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 MALA030140Pump · malfunctionedDURING FLIGHT 3396, HYDRAULIC ACCUMULATOR PRESSURE WENT TO ZERO AND THE HYDRAULIC PUMP DID NOT RUN IN AUTO. CREW DECLARED AN EMERGENCY AND LOWERED THE GEAR USING EMERGENCY EXTENSION METHOD (EXPLOSIVE BOLTS). CREW BLEW BOLTS TO DROP GEAR AND AIRCRAFT LANDED WSDR RAIA00301027O-Ring · brokenELM - RIGHT ENGINE LOW OIL PRESSURE, SHUT DOWN ENGINE IN FLIGHT, EMERGENCY LANDING. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP SHAFT O-RING, LEAK CHECK OK.SDR RAIA00301026Pump · malfunctioned5272-ECM- RIGHT HAND HYDRAULIC PUMP PRESSURE FOLLOWS THROTTLE MOVEMENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND ENGINE DRIVEN HYDRAULIC PUMP, OPS AND LK CH OK.SDR MEX2003009Pump · failedFLT 258 - MEX-CJS - AIRCRAFT RETURNED TO GATE DUE TO LEFT ENGINE HYDRAULIC PUMP OUT OF SERVICE WITH CERO PRESSURE INDICATION. LEFT ENGINE HYDRAULIC PUMP WAS REPLACED IAW MM 29-10-05, ALL CORRECT. (M)SDR SWIA200311737Pump · malfunctionedRECEIVED A HYDRAULIC NR 1 LOW PRESSURE CAUTION MESSAGE CLIMBING THROUGH 14,000 FT. TURNED ON HYDRAULIC 1B AS PER QRH, HYDRAULIC PRESSURE STILL SHOWED ZERO. RETURNED TO PHX. REMOVED AND REPLACED LT ENGINE HYDRAULIC PUMP IAW MM 29-11-01 AND LT HYD PUMP CASE DSDR MEX2003007Pump · failedFLT 945 - MTY-MEX - AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCES OF LEFT ENGINE HYDRAULIC PUMP OUT OF SERVICE WITH ZERO PRESSURE INDICATION. LEFT ENGINE HYDRAULIC PUMP WAS REPLACED IAW MM 29-10-05, ALL CORRECT. (M)SDR USAASB03010Pump · faultyPHL - FLT 390 - EN ROUTE FROM CLT-DTW, THE 'A' HYDRAULIC SYSTEM ELECTRIC MOTOR DRIVEN PUMP LOW PRESSURE LIGHT ILLUMINATED WITH THE PUMP CYCLING ON AND OFF. DECISION WAS MADE TO DIVERT TO PHL WHERE THE FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLAREDSDR HEEA083716Pump · noisyHYD PUMP MAKES NOISE ON LET DOWN.SDR HEEA083715Shaft · wornHYD PUMP HAS WORN SPLINES.SDR HEEA083714Pump · noisyHYD PUMP MAKING NOISE INTERMITTENTLY.SDR HEEA083713Pump · noisyHYD PUMP MAKING ABNORMAL NOISE.SDR HEEA083712Pump · failedPUMP FAILED DURING LET DOWN HYDRAULIC LIGHT ILLUMINATED AND WHINING NOISE WAS NOTICED WHILE LIGHT WAS ON.SDR HEEA083711Pump · malfunctionedPUMP PRODUCING HYD PRESSURE ABOVE MANUFACTURERS LIMITS.SDR CA030116002Pump · failed(CAN) PRODUCTION FLIGHT TEST NR 4 DATED 8 JAN 03, HYDRAULIC NR 2 HI TEMP CAUTION POSTED JUST AFTER LEVELING ATF 410 TEMP MAXIMUM 104C, RT ENGINE SHUTDOWN, TEMP DECREASE TO NORMAL LIMIT. ENGINE RELIT PRIOR TO LANDING. EDP REMOVED AND INSTALLED. GROUND RUN CARRISDR QXEA0300008Pump · failedSUP - PDX - FLIGHT 2069 - UPON GEAR SELECTION DOWN, THE NR 2 ENGINE HYDRAULIC CAUTION LIGHT ILLUMINATED AND THE NR 2 HYDRAULIC FLUID WENT TO 0. MAINTENANCE INSPECTED THE AIRCRAFT AND THE NUMBER 2 HYDRAULIC SYSTEM AND REPLACED THE NUMBER 2 ENGINE DRIVEN PUMP ANSDR USAASB04005Pump · overheatedCLT - FLT 1456 - EN ROUTE FROM DCA TO FLL, THE B-SYSTEM ELECTRIC HYDRAULIC PUMP OVERHEAT LIGHT ILLUMINATED. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE B-SYSTEM ELECTRIC HYDRAULSDR AUS20021459Pump · misinstalled(AUS) NR 2 ENGINE HYDRAULIC PUMP FAULTY. INVESTIGATION FOUND THAT THE PUMP CASE DRAIN CHECK VALVE HAD BEEN FITTED BACK TO FRONT AND THE HOSE FROM THE CASE DRAIN TO THE PYLON COLLAPSED. HYDRAULIC PUMP SEVERELY OVERHEATED. PERSONNEL/MAINTENANCE ERROR.SDR TSAA0229255Pump · failedNR 2 EDP LOW PRESSURE LIGHT CAME ON 2.5 HOURS INTO FLT. SUSPECT PUMP FAILURE AS PRESSURE FOR SYS 'A' BEGAN DROPPING WHEN NR 2 ENGINE HYD PUMP MOMENTARILY TURNED OFF, DETERMINED NORMAL AFTER EVALUATION. NR 1 EDP LOW PRESSURE LIGHT ILLUMINATED ABOUT 3.5 HOURS SDR CA021217011Pump · failed(CAN) AFTER TAKEOFF AT ABOUT 200 FT AGL ' HYD 1 HIGH TEMP ' MSG. CAME ON EICAS. WHEN CHECKED, HYD TEMP IT WAS 116-117OC PRESSURE WAS AT 3600 PSI DURING FURTHER CLIMB THE TEMP WENT UP TO 133OC ON LEVEL FLIGHT TEMP WAS STABILIZED AT 124-126OC. FOR REST OF THE FLSDR HEEA082520Seal · leakingHYDRAULIC PUMP SEAL IS LEAKING.SDR 2003FA0000037Commutator · wornPUMP OPERATED SLOWLY. SENT FOR OVERHAUL WHICH SHOWED THAT MOTOR BRUSHES WERE WORN AND THE COMMUTATOR WAS WORN IRREGULARLY. LED TO SLOW OPERATION OF THE LANDING GEAR.SDR VJ32003F00008Motor · failedDURING PROGRESSIVE INSPECTION AFTER BLOWING GEAR DOWN AND CYCLING GEAR MOTOR WINDING SMELLED AS BURNED OUT. GEAR WOULD NOT CYCLED AFTER THAT, AND WOULD POP CIRCUIT BREAKER TO THE HYD PUMP RCCB. MOTOR ACTED AS IF THE LOAD WAS TOO HEAVY FOR THE MOTOR TO PRODUCSDR VJ32003F00007Motor · inoperativeDURING PROGRESSIVE INSPECTION AND CYCLING THE GEAR THE HYDRAULIC PUMP RCCB CIRCUIT BREAKER WOULD POP. THE HYDRAULIC MOTOR ON THE HYDRAULIC PUMP UNIT WAS PUTTING OUT OVER 75 AMPS.SDR VJ32003F00006Motor · failedDURING PROGRESSIVE INSPECTION AFTER BLOWING GEAR DOWN AND CYCLING GEAR MOTOR WINDING SMELLED AS BURNED OUT. GEAR WOULD NOT CYCLED AFTER THAT AND WOULD POP CIRCUIT BREAKER TO THE HYDRAULIC PUMP RCCB. MOTOR ACTED AS IF THE LOAD WAS TO HEAVY FOR THE MOTOR TO PRSDR 2003FA0000093Housing · crackedHOUSING IS CRACKED IN PORT.SDR 2002UALA01790Pump · failedRIGHT ENGINE DRIVEN HYDRAULIC PUMP FAILED. DIVERTED TO JFK. NR 2 ENGINE PUMP FAILURE. REPLACED PUMP AND APPLICABLE FILTERS.SDR XNOA01091Pump · failedAFTER T/O COMPLETE LOSS OF SYS "A" HYDRAULICS. MEMORY ITEM & EMERGENCY ABNORMAL CHECKLISTS PERFORMED. FOUND NR 2 ENGINE DRIVEN PUMP LEAKING FROM FLANGE BOLTS. REMOVED & REPLACED PUMP AS PER MM 29-11-31.SDR 2003F00133Pump · intermittentFLT 4480 - PIT-TOL, ON TAXI OUT, AIRCRAFT RETURNED TO GATE, HYDRAULIC PUMP INTERMITTENT IN AUTO AND OVERRIDE. FIRST OF TWO SQUAWKS THIS FLIGHT. (M)SDR VE32002F00006Pump · leakingTHE HYDRAULIC PUMP WAS LEAKING. IT WAS SENT TO A LOCAL VENDOR FOR REPAIR. THE VENDOR BORE PLUGGED FROM RESEVOIR PORT TO RELIEF BORE. THE CAUSE WAS EXCESSIVE CASTING IN THE HOLE AT MANUFACTURE.SDR AALA20021646Pump · failedEN ROUTE LHR-EWR, RT ENGINE HYDRAULIC PUMP FAILED. AIRCRAFT DIVERTED TO BOS LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE HYDRAULIC DRIVEN PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR 2003F00068Pump · failedFLT 4504 - IN CRUISE, THE MAIN HYDRAULIC PUMP FAILED. THE PILOT DECLARED AN EMERGENCY AND RETURNED TO PIT. MAINTENANCE REMOVED AND REPLACED THE HYDRAULIC PUMP. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR 0203819875Pump · failedDuring climb out from MSP the left engine driven hydraulic pump failed. Crew performed COM procedures for pump failure and overweight landing. Flight returned and landed uneventfully back at MSP. Maintenance replaced the engine driven pump and filters. AircrafSDR DL777021310Pump · leaking"C" SYSTEM HYDRAULIC QUANTITY LEVEL DECREASED IN FLIGHT. EMERGENCY LANDING DECLARED TO AIRPORT. AIRCRAFT LANDED WITHOUT INCIDENT.AIRCRAFT TOWED TO GATE. FOUND C2 ELECTRIC HYDRAULIC PUMP LEAKING. PUMP REPLACED.SDR VNAA0211010Pump · failedDURING CLIMB, THE CREW RECEIVED A MAIN HYDRAULIC INOP BLUE CAS MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK PROCEDURE AND THE MESSAGE DID NOT CLEAR. MAINTENANCE CONTROL WAS CALLED AND FLIGHT 4064 RETURNED TO DCA. MAINTENANCE INSPECTED AND REPLACESDR AUS20021296Pump · overheated(AUS) NR 1 HYDRAULIC PUMP OVERHEATED.SDR AUS20021295Pump · overheated(AUS) NR 1 HYDRAULIC PUMP OVERHEATED.SDR AALA20021590Pump · failedSJC - FLT 828 - EN ROUTE SJC, LEFT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED WITH QUANTITY DECREASING TO ZERO. AIRCRAFT LANDED SJC WITHOUT INCIDENT. REPLACED ENGINE HYDRAULIC PUMP. REPLACED CASE DRAIN FILTERS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR ABXA020278Pump · defectiveMANUAL REVERSION LIGHTS CAME ON DURING FINAL APPROACH. RAN LOSS OF HYDRAULIC PROCEDURES. REPLACED BOTH LT AND RT ENGINE DRIVEN HYDRAULIC PUMPS IAW DC-8 MM 29-10-12-02 AND 29-10-12. SERVICED SYSTEM IAW DC-8 AMM 12-00. LEAK AND OPS CHECKED GOOD.SDR AUS20021210Control Valve · loose(AUS) LANDING GEAR HYDRAULIC PUMP PRESSURE CONTROL VALVE LOOSE IN HOUSING.SDR AUS20021202Pump · making metal(AUS) LANDING GEAR HYDRAULIC PUMP CONTAMINATED WITH SWARF. PUMP IS ANEW ITEM. SUSPECT POOR QUALITY CONTROL BY MANUFACTURER.SDR MEX2002330Pump · failedAIRCRAFT RETURN TO PLATFORM DUE TO LT ENGINE DRIVEN HYD PUMP FAILURE. LOST PRSSURE SUDDENLY. HYD PUMP WAS CHANGED AND RT HYD PUMP WAS DEFERRED IAW MEL. DURING OVERNIGHT SERVICE, RIGHT PUMP WAS REPLACED IAW MM, TESTS OK.SDR 171944Housing · crackedHOUSING IS CRACKED AT PORT INTERSECTIONS. PROBABLE CAUSE MATERIAL IS TOO THIN AT INTERSECTION. REMOVE THIN WALL AT INTERSECTION AND MAKE HOUSING STRONGER.SDR CA021031021Shaft · sheared(CAN) NR 2 ENGINE DRIVEN HYDRAULIC PUMP FAILED AFTER START. SHAFT ASSY FOUND SHEARED. PUMP REPLACED.SDR 02101401Pump · failedLeft engine hyd. pump overheat, overheat light out ten minutes later. Loss of Hyd. Qty.. Left elec. pump turned off. Hyd press. 600 P.S.I. PTU could be heard cycling, followed by total loss of pressure and PTU lower EICAS Msg. illuminated. An uneventful landinSDR ALG2003F00049Pump · failedDURING FLIGHT, PILOT REPORTED PARTIAL HYDRAULIC FAILURE, UPON LANDING THE MECHANIC REMOVED AND REPLACED THE HYDRAULIC PUMP AND HYDRAULIC FILTER, THE AIRCRAFT WAS CHECKED FOR LEAKS AND OPS CHECK WAS SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE.SDR SWIA200211303Pump · leakingLOSS OF ALL NR 3 SYSTEM HYDRAULIC FLUID. REMOVED AND REPLACED ELECTRIC HYDRAULIC PUMP 3A WITH SERVICEABLE UNIT IAW MM 29-12-03. OPS AND LEAK CHECK GOOD.SDR IU62002F00035Housing · erodedEROSION AROUND STROKING PISTON PORT. STEEL SLEEVE OR ALTERNATE SEAL.SDR MALA020588Pump · failedDURING TAXI OF FLIGHT 3329, A/C LOST ALL HYDRAULIC PRESSURE WITH ASSOCIATED LOSS OF NOSE WHEEL STEERING AND BRAKING, PIC UTILIZED DIFFERENTIAL POWER TO EXIT TAXIWAY INTO TURF DUE PROXIMITY TO END OF TAXIWAY. PROP STRIKE TO PROP. MAINTENANCE REPLACED HYDRAULISDR SWIA200211268Pump · failedGREEN SYSTEM MAIN HYDRAULIC PUMP FAILED ON TAKEOFF. ELECTRONIC PUMP TOOK OVER. COMPLIED WITH QRH. RETURNED FOR NORMAL LANDING AT SFO. REPLACED LEFT ENGINE MAIN HYDRAULIC PUMP. RAN ENGINE. OPS & LEAK CHECK GOOD.SDR MEX2002312Pump · failedFLT 579 - MEX-CUN - AIRCRAFT RETURNED TO BLOCKS DUE TO THE ABSENCE OF HYDRAULIC PRESSURE FROM THE LEFT ENGINE DURING TAXIING. TECHNICAL PERSONNEL REVIEWED THE HYDRAULIC PUMP AND IT WAS REPLACED IAW MM 29-10-05, TEST OK. (M)
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