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 CA150729008Pump · failed(CAN) HYD 1 FLUID HOT CAUTION ILLUMINATED. DEFECT ACTION LEAK ON ENGINE DRIVEN HYDRAULIC PUMP ENG 1 FOUND. HYDRAULIC QUANTITY AFTER LANDING 10%. ENG 1 HYDRAULIC PUMP REPLACED IAW AMM 29-11-01-000/400-801 2. FLUSHING OF HYDRAULIC SYSTEM NR1 PERFORMED IAW AMM 29SDR R61A201504280470Pump · inoperativeCREW RECEIVED A HYD LOW QTY 1 MESSAGE. CREW DID NOT DECLARE AN EMERGENCY AND DIVERTED, WHERE CREW LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R ENGINE DRIVEN PUMP IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.SDR CA150730007Pump · malfunctioned(CAN) CREW FOLLOWED CHECKLIST AND SELECTED CLOSED THE LT HYD SHUTOFF VALVE AND PUMP SWITCH TO OFF. ON APPROACH THE CYAN ICAS, LT ENGINE FAULT, POSTED ALSO. CREW DECLARED AN EMERGENCY AND LANDED ON THE RUNWAY AND HAD TO BE TOWED OFF RUNWAY. AFTER LANDING DEBSDR J7SA20150724001Pump · leakingWHILE IN CRUISE, DIVERTED DUE TO AMBER LT HYD PRESSURE LOW WARNING. DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. R & R THE LT EDP, THE CASE DRAIN & PRESSURE FILTERS & ALL THREE COUPLING HALVES MM 29-12-01, -15, -19, -23. OPERATIONS & LEAK CHECSDR CA150727016Powerpack · faulty(CAN) ON TAKEOFF WHEN THE LANDING GEAR WAS RETRACTED THE LANDING GEAR HYDRAULIC POWER PACK CONTINUED TO RUN EVERY 10 SECONDS. WHEN GEAR DOWN WAS SELECTED THE FREQUENCY OF RUN ON INCREASED. THE PILOT LANDED WITHOUT FURTHER INCIDENT AND RETURNED TO BASE FOR MASDR DATA2015072101Pump · leakingON DESCENT HYD RT CWP LIGHT ILLUMINATED. HYD PANEL SHOWED RESERVOIR CONTENTS, UPPER RED. LT & RT FLUID TEMP 70 DEG, MAIN SYS 3000 PSI. SHORTLY THEREAFTER BOTH HYD LT & HYD RT CWP WARNING LIGHTS ILLUMINATE. HYD PANEL SHOWED RESERVOIR CONTENTS LOWER RED. FLSDR CALA2015071700579Pump · failedDURING CLIMB FROM FL360 TO FL380, LT HYD QTY WENT FROM FULL TO ZERO WITHIN A SECOND. COMPLETED QRH CHECKLIST. ON ARRIVAL, FLEW APP & LOST PTU, NORMAL LANDING. R & R NR 1 EDP HYD & HOSE PN AE709566-1 IAW MM 29-11-05. OPERATIONS & LEAK CHECKED GOOD.SDR CA150715001Pump · failed(CAN) AFTER DEPARTURE GREEN HYD SYS FAILED. RETURNED FOR MX. PAN PAN DECLARED WITH ATC. CRASH FIRE RESCUE ON STANDBY FOR ARRIVAL. TOWED TO GATE. AFTER ARRIVAL RESOLUTION CHAFED HYD LINE REPLACED AS PP 320-54-57635. CASE DRAIN, LP & HP HYD FILTERS & EDP RSDR REXA2015071400713Pump · faultyAT CRUISE ALTITUDE JUST PRIOR TO TOD HYD 3 LO PRESS CAUTION MSG DISPLAYED. ASSOCIATED INBD GND SPLRS MSG DISPLAYED. RAN POM PROCEDURE, UNABLE TO ESTABLISH SYS 3 PRESS. PERFORMED ALTERNATE LG EXTENSION. REF PILOT WRITE UP AML PG 3197921-1 3A CB POPPED IN FLSDR AALA201507169010Pump · faultyFLIGHT 743 EN-ROUTE, WHILE IN CRUISE, CREW RECEIVED ECAM HYD G RSVR LO LVL MSG. THE CREW SHUTDOWN BOTH GREEN SYS HYD PUMPS, BUT CONTINUED ON. AN EMER WAS DECLARED, & THE FLIGHT LANDED WITHOUT AUTO BRAKES, NORMAL BRAKES & NOSE WHEEL STEERING. THE ACFT WAS TOSDR AALA201507169009Pump · faultyFLIGHT 743 EN-ROUTE, WHILE IN CRUISE, CREW RECEIVED ECAM HYD G RSVR LO LVL MSG. THE CREW SHUTDOWN BOTH GREEN SYS HYD PUMPS, BUT CONTINUED ON. EMER WAS DECLARED & THE FLIGHT LANDED WITHOUT AUTO BRAKES, NORMAL BRAKES & NOSE WHEEL STEERING. THE ACFT WAS TOWED SDR AALA201507169001Pump · defectiveFLIGHT 743 EN-ROUTE, WHILE IN CRUISE, CREW RECEIVED ECAM HYD G RSVR LO LVL MSG. THE CREW SHUTDOWN BOTH GREEN SYS HYD PUMPS, BUT CONTINUED ON. AN EMER WAS DECLARED, & THE FLIGHT LANDED WITHOUT AUTO BRAKES, NORMAL BRAKES & NOSE WHEEL STEERING. THE ACFT WAS TOSDR CA150710004Powerpack · malfunctioned(CAN) ON APPROACH THE CREW SELECTED LANDING GEAR TO THE DOWN POSITION AND THE CB POPPED AND GEAR DID NOT EXTEND. CB WAS RESET AND THE CB POPPED AGAIN. CREW DECIDED TO RETURN TO MAINTENANCE BASE. ON APPROACH THE GEAR WAS MANUALLY LOWERED AS PER CHECKLIST AND THSDR CA150713001Pump · failed(CAN) AT 18,000 NR 1 ENG HYD PUMP CAUTION LIGHT ILLUMINATED. COMPLETED THE REQUIRED CHECKLIST, THE NR 1 HYD ISO VLV CAUTION LIGHT ILLUMINATED ALONG WITH INBD ROLL SPLR & NR 1 RUD HYD & NO FLUID IN THE NR 1 HYD SYS. RAN THE NR 1 HYD SYS FAILURE CHECKLIST. UPOSDR CA150708013Pump · seized(CAN) DURING PREFLIGHT INSPECTION, MAIN ROTOR COULD NOT BE MANUALLY ROTATED IN THE DIRECTION OF ROTATION. UTILITY HYDRAULIC PUMP WAS FOUND TO BE SEIZED. AFTER PUMP REPLACEMENT, ROTOR TURNS NORMALLY.SDR CA150708001Pump · failed(CAN) FLIGHT CREW REPORT NR 1 HYD FLUID HOT CAUTION LIGHT ILLUMINATED, THEN PRESSURE DROPS FROM 3000 TO 2000, QUANTITY NOT CHANGED [AROUND 90%] THEN THEY HAVE TRIED TO PRESSURIZE NR 1 HYD SYS BY STANDBY PUMP BUT IN THE MOMENT THAT PRESSURE STARTED RISING QUANTSDR CA150706004Pump · leaking(CAN) YELLOW HYD SYSTEM LOSS. PAN PAN DECLARED WITH ATC TO ALLOW FOR MORE SPACING DUE TO THE SLOW MOVEMENT OF FLAPS. RESOLUTION YELLOW HYD SERVICED WITH 8L, FOUND HYD LEAK ON 32 ENG PYLON ABOVE FAN CASE BEHIND PANEL 423AL. CBS AB3 AND AB6 PULLED FOR YELLOW ELSDR SWAA2015070741463Pump · low pressureDECLARED EMER. DURING FLAP RETRACTION LOW PRESS ILLUMINATED ON NR 2 ENG B HYD PUMP. R & R NR 2 ENG HYD PUMP IAW AMM.SDR CA150710019Rod · fractured(CAN) QTY 2 THREADED RODS IN THE OTBD SHOCK MOUNTS OF AC MOTOR PUMP WERE FOUND FRACTURED. AN INITIAL MFG MATERIAL ANALYSIS INDICATES THE RODS HAVE FAILED DUE TO HYDROGEN EMBRITTLEMENT. THE CONDITION IS STILL UNDER HYDRAULIC SYSTEMS DIVISION INVESTIGATION. ASDR SIMA20150701004Pump · malfunctionedHYD 1 PUMP FAIL & HYD 1 LOW QTY IN FLIGHT. ELEC PUMP HELD AT 2900 PSI REMAINDER OF FLIGHT. UPON LANDING ELEC PUMP WENT TO 100 PSI & LOST STEERING. TRANSFERRED TO NRWC 694-ORD-02076. FROM NRWC 694-ORD-02076, REPLACED E1 HYD PUMP IAW AMM 29-10-03. REF ITEM'SDR CALA2015063000545Pump · malfunctionedSHORTLY AFTER TAKEOFF ENG NR 1 LOW PRESS HYD LIGHT ILLUMINATED. QRH PROCEDURE ACCOMPLISHED. A SYS QTY SHOWS 106% & PRESS STABILIZED AT 2960. INFLIGHT QTY DROPPED TO 97% ON LANDING. R & R NR 1 ENG HYD PUMP & SEAL. NO LEAKS NOTED AT THIS TIME. ACFT OK TO COSDR HALA201506290121Pump · leakingLINE SERVICE NOTED FLUID DRIPPING FROM NR 2 ENGINE. LINE MAINTENANCE FOUND RT ENGINE DRIVEN HYDRAULIC PUMP LEAKING. TROUBLESHOT, FOUND ENGINE HYD PUMP INOPERATIVE, R & R NR 2 ENGINE DRIVEN PUMP IAW AMM 29-11-01. RUN AND LEAK CHECKS GOOD.SDR CA150626004Pump · leaking(CAN) DURING APPROACH A TOTAL LOSS OF FLUID FROM NR 3 HYD SYS WAS OBSERVED. AN EMER DECLARED. MX FOUND 3A HYD PUMP LEAKING FROM CASE DRAIN DURING PUMP OPERATION. REPLACED 3A PUMP IAW AMM 29-12-03. HYD SYS 3 BLED IAW AMM 29-10-00, GEAR SWINGS CARRIED OUT WISDR UHLA201506250501Pump · leakingDURING CLIMBOUT, THE CREW RECEIVED A HYD SYSTEM 2 LOW QUANTITY EICAS MESSAGE. THE QRH PROCEDURES WERE FOLLOWED, THE SYSTEM CONTINUED SHOWING DECLINING LEVELS OF HYDRAULIC FLUID, AND THE CREW DECLARED AN EMERGENCY AND MADE AN UNEVENTFUL, UNSCHEDULED LANDING. SDR CA150625002Adapter · cracked(CAN) NR 1 ENG DRIVEN HYD PUMP ADAPTER PLATE CRACKED. THE CRACK CAUSED ONE OF FOUR HYD PUMP ATTACH STUDS TO SEPARATE FROM THE MOUNT. HYD PUMP FUNCTION & SECURITY OF ATTACHMENT WAS NOT AFFECTED.SDR SIMA20150615004Pump · faultyHYDRAULIC PUMP 1B PUMP EXTREMELY LOUD NOISE & BURNING SMELL WHEN TURNED ON. R & R NR 1 HYD PUMP IAW AMM 29-11-03. PERFORMED LEAK CHECK & OPERATIONS CHECK. NO LEAKS NOTED & OPERATIONS CHECKED GOOD.SDR 7GMB2015061211531Pump · leakingFOUND LEAKAGE FROM NR 2 ENG HYD PUMP HOUSING. R & R WITH REPAIRED UNIT. OPERATIONS CHECK & LEAK CHECKED GOOD. ACFT WAS RETURN TO SERVICE.SDR SIMA20150611001Pump · failedHYD LO QTY ON EICAS. HYD 1 FLUID LEVEL AT ZERO. R & R E1 EDP IAW AMM 29-10-03. OPERATIONS & LEAK CHECKED GOOD.SDR RAIA20150607001Pump · leakingONE HYDRAULIC FAIL EICAS MESSAE DURING LANDING, MADE EMERGENCY LANDING. MAINTENANCE INSPECTED AND REPLACED NR 1 ENGINE HYD PUMP, OPS AND LEAK CHECK GOOD.SDR AALA20150530004Pump · faultyEMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING APPROACH LT HYD LOW PRESS LIGHT ILLUMINATED WITH HYD QTY INDICATION HIGH. FOUND EXCESSIVE AIR IN BOTH HYD SYS, BLEED AIR. R & R NR 1 ENG HYD PUMP IAW AMM 29-10-05. SERVICED HYD SYS. PERFSDR R61A201505290340Pump · leakingTHE CREW REPORTED THAT THEY RECEIVED A HYDRAULIC SYSTEM 2 ENGINE DRIVEN PUMP FAILURE MESSAGE ON THE EICAS DURING FLIGHT. THE FLIGHT DIVERTED FROM ITS INTENDED COURSE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE ENGINE DRIVEN HYDRAULIC PUMP NRSDR HALA2015052600095Pump · malfunctionedLT HYDRAULIC ENGINE PUMP PSI 3340. R & R LT EDP IAW AMM 29-11-05. OPS CHECK, LEAK CHECK OK.SDR CA150520018Pump · failed(CAN) HYDRAULIC FLUID TURNING DARK, FLUID TESTED & CONTAMINATION DETERMINED TO BE COMING FROM PUMP. PUMP REPLACED.SDR CA150515011Pump · failed(CAN) THE AIRCRAFT WAS ON A CREW CHANGE FLIGHT FOR A CUSTOMER, UPON START UP FOR DEPARTURE, THE FLIGHT CREW SAW THE HYDRAULIC QUANTITY FALL TO 0. THEY DISEMBARKED THEIR PASSENGERS AND CALLED MAINTENANCE. MAINTENANCE ARRIVED AND FOUND THAT THE NR 3 PUMP, SN 16SDR 29GA2015051300001Motor · failedLOST MAIN HYDRAULIC PRESSURE DURING TAXI, THEN LOST BRAKES AND EMERGENCY PRESSURE. REPLACED HYDRAULIC PUMP MOTOR FUNCTION CHECK LEAK CHECK GOOD, OPS CHECK SATISFACTORY.SDR CA150504011Pump · leaking(CAN) IN CRUISE AT FL 250 NR 1 HYD ISO VLV CAUTION LIGHT COMPLETE LOSS OF FLUID. MX FOUND NR 1 EDP SEAL DRAIN LEAKING. REPLACED NR 1 EDP & FILTERS IAW MM CH 29-11-01 & SYS INSPECTED IAW TASK 05-54-00-280-801. LEAK & FUNCTION CHECK SERVICEABLE AFH 9795.33, SDR AALA20150503004Pump · leakingAT CRUISE, RT HYD QTY DECREASED TO 4 QTS WITH NR 2 ENG PUMP ON HIGH. HYD PRESS DROPPED TO ZERO. EMERGNECY DECLARED & LANDED WITHOUT INCIDENT, ON APPROACH, PRESSURIZED RT SYS USING AUXILIARY PUMP PRESS. FLAPS & SLATS EXTENDED NORMALLY. GEAR CAME DOWN BUT DOSDR CA150430005Pump · bypassing(CAN) HYDRAULIC FLUID LOSS FROM RESERVOIR BREATHER LINE. NR 2 ED PUMP FOUND TO BE BYPASSING THROUGH GARLOC SEAL. ED HYD PUMP REPLACED, CHECKED SERVICEABLE.SDR UHLA201504260329Pump · damagedCREW REPORTED HYDRAULIC 2, LOW QUANTY MESSAGE IN FLIGHT FOLLWED BY E2 HYDRAULIC PUMP FAIL MESSAGE. THE CREW MADE AN UNSCHEDULED LANDING. WHEN THE SPOILERS DEPLOYED ON TOUCHDOWN A HYDRAULIC SYSTEM 2 FAIL MESSAGE APPEARED. MAINTENANCE FOUND A FAULTY E2 HYDRAUSDR CA150427010Pump · leaking(CAN) WHILE IN CRUISE, CREW REPORTED A STEADY DECLINE IN HYDRAULIC FLUID QUANTITY. IN CONJUNCTION WITH DISPATCH, MOC, FLIGHT CREW IT WAS DECIDED THAT A DIVERSION WOULD BE PRUDENT. CREW DECLARED A PAN PAN WITH ATC. LANDING WAS UNEVENTFUL. HYDRAULIC QUANTITY SDR YENA20150420073Pump · leakingFLIGHT DIVERTED DUE TO ECAM MESSAGE HYD GRSVR LO LVL. FOUND GREEN HYDRAULIC SYSTEM EDP LEAKING ON NR 1 ENGINE. R & R EDP ASSEMBLY IAW AMM. NO LEAKS NOTED, OPS CHECK NORMAL.SDR 2015FA0000395Pump · failedENGINE DRIVEN HYDRAULIC PUMP FAILED, CAUSING A LOSS OF SYSTEM PRESSURE, PREVENTING THE LANDING GEAR FROM FULLY EXTENDING. HYDRAULIC PUMP PN 12801037.SDR SWAA2015041638612Pump · failedAIR TURN BACK, FLIGHT CONTROL LIGHT & NR 1 ENG HYD LOW PRESS LIGHT SYS A HYD QTY DECREASED. FOUND A ENG PUMP FAILED. R & R PUMP IAW AMM.SDR CA150414003Pump · failed(CAN) SHORTLY AFTER TAKEOFF THE CREW REPORTED A BLUE HYDRAULIC SYSTEM PUMP OVERHEAT, FLIGHT CONTINUED. BLUE ELECTRIC PUMP CHANGED IAW AMM TSK 29-12-51-000-001-A/400-001-A.SDR CA150413004Pump · leaking(CAN) THE CREW HAS REPORTED THAT THE GREEN HYDRAULIC SYSTEM HAS FAILED ENROUTE. NR 2 GREEN HYDRAULIC PUMP REPLACED IAW AMM 29-11-51 PB401.SDR AALA201504109005Pump · failedFLT 504 EN-ROUTE, WHILE IN CRUISE FLIGHT, THE ACFT EXPERIENCED A GREEN HYD SYS OVERHEAT WARNING, FOLLOWED BY A GREEN HYD ENG 1 PUMP LOW PRESS FAULT, THEN A PTU FAULT. AS A PRECAUTION, THE FLIGHT DIVERTED. THE FLIGHT CREW DECLARED AN EMER. THE FLIGHT LANDED SDR CA150323002Pump · split(CAN) EXPERIENCED NR 1 HYDRAULIC SYSTEM FAILURE, WITH TOTAL LOSS OF FLUID. DURING THE ENROUTE CLIMBOUT. FLIGHT CREW REPORT: WHILE CLIMBING THROUGH FL190 WE RECEIVED A NR 1 ENGINE HYD PUMP CAUTION LIGHT. AFTER ACTIONING THE QRH, A DECISION WAS MADE TO RETURNSDR R61A201503160172Motor · failedTHE NR 3 HYD PRESSURE LIGHT CAME ON AND THERE WAS NO PRESSURE SHOWING IN THE SYSTEM. AFTER CONSULTING WITH MAINTENANCE, CREW RETURNED TO DEPARTURE AND ATC DECLARED AN EMERGENCY FOR CREW. PASSENGERS DID NOT BRACE AND CREW LANDED AND TAXIED TO GATE WITHOUT INCSDR CA150312001Pump · failed(CAN) DURING CLIMB OUT, NR 1 HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED WITH THE NR 1 HYDRAULIC FLUID HOT CAUTION LIGHT. SHORTLY AFTER, A NR OF OTHER FLIGHT CONTROL RELATED CAUTION LIGHTS ILLUMINATED. THE QRH PROCEDURE WAS ACTIONED. HYDRAULIC PRESSURE WAS RESSDR 7MNA20180207001Bearing · seizedPILOT FLYING SOLO, DAY, VFR, OBSERVED "HYDRAULIC" AND "SERVO" CAUTION LIGHTS FOLLOWED BY HIGHER THAN NORMAL FORCES REQUIRED FOR TAIL ROTOR CONTROL. PILOT LANDED AS SOON AS PRACTICAL PER THE RFM. FOUND THE BELT DRIVEN HYDRAULIC PUMP BEARING HAD SEIZED.
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