT WAITING FOR MAINTENANCE.SDR MALA050284Isolation Valve · malfunctionedYELLOW HYD TEMP CAME ON IN FLT ENGINE 2 VALVE (NIPS) LIGHT STAYED ON WITH VALVE SHUT. HYD PRESS ON YELLOW STAYED AT 3100 PSI WITH VALVE SWITCH IN OFF POSITION. REMOVED AND REPLACED YELLOW HYD ISO VALVE P/N ON & OFF HTE9531-3, S/N ON FRTR023AX.SDR 05FDEA00608Shutoff Valve · leakingAPPROXIMATELY 5 MINUTES AFTER TAKEOFF, MASTER CAUTION LIGHT ILLUMINATED AND OBSERVED BOTH LT & RT NR 2 EDP LIGHT ON, PRESSURE AND QUANTITY RAPIDLY WENT TO ZERO. FOUND 1-2 NONREVERSIBLE MOTOR PUMP SHUTOFF VALVE LEAKING FROM BACKUP RING.SDR 20051Packing · cutNR 1 HYD SYSTEM FAILURE (ISO VALVE). CAUTION PANEL DID NOT HAVE NR 1 ISO VALVE CAUTION LIGHT, ONLY A LINE. EMERGENCY LANDING OGG. ENGINE SHUT DOWN ON RUNWAY. INSPECTED NR 1 HYD SYSTEM FOR LEAKS AND FOUND LT OUTER WING FITTING REDUCER PACKING RIPPED. REMOVSDR HNAA0500022Line · leakingIN FLIGHT NR 2 HYDRAULIC SYSTEM WENT TO 1 QT AND NR 2 ISO VALVE CAUTION LIGHT ILLUMINATED. NO OTHER CAUTION LIGHTS AND QUANTITY REMAINED ABOVE 1QT. FLIGHT DIVERTED TO MDT WHERE IT WAS FOUND HYDRAULIC FLUID WAS LEAKING FROM BEHIND THE NR 2 NACELLE GRAVEL GUARSDR 05FDEA00546Line · leakingAFTER GEAR EXTENSION GOT GREEN HYDRO SYS LOW AIR PRESSURE LIGHT. DECLARED AN EMERGENCY AND LANDED STRAIGHT AHEAD. AFTER LANDING LOW AIR LIGHT WENT OUT. TURNED BOTH GREEN PUMPS BACK ON IAW QRH. GREEN SYSTEM RECOVERED AND CLEARED THE RUNWAY. GREEN HYD SYSTESDR DXTA200500631Quick Disconnect · dirtyON LANDING BRAKE PEDALS FELT NORMAL, HOWEVER AIRCRAFT HAD DIFFICULTY COMING TO A STOP WITH HARD BRAKING ACTION PERFORMED. TROUBLESHOT SYSTEM, FOUND RT MAIN GEAR STRUT SQUAT SWITCH ELECTRICAL CONNECTOR VERY DIRTY. CLEANED CONNECTOR, OPS CHECK GOOD, REF CITATISDR DXTA200500630Line · leakingBRAKES FELT SPONGY, EXCESSIVE PEDAL TRAVEL BEFORE BRAKES ENGAGED. T/S SYSTEM, BLEED BRAKES. TAXI ACFT, OPS & LEAK CHECKS GOOD IAW 560 M/M CH 32-42-00.SDR MAC5301Line · crackedDURING TAXI, NORMAL BRAKING ACTION WAS LOST. AFTER TROUBLESHOOTING A TUBE TO THE BRAKE METERING VALVE WAS FOUND TO BE BROKEN. THE TUBE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR U30A200500002Pipe · leakingCREW RECEIVED AN ECAM MESSAGE, GREEN HYD LOW PRESS. TURNED OFF PUMP & PTU. STATUS PG INDICATED LOW PRESS & NIL QTY. DIVERTED, DECLARED AN EMERGENCY. ECAM GENERATED APPROACH LIST INSTRUCTS TO TURN PTU BACK ON TO TRY TO RESTORE PRESSURE, PRESSURE RESTORED. SDR ASMF200503008Servo Valve · leakingDURING TRANSIT CHECK WAS DETECTED HYDRAULIC LEAK IN THE DUAL SERVO VALVE OF LT WHEEL WELL . THE DUAL SERVO VALVE AND HYDRAULIC LINES WERE ADJUSTED IAW MM 32-43-03, TESTED CORRECT.SDR QXEA200500363Line · crackedBLI - FLIGHT 2136 - UPON GEAR DOWN SELECTION, THE NR 2 ENGINE HYDRAULIC FLUID QUANTITY AND PRESSURE WAS TOTALLY LOST. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NOSE LANDING GEAR DOWN HYDRAULIC LINE CRACKED. THE LINE WAS REPLACED AND OPERATIONAL CHECKSSDR TSAA0529012Line · leakingLOST A SYSTEM HYDRAULICS ON SHORT FINAL. MAINTENANCE MET THE AIRCRAFT ON THE RUNWAY. MAINTENANCE REPLACED THE NOSE GEAR DOWN ACTUATOR LINE PER AMM 32-3-11. SERVICED HYDRAULIC SYSTEM TO FULL. LEAK CHECK OKAY. REPLACED THE NR 1 AND NR 2 CASE DRAIN FILTERS, SDR AALA20050174Hydraulic Line · crackedMIA - GREEN SYSTEM QUANTITY SHOWED AT RED DOT. MANUALLY EXTENDED GEAR. FOUND PRESSURE LINE IN CENTER GEAR WELL CRACKED. REPLACED PRESSURE LINE IN CENTER GEAR WELL. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR ASOA05219Hydraulic System · leakingDURING CRUISE FROM ATL-FNT, THE CREW NOTICED THE NR 1 HYDRAULIC SYSTEM QUANTITY HAD FALLEN TO 45 PERCENT. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT DIVERTED TO CVG AND LANDED SAFELY. MAINTENANCE INSPECTED AND SERVICED THE NR 1 HYSDR AWXA200500304Module · faultyAFTER DEPARTURE AT APPROXIMATELY 1,000 FT A-SYSTEM HYDRAULICS AND FEEL DIFFERENTIAL LIGHT ILLUMINATED, TURNED BACK TO PHX, FLIGHT CONTROLS FELT STIFF BUT FUNCTIONAL. MAINTENANCE FOUND A-SYSTEM FLIGHT CONTROL MODULAR PACKAGE FAULTING, REPLACED MODULAR PACKAGE SDR CA050309001Tube · chafed(CAN) DURING ROUTINE MAINTENANCE, THE SUBJECT TUBE WAS FOUND WITH A (0.375 INCH X 0.187 INCH) HOLE THAT ORIGINATED FROM CHAFING WITH A HYDRAULIC OIL LINE. THE HOLE WAS LOCATED APPROXIMATELY IN THE CENTER OF THE TUBE. THE TOTAL CHAFING DAMAGE IN THIS AREA, COSDR CA050308018Line · chafed(CAN) LINE CHAFED WHERE LINE COMES THROGH THE COOLING TURBINE MODULATING VALVE. NEW LINE FABRICATED AND INSTALLED WITH ADDITIONAL CLAMPS TO PREVENT FUTURE CHAFING. W.S. 39.1 IPC FIG 29-10-50 FIG 2 ITEM 2SDR DXTA200500609B-Nut · leakingON DESCENT EGE NOSE GEAR BUMP (BUMP IN THE NIGHT) LOUD NOISE AND FELT IT IN THE FLOOR. FOUND A-SIDE HYDRAULICS AT 43 PERCENT AND A LOOSE B-NUT ON NLG ACTUATOR. JACKED AIRCRAFT TIGHTENED B-NUT, SERVICED HYDRAULICS WITH SKYDROL C/W GEAR SWINGS (15X), NO FAULTSSDR O3X05029373Flex Line · rupturedAIRCRAFT DEPARTED STL, WHEN BOTH HYDRAULIC PRESSURE GAUGES WENT TO ZERO. THE CREW ACTUATED BOTH MAIN HYDRAULIC SHUTOFF COCKS. THE AIRCRAFT RETURNED TO STL AND DECLARED AN EMERGENCY. THE LANDING GEAR WAS MANUALLY LOWERED AND THE AIRCRAFT LANDED. INSPECTION SDR HEEA107347Tube · leakingIN CRUISE FLIGHT UTILITY HYDRAULIC AND OIL COOLER SEGMENT LIGHTS ILLUMINATED. FOLLOWED APPROPRIATE EMERGENCY CHECKLISTS AND RETURNED TO MCY. MAINTENANCE FOUND PIN HOLE IN TUBE UNDER ADEL CLAMP.SDR MASA200500145Union · brokenDEN - RAP, CAPT RETURNED TO THE FIELD DUE TO NR 1 ENG HYD LIGHT ILLUMINATED IN FLIGHT. CAPT ALSO REPORTED, THERE WAS NO HYD QUANTITY INDICATION ON NR 1 HYD SYSTEM. MAINTENANCE FOUND A UNION AT NR 1 HYD MANIFOLD BROKE. AOG FOR PARTS AT THIS TIME. MAINTENANCSDR SWAA050496Hydraulic Line · leakingDIVERSION, INFLIGHT B-HYDRAULIC SYSTEM LOW PRESSURE LIGHT ILLUMINATED. FOLLOWED BY B-SYSTEM FLUID LOSS. REMOVED AND REPLACED HYDRAULIC HOSE AT B-SYSTEM ACOUSTIC FILTER PER MM.SDR 05FDEA00307Line · leakingAFTER SLAT RETRACTION LOST YELLOW SYS HYD PUMP, FOLLOWED BY LOW PRESSURE. ONE MINUTE LATER LOST YELLOW SYS QUANTITY. APPROX 1 MIN PUMP WAS RUNNING. FOUND LEAK AT FLEX LINE JUST BEHIND TOP OF LT MAIN GEAR LEG. ADDED MPN A2714201300000, CPN 2713423 QTY 1, ADSDR C2XA05SD015Hose · rupturedNR 1 ENG, ENGINE DRIVEN HYD PUMP PRESSURE LINE RUPTURED. THE LOCATION OF THE RUPTURE WAS ABOUT THE MIDDLE OF THE LINE. MAINTENANCE REMOVED AND REPLACED PRESSURE LINE AND ENGINE DRIVEN HYDRAULIC PUMP. HYD SYSTEM WAS SERVICED, OPS & LEAK CHECKED GOOD. AIRCRASDR DXTA200500594Line · leakingON LANDING BRAKES WERE VERY SOFT AND MADE STOPPING THE AIRPLANE DIFFICULT. ALSO CO-PILOTS BRAKES CONFIRMED THE BRAKE ISSUE. LEFT PEDAL ON CO-PILOTS SIDE WENT TO FULL TRAVEL. BLED CO-PILOT BRAKES IAW HAWKER 1000 MM 32-40-00. OPERATIONAL CHECK SATISFACTORY.SDR 45165021505Line · leakingCREW REPORTED "MAIN HYD QTY LOW" WHITE CAS FOLLOWED BY "LEFT HYD PUMP LOW", FOLLOWED BY "RIGHT HYD PUMP LOW", FOLLOWED BY AMBER "MAIN HYD PRESS" CAS MESSAGES. CREW DECLARED EMERGENCY AND LANDED AT DESTINATION AIRPORT WITHOUT INCIDENT. AFTER LANDING FOUND HYDSDR ARWA20050205Line · leakingAFTER LANDING LOST HYDRAULIC PRESSURE; QUANTITY DOWN TO AUX LEVEL. REMOVED AND REPLACED BOGIE TRIM CYLINDER (BTC) HYDRAULIC LINE AS PER MM 32-33-1. LEAK CHECK OK, NO LEAKS NOTED.SDR DXTA200500591Line · leakingBRAKES ARE SPONGY, LEFT SIDE IS WORSE THAN THE RIGHT SIDE. LEFT BRAKE ALMOST GOES TO HTE FLOOR FOR ANY REACTION. FOUND AIR IN BRAKE SYSTEM, BLED BRAKE SYSTEM IAW 560XL MM 32-42-00, TAXI CHECK GOOD.SDR AU510002203Clamp · broken(AUS) HYDRAULIC PIPES PN 1379007D441 AND PN 1379007D443 LOCATED IN LT WING LEADING EDGE RUBBING TOGETHER DUE TO A BROKEN CLAMP. ONE PIPE WAS WORN THROUGH. LOSS OF HYDRAULIC FLUID. (OTHER CAUSE: BROKEN CLAMP ) (CASA NR 510002203)SDR C1HA200578001Hydraulic Line · chafedAFTER TAKEOFF HYDRAULIC B-SYSTEM QUANTITY LEAK TO ZERO, ACCOMPLISHED COM EMERGENCY CHECKLIST, RETURNED FOR LANDING. FOUND CHAFED SPOILER PSI LINE IN RT WHEEL WELL AREA WHERE LINES GOES THROUGH WALKING BEAM INSTALLED TEMP FLEX LINE REF SUPPL MM 20-10-12, NO LSDR 2005FA0000409Line · chafedWHILE INVESTIGATING A GEAR UP LANDING, IT WAS NOTED THAT THE HYDRAULIC LINE FROM THE LANDING GEAR PUMP WAS CHAFING AGAINST THE FLIGHT CONTROL CABLES ROUTED IN THE BATTERY COMPARTMENT AREA. SUGGEST INSPECTING THIS AREA FOR CHAFING AND RE-ROUTE HYDRAULIC LINE TSDR O3X020109442Line · burstAIRCRAFT WAS ENROUTE, THE CREW NOTICED ONE HYDRAULIC GAUGE FLUCTUATING AND FINALLY GOING TO ZERO AND THE OTHER GAUGE AT ZERO. THEY WENT THROUGH THE PROCEDURES FOR HYDRAULIC FAILURE. THE GEAR WAS EXTENDED. THE NOSE INDICATED DOWN AND LOCKED. THE MAINS WERE SDR ASMF200502008Housing · crackedCAPTAIN REPORTED THAT QUANTITY AND PRESSURE WERE LOOSE ON LEFT HYDRAULIC SYSTEM. DURING ENGINE RUNNING, A LEAK WAS DETECTED IN THE HOUSING OF THE HYDRAULIC PUMP FILTER. THE MODE FILTER HYDRAULIC LEFT SIDE PUMP ENGINE DRIVE WAS REPLACED IAW MM 29-10-14, TES
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