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 2004F00276Line · leakingDURING TAXI, THE GREEN SYSTEM LOW LEVEL LIGHT CAME ON THEREFORE, NO BRAKING ACTION. FOUND HYDRAULIC LINE WITH PIN HOLE. REPLACED METERING VALVE LINE. (M)SDR CA040728003B-Nut · separated(CAN) PILOT WAS UNABLE TO HAVE GEAR DOWN INDICATION WITH BOTH ELECTRIC AND MANUAL EXTENSION. WHEEL RETRACTED BACK INSIDE WHEEL WELL ON LANDING. INSPECTION FOUND HYDRAULIC LINE INSIDE THE AIRFRAME BELLY TO RT FLOAT HAD BROKEN OFF FROM THE B-NUT. IT APPEARED SDR 63379Hydraulic System · lowRECEIVED CALL FROM CAPTAIN HIS LT BRAKE WAS BLEEDING OFF. THEN CALLED MAINTENANCE IN PIT. BLEED LT BRAKE AND SERVICED HYDRAULIC BRAKE GROUND CK GOOD. LEAK CK GOODSDR 2004UALA00690Hydraulic System · failedRETURN TO FIELD DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. LEAKING BYPASS VALVE, LOSS OF HYDRAULIC FLUID. REPLACED THE NOSE LANDING GEAR DOOR OPENING BYPASS VALVE. OPERATIONS CHECK NORMAL.SDR DXTA200400346Switch · malfunctionedLOST RT HYDRAULIC SYSTEM IN FLIGHT, RT HYD LEVEL LOW MESSAGE DISPLAYED. SYSTEM PRESSURE 400-600 PSI, LANDED AIRCRAFT USING EMERGENCY BRAKE SYSTEM. REMOVED AND REPLACED BRAKE CONTROL VALVE, PERFORM EMERGENCY BRAKE CHECK IAW MM CHAPTER 32-30-710-802. REPLACED RSDR E812004F00008Line · chafedWHILE INSPECTING FORWARD FUSELAGE BRAKE HYDRAULIC LINE TUBING DURING COMPLIANCE WITH RECOMMENDED SB, FOUND TUBING DAMAGED EXTERNALLY BY FLOOR PANEL 151BTC AND FLOOR PANEL 151DTC ATTACHMENT SCREWS. REPAIRED TUBING ASSY BY SPLICING IN REPAIR TUBE WITH PERM SWAGSDR SWAA042067Line · leakingDECLARED EMERGENCY, HYDRAULIC B-SYSTEM LOW PRESSURE LIGHT ILLUMINATED, WITH QUANTITY GOING DOWN. REMOVED AND REPLACED HYDRAULIC B-SYSTEM PUMP PRESSURE LINE PER MM.SDR SWAA042052Hose · leakingAIRTURN BACK, ON TAKEOFF NR 2 HYDRAULIC B-SYSTEM LOW PRESSURE LIGHT ILLUMINATED, WITH DROP IN QUANTITY. NR 1 HYDRAULIC B-SYSTEM LOW PRESSURE LIGHT ILLUMINATED, WITH LOSS OF PRESSURE. REMOVED AND REPLACED NR 1 BRAKE HOSE PER MM.SDR ASMF200407021Control Valve · leakingDURING TRANSIT CHECK, HYDRAULIC LEAK WAS DETECTED ON RT LANDING GEAR CONTROL VALVE. LEAK WAS DETECTED ON CONTROL VALVE NIPPLE AND PRESSURE LINE. RT LANDING GEAR CONTROL VALVE WAS REPLACED IAW MM 32-32-01 AND IT WAS PERFORMED EXTENSION AND RETRACTION LANDING SDR DXTA200400342Manifold · failedLANDING GEAR CYCLED IN FLIGHT AT FL 430 AND FL120 UNLOCK LIGHT ILLUMINATED THEN WENT OUT AFTER 1 MINUTE. TROUBLESHOT TO FAULTY LANDING GEAR HYDRAULIC MANIFOLD ASSEMBLY. REMOVED AND REPLACED HYDRAULIC MANIFOLD. BLED SYSTEM, OPS AND LEAK CHECKS GOOD, ALL WORSDR DLM88040657Line · crackedFL230 LOST RIGHT HYD QTY QTY DOWN TO 4 QTS. SHUT OFF RT HYD ENG PUMP PER CKLIST. QTY REMAINED CONSTANT AT 4 QTS UNTIL PUMP WAS TURNED ON IN PREP FOR LANDING. QTY THEN DECREASED TO 1 QT. MAINTENANCE NOTED HYD FLUID UNDER AIRCRAFT. APU NOT STARTED PER CREW SDR EHA2004F00003Line · chafedHYDRAULIC LEAK FROM AREA OF CARGO HOOK. TRACED TO TAIL ROTOR SAS LINK HYDRAULIC LINE CHAFED BY FUEL VENT LINE. REPLACED LINE, REROUTED AND SECURED FUEL VENT LINE. LEAK CHECKED AND MOC FLIGHT GOOD. (AL03200404250)SDR DLM88040651B-Nut · looseAFTER CONFIGURING FOR LANDING LEFT HYD QTY DROPPED TO 2 QUARTS WITH THE LOW LEVEL LIGHT. ACCOMPLISHED PROCEDURE, PRESSURE REMAINED NORMAL UNTIL TAXI WHEN LEFT PRESSURE DROPPED TO 0 PSI. FOUND LOOSE B-NUT FITTING AT TOP END AND BOTTOM END OF LEFT THRUST REVERSDR CA040823006Line · failed(CAN) AFTER ENGINE SHUT DOWN AT THE GATE, HYDRAULIC FLUID WAS NOTED LEAKING FROM THE NOSE GEAR AREA. NOSE GEAR DRAG STRUT ACTUATOR HOSE REPLACED DUE TO LEAKING P/N DSC252B40124. DAMAGE FOUND TO BRAIDING JUST AFT OF THE COLLAR DEFECT NR 416542. GEAR RETRACTIOSDR GTIA040656B-Nut · leakingFLT 1153 - VERTY STRONG ODOR OF OIL OR SKYDROL THROUGHOUT THE CABIN AND COCKPIT DURING CRUISE. FOUND HYDRAULIC FLUID LEAKING FROM LINE IN AFT PIT LEFT WALL. FLUID DRAINED ON BOTTOM OF FUSELAGE AND WENT INTO APU INLET AND FUMES FROM FLUID WENT INTO RECIRC FANSDR 2004UALA00734Hydraulic System · leakingLANDED UNDER AMBER ALERT DUE TO LOSS OF HYDRAULIC PRESSURE. RIGHT HAND ALTERNATING CURRENT MOTOR PUMP ASSY FAILED. REPLACED PUMP.SDR HNAA0408108Line · chafedFLIGHT 3847 REPORTED HAVING NR 1 HYDRAULIC CAUTION LIGHT FLICKERING DURING DESCENT INTO SYR. ISOLATION VALVE ACTIVATED. THERE WAS NO DISRUPTION TO HYDRAULIC SYSTEMS REMAINDER OF THE FLIGHT. MAINTENANCE FOUND A NR 6 HYDRAULIC LINE CHAFED THROUGH UNDER PANEL SDR P8UF200400001Valve · failedDURING CLIMB, FLIGHT CREW NOTICED HYDRAULIC LOSS ON SYSTEM NR 1, CAPTAIN DECIDED FLIGHT BACK TO POINT OF DEPARTURE.SDR ASMF200407012Line · leakingCAPTAIN REPORTED REVERSE INOPERATIVE DUE TO -LT REVERSE ACCUMULATOR LOW- LIGHT ILLUMINATED. DURING CHECK HYDRAULIC LEAK WAS DETECTED IN ACCUMULATOR LINE. HYDRAULIC LINE WAS REPLACED IAW MM 78-31-04, ALL CORRECT. DURING REVERSE TEST, ACCUMULATOR PRESSURE INDICSDR DL764040633Turbine · failedSHIP 1808 EXPERIENCED A ADP TURBINE FAILURE WHICH CAUSED SUPPORT ROD TO BREAK OFF AND BEND, ALSO 1 INCH HOLES IN ADP DOOR AND FAIRING WEB. REPAIRED AND REPLACED DAMAGED COMPONENTS.SDR DXTA200400330Manifold · failedGEAR PARTIALLY DEPLOYED UNCOMMANDED DURING DESCENT AT 14,000 FT, GEAR UNLOCK LIGHT CAME ON, AIRCRAFT LANDED SAFELY AT FLL. REMOVED AND REPLACED LANDING GEAR CONTROL HYDRAULIC MANIFOLD, BLED ALL HYDRAULICS AND LEAK CHECKED MANIFOLD, LEAK CHECKED GOOD. SERVICESDR ASMF200407009Servo Valve · leakingDURING TRANSIT CHECK, HYDRAULIC LIQUID LEAK WAS DETECTED ON RT MAIN LANDING GEAR WELL, BOTH SYSTEMS WERE PRESSURIZED, BRAKES AND CONTROL SURFACES WERE ACTUATED AND LEAK WAS DETECTED ON ANTI-SKID RT DOUBLE SERVO VALVE. SERVO VALVE WAS REPLACED IAW MM 32-43-02, SDR AWXA200400711Switch · malfunctionedEN ROUTE FROM PHX TO EWR AIRCRAFT DIVERTED TO ABQ FOR YELLOW HYDRAULIC LOW QUANTITY WARNING INDICATION. MAINTENANCE VERIFIED HYDRAULIC QUANTITY AS OK AND PLACED THE INDICATION SYSTEM ON THE MINIMUM EQUIPMENT LIST. MAINTENANCE REMOVED AND REPLACED YELLOW HYDRSDR 04FDEA01936Hose · leakingON T/O OUT OF MEM , GOT YELLOW HYD RES: LOW AND HYD YELLOW PRESS LOW WARNINGS. COMPLIED WITH ECAM , REVIEWED QRH, AND RETURNED TO MEM. UPON INSPECTION FOUND RT WING AILERON INB MOSTACTUATOR HYD HOSE RUPTURED. ORDERED HOSES AND PLACED IN A/C FOR TURN OVER. SDR 120631Warning Light · illuminatedFLIGHT 7982 FROM TYS TO IAD, ON FINAL WITH GEAR UP HYD LIGHT ILLUMINATED ON CWP. AIRCRAFT HAD LOW MAIN AND EMERGENCY INDICATIONS. AIRCREW FOLLOWED QRH. WHEN GEAR WAS SELECTED DOWN ONLY NOSE GEAR CAME DOWN. WHILE DOING A GO-AROUND THE RIGHT GEAR CAME DOWN. SDR SWAA041850Hose · leakingAIR TURNBACK/DECLARED EMERGENCY. AFTER TAKEOFF NLG WOULD NOT RETRACT AND A-SYSTEM HYDRAULIC QTY WAS DECREASING. REMOVED AND REPLACED NLG ACTUATOR UPLOCK HOSE.SDR VNAA0406017B-Nut · failedON CLIMBOUT, THE CREW RECEIVED A NR 2 LOW PRESSURE AMBER CAS MESSAGE. THE AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE RESECURED THE B-NUT ON THE LEFT HAND SIDE OF THE NOSE GEAR AND INSPECTED THE NR 2 SYSTEM HYDRAULIC LINE PRESSURE IN ACSDR 62683Valve · malfunctionedLANDING GEAR FAILED TO EXTEND ON FIRST ATTEMPT. GEAR FINALLY EXTENDED ON THE SECOND ATTEMPT. REMOVED AND REPLACED HYD SERVICE VALVE. OPS CK GOOD.SDR CA040630005Fitting · loose(CAN) ON FINAL APPROACH, WHEN FLAP/SLAT WERE EXTENDED, THE HYDRAULIC RESERVOIR LOW LEVEL ECAM WARNING CAME ON. AIRCRAFT OVERSHOT AND CHECKLIST PROCEDURE INDICATE A FAILURE OF GREEN HYDRAULIC SYSTEM. ALTERNATE GEAR EXTENSION PERFORMED. DURING INVESTIGATION,SDR 2004UALA00624Line · leakingRETURN TO FIELD UNDER AMBER ALERT DUE TO GREEN HYDRAULIC SYSTEM FAILURE. FOUND CUT SEAL ON HYDRAULIC LINE. REPLACED SEAL, FOUND GREEN RESERVOIR WITH THREE GALLONS OF HYD FLUID. RESET MANUAL GEAR EXTENSION. SERVICED SYSTEM TO FULL. RAN ALL HYDRAULIC PUMPS, NSDR 04FDEA01869Fitting · leakingIN LEVEL FLT, CRUISE AT FL310, GREEN HYD SYS LOW LEVEL OCCURRED. BOTH OVERHEAD QTY AND ECAM INDICATED RED DOT. QRH ACTIONS DIRECTED MANUAL LANDING GEAR EXTENSION. NORMAL LANDING. GEAR PINNED FOR TOW-IN AFTER LANDING. GREEN PUMPS TURNED OFF AT 3250 PSI. SDR ERAA097533Guide · brokenGUIDE ASSY HAS HYD BLOCK LIGHT ON. FOUND SOCKET BROKEN. DISASSEMBLED, CLEANED, INSPECTED, INSTALLED, NEW SOCKET, SPRING, POTTED AND TESTED. INSPECTED AND REPAIRED IAW MBB BO105 - REM 405.SDR 2004000008Hydraulic System · lowLEFT HYDRAULIC SYSTEM QUANTITY LOW. SERVICED LEFT HYDRAULIC SYSTEM.SDR 04FDEA01866Fitting · leakingIN LEVEL FLIGHT, CRUISE AT FL310, GREEN HYD SYS LOW LEVEL OCCURRED. BOTH OVERHEAD QTY AND ECAM INDICATED RED DOT. QRH ACTIONS DIRECTED MANUAL LANDING GEAR EXTENSION. NORMAL LANDING. GEAR PINNED FOR TOW-IN AFTER LANDING. GREEN PUMPS TURNED OFF AT 3250 PSISDR GTIA040629Line · leakingLGA - FLT 779 - JUST AFTER TAKEOFF LGA, STRANGE ODOR CAME THROUGH VENTS. BRAKE TEMP INDICATOR LIGHT WAS FLASHING AND TEMP NEEDLE MOVING, LEFT LANDING GEAR DOWN TO MAKE SURE NO BRAKE HEAT, LIGHT WENT OUT, ODOR WENT AWAY. FOUND NR 2 BRAKE AFT HYD LINE LOOSE ANSDR ARWA20040604Hydraulic System · contaminatedPRIOR TO TOP OF DESCEND BOTH HYDRAULIC PUMPS OUTPUT PRESSURE ZERO. AILERON AND RUDDER REVERSION LIGHTS ON. COMPLETED EMERGENCY ABNORMAL HYDRAULIC CHECKLIST. CHECKED A/C FOR HYDRAULIC LEAK, NO LEAKS NOTED. INSPECTED MAIN HYDRAULIC CASE DRAIN FILTERS FOR CONSDR 2005FA0000229Tube · leakingTUBE LEAKING THRU SEVERAL PIN HOLES, SUSPECT INTERNAL CORROSION. SLOW EVACUATION OF HYDRAULIC FLUID PREVENTED ACTUATION OF HYDRAULIC FUSE. TAKEOFF WITH GEAR (UP) SELECTION REVEALED SLOW ACTUATION AND A RETURN TO BASE. GEAR (DOWN) SLOW BUT CAME DOWN AND LOCKSDR CA040630001Line · leaking(CAN) DURING OPERATION, THERE APPEARED TO BE HYDRAULIC FLUID COMING FROM THE TAIL SECTION OF THE AIRCRAFT. UPON FURTHER INVESTIGATION , IT WAS FOUND THAT THE LINE WAS LEAKING AND IT WAS REPLACED WITH FLEX LINE AE24600160720 IAW MM 20-50-52.SDR SWAA041769Valve · leakingAIR TURNBACK, A-SYSTEM HYDRAULIC FLUID LOSS. REMOVED AND REPLACED FWD MLG MODULE VALVE, AND REMOVED AND REPLACED CASE DRAIN FILTERS, PER MM.SDR QXEA200400471Line · crackedSEA - FLIGHT 2029 - CREW REPORTED LOSS OF BOTH THE NR 2 HYDRAULIC PRESSURE AND QUANTITY WHILE ON APPROACH. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 1 AFT MAIN LANDING GEAR DOOR HYDRAULIC LINE CRACKED AND LEAKING. THE LINE WAS REPLACED, LEAK CHECKSDR CA040625009Hose · leaking(CAN) ON SELECTING GEAR RETRACTION AFTER TAKE-OFF , LOSS OF 32 SYSTEM HYDRAULIC FLUID. CAUTION LIGHTS FOR NR 2 HYD ISOLATION SYSTEM AND NR 2 HYD PUMP. AIRCRAFT RETURNED TO DEPARTURE AIRPORT AND USED ALTERNATE GEAR EXTENSION SYSTEM. NORMAL LANDING. MAINTENANSDR UPS04442609Line · chafedNR 3 HYD SYS LOST FLUID TO 0.5 GAL EDP ZERO WITH LOW PRESSURE LIGHT. ADP PRESSURE NORMAL. CHECKLIST COMPLETE FOR SYSTEM LEAK. FOUND PRESSURE LINE CHAFED ON PNEU DUCT IN UPPER SECTION OF NR 3 PYLON (MARKED WITH RED TAPE) BB 09326 INSTALLED NEW LINE, LEAK CHESDR CA040812009Bypass Valve · leaking(CAN) GREEN HYDRAULIC LOW LEVEL, LOST ALL GREEN HYDRAULIC PRESSURE WHILE TAXING, DOOR BY-PASS VALVE LEAKING MPN 114087005 S/N CWDDDH8197SDR CA040622001Hose · leaking(CAN) ENROUTE, THE CREW NOTICED SLOW BUT STEADY DEPLETION OF HYDRAULIC SYSTEM 2 . THE QUANTITY DOWN TO 2 QUARTS. CREW RETURNED AIRCRAFT BACK WHERE MAINTENANCE PERSONAL UPON INVESTIGATION FOUND THE HOSE TO THE DRAG STRUT ACTUATOR IN THE NOSE GEAR BAY LEAKING. SDR LX52004F00001Pressure Switch · leakingDURING A SCHEDULED FLIGHT, THE PILOT NOTICED THE LOW HYDRAULIC FLUID LIGHT HAD COME ON. UPON APPROACH, THE GEAR WAS SELECTED DOWN AND THE POWER PACK RAN FOR 14 SECONDS THEN TRIPPED THE BREAKER. THE GEAR WAS THEN MANUALLY PUMPED DOWN AND PLANE LANDED WITHOUT SDR CA040621008Powerpack · failedIT APPEARS THAT THE HYDROPACK HAD AN INTERNAL GEAR FAILURE. THE AIRCRAFT HAD NR INDICATIONS BUT NO HYDRAULIC PRESSURE. HYDROPACK WAS CHANGED AND AIRCRAFT RETURNED TO SERVICE.SDR 2004F00174Line · crackedDURING FINAL APPROACH HYDRAULIC SYSTEM A QUANTITY DROPPED TO ZERO LANDED SAFELY WITHOUT INCIDENT. FOUND NR 2 ENGINE SUPPLY LINE CRACKED REPLACED SAME PER MM 29-00. OPS CHECK GOOD AIRCRAFT RETURNED TO SERVIEC WITHOUT FURTHER INCIDENT. (M)SDR A6WA200440084Elbow · leakingHYDRAULIC NR 3 LOW PRESSURE CAS MESSAGE INFLGHT NR 3 HYDRAULIC SYSTEM QUANTITY AT ZERO PERCENT COMPLIED WITH QRH, PERFORMED MANUAL GEAR EXTENSION. FOUND FORWARD GROUND PRESSURE LINE FITTING LEAKING. REPLACED ELBOW FITTING. LEAK CHECK GOOD. SERVICED NR 3 SYSDR 04FDEA01746Warning Light · illuminatedT/O PLUS 1 HR, DURING DESCENT TO FL240, GOT ECAM MESSAGE FOR LOW GREEN HYDRAULIC QUANTITY. GAGE AND ECAM SCHEMATIC SHOWED QUANTITY AT THE RED DOT LEVEL. TURNED OFF GREEN PUMPS, MANUALLY EXTENDED THE GEAR, UTILIZED THE ALTERNATE BRAKE SYSTEM AND LANDED AT MSYSDR DLM90040552Pressure Switch · inoperativeWHILE TAXIING SLOWLY ARMED T/O MODE OF AUTOBRAKES A/C IMMEDIATELY AND ABRUPTLY STOPPED. RECEIVED AUTOBRAKE FAIL MESSAGE ON EOAP. NORMAL BRAKING OPERATES FINE. FAULTS IBCV1 SOV. REPLACED SAME.
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