JASC 2913
Service difficulty reports · 4,062
Reports filed under 2913 · Hydraulic Pump (Electric/Engine), 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 = '2913' 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 = '2913' 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 USAAD98164Pump · failedPIT-MDT - FLT 710 - AFTER TAKEOFF THE PRESSURE WENT TO ZERO FOR THE LEFT ENGINE HYDRAULIC PUMP. FOR MAINTENANCE CONVENIENCE THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE DRIVEN HYDRAULIC PUMP. (M)SDR AU981268Press Switch · failed(AUS) LANDING GEAR POWERPACK PRESSURE SWITCH OPEN CIRCUITED. PISTON P/N H2309 STUCK.SDR 98ZZZX3804Finger · looseDURING ROUTINE INSPECTION, FOUND SHOULDER SEPARATED FROM SCREEN. THIS CONDITION COULD LEAD TO POSSIBLE INJESTION OF SCREEN.SDR 99ZZZX100Power Pack · leakingUNABLE TO RETRACT GEAR DUE TO PUMP WEAKENING CAUSED BY LEAKING/WORN SEALS AND BLEED DOWN OF SYSTEM.SDR 98ZZZX4697Seal · failedHYDRAULIC PUMP DRIVE SEAL FAILED AND WAS DRIPPING SKYDROL FROM OVERBOARD DRAIN ON RT ENGINE. TIS: 2.4 HOURS. LANDINGS: 2. AIRCRAFT TT: 2,219.4 HOURS. LANDINGS: 1,477. DATE: 9-17-98.SDR 98ZZZX4695Seal · failedHYDRAULIC PUMP DRIVE SHAFT SEAL FAILED AND WAS DRIPPING SKYDROL FROM OVERBOARD DRAIN ON RT ENGINE. TIS: 60.7 HOURS. LANDINGS: 38. AIRCRAFT TT: 2,217.0 HOURS. LANDINGS: 1,475. DATE: 9-17-98.SDR 98ZZZX4030Pump · overheatedTHE AIRCRAFT WAS IN CRUISE AT 45,000 FEET WHEN THE R1 HYDRAULIC PUMP FAILED. TEN MINUTES LATER, R2 PUMP FAILED. THERE WAS NO FLUID LOSS AT THIS POINT. ON FINAL WHEN THE LANDING GEAR WAS SELECTED DOWN, THE RIGHT HYDRAULIC SYSTEM QUANTITY WENT TO ZERO.SDR 98ZZZX4029Pump · overheatedTHE AIRCRAFT WAS IN CRUISE AT 45,000 FEET WHEN THE R1 HYDRAULIC PUMP FAILED. TEN MINUTES LATER, R2 PUMP FAILED. THERE WAS NO FLUID LOSS AT THIS POINT. ON FINAL WHEN THE LANDING GEAR WAS SELECTED DOWN, THE RIGHT HYDRAULIC SYSTEM QUANTITY WENT TO ZERO.SDR 98ZZZX4018Pump · failedDURING ENGINE INSPECTION RUN-UP, FOUND NR 1 HYDRAULIC PUMP OPERATING AT 2,200 PSI (SHOULD BE 3,000). REMOVED FAILED PUMP AND INSTALLED REPAIRED UNIT.SDR 98ZZZX4017Pump · leakingON PRE-FLIGHT, FOUND NR 2 ENGINE HYDRAULIC PUMP LEAKING STATICALLY FROM CASE HALVES. REPLACED LEAKING PUMP.SDR 98ZZZX4016Pump · leakingON PRE-FLIGHT, FOUND NR 2 HYDRAULIC PUMP LEAKING STATICALLY FROM BETWEEN THE CASE HALVES. REPLACED LEAKING PUMP.SDR 98ZZZX4031Pump · failedNR 1 ENGINE HYDRAULIC PUMP L2 OVERHEATED AND FAILED IN-FLIGHT.SDR 98ZZZX4021Pump · leakingPUMP LEAKING STATICALLY FROM THE SHAFT SEAL.SDR 98ZZZX3620Pump · failedDURING START OF THE RIGHT (NR 2) ENGINE, THE CREW NOTICED AN UNUSUAL NOISE THAT LASTED APPROXIMATELY 30 SECONDS. SCANNING THE INSTRUMENTATION REVEALED THE 'HYD 2' LIGHT ILLUMINATED AND THE HYDRAULIC PRESSURE GAUGE INDICATED ZERO. EXAMINATION OF THE RT ENGINESDR SWAA982082Pump · failedAIRCRAFT FLT HOU-TUL, DIVERTED INTO DAL DUE TO HYDRAULIC A SYSTEM ENGINE DRIVEN PUMP FAILED IN FLIGHT. REMOVED AND REPLACED ENG DRIVEN HYDRAULIC PUMP PER BOEING MM, LK CHECK AND FUNCTION CHECK GOOD.SDR 98ZZZX4694Seal · failedHYDRAULIC PUMP DRIVE SHAFT SEAL FAILED AND WAS DRIPPING SKYDROL FROM OVERBOARD DRAIN ON LEFT ENGINE. TIS: 1,374 HOURS. LANDINGS: 897. AIRCRAFT TT: 2,206.0. LANDINGS: 1,468. DATE: 9-11-98.SDR 98ZZZX3667Bearing · mismanufacturedSUBMITTER RECEIVED 3 PARTS FROM STOCK OVER A PERIOD OF TIME THAT HAD THE BEARING PARTIALLY DISASSEMBLED. ONE RECEIVED INTACT. INSTALLED THE ASSY IN THE PUMP AND DURING THE RUN-IN PROCESS, THE LOWER BEARING CAME APART CAUSING FAILURE TO THE PUMP. SUBMITTER SSDR SWIA971248Pump · failedGREEN HYDRAULIC SYSTEM LOSS OF FLUID WITH SUBSEQUENT LOW PRESSURE INDICATION. REMOVED AND REPLACED LEFT ENGINE HYDRAULIC PUMP. RAN ENGINE AND SYSTEM OPS CHECKS GOOD. SERVICED GREEN SYSTEM.SDR VTZA98289Pump · failedFLT 6572 - IAD-SCE - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LOSS OF ALL HYDRAULIC PRESSURE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED HYDRAULIC PUMP, OPS CHECK OK. AIRCRAFT WAS RELSDR CA980916057Seal · leaking(CAN) ON TAKEOFF WHEN 90 PERCENT TORQUE APPLIED, THE NR 1 OIL PRESSURE WARNING LIGHT CAME ON. OIL PRESSURE INDICATOR SHOWED DROPPING OIL PRESSURE. AS SOON AS ENGINE WAS PUT IN DISCING OIL, PRESSURE RETURNED TO NORMAL. SHAFT SEAL FOUND LEAKING OIL.SDR 98ZZZX3669Pump · failedUNIT WOULD NOT PRODUCE PRESSURE TO TURN OFF PUMP. REMOVED AND SENT FOR OVERHAUL. INSTALLED SAME BACK IN AFTER OVERHAUL. REMOVED UNIT AND SENT FOR EXCHANGE. THIS OVERHAUL UNIT INSTALLED AND WORKED NORMALLY. AIRCRAFT RETURNED TO SERVICE.SDR 98ZZZX3668Pump · failedAIRCRAFT BROUGHT IN FOR MAINTENANCE. FOUND PUMP MOTOR CONTINUING TO RUN. TROUBLESHOOTING REVEALED THAT UNIT WOULD NOT PRODUCE PROPER PRESSURE TO TRIP PRESSURE SWITCH. REMOVED AND INSTALLED OVERHAULED UNIT. SYSTEM OPS NORMAL.SDR 98UAL900414Packing · failedNR 1 ENGINE HYDRAULIC PUMP WARNING LIGHT ILLUMINATED. *S/D* REPLACED PACKING FOR A ELECTRIC PUMP ACOUSTIC FILTER REF IPC 29-15-22-001. OPS AND LEAK CK NORMAL. A-SYS SERVICED TO FULL.SDR DHL98873002Seal · wornNR 4 ENGINE OIL QUANTITY INDICATION GOING TO ZERO, SHUT DOWN ENGINE AS PRECAUTIONARY. REPLACED HYDRAULIC PUMP PAD SEAL PER MM CHAP 29.SDR DL757981775Seal · tornLT HYD QTY EICAS MSG, STATUS PAGE SHOWED FLUID DECREASING. RAN THROUGH LOSS OF FLUID PROCEDURE. COULD NOT ISOLATE TO ANY SINGLE PUMP. WITH BOTH PUMPS OFF FLUID QTY DECREASED TO .14. FOUND TORN SEAL ON LEFT ENG HYD PUMP. REPLACED SEAL, RAN ENG, LEAK CK LEFSDR CA980909022Pump · leaking(CAN) TWO HOURS INTO FLIGHT, LOST ALL BLUE SYSTEM HYDRAULIC FLUID, APPROXIMATELY 45 MINUTES LATER, THE BLUE SYSTEM HYDRAULIC RESERVOIR OVERHEAT LIGHT CAME ON AND REMAINED ON FOR DURATION OF THE FLIGHT. MAINTENANCE FOUND BLUE SYSTEM ENGINE HYDRAULIC PUMP CASISDR 98ZZZX3867Spline · corrodedTHIS PUMP REMOVED DUE TO SHEARED DRIVE SPLINE. TOTAL TIME - 2,051. HOURS. EXAMINATION REVEALED CORROSION ON THE INSIDE OF THE SPLINE SHAFT.SDR 98ZZZX3866Spline · corrodedTHIS PUMP REMOVED DUE TO SHEARED DRIVE SPLINE. TOTAL TIME - NEW FROM PIPER FACTORY. EXAMINATION REVEALED CORROSION ON THE INSIDE OF THE SPLINE SHAFT.SDR AALA981587Pump · failedDFW - FLT 1564 - DURING CRUISE EN ROUTE NR 2 HYDRAULIC QUANTITY AND PRESSURE WENT TO ZERO. EXTENDED LANDING GEAR USING EMERGENCY HANDLE. LANDED DFW WITHOUT INCIDENT. REPLACED RIGHT ENGINE HYDRAULIC PUMP AND FILTERS. SYSTEM GROUND CHECKED NORMAL OPERATION. SDR 99ZZZX1333Pump · wornEXCESSIVE SPLINE WEAR. REPLACED PUMP WITH NEW UNIT, CORRECTED PROBLEM.SDR VNAA9808020Pump · failedON APPROACH, CREW RECEIVED FLAP CONTROL FAIL CAS MESSAGE. REVIEWED CHECKLIST AND PERFORMED 0 DEGREE FLAP LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE MAIN HYDRAULIC PUMP INOPERATIVE. REPLACED PUMP IN ACCORDANCSDR CALA9801498Hyd Pump · leakingTHE NR 2 ENGINE A-HYD PUMP LOW PRESSURE LIGHT ILLUMINATED AFTER TAKEOFF. THE NR 1 ENGINE A-HYD PUMP LOW PRESSURE LIGHT ILLUMINATED AND THE EMERGENCY CHECKLIST FOR LOSS OF HYD WAS COMPLETED. THE AIRCRAFT WAS RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE SDR 98ZZZX3238Power Pack · defectiveWHILE SELECTING LANDING GEAR DOWN, SYSTEM HAD TO BE CYCLED 4-5 TIMES, AND CIRCUIT BREAKER TRIPPED. WHEN ACFT WAS PUT ON JACKS, THE 5TH CYCLE, LANDING GEAR WOULD NOT COME DOWN. SHUTTLE VALVE STUCK IN THE UP POSITION (SPECIFIC PART P/N 1280802-1, MANIFOLD BODSDR 98UAL900394Pump · failedCREW REPORT, GREEN EDP LOW PRESSURE AND LOW GREEN SYSTEM PRESSURE. QUANTITY IS INDICATING ZERO AMBER ALERT. RETURNED TO DENVER. *S/D* GREEN SYSTEM HYD PUMP REPLACED.SDR HEEA0015654Pump · wornHYDRAULIC PUMP HAS WORN BEARING TRUNNIONS.SDR HEEA0015649Spline · wornINTERNAL SPLINE WORN ON HYDRAULIC PUMP.SDR HEEA0015648Shaft · wornHYDRAULIC PUMP SHAFT WORN.SDR HEEA0015647Shaft · wornHYDRAULIC PUMP SHAFT WORN.SDR HEEA0015646Pump · leakingPUMP LEAKING.SDR HEEA0015645Shaft · wornSHAFT SPLINE WORN.SDR HEEA0015641Shaft · wornDRIVE SHAFT WORN.SDR 98ZZZX3544Pump · failedPILOT LOST HYDRAULIC PRESSURE IN-FLIGHT. LANDED UNEVENTFULLY AT WILMINGTON AIRPORT. INVESTIGATION FOUND HYDRAULIC PUMP SEIZED AND SHAFT SHEARED.SDR 98ZZZX3627Pump · failedAPPROVED AIRCRAFT ACCESSORIES INC., CRS US2R225L OVERHAULED HYDRAULIC PUMP. WHEN INSTALLED, PUMP WOULD NOT PICK UP PRESSURE. BLED PUMP WITH NO RESULTS. WHEN THE PUMP WAS REMOVED, NOTED THE SNAP-RING IN THE BASE OF THE PUMP HAD COME OUT. THE INSIDE OF THE PSDR AALA981518Pump · failedMIA - FLT 915 - DURING CLIMB, YELLOW SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. FLIGHT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE UPPER ENGINE DRIVEN HYDRAULIC PUMP SHAFT SHEARED. REPLACED ENGINE DRIVEN HYDRAULIC PUMP AND MOTOSDR CA980814009Pump · leaking(CAN) HYDRAULIC PUMP FOUND LEAKING FROM THE AFT FLANGE.SDR AU981061Power Pack · failed(AUS) LANDING GEAR POWER PACK FAULTY. INVESTIGATION FOUND WORN `O' RING SEALS AND A STICKY TIME DELAY VALVE. PART TC: 9,639.SDR AU981398Power Pack · failed(AUS) HYDRAULIC POWER PACK FAILURE. LIMITED INFORMATION PROVIDED.SDR CA980818024Pump · worn(CAN) HYDRAULIC PUMP FAILURE ON LEFT SIDE FOLLOWING GEAR RETRACTION. PUMP SPLINES HAD WORN OFF UNTIL THEY STARTED TO SLIP. PUMP HARD TO TURN INDICATING A SPLINE PROBLEM.SDR AU980953Pump · failed(AUS) SYSTEM `B' ELECTRIC HYDRAULIC PUMP FAULTY. PART TC: 20,942.SDR HEEA0015398Spline · wornSPLINE WORN ON HYDRAULIC PUMP.
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