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 CA000830018Packing · leaking(CAN) CREW REPORTED HYDRAULIC LEVEL SYSTEM NR1 AT 30% AT TOP OF CLIMB. DROPPED TO 25% 3 MINUTES LATER. MAINTENANCE FOUND LEAK FROM HYDRAULIC PUMP. THEY REPLACED THE PACKING.SDR DLM11001451Seal · leakingLAST 10 MIN OF FLT, OIL QTY WENT TO 0 OIL PRESS, REMAINED ABOVE MINIMUM. FOUND 2 ENG FWD HYD PUMP GARLOCK SEAL LEAKING. REPLACED SEAL AND REMOVED PUMP PER MEL 29-11-01A. RAN ENGINE, LEAK CHECKS GOOD.SDR SIMA2111Pump · inoperativeDFW - FLT 3290 - ON FINAL APPROACH, HYDRAULIC CENTRAL WARNING PANEL LIGHT ILLUMINATED. MAIN LANDING GEAR NOT INDICATING DOWN. PERFORMED CHECKLIST. ALL GER SUBSEQUENTLY INDICATED DOWN AND LOCKED. HYDRAULIC QUANTITY NORMAL AT ALL TIMES. MAINTENANCE REMOVED SDR REXA00006Pump · malfunctionedDURING CRUISE AT FL270, CREW RECEIVED A NR 2 HYDRAULIC HI TEMP CAUTION ON EICAS. SECONDARY INDICATIONS ON THE SYNOPTIC PAGE REVEALED NR 2 SYSTEM PRESSURE WAS A 3600 PSI AND THE TEMPERATURE OF THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP WAS RAPIDLY CLIMBING. RETARDSDR HALA0000236Pump · failedFLT 006 - OGG - NR 2 ENGINE DRIVEN HYDRAULIC PUMP WOULD NOT DEPRESSURIZE WITH SWITCH IN OFF POSITION. REMOVED AND REPLACED NR 2 ENGINE DRIVEN HYD PUMP, LEFT PUMP. OPERATIONAL AND LEAK CHECK GOOD. ALL HYDRAULIC QUANTITIES ARE AT NORMAL FULL LEVEL. WORK DONESDR SIMA2014Pump · failedDFW - FLT 3576 - MAIN HYDRAULIC PUMP FAIL ON LANDING. REMOVED AND REPLACED HYDRAULIC PUMP IAW SAAB AMM 29-10-10. OPS CHECK GOOD. (M)SDR HALA0000229Pump · failedHNL - FLT 001 - NR 3 ENGINE RIGHT HYD PRESS LOW LIGHT ILLUMINATED DURING FLIGHT. PERFORMED ABNORMAL CHECK LIST, HYD QTY, TEMP AND PRESSURE NORMAL. FOUND NR 3 RIGHT ENGINE HYD PUMP LEAKING FROM CASE. REPLACED NR 3 RT ENGINE DRIVEN HYD PUMP. GROUND RUN UP ANSDR BJNA000702Seal · brokenNR 1 HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT. SYSTEM QUANTITY SHOWED 1-3 GALLONS. REMOVED AND REPLACED NR 1 HYDRAULIC PUMP, IAW BMM 29-11-31. OPS CHECK AND LEAK CHECK GOOD, IAW BMM 29-11-31. (M)SDR DL72S001346Pump · leakingCOMPLETE LOSS OF SYSTEM B HYDRAULICS IN FLIGHT. FOUND NR 1 B-SYSTEM ELEC PUMP LEAKING FROM PUMP DRAIN. CHECKED/REPLACED BOTH PRESSURE AND CASE DRAIN FILTERS, FOUND CLEAN. REPLACED NR 1 B-SYSTEM ELEC HYD PUMP. LEAK CHECK OF PUMP AND FILTERS OK.SDR AWXA0000469Pressure Switch · failedAIR TURNBACK, EMERGENCY DECLARED. LOST NR 1 AND NR 2 HYD PUMP ON DOWNWIND WHEN FLAPS WERE SELECTED (AC WENT TO DIRECT LAW). REMOVED AND REPLACED NR 1 AND NR 2 ENGINE PUMP PRESSURE SWITCHES IAW MM 29-32-12, OPS CHECK GOOD.SDR AWXA0000458O-Ring · leakingEMERGENCY DECLARED, ECAM SHOWS YELLOW HYDRAULIC SYS LOW LEVEL. FOUND NR 2 ENGINE HYD PRESS SWITCH LEAKING. REMOVED AND REPLACED PRESSURE SWITCH O-RING. LEAK AND OPS CK GOOD, RESERVICED 3 GAL SKYDROL.SDR AU000611Pump · failed(AUS) PILOT REPORTED LOW HYDRAULIC PRESSURE. INVESTIGATION FOUND THE RT HYDRAULIC PUMP WAS DAMAGED. ON NEXT FLIGHT THE PILOT REPORTED THAT THE HYDRAULIC PRESSURE HAD INCREASED TO THE 'RED LINE'. THE POWER PACK WAS THEN REMOVED AS A RESULT OF THECONTAMINATION FSDR 20001114SH012Pump · failedATL/MBJ - FLT JM 052 - PRIOR TO FLIGHT, AT ENGINE START, THE LEFT NR 1 ENGINE HYDRAULIC PUMP INDICATED ZERO PSI. AFTER TROUBLESHOOTING, PUMP REPLACED AND AIRCRAFT DISPATCHED FOR SERVICE. THIS REPORT REMAINS OPEN UNTIL A STRIP REPORT IS AVAILABLE. TOTAL LANDSDR 20001114SH002Pump · failedMBJ/ATL - FLT JM 053 - DURING ENGINE START, HYD PRESSURE REMAINED AT ZERO. CAUSE OF THE PUMP''S FAILURE SEEMED TO HAVE BEEN A WEAR-OUT OF ITS COMPONENTS. THIS WAS THE FIRST REMOVAL SINCE IT WAS INSTALLED IN A NEW CONDITION. THIS PART IS MAINTAINED ''ON CONDSDR 0002411236Pump · failedDURING CRUISE, NR 2 HYDRAULIC PRESSURE BEGAN TO FLUCTUATE AND EVENTUALLY DROPPED TO ZERO. FLIGHT RETURNED TO DTW. MAINTENANCE REPLACED THE NR 2 ENGINE HYDRAUILC PUMPS AND FILTER. OPERATIONAL CHECK OK.SDR 20000721SH028Gear · wornINTERNAL SPLINES ON HYDRAULIC PUMP WORN EXCESSIVELY CAUSING HYDRAULIC PUMP TO START TO FAIL. PUMP OVERHAULED 432.8 HOURS PRIOR TO FAILURE. REASON FOR FAST SPLINE WEAR UNKNOWN. (X)SDR CA000808016Pump · failed(CAN) DURING DESCENT EICAS MESSAGES INDICATED LT HYDRAULIC QUANTITY, THEN LT HYDRAULIC EDP AND THEN LT HYDRAULIC OVERHEATED PUMP WAS TURNED OFF. EDP CHANGED I.A.W. M.M. 29-11-05. LEFT OIL FILTER EICAS MESSAGE OBSERVED. DMI 18663 RAISED I.A.W. M.E.L. 79-35-2.AISDR 2000UALA00384Connector · failedLEFT HAND ELECTRIC HYDRAULIC PUMP FAILED. *S/D* CONNECTOR PIN WAS FOUND BURNED FROM ARCING. REPLACED PUMP AND AC CONNECTOR.SDR 0002315512Pump · failedENROUTE MSP-LAX, THE LEFT HYDRAULIC SYSTEM QUANTITY AND PRESSURE BEGAN DECREASING. THE FLIGHT DIVERTED TO DEN AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT ENGINE DRIVEN PUMP DEFECTIVE. THE LEFT ENGINE DRIVEN PUMP WAS REPLACED WITH A SERVICEABLE UNITSDR SIMA1787Pump · failedORD - FLT 4329 - FLIGHT CREW DECLARED EMERGENCY ANNOUNCING NR 1 HYDRAULIC SYSTEM OVERHEATED INDICATION DURING FLIGHT. REMOVED AND REPLACED NR 1 HYDRAULIC PUMP. OPS AND PRESSURE CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR 20000721SH030Connector · shortedHYA - FLT 13236 - PON TURNING ON AUXILIARY HYDRAULIC PUMP, SEVERAL OF THE LEFT ESSENTIAL BUS CIRCUIT BREAKERS TRIPPED. TROUBLESHOOTING IS STILL IN PROGRESS, HOWEVER, A FAULT/SHORTED CANNON CONNECTOR APPPEARS, AT THIS TIME, TO BE THE PROBLEM. (X)SDR G60A049Clamp · wornPRIOR TO DEPARTURE WHEN NR 1 AUXILIARY HYDRAULIC PUMP SELECTED ON, SPARKS WERE EMANATING FROM RIGHT MAIN WHEELWELL. FOUND 2 OF 3 AUXILIARY HYDRAULIC PUMP POWER WIRES CHAFED AND SHORTED TO WORN ADEL CLAMP THAT WAS MISSING RUBBER CUSHION. REMOVED AND REPLACED SDR GAIA00365APump · failedFLT 727 - MHR - LOSS OF HYDRAULIC FLUID, THEN PRESSURE (HYDRAULIC SYSTEM A). ALTERNATE FLAPS OPERATION REVERSED. AIRCRAFT RETURNED AND MADE UNEVENTFUL LANDING AT MHR. VERIFIED PROPER OPERATION OF I/N AND OUTBOARD ALTERNATE FLAPS. FOUND CONNECTORS TO INDICASDR SIMA1663Pump · failedDFW - FLT 3643 - DIVERTED BACK TO DFW FOR NR 2 HYD PUMP FAILURE. REMOVED AND REPLACED NR 2 ENGINE DRIVEN HYD PUMP ASSY AND BROKEN QUILL SHAFT ASSY IAW CMM 72-60-05 AND AMM 29-10-03. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR VNAA0006004Pump · failedAT THE START OF THE TAKEOFF ROLL, THE CREW RECEIVED A HYDRAULIC MAIN TEMPERATURE HIGH MESSAGE. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE MAIN HYDRAULIC PUMP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 29-SDR CA000621013Pump · defective(CAN) LANDING GEAR SELECTOR HANDLE WOULD NOT RETURN TO NEUTRAL DURING ENGINE SHUTDOWN CHECK. NEW HYDRULIC PUMP INSTALLED AND LANDING GEAR SELECTOR CHECK FUNCTIONED NORMALLY. SUSPECT LOW VOLUME AND/OR PRESSURE OUTPUT FROM REMOVED PUMP. DEFECTIVE PART RETURNED TSDR AU000485Pressure Switch · faulty(AUS) LANDING GEAR POWER PACK PRESSURE SWITCH FAULTY.SDR DLM88001118Pump · unserviceableON APPROACH LEFT HYD PRESS LOW LIGHT ON WITH 0 PRESS ON GAUGE. HYD QTY NORMAL. REPLACED ENG HYD PUMP CASE DRAIN FILTER AND PRESS FILTER.SDR CA000719027Screw · broken(CAN) HYDRAULIC PUMP CAP SCREWS BROKEN ALLOWING HEAD TO SEPARATE FROM BODY. HYDAULIC FLUID DISCHARGED THROUGH SEPARATION IN PUMP. CREW LANDED AIRCRAFT USING EMERGENCY HYDRAULICS.SDR HALA0000160Pump · failedHNL - FLT 128 - AIR TURN BACK, HYDRAULIC QUANTITY LOSS, RIGHT SYSTEM. REPLACED ENGINE DRIVEN HYD PUMP PER MM 29-10-5. REPLACED ELEC HYD PUMP PER MM 29-10-6. REPLACED ALL HYD FILTERS IN RIGHT SYSTEM. SERVICED SYSTEM TO PROPER LEVEL. GROUND RUN NR 2 ENGNE, SDR ARWA060002Pump · bypassingAFTER TAKEOFF OUT OF MIAMI, PERFORMED UPLATCH CHECK, GEAR NOT LATCHED, LIGHT ILLUMINATED AND HEARD NOSE GEAR FALL. PERFORMED ABNORMAL CHECK LIST AND GEAR FELL OUT IN HYD PUMP BYPASS POSITION. RETURNED TO MIAMI WITHOUT INCIDENT. T/S REMOVED AND REPLACED GEARSDR USAAD00089Pump · leakingPIT-ORD - FLT 909 - AFTER SELECTING HYDRAULIC PUMPS ON HIGH, RIGHT PRESSURE GAUGE STARTED TO OSCILLATE AND THEN WETN TO ZERO. QRH PROCEDURES WERE IMPLEMENTED AND FLIGTH LANDED WITHOUT INCIDENT. AIRCRAFT WAS TOWED TO THE GATE. MAINTENANCE REPLACED THE ELECTRSDR 20000609SH012Drive Gear · failedHYDRAULIC PUMP FAILED IN-FLIGHT. PRECAUTIONARY LANDING COMPLETED. INSP REVEALED DRIVE SPLINES AT HYD DRIVE COUPLING (FEMALE SPLINES), AND THE DRIVE SPLINES AT THE HYD PUMP (MALE SPLINES) WERE PREMATURELY WORN. SPLINE ENGAGEMENT INSUFFICIENT FOR DRIVE DEMANDSDR COMA0010126Pump · leakingGREEN HYDRAULIC SYSTEM LOW PRESSURE AND LOW QUANTITY. REPLACED THE LEFT HAND ENGINE HYDRAULIC PUMP.SDR VNAA0005012Pump · failedON FINAL APPROACH, THE CREW TRIED TO LOWER THE FLAPS AND THE CREW RECEIVED A FLAP CONTROL AND HYDRAULIC PUMP FAIL CAS MESSAGES. THE CREW DID A GO-AROUND AND SELECTED THE STANDBY PUMP WHICH INDICATED NORMAL AND FLIGHT 4014 LANDED WITHOUT INCIDENT. MAINTENANCESDR 20000608SH019Cover · crackedCOVER ON VALVE IS CRACKED COMPLETELY ACROSS. POSSIBLE CAUSE: FATIGUE, OVERPRESSURED. (X)SDR 20000608SH018Housing · damagedHOUSING HAS A PIN HOLE ON OPPOSITE SIDE OF PORT 1. POSSIBLE CAUSE: FATIGUE, HIGH TIME ON UNIT, AND/OR DEFECT IN HOUSING. (X)SDR QXEA0001161Pump · malfunctionedPDX- AFTER NORMAL TAKEOFF AT PDX ON CLIMBOUT, TORQUE ON NR 1 ENGINE STARTED DROPPING OFF. A 45 PERCENT TORQUE DIFFERENCE ON NR 1, 2.3 INCH SPLIT ON POWER LEVERS. AT CRUISE 50 PERCENT ON NR 1, 90 PERCENT ON NR 2. AIRCRAFT RETURNED TO FIELD, UNEVENTFUL LANDINSDR 2000UALA00231Pump · failedLEADING EDGE SLAT NR 6 DID NOT EXTEND FOR LANDING AT DEN. AIRCRAFT LOST SYSTEM A HYDRAULICS. AIRCRAFT TOWED TO THE GATE. *S/D* REPLACED NR 1 ENG HYD PUMP AND CASE DRAIN FILTER ASSY, NO CONTAMINATION WAS FOUND.SDR DL72W000876Pump · inoperativeFOUND NR 2 B SYS HYD PUMP 3 PHASE C/B A PHASE LUG BURNT NEARLY THROUGH. CHECKED PWR AT PUMP CONNECTOR AND A PHASE READ 19 VOLTS. LUG WAS BURNT AND CASE MELTED. ALSO, THE WIRE INSULATION WAS BURNT. REPLACED NR 2 B PUMP, REPLACED C/B 823 AND RE-TERMINATED LUSDR 2000UALA00218Switch · brokenABORTED TAKEOFF AT 110 KNOTS, DUE TO THE NR 1 CENTER HYDRAULIC PUMP SWITCH. *S/D* LEFT HYDRAULIC ELECTRIC PUMP SELECT SWITCH POPPED OUT ON TAKEOFF ROLL. REPLACED SWITCH.SDR DLM88000807Pump · inoperativeDURING SLAT EXTENTION ON APPROACH, LEFT HYDRAULIC SYSTEM PRESSURE WENT TO 0. LEFT HYDRAULIC QUANTITY REMAINED STEADY AT 19 QTS. REMOVED AIR FROM SYS, REPLACED ENG DRIVEN PUMP PER M/M, CKS OK. NO LEAKS, OPERATED ALL FLIGHT CONTROLS, PRESS REMAINED STEADY, OSDR AU000348Bearing · failed(AUS) SYSTEM A HYDRAULIC PUMP FAILED INTERNALLY. SUSPECT CAUSED BY FAILED TRUNNION BEARINGS. METAL CONTAMINATION OF HYDRAULIC FILTERS.SDR A6WA0000030Motor · failedOVER TEMP AND HYDRAULIC MAIN PUMP LOW PRESSURE FLUCTUATING. REMOVED AND REPLACED MAIN HYDRAULIC PUMP IAW AMM.SDR CA000412019O-Ring · damaged(CAN) DURING CLIMB, A/C MADE AN UNSCHEDULED LANDING DUE TO R/H ENGINE SHUT-DOWN.SDR CA000427034Pump · failed(CAN) THE LANDING GEAR WAS SELECTED DOWN BUT THE GEAR REMAINED IN THE UP POSITION. MAINTENANCE FOUND THE MOTOR OF THE POWER PACK TO BE UNSERVICEABLE. THE ASSEMBLY WAS REPLACED.SDR 2000UALA00164Pump · failedRT HYD PRIMARY HYDRAULIC PUMP EICAS MSG WITH ASSOCIATED PRESS LT ILLUMINATED. AMBER ALERT, OTHERWISE NORMAL LANDING. *S/D* ENGINE DRIVEN PUMP HAD INTERNAL FAILURE. REPLACED PUMP.SDR DL757000591Pump · failedLT HYD QTY DECREASED TO 0 AND SYS PRESS LIGHT ILLUMINATED. EICAS MESSAGE L HYD SYS PRESS DISPLAYED AND RUDDER RATIO LIGHT. REPLACED LT ENGINE HYD OUT PRESSURE LINE AND LT ENGINE HYD PUMP. SERVICED LT SYSTEM AND RAN LT ENG ALL CHECK NORMAL. INSPECTED HYD FSDR SWAA000577Pump · inoperativeNR 2 ENGINE HYD PUMP FAILED AND LOST A-SYS HYD FLUID. R&R BOTH NR 1 AND NR 2 ENGINE HYD PUMPS, R&R ALL A-SYS HYD FILTERS PER MM.SDR 0001001150Pump · failedDURING CRUISE AT FL350, THE NR 3 ENGINE RIGHT HYDRAULIC PUMP TEMPERATURE HIGH LIGHT ILLUMINATED. FOLLOWED COM PROCEDURE AND RETURNED TO MSP. FLUID QUANTITY IN NR 3 SYSTEM WENT TO ZERO. FLIGHT LANDED IN MSP WITHOUT INCIDENT. REPLACED BOTH HYDRAULIC PUMPS AN
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