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 ASOA201705201598Pump · failedHYDRAULIC NR 1 LOW PRESSURE INDICATION IN FLIGHT. FOLLOWED QRH AND DIVERTED TO NEAREST SUITABLE AIRPORT. REMOVED AND REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP IAW AMM 29-10-01. OPS AND LEAK CHECKED GOOD.SDR A6WA2017051644997Pump · failedAFTER TAKEOFF WITH GEAR SELECTOR UP, FOR MORE THAN 30 SECONDS RECEIVED GEAR DISAGREE WARNING MESSAGE. MAIN LANDING GEAR SHOWED WHITE HASH MARKS. NOSE GEAR SHOWED RED HASH MARKS. MESSAGE PERSISTED FOR MORE THAN 20 SECONDS. COMPLIED WITH QRH. TURNED ON HYD PUMSDR SWAA2017050213525Pump · leakingAIR TURNBACK, ON CLIMB OUT PASSING 10,000 FEET ENGINE AND ELECTRIC A HYDRAULIC LOW PRESS LIGHT ILLUMINATED. R&R A SYSTEM ENGINE DRIVEN HYDRAULIC PUMP IAW AMM.SDR FDEA201705011301Pump · inoperativeIN CRUISE FL360 GOT GREEN HYD SYSTEM OVERHEAT. ECAM ADVISED TO TURN OFF GREEN ENGINE PUMPS 1 AND 2. ENG HYD 1 PUMP SHUT OFF NORMALLY. ENG HYD 2 GREEN PUMP TURNED OFF MOMENTARILY. ITS CB POPPED AND THE PUMP STARTED OPERATING AGAIN. CORDINATED WITH MOCC TO RESETSDR 2017F00161Pump · cloggedEXPERIENCED A SIGNIFICANT DELAY EVENT IN APRIL 29TH CAUSED BY ECAM MESSAGE HYD B RSVR OVHT, HYD B RSVR LO AIR PR AND HYD B SYS LO PR IN FLIGHT. AFTER LANDING AT KMQ, MX FOUND THE BLUE SYSTEM EDP CASE DRAIN FILTER DPI WAS POP OUT. A LOT OF CONTAMINATION AND METSDR HALA2017042800109Pump · leakingLT ENG GREEN SYS HYD PUMP LEAKING FLUID. R&R PUMP IAW AMM 29-11-51 PUMP, HYDRAULIC OFF HYD PUMP 40511 ON 33-2912-9-0002 10643.SDR FDEA201704281299Pump · malfunctionedL HYD QUANTITY LO HYD PSI EICAS. DECLARED AN EMERGENCY AND FOLLOWED QRH WE STILL HAD PSI. REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP IAW AMM 29-11-05-4-2 NEEDS TO BE LEAK CHECKED RAN NR 1 ENGINE PER JRH TO LEAK CHECK ENGINE DRIVEN HYDRAULIC PUMP, NO LEAKS FOUNSDR SWAA2017050113483Pump · low pressureB SYSTEM HYDRAULIC LOW PRESSURE AND QUANTITY LOSS IN FLIGHT. EMERGENCY DECLARED AND DIVERTED. R & R THE NR 2 ENGINE DRIVEN PUMP IAW MMM.SDR YENA201704260312Pump · failedFLT 2115, DCA-JAX. THE CREW DECLARED AN EMERGENCY LANDING INTO JAX WHEN THEY RECEIVED A SYSTEM 2 LO HYD MESSAGE. THE AIRCRAFT LANDED UNEVENTFULLY. R&R EDP NR 2 IAW AMM 29-11-01 OPS CK GOOD.SDR ASMF201704011Warning Light · illuminatedAIRCRAFT RETURN TO PLATFORM AS A CONSEQUENCE OF THE ELECTRICAL HYDRAULIC PUMP SYSTEM B LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORM RESET TO CIRCUIT BREAKER OF THE ELECTRICAL HYDRAULIC PUMP IAW AMM 29-11-21 AND THE CONNECTORS WERE CHECKED IAW WDM 29-11-12, ASDR HALA2017041200096Pump · leakingON ARRIVAL HYDRAULIC FLUID LEAKING NR 1 ENG DRAIN MAST. ON INSPECTION FOUND BLUE SYSTEM PUMP AT FAULT. BLUE SYS HYD PUMP REMOVED AS PER MM 29-12-51-000-801-A. SEE LOG 8986422 FOR PUMP REPLACEMENT AND PUMP DETAILS. NR 1 ENGINE BLUE SYSTEM EDP IS A BORROWED PARTSDR DALA2017040502841Pump · failedLEFT HYDRAULIC TEMP HIGH DURING CRUISE. TURNED ON TRANSFER PUMP PRESSURE WENT TO ZERO. LEFT ENGINE HYDRAULIC PUMP ON. PRESSURE IS ZERO. REMOVED AND REPLACED THE NR 1 ENGINE DRIVEN PUMP IAW MM. OPERATIONS CHECKED GOOD.SDR VNAA2017040400003Warning Light · illuminatedHYDRAULIC PUMP 2A CAUTION MESSAGE IN FLIGHT, AN EMERGENCY WAS DECLARED. OPENSDR AALA201704039018Pump · failedHYDRAULIC RESIVOIR OVERHEATED, PERFORMED EMERGENCY LANDING. REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP ASSEMBLY. AIRCRAFT WAS GROUNDED.SDR AALA201703309025Pump · failedTHE CREW REPORTED A LOW GREEN HYDRAULIC PRESSURE ALERT, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED, AND LANDED SAFELY WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED THE NR 1 ENGINE HYDRAULIC PUMP ASSY. AIRCRAFT WAS GROUNDED.SDR SWAA2017032712786Pump · faultyDECLARED EMERGENCY, NR 1 ENGINE HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. R&R NR 1 ENGINE DRIVEN HYDRAULIC PUMP PER AMM.SDR SWAA2017032712783Module · faultyDIVERSION, HYDRAULIC B, NR 2 ENGINE LOW PRESS LIGHT ILLUMINATED AT CRUISE. R&R HYDRAULIC SYSTEM B PRESSURE MODULE PER AMM.SDR FDEA201703220971Pump · damagedHOLDING SHORT OF RWY 5R IND RECEIVED LVL 2 HYD 2 QTY LOW. PUT HYD SYS IN MANUAL TURNED HYD PUMPS OFF. TEMP WAS 33C AT HYD PUMP SHUTOFF. HYD QTY WENT TO ZERO. PER CREW DEBRIEF, HYDRAULIC QUANTITY WAS 1.1 WHEN PUMPS WERE SHUTOFF AND PUMPS WERE NOT OPERATING WHESDR UIEA2017031100321Warning Message · false activationRIGHT PRIMARY HYD PUMP EICAS MESSAGE CAME ON IN FLIGHT. TROUBLESHOT IAW FIM 29-11. ALL OPS CHECKS NORMAL. INSPECTED PRESSURE SWITCH CONNECTOR IAW AMM 29-11-17, CONNECTOR IS CLEAN NO CORROSION PRESENT. ACFT OK FOR SERVICE.SDR CALA2017031000557Pump · faultyLOST HYD B SYSTEM. EMERGENCY DECLARED. SERVICED B SYSTEM HYDRAULICS TO FULL 7 GALLONS. WITH ENGINE NR 2 RUNNING FOR 30 MIN AND THEN WITH B SYSTEM ELECTRIC PUMP NO EXTERNAL HYDRAULIC LEAKS FOUND. B SYSTEM FLUID STARTED AT 105% BEFORE ENGINE RUN AND DROPPED TO SDR Q5QA2017030800067Pump · failedBRAKE SYSTEM FAILURE CAUSED BY HYDRAULIC PUMP FAILURE.SDR AALA201703089001Pump · faultyAIRCRAFT WAS GROUNDED. SYSTEM B ELECTRIC HYDRAULIC PUMP OVERHEAT LIGHT INDICATION. ODOR IN COCKPIT WHICH DISSIPATED AFTER PUMP TURNED OFF. REMOVED AND REPLACED SYSTEM B ELECTRIC MOTOR-DRIVEN PUMP IAW AMM 29-11-21 AND SYSTEM B HYDRAULIC FLUID OVERHEAT WARNING SDR A6WA2017021544790O-Ring · leakingIN CRUISE FLIGHT RECEIVED HYD 3 LOW PRESS CTN MESSAGE, HYD 3 QUANTITY 5 % , HYD 3 PRESS 2000. COMPLIED WITH QRH, HYD 3 B ACMP TURNED ON. UPON LANDING HYD 3 QUANTITY 5% AND PRESSURE 0. INSPECTED AND FOUND HYD PUMP 3A BALL ATTENUATOR LEAKING. REMOVED AND REPLACESDR JJBA20170203006Pump · inoperativeNR 1 HYD PRESSURE AND NR 1 HYD STANDBY PRESSURE READS ZERO. QUANTITY READS 2 QUARTS. FOUND CASE DRAIN TUBE ASSY LEAKING. R & R DRAIN TUBE LEAK & OPS CHECKED. EDP INSPECTED. R & R EDP CASE DRAIN TUBE, FAILED OPS CHECK. R & R CASE DRAIN FILTER. R & R THE SDR YENA201702020057Pump · failedFLIGHT CREW REPORTED EDP 2 FAIL FOLLOWED BY COMPLETE LOSS OF NR 2 HYDRAULIC SYSTEM. DIVERTED. EMERGENCY DECLARED. REPLACED NR 2 ENGINE EDP HYDRAULIC PUMP IAW AMM 29-11-01. PERFORMED OPS CHECK. OPS CHECK TEST PASSED.SDR SWAA2017012411442Pump · overheatedAIR TURNBACK, NR 1 ELECTRIC OVERHEAT LIGHT ILLUMINATED INFLIGHT. R&R NR 1 ELECTRIC HYDRAULIC PUMP IAW AMM.SDR WWQA201701160001Pump · failedDURING DECENT THE CREW HAD A CASS MESSAGE WITH LOW HYDRAULICS. THEY THEN NOTICED THAT THE COMBINED HYDRAULIC SYSTEM WAS INDICATING LOW. THEY THEN RECEIVED ANOTHER CASS MESSAGE STATING TR LOCKED. WITH LOW HYDRAULIC QUANTITY THEY WERE UNABLE TO EXTEND THE LANDINSDR SWAA2017010911061Pump · faultyDECLARED EMERGENCY, HYDRAULIC SYSTEM A QUANTITY AND PRESSURE LOSS. SYSTEM A ENGINE & ELECTRIC LOW PRESSURE LIGHTS ILLUMINATED. REPLACED NR 1 ENGINE HYDRAULIC PUMP PER AMM.SDR AALA20170106036Pump · failedAIRCRAFT WAS GROUNDED. EMERGENCY DECLARED ON APPROACH ACCOUNT RIGHT HYDRAULIC PUMP FAILURE. LANDING UNEVENTFUL. REMOVED AND REPLACED RIGHT ENGINE DRIVEN HYDRAULIC PUMP ASSEMBLY IAW AMM 29-10-05 AND THE ENGINE DRIVEN HYDRAULIC SUPPLY LINE IAW AMM 20-30-02 (AALASDR JJBA20170104003Pump · inoperativeNR 2 HYD QUANTITY AT ZERO AND PRESSURE FELL TO ZERO. NR 2 ENGINE HYD CAUTION LIGHT ILLUMINATED. SECURED A B-NUT TO THE RT SPOILER ACTUATOR AND R & R THE NR 2 ENGINE DRIVEN PUMP. OPS AND LEAK CHECKED GOOD.SDR AALA201701079006Pump · failedFLIGHT CREW REPORTED THAT WHILE ENROUTE THE CIRCUIT BREAKER FOR THE HYDRAULIC B ELECTRIC PUMP TRIPPED AND ECAM MESSAGES FOR HYD B ELECTRIC PUMP PRESSURE LOW AND HYD B SYSTEM LOW PRESSURE. DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFTSDR DXTA2017010306354Pump · leakingDURING FLIGHT, FELT A HIGH SPEED FREQUENCY VIBRATION, FOLLOWED BY A CYAN FLAPS RATE LOW AND RT HYD ENG PUMP FAIL. SYNOPTIC PAGE SHOWED A FAILED RT HYD PUMP AND 0% FLUID IN THE RESERVOIR. AFTER LANDING, DISCOVERED FLUID LEAKING FROM ENGINE NACELLE. 0 FLUID IN SDR PCPR201701171Bolt · shearedAFTER TAKEOFF PILOT COULD NOT RETRACT GEAR. DETERMINED BY MAINTENANCE CREW THAT THE LANDING GEAR HYDRAULIC POWER PACK MOTOR CAGE BOLT HAD SHEARED AND BACKED OUT INTO MOTOR FAN ASSEMBLY. MOTOR SEIZED AND SUBSEQUENTLY BURNED OUT. ADDITIONAL DAMAGE CAUSED TO LESDR XV6A2016122700004Pump · inoperativeAFTER STARTING ENGINES AND TURNING HYDRAULICS ON, THERE WAS NO PRESSURE. INSTALLED SERVICEABLE HYDRAULIC POWER PACK ASSY IAW DO228 AMM 29-10-19. FUNCTIONAL AND LEAK CHECKED GOOD. (SUSPECT HYDRAULIC PUMP FAILED INTERNALLY. HYDRAULIC PUMP MOTOR OPS CHECK GOOSDR AALA201612299015Pump · leakingAIRCRAFT WAS GROUNDED. RETURNED TO PHL ACCOUNT HYDRAULIC QUANTITY DECREASED. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED OVERWEIGHT WITHOUT INCIDENT. AIRCRAFT WAS REMOVED FROM SERVICE. MAINTENANCE FOUND SMALL HOLE IN ENGINE DRIVEN PUMP NR 1 CASTING. REPLACSDR ASAA2016122619168Pump · leakingDURING CRUISE, THE NR 1 ENGINE LOW PRESSURE LIGHT CAME ON FOLLOWED BY LOSS OF SYS A. RAN QRH FOR BOTH. ACFT GROUNDED. EMERGENCY LANDING. INSPECTED SYSTEM A FOUND EDP LEAKING. REMOVED SYSTEM A EDP IAW AMM 29-11-21-000-801-001. INSPECTED CASE DRAIN FILTER. NSDR AALA20161223001Pump · faultyLEFT ENGINE HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED AFTER 15 MINUTES. SYSTEM A HYDRAULIC QUANTITY DROPPED TO 18%. EMERGENCY DECLARED, DIVERTED, AIRCRAFT WAS GROUNDED. LANDING UNEVENTFUL. REMOVED AND REPLACED LEFT ENGINE HYDRAULIC PUMP IAW AMM 29-11-SDR HALA2016121300542Control Unit · faultyATB, RT HYD DEMAND PUMP INOP. T/S PER WP 29-11-22 SWAPPED R HYD PUMP ELCU M896 WITH CENTER PUMP 2 ELCU M898. OPS CK'D R HYD DEMAND PUMP OP CK'D GOOD IAW AMM 29-11-00 AND WP 29-11-22.SDR SIMA20161211002Pump · failedHYD 1 LOW QTY IN FLIGHT ON EICAS FOLLOWED BY E1 HDY PUMP FAIL. FOLLOWED BY HYD 1 SYSTEM FAIL. AFTER LANDING NO OUTBOARD BRAKES, NO STEERING. REMOVED AND REPLACED THE NR 1 HYDRAULIC PUMP IAW AMM 29-10-03. OPS AND LEAK CHECKED GOOD.SDR 29GA2016121000001Pump · inoperativeFLIGHT 0075, LOST HYDRAULIC PRESSURE FOR STEERING AND BREAKING DURING TAXI. OVERIDE INOPERATIVE. R & R HYDRAULIC DRIVEN MOTOR PUMP IAW AMM 29-10-10. OPS AND LEAK CHECKED GOOD.SDR YENA201612061082Pump · failedFLIGHT CREW REPORTED A COMPLETE LOSS OF NR 2 SYSTEM HYDRAULIC QUANTITY AND PRESSURE. ACCOMPLISHED QRH 10-11 PROCEDURE. R & R THE NR 2 PUMP IAW AMM 29-11-01. PERFORMED OPS & LEAK CHECK. OPS & LEAK CHECKED PASSED.SDR R61A201612020695Pump · leakingDURING FLIGHT, CREW RECEIVED A HYD 2 LOW QTY MESSASGE AND WAS AT 22%. DECLARED AN EMERGENCY, AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE NR 2 EDP IAW AMM AND OPS CHECKED GOOD.SDR YTRA2016112933001Drive Shaft · damagedPILOT REPORTED HYDRAULIC FAILURE IN CRUISE FLIGHT. ON INSPECTION FOUND HYDRAULIC PUMP DRIVESHAFT SPLINES WORN.SDR JJBA20161123028Pump · inoperativeNR 2 HYD PUMP CAUTION ILLUMINATED IN FLIGHT. REMOVED AND REPLACED THE HYDRAULIC PUMP.SDR JJBA20161122027Pump · inoperativeNR 2 HYD FLUID LOSS IN FLIGHT. R & R THE NR 2 EDP. OPS CHECKED GOOD. NO LEAKS NOTED.SDR SIMA20161118003Pump · failedHYD SYSTEM NR 1 FAILURE IN FLIGHT. HYD NR 1 QUIANTY INDICATOR AMBER FULL SCALE LEFT. RAN PROCEDURE. REMOVED AND REPLACED THE NR 1 EDP IAW AMM 29-10-03, AND PRESSURE LINE. LEAK CHECKED GOOD.SDR JJBA20161110013Pump · inoperativeNR 2 HYD PUMP CAUTION ILLUMINATED IN FLIGHT. R & R NR 2 EDP. OPS & LEAK CHECKED GOOD. LEFT AND NOSE DOORS REMAINED OPEN DURING RETRACTION. BLED AIR FROM HYD SYSTEMS 1 & 2. PERFORMED GEAR SWING. OPS & LEAK CHECKED GOOD. THE GEAR PINS WHERE INSTALLED. RETURNSDR Q5QA20161115006Pump · failedWHILE CRUISING AT 22,000 FT, PILOT EXPERIENCED HYD AUTO PRESSURE FLUCTUATION BETWEEN 1600/3200. HYD ON, PRESSURE FLUCTUATIONS AND SPIKES TO 3800. HYD OFF, PRESS 0 AND LANDING GEAR FALLS OUT. PILOT LANDED WITH HYD PRESSURE ON AND SEEING PRESSURE FLUCTUATIONS ANSDR SWAA2016110809483Pump · faultyLOSS OF A SYSTEM HYDRAULICS INFLIGHT WITH BOTH HYDRAULIC LOW PRESSURE LIGHTS AND FLT CONTROL A LOW PRESSURE LIGHT. R & R THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP IAW AMM.SDR 6EER20161104001Bearing Seal · leakingPILOT REPORTED, INBOUND FOR LANDING, A CHANGE IN AIRCRAFT NOISE WAS HEARD FOLLOWED BY A HYDRAULIC SYSTEM FAULT ADVISORY THEN A HYDRAULIC LOW PRESSURE CAUTION MESSAGE. THERE WERE SEVERAL OTHER MESSAGES ASSOCIATED WITH THE LOSS OF HYDRAULIC PRESSURE. PILOT DECLA
Back to JASC 2913