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 ASOA05748Pump · malfunctionedDURING DESCENT INTO CRW FROM ATL, AT APPROXIMATELY 20,000 FEET THE CREW RECEIVED A 3A HYD LOW PRESS CAUTION MESSAGE. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT DIVERTED TO TRI AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THSDR CA050915003Drive Shaft · sheared(CAN) ON CLIMB-OUT, THE NUMBER 1 ENGINE DRIVEN HYDRAULIC PUMP FAILED AND AIRCRAFT RETURNED TO DEPARTURE AIRPORT. THE NUMBER 1 HYDRAULIC PUMP AND HYDRAULIC RETURN FILTER WERE REPLACED (SHAFT SHEARED ON PUMP) AND AIRCRAFT WAS RETURNED TO SERVICE. TIME SINCE LASDR MALA050714Pump · failedCREW SENT ACARS ABOUT LOSING GREEN HYD SYS. RESPONDED BY SAYING YELLOW HYD SYS HOT. DECLARED EMERG & LANDED. REPLACED NR 3 ENG EDP & C/W FCA29004. NO LEAKS NOTED. PERFORMED GREEN HYD SYS CHECK FOR 50 MIN. NO DEFECTS NOTED. DISC NR 1 FOR GREEN SYS HIGH TEMSDR FE5F200500002Housing · crackedTHE A/C, LOST BOTH HYD PRESS (BOTH PRESS 0) WHILE TOUCH DOWN AND USE REVERSE THRUST(BOTH SIDE HYD QTY NORMAL.L:15, R:17 PROCEED QRH(L/R)HYD PRESS LOW PROCEDURE:TRANS PUMP SW OFF CHECK PRESSURE AND QTY NORMAL.TAXI BACK TO GATE. ENGINEERS VISUAL CHECKED, FOUND SDR DJFA2005135Pump · wornTHE CREW REPORTED THAT THE HYDRAULIC PRESSURE WAS READING HIGH IN FLIGHT. WHEN THE HYDRAULIC PRESSURE DROPPED TO ZERO THE CREW CLOSED THE EMERGENCY DUMP VALVE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS DIVERTED TO KSAN DUE TO THE HIGHER RUNWAY LENGTH INSDR 05FDEA02597Pump · malfunctionedAT CRUISE FL 340 GOT (HYD 3 ELEV OFF) LEVEL 1 ALERT. NR 3 QTY DECREASED SLOWLY TO 3.2 GAL. THEN GOT (HYD 3 OFF) LEVEL 1 ALERT. PUMPS TURNED OFF AND QUANTY STABILIZED AT 3.6. AFTER SLATS EXTENDED AND GEAR EXTENDED, QUANTITY DECREASED TO 1.2. COMPLIED WITH SDR CA050825005Drive Assy · worn(CAN) HYD WARNING HORN AND LIGHT CAME ON IN FLIGHT. PILOT FOLLOWED LOST HYD PROCEDURE AND RETURNED TO BASE AND SHUT DOWN. INVESTIGATION SHOWED THAT THE HYD PUMP DRIVE SPLINES WERE COMPLETLY WORN. PUMP, COUPLING AND BEARING CHANGE.SDR COMA0560447Pump · malfunctionedFLIGHT 5003 - HYDRAULIC SYSTEM 3 LOW PRESSURE CAUTION. REPLACED THE NR 3A ACMP.SDR COMA0560444Pump · malfunctionedFLIGHT 5428 - GEAR DISAGREE WARNING. REPLACED HYDRAULIC PUMP 3A.SDR C1HA200592003Pump · failedNR 2 B PUMP FAILED INFLIGHT, REPLACED NR 2 B HYD PUMP, CASE DRAIN AND PRESSURE FILTER, OP'S CHECK GOOD. LEAK CK GOOD REF MM 29-12-3.SDR CA050808003Pump · failed(CAN) AIRCRAFT RETURNED TO THE STATION DUE TO NR 1 ENGINE LOW HYDRAULIC PRESSURE AND LOSS OF HYDRAULIC FLUID GREEN SYSTEM. DURING INVESTIGATION THE HYDRAULIC PUMP HAD FAILED WITH A HOLE INTO THE HOUSING. HYDRAULIC PUMP AND FILTER REPLACED AND AIRCRAFT WAS RESDR VNAA0508003Pump · leakingON SHORT FINAL THE HYD EDP 2A MESSAGE ILLUMINATED AND NR 2 HYDRAULIC SYSTEM QUANTITY INDICATED 0 PERCENT. THE CREW MADE AN UNEVENTFUL LANDING. MAINTENANCE FOUND THE RT ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE RT EDP WAS REMOVED & REPLACED IAW CRJ700 AMM 29SDR 05FDEA02124Pump · failedHYD SYS B OVERHEAT LIGHT IN FLT TURNED ELEC PUMP NR 1 OFF AND LIGHT WENT OUT. REMOVED AND REPLACED NR 1 B PUMP PER MM-29-12-011-2. OPS CKS AND LEAK CKS GOOD. CYCLED ALL FLIGHT CONTROLS ON B SYS TO ENSURE NO AIR IN SYSTEM. NOTE, CASE DRAIN ALSO REMOVED AND SDR SFO2005F00001Pump · failedAFTER LANDING, THE NR 2 HYDRAULIC LIGHT CAME ON AND THE NR 2 HYDRAULIC PRESSURE WENT TO -0- PSI. INVESTIGATION REVEALED THE NR 2 HYDRAULIC PUMP HAD FAILED. THE PUMP AND REQUIRED FILTERS WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. THIS FAILED, OVSDR 2005UALA00731Pump · leakingLOST GREEN HYDRAULIC SYSTEM. CREW SECURED PUMP AND PTU.SDR VNAA0507019Pump · failedTHE CREW REPORTED A HYD EDP 2A CAUTION MESSAGE EN ROUTE TO DTW. MAINTENANCE REMOVED AND REPLACED THE RT ENGINE DRIVEN HYDRAULIC PUMP IAW CRJ700 AMM 29-11-01-000-801-A01 & 29-11-01-400-801-A01. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELSDR MASA200500592Pump · failedASH 6264 PHX. LEFT GEAR DISAGREE IN FLIGHT. MX REPLACED NR 3A HYD PUMP.SDR 2005UALA00690Motor · failedRETURN TO FIELD WITH A BLUE HYDRAULIC OVERHEAT INDICATION. BLUE HYD ELECT OVERHEAT. SHUTDOWN BLUE PUMP. WARNING CLEARED AFTER 5 MINS. CYCLED CB C12 PER SAMC AND RESTARTED BLUE PUMP. FAULT THEN RETURNED. QTY NORMAL. PUMP JUST REPLACED DUE TO POPPED CB ABSDR MALA050605Pump · inoperativeGREEN HYD HIGH TEMP ILLUMINATED. REMOVED AND REPLACED NR 3 GREEN HYD EDP PN 521449 SN OFF MX651419, SN ON F9911203SDR 2005FA0001319Pump · failedPILOT WAS ON HIS INTENDED ROUTE AND NOTIFIED OPERATIONS BASE THAT HE WAS TURNING AROUND AND THAT HAD LOST HYDRAULIC ASSIST TO FLIGHT CONTROLS. RETURNED TO BASE AND LANDED WITH NO INCIDENT. MAINT FOUND THAT THE HYDRAULIC PUMP SPLINES HAD FAILED AND REMOVED ANSDR VNAA0507015Pump · failedTHE HYD EDP 2A CAUTION MESSAGE ILLUMINATED ONE MINUTE PRIOR TO LANDING AT CLT. MAINTENANCE DEFERRED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP AND COMPLIED WITH THE M FUNCTION IAW CRJ700 MEL 29-11-01-2, CODE A. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. ON 07/2SDR MASA200500575Pump · failedASH 7055 ASE, NR 1 HYD SYSTEM WENT TO ZERO QTY AND ZERO PRESSURE ON TAKEOFF. CONTRACT MX REMOVED AND REPLACED THE PRESSURE MANIFOLD HYDRAULIC PUMP EDP.SDR AALA20050446Pump · inoperativeRT ENGINE PUMP INOPERATIVE. RT HYDRAULIC PRESSURE LOW LIGHT ON. LANDED ORD WITHOUT INCIDENT. REPLACED RT ENGINE HYDRAULIC PUMP AND FILTERS. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR VNAA0507010Pump · leakingDURING CRUISE THE CREW REPORTED TOTAL LOSS OF THE NR 1 HYDRAULIC SYSTEM PRESSURE AND FLUID QUANTITY. MAINTENANCE FOUND THE LEFT ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE LEFT EDP WAS REMOVED & REPLACED IAW CRJ700 AMM 29-11-01-400-801-A01. ALL OPERATIONAL CHSDR CA050725017Pump · failedSHORTLY AFTER TAKEOFF, THE CREW REPORTED HAVING HYD NR 1 LOW PRESS CAUTION MESSAGE. QUANTITY OF THE HYDRAULIC RESERVOIR WAS DROPPING FAST. CREW COMPLIED WITH THE QRH AND RETURNED TO THE BASE. FOUND HYDRAULIC LEAKING FROM THE HYD EDP AT THE PORT CAP. EDP WASDR 2005FA0001255Shaft · shearedWHILE PERFORMING AN ENGINE GROUND OPERATION THE HYDRAULIC PUMP OUTPUT CEASED. A SHEARED PUMP EXTERNAL DRIVE SHAFT WAS DISCOVERED. SYSTEM REGULATION AND RETURN FILTERS AND PUMP HOSES SHOW NO INDICATIONS OF METAL CONTAMINATES. THE PUP STUB SHAFT STILL TURNS BSDR EIA2005135Pump · leakingNR 1 HYD SYS SLOWLY LOST HYD QUANTITY AT TO GAGE SHOWED 9 GAL. GAGE SHOWED SLOW LOSS APPROX 2 HRS AFTER T/O. DID LEAK/LOSS PROCEDURES BUT LEAK CONTINUED, SYSTEM DEPRESSURIZED AND ADP OFF REMAINDER OF FLIGHT. REMOVED AND REPLACED NR 1 ENG HYDRAULIC PUMP PER SDR 05FDEA01777Pump · failedNR 1 GREEN HYD PUMP FAILED. LOST ALL GREEN HYDRAULIC FLUID. R & R NR 1 ENGINE GREEN SYSTEM EDP PER MM 29-11-32-4-02, ALSO REPLACED NR 1 ENGINE CASE DRAIN FILTER PER MM 29-11-36-4-02, ACP DRY MOTOR AND LEAK CHECKED REF JRH 5-37. CHECKED GOOD. ALSO CHECKED NSDR CA050629002Pump · failed(CAN) ON APPROACH THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP (EDP) LOW PRESSURE LIGHT ILLUMINATED. THE A-SYSTEM HYDRAULIC QUANTITY WAS ALSO LOW AT 22 PERCENT. THE AIRCRAFT CONTINUED TO THE DESTINATION WITHOUT ANY INCIDENT. MAINTENANCE INSPECTION REVEALED A DAMAGSDR HEEA107332Nut · splitSHORTLY AFTER TAKEOFF, THE NR 2 HYDRAULIC LIGHT ILLUMINATED. RETURNED TO MORGAN CITY. MAINTENANCE FOUND A JAM NUT ON A FITTING ON THE HYDRAULIC MANIFOLD SPLIT ALLOWING THE PACKING TO UNSEAT UNDER PRESSURE CAUSING THE LOSS OF HYDRAULIC FLUID. REPLACED THE NSDR SWAA051854Pump · failedDECLARED EMERGENCY. ENGINE DRIVEN HYDRAULIC A-PUMP LOW PRESSURE LIGHT ILLUMINATED. AFTER 10 MINUTES A-SYSTEM HYDRAULIC QUANTITY DROPPED TO 20 PERCENT. A ELECTRIC TURNED OFF UNTIL LANDING. REMOVED AND REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP PER MM.SDR MALA050497Pump · malfunctionedDURING CLIMB-OUT, YELLOW HYDRAULIC SYSTEM HIGH TEMP LIGHT ILLUMINATED. FOLLOWED QRH AND LIGHT EXTINGUISHED. RETURNED TO MEM. REMOVED AND REPLACED NR 2 EDP.SDR 1290501O-Ring · cutCOMPLETE A-SYSTEM HYDRAULIC FLUID LOSS IN FLIGHT. REPLACED O-RING P/N NAS 1612-4 ON "A" SYSTEM ELECTRIC MOTOR DRIVEN HYDRAULIC PUMP BLANKING PLUG. RESERVOIR "A" RESERVICED AND LEAK CHECKED SATISFACTORY. A RECORDS REVIEW REVEALED THAT THIS PUMP WAS INSTALLED OSDR CA050617002Pump · failed(CAN) DURING FLIGHT, AN OPERATOR EXPERIENCED A NR 2 HYDRAULIC SYSTEM FAILURE DUE TO A FAILED NR 2 HYDRAULIC PUMP (EDP). NR 2 EDP REPLACED, FULL HYDRAULIC SYSTEM FLUSHED.SDR AALA20050391Pump · inoperativeAT FL 230 RT HYDRAULIC PRESSURE BEGAN TO FLUCTUATE VERY RAPIDLY AND FOLLOWED SHORTLY BY RT HYDRAULIC PRESSURE LOW ANNUCIATOR AND RAPIDLY DECREASING HYDRAULIC QUANTITY. TURNED OFF RT ENGINE PUMP AND STOPPED QUANTITY LOSS AT 8. USED MANUAL LANDING GEAR EXTENSISDR COMA0560356Pump · faultyRECEIVED HYDRAULIC NR 2 LOW PRESSURE CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND DIVERTED TO IAD. ACFT LANDED WITHOUT INCIDENT. REPLACED RT ENGINE HYDRAULIC.SDR COMA0560353Pump · faultyFLIGHT 5851 - DURING CLIMBOUT OF DSM RECEIVED A GEAR DISAGREE CAUTION. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD, LANDING WITHOUT INCIDENT.SDR DXTA200500775Pump · leakingON SHORT FINAL, ANTI-SKID INOP AND POWER BRAKE LOW PRESS LIGHTS ILLUMINATED. NO BRAKES ON LANDING. LARGE HYD FLUID LEAK NOTICED ON POST FLIGHT. FLUID ON NOSE GEAR & INSIDE NOSE COMPARTMENT. REMOVED AND REPLACED PUMP ASSY, REPLACED FILTER ELEMENT & FILTER CSDR CA050615006Pump · failed(CAN) PILOT NOTICED STRANGE NOISE IN FLIGHT. UPON LANDING, CONDUCTED AN INVESTIGATION OF NOISE WHILE AC REMAINED RUNNING. NOISE DETERMINED TO BE COMING FROM HYD DRIVE AREA. AC WAS SHUTDOWN, PART REMOVED. DRIVEN PULLEY OF HYD SYS WAS FOUND TO HAVE ITS BEARISDR VNAA0506001Pump · failedON CLIMBOUT FROM CLE THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP FAILED. THE CREW CONTINUED TO DESTINATION CLT. MAINTENANCE REMOVED & REPLACED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP IAW CRJ 700 AMM 29-11-01-400-801-A01. OPERATIONAL AND LEAK CHECKS WERE GOOD. THE SDR CA050608007Pump · separated(CAN) THE AIRCRAFT WAS ON APPROACH WHEN THE LANDING GEAR WAS SELECTED AND IT DID NOT EXTEND. HYDRAULIC PRESSURE WENT TO 0 AND THE CREW INITIATED AN EMERGENCY LOWERING. THE GEAR EXTENDED AND A SUCCESSFUL LANDING WAS MADE WITHOUT INCIDENT. AN INVESTIGATION REVEASDR 0500809856Pump · leakingAFTER ACFT LEVELLED OFF AT FL 290, PILOT NOTICED DROP IN RT HYDRAULIC SYSTEM QUANTITY FROM 6 QTS TO 4 QTS. QUANTITY CONTINUED TO SLOWLY DECREASE AND WHEN REACHED 2 QTS COM PROCEDURES WERE COMPLIED WITH. CREW REQUESTED LONGEST RUNWAY. GEAR EXTENSION NORMAL BUSDR CA050601006Pump · failed(CAN) DURING FLIGHT, AN OPERATOR EXPERIENCED A NR 2 HYDRAULIC SYSTEM FAILURE DUE TO FLUID LOST FROM NR 2 EDP. NR 2 EDP AND PTU REPLACED.SDR 2005UALA00469Pump · failedLOST GREEN HYD SYSTEM WHILE IN A HOLDING PATTERN ABOVE PLANNED DESTINATION. GREEN SYSTEM EDP REPLACED AWAITING FINDINGS FROM THE VENDOR (ARINC). REPLACED NR 1 ENG DRIVEN PUMP, REF MM29-11-51. REPLACED CASE DRAIN FILTER, PDI NOT POPPED. NO DEBRIS FOUND IN FILSDR SSHA100897Pump · failedPILOT REPORTED LOSS OF HYDRAULICS SHORTLY AFTER TAKEOFF. INSPECTION FOUND THAT HYDRAULIC PUMP HAD FAILED INTERNALLY. PUMP WAS REMOVED AND REPLACED. AIRCRAFT WAS RETURNED TO SERVICE.SDR AU510001548Bearing · failedHYDRAULIC SYSTEM `B` NR 1 ELECTRIC HYDRAULIC PUMP FAILED. NIL PRESSURE AND METAL CONTAMINATION. INVESTIGATION FOUND THE FAILURE WAS DUE TO FAILURE OF THE PRE-MOD SB 57186-29-291 TRUNNION NEEDLE BEARING P/N 21830.SDR CA050609017Pump · worn(CAN) PULLEY SPLINES FOUND TO BE WORN BEYOND 2/3 DURING A 100 HR INSPECTION. COUPLING S40 REPLACED 336.4 HOURS PREVIOUSLY FOR THE SAME REASON. HYDRAULIC PUMP SPLINES FOUND 2/3 WORN. A NEW PUMP HAD BEEN INSTALLED 336.4 HOURS PREVIOUSLY FOR THE SAME REASON.SDR QXEA200500839Pump · failedSEA - EXPERIENCED A TOTAL LOSS OF NR 2 MAIN HYDRAULIC SYSTEM PRESSURE. THE GEAR WAS EXTENDED VIA ALTERNATE EXTENSION SYSTEM, AND THE AIRCRAFT LANDED IN SEA WITHOUT INCIDENT. AN INSPECTION OF THE NR 2 HYDRAULIC SYSTEM REVEALED THAT THE NR 2 EDP HAD FAILED, DUSDR 2005FA0000909Housing · crackedHOUSING CRACKED. HOUSING IS TOO WEAK. MAKE HOUSING STRONGER. (K)SDR MALA050420Pump · malfunctionedCREW RETURNED TO MSP AFTER DEPARTURE FOLLOWING YELLOW HYDRAULIC SYSTEM HIGH TEMPERATURE. EMERGENCY TRUCKS WERE CALLED AND FLIGHT LANDED WITHOUT FURTHER INCIDENT. FOUND AC PUMP COMING ON LINE CAUSING YELLOW HYD HIGH TEMP NOTED DURING YELLOW SYS FLT CONT OPERA
Back to JASC 2913