JASC 2913
Service difficulty reports · 4,062
Reports filed under 2913 · Hydraulic Pump (Electric/Engine), Main, newest first.
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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 2001F00231Pump · failedSAL - FLT 390 - DURING CLIMB, THE CAPTAIN REPORTED AIR ENG 1 BLEED ABNORMAL PRESSURE, AIR ENG 1 BLEED FAULT AND HYD GREEN ENG 1 PUMP LOW PRESSURE. THE AIRCRAFT RETURNED TO SAL STATION FOR MAINTENANCE. AFTER LANDING, MAINTENANCE TECHNICIAN PERFORMED FAULT ANASDR HNAA010049Connector · corrodedNR 2 ENGINE HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED IN FLIGHT, PRESSURE INDICATION WAS NORMAL. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. FOUND CORROSION ON CONNECTOR PINS. CLEANED CONNECTOR PINS OF CORROSION.SDR ASOA01136Pump · leakingFLT 4288 - DURING FLIGHT FROM CHA TO ATL, THE BLUE HYDRAULIC SYSTEM FAILED. AN EMERGENCY WAS DECLARED. AIRCRAFT CONTINUED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BLUE AC HYDRAULIC PUMP. OPERATIONAL CHECKS GOOD. AIRCRAFT RESDR AUS20010977Motor · dirty(AUS) LANDING GEAR HYDRAULIC POWER PACK ELECTRIC MOTOR FAULTY.INVESTIGATION FOUND LIGHT CORROSION IN COMMUTATOR END OF MOTOR. THE MOTOR WAS ALSO DIRTY WITH THE BRUSHES STICKING IN THE BRUSH HOLDERS. HYDRAULIC RETURN FILTER DIRTY.SDR 2001UALA01609Pump · failedAIRCRAFT EXPERIENCED B-HYDRAULIC SYSTEM ZERO QUANTITY INDICATION DURING CRUISE. AIRCRAFT CONTINUED TO ORD. THE NR 1 ENGINE HYDRAULIC PUMP FAILED. REPLACED NR 1 ENGINE HYDRAULIC PUMP, SYSTEM TESTS NORMAL.SDR AUS20011409Pump · malfunctioned(AUS) NR 1 ENGINE NR 2 HYDRAULIC SYSTEM PUMP LOW PRESSURE.SDR KBMA88815Sleeve · strippedCOUPLING SLEEVE - SPLINES STRIPPED OUT. REMOVED AND REPLACED WITH NEW HYDRAULIC PUMP/ BEARING AND SERVICEABLE COUPLING SLEEVE.SDR DL76L011243Pump · leaking4 HOURS INTO FLIGHT, CTR HYD "RSVR" LIGHT AND "CTR HYD QTY" EICAS MESSAGE CAME ON. CTR HYD QUANTITY INDICATED 0.47RF. SWITCHED OFF ELEC PUMPS AND QTY CONTINUED TO DECREASE. SWITCHED ELEC PUMPS BACK ON AND ADP OFF AND QUANTITY CONTINUED TO DECREASE. SWITCHED SDR CA010809006Pump · failed(CAN) EMERGENCY LANDING WITH SMOKE IN COCKPIT. FOUND ELECTRIC HYDRAULIC PUMP BYPASSING THRU CASE DRAIN AND PUMP DEVELOPING 2,700 PSI ONLY. AFTER INSPECTION AIRCRAFT WAS FERRIED TO MAINTENANCE BASE WITH GEAR DOWN AND PUMP OFF. AC PUMP REPLACED. MULTIPLE GEAR RESDR 0102516306Service difficultyDURING FLIGHT, RECEIVED "HYD PRES ENG 4" AND "HYD QTY LOW" MESSAGES. THE HYDRAULIC FLUID QUANTITY IN THE NBR 4 SYSTEM INDICATED ZERO. TURNED OFF THE HYDRAULIC PUMPS FOR THE NBR 4 SYSTEM AND THE CREW DECLARED AN EMERGENCY. ALTERNATE EXTENDED THE LANDING GEAR ANSDR 2001F00167Pump · failedNR 1 ENGINE EDP EICAS STATUS MESSAGE, LOW PRESSURE LIGHT AND STATUS MESSAGE POWER XFER CAME ON. AIRCRAFT RETURNED TO STATION, AN UNEVENTFUL LANDING WAS ACCOMPLISHED. REPLACED ENGINE DRIVEN HYDRAULIC PUMP, OPERATIONAL CHECK GOOD. POWER TRANSFER UNIT OPERATIOSDR SWIA200110051Pump · inoperativeHYDRAULIC EDP 1A CAUTION MESSAGE ON EICAS , NO HYDRAULIC FLUID QUANTITY IN SYSTEM NR 1. FOUND LEAKING HYDRAULIC LINE IN PYLON, REMOVED AND REPLACED HYDRAULIC LINE AND ENGINE DRAIN PUMP IAW MM 29-11-01. OPS CHECK GOOD. LEAK CHECK GOOD.SDR DL73K011157Pump · defectiveHYD SYSTEM A PUMP 2/ LOW PRESSURE. REMOVED AND REPLACED RT EDP, REPLACED CASE DRAIN AND A SYS FILTERS SERV HYD, LEAK CKS GOOD.SDR JBXA000307Hydraulic System · failedDiscrepancy : Lost #2 engine driven hydraulic pump and all fluid. Corrective Action : Removed and replaced #2 ED hydraulic pump I-A-W AMM 29-11-01 Ops check and leak check good.SDR MASA01065Pump · failedFLT 6334 - BFL-PHX - DECLARED AN INFLIGHT EMERGENCY, THE NR 2 HYDRAULIC SYSTEM LOST QUANTITY. INDICATED 4 PERCENT DURING FLIGHT. THE ENGINE PUMP OPERATED AT LOW FLUID FOR 15 MINUTES DURING FLIGHT. MAINTENANCE REPLACED THE NR 2 ENGINE HYD PUMP. OPS CHECKS GSDR AUS20010793Pump · worn(AUS) ENGINE DRIVEN HYDRAULIC PUMP INTERNAL AND EXTERNAL DRIVE SPLINES WORN EXCESSIVELY.SDR CA010629039Pressure Switch · failed(CAN) DEPARTED YUL FOR KEF. WHILE IN CLIMB THE ENGINE NR 2 YELLOW HYDRAULIC PUMP FAULT LIGHT ILLUMINATED. THE PUMP WAS DE-ACTIVATED AND THE AIRCRAFT DIVERTED TO YHZ. MAINTENANCE TROUBLESHOOTING LOCATED A HYDRAULIC LEAK FROM THE HYDRAULIC PUMP NR 2 PRESSURE SWSDR 2001F00153Pump · failedSHORTLY AFTER GEAR RETRACTION LOST HYD SYSTEM 'A'. ACCOMPLISHED ABNORMAL PROCEDURE. RETURNED TO DFW. REMOVED AND REPLACED NR 1 AND NR 2 ENGINE DRIVEN HYD PUMP. RUN AND LEAK CHECK. REMOVED AND REPLACED NR 1 AND NR 2 ENGINE HYD FILTER, RUN OPS AND LEAK CHECSDR 2001F00135Pump · damagedSHORTLY AFTER GEAR RETRACTION LOST HYD SYSTEM 'A'. ACCOMPLISHED ABNORMAL PROCEDURE. RETURNED TO DFW. REMOVED AND REPLACED NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMP. RUN AND AND LEAK CHECK. REMOVED AND REPLACED NR 1 AND NR 2 ENGINE HYDRAULIC FILTER, RUN OSDR DHL2001363008Pump · failedGREEN PUMP NR 2 ENGINE DRIVEN PUMP FAILED. REMOVED AND REPLACED PUMP.SDR MALA010538Pump · malfunctionedDURING FLIGHT 3685 FROM MEM, THE GREEN HYDRAULIC HI TEMP CAUTION LIGHT ILLUMINATED. FOLLOWED QRH, AIR RETURN TO DTW. MAINTENANCE REPLACED NR 3 EDP IAW AMM 29-10-17 (201). OPS CHECK GOOD. P/N ON AND OFF 521449, S/N ON MX639940, S/N OFF MX619638. REPLACED GSDR CA010713008Belt · frayed(CAN) FRAYING AT SEAM. THESE BELT ARE GOOD FOR 600 HOURS. WE HAD TO REPLACE THIS BELT EARLY AS WE THOUGHT IT WOULD NOT GO THE FULL 600 HOURS DUE TO THE FRAYING AT ITS SEAM.SDR ERA2001F00003Belt · brokenHYDRAULIC PUMP DRIVE BELT FAILED. HYDRAULIC CAUTION LIGHT ILLUMINATED AND HORN ACTIVATED ABOUT ONE MILE FROM LANDING LOCATION. PILOT CONTACTED CONTROL TOWER AND ADVISED HYDRAULICS HAD FAILED. ROTORCRAFT MADE UNEVENTFUL RUNNING LANDING AT AIRPORT AND SHUT DOSDR ERA2001F00001Belt · failedHYDRAULIC PUMP DRIVE BELT FAILED. HYDRAULIC CAUTION LIGHT ILLUMINATED AND HORN ACTIVATED ABOUT ONE MILE FROM LANDING LOCATION. PILOT CONTACTED CONTROL TOWER AND ADVISED HYDRAULICS HAD FAILED. ROTORCRAFT MADE UNEVENTFUL RUNNING LANDING AT AIRPORT AND SHUT DOSDR AWXA0001851Pump · leakingAIR TURNBACK,EN ROUTE FROM LAS TO SNA THE A/C LOST B-HYD SYSTEM QUANTITY AND THE NR 2 ENG DRIVEN HYD PUMP LOW PRESSURE LIGHT ILLUMINATED FOLLOWED BY THE B-SYSTEM ELEC PUMP LOW PRESSURE LIGHT. A/C RETURNED TO LAS MAKING AN UNEVENTFUL LANDING. MX FOUND HYD FLUSDR SWIA972625Pump · failed30 SECONDS AFTER GEAR WAS SELECTED DOWN, NR 2 HYDRAULIC PRESSURE MESSAGE HYDRAULIC LEVEL IN NR 2 INDICATED 0 PERCENT FLUID. AFTER SHUTDOWN LEVEL ROSE TO 15 PERCENT. EDP RUNNING DRY FOR 5 MINUTES. REPLACED RIGHT ENGINE HYDRAULIC PUMP IAW MM 29-11-01. PN ONSDR 0102086303Pump · failedDURING FLIGHT, RECEIVED HYD PRESS SYS 4 AND HYD QTY LOW 4 MESSAGE AND THE HYDRAULIC FLUID QUANTiTY IN THE NR 4 SYSTEM INDICATED ZERO. FOLLOWED COM PROCEDURE AND THE AIRCRAFT CONTINUED TO NRT. DURING APPROACH WHILE ALTERNATE EXTENDING THE LANDING GEAR, THE RISDR CA010703006Pump · misinstalled(CAN) RECEIVED MOTOR P/N 115-380002-5 S/N 1783 FROM TRANSPORT CANADA STICK INSTALLED THE O/H MOTOR ON THE AIRCRAFT AS PER WIRING DIAGRAM IN WESTERN AIRCRAFT MAINTENANCE MANUAL. FOUND THAT THE HYDRAULIC PUMP ROTATION WAS INCORRECT. THE WIRING DIAGRAM WAS REVERSDR 2001F00093Powerpack · malfunctionedDURING NORMAL RUNUP PROCEDURES, THE HYDRAULICS ARE SWITCHED OFF AS PART OF THE SYSTEM CHECK. UPON ACTIVATING THE HYDRAULIC SWITCH ON THE COLLECTOR THE HYDRAULIC LIGHT ILLUMINATES BUT THE CONTROLS STILL HAD HYDRAULIC BOOST SUPPLIED BY THE ACCUMULATOR. THIS SHSDR 2001F00305Pump · failedHYD PUMP HAD SEAL FAILURE. SHAFT SEAL FAILED. (M)SDR ALG2001F00010Filter · corrodedFOUND DURING FIELD MAINTENANCE INSPECTION. RUST FOUND ON FILTER ASSEMBLY BODY.SDR 20010613CW016Pump · deterioratedFLUID SAMPLE TAKEN AT 100 HR INTERVAL SHOW THAT THE PUMP NEEDS TO BE REPLACED. REPLACE PUMP AND BLED SYSTEM WITH SIGHT GAUGE INSTALLED IN RETURN LINE OF HYDRAULIC RIG, TO HELP EVALUATE AIR REMOVAL FROM SYSTEM.SDR DL73K010851Pump · defectiveIN CRUISE FLT 28,000 FEET, SYS-A HYD LOW PRESS LIGHT ON NR 1 ENGINE CAME ON. A-SYS HYD PRESS DROPPED. TURNED OFF THAT SWITCH. 3-5 MINUTES LATER THE OTHER LOW PRESS LIGHT CAME ON. THIS DROPPED SYS-A PRESS FROM 2500 PSI TO ZERO. FOLLOWED LOSS OF SYSTEM-A PROSDR WP012001B2839Screw · corrodedRECEIVED HYDRAULIC PUMP PN 212-076-011-101, SN 253750 FOR OVERHAUL WITH THE FOUR SCREWS HOLDING THE PORT CAP THE HEADS WERE MISSING PN NAS1351-3-32P. THE SCREW SHANK SHOW SIGNS OF HYDROGEN EMBRITTLEMENT AND RUST.SDR WVBA2001035Pump · failedPILOT REPORTED RIGHT HYDRAULIC PUMP FAILED CHECK DURING RUN UP. PUMP WAS REMOVED AND IT WAS DISCOVERED THAT THE SHAFT HAD SHEARED. DURING REMOVAL OF THE FITTINGS IT WAS DISCOVERED THAT THE SMALL PRESSED IN NOZZLE, SPRING AND BALL HAD COME LOOSE WITH THE BALLSDR DLM11010802Pump · failedNR 3 HYDRAULIC, RIGHT EDP FAILED FOR TEMP. REPLACED BOTH NR 3 HYDRAULIC PUMPS. REPLACED SYSTEM FILTERS. SERVICED, BLED AND LEAK CHECKED SYSTEM.SDR S9HA265YPump · failedTOTAL PUMP/HYDRAULIC FAILURE ON GROUND. 2ND OCCURANCE THIS COMPANY LOCATION, BUT NOT THIS AIRCRAFT.SDR C2XA01CL099Powerpack · failedCLE FLIGHT 3130 THE CREW REPORTED THE GEAR WOULD NOT EXTEND IN FLIGHT. THE GEAR HAD TO BE EXTENED MANUALLY. THE CREW ALSO REPORTED THE HYDRAULIC POWERPACK CIRCUIT BREAKER DID POP. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REPLASDR CA010523010Belt · failed(CAN) WHILE IN CRUISE FLIGHT THE PILOT LOST HYDRAULIC PRESSURE. SLOWED THE A/C AND LANDED. HYDRAULIC PUMP BELT BROKEN.SDR CA010531009Shaft · sheared(CAN) DURING CRUISE FLIGHT CREW REPORTED R/H ENGINE HYDRAULIC PRESSURE LOW LIGHT CAME ON WITH ECIAS MESSAGE "R/H ENG EDP". AIRCRAFT DIVERTED AND LANDED. R/H EDP FOUND SHAFT SHEARED, PUMP REPLACED, FILTERS REPLACED AND SYSTEM FLUSHED AS PER AMM 29-11-00 AND 29-SDR HEEA072748Pump · leakingWHILE IN CRUISE FLIGHT, LOST UTILITY HYDRAULIC POWER. RETURNED TO BASE FOR MAINTENANCE.SDR SWAA011203Pump · vibratesAIR TURNBACK, DURING CLIMB OUT DETECTED ABNORMAL ENGINE VIBRATION FROM NR 1 ENGINE, ABOVE 1.7 EPR. R&R NR 1 ENG HYD PUMP & CASE DRAIN FILTER PER MM. OPS & LEAK CHECK GOOD.SDR 01FDEA00292Pump · overtempAFT T/O HYD NR 2 LEFT PUMP OFF FOR HIGH TEMP. SWITCH TO AUTO PUMPS TURNED OFF, TEMP WENT BACK UP AGAIN.SDR CA010504021Bracket · cracked(CAN) UPON INSPECTION THE ENGINEER NOTICED A CRACK ON THE HYDRAULIC PUMP MOUNTING BRACKET. THE CRACK SEEMS TO ORIGINATE FROM TOOL MARKS CAUSED BY MAINTENANCE.SDR SWAA011127Pump · failedAIR TURNBACK, DURING GEAR RETRACTION, NR 1 ENG HYD PUMP FAILED. NO LOSS OF HYD FLUID. R&R NR 1 HYD PUMP & CASE DRAIN FILTER PER MM, OPS CHECK GOOD.SDR ABXA010131Pump · failedTHE LEFT HYDRAULIC QUANTITY WENT TO ZERO IN FLIGHT. THE LEFT ENGINE PRIMARY HYDRAULIC PRESSURE LIGHT ILLUMINATED. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP IAW B767 MM 29-11-05.SDR 20010509CW003Pump · failedAC ON DECENT WHEN AMBER EICAS INDICATION OF HYD VOLUME LOW(A) ILLUMINATED. FLIGHT CREW CONFIRMED THE EICAS INDICATION WAS AN ACTUAL PROBLEM BY VIEWING EICAS WHICH SHOWED, HYD LEVEL AT 16 PERCENT AND DECREASING. PRESSURE DROPING AND FLUID TEMP INCREASING. FLIGHSDR 0101365523Pump · leakingAFTER TAKEOFF, THE NR 2 CENTER HYDRAULIC PUMP PRESSURE LIGHT AND EICAS MESSAGE ILLUMINATED. THIS WAS SHORTLY FOLLOWED BY NR 1 CENTER HYDRAULIC PUMP PRESSURE LIGHT AND EICAS MESSAGE. CENTER HYDRAULIC SYSTEM QUANTITY THEN FELL TO ZERO. FOLLOWED COM PROCEDURESSDR HEEA072387Pump · noisyNOISE COMING FROM HYDRAULIC SYSTEM DURING CRUISE AND ON APPROACHES INTERMITTENT. REPLACED WITH SERVICEABLE PART.SDR SWAA011099Pump · overheatedAIR TURNBACK. A SYSTEM HYD ELECTRIC PUMP OVERHEAT LIGHT ILLUMINATED. REMOVED AND REPLACED A HYD PUMP AND ELECTRICAL CONNECTOR PER MM. OPS CHECK GOOD.
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