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 VNAA2010022200007Pump · failedCREW REPORTED HYD 2 LO PRESS MSG FOLLOWED BY RAPID LOSS OF SYSTEM 2 HYDRAULIC FLUID. AIRCRAFT DIVERTED TO ATL LANDING WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT USING AIRCRAFT MAINTENANCE MANUAL AND REMOVED AND REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP. SDR IXXA100016OPump · crackedDURING CRUISE, THE AILERON AND RUDDER REVERSION LIGHT CAME ON, THE CREW ALSO NOTICED LOSS OF HYD PRESSURE AND QUANTITY. CREW ACCOMPLISHED PROCEDURES IAW QRH NR 27. DECLARED EMERGENCY LANDING WITHOUT FURTHER INCIDENT. MX FOUND CABIN AIR CHECK VALVE CLOGGED ANSDR MASA2010021500139Pump · failedRTF DUE TO GEAR DISAGREE ON RETRACTION. MX T/S TO FAILED 3A HYD PUMP. MX REPLACED THE PUMP AND PERFORMED GEAR SWINGS.SDR UALA2010021500585Pump · failedNR 2 ENG HYD PUMP HAS FAILED. INSTALLED NEW HYD PUMP AND REPLACED CASE DRAIN AND PRESS FILTERS. HYD LINES STILL NEED TO BE FLUSHED AND CONNECTED TO HYD PUMP. FLUSHED AND CONNECTED LINES. LEAK CK OF PUMP AND FILTERS WAS GOOD.SDR AALA20100211JFK01Pump · leakingJFK - CREW REPORTED RIGHT HYDRAULIC SYSTEM FAILURE. EMERGENCY DECLARED RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE DRIVEN PUMP THAT WAS LEAKING. SYSTEM GROUND CHECK NORMAL OPERATION.SDR UALA2010020900508Pump · faultyRT ELEC HYD DEMAND PUMP INOPERATIVE. SWAPPED RT ELEC PUMP AND CTR ELEC PUMP NR C2 IAW MM AND NOW RT ELEC PUMP TESTS NORMAL. DF ITEM CREATED FOR C2 ELEC PUMP. PUMP STOPPED WORKING AND REPLACED ELCU M29203 AND OPS NORMAL. DF ITEM CREATED FOR C2 ELEC PUMP. PUSDR FDEA201002050334Pump · failedLOST YELLOW HYD SYS QUANTITY AT CRUISE C/W ECAM AND C/W QRH. EDP RUPTURED. PER MM 29-00-00-3, INSPECTED CLOGGING INDICATORS OF CASE DRAIN, DELIVERY AND RETURN FILTERS. NONE OUT. VISUALLY INSPECTED CASE DRAIN FILTER, NO CONTAMINATION OR DECOMPOSED FLUIDSDR HEEA127272Pump · failedNR 3 HYD SYS FAILED. PERFORMED EMERGENCY PROCEDURES AND RETURNED TO BASE. MX FOUND THE SPLINE ADAPTER PN 92351-15284-101 HAD BACKED OFF THE DRIVE SHAFT IN THE TRANSMISSION. HYD PUMP INSTALLED HAD THE OLD STYLE SHAFT WHICH WOULD ALLOW THE SPLINE ADAPTER TO SSDR UALA2010020100407Pump · overheatedRT EDP HYD PUMP 'OVHT' LIGHT ILLUMINATED WITH ASSOCIATED STATUS MSG. DISPLAY ELEC- HYD PG AND NOTICED A STEADY RISE IN RT HYD TEMP. REPLACED EDP AND REPLACED PRESSURE FILTER. PERFORMED LEAK CHECK ALL OK. RAN ENG AND ALL INDICATIONS GOOD.SDR DGCA10501Pump · failedHYDRAULIC PUMP FAILURE.SDR 2010FA0000075Motor · burned outAUX PUMP LIGHT ILLUMINATED AFTER PICK UP. PUMP MOTOR DEFECTIVE, WILL NOT TURN WHEN POWER APPLIED.SDR CA100219004Pump · failed(CAN) CREW REPORT: DURING THE CLIMB THE NR 1 HYD PUMP CAUTION LIGHT ILLUMINATED. QRH PROCEDURES WERE FOLLOWED RESTORING ALL HYD SYSTEMS. A RETURN TO BASE WAS COMPLETED. MX REPORT: NR1 ENGINE EDP REPLACED IAW AMM 29-11-01. MAIN SYS 1 PRESSURE FILTER REPLACED.SDR CA100127003Shaft · broken(CAN) GROUND TEST AFTER FLIGHT, LANDING GEAR HANDLE DIDN`T RETURN TO NEUTRAL AFTER TEST. PUMP REMOVED AND FOUND DRIVING SHAFT BROKEN, PUMP REPLACED & CHECK OK. THIS KIND OF EVENTS HAPPEN FOR THE SECOND TIME FROM THE SAME SUPPLIER.SDR UALA2010012100258Pump · failedYELLOW SYS HYD LOSS, RTFL. REPLACED HP FILTER ELEMENT. NO EVIDENCE OF DEBRIS. TROUBLESHOT OVERHEAT PROBLEM AND FOUND BAD CHECK VALVE 3083G. REMOVED DEFECTIVE CHECK VALVE. REPLACED AND PERFORMED HIGH POWER RUN FOR 25 MINS. REPLACED TEMP TRANSMITTER 3381GRSDR CALA2010090900424Pump · leakingB-SYSTEM HYD LOW PRESSURE ENGINE LIGHT CAME ON. HYD FLUID DECREASED FROM 105 TO 0 PERCENT. REPLACED EDP REF MM 29-11-400. OPS CHECK AND LEAKS CHECK GOOD. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1384130 S/N OFF 05888 PUMP, HYD ENG D OFF 29-2910-9-0003 5SDR CALA2010012500018Pump · leakingB-SYSTEM HYD LOW PRESSURE ENGINE LIGHT CAME ON. HYD FLUID DECREASED FROM 105 PERCENT TO 0 PERCENT. REPLACED EDP REF MM 29-11-400. OPS CHECK AND LEAKS CHECK GOOD. ROTABLE PARTS CHANGE WAS INDICATED - TT 1384130, S/N OFF 05888 PUMP, HYD ENG D OFF 29-2910-9-0SDR HALA2010011300019Pump · leakingETOPS SIGNIFICANT SYSTEM - ON WALK AROUND FOUND NR 1 ENG HYDRAULIC PUMP LEAKING. REMOVED AND REPLACED HYDRAULIC PUMP AT NR 1 ENG PER AMM 29-11-5. LEAK CHECK AND SECURITY CHECK OK.SDR MALA100006Pump · failedAFTER TAKE OFF, THE HYD PUMP FAILED TO PRESSURIZE. LANDING GEAR DID NOT FULLY RETRACT. REPLACED RELAY 7ML.SDR UALA2010010400052Pump · leakingG HYD SYS LOSS. ACCOMPLISHED FREEFALL EXTENSION. NR 1 ENG EDP WAS TURNED OFF APPROX 1 MINUTE AFTER SYS PRESSURE WENT TO 0-PSI. LEAKING LINE IDENTIFIED IN PYLON. REPLACED GREEN SYS EDP. REPLACED EDP FILTER AND GREEN SYS CASE DRAIN FILTER REPLACED PRESS LINSDR YENA20100102002Pump · leakingFLT JB919 JFK-ORD DECLARED AN EMERGENCY DUE TO HYDRAULIC SYSTEM 1 QUANTITY WAS LOW 0 PERCENT IN FLIGHT, NO LOW PRESSURE. A/C LANDED UNEVENTFULLY AND TAXIED TO THE GATE ON ITS OWN POWER. AT ORD MX SERVICED HYDRAULIC SYSTEM NR 1 IAW AMM 12-12-01 AND PERFORMED SDR CA091229003Pressure Switch · defective(CAN) IN CRUISE, EICAS MESSAGE ANNUNCIATION "LT ENG HYD PUMP". IN-FLIGHT TURNBACK INITIATED TO YYZ FOR COMPANY CONVENIENCE. THE LEFT ENGINE HYDRAULIC PUMP PRESSURE SWITCH WAS FOUND DEFECTIVE. (TC NR 20091229003)SDR CA091223012Key · broken(CAN) GROUND TEST AFTER FLY, LANDING GEAR HANDLE DIDN’T RETURN TO NEUTRAL AFTER TEST. MAINTENANCE ACTION, HYDRAULIC LEVEL CHECK OK, HYDRAULIC PUMP REMOVED AND FOUND DRIVING SHAFT KEY BROKEN. PUMP REPLACED AND CHECK OK (TC NR 20091223012)SDR YENA20091220176Pump · failedFLT 1244 CLT-BOS DURING CRUISE AT FL350 PILOT DECLARED EMERGENCY DUE TO EICAS MESSAGE "HYD 2 EDP FAIL" LOSE OF NR 2 HYDRAULIC SYSTEM. RETURNED BACK TO CLT AND LANDED AIRCRAFT UNEVENTFULLY AND TAXIED TO THE GATE. MX REMOVED AND REPLACED ENGINE DRIVEN HYD PUMPSDR 2009FA0001044Pump · leakingDISCOVERED A LARGE AMOUNT OF HYDRAULIC FLUID HAD LEAKED FROM THE RT ENG. FURTHER INVESTIGATION SHOWED A LEAK COMING FROM THE RT HYD PUMP CASE DRAIN INDICATING THAT THE HYD PUMP HAD INTERNALLY FAILED. REMOVED AND REPLACED HYD PUMP, PN 4018301, SN AL212AB IAW SDR ASOA200901410Pump · failedHYD SYS (2) VOLUME DROPPED TO 5 PERCENT EDP 2 AND PUMP 2B BOTH GAVE CAUTION MESSAGES. PRESSURE STAYED AT 2800 UNTIL FINAL APPROACH. TT FOR EDP PUMP WAS AT 55 MINUTES, TT FOR PUMP 2A WAS AT 20 MINUTES. SYS 2 VOLUME DROPPED TO 0 PERCENT ON FINAL (10 MIN) EMERGSDR DL76L091970Pump · failedRTB DUE TO ADP FAILED ON TAXI OUT, FWD TO MCO IAW MEL 29-11-03. R & R CTR ADP IAW MM. R & R M1057 OVERSPEED CARD IN P50 CARD FI ALL OPS NML. MCO PLAC RMVD. ETOPS CATEGORY 'E': PROBLEMS WITH SYS CRITICAL TO ETOPS.SDR DL76L091936Pump · failedRTB DUE TO C1 DEMAND PUMP EICAS MSG. CHECKED ON GROUND-OK. AT REQUEST OF MCC PERFORMED SWAP BETWEEN CENTRAL HYD PUMP 1 AND 2 FOR TROUBLE SHOOTING AND CONVENNCE AS AMM 29-11-02-004-001 AND AMM 29-11-02-404-018. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICSDR IPXA09557966Pump · malfunctionedINSPECTION TYPE:N/A DURING APPROACH THE NR 2 CENTER ELECTRIC HYDRAULIC PUMP LOW PRESSURE LIGHT CAME ON. THE PUMP WAS NOT PRODUCING ANY PRESSURE. MAINTENANCE FOUND THE NR 2 ELECTRIC HYDRAULIC PUMP HAD OVERHEATED AND THERE WAS A STRONG BURNED ELECTRICAL SMELL SDR CA091209010Shaft · sheared(CAN) DURING CRUISE NR 1 ENG HYD PUMP CAUTION LIGHT ILLUMINATED AND PRESSURE DROPPED TO ZERO. STANDBY HYD PUMP SELECTED ON AND PRESSURE RETURNED, CONTINUED TO DESTINATION. NR 1 ENG HYD PUMP REPLACED DUE TO SHEARED SHAFT.SDR CA091130005Pump · malfunctioned(CAN) NR 1 STBY HYD PUMP NOT COMING ON LINE. (RESOLVED ON W/O: 216586 TASKCARD: NR-00001) FOUND BURNT WIRES ON THE UPPER AFT CORNER OF NR 2 AC CONTACTOR BOX, (CB POPPED AS WELL) WIRES ON TOP OF BOX HAVE ARCED AND BURNED A HOLE IN THE AC CONTACTOR BOX AS WELL SDR UALA2009112503662Pump · leakingLEFT HYD QTY SLOWLY DECREASING NOW AT .32. FOUND HYD LEAK COMING FROM LEFT ENG DRIVEN PUMP BODY. PUMP REPLACED. LEAK CHECK PERFORMED OKAY. LEFT HYD SYS FILLED UP. ALL OPS NORMAL.SDR HALA2009112400545Pump · leakingHYD R QTY 2 ALERT ILLUMINATED. FOLLOWED CHECKLIST PROCEDURES. OBSERVED HYD QUANTITY AT 1.0 PERFORMED MANUAL GEAR EXTENTION. RE-STOWED ALT GEAR EXTENSION LEVER, GEAR DOORS RETRACTED. SERVICED RT HYD SYS FOUND AUX PUMP LEAKING. REMOVED AND REPLACED AUX HYD SDR C2XA09IA292Pump · failedIAH - FLIGHT 2989, DURING CRUISE FLIGHT THE CREW REPORTED LOSING THE NUMBER TWO HYDRAULIC SYSTEM. THE CREW DECLARED AN EMERGENCY, AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE NUMBER TWO ENGINE DRIVEN HYSDR HALA2009112300543Pump · inoperativeRT HYD SYS PRESS EICAS ALONG WITH RT ENG PRESS LIGHT ON AT SWITCH. PRESS IS 0 WITH DEMAND PUMP OFF. REPLACED NR2 ENG HYD PUMP IAW AMM 29-11-05. CONDITION SAME. RESET NR2 ENG. FIRE HANDLE, OPS CK GOOD.SDR UALA2009112303645Pump · leakingNR 2 ENG DRIVEN HYD PUMP LEAKING 20 DPM AT A PUMP SEAM. REPLACED NR 2 ENG DRIVEN HYD PUMP. NO LEAKS NOTED.SDR 2010F00109Pump · making metalDPI FOUND EXTENDED DURING INITIAL 100 HOUR INSPECTION. REMOVED FILTER AND FOUND METAL IN FILTER AND FILTER HOUSING. REPLACE RT HYDRAULIC ENGINE DRIVEN PUMP.SDR J7SA60247111709Pump · cavitatesBOTH AMBER HYD QTY LOW CAS MESSAGES ILLUMINATED DURING CRUISE. CREW DECLARED AN IFE AND MADE A SUCCESSFUL, UNSCHEDULED LANDING. MX FOUND A 'B' NUT HAD BACKED OFF ON THE PRESSURE LINE BETWEEN THE LT PRESSURE TRANSDUCER AND A CHECK VALVE LOCATED IN THE AFT BAGGSDR QXEA2009112000970Pump · failedBLI- ON FINAL NR 1 HYD PUMP CAUTION LIGHT WITH OTHER ASSOCIATED LIGHTS CAME ON. SELECTED STANDBY THROUGH NORMAL CHECKLIST, THEN LOST ALL HYD QUANTITY ON NR 1 SYS. LANDED WITH NO FLUIDS, ENOUGH PRESSURE TO PARK, THEN LOST BRAKES AT PARKING. PERFORMED INSP OFSDR CA091202009Pump · leaking(CAN) PUMP FOUND LEAKING ON SUCTION SIDE, REPLACED WITH A SERVICABLE PUMP (TC NR 20091202009)SDR UALA2009111003515Pump · inoperativeRIGHT EDP EICAS MSG. OVERHEAT LIGHT CAME ON WITH LOW PRESS, CREW TURNED THE PUMP OFF AND OVERHEAT LIGHT WENT OUT, PUMP LOW PRESS LIGHT ON. REPLACED NR 2 ENG EDP. OP CHECKS NORMAL.SDR UALA2009110903469Pump · leakingEDP HYD OVHT LIGHT ILLUMINATED EICAS MSG (L,R) PRIM HYD OVHT DISPLAYED. PUMP WAS DEACTIVATED. POS 2 (01=L,02=R). CREW COMMENTS: R PRIM HYD PUMP OVHT SHUT OFF PUMP OVHT CAUTION EXTINGUISHED AFTER 12MIN 20SEC. SUPPLEMENTAL DATA UPDATE, FOUND NR 2 ENGINE (EDPSDR PNSA091101Pump · malfunctionedDURING THE ARRIVAL INTO ANC THE HYDRAULIC WARNING LIGHT ILLUMINATED, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT.SDR IPXA99557903Pump · inoperativeATB - RIGHT HYD PUMP LIGHT ILLUMINATED WITH EICAS MESSAGE. REMOVED AND REPLACED RIGHT HYD EDP IAW AMM 29-11-05-4. NO LEAKS NOTED. OPS NORMAL.SDR CA091119002Pump · failed(CAN) SHORTLY AFTER TAKEOFF (5 MIN) CLIMBING THROUGH FL080 AN (AMBER) R HYD TEMP HIGH CAS POSTED. CREW ELECTED HYD SYNOPTIC PAGE AND THE RT HYD TEMP DISPLAYED WAS 115C AND RAPIDLY CLIMBING. CREW BEGAN TO PERFORM QRH PROCEDURES AND WITHIN ONE MINUTE RT HYD TEMPSDR C2XA09IA277Pump · leakingIAH - FLIGHT 2363 THE CREW REPORTED THAT THE NUMBER ONE HYDRAULIC SYSTEM FAILED ON TAXI. THE AIRCRAFT WAS SHUTDOWN AND TOWED TO THE GATE WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE DRIVEN HYDRAULIC PUMP, SERVICED HYDRAULICS, OPERATIONALLY / LSDR HALA2009102800492Pump · warning lightETOPS SIGNIFICANT SYS - C HYD DEM PUMP EICAS MESSAGE AND OVHD PRESS ILLUMINATED WHEN FLAPS WERE EXTENED. OPS CHECK C HYD DEM PUMP IAW DAL AMM 29-11-00. OPS CHECK NML. MOVED FLAPS AND CONTROL SURFACES. CK GOOD. OK FOR SERVICE.SDR CA091104002Seal · damaged(CAN) ON GEAR EXTENSION AN AMBER PTU FAIL CAS MESSAGE POSTED FOLLOWED BY THE LT HYD ENG PUMP FAIL CYAN CAS MESSAGE FOLLOWED BY HYD LOW CAS AND A 0 QUANTITY READING. PILOT SAID THE GEAR DID NOT EXTEND AND HE HAD TO PERFORM EMER EXTENSION, THE FLAPS WENT TO 10 DSDR J7SA20036102609Pump · failedUPON GEAR EXTENSION, GOT A "GEAR PTU FAIL" CYAN FOLLOWED BY "L ENG HYD PUMP FAIL" AMBER AND LT HYD QUANTITY READS ZERO. EMERGENCY GEAR EXTENSION PROCEDURE WAS USED TO LOWER AND LOCK GEAR. LANDING AND TAXI UNEVENTFUL. T/S HYDRAULICS, FOUND SEALS ON LT EDP QDSDR ASMF200910005Pump · leakingDURING FLIGHT, THE ENG 2 LOW PRESSURE LIGHT TURNED ON WITH CODE 293 210 52. MX DETECTED A HYD LEAK ON RT HYD PUMP, SO HYD PUMP WAS REPLACED IAW MM 29-11-11, TESTED CORRECT.SDR ASMF200910004Carbon Seal · leakingDURING OVERNIGHT CHECK, A FUEL AND OIL LEAKS WERE DETECTED ON HPTACC VALVE DRAIN AND ON HYD PUMP DRAIN. MX REPLACED THE FUEL PUMP AND THE HYD PUMP CARBON SEAL IAW MM 75-21-01 AND 72-60-00, TESTED CORRECT.
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