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 6JPA20121212001Pump · failedUPON STOPPING THE AIRCRAFT ON THE RAMP TO PARK AT THE FBO AT KLNS (LANCASTER PA) THE HYDRAULIC PUMP FAILED AND BLEW THE HYDRAULIC POWER ELECTRICAL FUSE. MAINTENANCE CREW REMOVED AND REPLACED THE HYDRAULIC POWER PACK ASSEMBLY AND ELECTRICAL FUSE IAW PHENON 100SDR SWIA201230995Pump · failedRECEIVED GEAR DISAGREE MESSAGE AFTER SELECTING GEAR UP. (FLT 4513) REPLACED NR 3B HYDRAULIC SYSTEM ACMP. P/N: 848847, S/N OFF: MX665217.SDR ASOA201201777Pump · leakingDURING FLIGHT, LOST ALL HYD SYS 2 PRESSURE AND QTY WENT DOWN TO 5 PERCENT. DIVERTED, AFTER RUNNING QRH. EMERGENCY DECLARED. FOUND O-RING LEAKING FROM NR 2 HYD RESERVOIR. R & R NR 2 HYD RESERVOIR O-RING IAW AMM 29-11-30. R & R EDP IAW AMM 29-11-01. OPS ASDR SWIA201230948O-Ring · leakingHYDRAULIC FLUID LEAKING AND HYDRAULIC 3 LOW CAUTION MESSAGE. (FLT 5198) REPLACED NR 3 HYDRAULIC PUMP O-RINGS IAW CMM.SDR ASOA20120606041Pump · failedNR 1 HYD PUMP FAILED AND LOST ALL HYD FLUID IN FLIGHT. R & R NR 1 ENGINE DRIVEN HYD PUMP IAW AMM 29-10-03, LEAK AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR AALA20120606006Pump · inoperativeYYC - CREW REPORTED LOSS OF LEFT HYDRAULIC SYSTEM QUANTITY WITH NO PRESSURE. EMERGENCY DECLARED FLIGHT LANDED YYC WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE DRIVEN HYDRAULIC PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.SDR UALA2012060403085Pump · malfunctionedAIR RETURN TO DEPARTURE FOR HYDRAULIC PUMP PROBLEM. UNABLE TO CONTROL, DEPRESSURE LT HYD PUMP. HYD PUMP REPLACED.SDR AALA20120604001Pump · failedEZE - CREW REPORTED RIGHT ENGINE DRIVEN HYDRAULIC PUMP FAILED. HYDRAULIC PRESSURE AND TEMPERATURE INDICATIONS WERE HIGH. EMERGENCY DECLARED FLIGHT LANDED EZE WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE DRIVEN HYDRAULIC PUMP. SYSSDR VNAA2012060100001Pump · failedCREW REPORTED HYDRAULIC SYSTEM TWO (2) AT ZERO PSI AND ZERO PERCENT IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED NUMBER TWO (2) EDP (ENGINE DRIVEN PUMP) AND PERFORMED CHECKS USING AIRCRAFT MAINTSDR REXA2012052900798Pump · leakingHYDRAULIC SYSTEM PUMP 3B LEAKING AND FOLLOWED WITH LOW CAUTION MESSAGE. MANUALLY EXTENDED GEAR FOR LANDING. EMERGENCY DECLARED. ALL OPS CHECK GOOD. REMOVED AND REPLACED HYDRAULIC SYSTEM NR 3B. OP CHECK LEAK CHECKED GOOD IAW AMM 29-12-00. OK FOR SERVICESDR CA120608008Pump · failed(CAN) INFLIGHT, THE CREW RECEIVED A HYD SYS 2 LOW PRESS EICAS MESSAGE. THE CREW DECLARED AN EMERGENCY AND PERFORMED AN UNEVENTFUL LANDING WITH ARFF STANDING BY. MAINTENANCE REPLACED THE NR 2 ENGINE DRIVEN PUMP, EDP, IAW AMM 29-11-01 AND AFTER AN OPS CHECK THESDR SIMA20120528003Pump · inoperativeON FLIGHT 3832, THE CREW REPORTED THAT WHILE ON DESCENT THEY RECEIVED A HYDRAULIC 2 LOW PRESSURE CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. AIRFCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ENGINE DRIVEN HYDRAULIC PUMP PER ASDR SIMA20120527001Pump · inoperativeON FLIGHT 3549, AFTER CLIMB OUT, CREW REPORTED THEY RECEIVED HYD 1 LOW QUANTITY MESSAGE AND THEN RECEIVED AN E1 HYD PUMP FAIL MESSAGE. THE CREW DECLARED AN EMERGECNY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED SDR CVGA20120529001Pump · failedNR 1 HYD HIGH TEMP CAS ILLUMINATED IN-FLIGHT, JUST PRIOR TO DESCENT. MAX TEMP 98C, TEMP WAS NORMAL PRIOR TO LANDING.SDR SWIA201230829Pump · failedRECEIVED GEAR DISAGREE WARNING ALONG WITH MAIN GEAR INDICATING UP AND NOSE GEAR INDICATING RED DISAGREE. (FLT 5267) REPLACED HYDRAULIC PUMP 3A IN REFERENCE TO AMM. P/N 848847 S/N OFF MX679140.SDR REXA2012052300624Pump · malfunctionedON TAKEOFF ROLL AT 80 KTS, RECEIVED HYD 3 LOW PRESSURE CAUTION. CONTINUED TAKEOFF, HAD A GEAR DISAGREE CAUTION THEN GEAR UNSAFE WARNING, & NOSE DOOR WARNING. AFTER ABOUT 15 SECONDS HYD PRESSURE WAS RESTORED AND WARNINGS AND CAUTIONS CLEARED. REPLACED NR 3SDR YENA20120520504Pump · damagedFLT 1208 RSW-HPN, AIRCRAFT DIVERTED TO MCO DUE TO HYD 2 EDP FAIL ON EICAS. REMOVED AND REPLACED NR 2 ENGINE DRIVEN PUMP IAW AMM 29-11-01. OPS AND LEAK CHECK GOOD. NOTE: REMOVED PUMP HAD A HOLE IN IT.SDR SWIA201230736Pump · failedRECEIVED A HYD 2 LOW PRESSURE MESSAGE. (FLT 4792) REPLACED NR 2 ENGINE DRIVEN HYDRAULIC PUMP AND NR 2 HYD CASE DRAIN FILTER. PN OFF: 887055 SN: MX644744A.SDR CA120511002Pump · failed(CAN) EMERGENCY DECLARED DUE TO HYDRAULIC 2 EDP FAIL. EICAS HYD 2 LOW QTY IN CRUISE . HYD FLUID UPLIFT CARRIED OUT AFTER HYD PUMP REPLACED.SDR UALA2012051002699Pump · leakingLOST ALL HYD QUANTITY ON LEFT SIDE ON SHORT FINAL. LT ENGINE PUMP LOW PRESSURE LIGHT FLICKERED FOLLOWED BY LT SYSTEM LOW PRESSURE LIGHT. BOTH LT ENGINE AND LT ACMP SHUTOFF. AFTER LANDING LT REVERSER DID NOT OPERATE BUT STEERING OPS NORMAL. LT QTY AFTER PARSDR UALA2012051002681Pump · failedNOSE WHEEL STEERING SYS UNRESPONSIVE THRU TILLER PROG TEXT. REPLACED CHECK VALVE ELECTRIC PUMP. SERVICED YELLOW HYD SYSTEM TO FULL. OPS CHECKED NORMAL. REF AMM 29-2 4-21.SDR UALA2012051002708Pump · malfunctionedWITH LEFT ELECTRIC HYDRAULIC PUMP SELECTED, SYSTEM PRESSURE LIGHT IS ON. REPLACED PUMP, OPS CHECKED OK.SDR UALA2012050802657Pump · failedRT ENG HYD PUMP OVERHEAT LIGHT ILLUMINATED ON TAKEOFF. CREW SELECTED ENG PUMP SWITCH TO OFF AND LIGHT WENT OUT. FLIGHT DIVERTED. REPLACED RT ENG HYD PUMP ASSY PER AMM. ALSO REPLACED RH SYS CASE DRAIN AND PRESS FILTERS PER AMM. NO LEAKS NOTED.SDR YENA20120505491Pump · leakingFLT 1242 CLT-BOS, CREW DECLARED EMERGENCY DUE TO HYDRAULIC 2 LOW PRESSURE IN FLIGHT. RAN QRC/QRH, AIRCRAFT WAS TOWED TO THE GATE DUE TO HYDRAULIC SYSTEM 2 LOSS. REMOVED AND REPLACED NR 2 ENGINE EDP PER AMM 29-11-01. REMOVED AND REPLACED NR 2 HYD SYS PRESS, SDR UALA2012050402644Pump · failedCREW REPORTS LEFT ENG HYD PUMP FAILED AND LEFT SYSTEM FLUID QTY IS AT 65 PERCENT. REPLACED LEFT ENGINE DRIVEN PUMP PER AMM.SDR UALA2012050402641Switch · faultyLEFT ELECTRICAL HYD SWITCH DOES NOT SHUT SYSTEM OFF. REPLACED LT HYD PUMP SWITCH CAP AND MASTER MODULE. PRESSURE LIGHT IS NOW SOLID AND PUMP OPERATION AND INDICATIONS ARE ALL CORRECT.SDR CA120426007Pump · leaking(CAN) ON SCHEDULED APPROACH IN DESCENT INTO BASE, THE CREW NOTED LOSS OF NR 2 HYDRAULIC FLUID. ALTERNATE EXTENSION REQUIRED AND UNEVENTFUL LANDING. UPON INVESTIGATION OF FLUID LOSS IT WAS NOTED THE NR 2 EDP CASE WAS FOUND LEAKING. EDP TO BE REPLACED.SDR AALA20120417005Pump · leakingLIM - CREW REPORTED LEFT HYDRAULIC SYSTEM QUANTITY LOSS. EMERGENCY DECLARED FLIGHT LANDED LIM WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND FLUID LEAKING FROM LEFT ENGINE DRIVEN PUMP.SDR UALA2012041502285Pump · leakingNR 1 ENGINE HYDRAULIC PUMP CASE DRAIN LEAKING 12 DROPS PER MIN LIMIT IS 6 DPM PER MM. CHANGED PUMP IAW MM 29- 11-05. STILL LEAKING HYD FLUID FROM PUMP CASE DRAIN LINE. WHILE ENG RUNNING LEAK IS AT 50 DROPS PER MINUTE. NOT RUNNING LEAK IS AT 25 DROPS PER MISDR UHLA2012041400127Pump · leakingWHILE AT CRUISE ALT FL340 APPROX 1 HOUR INTO FLIGHT, EICAS MESSAGE HYD 3 QTY LOW APPEARED. PULLED UP HYD PAGE ON MFD AND QTY WAS AT 16 PERCENT. ATC DECLARED EMERGENCY AFTER BEING NOTIFIED. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ACMP 3A IAW EMB 170 MSDR UALA2012041202193Pump · leakingNR 1 ENGINE HYDRAULIC PUMP HAS EVIDENCE OF A HYD LEAK. CLEANED AREA MOTORED ENGINE CHECKED HYD PUMP AND FITTINGS, NO LEAKS NOTED.SDR AALA20120411022Pump · failedINFLIGHT, CREW REPORTED LOSS OF LEFT HYDRAULIC SYSTEM FLUID. EMERGENCY DECLARED FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE DRIVEN PUMP. SYSTEM GROUND CHECKED NORMAL.SDR REXA2012041000491Pump · failedHYDRAULIC 3 LOW PRESSURE CAUTION MESSAGE DURING GEAR EXTENSION. CAME ON FOR 5 SECONDS AND WENT AWAY. 2900 PSI SHOWING 65 PERCENT 35C. GEAR SEEMED TO TAKE LONGER THAN NORMAL TO EXTEND AND RT MAIN WAS LAST TO LOCK DOWN. REMOVED AND REPLACED HYD PUMP 3B IAW ASDR P5CA2012040900024Pump · overheatedNR 1 HYDRAULIC SYSTEM OVERHEAT USING EDP, ADP TURNED ON, ALL FLUID EVENTUALLY LOST FROM NR 1. FOUND EDP TO BE OVERHEATED, INOPERATIVE AND LEAKING. REPLACED EDP AND CORRELATED FILTERS.SDR UALA2012040502110Pump · leakingNR 2 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. REPLACED NR 2 ENGINE DRIVEN PUMP PER MM.SDR JJBA20120405002Pump · failedAFTER TAKEOFF, THE NR 2 ENGINE HYD PUMP CAUTION LIGHT ILLUMINATED AND THE NR 2 HYD SYS LOST PRESSURE AND ALL ASSOCIATED EQUIPMENT DID NOT WORK. THE CREW RETURNED TO FIELD. THE GROUND CREW REPLACED THE NR 2 ENGINE DRIVEN HYD PUMP. A SATISFACTORY OPERATIONALSDR ASOA201201012Pump · failedHYD SYS 1 HAS LOW PRESSURE IN FLIGHT. EMERGENCY DECLARED. R & R ENGINE DRIVEN PUMP ON SYS 1A IAW AMM 29-11-01. OPS AND LEAK CHECKED GOOD.SDR J7SA20120323001Pump · failedAMBER HYD NR 2 HI TEMP CAS MESSAGE INFLIGHT. REPLACED NR 2 HYD EDP.SDR CA120322001Pump · failed(CAN) AFTER SUCCESSFUL GROUND TEST OF ACCUMULATORS AT 70 PERCENT NG, AND ENGINE BROUGHT UP TO FLIGHT IDLE, HORN AND LOW HYDRAULIC PRESSURE LIGHT ILLUMINATED AND LOSS BOOSTED CONTROL WAS NOTED BY FLIGHT CREW. ACFT SHUTDOWN. SUBSEQUENT INSPECTION FOUND HYD PUMSDR YENA20120319460Pump · leakingFLT 696 MCO-DCA, 100 MILES SOUTH OF RDU AT FL 370 CASS "HYD 2 LO QTY" APPEARED WITH 22% QTY REMAINING. QTY EVENTUALLY WENT TO ZERO / NO OTHER INDICATIONS. UPON GEAR EXTENSION CASS "HYD 2 ELEC PUMP FAIL" ILLUMINATED. GEAR AND FLAPS CAME DOWN NORMALLY, APPROASDR CALA2012031900198Pump · leakingTHE NR 1 "ONE" ENGINE HYD LOW PRESS, LOSS OF SYSTEM FLUID TO 18 %. T/S PER FIM 29-30-00-810-812, FOUND 1 ENG EDP CASE DRAIN QUICK DISCONNECT NOT CONNECTED, CONNECTED QUICK DISCONNECT, R&R''D HYD PUMP & PRESSURE, SUPPLY AND CASE DRAIN HOSES PER MM 29-11-1 1, CSDR REXA2012031700395Pump · malfunctionedTAKEOFF FROM P/NS 15-20 MINUTES IN FLIGHT, RECEIVED 3B CAUTION MSG. WRH COMPLETED AND 3B WAS TURNED OFF ABOUT 20 MINUTES LATER BEGAN TO RECEIVE INTERMITTANT HYD 3 LO PRESSURE MSGS. THE PRESSURE THEN RETURNED TO NORMAL. THE GEAR WAS PUT DOWN FOR LANDING AND TSDR HNAA2012031400689Pump · inoperativeDURING CRUISE, NR 2 HYD PUMP CAUTION LIGHT ILLUMINATED WITH ZERO QTY. ENGINE OPERATED APPROX 30 MINUTES DURING RETURN TO FIELD. NO HYD PUMP HOT LIGHT ILLUMINATED. R & R FORWARD FITTING O-RING AT PRESSURE MANIFOLD. INSPECTED DELT- P FOR BYPASS. NONE FOUND. SDR CA120402007Pump · leaking(CAN) LOSS OF NR 2 HYD QTY WHEN GEAR WAS SELECTED DOWN FOR APPROACH. MAINTENANCE FOUND NR 2 EDP LEAKING. REPLACED EDP AND FLUSHING PERFORMED.SDR SIMA201207301Pump · failedON FLIGHT 4127 THE CREW REPORTED THAT WHILE EN ROUTE TO YUL RECEIVED AN E1 HYDRAULIC PUMP FAIL MESSAGE. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND HYDRAULIC LEAK ON EDP 1 FLANGE. REPLACED HYDRASDR UALA2012030901541O-Ring · leakingAT DEPARTURE TIME RAMP REPORTS HYDRAULIC LEAK NR 2 ENGINE. FOUND RIGHT ACMP HYD PUMP LEAKING FROM DRAIN PLUG. REPLACED O-RING, LEAK CHECKED GOOD, SERVICED RT SYS.SDR CA120306001Pump · failed(CAN) AROUND 60 SECONDS AFTER LANDING THE NR 3 HYD PUMP CAUTION LIGHT CAME ON. THE QRH CHECKLIST WAS EXECUTED WITH NO ACTION REQUIRED. TO CHECK THE SYS, CREW ACTIVATED THE NR 3 ISOLATION VALVE TO SEE HOW MUCH PRESSURE WAS IN THE NR 3 SYS. THE NR 3 SYS QUICKLYSDR QMLA2012030112048Bolt · failedDURING AIRWORTHINESS CHECK, A BOLT WAS DISCOVER UNSECURED ON THE TRANSMISSION DECK JUST FWD OF THE MAIN GEAR BOX DIRECTLY BELOW THE PART THAT WAS REPLACED. VISUAL EXAMINATION DISCOVERED THAT THE BOLT HAD ORIGINATED FROM THE FORWARD GEAR DRIVEN HYD PUMP. WAS SDR REXA2012022700284Pump · malfunctionedHYD PUMP 3A CAUTION ILLUMINATED. RESET HYD PUMP 3A IAW AMM 29-10-10.SDR HNAA2012022800628Pump · failedON ENGINE START NR 2 HYD QTY WENT BELOW MIN DISPATCH. TRANSFER FLUID FROM NR1 TO MEET MIN ON GEAR RETRACTION, NR 2 ENGINE HYD PUMP CAUTION LIGHT ILLUMINATED. ON GEAR EXTENSION NR 2 ENGINE HYD PUMP NR 2 RUDDER HYD AND RUDDER FULL PRESSURE CAUTION LIGHT ILLUMI
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