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 REXA96077Pump · failedHYD PRESSURE DROPPED TO A 1000 PSI AFTER GEAR RETRACTION AND INTRANSIT LIGHT STAYED ILLUMINATED. REOVED AND REPLACED HYD PUMP. (M)SDR 97ZZZX634Power Pack · malfunctionAIRCRAFT WAS ON A PART 91 TRAINING FLIGHT. ON APPROACH TO AIRPORT, PILOT PUT THE LANDING GEAR LEVER DOWN. LANDING GEAR WENT DOWN, BUT DID NOT GET A GREEN (NOSE DOWN AND LOCKED LIGHT). THE PILOT RECYCLED THE LANDING GEAR. THE LANDING GEAR CAME DOWN, BUT, AGSDR 97ZZZX201Pump · seal leakHYDRAULIC PUMP LEAKING STATICALLY AT INPUT SEAL. TBO TIME IS 3600 HRS ON THIS COMPONENT. REPLACED WITH SERVICEABLE UNIT.SDR 97ZZZX658Pump · malfunctionHYDRAULIC PUMP, NR 2 SYSTEM PRESSURE TOO HIGH, 860 PSI. REPLACED WITH NEW UNIT, CORRECTED PROBLEMSDR DL757962591Hyd Pump · leakingLEFT HYD QTY DECREASED IN FLT WITH BOTH LEFT ELEC AND ENG PUMPS OFF AND PTU CB. PULLED, LOSS WAS SLOWED CONSIDERABLY. FOUND LEFT ENG PUMP PRESSURE FILTER DIFFERENTIAL BUTTON ASSY LEAKING. REPLACED BUTTON ASSY, LEFT PRESSURE AND CASE DRAIN FILTERS. NO CONTAMSDR 97ZZZX78Pump · defectiveHYDRAULIC PUMP LOW PRESSURE OUTPUT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 96ZZZX6142Power Pac · failedNOSE GEAR WOULD NOT COME DOWN. EMERGENCY BOTTLE USED TO LOCK GEAR. HYD POWER PAC FAILURE.SDR CA970327011Bolt · misinstalled(CAN) SERVO SENT FOR REPAIR. PER AD CF96-11R2 AND BELL SB 206-67A-01, A BOLT WAS FOUND SUSPECT. UNIT REPAIRED, BOLT REPLACED.SDR HAIW6HR0050Pump · worn excessivelyPUMP IS WORN EXCESSIVELY. PUMP LEAKS AT SHAFT SEAL. PUMP HAS ONLY BEEN INSTALLED 1 MONTH. BHT P/N: 222-380-009-103. . REPLACED WITH SERVICEABLE UNIT.SDR 96ZZZM1542Hyd Pump · failedEN ROUTE FROM LAGUARDIA TO NICE FRANCE ON AN FAR PART 91 FLT, WHEN DURING CRUISE CONFIGURATION COMBINED HYD PRESSURE WAS LOST. THE FLIGHT CREW CONTINEUD TO DESTINATION DEPLOYING THE LANDING GEAR USING THE ALTERNATE SYSTEM AND LANDED WITHOUT INCIDENT. MAINTENSDR 96ZZZX5721Pump · seal failedLT AND RT HYD LOW FLOW LITES CAME ON IN FLIGHT. LANDING GEAR HAD TO BE EXTENDED USING THE LANDING GEAR EMERGENCY PROCEDURE. ACFT LANDED WITHOUT INCIDENT. RIGHT HYD PUMP NOSE SEAL LEAKED HYDRAULIC FLUID OVERBOARD THROUGH THE NOSE CASE DRAIN. PUMP REPLACED. SDR 96ZZZX5810Power Pack · failedLANDING GEAR POWER RACK WOULD NOT PUT GEAR IN EXTENDED POSITION - UPON DISASSEMBLY - COMMUTATOR ARMATURE SEEMED TO BE 'OUT OF ROUND DUE TO THE BRUSH MARKS. THE BRUSHES WERE NOT WORN EXCESSIVE.SDR COMA9630156Hyd Pump · weakHYDRAULIC SYSTEM WARNING ON CWP SYSTEM PRESSURE INDICATED ZERO AND LANDING GEAR INDICATED UNSAFE. REPLACED THE HYDRAULIC SYSTEM PUMP.SDR COMA9660191Hyd Pump · leakingNR 2 HYDRAULIC SYSTEM INDICATES ZERO QUANTITY, PRESSURE DROPPED TO 1700 PSI. REPLACED THE NR 2 HYDRAULIC SYSTEM ENGINE DRIVEN PUMP.SDR CALA9601510Hyd Pump · leakingAIRCRAFT LOST B-SYSTEM HYDRAULICS WHILE EN ROUTE. THE AIRCRAFT WAS DIVERTED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC LEAK ON THE RT ELECTRIC B-PUMP PRESSURE ACCESS PLUG. THE O-RING ON THE PLUG WAS FOUND BROKEN. THE O-RING WASDR RAIA961021Hydraulic Pump · failedFAT - FLT 4750 - LEFT HYDRAULIC PUMP PRESSURE DROPS TO ZERO. MAINTENANCE REPLACED THE LEFT HYDRAULIC PUMP. (M)SDR HEEA968260Pump · metal contamHYD PUMP METAL CONTAMINATION.SDR 96UAL900800Pump · leakingLOST NR 4 HYDRAULIC SYSTEM FLUID. *S/D* FOUND HYDRAULIC FLUID LEAKED FROM ENGINE DRIVEN PUMP. REPLACED ENGINE DRIVEN PUMP, CASE DRAIN FILTER AND PRESSURE FILTER.SDR 96UAL900797Pump · failedNR 1 ENGINE HIGH VIBRATION. ENGINE SHUT DOWN, LOUD NOISE FROM ENGINE DURING SHUTDOWN. COULD NOT DUPLICATE NOISE. TWO DAYS LATER IN DEN MECHANICS REPORTED NR 1 ENGINE NOISY WITH HYDRAULIC PUMP ON AND STOPS WITH PUMP OFF. REPLACED PUMP AND RUN-UP WAS GOOD.SDR 96ZZZX5478Pump · failedPOWER PACK PUMP LASTED ONLY 317.13 HRS. SUBMITTER STATED PUMP SHOULD HAVE LASTED LONGER.SDR COMA9660164Pump · leakingNR 1 HYD RESERVOIR AT 40 DEGREES. FOUND NR 1 ENGINE DRIVEN PUMP LEAKING. REPLACED HYDRAULIC PUMP.SDR COMA9660162Pump · leakingNR 2 HYDRAULIC QUANTITY FLUCTUATING BETWEEN O AND 10 PERCENT ON TAXI OUT. REPLENISHED SYSTEM, FERRIED A/C TO CVG WHERE THE RIGHT ENGINE DRIVEN HYDRAULIC PUMP WAS REPLACED.SDR CALA9601328Hyd Pump · leakingTHE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO APPROXIMATELY 2 .75 AND BOTH A-PUMP LOW PRESSURE LIGHTS ILLUMINATED AFTER TAKEOFF, WHEN THE GEAR LEVER WAS RAISED TO THE UP POSITION. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOSDR 9620259856Pump · failedDURING CRUISE, THE RIGHT HYDRAULIC SYSTEM QUANTITY AND PRESSURE WENT TO ZERO. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT EDP AND FILTERS. REPLACED RIGHT AUXILIARY PUMP AND FILTERS AND PRESSURE LINE FROM AUXILIARY PUMP. SERVICEDSDR AALA961374Pump · failedATL - FLT 455 - AFTER TAKEOFF ATL DURING CLIMB-OUT WHEN SWITCHING ENGINE HYDRAULIC PUMPS TO LOW, RIGHT PUMP FAILED WITH COMPLETE LOSS OF HYDRAULIC FLUID. ACCOMPLISHED ABNORMAL PROCEDURES, MANUALLY EXTENDED LANDING GEAR AND AIRCRAFT RETURNED TO ATL, LANDING WISDR 96UAL900705Over Heat Light · illuminatedB HYDRAULIC SYSTEM OVERHEAT LIGHT ON DURING CLIMB. OVERHEAT LIGHT OFF WITH NO. 2 ELECTRIC PUMP OFF.SDR PLGA9609071Power Pack · failedBOS - FLT 4523 - ON APPROACH, THE GEAR DOWN AND LOCK LIGHT FAILED TO ILLUMINATE, THE LANDING GEAR RELAY CIRCUIT BREAKER WAS FOUND POPPED AND WOULD NOT RESET. THE GEAR WAS EXTENDED MANUALLY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. BOS MAINTENANCE PINNED THE SDR 97ZZZX905Belt · failedSUSPECT AIR CONDITIONER COMP BELT BROKE AND TOOK OUT HYD BELT. FOUND BELT (AC) RUNNING TOO CLOSE TO DRIVESHAFT COUPLING BOLTS. SHIMMED AC COMPRESSOR BRACKET TO OBTAIN PROPER CLEARANCE. CHECKED COMP PULLEY TO DRIVESHAFT FOR PARALLELISM. SUGGEST INSP OF AC BESDR TWRA96301Seal · wornDURING FLIGHT, NR 3 ENGINE OIL QUANTITY DROPPED TO 75 GALLONS, OIL PRESSURE 32-45-PSI, OIL TEMPERATURE ROSE TO 109 DEGREES CELSIUS. ENGINE WAS SHUT DOWN. PERFORMED WINDMILL INSPECTION PER MM 72-00-00 PAGE 682. DURING GROUND IDLE FOUND HYDRAULIC PUMP DRIVE SSDR COMA9610262Pump · leakingBLUE (RT) HYDRAULIC SYSTEM LOW FLUID LEVEL WARNING DURING APPROACH. QUANTITY GAUGE INDICATED EMPTY. REPLACED THE RT ENGINE DRIVEN HYDRAULIC PUMP DUE TO INTERNAL LEAKAGE TO CASE DRAIN. PART TOTAL CYCLES, 5,227.SDR CALA9601210Pump · leakingTHE B-SYSTEM HYDRAULIC QUANTITY BEGAN TO DECREASE WHILE EN ROUTE. THE AIRCRAFT LANDED AT CLE WITHOUT INCIDENT. MAINTENANCE FOUND THE RT B-SYSTEM ELECTRIC HYDRAULIC PUMP LEAKING AT HOUSING. THE PUMP WAS REMOVED AND REPLACED, LEAK AND OPERATIONAL CHECKS WERE SDR SRAA960809Pump · failedDURING FLIGHT, NR 1 HYDRAULIC PUMP PRESSURE WENT TO O PSI WHEN RAISING MLG. ACCOMPLISHED AIR TURNBACK, AIRCRAFT LANDED WITHOUT INCIDENT. FOUND NR 1 HYD PUMP FAILED. REPLACED PUMP AND FILTER, INSPECTED UTILITY SYSTEM MAIN AND DRAIN FILTERS, NO CONTAMINATION SDR CALA9601188Hyd Pump · leakingTHE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO FOLLOWED BY LOSS OF PRESSURE ON NR 2 ENGINE WHILE EN ROUTE. AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE PUMP WAS REMOVED SDR SCNA96214O-Ring · cutDURING FLIGHT NOTICED THAT THE NUMBER 2 ENGINE OIL QUANTITY WAS AT 0 AND THE OIL PRESSURE WAS FLUCTUATING BETWEEN 20 PSI AND 40 PSI. AFTER MONITORING, THE OIL PRESSURE DROPPED BELOW RED LINE AND NUMBER 2 OIL PRESSURE LIGHT ILLUMINATED. NUMBER 2 ENGINE WAS SHSDR CA960826072O-Ring · deteriorated(CAN) #2 HYDRAULIC SYSTEM LOST ALL HYDRAULIC FLUID DURING FLIGHT. POST FLIGHT INVESTIGATION FOUND "O" RING AT #2 ENGINE DRIVEN HYDRAULIC PUMP DETERIORATED CAUSING LEAK OF ALL FLUID.SDR WRLA96029Hyd Pump · failedON CLIMB-OUT, CREW RECEIVED 'HYD PUMP 3 OFF' ANNUNCIATION. HYD CONTROLLER OPERATED NORMALLY, NR 3 STANDBY PUMP CAME INTO OPERATION. FLT CREW CONTINUED WITH FLT. AFTER 1HR 45 MINS AT CRUISE, FLT CREW RECEIVED 'HYD SYSTEM 3' FAILED ANNUNCIATION. AT THAT TIMESDR MALA965086Hyd Pump · failedFLT NR 3159 - EN ROUTE, THE AIRCRAFT LOST HYDRAULIC PRESSURE ON THE LEFT SIDE. THE NR 1 STANDBY PUMP WAS IN THE NORMAL POSITION. THE CREW PERFORMED QUICK REFERENCE PROCEDURES AND RETURNED TO DTW. MAINTENANCE REPLACED THE LEFT HYDRAULIC PUMP. ALL CHECKS SATSDR COMA9660125Hyd Pump · low pressureGEAR DISAGREE WARNING WHEN SELECTED DOWN DURING LANDING APPROACH. SECOND ATTEMPT WAS NORMAL. REPLACED HYDRAULIC PUMP 3A. PART TOTAL CYCLES, 5,295.SDR CA960801007Pump · leaking(CAN) DURING CLIMB A SYSTEM HYDRAULIC PRESSURE DROPPED TO ZERO. AIRCRAFT LANDED USING B SYSTEM. FLUID FROM #2 ENGINE HYDRAULIC PUMP REPALCED. #1 PUMP REPLACED AS PRECAUTION.SDR 96ZZZX3905Pump · seal failedHYDRAULIC PUMP SHAFT SEAL FAILURE IN-FLIGHT 'WITHOUT INCIDENT', BUT ELECTRIC DRIVE MOTOR AND SURROUNDING AFT FUSELAGE AREA TO TAIL WAS SATURATED WITH APPROXIMATELY 2 GALLONS OF FLUID WHICH POSED A SEVERE FIRE HAZARD.SDR DLL10961753Pump · crackedIN CRUISE B-SYSTEM HYDRAULIC RESERVOIR LOW QUANTITY LIGHT ON WITH FLUID LEVEL AT THREE-EIGHTS FULL. AT SAME TIME, NOTED B2 ATM ON PRESSURIZING B-HYDRAULIC SYSTEM AND B-PUMP LOW PRESSURE LIGHT ON FLUID LOSS STOPPED WITH PUMPS TURNED OFF. FOUND B-SYSTEM ENGINESDR CA960826066Pump Body · cracked(CAN) PUMP WAS REMOVED TO FACILITATE TRANSMISSION REPLACEMENT WHEN PUMP MOUNTING FLANGE WAS FOUND CRACKED APPROXIMATELY 1 INCH ACROSS THE THINNEST PORTION OF THE FLANGE ADJACENT TO THE 1 O'CLOCK MOUNT HOLESDR PNSA960716Pump · failedLEFT HYDRAULIC FAIL LIGHT ILLUMINATED DURING CLIMB. RETURNED TO ANC.SDR USAAD96103Hydraulicpump · failedFLT 1240 - PIT-BGM - IN CRUISE, RIGHT HYDRAULIC SYSTEM LOW PRESSURELIGHT AND RUDDER CONTROL MANUAL LIGHT ILLUMINATED. NO QUANTITY LOSS.RETURNED TO PIT. REPLACED NR 2 ENGINE DRIVEN PUMP. (M)SDR AWXA960321Hydraulic Pump · failedPHX - FLT 2830 - GATE RETURN. A-SYSTEM ELECTRIC PUMP FAILED ON TAXI OUT. OVERHEAT AND LOW PRESSURE LIGHTS ILLUMINATED. REMOVED AND REPLACED A-SYSTEM ELECTRIC HYDRAULIC PUMP PER CARD R4M29002. OPS AND LEAK CHECK GOOD. PART TOTAL CYCLES, 24,482. (X)SDR CALA9600962Hyd Pump · leakingTHE LEFT HYDRAULIC SYSTEM QUANTITY DECREASED SHORTLY AFTER TAKEOFF FROM EWR. WHILE COMPLYING WITH ABNORMAL PROCEDURES THE LT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED. THE LEFT HYDRAULIC PUMP AND TRANSFER PUMP WERE SECURED. THE AIRCRAFT WAS RETURNED TO EWR WSDR 96FDEA01191Pump · inoperativeENG NR 1 GREEN HYD PUMP INOP. FAILURE OCCURRED IMMEDIATELY AFTER TAKEOFF. REMOVED AND REPLACED NR 1 GREEN SYSTEM PUMP, SHAFT AND CASE RETURN FILTER, OPS CHECK GOOD.SDR QXEA9600230Hyd Pump · leakingUTILITY SYSTEM HYDRAULIC QUANITY DROPPED TO ZERO. ALTERNATE GEAR EXTENSION PERFORMED AND AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. NR 1 HYDRAULIC PUMP REPLACED AND SYSTEM OPS CHECKED GOOD.SDR CALA9600926Hyd Pump · leakingTHE B-SYSTEM HYDRAULIC QUANTITY DROPPED TO 1/2 ACCOMPANIED BY ILLUMINATION OF THE B-ENGINE HYDRAULIC PUMP LOW PRESSURE LIGHT WHILE EN ROUTE. THE B-ENGINE HYDRAULIC PUMP WAS SHUT OFF AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTSDR 96ZZZX3558Relay · stuckGEAR POWER PACK RUNS ALL THE TIME WHEN RELAY IS IN STUCK POSITION.
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