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 O842009F00000Bolt · sheared2 BOLTS HOLDING THE BACK PUMP COVER ON, SHEARED AND ALLOWED ALL OF THE FLUID IN THE SYSTEM TO BE PUMPED OVERBOARD CAUSING A LOSS OF THE NR 1 HYD SYS. (K)SDR UALA2009102303314Pump · damagedRIGHT ELECT HYD PUMP WAS RUN WITH RIGHT HYD SYSTEM EMPTY. REPLACED PUMP. ALL OPS NORMAL.SDR UALA2009102103283Pump · leakingCREW RECEIVED HYD QTY LOW R INDICATION. NEED TO REPLACE RT ENG EDP. REPLACED RIGHT EDP. ACCMP'D LEAK CHECK, CHECK OKAY. NEED TO REPLACE SWITCH AND O-RING SWITCH. REPLACED NORMAL BRAKE SOURCE PRESS SWITCH. ALL OPS NORMAL.SDR UALA2009102103279Connector · arcedCTR SYSTEM NR 1 ACMP ELECTRICAL CONNECTOR D482P PINS SHOW SIGNS OF ARCING. INSTALLED NEW CONNECTOR D482P. OPS CHECKS GOOD.SDR SWAA096713Pump · leakingDECLARED EMERGENCY, 45 MINUTES INTO FLIGHT NR 2 EDP "LOW PRESSURE" LIGHT ILLUMINATED. PERFORMED QRH PROCEDURES. ALL HYD PRESSURES AND QUANTITIES NORMAL. FOUND PUMP LEAKING. REMOVED AND REPLACED HYD ENGINE DRIVEN PUMP PER MM.SDR COMA2009101550196Pump · faultyEN ROUTE FROM SAV TO LGA RECEIVED HYD NR 2 LOW PRESS MSG. EMERGENCY DECLARED, A/C DIVERTED TO GSP LANDED SAFELY. REMOVED AND REPLACED NR 2 HYD EDP.SDR HNAA2009101500312Garlock Seal · leakingNR 2 ENGINE PRESSURE FLUX BETWEEN 50-55 PSI, THEN WENT TO 35-40 PSI WITH LOW WARNING LIGHT. ENGINE MANUAL SHUTDOWN. OIL PRESSURE NEVER REACHED O PSI RAN ENGINES AT OR BELOW 40 PSI FOR 2 MINUTES. INSPECTED AND FOUND ENG LOW ON OIL. HYD PUMP GARLOC SEAL LEAKISDR N8UA10102009APump · leakingMX TEST FLIGHT, AFTER REPLACEMENT OF SUSPECT LEAKING RT GEARBOX (THIRD UNIT TO BE INSTALLED IN THE PROBLEM DIAGNOSIS). (2) HOURS OUT, RT ENG GEARBOX LOW OIL PRESSURE WARNING LIGHT. ACFT WAS DIRECTED TO RETURN TO DEPARTURE. PROP WAS FEATHERED AND ENGINE SHUTSDR UALA2009101403230Pump · leakingNR 1 ENG HYD PUMP LEAKING FROM SPLIT FLANGE. REPLACED PUMP, ONE MOUNT NUT AND PRESSURE FITTING. LEAK CHECKED OKAY.SDR QXEA2009101200776Pump · failedON APPROACH LOST NR 2 HYD QUANTITY. ENGINE SHUTDOWN ON GROUND LESS THEN ONE MINUTE AFTER TOTAL FLUID LOSS. FOUND ENG DRIVEN HYD PUMP FAILED AND LEAKING. REPLACED IAW 29-11-01-000-801 AND 29-11-01-400-801. ALSO PERFORMNED CHAP 5 INSP FOR EDP OPERATION WITHOUTSDR HAEA200900211Pump · failedON DESCENT, ACFT HYD PRESSURE GAUGE READ ZERO. LANDING GEAR EXTENDED MANUALLY. ACFT LANDED NORMALLY. MX REPLACED NR1 AND NR2 ENGINE DRIVEN HYD PUMP. OPS CHECK GOOD AFTER MX. [CLOSED]SDR CA091013001Pump · failed(CAN) DURING FLIGHT, HYD PUMP EDP NR 2 FAILED. AFTER NORMAL LANDING PILOT WROTE: NR 2 ENG HYD PUMP U/S NR 2 RUD HYD CAUTION LIGHT ON ON GROUND NWS U/S WITHOUT ANY CAUTION. PERFORMED FLUSHING OF THE NR 2 HYD SYS IAW AMM TASK 29-10-00-617-803 TR 29-108. IN ADDISDR UALA2009092903061Pump · faultyTHE C HYD DEM PUMP EICAS MSG DURING GEAR FLAP RETRACTION. REPLACED ADP PRESSURE SWITCH S28, NO HELP. FOUND CTR DEM PUMP ADP OVERSPEED. REPLACED ADP. NO LEAKS AND OPERATIONAL TEST PASSED.SDR AALA20090927DFW02Pump · failedCREW REPORTED THE RIGHT HYDRAULIC PRESSURE LOW AND THE RUDDER CONTROL MANUAL LIGHT ILLUMINATED IN FLIGHT. CREW RAN THE EMERGENCY GEAR EXTENSION CHECKLIST TO GET THREE GREEN LIGHTS. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE HYDRAULICSDR YENA20090927125Pump · leakingFLT 592 MCO-HPN - NR 2 HYD QTY LOW LIGHT ILLUMINATED DURING CRUISE INITIAL HYD QTY DECREASED FROM 20 PERCENT TO 2 PERCENT OVER A PERIOD OF ABOUT 10 MIN. DIVERTED TO JFK FOR EMERGENCY LANDING. FOUND NR 2 ENGINE HYDRAULIC PUMP LEAKING, REMOVED AND REPLACED ENGSDR 2009FA0000798Shaft · shearedSHAFT SHEARED ON NR1 (L) HYD PUMP WHILE ACFT WAS IN A CLIMB AFTER TAKE OFF. THIS RESULTED IN THE HYD RESERVOIR TO BE EMPTIED OVERBOARD THRU THE PUMP DRAIN. THE PILOT'S THEN GOT A HYD FLOW LOW ANNUNCIATOR, FIRST ON THE RT SIDE AND THEN A FEW SECONDS LATER ON THSDR CA090924009Motor · failed(CAN) ON APPROACH GEAR WAS SELECTED DOWN, HYDRAULIC POWERPACK FAILED. GEAR HAD TO BE MANUALLY EXTENDED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. UPON INSPECTION IT WAS FOUND THAT THE ELECTRIC MOTOR THAT DRIVES THE HYDRAULIC PUMP HAD FAILED DUE TO INTERNAL SHOSDR MASA2009092200296Pump · leakingCAPTAIN REPORTED, LOST ALL NR 3 HYD QTY IN FLIGHT. GEAR WAS EXTENDED MANUALLY AND DECLARED EMERGENCY. MX FOUND HYD FLUID ON BELLY AROUND MAIN GEAR AND WAS TAKEN TO HANGAR TO OPEN UP AND INSPECT FOR CAUSE OF LEAK. REPLACED 3A/3B PUMP AND REPLACED THE ACOUSTISDR AALA20090923DFW01Pump · failedDURING GEAR RETRACTION BOTH SYSTEM A HYDRAULIC LOW PRESSURE LIGHTS ILLUMINATED FOR A SHORT TIME. UPON REACHING CRUISE ENGINE HYDRAULIC A LIGHT ILLUMINATED FOLLOWED BY QUANTITY A DECREASING TO 15 PERCENT AT LANDING. LANDED DFW WITHOUT INCIDENT. REPLACED LEFTSDR UALA2009092303016Pump · malfunctionedTHE C-HYD PRIM 1 EICAS AND C OVERHEAT 1 ILLUMINATED. THE C-HYD 1 PUMP TURNED OFF PER FLT MANUAL. REPLACED C1 HYD PUMP. OPS AND LEAK CHECK NORMAL.SDR HALA2009091800429Pump · leakingETOPS SIGNIFICANT SYSTEM - ON WALKAROUND FOUND NR 1 ENG LEAKING HYD . FLUID. R&R NR 1 ENG HYD PUMP (ED0) PER AMM29-11-05 OPS & LEAK CHECK GOOD.SDR SIMA200926101Pump · malfunctionedON FLIGHT 4224 THE CREW REPORTED THE E1 HYDRAULIC PUMP FAILED. INDICATIONS WERE ALSO A LOSS OF HYDRAULIC SYSTEM 1 FLUID AND A LOSS OF HYDRAULIC SYSTEM 1 PRESSURE. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO GRR. THE AIRCRAFT LANDED SAFELY WITH NO INCIDENSDR UALA2009091602938Pump · leakingLEFT CTR ADP LEAKING HYD FLUID. APPEARS TO BE A CAPPED FITTING ON INBOARD BOTTOM OF PUMP. REMOVED CENTER HYD SYS ADP. CONTINUING ADP INSTALLATION. INSTALLED ADP, OP CHECKS GOOD.SDR CA090917003Hose · worn(CAN) HOSE , MIL-H-6000 CONNECTING WOBBLE PUMP RELIEF VALVE TO ADAPTER FOUND TO BE CHAFED (NOT LEAKING) FROM CONTACT WITH BOTTOM PANEL SUB ASSY CENTER. HOSE WAS REPLACED AND TIED OFF TO PREVENT CONTACT WITH BOTTOM PANEL. (TC# 20090917003)SDR UALA2009091102873Spline · shearedCENTER ADP C2 INOP PRIOR TO DEPARTURE. TESTED TRANSDUCER & FOUND NOT AT FAULT. FOUND C2 HYDRAULIC PUMP SHEARED SPLINE. REPLACED UNIT. OPS CHECK NORMAL.SDR UALA2009091102871Pump · malfunctionedCTR HYD PRESS LIGHT ON, EICAS "C HYD DEM PUMP" MSSG W/ SWITCH IN "ON" POS. AS PER VERBAL WITH ARRIVING CREW. EICAS C-HYD DEM PUMP DURING GEAR AND FLAP RETRACTION. LIGHT EXTINGUISHED AFTER RETRACTION. CHECKED ADP. OPS NORMAL ON GROUND. REMOVED ADP, AND HUSDR FDEA200909103285Plug · leakingWHEN APU WAS STARTED AND APU BLEED TURNED ON, CABIN FILLED WITH SMOKE, TURNED OFF BLEEDS FOUND HYD FLUID RUNNING FROM AFT DRAIN HOLE INTO APU INLET. FOUND REV MOTOR PUMP S/O VALVE M1-165 DRIPPING IN AFT COMPT PN 148995, AIPC 29-12-60-03, FACT 10SEP09 06:58SDR SWAA095827Pump · faultyAIR TURNBACK, A HYDRAULIC ELECTRIC PUMP LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT. REMOVED AND REPLACED A SYSTEM HYDRAULIC PUMP PER MM.SDR SWIA200922506Pump · faultyGEAR DISAGREE WARNING DISPLAYED. (FLT 5958) REPLACED ACMP NR 3B.SDR UALA2009083102733O-Ring · cutHYD QTY DECREASED. QTY STABLE WITH EDP DEPRESSURIZED & ACMP OFF. POS 2 (01=L,02=R). CREW COMMENTS: WITH R PUMPS ON R HYD QTY SYS DECREASED FAST R HYD QTY LT ON. FOUND THE EDP DIFFERENTIAL PRESS INDICATOR LEAKING. FOUND THE O-RINGS WORN/CUT. REPLACED O-RSDR CA090831004Pump · leakingPUMP LEAKING, SERVICABLE PUMP INSTALLED.SDR DXTA2009082403766Pump · leakingHYD PERCENT QTY DECREASED TO 16 PERCENT ON "A" SIDE AT FL410; FLUID LEAKING FROM LT ENGINE. OPERATED "A" SIDE HYDS & INSPECTED ACFT FOR LEAKS. NOTED ONLY FLUID DRAINING OVERBOARD IS FROM LT ENG HYD PUMP CASE DRAIN. THIS IS AN INDICATION OF FLUID PASSING THRSDR UALA2009082502632Pump · failedEICAS MESSAGE RE C2 ELEC HYD PUMP TEMP INDICATION INOP. C2 PUMP SPRANG A LEAK AT GATE. REPLACED PUMP AND CHECKED OKAY.SDR WRLA20090819198Pump · leakingDURING CLIMBOUT, NR 3 ENGINE LT EDP INDICATED OVERTEMP. ONE HOUR AFTER DEPARTURE, NR 3 ENGINE RT EDP INDICATED OVERTEMP. ONE HOUR FIFTEEN MINUTES AFTER DEPARTURE NR 3 HYDRAULIC SYSTEM INDICATED 0 HYDRAULIC FLUID QUANTITY. DIVERTED TO LEJ (EDDP) FOR MAINTENASDR AALA20090818DFW01Pump · failedDFW - CREW REPORTED RIGHT ENGINE DRIVEN HYDRAULIC PUMP FAILED. RETURNED TO DFW WITHOUT INCIDENT. FOUND RIGHT ENGINE DRIVEN HYDRAULIC PUMP SHAFT SHEARED. REMOVED AND REPLACED RIGHT ENGINE DRIVEN HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR AALA20090810LAX01Pressure Switch · failedLAX - SHORTLY AFTER TAKEOFF DURING FLAP RETRACTION A VIBRATION AND RUMBLE SOUND STARTED FOLLOWED BY RIGHT ENGINE HYDRAULIC PUMP EICAS MESSSAGE AND PRESS LIGHT ON. RETURNED LAX WITHOUT INCIDENT. REPLACED ENGINE PUMP PRESS SWITCH S10541. ALSO PERFORMED AIRFRASDR HALA2009080800355Pump · leakingETOPS SIGNIFICANT SYS - RAMP REPORTED NR 1 ENG FLUID LEAK. FOUND NR 1 ENG DRIVEN HYD PUMP LEAKING. REPLACED NR 1 ENG DRIVEN PUMP IAW AMM 29-11-05-004-006. GROUND RUN UP AND LEAK CHECK OK. OK FOR SERVICE.SDR CA090901006Pump · inoperativeCREW REPORTED THEY HAD TAXIED OUT FOR TAKEOFF AND JUST PRIOR TO APPLYING TAKEOFF PWR AMBER CAS (L GEN FAIL) POSTED AND LT GENERATOR DROPPED OFF LINE. A FEW SECONDS LATER AMBER CAS (APU GEN FAIL) POSTED. CREW TAXIED BACK OFF THE RUNWAY. DURING TAXI, CREW NOTSDR UALA2009080602372Pump · leakingLEFT ENGINE HYDRAULIC PUMP LEAKING COPIOUS AMOUNTS OF FLUID ON GROUND. REPLACED LEFT ENGINE HYDRAULIC PUMP. NO LEAKS DETECTED. OP CKS OKAY.SDR DXTA2009073003748Pump · leakingLOST HYD B SYS QUANITY IN FLIGHT RAN CHECKLIST AND UNLOADED THE B PUMP. FOUND THAT RT ENG HYD PUMP FAILED. REMOVED HYD PUMP AND INSTALLED REPAIRED UNIT (REF WO 29760 1.15) PRIMED PUMP, BLED HYD SYS B, RAN ENGINES, AND FOUND NO LEAKS AT THIS TIME AND HYD SYS BSDR UALA2009072302177Pump · failedTHE C ADP INOP IN AUTO OR MAN MODE. CREW COMMENTS: AFTER PUSHBACK & AFTER FLAP ACTIVATION GOT EICAS C HYD DEM PUMP. SWITCH TO ON-NO CHANGE. AREA AROUND ADP REQUIRES CLEAN-UP. APPEARS THAT PAINT HAS DEGRADED DUE TO HYD LEAK. REQUIRES CLEAN-UP. REPLACED CSDR 3LYA090722Pump · leakingNUMBER 1 HYD CAUTION LT ILLUMINATED, THEN NUMBER 1 HYD ISO VALVE ILLUMINATED. FOLLOWED QRH SELECTED STANDBY POWER UNIT. NOTICED OF FLUID QUANTITY. CREW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NUMBER 1 ENGINE DRIVEN PUMP. OPS TSDR AALA20090721DFW01Pump · failedDFW - ON DESCENT PASSING ABOUT FL310 RUDDER CONTROL MANUAL LIGHT ILLUMINATED FOLLOWED BY RIGHT HYDRAULIC PRESS LOW LIGHT. RIGHT HYDRAULIC PRESSURE INDICATED 500 PSI, FOLLOWED CHECKLIST RIGHT PRESS REMAINED AT 500 PSI, LEFT PRESS WAS NORMAL. AT APPROX 10,000 SDR MASA2009072100218Pump · malfunctionedFLT 7092 MTJ-DEN - CREW REPORTED DURING APPROACH INTO DEN, THE AIRCRAFT LOST ALL NR 2 HYD SYSTEM PRESSURE AND QUANTITY. CREW ELECTED TO DECLARE AN EMERGENCY LANDING. AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MX REPLACED NR 2 EDSDR 2009FA0000635Shaft · failedDURING CRUSE BOTH HYD LOW-PRESSURE LIGHTS ILLUMINATED. CREW COMPLETED ABNORMAL CHECKLIST FOR CONDITION. CREW DIVERTED FROM ORIGINAL DESTINATION (PWK) TO AIRPORT WITH LONGER RUNWAY (RFD) AS PRECAUTIONARY MEASURE. CREW DECLARED EMERGENCY AS A PRECAUTIONARY MESDR DXTA2009071303726Pump · malfunctionedDURING DESCENT, "HYD VOL LOW B" CAS ILLUMINATED IN FLIGHT. ACCOMPLISHED CHECKLIST AND LANDED WITHOUT INCIDENT. VOLUME QTY INDICATED 10 PERCENT AT FIRST THEN DROPPED TO 0 PERCENT ON LANDING. REPLACED NR 2 HYDRAULIC PUMP OPS CK GOOD IAW MM 29-10-02.SDR AALA20090709DFW01Module · leakingDFW - AIRCRAFT RETURNED TO DFW DUE TO LOSS OF CENTER HYDRAULIC SYSTEM. AIRCRAFT REMOVED FROM SERVICE. REPLACED ENGINE DRIVEN PUMP MODULE IN LEFT WHEEL WELL. SYSTEM GROUND CHECK NORMAL OPERATION.SDR AALA20090709DFW02Pump · inoperativeDFW - CENTER HYDRAULIC SYSTEM WARNING WITH CENTER HYDRAULIC LOSS. RETURNED TO DFW LANDED WITHOUT INCIDENT. AIRCRAFT WAS TOWED TO GATE. AIRCRAFT REMOVED FROM SERVICE. REPLACED CENTER AIR DRIVEN HYDRAULIC PUMP, CASE, PRESSURE FILTERS, AND TEMPERATURE SWITCH.SDR FDEA200907062498Shaft · failedHYD 2 QTY LOW LVL 2 ALERT FOLLOWED BY HYD 2 OFF LVL 2 HYD QTY WENT TO 0. LANDED LAX WITHOUT INCIDENT. INSPECTED HYD FILTERS ON ENGINE FOUND AFT PUMP CASE DRAIN FILTER HAD LARGE QUANTITY OF METAL DEBRIS & DELTA P INDICATOR POPPED. FOUND SHAFT SHEARED ON AFT HSDR AALA20090702MIA01Pump · inoperativeMIA - INFLIGHT PAP-FLL. SYSTEM A HYDRAULIC ENGINE LOW PRESS LIGHT ILLUMINATED. EMERGENCY DECLARED, LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NUMBER ONE ENGINE HYDRAULIC PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.
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