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 AALA20020375Hydraulic Line · leakingDFW - FLT 576 - ON TAKEOFF DFW, ACRID SMOKE FILLED CABIN. RETURNED TO DFW AND LANDED WITHOUT FURTHER INCIDENT. REPAIRED HYDRAULIC LEAK INTO DISTRIBUTION DUCT. REPLACED RECIRCULATION FAN FILTERS AND PRESSURE REGULATOR ON NR 1 AND NR 2 SYSTEM, AND PNEUMATIC DSDR GMZ2002F00000Hose · failedNOSE GEAR WILL NOT EXTEND. NEW HOSES FABRICATED 8 HOURS BEFORE, MALFUNCTIONED. RETEST HOSE, REMOVED AND CHECKED FOR RESTRICTIONS. RESTRICTION EVIDENT. REMOVED ORIFICE AND FILTER AT FIREWALL. FOUND RUBBER TRAPPED ORIFICE (UPSTREAM) AND RUBBER AND METAL PARSDR MEX2002093Hydraulic Line · brokenFLT 402 - PVR-MEX - DURING TRANSIT CHECK DETECTED A LEAK IN THE RIGHT HYDRAULIC SYSTEM. A BROKEN LINE AT ACCESSORY COMPARTMENT AFFECTING THE VENTRAL STAIRWAYS, THE RIGHT ENGINE REVERSE AND THE DIRECTION RUDDER. A FLEXIBLE TUBE WAS INSTALLED. DURING OVERNIGHSDR AWXA200200259O-Ring · leakingPHX - EMERGENCY - FLT 0005 - YELLOW HYDRAULIC SYSTEM INDICATED LOW PRESSURE AND QUANTITY, MADE NORMAL LANDING, BUT BRAKES OVERHEATED. INSPECTION OF HOT BRAKES. AFTER BRAKES INSPECTED TAXIED TO GATE, HYDRAULIC QUANTITY WHEN AIRCRAFT TAXIED IN WAS "0". BELLY SDR 02088650TransducerDuring cruise of the flight, the crew noted the #1 hydraulic temperature at greater than 178 degrees C. The crew followed the QRH procedures shutting down the #1 engine and returned to IAD where the aircraft landed without incident. Maintenance personnel remSDR MEX2002087Bearing · failedFLT 574 - CUN-MEX - AIRCRAFT ARRIVED TO PLATFORM WITH HYDRAULIC FLUID LEAK IN THE RIGHT SYSTEM. IT WAS CHECKED AND THE LEAK WAS FOUND AT THE PTU SHUTOFF VALVE. BEARINGS WERE CHANGED IAW MM 29-10-08. DURING OVERNIGHT SERVICE WERE DETECTED THAT THE SEPARATOR SDR ERA2002F00000Nut · splitON INBOUND FLIGHT, THE PRIMARY HYDRAULIC SYSTEM FAILED. AIRCRAFT WAS LANDED AT THE FIRST AVAILABLE PLACE. INSPECTED AND FOUND PRIMARY HYDRAULIC TANK EMPTY DUE TO LEAK AT SPLIT HYDRAULIC FITTING JAM NUT. REMOVED AND REPLACED WITH A SERVICEABLE NUT AN ORING. SDR SWAA020652Fuse · defectiveAIR TURNBACK, DURING CLIMB L/E DEVICES WOULD NOT RETRACT. UPON LANDING DEVICES WOULD NOT FULLY EXTEND. REMOVED AND REPLACED EXTEND AND RETRACT HYD FUSES PER MM.SDR PCAA0203039Hydraulic Line · leakingPHL-HPN FLIGHT 3668 AT 13,000 FEET IN CRUISE FLIGHT NR 1 HYDRAULIC SYSTEM FAILED. ROLL SPOILER INBOARD HYDRAULIC AND NR 1 HYDRAULIC ISOLATION LIGHTS ILLUMINATED. EMERGENCY DECLARED AND FLIGHT DIVERTED TO ISP. HYDRAULIC QUANTITY AT .5 QUART UPON LANDING. NOSDR CA020415002Line · leaking(CAN) ON SELECTION OF FLAPS NR 1 HYD PRESSURE CAUTION LIGHT ILLUMINATED AND STANDBY AND MAIN PRESSURES WENT TO ZERO. FLAPS STOPPED AT 4 DEGREES. RUNWAY LENGTH IN YSB NOT SUFFICIENT DIVERTED TO YYB.SDR HEEA078523Hose · kinkedHOSE KINKED. SCRAPPED AND REPLACED WITH SERVICEABLE PART.SDR AUS20020281Hose · ruptured(AUS) NR 1 ADP PRESSURE HOSE LOCATED BETWEEN THE PUMP AND THE PRESSURE MODULE RUPTURED. LOSS OF HYDRAULIC FLUID.SDR 2002UALA00529Hydraulic Line · rupturedLOSS OF LEFT HYDRAULIC QUANTITY LEVEL DECREASED TO 1.8 WITH ASSOCIATED SYSTEM PRESSURE LIGHT ILLUMINATION. LEFT MAIN DOWNLOCK ACTUATOR HYDRAULIC LINE RUPTURED. REPLACED HYDRAULIC LINE.SDR ARWA20020314Fluid · lowUPON LANDING, HYDRAULIC PRESSURED DROPPED TO ZERO AFTER GEAR EXTENSION. ALL CHECKLIST ACCOMPLISHED. SERVICED HYDRAULIC IAW MM 12-4-0, NO LEAKS NOTED.SDR HEEA078366Hose · kinkedHYDRAULIC HOSE KINKED.SDR HEEA078358Hose · corrodedTAIL ROTOR SERVO PRESSURE HOSE IS CORRODED AT SLEEVE DUE TO DISSMILAR METAL.SDR CA020408007Line · ruptured(CAN) AFTER LANDING, HYDRAULIC FLUID NOTICED STEAMING FROM NR 3 BRAKE UNIT AND DRIPPING FROM NR 3 & 4 BRAKE UNIT. LEAK CHECK REVEALED FLUID LOSS FROM NR 4 (RT OUTBOARD) BRAKE UNIT PIPE 1/8 INCH FORWARD OF BANJO FITTING LOCATED ON TOP OF BRAKE. IMPROVEMENTS ISDR CA020326001Belt · debonded(CAN) HYDRAULIC BELT WAS STARTING TO DEBOND NEAR THE DIRECTION OF ROTATION ARROW NEAR THE BONDED JOINT. THE TTSN OF THE BELT BY THE MANUFACTURE IS 600 HOURS. WE HAVE FOUND THAT THE OCCURRENCE OF DEBONDING IS HAPPENING TOO OFTEN, SO OUR INSPECTION OF THE BELT ISDR 2002F00364Manifold · leakingAT THE ARRIVAL OF FLT 221, FLIGHT CREW REPORTED THE YELLOW RESERVOIR LOW LEVEL. ON GROUND TECHNICIANS FOUND A LEAK AT THE PTU MANIFOLD. THE PTU MANIFOLD WAS REPLACED AS PER AIRCRAFT MM 29-13-15 AND OPERATIONAL TEST WAS PERFORMED IAW AIRCRAFT MM 29-23-00. RESDR ARWA20020310Hydraulic Line · leakingWHEN READY TO TAXI, HYDRAULIC QUANTITY GAUGE INDICATED LOSS OF FLUID, HYDRAULIC PRESSURE GAUGE INDICATED LOSS OF PRESS. ACCOMPLISHED APPROPRIATE CHECKLIST, RETURNED TO RAMP. REMOVED AND REPLACED HYDRAULIC PRESSURE LINE FROM NR 3 ENGINE HYDRAULIC PUMP, OPS CHSDR 2002FA0000596Housing · brokenHOUSEING IS BROKEN. BODY IS TOO WEAK.SDR CA020411003Line · cracked(CAN) -DURING APPROACH PILOT SELECT GEAR DOWN. THEN PILOT NOTICE MANY CAUTION LIGHTS: SPOILER, ISOVALVE, STEERING AND HYD TANK NR 2 LEVEL EMPTY. BUT GEAR LOCK DOWN OK 3 GREEN LIGHTS. AIRCRAFT LAND NORMALLY AND SAFELY. MAINTENANCE FOUND ALUMINIUM HYDRAULIC LISDR C2XA02CL077Switch · crackedCLE FLIGHT#3232 THE CREW REPORTED #1 HYDRAULIC SYSTEM FAILED IN FLIGHT.THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND FOUND THE #1 HYDRAULIC SYSTEM PRESSURE SWITCH HAD CRACKED.THE SWITCH WAS REPLACED.OPOERATIONAL CHECKS WERSDR 2002FA0000775Fitting · brokenPLASTIC T FITTING IN HYDRAULIC LINE BETWEEN RESERVOIR AND BRAKE CYLINDERS BREAKS OFF. THIS ALLOWS THE BRAKE FLUID TO ESCAPE.SDR XNOA01039Valve · leakingDURING CRUISE, HYDRAULIC GREEN SYSTEMS 'LEVEL LO' LITE ILLUMINATED WITH HYD QTY INDICATING NEAR ZERO. HYDRAULIC SYSTEMS LOSS AND LANDING GEAR GRAVITY EXTENSION CHECKLIST ACCOMPLISHED. UPON INSPECTION FOUND NLG VENT VALVE LEAKING. R2 NLG VENT VALVE IAW A300 SDR CA020328003Power Unit · failed(CAN) IN CRUISE AFTER APPROXIMATELY 1.5 HOURS IN FLIGHT, YELLOW HYDRAULIC FLUID LEVEL WENT LOW LEVEL. AIRCRAFT DIVERTED AND LANDED IN WINNIPEG. POWER TRANSFER UNIT (PTU) REPLACED. OPERATION CHECKED SERVICEABLE AS PER AIRCRAFT MAINTENANCE MANUAL REFERENCE 29-SDR DLM88020279Hydraulic Line · looseRETURNED ACFT TO GATE DUE TO SMOKE INSIDE CABIN AND COCKPIT. FOUND LOOSE HYDRAULIC LINE ON THRUST REVERSER CONTROL VALVE. TIGHTENED SAME, PERFORMED DUCT BURNOUT.SDR 2002F00401Line · damagedDURING CLIMB-OUT OF SWA, HYDRAULIC SYSTEM B PRESSURE LOSS IND SHOWED 0 QTY ABNORMAL CHECKLIST FOLLOWED A/C DIVERTED TO SVMI, LANDED WITH NO INCIDENT. FOUND HYD LINE IN SERVICE PORT DAMAGED. REMOVED AND REPLACED LINE PER MM 20-10-05 SERVICED HYD QTY LEAK AND SDR UPS02837802Hydraulic Line · failedINSPECTION TYPE:N/A, HYD FAILURE IN FLIGHT. EMERGENCY DECLARED. ON CLIMBOUT LOSS OF HYDRAULIC FLUID DOWN TO AUX QUANTITY POSITION. R&R MS ON AILERON RETURN LINE I/B RT WING BEHIND O/B FALSE PANEL. RAN NR 2 & 3 ENG, ALL SYS RAN AND NO LEAKS NOTED. REMOVED SDR CA020315005Line · leaking(CAN) AFTER TAKEOFF, DURING FLAP RETACTION ECAM MSG HYDRAULIC BLUE ENGINE PUMP PRESSURE LOW CAME ON INTERMITTENTLY. AIRCRAFT RETURNED TO VANCOUVER. FOUND NR 2 ENGINE RETURN LINE LEAKING FROM A CRACK ELBOW. LINE REPLACED AND LEAK CHECKED OK. ALL FILTERS AND ENGSDR P9R2002F00000Check Valve · contaminatedON TAXI OUT IN MSP CABIN AND COCKPIT FILLED WITH SMOKE. RETURNED TO GATE. REMOVED AND REPLACED NR 1 ENGINE SYSTEM. A CHECK VALVE IAW MM. CLEANED RESIDUAL FLUID OUT OF LINE FROM NR 1 ENGINE CHECK VALVE FOR SYSTEM A HEAD PRESSURE. REMOVED AND REPLACED WATERSDR SWIA200210701O-Ring · leakingGREEN SYSTEM HYDRAULIC LOW LEVEL MAP LIGHT ILLUMINATED AT 22,000 FT WHILE EN ROUTE TO ACV. RESERVOIR PRESSURE WAS DECREASING AND ELECTRIC PUMP TURNED OFF. RETURNED TO SFO AND USED FREE FALL LANDING GEAR EXTENSION. REPLACED O-RING ON GREEN SYSTEM HYDRAULIC RSDR AUS20020264Line · worn(AUS) HYDRAULIC SUCTION LINE WORN THROUGH BY ELECTRICAL WIRINGASSOCIATED WITH THE LH OUTBOARD GEAR DOOR POSITION SWITCH. THELINE IS VISIBLE THROUGH PANEL 513 LOCATED IN THE LH WHEEL WELL.SDR AWXA200200190B-Nut · looseIAH - DIVERSION - FLT 555 - C - EN ROUTE FROM MIA TO LAS AT FL 350 ECAM MESSAGE FOR GREEN HYDRAULIC SYSTEM LOW PRESSURE INFLIGHT, POWER TRANSFER UNIT AND NR 1 ENGINE HYDRAULIC PUMP WERE TURNED OFF AND AIRCRAFT DIVERTED SAFELY INTO IAH. MAINTENANCE FOUND 2 EACSDR QXEA0200409Hydraulic Line · rupturedBOI- NR 2 HYD QTY SLOWLY WENT TO ZERO IN FLT NR 2 HYD ISO VALVE CAUTION LIGHT ILLUM, NR 2 HYD PUMP CAUTION LIGHT THEN CAME ON ALONG WITH RUD HYD CAUTION LIGHT. AFTER THE 3 CAUTION LIGHTS CAME ON, ELE PRESS LIGHT ILLUM. CHECK LIST WAS RAN AND ALTERNATE GEAR ESDR PCAA0202031Hydraulic Line · crackedBWI- FLIGHT 3923. CREW REPORTED THAT NR 1 HYDRAULIC QUANTITY WAS READING ZERO AFTER TAKEOFF. AN EMERGENCY WAS DECLARED, AND PLANE LANDED SAFELY IN BWI WITH A LOSS OF BRAKES AND FLAPS. MAINTENANCE FOUND A CRACK IN A FLARE OF HYDRAULIC PRESSURE LINE AT NR 1 HYSDR AWXA200200182Hydraulic Line · burstON FINAL TURN INTO PHX WHEN LANDING GEAR WAS EXTENDED ECAM INDICATED A LOSS OF GREEN SYSTEM HYDRAULIC PRESSURE. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED UNEVENTFULLY WITH ALTERNATE HYDRAULIC SYSTEM OPERATING NORMALLY. NOSE WHEEL STEERING INOPERATIVE AFTER SDR AUS20020149Hose · burst(AUS) NOSE LANDING GEAR ACTUATOR RETRACTION HOSE BURST. LOSS OF GREEN HYDRAULIC SYSTEM FLUID.SDR 2002UALA00332Connector · burnedSHORTLY AFTER TAKEOFF, EICAS DISPLAYED C-HYD PRI 1 WITH ASSOCIATED PRESS LIGHT ON CENTER ELEC 1 PUMP SWITCH. AIRCRAFT RETURNED TO SFO. PUMP CONNECTOR FOUND BURNED. REPLACED PUMP PER MM 29-11-02, SERVICED HYD SYSTEM. REPLACED CONNECTOR D482, OPS CHECKED ANDSDR CA020315004Line · leaking(CAN) AIRCRAFT HAD A COMPLETE LOSS OF GREEN HYDRAULIC SYSTEM FLUID AND PRESSURE IN FLIGHT OVER WASHINGTON STATE. FLIGHT DIVERTED TO VANCOUVER. PTU GREEN PRESSURE FLEX LINE FOUND LEAKING. FLEX LINE REPLACED AND SYSTEM LEAK CHECKED SERVICEABLE.SDR 2002FA0000297Hose · damagedHOSE ASSEMBLY FAILED AFTER TAKE-OFF AND NOSE GEAR WOULD NOT RETRACT. PILOT TRIED TO HAND PUMP THE MANUAL HYDRAULIC PUMP WITH SO SUCCESS. INSPECTION NOTED LINE BLEW A HOLE BELOW THE TSO TAG AREA. IT IS RECOMMENDED THAT ON ANNUAL INSPECT BOTH ACTUATOR HOSE ASSDR CA020226011Line · leaking(CAN) UPON A WALK AROUND INSPECTION, MAINTENANCE NOTICED A LARGE AMOUNT OF FLUID DRIPPING FROM THE LEFT NACELLE. THE LEFT MAIN LANDING GEAR DOORS MECHANICAL SEQUENCE VALVE "DOWN" PRESSURE LINE WAS FOUND LEAKING. THE LINE WAS REPLACED AND THE SYSTEM LEAK CHECKESDR CA020226012Line · leaking(CAN) THE FLIGHT CREW REPORTED A HYDRAULIC FLUID LEAK FROM THE RT NACELLE AND NR 4 FLAP TRACK AREA.MAINTENANCE FOUND THE NR 1 HYDRAULIC SYSTEM "DUMP" LINE FOR THE RT INBOARD SPOILER LEAKING. THE LINE WAS REPLACED AND THE SYSTEM LEAK CHECKED AND FUNCTION CHECKESDR ANCF200200004Line · brokenDURING CLIMB TO BOGOTA, THE CREW NOTICED THAT THE RT HYDRAULIC QUANTITY DROPPED TO 4 QTS, WITH PUMP IN LOW AND OFF OPERATION. THE SYSTEM WAS DEPRESSURIZED AND THE QUANTITY AUGMENTED TO 7 QTS. DURING CRUISE RH HYDRAULIC QUANTITY MAINTAINED IN 7 QTS, HOWEVER DURSDR CA020220001Line · leaking(CAN) PIN HOLE DEVELOPED IN FLEX LINE PORTION OF HYDRAULIC PUMP PRESSURE LINE CAUSING DUMPING OF ALL HYD FLUID AND CAVITATION OF HYD PUMP (EDP), ASSOCIATED MASTER CAUTION LIGHT AND LOSS OF NR 2 HYD SYSTEM. PROBLEM OCCURED 5 MINUTES BEFORE LANDING. SMALL AMOSDR MWEA020131Reservoir · leakingRIGHT HYDRAULIC QUANTITY DECREASING DURING TAKE-OFF AND CRUISE. -- REPLACED O'RINGS AT POPPET VALVE.SDR HNAA0200062Line · malfunctionedNR 2 HYDRAULIC CAUTION LIGHT CAME ON AND REMAINED ON AT GEAR RETRACTION, LANDING GEAR REMAINED IN TRANSIT. PREFORMED ALTERNATE EXTENSION. ON LANDING NR 2 HYDRAULIC PRESSURE RETURNED TO NORMAL. BLED AND SERVICED NR 2 HYDRAULIC SYSTEM. AIRCRAFT RELEASED FORSDR MEX2002044Hydraulic Line · leakingFLT 448 - BJX-LAX - DURING RAMP INSPECTION IT WAS DETECTED AN HYDRAULIC LEAK IN THE RIGHT MLG COMPARTMENT. A PRESSURE LINE OF THE BRAKE MANIFOLD AND MANIFOLD SEAL CAP WAS REPLACED IAW MM 32-42-03, IPC ITEM 102, TEST OK. 5 QUARTS OF HYDRAULIC FLUID WERE NEEDESDR 0200495528Line · leakingON INITIAL CLIMB, CREW RECEIVED EICAS MESSAGE "L HYD QTY" AND "RSVR" LIGHT ON LEFT SYSTEM. QUANTITY WAS VERIFIED AS DECREASING. LATER, "L HYD SYS PRESS" EICAS MESSAGE APPEARED AND CONFIRMED. CREW FOLLOWED ALL CHECKLISTS AND DECLARED AN EMERGENCY. FLIGHT RETURNSDR 020048528Hydraulic System · malfunctionedDURING TAKEOFF ROLL AT 95 KNOTS, CREW RECEIVED LEFT ENGINE HYDRAULIC CAUTION LIGHT. CREW SUCCESSFULLY ABORTED TAKEOFF AT 110 KNOTS. DURING TAXI, CREW AGAIN RECEIVED THE SAME ENGINE HYDRAULIC LIGHT. MAINTENANCE INSPECTED THE HYDRAULIC SYSTEM AND FILTERS AND
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