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 JBXA000263Pump · failedNR 1 HYDRAULIC SYSTEM LOST ALL PRESSURE AND FLUID AT 26,000 FEET. RETURNED TO RDU. REMOVED AND REPLACED ALL NR 1 SYSTEM HYDRAULIC FILTERS IAW CRJ AMM 29-11-09, 29-11-40, AND 29-11-46. REMOVED AND REPLACED NR 1 SYSTEM ENGINE DRIVEN HYDRAULIC PUMP IAW CRJ AMMSDR 2001UALA00420Pump · failedON GEAR RETRACTION DURING T/O FROM OGG, AIR DEMAND PUMP LOW PRESS LIGHT CAME ON. DIVERTED TO HNL. *S/D* REPLACED AIR DRIVEN PUMP.SDR AALA20010670Pump · leakingDFW - FLT 320 - EN ROUTE DFW-DEN, DETECTED RIGHT SIDE HYDRAULIC PUMP FAILURE DURING CLIMB-OUT. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED RIGHT SIDE HYDRAULIC PUMP. SERVICED HYRAULIC SYSTEM. RAN ENGINES. LEAK CHECKS GOOD. SYSTEM GROUND CHSDR DL72S010523Pump · failedDURING CLIMB CHECK SWITCHED THE NR 1 B ELECTRIC PUMP OFF AND NOTICED PRESSURE FLUCTUATION ON B SYSTEM GUAGE. TURNED NR 1 ELEC PUMP BACK ON AND SEVERAL SECONDS LATER LOW NR 1 PUMP LOW PRESSURE LIGHT ILLUMINATED AND SYSTEM PRESSURE DROPPED TO 2200 PSI- UPON EXSDR DHL2001720009Pump · failedDURING PREDEPARTURE NR 2 HYD B SYS PUMP INOP. CORRECTIVE ACTION: REPLACED NR 2 HYD ''B'' SYSTEM ELECTRIC PUMP AND RESET NR 2 HYD PUMP FAULT DETECTOR. OPS CK GOOD IAW MM 29-12-11, MM 29-12-0, WDM 29-21-01.SDR 20010503CW002Pump · defectiveFLUID CONTAMINATION IN RIGHT ENGINE PUMP WAS THE LATEST MODEL AND WAS NEW AT INSTALLATION AND HAS ONLY BEEN OPERATED FOR 48.4 HOURS. WE ARE GETTING BETTER TIME OUT OF THE OLD STYLE PUMPS.SDR USAASB01096Pump · leakingMIA - FLT 1975 - EN ROUTE FROM CLT TO MBJ, FLYING OVER CUBA, CAPTAIN REPORTED THAT THE NR 1 ENGINE HYDRAULIC PRESSURE LIGHT FLICKERED AND THAT HE WAS LOSING A-SYSTEM HYDRAULIC FLUID. THE FLIGHT WAS 45 MINUTES FROM MBJ OR MIA, AND AFTER DISCUSSION, CAPTAIN AGRSDR 20010427CW009Pump · unserviceableHYDRAULIC PUMP CASE DRAIN FILTER SAMPLES FOR LEFT ENGINE DID NOT PASS THE PATCH TEST. REPLACED PUMP WITH SERVICEABLE UNIT, BLED AIRCRAFT SYSTEMS AND RETURNED AIRCRAFT TO SERVICE. WE WILL CONTINUE SAMPLE SYSTEM FLUID AS REQUIRED.SDR 20010514SG006Pump · failedLANDING GEAR DID NOT DEPLOY NORMALLY. EMEREGNCY BLOW DOWN PROCEDURES EMPLOYED PER ROTORCRAFT FLIGHT MANUAL. HYDRAULIC PUMP MOTOR FAILURE CAUSED LACK OF PRESSURE TO OPERATE GEAR. DATE OF LAST INSPECTION WAS FEB 25, 2000. TYPE OF LAST INSPECTION WAS OVERHAULSDR MWEA010391Pump · inoperativeLEFT HYDRAULIC QUANTITY DROPPED TO 1 1/2 QUARTS IN FLIGHT, LEFT ENGINE DRIVER HYDRAULIC PUMP LEAKING. REPLACE LEFT ENGINE DRIVEN HYDRAULIC PUMP.SDR AU010267Coupling · cracked(AUS) NR 1 HYDRAULIC SYSTEM HYDRAULIC PUMP PRESSURE LINE ELBOW COUPLING THREADED SECTION CRACKED AND LEAKING. LOSS OF HYDRAULIC FLUID.SDR JBXA000260Pump · leakingHYDRAULIC NR 2 LOW PRESSURE IN FLIGHT AIR-RETURN TO RDU. REMOVED AND REPLACED NR 2 HYDRAULIC ENGINE DRIVEN PUMP AND HIGH PRESSURE RETURN LINE IAW CRJ AMM 29-11-52. LEAK AND OPS CHECK GOOD.SDR 20010424CW007Pump · inoperativePILOT REPORTED HYDRAULIC LIGHT ILLUMINATION DURING FLIGHT, IMMEDIATELY SHUT DOWN HYDRAULIC SYSTEM. ON THE GROUND, PILOT STARTED THE AIRCRAFT FOR MAINTENANCE RUN AND HOVERED THE AIRCRAFT FEELING FULL HYDRAULIC CONTROL. MECHANICS REMOVED HYDRAULIC PUMP AND REPSDR CA010503007Pump · failed(CAN) THE FLIGHT CREW REPORTED THAT THE C.B. FOR THE AC HYDRAULIC PUMP COOLING FAN POPPED WHEN THE AC PUMP WAS SELECTED ON. THE FAN WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE FAN HAD BEEN IN SERVICE FOR 62 DAYS, 512 HOURS, AND 311 CYCLES SINCE SDR 20010328CW012Belt · separatedHYDRAULIC BELT FAILED AT BOND LINE DURING FLIGHT WHICH LEAD TO PRECAUTIONARY LANDING. BELT CONDITION AND TENSION APPEARED NORMAL DURING PREFLIGHT.SDR AU010242Pump · leaking(AUS) NR 2 HYDRAULIC SYSTEM ENGINE DRIVEN PUMP SILENCER LEAKING INTERNALLY.SDR CA010313015Pump · failed(CAN) HYDRAULIC PUMP FAILED CAUSING FAILURE OF NR 1 HYDRAULIC SYSTEM.SDR USAAD01042Pump · failedMHT-PIT - FLT 1770 - DURING CLIMB-OUT, THE RIGHT HYDRAULIC PRESSURE DROPPED FOLLOWED BY THE LEFT HYDRAULIC PRESSURE. THE ALTERNATE GEAR EXTENSION WAS USED. THE AIRCRAFT LANDED WITHOUT INCIDENT AND WAS TOWED TO THE GATE. MAINTENANCE REPLACED THE RIGHT ENGINESDR 2001UALA00390Pump · failedAFTER T/O DURING FLAP RETRACTION A LOUD METAL ON METAL SOUND WAS HEARD THROUGHOUT THE ACFT. THIS NOISE CONFIRMED BY FLT CREW WHILE FLAPS IN MOTION AND CEASED IMMEDIATELY WHEN FLAPS STOPPED. *S/D* INTERNAL FAILURE OF CENTER HYDRAULIC SYSTEM AIR DRIVEN PUMP (SDR AALA20010363Pump · leakingBOS - FLT 1859 - EN ROUTE BOS-DCA, SHORTLY AFTER TAKEOFF BROUGHT GEAR AND FLAPS UP. FLAPS STOPPED AT SIX DEGREES. LOST HYDRAULIC PRESSURE. RETURNED BOS AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 1 ENGINE HYDRAULIC PUMP. LEAK CHECKS GOOD. SYSTEM GROUSDR AALA20010280O-Ring · leakingSTL - FLT 1618 - EN ROUTE STL-LGA - DETECTED NR 1 HYDRAULIC SYSTEM SLOWLY DECREASE TO TWELVE PERCENT. ON FINAL APPROACH NR 1 HYDRAULIC SYSTEM LOW LIGHT ILLUMINATED. LANDED JFK WITHOUT FURTHER INCIDENT. REPLACED NR 1 SYSTEM ENGINE HYDRAULIC PUMP O-RING. SYSSDR RAIA00102007O-Ring · leaking7145-MEM- CREW REPORTS LOSS OF BLUE SYSTEM HYDRAULIC PRESSURE ON DESCENT. MAINTENANCE INSPECTED AND REPLACED O-RING SEAL AT BLUE SYSTEM HYDRAULIC PUMP.SDR AALA20010333Pump · leakingORD - FLT 2353 - EN ROUTE ORD-JAC, SHORTLY AFTER TAKEOFF DETECTED HYDRAULIC QUANTITY QUICKLY DROP TO ZERO. RETURNED ORD AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 1 ENGINE HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR 20010406CW004Cover · crackedCOVER HAS A CRACK FROM THE EDGE OF THE CENTER HOLE OUT TO THE EDGE OF THE COVER.SDR CA010307016Pump · cracked(CAN) IN CRUISE AT FL300, HYDRAULIC SYSTEM C, LOST OF PRESSURE, EDP SHUT-OFF ACTIVATED BY FLIGHT CREW AND GEARS EXTENDED USING MANUAL SYSTEM. MAINTENANCE FOUND A 7.5 INCH CRACK IN EDP CASING, EDP REPLACED AND AIRCRAFT RETURNED TO SERVICE. PART IS AVAILABLE.SDR JBXA000246O-Ring · wornSYSTEM NR 1 HYDRAULIC QUANTITY INDICATED 25 PERCENT. REMOVED AND REPLACED O-RINGS ON ENGINE DRIVEN PUMP IAW SERVICE BULLETIN NR 887055-29-04. SERVICED HYDRAULICS, OPS CHECK AND LEAK CHECK GOOD.SDR CA010305005Pump · worn(CAN) AFTER START HYDRAULIC PRESSURE WAS AT 0. PUMP REPLACED AND IT WAS FOUND THAT THE DRIVE SPLINES WERE WORN OUT ON THE HYDRAULIC PUMP. PUMP SPLINES ARE SOFTER THAN THE ENGINE DRIVE.SDR 2001UALA00114Pump · overheatedBLUE SYSTEM HYDRAULICS ELECTRIC PUMP OVERHEATED. *S/D* REPLACED BLUE SYSTEM ELECTRIC HYDRAULIC PUMP. SYSTEM CHECKS NORMAL.SDR AALA20010190Pump · leakingLGA - FLT 708 - EN ROUTE DFW-LGA, SHORTLY BEFORE ARRIVAL LEFT SIDE HYDRAULIC QUANTITY DECREASED TO ZERO. HYDRAULIC PRESSURE DECREASED. LANDED LGA WITHOUT FURTHER INCIDENT. REPLACED LEFT SIDE HYDRAULIC PUMP. ACCOMPLISHED LEAK CHECK PER THE MM. NO LEAKS NOTSDR USAASB01029Pump · failedCLT - FLT 1633 - EN ROUTE FROM IAH-PHL, THE ''A'' HYDRAULIC SYSTEM LOW PERSSURE LIGHT ILLUMINATED ALONG WITH ''A'' HYDRAULIC QUANTITY READING BELOW QUARTER. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE RSDR SIMA0262Pump · failedMIA - FLT 5339 - CREW REPORTED AFTER TAKEOFF, THE LANDING GEAR WOULD NOT FULLY RETRACT. CREW ALSO REPORTED A THUMPING NOISE AND RECEIVED A LEFT MLG UNLOCK LIGHT. CREW RETURNED TO MIA AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE GREEN SYSTEM HYDRASDR 20010227CW005Powerpack · inoperativeWHEN LANDING GEAR WAS SELECTED DOWN, GEAR DID NOT EXTEND. EXTENDED LANDING GEAR USING EMERGENCY PROCEDURES. GEAR EXTENDED AND LOCKED. LANDING MADE WITHOUT INCIDENT. FOUND HYDRAULIC POWER PAK MOTOR INOPERATIVE. INSTALLED OVERHAULED HYDRAULIC POWER PAK. GESDR AALA20010142Pump · failedDFW - FLT 1431 - EN ROUTE DFW-ONT, DETECTED NR 1 ENGINE HYDRAULIC PUMP FAILURE. AIR INTERRUPTED, RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 1 SIDE ENGINE HYDRAULIC PUMP. ACCOMPLISHED LEAK CHECK. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORSDR MWEA010107Pump · inoperativeRIGHT HYDRAULIC PRESSURE WENT TO ZERO AND RIGHT HYDRAULIC PRESSURE LOW LIGHT CAME ON WHEN AUXILLARY HYDRAULIC PUMP WAS TURNED OFF. REMOVED AND REPLACED RIGHT HAND ENGINE DRIVEN HYDRAULIC PUMP.SDR 20010216SG008Pump · leakingWHILE AT CRUISE, THE CREW OBSERVED NR 2 HYD SYSTEM QTY WAS LOW. CREW MONITORED NR 2 HYD SYSTEM QUANTITY AND TEMPERATURE, HYD TEMP ROSE ABOVE 135 DEGREES CELSIUS AND QUANTITY DEPLETED TO ZERO. CREW SHUT DOWN NR 2 ENGINE PER CNDAIR ''QUICK REF HANDBOOK'' ABNORSDR USAASB01007Pump · failedPIT - FLT 9228 - DURING CRUISE, EN ROUTE FROM YUL-YYZ, THE NR 2 ELECTRIC HYDRAULIC PUMP OVERHEAT LIGHT ILLUMINATED. DECISION WAS MADE FOR FLIGHT TO DIVERT TO PIT. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DELCARED. MAINTENANCE REMOVED AND REPLACED TSDR ANCF200100005Pump · failedDURING FLIGHT FROM FRA TO SJU RH EDP HYD LOW PRESSURE CAME ON, FLIGHT PROCEDED TO BAQ. RT EDP WAS REPLACED IAW AMM 29-11-05, TEST WAS SATISFACTORYSDR AALA20010020Pump · leakingLAX - FLT 181 - EN ROUTE BOS-LAX, DETECTED RIGHT SIDE HYDRAULIC QUANTITY LOSS. LANDED LAX WITHOUT FURTHER INCIDENT. REPLACED RIGHT SIDE HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR MWEA010026Pump · inoperativeRIGHT HYDRAULIC PRESSURE AND FLUID SHOWED ZERO AFTER TAKE OFF. -- REPLACED BROKEN HYDRAULIC LINE FROM AUX GEAR PUMP. REPLACED AUXILIARY ELECTRIC PUMP AND ENGINE DRIVEN PUMP.SDR SWA002785Module · inoperativeDIVERSION, LOST NR 1 & NR 2 ENG DRIVEN HYD PUMPS, LOW PRESS LIGHTS ILLUMINATED. PRESS AND QUANTITIES REMAINED NORMAL. REMOVED AND REPLACED RESERVOIR PRESS MODULE, OPS CHECK GOOD. LEAK CHECK GOOD AND CHECKED CASE DRAIN FILTERS PER MM.SDR CA010118007Pump · overheated(CAN) FOLLOWING LT ENGINE RELIGHT HYDRAULIC HIGH TEMPERATURE CAUTION MESSAGE HYDTEMP 135 DEGREES C. AFTER FOUR MINUTES PRESSURE +/- 3750 P.S.I., LEFT ENGINE SHUT DOWN. LANDING CARRIED OUT SINGLE ENGINE.SDR CA010110023Gear · failed(CAN) BURR ON GEAR FACE CAUSED DAMAGE TO THE BEARING.SDR SWIA972206Pump · failedCLIMBING OUT OF SLC HYDRAULIC ''LOW LEVEL'' LIGHT GAUGE SHOWED IN YELLOW TRENDING TO EMPTY. ALSO ''LOW PRESS H'' ON HYDRAULIC PANEL. RETURNED TO SLC FOR NORMAL LANDING, GEAR AND FLAPS OPS NORMAL. REPLACED LEFT ENGINE DRIVEN HYDRAULIC PUMP IAW 29-10-03. SERVSDR DHL2000801157Pump · unserviceableUPON EXECUTING HORIZONTAL STABILIZER BEFORE TAXI FLOW, CAPT FOUND NR 2 HYDRAULIC PUMP INOP. R&R ENGINE DRIVEN HYD PUMP & CASE DRAIN FILTER. OPS CHECKED OK PER M/M 29-10-15.SDR SWIA972195Pump · failedLEFT MAIN HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATES IN FLIGHT. REFERRED TO QRH. RETURNED TO LAX FOR LANDING. REPLACED LEFT ENGINE HYDRAULIC PUMP WITH SERVICEABLE UNIT, CHECKED GOOD. NO LEAKS. SN OFF MA575897 SNON: MX521768. ALSO REMOVED INSPECTSDR AC2A072802Pump · malfunctionedPSI ABOVE 1600 AT 10 DEGS. OAT. REPLACED PUMPSDR COMA0061056Pump · failedLeft engine low hydraulic pressure message. Replace the left engine hydraulic pump.SDR MWEA001238Pump · inoperativeDURING TAKE-OFF RIGHT HYDRAULIC TEMP HIGH LIGHT CAME ON. TAKE-OFF ABORTED. -- REPLACED ELECTRIC HYDRAULIC PUMP.SDR AU001194Pump · leaking(AUS) RT ENGINE DRIVEN HYDRAULIC PUMP LEAKING FLUID FROM BETWEEN PARTING FACES. INVESTIGATION FOUND THAT A CHECK VALVE IN THE RT HYDRAULIC PUMP BYPASS LINE WAS BLOCKED BY DEBRIS FROM PREVIOUS PUMP FAILURES CAUSING A BUILDUP OF PRESSURE ACROSS THE PUMP WHICH COSDR 20001219SH002Pump · wornFLUID SAMPLE TAKEN AT 100-HOUR INTERVAL SHOWS THE PUMP NEEDED TO BE REPLACED. REPLACED PUMP, WILL CONTINUE TO TAKE FLUID SAMPLES AT 100-HOUR INTERVALS AND CHANGE PUMPS AS REQUIRED. AIRCRAFT TOTAL TIME 640.8 HOURS. TOTAL CYCLES 347. (X)
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