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 2000UALA00310Switch · failedAFTER PUSH, BEFORE TAXI, GOT ECAM HYDRAULIC GREEN SYSTEM LOW PRESSURE. SYSTEM PRESSURE SHOWS 3000 PSI. QUANITITY NORMAL. NOSEWHEEL STEERING INOPERATIVE. *S/D* REPLACED GREEN SYSTEM FLIGHT CONTROL PRESSURE SWITCH, ITEM 1151GN.SDR AU000443Pipe · cracked(AUS) LEFT HYDRAULIC FILTER HOUSING PRESSURE PIPE SPLIT AT OUTBOARD RADIUS OF BEND. LOSS OF HYDRAULIC FLUID.SDR SCNA00052Line · rupturedAFTER TAKEOFF FROM PVR, THE LANDING GEAR HANDLE WOULD NOT MOVE FROM THE DOWN POSITION. THE CREW RETURNED TO POINT OF ORIGIN. A HYDRAULIC LINE WAS FOUND RUPTURED ON THE LT MLG BOOGIE TRIM CYLINDER. THE HYDRAULIC LINE WAS REMOVED AND REPLACED WITH A TEMPORARYSDR CA000614030Pressure Switch · failed(CAN THE HIGH PRESSURE CONDITION COULD NOT BE DUPLICATED IN THE HANGAR. THE PREVIOUS DAYS FLYING WAS A TRIP FROM ST. JOHNS TO GOOSE BAY, 2 HRS AT FL 280 AND -45 DEGREES. SUSPECT THE HYD SYSTEM, UPON BEING SUPER CHILLED AT ALTITUDE, IS CAUSING THE OVER PRESSDR SWAA001002Valve · inoperativeDECLARED EMERGENCY, A-SYS HYD FAILED DURING APPROACH. REMOVED AND REPLACED A-SYS HYD MODULE CHECK VALVE PER MM.SDR AU000805Hose · worn(AUS) NR 2 ENGINE HYDRAULIC PUMP PRESSURE HOSE CHAFED THROUGH BY ADEL CLAMP. LOSS OF YELLOW' SYSTEM HYDRAULIC FLUID.SDR 20000720SH031B-Nut · looseGEAR WOULD NOT EXTEND. CIRCUIT BREAKER TRIPPED. RE-SET, BUT NO HELP. GEAR FREE FALL FAILED TO LOCK ALL GEAR DOWN. RIGHT MAIN COLLAPSED UPON LANDING. FOUND B-NUT ON RIGID LINE BELOW HYDRAULIC POWER PACK LOOSE AND LEAKING HYDRAULIC FLUID. GEAR OPERATED NORSDR 0002081239Hydraulic Line · rupturedDURING CLIMB AT 4000 FEET (BOM), LOST NR 2 HYDRAULIC SYSTEM. FLIGHT ATTENDANTS REPORTED HOLE IN LEFT WING. DUMPED FUEL AND RETURNED TO BOM. INSPECTION REVEALED TIRE BLOWN SEVERING HYDRAULIC LINES AND DAMAGING WING AND FLAP AREA. WORK IN PROGRESS.SDR DLM11001042Line · crackedNR 2 HYD SYST EMPTY, LOSS OF FLUID DURING ENG REV ON GROUND. LEAK TRACED TO STOW LINE, CRACKED AT TOP OF HCU HYD LINE END. REPAIRED PIPE SECTION APPROX 20 INCHES LONG AND NEW COULPLING FITTED BY KLM IAW 20-10-01-02. REV CYCLED SEVERAL TIMES AND NO LEAKS FOSDR DL72S001033Line · rupturedTOTAL LOSS OF B HYDRAULIC SYS. HYDRAULIC QTY WAS ZERO, PRESS WAS FLUCTUATING. FLIGHT CREW ADVISES LOSS BEGAN 50 MILES FROM ATL. NO CONFIGURATION CHANGE. FOUND PRESS LINE ON B SYS ELEC PUMP RUPTURED. REPLACED LINE.SDR DLM88001029Line · looseRIGHT HYD SYS QTY DECREASED TO 4 QTS. RT HYD SYS TURNED OFF. SECURED LOOSE HYD PRESS LINE IN RIGHT SIDE OF TAIL COMPARTMENT.SDR 20000816AP005Line · brokenDFW - FLT 1321 - DURING CRUISE FLIGHT, THE CREW NOTICED THE HYD PRESSURE LOW LIGHTS CAME ON. HYDRAULIC PRESSURE GAUGES WERE CHECKED AND THE LACK OF HYD PRESSURE WAS CONFIRMED. THE FLIGHT CONTINUED NORMALLY. THE CREW PERFORMED AN EMERGENCY GEAR EXTENSION ANDSDR AU000427Pipe · corroded(AUS) LANDING GEAR ''UP'' PIPE CORRODED AND LEAKING. LOSS OF HYDRAULIC FLUID. LEFT MLG DOWNLOCK STIFF TO OPERATE. AIRCRAFT OPERATES IN A SALT LADEN ENVIRONMENT.SDR DLM88001018Line · crackedPOST FLIGHT ARRIVAL AT GATE, CABIN FILLED WITH OILY SMOKE. APU WAS OPERATING AS WELL AS LEFT AIR CONDITIONING PACK. FOUND HYDRAULIC LINE LEAKING RIGHT T/R CONTROL VALVE, LOCATED IN TAIL COMPARTMENT. APU INGESTED HYDRAULIC FLUID. REPLACED HYDRAULIC LINE ANDSDR AWXA0000331Solenoid Valve · leakingEMERGENCY LANDING, GREEN HYDRAULIC SYSTEM LOW PRESSURE. FOUND LEAK AT PTU SOLENOID VALVE. REPLACED BOBBINS AND SEALS ON SOLENOID VALVE, LK AND OPS CHK GOOD. RECOMMENDATION: MONITOR.SDR CA000530006Line · failed(CAN) HYD LEAK AT NLG DOOR LINE. REPLACED LINE.SDR LR7A0051Line · leakingAFTER LANDING GEAR EXTENSION ON APPROACH KUZ FLIGHT CREW NOTED LOSS OF UTILITY HYDRAULIC SYSTEM PRESSURE. LANDED KUZ WITHOUT INCIDENT.REPLACED NLG DOWN FLEX LINE IAW SMP 581 91-00 PG 201 DUE LEAKING. OPS CHECK GOOD PER TABLE 29-00-08, NO LEAKS. SERVICED UTISDR 20000703AP009Pressure Switch · looseJFK-SAL - FLT 571 - THE AIRCRAFT LOST THE GREEN HYDRAULIC SYSTEMS QUANTITY, FLIGHT CREW PERFORMED ABNORMAL PROCEDURES FOR GREEN HYDRAULIC SYSTEM LOSS. THE AIRCAFT PERFORMED AN UNEVENTFUL LANDING AT EL SALVADOR STATION. AT EL SALVADOR STATION MAINTENANCE TECHSDR ASOA00058Line · failedFLT 4582 - EN ROUTE TO QRH AT 29,000 FEET, CREW RECEIVED HYDRAULIC 2 LOW PRESSURE MESSAGE WITH A SLIGHT SHUTTER AND A DIPPING OF WING WHILE IN AUTOPILOT. CREW FOLLOWED QRH PROCEDURES AND DIVERTED TO RIC. AIRCRAFT LANDED SAFELY. MAINTENANCE REPLACED THE FLEXSDR 2000UALA00274Hose · rupturedLANDED IN DEN UNDER AMBER ALERT DUE TO HYDRAULIC SYSTEM FAILURE. *S/D* AIRCRAFT EXPERIENCED A COMPLETE LEFT SYSTEM HYDRAULIC LOSS WHEN THE RT MLG PRESSURE HOSE FOR THE UPLOCK ACTUATOR RUPTURED. REPLACED HOSE.SDR CA000530073Line · ruptured(CAN) ON LANDING CENTER HYD SYSTEM FLUID DROPPED TO ZERO. PRESSURE LINE FROM CENTER HYD SYS PUMP RUPTURED. LINE REPLACED, SYS SERVICED AND LEAK CHECK OK.SDR 2000UALA00265Coupling · leakingDIVERTING WITH LOSS OF YELLOW SYSTEM. *S/D* FOUND DAMAGED O-RING AT POWER TRANSFER UNIT QUICK DISCONNECT FITTING. REPLACED O-RING, SERVICED SYSTEM AND LEAK CKD. NO FURTHER LEAKS NOTED.SDR N8TA00051701Hose · leakingTHREE MINUTES AFTER TAKEOFF, CREW OBSERVED EICAS MESSAGE, LEFT HYDRAULIC SYSTEM QUANTITY AND QUANTITY DROPPED TO .20; SYSTEM WAS DEPRESSURIZED. ALL GEAR EXTENSIONS AND ALT FLAP EXTENSIONS ACCOMPLISHED FOLLOWED BY AN UNEVENTFUL LANDING. UPON INVESTIGATION, THSDR F3LA00093Line · leakingLAS - FLT 778 - AIR TURN BACK. FLIGHT CREW REPORTED B-SYSTEM HYDRAULIC FAILURE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING HYDRAULIC LINE TO THE RUDDER PCU. (X)SDR 2000UALA00256Line · leakingLOST A HYDRAULIC SYSTEM. CONTINUED TO ORD. EXTENDED GEAR MANUALLY. TOWED TO GATE. *S/D* FOUND NR 2 ENG HYD PUMP PRESS OUT LINE CRACKED AT SUPPORT CLAMP. REPLACED INLET PRESSURE LINE AND RETURN LINE. CHECKED CASE DRAIN FILTER. SERVICED HYDRAULIC SYSTEM.SDR AU000398Hose · leaking(AUS) HORIZONTAL STABILISER TRIM CONTROL MODULE HYDRAULIC HOSE LEAKING. LOSS OF HYDRAULIC FLUID. HOSE IS ORIGINAL FITMENT ITEM FROM AUGUST 1987.SDR RRXA000295Line · leakingHYDRAULIC FAILURE AND COMPLETE FLUID LOSS DURING APPROACH. SAFETY WIRE BROKEN ON AIR BRAKE HANDLE. FOUND HARD LINE LEAKING AT LT MID FLAP ACTUATOR. INSTALLED FLEX LINE PER EWA ACFT MM CHAP 7. LEAK CK OK. RESAFTIED AIR BRAKE HANDLE.SDR 20000717AP002Line · brokenFLT 1315 - DEN - BOTH HYDRAULIC PUMP LIGHTS CAME ON DURING CRUISE AND HYDRAULIC PRESSURE DROPPED BELOW NORMAL RANGE, BUT DIDN''T GO TO 0 PSI. CREW EXTENDED GEAR MANUALLY AND LANDED WITH NO FURTHER INCIDENT. THE HYDRAULIC PRESSURE LINE BROKE JUST AFT OF THE FSDR AALA20000742Transmitter · leakingMCO - FLT 915 - DURING FLIGHT, GREEN HYDRAULIC SYSTEM LEAKING. DIVERTED AND LANDED MCO WITHOUT INCIDENT. REPLACED HYDRAULIC PRESSURE TRANSMITTER. SYSTEM GROUND CHECK NORMAL OPERATION. (M)SDR 20000614SH002Line · brokenDEN - FLT 1315 - BOTH HYDRAULIC PUMP LIGHTS CAME ON DURING CRUISE AND HYDRAULIC PRESSURE DROPPED BELOW NORMAL RANGE, BUT DID NOT GO TO ZERO PSI. CREW EXTENDED GEAR MANUALLY AND LANDED WITH NO FURTHER INCIDENT. THE HYDRAULIC PRESSURE LINE BROKE JUST AFT OF THSDR 20000602SH017Line · failedDEN - FLT 1315 - BOTH HYD PUMP LIGHTS CAME ON DURING CRUISE AND HYD PRESSURE DROPPED BELOW NORMAL RANGE, BUT DID NOT GO TO ZERO PSI. CREW EXTENDED GEAR MANUALLY AND LANDED WITH NO FURTHER INCIDENT. HYD PRESSURE LINE BROKE AFT OF FLARE UNDER FERRULE. TWO CLASDR CA000516016Line · chafed(CAN) BETWEEN FS 52.00 AND LWS 60.8 WHERE LEFT FUEL TUBE ASSY AND HYD TUBE ASSY GO THROUGH THE WING ROOT. IT WAS FOUND THAT THE HYD PRESSURE TUBE WAS CHAFING AGAINST LT FUEL TUBE ASSY.SDR CA000516011B-Nut · loose(CAN) DURING FLIGHT, BOTH HYDRAULIC LIGHTS ILLUMINATED. THE AIRCRAFT RETURNED TO BASE AND HAD TO USE EMERGENCY LANDING GEAR EXTENSION PROCEDURES. AFTER AN UNEVENTFUL LANDING, MAINTENANCE PERSONNEL FOUND A LOOSE AND LEAKING B NUT ONTHE HYDRAULIC RESERVOIR (POWSDR CA000530062Power Unit · leaking(CAN) LOSS OF YELLOW SYSTEM HYD. SYS FLUID. POWER TRANSFER UNIT DEACTIVATED. INVESTIGATION REVEALED PTU LEAKING AT QUICK DISCONNECT. SEALS REPLACED.SDR DLM88000912Line · leakingAT CRUISE, RT HYD QTY DECREASED TO 1 QT. FOUND FLEX LINE TO RETURN MODULE LEAKING. REPLACED SAME.SDR SCNA00041Control Valve · crackedDURING CLIMB, HYDRAULIC QUANTITY IN THE NR 3 SYSTEM WENT TO ZERO. FOUND UPPER PRIMARY STABILIZER TRIM CONTROL VALVE CRACKED. REMOVED AND REPLACED VALVE IAW 27-40-2. OPERATIONAL AND LEAK CHECKS GOOD.SDR CA000516004Shutoff Valve · failed(CAN) DURING HYD PUMP REPLACEMENT EXCESSIVE AMOUNT OF OIL WAS PUMPED WHEN INLET LINE TO HYD PUMP DISCONNECTED. FURTHER INVESTIGATION FOUND THE FIREWALL S/O VALVE DID NOT CLOSE WHEN SELECTED. DIODE D101 FAILED. PARTS REPLACED.SDR USAASB00134Hose · failedIAD - FLT 2755 - DURING CLIMB-OUT FROM IAD, THE NOSE LANDING GEAR WOULD NOT RETRACT. CREW NOTICED A DROP IN HYDRAULIC PRESSURE. THE NOSE LANDING GEAR NEVER UNLOCKED AS A STEADY NOSE GEAR GREEN LIGHT REMAINED ILLUMINATED. FLIGHT RETURNED TO FIELD AT IAD AND SDR GAIA00276Line · leakingFLT 1772 - BNA-FWA - EN ROUTE TO FWA, THE AIRCRAFT WAS REQUIRED TO DIVERT TO ORD DUE TO WEATHER IN FWA. SHORTLY AFTER DIVERTING THE ENTIRE ''A'' SYSTEM HYDRAULIC PRESSURE AND QTY WAS LOST. THE CREW DECLARED AN EMERGENCY AND CONDUCTED THE ABNORMAL CHECKLIST. SDR 2000UALA00233Hose · rupturedRETURNED TO DEN DUE TO LOSS OF HYDRAULIC FLUID IN THE LEFT HYDRAULIC SYSTEM. *S/D* PRESSURE HOSE FOR DOWNLOCK ACTUATOR WAS LEAKING. REPLACED HOSE.SDR 2000UALA00232Selector Valve · leakingYELLOW SYSTEM LO QTY IN FLIGHT. TURNED OFF PUMP PER ECAM. *S/D* FOUND LEAK AT AUTO BRAKE SELECTOR. REPLACED PACKING. SERVICED YELLOW SYSTEM TO FULL.SDR ABXA000225Line · leakingON DEPARTURE, AIRCRAFT EXPERIENCED LOSS OF HYDRAULICS. RESERVOIR LOW LIGHT ILLUMINATED AND HYDRAULIC QUANTITY WAS DECREASING. IMMEDIATE ACTION ITEMS WERE ACCOMPLISHED, RESULTING IN HYDRAULIC QUANTITY DECREASE STOPPING IN NORMAL RANGE. REPLACED LEAKING LINE SDR IXXA0000018Line · defectiveEN ROUTE FROM KWI TO HIK, THE FLIGHT CREW NOTICED THE MAIN HYDRAULIC SYSTEM FLUID QUANTITY DECLINING. THE FLIGHT CREW FOLLOWED COMPANY EMERGENCY PROCEDURES, DECLAIRED AN EMERGENCY, AND CONTINUED TO HIK FOR AN UNEVENFUL LANDING. MAINTENANCE INSPECTED THE AIRCSDR DHL200074002Line · brokenNR 1 A SYSTEM PUMP LIGHT ILLUMINATED AFTER TAKEOFF, HYD PRESS 3000 PSI, HYD QTY ZERO. SOON AFTER NR 2 PUMP A SYSTEM LIGHT ILLUMINATED AS HYD PRESS DECREASED. FOUND NR 1 PUMP CASE DRAIN LINE BROKEN. REPLACED CASE DRAIN LINE PER MM 29-11-33, REPLACED NR 1 HYDSDR 20000501SH037Manifold · mismanufacturedFLUID PORT NOT DRILLED IN THE MANIFOLD COMPLETELY FOR PROP ''P''.SDR 8GA200000002Hydraulic System · leakingFLT 033 FROM KELP TO KDAY, AFTER TAKEOFF DURING CLIMB TO CRUISE ALTITUDE, FLIGHT CREW OBSERVED STEADY AND CONTINUAL LOSS OF SYSTEM A HYDRAULIC FLUID TO BELOW 2.4 GALLONS FLUID QUANTITY. RETURNED TO KELP AND LANDED WITHOUT FURTHER INCIDENT. CHECKED AIRCRAFT HSDR C2XA00CL034Hydraulic Line · failedCLE - FLT 3210 - THE CREW REPORTED THAT AFTER TAKEOFF, LOST ALL GREEN HYDRAULIC PRESSURE. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND CHAFFED HYDRAULIC LINE AT RESERVOIR. MAINTENANCE REPLACED HYDRAULIC LINE. SDR CA000501004Line · split(CAN) ON SHORT FINAL, THE 32 HYD ISO VALVE, ROLL SPOILER O/B HYD AND NOSE WHEEL STEERING CAUTION LIGHTS ILLUMINATED.ON THE RUNWAY, PILOTS OBSERVED NO NOSE WHEEL STEERING. LT WING SPOILER O/B ACTUATOR PRESSURE LINE FOUND SPLIT.SDR P2EA00115Line · leakingCANCUN - FLT 8009 - LOST A-SYSTEM HYDRAULIC QUANTITY DURING FLIGHT FROM BRO/MRO. DIVERTED TO MMUN (CANCUN) LANDING UNEVENTFUL. REPAIRED .25 INCH HYDRAIULIC LINE PER MM CHAPTER 20, SERVICED HYDRAULIC SYSTEM, LEALK CHECKED OK. (X)SDR AU000204Fitting · mismanufactured(AUS) NR 6 AND NR 7 SPOILER PANELS HYDRAULIC CROSS FITTING PASSAGEWAYS NOT DRILLED. THE FITTING WAS A NEWLY INSTALLED ITEM.
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