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 SWAA2014091031783Pump · failedDIVERSION DECLARED EMERGENCY. A HYD SYS FAILED BOTH LOW PRESS LIGHT ILLUMINATED & A QTY DEPLETED. R & R A ELEC HYD PUMP IAW MM.SDR CA140908027Pump · failed(CAN) FLIGHT CREW RECEIVED NR 2 ENGINE, HYDRAULIC PRESSURE CAUTION LIGHT DURING CLIMB OUT. FLIGHT RETURNED TO DEPARTURE AIRPORT. LANDED WITHOUT INCIDENT. NO EMERGENCY DECLARED. NR 2 EDP FAILED, NR 2 EDP WAS REPLACED. FILTERS WERE FOUND TO BE CONTAMINATED,SDR CALA2014090392058Pump · leakingCENTER HYDRAULIC PRESSURE EICAS ALERT. HYDRAULIC PUMP LEAKING FLUID, CREW POWERED DOWN SYSTEM AND CONT. EMERGENCY DECLARED DURING ARRIVAL PHASE. LAND WITHOUT INCIDENT FOUND LINE FROM C2 PUMP TO CASE DRAIN FILTER LEAKING. TIGHTENED LINE, LEAK CHECK OF C2 PSDR CA140902006Pump · leaking(CAN) ON DESCENT, CREW NOTICED A LOSS IN HYDRAULIC QTY AND FLUCTUATING HYDRAULIC PRESSURE. A/C LANDED SAFELY WITH OUT FURTHER INCIDENT. UPON INSPECTION, LT ENGINE HYD PUMP WAS FOUND LEAKING FLUID FROM A CRACK IN THE PUMP HOUSING. MAINTENANCE REPLACED THE HYD PSDR 7EMA20140902006Coupling · failedHYDRAULIC PUMP DRIVE COUPLING SPRING INTERNAL SPLINES FAILED CAUSING DISENGAGEMENT OF HYD PUMP. RESULTING HYD FAILURE CAUSED UNPLANNED LANDING OF ACFT. NO DAMAGE OR INJURIES REPORTED. HIS DRIVE ASSEMBLY HAS BEEN THE SUBJECT OF NUMEROUS SB'S & AT LEAST ONE ASDR CA140827001Shaft · sheared(CAN) FLIGHT CREW REPORTED NR 2 HYD EDP CAUTION LIGHT ILLUMINATED AFTER LANDING GEAR DOWN SELECTION ON APPROACH. ALL WITH HYDRAULICS FUNCTIONED NORMALLY WITH STANDBY PUMP #2 ON. MAINTENANCE FOUND THE NR 2 EDP SHAFT SHEARED WITH DAMAGE ON SPLINES OF THE SHAFT. SDR CA140827003Pump · cracked(CAN) IN CRUISE FLIGHT CREW OBSERVED THE GREEN HYDRAULIC QTY SLOWLY STARTING TO DECREASE. APPROXIMATELY 1.5 HOURS PRIOR TO LANDING LOW LEVEL ADVISOR WAS TRIGGERED. THE CREW CARRIED OUT THE QRH PROCEDURE AND SHUT DOWN THE PUMP TO PREVENT PUMP CAVITATION AND DAMSDR SIMA20140816001Pump · failedEICAS DISPLAYED E1 HYD PUMP FAIL AS WELL AS HYD SYS 1 FAIL. HYD FLUID QTY SHOWED IN AMBER RANGE. AOM PROCEDURES COMPLIED WITH. PRESS FLUCTUATIONS WERE OBSERVED BETWEEN 2300 - 300 PSI. R & R NR 1 ENG EDP HYD OPERATIONAL & LEAK CHECKED OK IAW AMM 29-10-03.SDR CA140818007Gasket · failed(CAN) ENROUTE, CREW ADVISED DISPATCH THEY HAD HYDRAULIC ENGINE DRIVEN PUMP 2A CAUTION MESSAGE AND NEEDED TO DESCEND TO FL 260. HALF HOUR LATER THEY ADVISED THEY HAD LOST NUMBER TWO HYDRAULIC SYSTEM. CREW DECLARED AN EMERGENCY WITH ATC. FLIGHT SUCCESSFULLY LANDSDR 6CBA20140814133Motor · faultyAFTER DEPARTURE HYD CAWS IN FLIGHT, GEAR EXTENDED MANUALLY IAW QRH. THE ACFT DIVERTED & LANDED SAFELY. A FERRY PERMIT WAS OBTAINED FOR ACFT RELOCATION WHERE REPAIRS WERE MADE. THE HYD POWER PACK MOTOR PN 960.30.02.104 & RELAY 974.09.26.112 FOUND TO BE FAULTYSDR DXTA2014081505856Motor · unserviceableAFTER NORMAL LANDING THE LOW BRAKE PRESS ANTI-SKID INOPERATIVE ANNUNCIATOR ILLUMINATED. NORMAL BRAKES NOT AVAILABLE DURING TAXI, HAD TO USE EMER BRAKES TO STOP ACFT. PUSHED IN CB, RAN POWER BRAKES 24X, COULDN'T DUPLICATE. IAW AMCC REPLACED MOTOR WITH AN OVESDR REXA2014080500792Pump · malfunctionedHYD SYS 2 RESERVOIR COMPLETELY EMPTIED. SECURED HYD SYS 2 & RETURNED. ACCUMULATOR ALSO LOST PRESS & OTBD BRAKES WERE LOST AS WELL. LANDED AT 72900 POUNDS. COMPLETED INSPECTION OF NR 2 EDP IAW AMM 05-51-33. ALL CHECKED GOOD. R & R NR 2 AC MOTOR PUMP PN ONSDR XV6A2014080500005Motor · failedGEAR HANDLE DOWN & NO INDICATION OF ANY HYD PRESS OR GEAR MOVEMENT. RAN QRH & PERFORMED EMER GEAR EXTENSION CHECKLIST. R & R HYD POWER PACK, OPERATIONS CHECKED GOOD. DISCOVERED HYD ELEC MOTOR FAILED ON HYD POWER PACK, ELEC MOTOR SENT FOR OVERHAUL FOR FINDINSDR CA140731010Pump · failed(CAN) ENGINE HYDRAULIC EDP FAILURE DURING FLIGHT. INITIAL INVESTIGATION CONFIRM PUMP FAILURE AS ALL HYDRAULIC FILTERS DPIÏ¿½S ARE FLAGGED. EMERGENCY WAS DECLARED UPON LANDING. CREW DID A FLAPLESS LANDING. AIRCRAFT LANDED SAFELY.SDR CALA2014073101052Pump · failedAFTER LEVEL OFF, TAKEOFF +30 MIN B HYD SYS FAILED. FOUND HYD PUMP ON NR 2 SEIZED. R & R NR 2 ENG HYD PUMP IAW AMM 29-11-11-401. OPERATIONS & LEAK CHECKED GOOD. FLUSH & FILTER REPLACEMENT SCHEDULED.SDR CA140731014Pulley · worn(CAN) BEARING, WAS SPINING ON PULLEY MADE A GROOVE IN THE CIRCLIP AND PULLEY.SDR IPXA2014072583761Valve · failedAIR TURNBACK, LEVEL 2 ALERT HYD 2 FAILURE. R & R NR 2 EDP ELECTRIC DEPRESSURIZATION VALVE IAW MM 29-11-21-400-802. OPS AND LEAK CHECK GOOD. THIS WAS THE LT PUMP (UPPER) IPC REF 29-11-22-01.SDR SIMA20140723004Pump · failedHYD 2 LOW QTY ADVISORY IN FLIGHT, ABOUT 20 - 30 MINUTES LATER HYD 2 PUMP FAIL MSG. POST FLIGHT SHOWS HYD FLUID COATING INSIDE NR 2 WW. R & R NR 2 ENG DRIVEN PUMP IAW AMM 29-10-03. RAN ENGS LEAK & OPERATIONS CHECKED GOOD, NO DEFECTS NOTED.SDR DXTA2014072205826Motor · failedDURING FLIGHT, ANTI-SKID INOPERATIVE ANNUNCIATOR LIGHT ILLUMINATED. LANDED AFTER RUNNING ABNORMAL CHECKLIST. LOST BRAKES AFTER LANDING, LOW BRAKE ANNUNCIATOR LIGHT ILLUMINATED & POWER BRAKES CIRCUIT BREAKER TRIPPED. USED THE EMERGENCY BRAKE HANDLE TO STSDR SWAA2014072130103Pump · leakingDECLARED EMER HYD SYS A QTY & PRESS REDUCED TO ZERO INFLIGHT. R & R NR 1 ENG HYD PUMP IAW MM.SDR SIMA20140716006Pump · failedNUMBER 1 HYD QTY LOW. GEAR DEPLOYED WITH FREE FALL HANDLE. GEAR PINS INSTALLED. R & R NR 1 ENG HYD PUMP IAW AMM 29-10-03. OPERATIONS CHECKED GOOD. LEAK CHECKED GOOD.SDR 8EKA20140723001Relay · stuckCREW PUT THE LG UP WITH NO ISSUES. WHEN THEY PUT THE GEAR HANDLE DOWN, THE GEAR DID NOT GO DOWN. THEY NOTICED THAT THE LG CONTROL CB WAS POPPED & ATTEMPTED TO PUSH IT IN. WHEN THEY DID THIS THE GEAR UNLOCKED & STARTED TO DROP & THE GEAR CONTROL BREAKER POPPSDR SWAA2014070929840Pump · failedB ELEC HYD PUMP LOW PRESS LIGHT ON SWITCH FAILED. R & R PUMP IAW MM.SDR CHQA20140705207Pump · leakingCREW REPORTED THAT THEY RECEIVED A HYD 1 LOW QTY MSG FOLLOWED BY A HYD SYS 1 FAIL MSG. THE CREW PERFORMED A MANUAL EXTENSION ON THE LG. THE ACFT LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE HYD SYS 1 ENG DRIVEN PUMP & PERFORMED THE LG FREE FALL CHECK. SDR RAIA201407040001Pump · leakingDURING LANDING, LOSS OF HYDRAULIC FLUID FROM SYSTEM 2, FOLLOWED BY HYD 2 LOW QUANTITY, RUDDER SYS 2 INOPERATIVE, AILERON SYS 2 INOPERATIVE MESSAGE. MAINTENANCE INSPECTED AND REPLACED NR 2 ENGINE DRIVEN HYD PUMP, OPS AND LEAK CHECK GOOD.SDR ASAA2014070308458Pump · failedSYSTEM A ENGINE DRIVEN PUMP LOW PRESSURE LIGHT CLIMBING THROUGH 30,000 FT.
ACCOMPLISHED QFR PROCEDURE. CREW DECLARED EMERGENCY AS HYD QTY CONTINUED TO DROP. RETURNED TO DEPARTURE. ACFT GROUNDED. REMOVED A SYSTEM ENGINE DRIVEN PUMP REF AMM 29-11-000-801-SDR 5MFA20140709001Pump · failedTHE LT ENGINE DRIVEN HYDRAULIC PUMP FAILED AND BEGAN DUMPING HYDRAULIC FLUID OVERBOARD. THIS RESULTED IN THE CAVITATION OF BOTH ENGINE-DRIVEN HYDRAULIC PUMPS AND THE FAILURE OF THE MAIN HYD SYSTEM.SDR 5MFA201407140001Bushing · failedENROUTE, LT ENGINE DRIVEN HYD PUMP FAILED AND BEGAN DUMPING HYD FLUID OVERBOARD. RESULTING IN CAVITATION OF BOTH HYD EDP`S AND FAILURE OF THE HYDRAULIC SYSTEM. MX FOUND BUSHINGS THAT THE DRIVE USES AS A BEARINGS, FAILED. BOTH PUMPS WERE REPLACED. OPS CHECKEDSDR 5MFA20140709002Pump · leakingTHE LT ENGINE-DRIVEN HYDRAULIC PUMP FAILED AND BEGAN DUMPING HYDRAULIC FLUID OVERBOARD. THIS RESULTED IN THE CAVITATION OF BOTH ENGINE-DRIVEN HYD PUMPS AND THE FAILURE OF THE MAIN HYD SYSTEM.SDR CA140702004Pump · misinstalled(CAN) ON THE FIRST DEPARTURE AFTER AN ENGINE DRIVEN HYDRAULIC PUMP REPLACEMENT, AFTER SELECTING GEAR UP THERE WAS AN A SYS HYDRAULIC LOW PRESSURE INDICATION WHICH LASTED APPROXIMATELY 30 SECONDS. 10 MINUTES LATER THE HYDRAULIC LOW PRESSURE INDICATION RETURNEDSDR SWIA201438597Pump · failedON APPROACH, WITH FLAPS UP, LOWERED THE GEAR. HYD 3 LOW PRESSURE CAUTION FOLLOWED BY GEAR DISAGREE AND NOSE DOOR WARNINGS. TURNED 3B ON. ALL MESSAGES DISAPPEARED, GEAR LOWERED AND LOCKED NORMAL LANDING. 2800 PSI SHOWS ON HYD 3A. ONLY 3000 PSI SHOWS ON HYD 3B.SDR AALA20140627032Pump · leakingLOSS OF SYS A HYD FLUID. EMER DECLARED FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED NR 1 ENG DRIVEN HYD PUMP THAT WAS LEAKING FROM THE CASE DRAIN. SYS GND CHECKED NORMAL OPERATION CLOSED.SDR CA140627011Pump · failed(CAN) GREEN HYD FAILURE ENROUTE, CARRYING ON TO DESTINATION, DECLARING A PAN PAN ON ARRIVAL. FOUND NR 1 ENGINE GREEN HYD EDP DAMAGED ALSO CAUSING NR 2 ENG GREEN EDP TO BE OVERHEATED. BOTH PUMPS REPLACED TASK 29-00-00-280-092-AAND TASK 29-00-00-280-805-A CARSDR SWIA201438297Pump · failedHYDRALIC NR 1 LOW PRESSURE CAUTION MESSAGE DURING DESCENT. AFTER TURNING ON HYD 1B PUMP PER THE QRH, RECEIVED HYD EDP 1A CAUTION MESSEGE. HYD FLUID RESERVOIR INDICATES 5 PERCENT. R & R NR 1 EDP IAW AMM.SDR CA140620009Pump · failed(CAN) PILOT REPORTED AFTER LANDING THAT DURING FLIGHT HE HAD STRONG VIBRATIONS, HYD PUMP NR 2 CAUTION LIGHT, RESERVOIR NR 2 EMPTY ROOT CAUSE, INSPECTION FOUND NR 2 EDP FAILED.SDR VNAA2014061300011Pump · failedCREW REPORTED, NR 1 HYD SYSTEM FAILED IN FLIGHT WITH NO PRESSURE AND NO FLUID LEVELS. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED REPAIR TO PRESSURE LINE FROM NR 1 ENGINE DRIVEN PUMP AFTER FINDING LINE CHAFED THROUGH AT CLSDR HALA2014061200082Warning Light · false activationC HYD DEM PUMP LIGHT CAME ON DURING DECENT, OVERHEAD LIGHT A EICAS LIGHT. PERFORMED CHECKLIST NO CHANGED SWITCH OFF. PERFORMED OPS TEST OF CTR HYD SYS IAW AMM 263-11-00-175.896 C HYD DEM PUMP OPS CHECKED GOOD. NO FAULTS NOTED.SDR JJBA20140612004Pump · failedNUMBER 1 HYD PX WENT TO ZERO IN FLIGHT & NR 1 ENG HYD PX LIGHT ILLUMINATED. R & R NR 1 HYD PUMP.SDR CALA2014060591219Pump · faultyENGINE 2 EDP LOW PRESS DISPLAYED. YELLOW RESERVOIR QTY IS DECREASING. EDP & PTU SELECTED OFF IAW QRH. ACCOMPLISHED CHECK OF ALL DPI NONE WERE POPPED & NO METAL FOUND IN FILTER. REPLACED ENG CASE DRAIN FILTER IAW MM29-11-43-000-010-A 13 & REPLACED ENG HYD PSDR AALA20140531013Pump · failedORD CREW REPORTED RT HYD QTY DOWN TO ZERO DURING CLIMBOUT. GEAR MANUALLY EXTENDED. EMER DECLARED FLIGHT RETURNED ORD LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT ELEC HYD PUMP & ENG DRIVEN PUMP MPN 3029981001. SYS GND CHECKED NORMAL, OPSDR SAJF2014060303019Pump · leakingHYD 2 QTY LOW HYD QTY DROP TO 0.34 & CONTINUED TO DROP TO 0 BUT PRESS 3080 TEMP 50, 1.5 HRS LATER HYD PRESS ENG 2 MSG CAME ON, TURN OFF EDP, 1 HR 20 MINS BEFORE LD HYD PRESS SYS 2 MSG ON HYD PRESS READ 0. GND CHK FOUND LT WW WING GEAR LCCA SOLENOID VLV & ENG SDR CA140529007Garlock Seal · failed(CAN) SHORTLY AFTER LEVELING OFF AT FL170 NR 1 ENGINE OIL PRESSURE WAS OBSERVED FLUCTUATING, CAUTION LIGHT ILLUMINATED AND THE ENGINE WAS SHUTDOWN. ENGINE HYDRAULIC PUMP GARLOC SEAL REPLACED AND ACFT WAS RETURNED TO SERVICE.SDR SWAA2014060328654Pump · faultyDIVERSION, HYD PUMP TURNED OFF IAW QRH. R & R ELEC 1 B SYS HYD PUMP & ELEC CONNECTOR D2666 IAW AMM.SDR USAA2014052200010Pump · leakingFLIGHT 787, CDG - CLT LOST BLUE HYD SYS PRESS & QTY, CONTINUING TO CLT. DECLARED AN EMERGENCY & THE FLIGHT LANDED UNEVENTFULLY. R & R THE NR 1 ENG BLUE SYS HYD PUMP.SDR USAA2014051600004Pump · malfunctionedON TAKEOFF ROLL ABOVE 80 KNOTS, CREW RECEIVED B SYS HYD LOW PRESS INDICATION. ONCE CREW GOT ACFT CONFIGURED AFTER TAKEOFF THEY NOTIFIED CLT OF INDICATION PROBLEM & ADVISED THEY WERE RETURNING TO FIELD. NO EMERGENCY WAS DECLARED & THE ACFT WAS ABLE TO TAXI TOSDR VQI2014F00014Pump · failedCREW REPORTED AT INITIAL ACCELERATION, CLIMBING THRU 10000 FT, BLUE HYD OVERHEAT AND FAULT W/ASSOCIATED BLUE FLT CONTROL LOSS. CREW RETURNED TO DEPARTURE AND DECLARED AN EMERGENCY. ACFT LANDED WITHOUT INCIDENT AND TAXIIED TO THE GATE UNDER POWER. PROBLEM WSDR USAA2014051500005Pump · leakingTHE CAPTAIN CALLED DISPATCH SHORTLY AFTER TAKEOFF FROM CLT TO REPORT A GREEN HYD SYS LEAK. THE FLIGHT RETURNED TO CLT & LANDED SAFELY. REMOVED THE NR 2 GREEN HYD PUMP. CLEANED PANELS 191AB & 197FB.SDR USAA2014051500004Pump · leakingTHE CAPTAIN CALLED DISPATCH SHORTLY AFTER TAKEOFF FROM CLT TO REPORT A GREEN HYD SYS LEAK. THE FLIGHT RETURNED TO CLT & LANDED SAFELY. REMOVED THE NR 1 GREEN HYD PUMP. CLEANED PANELS 191AB & 197FB.SDR CA140613007Pump · failed(CAN) NR 1 HYDRAULIC SYS OVERHEAT LIGHT CAME ON IN FLIGHT COINCIDING WITH FAILED GENERATOR SDR 20140613006.SDR SWAA2014050527647Pump · failedDIVERSION, DECLARED EMERGENCY. DURING CLIMB OUT A SYS HYD SYS FAILED. R & R NR 3 FLT SPOILER TEST PORT CAP, O RING & ENG DRIVEN PUMP IAW MM.
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