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 BG001Line · failedDOWN HYDRAULIC PRESSURE LINE FAILED AT ACTUATOR. LINE PULLED OUT OF SWAGED END FITTING.SDR DXTA200501004Line · leakingRIGHT BRAKE PEDAL LOOSES PRESSURE DURING BRAKING. BLED LT & RT BRAKE SYSTEM & PERFORMED SYSTEM PRESSURE CHECKS IAW CHAPT 32-43-00 CESSNA 560XL MM. ALL CHECKS GOOD. OPERATED SYSTEM NUMEROUS TIMES AND DID NOT EXPERIENCE PRESSURE LOSS. SERVICE LEVELS GOOD.SDR 05FDEA03237Control Valve · leakingEVIDENCE OF HYDRAULIC LEAK AT I/B SLAT CONTROL VALVE IN CAC COMPARTMENT. REMOVED AND REPLACED I/B SLATE CONTROL VALVE IAW DC10 M/M 27-82-02-2. LEAK CHECK GOOD IAW DC10 M/M 27-82-02-2.SDR 05FDEA03236Control Valve · leakingRT O/B SLAT CONTROL VALVE LEAKING AT SPLINE SHAFT. REMOVED AND REPLACED RT O/B SLATE CONTROL VALVE IAW DC 10 M/M 27-82-02-2. LEAK CHECK GOOD IAW DC10 M/M 27-82-02-2.SDR CNQ2005F00000Line · chafedFLEXIBLE HYDRAULIC HOSE CHAFED THROUGH ALLOWING HYDRAULIC FLUID TO BE LOST IN THE (B-SYSTEM). HOSE WAS CONTACTING LT ELEVATOR POWER CONTROL UNIT. REPLACED HOSE AND VERIFIED ROUTING UNIT. REPLACED HOSE AND VERIFIED ROUTING TO PREVENT CHAFING. MFG IS ISSUINGSDR DLM90050592Hose · leakingON APPROACH LOST ALL RIGHT SIDE HYDRAULIC QUANTITY. REPLACED LEAKING RT ENGINE PUMP PRESSURE LINE.SDR 139810042005Hydraulic System · failedLOST FLIGHT SIDE HYDRAULIC FLUID AFTER LANDING.SDR DXTA200501001Hose · chafedAFTER TAKEOFF, LOST ALL HYDRAULIC FLUID ON THE -B- SYSTEM WITH ASSOCIATED HYD PRESS LOW -B- AND HYD FLUID LOW -B- AMBER CAS MESSAGES. AFTER LANDING, COULD SEE FLUID DRIPPING DOWN FROM THE TAIL. REMOVED LEFT ELEVATOR OUTBOARD PCU HOSE ASSEMBLY DUE TO BEING CHSDR TIM2005F00010Line · leakingNOSE GEAR WARNING LIGHT ILLUMINATED WHEN LANDING GEAR EXTENDED. GEAR DEPLOYED AFTER 15 TO 20 SECONDS. PROBLEM WAS A LEAK IN THE HYDRAULIC LINE. THE LINE DEVELOPED A PIN HOLE LEAK BECAUSE OF CORROSION FROM THE INSIDE OF THE LINE. (K)SDR TIM2005F00008Line · leakingNOSE GEAR WARNING LIGHT ILLUMINATED WHEN LANDING GEAR EXTENDED. GEAR DEPLOYED AFTER 15 TO 20 SECONDS. PROBLEM WAS A LEAK IN THE HYDRAULIC LINE. THE LINE DEVELOPED A PIN HOLE LEAK BECAUSE OF CORROSION FROM THE INSIDE OF THE LINE. (K)SDR DL73S050589Line · leakingLOSS OF A SYSTEM HYD, ALT GEAR EXTENSION. REPLACED LEAKING PRESSURE LINE IN RIGHT PYLON.SDR UPS05545561Line · leakingINSPECTION TYPE:N/A ON FINAL APPROACH LEFT HYD QTY EICAS MSG APPEARED WITH GEAR DOWN & FLAPS 20. LANDED NORMAL WITH FLAPS 20. CLEARED RUNWAY & UNABLE TO STEER ACFT. STOPPED FOR TOW. REMOVED AND REPLACED LEFT MAIN GEAR DOWNLOCK PRESS LINE AND CARRIED OUT LESDR 10072005APressure Switch · malfunctionedDURING DESCENT HYD LIGHT ILLUMINATED (NO PRESSURE IN MAIN RESERVOIR) DID CHECKLIST, COULD NOT BRING IT BACK TO GREEN. ALSO, DID CHECKLIST FOR MANUAL EXTENSION OF GEAR AND FLAPS, IT DID MAINTAIN HYDRAULIC PRESSURE WITH HAND PUMP. AFTER LANDING, OVERRIDE SWITCSDR B65A106278Hydraulic System · leakingLEAKING HYDRAULIC UNIT.SDR NACA20050022Swivel Fitting · brokenHYDRAULIC BLUE LOW LEVEL LIGHT ON. RT OB SWIVEL FITTING FOUND BROKEN. REMOVED AND REPLACED WITH NEW FITTING. REF JIC 32-11-00-RAI-10020 TASK 1-3. BLED ALL MAIN LANDING GEAR BRAKES IAW ATR42 JIC 32-42-00-BLD-10010. SYSTEM OPS LEAK CHECKED GOOD.SDR 05FDEA03152Socket · leakingEN ROUTE AT FL330 RECEIVED ECAM FOR GREEN SYSTEM HYDRAULIC RESV LO. COMPLIED WITH ECAM AND DESELECTED GREEN PUMPS. AFTER NR 1 GREEN PUMP DESELECTED, ENGINE NR 1 GREEN PUMP C/B POPPED AND WOULD NOT ALLOW NR 1 GREEN PUMP TO BE DESELECTED. REFERENCE A300-600 ASDR DELA200500009Line · chafedHYDRAULIC FLUID LOSS WAS NOTED BY FLIGHT CREW DURING POST FLIGHT INSPECTION. INSPECTION BY MAINTENANCE NOTED THAT THE LEFT HAND CASE DRAIN LINE AND PRESSURE LINE WERE CHAFFED. THE CASE DRAIN LINE WAS LEAKING DUE TO A CHAFFED HOLE. BOTH LINES WERE REPLACED.SDR AALA20050621Line · failedJFK - INFLIGHT T9646/26 SEPT - GREEN HYDRAULIC SYSTEM QUANTITY DECREASED TO AMBER AND PRESSURE WAS DECREASED BELOW LIMITS. MANUALLY EXTENDED LANDING GEAR. LANDED JFK WITHOUT INCIDENT. REPLACED GREEN SYSTEM HYDRAULIC RESERVOIR AND SUPPLY TUBE. SYSTEM GROUNDSDR AWXA200501117Ptu · noisyEMERGENCY LANDING - FLT 113 - DURING DESCENT, CREW NOTICED NOISE COMING FROM PTU. DESELECTED PTU AND RECEIVED HYD Y ENG PUMP LO PR MSG. MADE EMERGENCY LANDING IN LAX, LANDED WITHOUT FURTHER EVENT. TAXIED TO THE GATE. MX TROUBLESHOT AND TESTED THE YELLOW ENSDR AWXA200501116Line · rupturedCREW REPORTED SYS "A" HYD FAILURE ON FINAL WHEN LOWERING GEAR. LT GEAR INTRANSIT INDICATION ILLUMINATED. MANUALLY EXTENDED GEAR AND RECEIVED THREE GREEN GEAR DOWN AND LOCKED INDICATION. TOWER VERIFIED ALL THREE GEARS WERE DOWN. A/C LANDED WITH NO NLG STEERSDR AWXA200501091O-Ring · leakingPHX - EMERGENCY LANDING - FLT 506 - DURING CRUISE, EN ROUTE TO PHX, CREW RECEIVED ECAM MSG HYD Y RSVR LO LVL. CREW MADE PRECAUTIONARY EMERGENCY LANDING IN PHX. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED UNION O-RINGS ON THE HYDRAULIC SDR QXEA200501254B-Nut · looseGEG FLIGHT NR 2365: ON PUSHBACK, HYDRAULIC FLUID WAS NOTED LEAKING FROM NOSE GEAR. AIRCRAFT WAS PULLED BACK TO GATE. MAINTENANCE TIGHTENED LOOSE B-NUT AT NLG DOWN ACTUATOR LINE. PRESSURIZED ALL HYDRAULIS SYSTEMS. NO LEAKS FOUND. CYCLED NOSE WHEEL STEERINGSDR XN0A1267Hydraulic System · leakingLOSS (A) SYS HYD ON TAKEOFF. (ORIG/OPEN)SDR AWXA200501074Line · rupturedLAS - AIR TURN BACK - FLT 372 - DURING CLIMB, CREW RECEIVED GREEN HYDRAULIC LOW RESERVOIR MESSAGE AFTER SHORTLY RAISING GEAR. RETURNED TO LAS AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT WAS TOWED BACK TO THE GATE. MAINTENANCE FOUND THE LT LANDING GEAR DOOSDR COMA0560506Actuator · faultyFLIGHT 5321 - DURING CLIMBOUT OF CVG THE NR 2 HYDRAULIC C/B TRIPPED. REPLACED THE NR 2 HYDRAULIC SOV ACTUATOR.SDR 2005UALA00995Hydraulic System · malfunctionedRETURNED TO FIELD DUE TO HYDRAULIC PROBLEMS. FOUND HYDRAULIC PRESSURE LINE WITH STREAMING LEAK. REPLACED HOSE, REPLACED RETURN AND CASE DRAIN FILTERS, AND SERVICED SYSTEM TO FULL. LEAK CHECKED SAME. PRESSURE WASHED FUSELAGE BELLY AS REQUIRED. RETURNED AIRSDR RYNA200500029Line · leakingEICAS MESSAGE LEFT HYDRAULIC QUANTITY AND PRESSURE LOST. QUANTITY LEVEL 0.10 LT. REMOVED AND REPLACED RIGHT DOWNLOCK ACTUATOR RETURN LINE. LEAK CHECK GOOD, ALSO FOUND NR 1 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. REMOVED AND REPLACED ENGINE DRIVE PUMP AND PRESDR KBM2005F00271Line · leakingIN-FLIGHT HYDRAULIC BOOST, INOPERATIVE. REPLACED LEAKING HYDRAULIC SUPPLY LINE FROM PUMP TO FILTER. (K)SDR N93A1316O-Ring · leakingLOSS OF HYDRAULIC FLUID ON THE FLIGHT SIDE HYDRAULIC SYSTEM. FOUND PRESSURE TRANSMITTER O-RING AT FAULT.SDR DXTA200500966Pressure Switch · leakingTOTAL LOSS OF HYDRAULIC FLUID ON THE NR 1 HYD SYSTEM IN FLIGHT. REMOVED NR 1 HYDRAULIC SYSTEM PRESSURE SWITCH CODE (L30GI) P/N 7G979, S/N 1722 AND REPLACED WITH NEW SWITCH P/N 7G979 , S/N 2784. REMOVED NR 1 & NR 2 ENGINE HYDRAULIC PUMPS AND INSPECTED FLUID ASDR DXTA200500969Line · brokenHYDRAULIC LINE IN RIGHT MAIN GEAR WELL BROKE AFTER T/O HAD TO BLOW GEAR DOWN AND USE ALL BACKUP SYSTEMS HAD RIGHT AND LEFT HYD LOW VOLUME AND PRESSURE LIGHTS. ITEM IS UNDER INVESTIGATION.SDR CA050920003Fitting · cracked(CAN) AFTER LANDING GEAR HAD RETRACTED, THE PILOTS NOTICED A DROP IN HYDRAULIC QUANTITY AND PRESSURE. AIRCRAFT RETURNED TO BASE. INSPECTION FOUND A CRACKED FITTING ON THE NR 2 HYDRAULIC PRESSURE MANIFOLD. EDP WAS REPLACED AS IT WAS RUN DRY FOR MORE THAN 15 SDR SF200509121Warning Light · illuminated9-12-2005, FLIGHT 7571 FROM IAD TO DAY, ON DESCENT, AIRCREW RECEIVED HYD LIGHT ON WITH BOTH MAIN AND EMERGENCY ACCUMULATOR'S LOW. AIRCREW FOLLOWED MEMORY ITEMS AND QRH AND LANDED A/C IN DAY.SDR AU510002120Line · failedNOSE LANDING GEAR ACTUATOR FLEXIBLE HYDRAULIC LINE RUPTURED. LOSS OF NR 2 SYSTEM HYDRAULIC FLUID.SDR 2005FA0001476O-Ring · leakingHYD LINE WAS REPLACED DUE TO CRACK IN FLARE AT TEE FITTING. REPLACEMENT OF LINE REQUIRED INSTALL OF NEW O-RING, WHERE TEE FITTING ATTACHES TO FLIGHT CTRL HYD SHUT OFF VALVE. AFTER INSTALL OF HYD LINE AND O-RING, A LEAK CHECK WAS PERFORMED. NO LEAKS WERE NOTSDR VTZA200500179Line · leakingHYDRAULIC 3 LOW PRESSURE MESSAGE. REPLACED LINE ON 3A PUMP.SDR AU510001838Hose · leaking(AUS) RT ENGINE DRIVEN HYDRAULIC PUMP TO PYLON QUICK DISCONNECT PRESSURE HOSE LEAKING.SDR ASOA05747Transducer · failedFLT 4620 - DURING CRUISE FROM ABE-ATL, AT APPROX 28,000 FEET THE CREW RECEIVED A HYD NR 1 HI TEMP MESSAGE. THE QRH WAS COMPLIED WITH AND THE CREW SHUTDOWN THE LEFT ENGINE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO GSP, LANDING SAFELY. MAINTENANSDR DL76L050533Filter · bypassingRETURN TO GATE FOR PASSENGER CONCERN OF SURGING SOUND UNDER FLOOR AT MID CABIN AREA. REPLACED MODULATING AIR VALVE, NO HELP. REPLACED CONTROL PRESSURE SWITCH, NO HELP. FOUND FILTER BYPASS POPPED. REPLACED FILTER AND ADP, LEAK CHECK GOOD. OPS CHECK NORMAL.SDR ASMF200509004Hose · damagedDURING TRANSIT CHECK, IT WAS DETECTED A HYDRAULIC LEAK AT THE SLATS PRESSURE LINE FORWARD ADF ANTENNA. THE SLATS PRESSURE LINE WAS REPLACED IAW MM 29-10-00, TESTED CORRECT.SDR CA050913004Tube · cracked(CAN) DURING A POST FLIGHT WALK AROUND PILOT NOTICED HYDRAULIC FLUID DRIPPING FROM LT WHEEL WELL. FURTHER INVESTIAGTION FOUND FLUID ACTUALLY DRIPPING FROM ABOVE IN THE FORWARD LT BAGGAGE AREA WHERE THE HYDRAULIC SYSTEM PIPING RUNS. A SINGLE PIPE GOING INTO A MSDR KC82005F00007Hose · leakingCREW NOTICED A LOSS OF HYDRAULIC PRESSURE. PERFORMED EMERGENCY GEAR EXTENSION AND LANDED WITHOUT INCIDENT. AUX HYDRAULIC PUMP SUPPLIED PRESSURE FOR FLAPS AND BRAKES UPON LANDING. FOUND NOSE GEAR ACTUATOR RETRACT HOSE LEAKING AT BULKHEAD FITTING IN THE NOSE SDR HALA0500914Line · leakingCENTER HYD QTY DROPPED TO .24 AND MAY HAVE LEAKED FROM RIGHT MAIN AREA. GROUND CONTROL REPORTED FIRE FROM 45 MAIN AREA WHICH WAS PUT OUT BY FIRE TRUCKS. FOUND PIN HOLE LEAK ON HYD LINE. REPLACED BOTH HYD FLEX LINES TO RIGHT MLG POSITIONER ACT. ACCOMP HEAT SDR DLM88050513Hydraulic System · contaminatedLEFT HYD PRESS WENT TO 0 QUANTITY, NORMAL ON DESCENT INTO BDL. RECOVERED PRESS WITH TRANS PUMP ON. DECLARED EMERGENCY AND LANDED UNEVENTFULLY. BLED AIR FROM LEFT HYD RESERVIOR, RAN LEFT ENGINE, CYCLED ALL FLT CONTROLS THRU SEVERAL TIMES. SERVICED AND BLED SDR SWAA052673Line · chafedAIR TURNBACK/DECLARED EMERGENCY, LOST A-SYSTEM HYDRAULICS. REMOVED AND REPLACED A-SYSTEM HYDRAULIC SUPPLY LINE PER MM.SDR CA050909006Line · cracked(CAN) AIRCRAFT LANDED AND FLIGHT CREW NOTICED HYD LEAK. MAINTENANCE WAS CONTACTED. FOUND A CRACKED FLAP UP LINE IN THE BELLY OF THE AIRCAFT. TUBE WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE.SDR SWAA052672Line · leakingDIVERSION, LOST A-SYSTEM HYDRAULIC PRESSURE & FLUID. REMOVED AND REPLACED A-SYSTEM HYDRAULIC HEAT EXCHANGER LINE & HYDRAULIC CASE DRAIN FILTER PER MM.SDR 637090205Actuator Valve · defectiveL-R AIL HYD OFF WARNING ACTIVATED IN FLIGHT, L - AIL CB POPPED ON GROUND.SDR CA050913006Hose · ruptured(CAN) PILOT NOTICE HYDRAULIC FLUID LEAKING FROM RT LOWER FUSELAGE TO WING FAIRING AFT MAIN SPAR. AP ON INSPECTION, FOUND LANDING GEAR HOSE RUPTURED. REPAIRED HOSE ASSY P/N 17766-02 BY REPLACING HOSE.SDR 05FDEA02717Tube · chafedHYD SYS A FAILED (W/FLAPS 15) WHILE CONFIGURING TO LAND AT MEM. REPLACED ENGINES NR 1 AND 2 ENGINE DRIVEN HYDRAULIC PUMPS, REF MM29-11-041-2. REPLACED BOTH CASE DRAIN FILTERS. REPLACED SYSTEM "A" HYDRAULIC RETURN FILTER, R/I. REMOVED AND REPLACED SYSTEM A
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