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 QXEA2013092201397Relay · malfunctioned"FAIL" LIGHT ON PTU CONTROL SWITCH UNTIL TAXI IN. FAIL LIGHT WAS ON WHEN PTU SWITCH WAS ON. RETURNED TO FIELD. LANDING UNEVENTFUL. REPLACED RELAY 2-K1. FUNCTIONAL CHECKED NORMAL. RETURNED TO SERVICE.SDR CA130923017Pressure Switch · burned(CAN) DURING CRUISE WHEN THE CREW SMELLED SMOKE. THERE WAS NO IMMEDIATE CAS MESSAGE THAT ANYTHING WAS WRONG BUT IT SOON DISPLAYED THAT THE HYDRAULIC PUMP AAT-600-029-100-1 WAS OVERHEATING. THE CREW PULLED THE APPROPRIATE C/B AND THE SMOKE ABATED. UPON LANDINGSDR R61A201309200894Valve · leakingON DECENT, CREW REPORTED NR 1 HYD QTY INDICATING ABNORMALLY LOW AND SOON AFTER THEY RECEIVED A NR 1 HYD PUMP CAUTION LIGHT. ALSO RECEIVED A FLAP POWER CAUTION LIGHT AFTER ATTEMPTING TO SELECT FLAPS 5. RAN QRH CHECKLIST, DECLARED AN EMERGENCY. LANDED WITHOUTSDR 29GA34629092013Pressure Switch · failedLOST HYD PRESSURE IN MAIN ACCUMULATOR BEFORE LANDING, NO LANDING GEAR EXTENSION AND LOSS OF STEERING, PULL EMERGENCY LANDING GEAR HANDLE DECLARED EMERGENCY 1. TRY ON PUMP. REPLACED HYD PRESSURE SWITCH OPS AND FUNCTIONAL CHECKS GOOD. THIS SDR SUBMITTED UNDER SDR 2013FA0000550Hydraulic System · malfunctionedMAIN HYD ACCUMULATOR SEEMS TO BE DROPPING PRESSURE MORE QUICKLY THAN NORMAL. AS PRESSURE DROPS WE LOSS BRAKE EFFECTIVENESS UNTIL PUTTING PUMP IN OVERRIDE. DURING FLIGHT MAIN ACCUMULATOR GOT TO THE POINT WHERE IN AUTO MODE WAS KICKING BACK ON EVERY 3 MINUTES. SDR 2013FA0000549Hydraulic System · failedLOST HYD PRESSURE IN MAIN ACCUMULATOR BEFORE LANDING, NO LANDING GEAR EXTENSION AND LOSS OF STEERING, PULL EMERGENCY LANDING GEAR HANDLE, DECLARED EMERGENCY 1 TRY ON PUMP.
SDR 2013FA0000548Hydraulic System · failedLOST HYD PRESSURE IN MAIN ACCUMULATOR, BEFORE LANDING, NO LANDING GEAR EXTENSION AND LOSS OF STEERING, PULLED EMERGENCY LANDING GEAR HANDLE DECLARED EMERGENCY 1 TRY ON PUMP.SDR VIBR20131202008Check Valve · leakingAUXILIARY HYDRAULIC RESERVOIR OVERBOARD DRAIN DRIPPING FLUID IN NOSE WHEEL WELL. REPLACE THE AUXILIARY HYDRAULIC CHECK VALVE.SDR SWIA201334732Unknown · malfunctionedRECEIVED INTERMITTENT NR 2 HYD LOW PRESS, "INBD SPOILERON" & "INBD FLIGHT SPOILERS" CAUTION MESSAGES. RESERVOIR QUANITY INDICATED 5%, RAN QRH FOR "HYD 2 LOW PRESS" CAUTION & LANDED UNEVENTFULLY. FLT#4625 RAN NR 2 ENGINE AT 85 1/2 % FOR 10 MINUTES. NO LEAKS SDR FDEA201309192250B-Nut · leakingENROUTE AT FL310, HYD SYS 1 FAILED. FLUID IN NR 1 HYD SYS FELL TO 2.5 GALS , PUMPS TURNED OFF. FOUND NR 1 HYD SYS MANIFOLD PRESSURE LINE B-NUT AND UNION LOOSE AND LEAKING. TIGHTEN AND TORQUED BOTH REF AMM 29-12-07-2 AND AMM 20-50-01. NO LEAKS NOTED, SERVISDR CLCA201309180001Line · leakingDURING CRUISE FLIGHT, SMOKE /FUMES OF UNKNOWN ORIGIN, ODOR. SMOKE AND FUMES IN THE COCKPIT AND CABIN. ACFT DEPARTED AND DIVERTED. FOUND HYDRAULIC LEAK ON NR 2 ENGINE RETURN LINE WHICH WAS DRIPPING DIRECTLY ONTO A AIR SUPPLY DUCT. TIGHTENED HYD LINE AND CLEANSDR CALA2013092391342Hydraulic Line · leakingHYD QUANTITY LOW CENTER HYD SYSTEM LOW RESERVOIR QUANTITY. QTY < .40 ADVISORY MSG01- ACTIVE APPROACH HARD; RESERVOIR CENTER FLUID QUANTITY IS LOW. HYDIM CL MSG-2910150 ACTIVE AP HARD. IAW TO IPC 32-51-80-005 ITEM 40 HYD HOSE LEAKING. REPLACED HYD HOSE & SSDR DXTA2013091905510Hose · leakingAFTER TAKEOFF, RETRACTED LANDING GEAR AND WITHIN A FEW SECONDS RECEIVED AN AMBER "HYDRAULIC VOLUME LOW" MESSAGE. AFTER LANDING, HYDRAULIC FLUID WAS SEEN IN NOSE GEAR COMPARTMENT AND DRIPPING FROM LT MAIN GEAR AREA AND DOWN SIDES OF FUSELAGE. INSPECTED NOSE SDR SWIA201334648Hydraulic Line · failedAFTER LANDING GOT HYD PUMP 3B, HYD 3 LOW PRESS & INBD BRAKE PRESS MESSAGES, HYD SYSTEM AT 0%. FLT#4568 REPLACED NLG ACTUATOR RETRACT HYD HOSE ASSEMBLY IAW AMM. EXTENDED & LOWERED LANDING GEAR SEVERAL TIMES. PN ON AE713578-12.SDR CALA2013091891268Hydraulic Line · leakingFOUND LT SIDE STAY ACT LINE LEAKING.SDR USAA2013091600005Pressure Switch · malfunctionedECAM HYD ENGINE 1 PUMP LOW PRESSURE GREEN SYSTEM LOW PRESSURE. R & R HYD LOW PRESSURE SWITCH TUBE NR 1 ENGINE IAW AMM 29-11-49, LEAK CHECK GOOD.SDR CA130910001Spu · leaking(CAN) AN ACFT EXPERIENCED PROBLEM ON NR 2 HYDRAULIC SYS DURING APPROACH. THE CREW DECLEARED AN EMERGENCY, PERFORMED ALTERNATE LG EXTENSION AND LANDED. HYDRAULIC LEAKAGE WAS CONFIRMED FROM NR 2 SPU, PN 731840, 2 MECHANICS AND 1 QA INSPECTOR WERE DISPATCHED ONSDR QXEA2013091001383Relief Valve · malfunctionedWHITE HYD SHUTOFF VALVE ON THE OVERHEAD PANEL STARTED BLINKING OFF AND ON. NR 1 HYD QTY WENT TO ZERO. FOLLOWED ABNORMAL CHECKLIST ACCOMPLISED ZERO FLAP LANDING. LANDING UNEVENTFUL. R & R NR 1 HYD BALANCED RELIEF VALVE IAW AMM 29-11-51-000-801, 29-11-57-400SDR CA140221003Relief Valve · leaking(CAN) DURING APPROACH, THE NR 1 HYD SOV CLOSED LIGHT CAME ON AND NR 1 ENGINE HYD PUMP CAUTION LIGHT. NR 1 SYS QTY WENT TO ZERO. PERFORMED ZERO FLAP LANDING. MAINTENANCE FOUND FLUID LEAKING FROM BALANCED RELIEF VALVE. VALVE REPLACED.SDR V6NA20130909001Regulator · leakingAFTER TAKEOFF, SMELLED A PETROLEUM TYPE ODOR. CLIMB OUT DURING DEPARTURE, TRIED BLEED AIR FUNCTIONS TO ISOLATE THE ODOR. TURNED ON HEAT IN CABIN AND SAW SMOKE COMING FROM VENTS. RETURNED TO AIRPORT. TURNED OFF HEAT AND SMOKE STOPPED. NO INDICATION OR IMMSDR CALA2013091091185Solenoid Valve · leaking'G' SYSTEM FLUID LOSS, RTFL FOUND SOLENOID VALVE OF THE PTU BROKEN. REPLACED IAW MM. REPLACED PUMP IAW MM. RE-INITIALIZED SYSTEM & ACCOMPLISHED AVEC TEST & OK NO MESSAGES.SDR 9JLA2013092306702Pressure Switch · defectiveFLIGHT CREW REPORTED THAT DURING FLIGHT THE "HYD 1 LO PRESS" ANNUNCIATOR ILLUMINATED. TROUBLESHOOTING IDENTIFIED THE NR 1 HYD PRESSURE SWITCH DEFECTIVE. INSTALLED NEW SWITCH. FUNCTIONAL AND LEAK CHECKS SATISFACTORY.SDR CALA2013090991101Packing · leakingGREEN SYSTEM HIGH PRESSURE MANIFOLD LEAKING RT WW CENTER CEILING AREA. REPLACED UNION & PACKING FOR GREEN SYSTEM HIGH PRESSURE MANIFOLD IAW IPC 29-11-15-05 PAGE 1 OF 12 ITEM 50 & ITEM 60.SDR QXEA2013090601329Shutoff Valve · malfunctionedON CLIMB NR 1 RUDDER HYD CAUTION LIGHT ILLUMINATED. RETURNED TO FILED. LANDING UNEVENTFUL. FOUND FAULT CODES 6E AND 6D. C/W FIM 27-00-00-810-805 FOR CODE 6E AND FIM 27-21-26-810-802 FOR CODE 6D. OHM AND MEGGERED WIRES, CHECKED GOOD. INSPECTED CONNECTOR PLUGSDR TXHA2013F00174Accumulator · leakingON TAKEOFF ROLL HYD RT ILLUMINATED. MAIN SYS PRESSURE DROPPED TO 2000 PSI.SDR CA130906007Hose · failed(CAN) AT APPROXIMATELY 4-5 MILES ON FINAL FOR RUNWAY 30, AFTER SELECTING GEAR DOWN, NR 2 HYD ISO AND OTBD ROLL SPOILER, CAUTIONS ILLUMINATED. NR 2 HYDRAULIC SYSTEM CONTENTS WERE NOTED AS ALMOST COMPLETELY DEPLETED. THE INDICATION WAS PERHAPS 1 OR 2 MILLIMETRESDR JIKA2013090601Flex Hose · leakingDURING CRUISE FLIGHT, BOTH HYDRAULICS FAILED ANNUNCIATORS ILLUMINATED. HYD PRESSURE READ 200PSI. PERFORMED AN EMERGENCY GEAR EXTENSION AND A FLAPS UP LANDING WITHOUT INCIDENT. MX INSPECTED THE ACFT AND FOUND THE LT FLAP ACTUATOR "UP" FLEXIBLE HYDRAULIC LISDR CALA2013090590998O-Ring · damagedECAM CAUTION MESSAGE, Y RSVR LO LVL MESSAGE INOPERATIVE, HYDRAULIC. FOUND HYDRAULIC LEAK FROM AUTO BRAKE SELECTOR VALVE CENTER B-UNION PIPE. REPLACED O-RING, SERVICED HYDRAULIC TO FULL. LEAK & OPERATIONS CHECKED OK. ECAM MESSAGE CLEARED.SDR CALA2013090490983Check Valve · faultyGREEN HYDRAULIC RESERVOIR PRESSURE SYSTEM TROUBLESHOOTING - CHECK OF PRESSURE LINES FOR INTEGRITY-LEAKS. REMOVE SEAT ROWS 22-24 ABC, REMOVED FLOOR PANEL 241LF, FOUND CHECK VALVE 1388GM & REMOVE CHECK VALVE FROM MANIFOLD. APPLY EXT AIR PRESSURE AT 50 PSI THRSDR CALA2013090490975Hydraulic Line · leakingFOUND HYDRAULIC LEAK FROM THE LT MLG DOWNLOCK ACTUATOR LINES. PCN 170-5394 & 170-5393. REPLACED LINE 170-5393 REF IPC 32-32-51-015. OLD LINE REMOVED REF IPC 32-32-51-015.ITEMS 270 & 275.SDR CA131001006Relief Valve · malfunctioned(CAN) ON PASSING FL100, NR 1 HYD SYSTEM QTY WAS NOTICED TO BE LOW AT 50 PERCENT. WHILE MONITORING OVER THE NEXT FEW MINUTES IT WAS NOTICED THAT THE QTY WAS REDUCING. AT APPROXIMATELY IT WAS DECIDED TO TURN BACK TO BASE. ON RETURN SLOWED THE ACFT DOWN AND LOSDR CA130904001Filter · worn(CAN) BORE SCOPE INSPECTION REVEL THAT NR 6 CYLINDER INTAKE AND EXHAUST HYDRAULIC FILTERS SHOW SIGNS OF WEAR.SDR CA130903008Valve · fractured(CAN) AFTER LANDING, THE PILOT REPORTED BOTH HYDRAULIC SYSTEMS NEEDED TOP UP. MAINTENANCE INVESTIGATION FOUND A HYDRAULIC LEAK IN THE LT NACELLE. THE LEAK WAS TRACED TO THE FORWARD HYDRAULIC QTY LIMITING VALVE, HYDRAULIC FUSE, WHICH WAS FOUND WITH THE END CAPSDR CALA2013090290914Unknown · malfunctionedREPEAT FAULT HYDRAULIC PRESSURE DEM 1 ON TAXI OUT. CREW SET ENGINE PUMP TO OFF THEN SELECTED AIR DRIVEN PUMP TO ON & SYSTEM PRESSURE DROPPED TO 700 PSI. AIR DRIVE PUMP 1 NOT PRODUCING HYDRAULIC PRESSURE. FAULT MESSAGE 29037. REPLACED HYDRAULIC PUMP & PRESDR CALA2013090290907Hydraulic Line · leakingHYDRAULIC FLUID LEAKING FROM UPPER SIDE OF LT MLG. FOUND UPPER FLEX HOSE LINE BROKEN TO NR 10 ANTI SKID SHUTOFF VALVE. REPLACED HOSE PRESSURE ON ALL THREE HYDRAULIC SYSTEMS, NO LEAKS NOTED.SDR REXA2013083001720Line · leakingDURING APPROACH, WHILE TRYING TO BRING GEAR DOWN, RECEIVED A MASTER WARNING GEAR DISAGREE. NOSE WHEEL DOOR WAS OPEN BUT GEAR DID NOT COME DOWN. WARNING SOUNDED WITHIN 5 SECONDS OF GEAR HANDLE DOWN. HAD AMBER DASHES FOR NOSE WHEEL, FOLLOWED QRH ON 2ND ATT. SDR CA130829006Warning Light · false indication(CAN) ACFT HAD A REJECTED TAKEOFF, AFTER THE FLIGHT CONTINUED, BELOW PRESSURE LIGHT ILLUMINATED AT APPROXIMATELY 70 KNOTS. MAINTENANCE TESTED THE SYSTEM WITH NO FAULTS FOUND, IAW FAULT ISOLATION PROCEDURES AND A HIGH ENERGY STOP INSPECTION WAS CARRIED OUT WITSDR CA130829005Hydraulic System · overserviced(CAN) ON TAKEOFF, THE CREW DETECTED A STRONG ODOR THROUGHOUT THE ACFT. THE ACFT RETURNED WITHOUT INCIDENT. MAINTENANCE DISCOVERED BOTH A AND B SYS HYDRAULIC RESERVOIRS SLIGHTLY OVER SERVICED. THE RESERVOIRS WERE DRAINED TO THE PROPER LEVEL AND HIGH POWER ENSDR CALA2013082990852Valve · leaking'Y' SYSTEM LOW PRESSURE MESSAGE, RETURN TO FIELD. REPLACED POWER TRANSFER UNIT MANIFOLD 2-WAY VALVE. OPERATIONS & LEAK CHECKED OKAY.SDR IPXA2013083018047Line · leakingHYD YELOW SYS FAILURE AFTER TAKE OFF. LOST QUANTITY DOWN TO RED DOT FOUND RT WING YELLOW SYS PRESSURE LINE LEAKING OVER RT MLG. R & R PRESSURE LINE, SERVICED APPROX 5 GALLONS HYD FLUID. NO LEAKS. REF AMM 20-23-11-00001, 12-12-29-0001, 27-14-05-29.SDR UIEA2013082700468Line · leakingAFTER TAKEOFF, HYDR QTY AND PRESSURE WENT TO ZERO ON SYS 4 FLAPS ASYMETRIC AND WOULD NOT RETRACT. FUEL JETTISONED AND RETURNED TO DEPARTURE. REPAIRED IAW AMM 12-00-00.SDR CALA2013082990841B-Nut · looseG RESERVOIR LOW AIR PRESSURE DISPLAYED ON UPPER ECAM SCREEN. FOUND 'B'-NUT LOOSE AT RESERVOIR PRESSURE GAUGE SERVICED SYSTEM LIGHT OUT AT UPPER ECAM SCREEN. OPERATION CHECKED GOOD IAW MM.SDR CA130826016Hose · leaking(CAN) DURING THE ALF INSPECTION IT WAS NOTICED THAT THE HYDRAULIC TANK HAD LOST 50 PERCENT OF IT FLUID. UPON FURTHER INVESTIGATION THE LOSS OF FLUID WAS FROM THE HYDRAULIC PRESSURE LINE, PN 70A34-412-251. NEW LINE WAS REPLACED AND ACFT RETURNED TO SERVICE.SDR CA130826003Line · cracked(CAN) DURING FLIGHT THE GREEN HYDRAULIC FLUID NOTICED TO BE DECREASING, FOLLOWED BY ECAM LOW LEVEL WARNING. LANDING MANUALLY EXTENDED FOR LANDING. ACFT HAD TO BE TOWED OFF RUNWAY DUE TO LOSS OF STEERING FROM GREEN HYDRAULIC SYSTEM FLUID LOSS. FOUND NR 2 ENGISDR USAA2013082600005Hose · rupturedINFLIGHT, LOST ALL GREEN HYDRAULIC FLUID. RECEIVED ECAM ON "HYD LOW" AND ZERO FLUID LEVEL. FOUND RUPTURED LT MLG DOOR ACTUATOR HOSE & SWIVEL. REPLACED REF AMM 32-31-39 & 32-31-38.SDR CALA2013082390701Hydraulic System · lowCREW REPORT RT HYDRAUIC SYSTEM LOW.SDR CA130823008Line · ruptured(CAN) ON THE TAXI IN, ENGINE NR 1 RUNNING, ENGINE NR 2 WAS OFF. LOW QTY INDICATION HYD 1. MAINTENANCE INVESTIGATION REVEALED THERE WAS A LEAK AND HYDRAULIC QUANTITY WAS ZERO. ACFT OFF-LINE FOR REPAIR. NR 1 ENGINE EDP HIGH PRESSURE LINE RUPTURED IN FWD PYLONSDR CA130822012Manifold · leaking(CAN) O-RING FAILURE BETWEEN MANIFOLD ASSY FIN 291112, PN A2901150800000 AND BOSS FITTING MS21902-10. CAUSING ACFT TURN BACK DUE HYDRAULIC LOSS. IPC REF 24-24-03-04 050, O-RING REPLACED ON MANIFOLD ASSY FIN 291112. DEFECT ITEM NR 1100188.SDR SWIA201334374Hydraulic Line · failedHYDRO 3 LOW PRESSURE CAUTION MESSAGE. FLT#4970 REPLACED FLEX HOSE ASSEMBLY. PN AE13578-12.SDR NOZA2013F00160Line · failedNOSE LANDING GEAR RETRACT HYDRAULIC LINE WAS COMPROMISED ON GEAR RETRACTION SHORTLY AFTER TAKEOFF, RESULTING IN LOSS OF THE A SYSTEM HYDRAULICS. POSTFLIGHT INSPECTION REVEALED A BLOWOUT OF THE HOSE JUST BELOW THE ATTACH FITTING. HOSE REPLACED AS WELL AS THE
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