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 CA110616004Pump · failedDURING CRUISE FLIGHT, CREW NOTED A HYD VOLUME LOW (B SYS) ANNUNCIATION ON THE EICAS. FLIGHT CREW FOLLOWED CHECKLIST PROCEDURES AND OFFLOAD HYD B SYS. ACFT DIVERTED, WHERE A PAN CALL WAS INITIATED. ACFT LANDED WITHOUT INCIDENT. A VISUAL INSP OF THE ACFT REVESDR DXTA2011061704620Pump · leakingENROUTE, LOST NR 1 HYD FLUID QTY. NEAR ZERO LEVEL ON LANDING. ON POST FLIGHT INSPECTION, HYD FLUID WAS VISABLE DRIPPING FROM THE NR 2 NACELLE. VERIFIED LEAKS AT REGULATOR ON HYD PUMP. R & R NR 2 FWD HYD PUMP IAW MM 29-104, REV DATE 05/2009. RAN ENGINE NO SDR YENA20110615278Pump · failedFLT 263 SMF-LGB, AT FL390 HYD BLUE ELECTRIC PUMP LOW PRESSURE IN ECAM. THE CREW ADVISED ATC TO HAVE EMERGENCY EQUIPMENT STANDING BY AND APPLIED LANDING DISTANCE PROCEDURE. THE TECHNICIAN REMOVED AND REPLACED BLUE ELECTRIC HYDRAULIC PUMP AS PER AMM 29-12-51. SDR SWAA114408Pump · faultyDECLARED EMERGENCY -- FLASHING MASTER CAUTION FOR NR 1 ENGINE DRIVEN HYDRUALIC PUMP LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT. A SYSTEM HYDRAULIC QUANTITY DROPPED TO 1/4. REMOVED AND REPLACED NR 1 ENGINE DRIVER HYDRAULIC PUMP PER MM.SDR SWIA201126473Pump · leakingHYD EDP 2A CAUTION IN CRUISE WITH 0 PERCENT QUANTITY AFTER LANDING. (FLT 5608) REPLACED NR 2 HYDRAULIC ENGINE DRIVEN PUMP, REPLACED PRESSURE MANIFOLD FILTERS FOR SYSTEM NR 2, AND REPLACED NR 2 CASE DRAIN FILTER. P/N: 66190-05 S/N OFF: K0414ASDR CA110623002Pump · failedNR 2 EDP WAS FAILED IN FLIGHT, FOLLOWED BY THE LOSS OF ALL HYD FLUID OF SYS 2 AFTER NR 2 ACMP ACTIVATION.SDR CA110610011Pump · brokenFLIGHT CREW DECLARED EMERGENCY DUE TO LOSS OF NR1 HYD FAILURE. AFTER UNEVENTFUL LANDING, MX PERFORMED A FULL INSP TO THE ACFT WHERE IT WAS DISCOVERED THAT THE NR1 EDP BOTTOM PLATE CAME OFF. ALL THE HYD FLUID WAS DEPLETED DUE TO THE MISSING PLATE. MX REPLACED SDR UALA2011060902834Pump · malfunctionedAIR DEMAND PRESS LIGHT ILLUMINATED AND EICAS C HYD DEM PUMP. CTR AIR DEMAND PMP INOP, CYCLED BREAKER, RESET OVERSPEED SWITCH, NO HELP. NEEDS FURTHER TROUBLESHOOTING. SUSPECT PUMP INOP. NO EXHAUST AIR OUT OF PUMP. REPLACED OVERSPEED CARD M1 057, NO HELP. RSDR UHLA2011060900199Pump · leakingIN CRUISE FLIGHT RECEIVED HYD SYS 2 LO QTY. DECLARED EMERGENCY, LANDING UNEVENTFUL. FOUND E2 EDP LEAKING AT CASE, REMOVED AND REPLACED E2 EDP IAW EMB 170 MM 29-11-01. OPS AND LEAK CHECK GOOD.SDR SWAA114181Pump · faultyAIR TURNBACK/DECLARED EMERGENCY. NR 2 ENGINE DRIVEN LOW HYDRAULIC PRESSURE LIGHT FLICKERING WITH ASSOCIATED FLUCTUATING PRESSURE INDICATION. REMOVED AND REPLACED NR 2 ENGINE DRIVEN PUMP PER MM.SDR UALA2011060602745Pump · leakingNR 2 ENGINE HYD PUMP LEAKING AT MATING SURFACES. REPLACED NR 2 EDP PER MM. GROUND RUN OKAY.SDR SIMA201115801Pump · failedON FLIGHT 2944 DURING TAKEOFF THE CREW REPORTED, RECEIVED A NR 1 HYDRAULIC PUMP FAIL EICAS MESSAGE AT GEAR RETRACTION. THE CAPTAIN ELECTED TO RETURN TO MAF. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NSDR REXA201100342Pump · malfunctionedA/C DIVERTED FROM IND - DTW TO FWA FOR TOTAL HYDRAULIC FAILURE ON SYSTEM NR 3 CREW DECLARED EMERGENCY. STILL IN WORK FOR HYD PUMP REPLACEMENT & GEAR SWING.SDR SWIA201126384Pump · faultyGEAR DOWN DISAGREE WARNING MESSAGE. (FLT 6804) REPLACED 3B HYDRAULIC ACMP, MLG SELECTOR VALVE, REPLACED LT MLG UPLOCK LOCK. P/N: 17051-101, S/N OFF: NGL/1434/03, P/N: 750005000, S/N OFF: 0619, P/N: 848847, S/N OFF: MX657967.SDR AALA20110622TUL07Pump · failedBOS - CREW REPORTED LEFT HYDRAULIC PUMP FAILED DURING APPROACH. EMERGENCY DECLARED FLIGHT LANDED BOS WITHOUT INCIDENT. REPLACED LEFT ENGINE DRIVEN PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.SDR CA110610007Pulley · wornHYD PUMP PULLEY ASSY WAS FOUND TO BE WORN BEYOND LIMITS AND REQUIRED REPLACING THE PULLEY ASSY AND BEARING. THE BEARING IS NORMALLY A PRESSED FIT REQUIRING HEATING ONE PART AND COOLING THE OTHER BUT ON INSP THE BEARING WAS LOOSE ENOUGH TO FALL OFF THE PULLEY SDR CA110610006Pulley · wornDURING THE 100 HR INSP SB 63-005 WAS COMPLETED ON THIS ACFT IAW THE S/B THE PULLEY ASSY WAS FOUND TO BE WORN BEYOND LIMITS AND REQUIRED REPLACING THE PULLEY ASSY AND BEARING. THE BEARING IS NORMALLY A PRESSED FIT REQUIRING HEATING 1 PART AND COOLING THE OTHESDR SWIA201126366Pump · failedNOSE GEAR WOULD NOT RETRACT. (FLT 6615) REPLACED NLG SELECTOR VALVE, PROXIMITY SENSOR UNIT AND REPLACED HYDRAULIC ACMP 3A. / P/N ON 750006000 S/N OFF 2255T, P/N ON 8-648-08 S/N OFF D665, P/N ON 848847 S/N OFF MX 653145.SDR CA110525003Pump · failedAPPROX HALFWAY THROUGH THE FLIGHT THE CREW REPORTED A BLUE HYD SYS LOW PRESSURE. ECAM HYD B SYS LOW PR ECAM ACTION , B SYS HYD TURNED OFF B HYD PUMP REPLACED IAW AMM 29-12-51.SDR F3LA2011052300652Pump · leakingPILOT REPORT YELLOW HYDRAULIC LOW RESERVOIR LEVEL. REMOVED AND REPLACED ENGINED NR2 HYDRAULIC PUMP DRIVER IAW AMM 29-13-51, PB 401, OPS CHECKS GOOD. FOUND SEVERAL LEAK YELLOW SYSTEM LINE TO PRESSURE SWITCH. REMOVED AND REPLACED LINE IAW AMM 28-23-11 LEAKED CHSDR CA110601001Drive Shaft · damagedACFT WAS STARTED, ROTOR WAS WOUND UP. HYD PRESSURE CAME ON-LINE FOR NR 1 SYS, NR 2 SYS GAVE ERRATIC INDICATION AND THEN WENT TO ZERO PRESSURE. ACFT WAS SHUTDOWN. NR 2 HYD PUMP WAS REMOVED FROM MAIN GEARBOX. DRIVE SHAFT SPLINES ON PUMP SIDE WERE FOUND STRIPPSDR UALA2011051302364Pump · leakingNR 1 ENG EDP CASE LEAK. REPLACED WITH NEW EDP AND INSTALLATION TEST OKAY.SDR REXA201100291Pump · malfunctionedNOSE LANDING GEAR DISAGREE. REMOVED AND REPLACED HYD SYSTEM 3B PUMP IAW AMM 29-11-03. COMPLYING PA & WORKSCOPE.SDR AALA20110505DFW01Pump · failedDFW - CREW REPORTED LEFT HYDRAULIC SYSTEM PRESSURE ZERO. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE HYDRAULIC PUMP THAT WAS BAD AND FILTERS. SYSTEM GROUND CHECK NORMAL OPERATION.SDR CA110503009Pump · failed(CAN) AIRCRAFT CAME IN WITH DISCREPANCY AUX HYD SYS FAIL MESSAGE IN FLIGHT . TROUBLESHOOTING ON GROUND REVEALED A BURNED MOTOR ASSEMBLY, THE AREA AROUND THE MOTOR PUMP ASSEMBLY IS AFFECTED . NO PRESSURE BUILT UP ON AUX HYD SYST WHEN PUMP SELECTED TO AUTO. FOSDR QXEA2011050600321Pump · leakingSLIGHT BURNING ODOR NOTICED DURING POWER REDUCTION AT ALTITUDE. COMPLIED WITH FIM TASK 71-00-00-810-817 AND SL DH8-400-SL-012A. OPERATED BLEED AIR IAW AMM 36-11-00-710-802 FOR 30 MINS. NO ODOR NOTED. REPLACED ENGINE DRIVEN HYD PUMP FOUND TO BE LEAKING. RETSDR UALA2011050202136Control Unit · faultyLT HYD ELEC PUMP. REPLACED LEFT ELCU, OPS CHECKED GOOD.SDR UALA2011050202163Pump · faultyLEFT HYD ELECTICAL PUMP EICAS CAME ON AGAIN WITH LOW PRESSURE LIGHT IN SWITCH. TURNED OFF PER CHECKLIST. REPLACED L-ELEC HYD PUMP PRESSURE SWITCH. ALSO CHECKED ALL DELTA P'S. NONE WERE POPPED PRESSURIZED SYS, ALL PARAMETERS NORMAL. RAN GEAR DOORS UP AND DSDR UALA2011050202135Pump · failedNUMEROUS TIMES IN CLIMB AND CRUSE, LEFT ELEC HYD PUMP LOW PRESSURE LIGHT AND EICAS LT HYD ELEC. DUE TO PREVIOUS HISTORY REPLACE LT ELECT PUMP. REPLACED LEFT ELEC HYD PUMP AND FILTERS.SDR CA110428017Coupling · failedTHE MAIN COUPLING THAT DRIVES THE HYD PUMP HAD FAILED. THERE WAS NO LOSS OF HYD POWER YET AS THE RUBBER COUPLING HAD LODGED ITSELF IN SUCH A WAY THAT IT COULD STILL DRIVE THE PUMP.SDR CNQR528863Shaft · shearedHYD VOLUME LOW (A) CAS MESSAGE ILLUMINATED. VERIFIED ZERO QUANTITY ON THE EICAS SYS. THE HYD PUMP FAIL (A) CAS MESSAGE CAME ON. THE CREW ACCOMPLISHED THE CHECKLIST INCLUDING THE GEAR BLOW DOWN AND EMERGENCY BRAKING.SDR Z5FA20110426001Pump · failedENROUT, CREW NOTICED "A" SYS HYD FAILURE. CREW FOLLOWED AFM EMERGENCY PROCEDURES AND DIVERTED. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. SYS WAS TROUBLESHOT TO A LT ENGINE HYD PUMP FAILURE. REPLACED LT ENGINE HYD PUMP, CASE DRAIN FILTER, PRESSURE FILTESDR C2XA11SH085Pump · failedDURING FLIGHT, THE AIRCREW RECEIVED AN EICAS MESSAGE THAT THE E1 HYD PUMP FAILED. THE FLIGHT WAS DIVERTED AND THE ACFT LANDED WITHOUT INCIDENT. AN EMERGENCY WAS NOT DECLARED. MX R & R THE DEFECTIVE PUMP IAW AMM 29-10-03. THE ACFT WAS APPROVED FOR RETURN TSDR USAA20110421SB058Relay · stuckPHL - IN FLIGHT, FLIGHT ATTENDANT REPORTED AN ODOR SIMILAR TO AN ELECTRICAL APPLIANCE (COMPUTER, ETC) OVERHEATING. NO SMOKE VISIBLE. SOURCE COULD NOT BE IDENTIFIED. ODOR SEEMED TO ORIGINATE IN REAR OF AIRCRAFT AND MOVED FORWARD. NO ODOR IN COCKPIT OR FROM SDR UALA2011042101936Pump · failedL ENG HYD PUMP OVHT, FLIGHT DIVERTED. REPLACED THE LEFT ENGINE DRIVEN HYD PUMP DUE TO PUMP FAILURE. PUMP FAILURE ALSO CAUSE OF FLUID LEAK.SDR MASA2011042102466Pump · vibrationABNORMAL LEFT ENG VIBE ABOVE 77 PC N2. REMOVED AND REPLACED NR 1 EDP, OPS CHECK GOOD.SDR CA110415006Pump · leakingENROUTE AND IN CRUISE, CREW EXPERIENCED A NR 2 HYD FAILURE. QRH WAS FOLLOWED AND FLIGHT CONTINUED TO PLANNED STATION. AN EMERGENCY WAS NOT DECLARED. AN UNEVENTFUL LANDING WAS CARRIED OUT AND ACFT TOWED TO GATE. NR 2 EDP REPLACED IAW AMM 29-11-01-04. NR 2 SDR ASMF201104002Pump · leakingCAPTAIN REPORTED THAT DURING CRUISE, THE HYD QTY LOW LT AND HYD PRESS PRI LT LIGHTS TURNED ON. THE FLIGHT CREW PERFORMED THE QRH 13.3 AND 13.22 PROCEDURES, CONFIRMING THE FAILURE AND CONTINUING TO DESTINATION. MX PERSONNEL, A REVISION, DETECTING HYD LEAK IN THSDR CA110406011Pump · failed(CAN) NUMBER 2 ENG HYD PUMP CAUTION LIGHT ON CLIMBING THRU 10,000 FT. PRESSURE WAS 0 UNTIL ACFT SPU TURNED ON. ATB TO BASE. REPLACED THE NR 2 EDP.SDR QXEA2011040700270Pump · failedNR 2 ENG HYD PUMP CAUTION LIGHT ILLUMINATED GOING THRU 10000'. RETURNED TO THE FIELD. LANDED ACFT AT 62900 LBS, DUE TO RETURN TO FIELD WHICH IS 900 LBS OVERWEIGHT. DESCENT RATE WAS 300FT/ MIN NOTED: NR 2 HYD PRESSURE WAS "0" ONCE A/C POWER TURNED OFF. PERSDR UALA2011033101546Pump · leakingHYD LEAK OUT OF ADP COMPARTMENT. SUSPECT WEEP HOLE ON ADP. REPLACED AIR DRIVEN HYD PUMP PER MM. LEAK AND OPS CHECK GOOD.SDR FDEA201103311256Pump · leakingTOTAL LOSS OF NR 2 HYD. FOUND UPPER RUDDER NON REV PUMP SHUTOFF VALVE LEAKING. REPLACED VALVE . REPLACED BOTH NR 2 ENG DRIVEN PUMP CASE DRAIN FILTERS. NO CONTMINATION NOTED. FOUND FLUID IN NR2 RESERVIOR AND BOTH CASE DRAIN FILTERS. RAN NR 2 ENG HYD PUMPSSDR NSVA2011064Pump · malfunctionedON APPROACH TO AEX, ABOUT 30-35 NM OUT AT 8,000 FT, CREW FOUND THE HYDRAULIC PUMP WAS RUNNING CONSTANTLY. DECLARED AN EMERGENCY AS A PRECAUTION, AND LANDED WITH ALL HYDRAULICS WORKING NORMALLY. OPERATED FLAPS WITH GEAR UP AND DOWN. CLEANED CONNECTORS ON RIGSDR UALA2011032101325Pump · failedC HYDRAULIC PRI 2 PUMP FAILED IN FLIGHT. REMOVED AND REPLACED NR 2 ACMP PER MM AND LEAK CHECKED GOOD PER MM.SDR RMXA308855Pump · unserviceableAFTER AIRCRAFT START UP, THE PILOT REALIZED HE DID NOT HAVE HYDRAULIC POWER. THE AIRCRAFT WAS THEN SHUT DOWN. UPON INSPECTION OF THE HYDRAULIC SYSTEM AND CONSULTATION WITH EUROCOPTER TECHNICAL REPRESENTATIVES, IT WAS DISCOVERED THAT THE HYDRAULIC PUMP HAS FAILSDR UALA2011031701291Pump · faultyL ELEC HYD PUMP OVERHEAT EICAS, FLIGHT DIVERTED. LOW PRESSURE LIGHT OPERATED NORMAL. PUMP PRESSURE VERIFIED TO BE OPERATING NORMAL. TEMP INDICATION 24 DEGREES C. REPLACED L ELEC HYD PUMP PER AMM. LEAK CHECKED GOOD.SDR MZZA2011031500010Pump · defectiveENGINE DRIVEN "A" PUMP LOW PRESSURE LIGHT CAME ON, ON APPROACH TO GUAM. QRH PROCEDURE COMPLETED. FOUND EDP BAD. REMOVED AND REPLACED ENGINE DRIVEN PUMP PER AMM 29-11-11. OPS AND LEAK CHECK NORMAL. OK FOR SERVICE. ROTABLE PARTS CHANGE WAS INDICATED - TT 1SDR UALA2011031401214Pump · leakingRT ENGINE: FOUND HEAVY LEAK ON THE MAIN HYDRAULIC PUMP. RT MAIN HYD PUMP REPLACED IAW AMM. DRY RUN PERFORMED AND NO LEAK OBSERVED. GND IDLE RUN WILL BE PERFORMED BY CREW BEFORE DEPARTURE. DUE TO RH HYDRAULIC PUMP REPLACEMENT ACCOMPLISH ENGINE RUN TEST. PSDR CA110314006Shaft · sheared(CAN) THERE WAS AN ISSUE WITH THE GEAR WHEN IT WAS SELECTED TO THE UP POSITION, THE INTRANSIT LIGHT REMAINED ILLUMINATED FOR AN EXTENDED PERIOD OF TIME SO THE CREW BROUGHT THE GEAR HANDLE BACK TO THE NEUTRAL POSITION. THERE WAS AN INDICATION OF THREE GREEN ANDSDR NSVA2011047Pump · failedAT 40-50 MN FROM LFT CREW RECEIVED A HYDRAULIC PUMP FAIL WARNING. CREW DECLARED EMERGENCY. LFT HAD WINDS FROM THE SOUTH, LOW CIGS/VIS AND ONLY A VOR APPROACH TO A SHORT RUNWAY AVAILABLE. CAPT DID NOT FEEL COMFORTABLE WITH THIS, SO DIVERTED TO LCH. CAPT USE
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