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 20001219SH001Pump · 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.SDR 20001218SH037Pump · wornFLUID SAMPLE TAKEN AT 100-HOUR INTERVAL SHOWS THE PUMP NEEDS 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)SDR 20001218SH028Pump · wornFLUID SAMPLE TAKEN AT 100-HOUR INTERVAL SHOWS THE PUMP NEEDS TO BE REPLACED. REPLACED PUMP WILL CONTINUE TO TAKE FLUID SAMPLES AT 100-HOUR INTERVALS AND CHANGE PUMPS AS REQUIRED. AIRCRAFT TOTAL TIME 812.0 HOURS. TOTAL CYCLES 546. (X)SDR 20001218SH027Pump · wornFLUID SAMPLE TAKEN AT 100-HOUR INTERVAL SHOWS THE PUMP NEEDS TO BE REPLACED. REPLACED PUMP, WILL CONTINUE TO TAKE FLUID SAMPLES AT 100-HOUR INTERVALS AND CHANGE PUMPS AS REQUIRED. AIRCRAFT TOTAL TIME 812.0 HOURS. TOTAL CYCLES 546. (X)SDR 20001218SH025Pump · wornFLUID SAMPLE TAKEN AT 100-HOUR INTERVAL SHOWS THAT THE PUMP NEEDS TO BE REPLACED. REPLACED PUMP. WILL CONTINUE TO TAKE FLUID SAMPLES AT 100-HOUR INTERVALS AND CHANGE PUMPS AS REQUIRED. AIRCRAFT TOTAL TIME 850.3 HOURS. TOTAL CYCLES 567. (X)SDR 20001218SH024Pump · wornFLUID SAMPLE TAKEN AT 100-HOUR INTERVAL SHOWS THE PUMP NEEDS TO BE REPLACED. REPLACED PUMP WILL CONTINUE TO TAKE FLUID SAMPLES AT 100-HOUR INTERVALS AND CHANGE PUMPS AS REQUIRED. AIRCRAFT TOTAL TIME 850.3 HOURS. TOTAL CYCLES 567. (X)SDR AU001150Pump · cracked(AUS) RT ENGINE DRIVEN HYDRAULIC PUMP CASING CRACKED. PUMP DRIVESHAFT FAILED AT SHEAR POINT. SEVERE INTERNAL DAMAGE TO PUMP. SUSPECTPISTON AND SHOE SUBASSEMBLY FAILED FIRST. LOSS OF HYDRAULIC FLUID.SDR 2000UALA00686Valve · bypassingBOTH PUMPS ON THE A HYDRAULIC SYSTEM WERE INDICATING OVERHEAT. CONTINUED TO DEN AND AMBER ALERT DECLARED. AIRCRAFT TOWED TO GATE. SUPPLEMENTAL DATA UPDATE FOUND HYDRAULIC RUDDER MODULE BYPASSING. REPLACED MODULE AND RELATED COMPONENTS PER MAINTENANCE MANUAL.SDR CA001212021Powerpack · failed(CAN) FLIGHT CREW REPORTED LANDING GEAR SELECTOR HAD TO BE ACTIVATED SEVERAL TIMES BEFORE GEAR LOWERED AND THREE GEARLIGHTS ILLUMINATED. SUBSEQUENT GEAR SWINGS RESULTED IN POWER PAC REPLACEMENT.SDR 20001212SH019Cover · crackedCOVER IS CRACKED ACROSS EXTERIOR SURFACE FROM THE SHAFT HOLE OUTWARD. POSSIBLE CAUSE, STRESS, FATIGUE AND/OR WEAK POINT IN DESIGN OF COVER. (X)SDR CA001214015Pump · leaking(CAN) INVESTIGATION OF A HYDRAULIC FLUID LEAK FROM THE NR 2 ENGINE RESULTED IN REPLACEMENT OF THE ENGINE DRIVEN HYDRAULIC PUMP, WHICH WAS FOUND TO BE LEAKING FROM THE SHAFT SEAL. THIS UNIT HAD ONLY ACCUMULATED 272 HOURS AND 172 CYCLES SINCE REPAIR FOR A SIMILSDR 0004231141Pump · failedDURING CRUISE, NR 1 SYSTEM HYDRAULIC QUANTITY DECREASED. FOLLOWED COM PROCEDURE, DEPRESSURIZED AND ISOLATED NR 1 SYSTEM. QUANTITY STABILIZED AT 3.5 GALLONS. UPON APPROACH TO HNL, RESTARTED NR 1 SYSTEM AND QUANTITY WENT TO ZERO. REQUESTED EMERGENCY EQUIPMENSDR 20001120SH022Powerpack · malfunctionedLANDING GEAR HYDRAULIC POWER PACK BUILDS UP 16 PSI. (AFTER GEAR EXTENSION) IN THE ''UP'' SIDE OF HYDRAULIC CIRCUIT CONTRARY TO COMMANDER 112 SM. POWER PACK VENDOR STATES THE OVERHAUL IS IAW COMMANDER SPECS AND COMMANDER STATES PROBLEM IS WITH POWER PACK VENDSDR AALA20001859Pump · leakingPHX - FLT 77 - EN ROUTE IAD-LAX - LEFT SIDE HYDRAULIC SYSTEM FAILED WITH COMPLETE LOSS OF FLUID. AIR INTERRUPTED, DIVERTED AND LANDED PHX WITHOTU FURTHER INCIDENT. REPLACED LEFT SIDE HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR AALA20001844Pump · defectiveORD - FLT 792 - EN ROUTE ORD-EWR - DURING INSPECTION, BEFORE FLIGHT, CO-PILOT DETECTED SMOKE IN WHEEL WELL AREA. REPLACED AUXILIARY ELECTRIC HYDRAUIC PUMP. ACCOMPLISHED LEAK CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR 20001219SH006Pump · damagedDFW - TA440 - DURING APPROACH, HYD SYS-A LOST, MASTER CAUTION ON A-FLT CNTRL, LOW PRESS LIGHTS ON, ENG 1, 2. UNEVENTFUL LANDING. MAINT TECH PERFORMED INSP, FND HYD A-SYS RESERVOIR WITH LOW LEVEL QTY, AIR FILLING VALVE WITH LEAK. ENG NR 2, HYD PUMP SUPPLY SDR 2000UALA00646Pump · failedDIVERTED TO IAD DUE TO LOSS OF A-SYSTEM HYDRAULICS. REPLACED NR 1 ENGINE HYDRAULIC PUMP.SDR 20001215SH005Pump · damagedDRIVESHAFT WAS TORQUED TOO TIGHTLY IN PLACE AT THE FACTORY. WHILE MECHANIC WAS REMOVING THE PUMP FOR INSPECTION, THE SHAFT PULLED LOOSE. REPLACED WITH USED UNIT, CORRECTED PROBLEM. (X)SDR DLM88002101Pump · inoperativeLEFT HYD PUMP FAILED. REPLACED LEFT ENGINE HYDRAULIC PUMP.SDR CA001110009Motor · failed(CAN) ON APPROACH TO TORONTO, CENTRE HYDRAULIC LOSS. EXTENDED THE GEARS MANUALLY, AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. HYDRAULIC FILTERS, AC MOTOR HYDRAULIC PUMP DRIVE, AND AIR DRIVEN PUMP UNIT WERE CHANGED. OPERATION CHECK CARRIED OUT, NORMAL.SDR AWXA0000796Pump · failedEMERGENCY LANDING, BLUE SYS HYDRAULIC PRESS WENT TO ZERO PSI. REMOVED AND REPLACED BLUE SYS HYD PUMP.SDR USAASB00299Pump · leakingATL-CLT - FLT 1273 - DURING APPROACH, THE A-HYDRAULIC QUANTITY DROPPED TO THE STAND PIPE LEVEL AND THE LOW PRESSURE LIGHT ILLUMINATED. MAINTENANCE REPLACE THE LEFT ENGINE DRIVEN HYDRAULIC PUMP. THE ENGINE DRIVEN CASE DRAIN AND PRESSURE FILTERS WERE REPLACED.SDR RAIA0010010Pump · failed6881-DCA- RIGHT ENGINE HYDRAULIC LOW PRESSURE CAPTION ILLUMINATED DURING TAXI. MAINTENANCE INSPECTED AND REPLACED LEFT ENGINE DRIVEN HYDRAULIC PUMP.SDR 20001212SH017Cover · crackedCOVER IS CRACKED FROM THE CENTER BORE OUTWARD ACROSS THE TOP. (X)SDR 20001214SH039Pump · wornHYDRAULIC PUMP HAD EXCESSIVE SPLINE WEAR. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)SDR HALA0000321Pump · failedHNL - FLT 212 - NR 2 HYD QTY DROPPED TO 1 GALLON AND NR 2 SYSTEM PRESSURE WENT OT ZERO. FOLLOWED CHECKLIST AND LANDED NORMALLY. REPLACED NR 2 LEFT ENGINE DRIVEN HYD PUMP. SERVICED NR 2 HYD RES PUMP, LEAK CHECK OK. (M)SDR ZIAA00011Pump · leakingYIP - IN FLIGHT NR 1A PUMP LOW PRESSURE LIGHT CAME ON, TURNED OFF. REMOVED AND REPLACED NR 1A HYD PUMP PER CARD N29-01. OPS AND LEAK CHECKS GOOD ON GROUND. (M)SDR CA001026014Motor · shorted(CAN) MOTOR WOULD RUN AS DESIGNED BUT BECAUSE OF ONE BAD COMUTATOR SEGMENT WOULD NOT TURN WHEN SELECTED IF BRUSH WAS ON BAD SEGMENT. DURING FLT AS HYD PRESS IS LOWERED (DUE TO TEMP) PUMP WILL COME ON FOR 1-2 SECONDS TO BUILD UP FROM 2,750 PSI TO 3,000 AND SHUSDR ASOA00104Motor · inoperativeFLT 4411 - DURING FLIGHT FROM SBN TO ATL, CREW REPORTED HYDRAULIC 3 PRESSURE EICAS MESSAGE DURING INITIAL DESCENT TOWARD ATL. SYNOPITC PAGE SHOWED HYDRAULIC QTY OF 5 PERCENT IN NR 3. CREW FOLLOWED QRH FOR ABNORMAL PROCEDURES, INCLUDING MANUAL GEAR EXTENSION.SDR 0003546633Pump · failedDURING CLIMB AFTER LANDING GEAR RETRACTION, THE RED LANDING GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED ACCOMPANIED BY VIBRATION. RECYCLED LANDING GEAR AND LIGHTS EXTINGUISHED AND AIRCRAFT CONTINUED TO DESTINATION WITHOUT FURTHER INCIDENT. REPLACED NR 4 ENGINESDR COMA0060780Pump · failedLANDING GEAR DISAGREE MESSAGE. REPLACED HYDRAULIC PUMP 3A.SDR 0003372702Pump · leakingON DEPARTURE FROM MSY, THE HYDRAULIC ''B'' SYSTEM FAILED. COMPLIED WITH COM PROCEDURE AND DECLARED AN EMERGENCY. MAINTENANCE CONTROL AND CAPTAIN MADE A DECISION TO CONTINUE TO MEM BASED ON POOR WEATHER AT MSY. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE RESDR CA001122033Clip · missing(CAN) CIRCLIP AT END OF PUMP, (SOME PARTS FOUND IN PUMP P/S CAVITY) WAS FOUND MISSING, AND ALLOWED THE DRIVE SHAFT TO DISENGAGE FROM PUMP AND MOVE INTO THE TRANSMISSION DRIVE QUILL. THE PUMP WAS REMOVED AND SENT FOR TEST AND INSPECTION WHICH CONFIRMED SUSPICIOSDR TWAA0014202Pump · failedFLIGHT EXPERIENCED A LOSS OF B HYDRAULIC SYSTEM FLUID. USED ALTERNATE SYSTEM FOR BRAKING. REPLACED THE NUMBER 2 B HYD PUMP DUE TO FAILURE. A STUD ON THE PUMP FAILED CAUSING SEAL FAILURE. CHECK-C 12-12-99 MCI.SDR CA000928011Line · leaking(CAN) HYDRAULIC POWER PACK STARTED TO CYCLE FREQUENTLY AND THE HYDRAULIC LOW LIGHT CAME ON AND STAYED ON. HYDRAULIC CONTROL CIRCUIT BREAKER TRIPPED. PILOT RETURNED TO BASE AND DID A MANUAL EXTENSION AND LANDED AIRCRAFT WITH 3 GREEN. MAINTENANCE FOUND LINE GSDR RAIA0009008Pump · failed7607-CHS- SYSTEM ONE HYDRAULIC OVERHEAT EICAS MESSAGE ILLUMINATED IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED LEFT HYDRAULIC PUMP.SDR COMA0060731Pump · malfunctionedGEAR DISAGREE WARNING, WHEN LANDING GEAR SELECTED DOWN. REPLACED HYRAULIC PUMP 3A.SDR AWXA0000622Pump · failedAIR TURNBACK, LOST NR 2 ENGINE DRIVEN B-PUMP AND B-SYS HYD. REMOVED AND REPLACED ENGINE DRIVEN PUMP (SECOND TIME).SDR COMA0060730Pump · malfunctionedLANDING GEAR DISAGREE WARNING WHEN GEAR SELECTED DOWN. REPLACED HYDRAULIC PUMP 3A.SDR AU000660Pump · failed(AUS) LEFT ENGINE DRIVEN HYDRAULIC PUMP DRIVESHAFT SHEARED. PUMP HAD ONLY COMPLETED 1.7 HOURS TIS SINCE OVERHAUL. (X)SDR AU000634Brush Block · worn(AUS) HYDRAULIC POWER PACK MOTOR BRUSHES WORN. (X)SDR CA000901016Coupling · worn(CAN) THE PILOT WAS IN CRUISE WHEN HE LOST HYDRAULIC BOOST. THE PILOT INITIATED A HYDRAULIC FAILURE PROCEDURE AND LANDED THE HELICOPTER WITHOUT AN ACCIDENT. AN ENGINEER FOUND WORN OUT SPLINES ON THE COUPLING SLEEVE OF THE HYDRAULIC PUMP PULLEY ASSEMBLY. AS ASDR 20001023SH001Motor · failedMOTOR QUIT.SDR USAASB00234Pump · leakingMCO - FLT 808 - DURING CLIMB-OUT FROM MCO, EN ROUTE TO PHL, CREW NOTICED A LOSS OF NR 1 ENGINE HYDRAULIC PRESSURE ON THE ENGINE DRIVEN PUMP AND THE SYSTEM A HYDRAULIC QUANTITY INDICATOR READING BELOW ONE-QUARTER GALLON. CREW DECLARED AN EMERGENCY AND RETURNEDSDR 2000UALA00511Pump · failedAFTER TAKEOFF NOTICED CENTER HYDRAULIC QUANTITY DECREASING. SECURED CENTER HYDRAULIC PUMPS AT .72 QUANTITY. *S/D* REPLACED NR 2 CENTER AC MOTOR PUMP.SDR 20000918SH001Shaft · wornHYDRAULIC PUMP SHAFT SPLINE WORN MAKING HYDRAULIC SYSTEM INOPERATIVE. THIS HAPPENED ON A FERRY FLIGHT. INSPECTION REQUIREMENTS ARE EVERY 500 HOURS. THE LAST INSPECTION ON THIS UNIT WAS ABOUT 390.2 HOURS AGO.SDR TI1R001418Shaft · separatedHYDRAULIC PUMP - SHAFT SEPARATED. REMOVED AND REPLACED.SDR CA000907020Pump · malfunctioned(CAN) AT 4 MILES FINAL FLAPS SELECTED TO 15 DEGREES NR1 ENGINE HYDRAULIC CAUTION LIGHT ILLUMINATED TOGETHER WITH ROD PRESSURE NR1 AND ROD HYDRAULIC NR1 AND MASTER CAUTION.STANDBY AND MAIN PRESSURES OBSERVED TO BE 1500 PSI FLAPS CONTINUED TO TRAVEL TO 15 DEGREESDR RAIA0008008Pump · failed6102-JFK- ON APPROACH INTO BOS GEAR HORN SOUNDED, 3 MAIN GREEN, MINUS NOSE STDBY, RIGHT HYDRAULIC LOW PRESSURE CAPTION ILLUMINTED. CYCLED GEAR, HORN SILENCED AND NOSE STDBY INDICATOR ILLUMINATED. MAINTENANCE INSPECTED AND RELEASED AIRCRAFT FOR ONE TIME FERRYSDR COMA0010316Pump · leakingGREEN HYDRAULIC SYSTEM LOST ALL FLUID. REPLACED THE LEFT ENGINE HYDRAULIC PUMP.
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