JASC 2910
Service difficulty reports · 11,292
Reports filed under 2910 · Hydraulic System, 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 = '2910' 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 = '2910' 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 CAL950128O-Ring · rupturedFLT NR 0318 - EWR - THE LEFT HYDRAULIC SYSTEM FLUID QUANTITY BEGAN TO DECREASE WHILE IN FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A RUPTURED O-RING ON THE CAPPED END OF VALVE ASSEMBLY LEADING TO LEFT BRAKE PRESSURE TRANSMITTER. THE O-RSDR BUFA9504Hyd Fitting · leakingDURING FINAL APROACH, ACFT HYDRAULIC PRESSURE DROPPED DOWN TO 500-600. FOUND HYDRUALIC LINE FITINGS AT LT MLG RETRACT ACTUATOR, PN 57740355507, LEAKING. REPLACED PACKING AT SAME FITTINGS. LEAK CHECK C/W IWA MM 29-01. AIRCRAFT RETURNED TO SERVICE. (X)SDR QXEA9500049Hyd Line · leakingFCA - LOST HYDRAULIC PRESSURE, NOSE GEAR UNSAFE LIGHT ILLUMINATED, CREW PERFORMED EMERGENCY GEAR EXTENSION AND RETURNED TO FIELD. FOUND HYDRAULIC LINE IN LEFT WHEEL WELL LEAKING. REPLACED LINE, AND NR 1 AND NR 2 HYDRAULIC PUMPS AND FILTERS. SERVICED RESERVOSDR CAL950120Hyd Valve · leakingBWI - FLT 1555 - THE AIRCRAFT LOST THE 'A' SYSTEM HYDRAULIC QUANTITY SHORTLY AFTER TAKEOFF FROM BWI. THE AIRCRAFT WAS RETURNED TO BWI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE 'A' SYSTEM HYDRAULIC MANUAL SHUT-OFF VALVE IN THE TAIL COMPARTMENT LSDR 95UAL747009Hyd Syst · failedNR 1 HYDRAULIC SYSTEM FAILED DURING FLAP RETRACTION.SDR CAL950119Hyd Line · leakingFLT NR 1688 - JAX - THE RT HYDRAULIC SYSTEM FLUID QUANTITY WAS LOST WHILE EN ROUTE TO JAX. 'ABNORMAL' PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT LANDED IN JAX WITHOUT INCIDENT. MAINTENANCE FOUND THE ELECTRIC PUMP HYDRAULIC PRESSURE LINE TO FILTER LINE LESDR SIMA950411Hyd Line · chafedRSW - FLT 3525 - IN-FLIGHT FROM MIA TO RSW, BLUE SYSTEM HYDRAULIC LOW LEVEL INDICATION CAME ON FOLLOWED BY BLUE PUMP LOW PRESS AND LOSS OF BLUE HYD SYSTEM. AIRCRAFT DECLARED EMERGENCY AND MADE ZERO DEGREE FLAP LANDING AT RSW. EMERGENCY EVACUATION WAS NOT REQSDR CAL950115Hyd Module · leakingCLE - FLT 1255 - THE 'A' HYDRAULIC SYSTEM WAS LOST AFTER DEPARTING LGA. THE AIRCRAFT LANDED AT CLE WITHOUT INCIDENT. MAINTENANCE FOUND PLUG BROKEN ON 'A' SYSTEM HYDRAULIC MODULE. THE 'A' SYSTEM HYDRAULIC MODULE WAS REMOVED AND REPLACED AND LEAK CHECKS WERE SDR ASOA95008Hydraulic Line · failedATL/ABY - FLT 7002 - EN ROUTE, BLUE HYDRAULIC SYSTEM FAILED. ON FINAL APPROACH TO ATL, GEAR WOULD NOT COME DOWN. EXECUTED FREE FALL OF GEAR AND GEAR EXTENDED. LANDED IN ATL SAFELY AND WITHOUT INCIDENT. REPLACED HYDRAULIC LINE ON RIGHT HYDRAULIC RESERVOIR. SDR 95ZZZX1346Hose · leakingAFTER LANDING, COPILOT NOTED HYDRAULIC FLUID COMING FROM LEFT SIDE OF ENGINE INLET COWLING. HOSE ASSY FOUND LEAKING. REPLACE HOSE ASSY.SDR 9502312292Hyd Fluid · low qtyDURING CRUISE, 'A' SYSTEM HYDRAULIC QUANTITY LOW. DURING FLAP EXTENSION QUANTITY DECREASED TO 2.0 GALLONS, UPON GEAR EXTENSION QUANTITY RETURNED TO NORMAL. CLOSED 'A' SYSTEM HYDRAULIC FLUID SHUTOFF VALVES AND CALLED OUT EMERGENCY EQUIPMENT AS A PRECAUTION. SDR CAL950102Hyd Line · looseEWR - FLT 0261 - THE GREEN SYSTEM HYDRAULIC FLUID QUANTITY DROPPED TO 1.3 GALLONS WHILE IN-FLIGHT AND WAS ACCOMPANIED BY ILLUMINATION OF WARNING LIGHT. THE HYDRAULIC LOSS CHECKLIST WAS COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUNDSDR ABXA9500069Hyd Hose · rupturedON SHORT FINAL, THE HYDRAULIC FLUID QUANTITY LEVEL DROPPED TO THE STANDPIPE LEVEL AFTER GEAR AND FLAP EXTENSION. LEVEL REMAINED THERE AFTER LANDING. FOUND THE RIGHT GEAR UNLOCK BOGIE TRIM LINE RUPTURED. REMOVED AND REPLACED THE HYDRAULIC LINE IAW DC 8 MM CHSDR BUFA9502Line · looseMIA - ON CLIMB, THE HYDRAULIC FLUID LOSS TO STANDPIPE. RETURNED TO MIA, NO EMERGENCY DECLARED, AND HAD UNEVENTFUL LANDING. FOUND LOOSE LINE AT CASE DRAIN. TIGHTENED 'B' NUT, RAN ENGINE AND PERFORMED OPERATION AND LEAK CHECK. CHECK OK PER MM. (W)SDR AWXA9500073Manifold · leaksATL - FLT 19 - ATL-PHX - AFTER NR 1 ENGINE START, GROUND CREW NOTICED LARGE HYDRAULIC LEAK ASSOCIATED WITH YELLOW HYDRAULIC LOW LEVEL. LEAK NOTED AT YELLOW HYDRAULIC RESERVOIR DOOR. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER PROBLEMS. CONTRACT MAINTENANCE RESDR DLM88950466Hose · leakingSHORTLY AFTER TAKEOFF USING NORMAL POWER, THE FLIGHT ATTENDANTS REPORTED THE SMELL OF SMOKE THROUGHOUT THE CABIN. FOUND HYD LEAK IN RT SIDE TAIL COMPARTMENT. HOSE MFG NR AS153-08-0254. REPLACED HOSE RETURNED TO SERVICE.SDR CAL950084Hyd Line · leakingFLL - FLT 0164 - THE AIRCRAFT LOST GREEN SYSTEM HYDRAULIC FLUID QUANTITY AFTER TAKEOFF FROM FLL. THE FLUID LOSS WAS ACCOMPANIED BY ILLUMINATION OF THE HYDRAULIC LOW LEVEL LIGHT AND LOW PRESSURE LIGHT. THE AIRCRAFT WAS RETURNED TO FLL WHERE IT LANDED WITHOUT SDR 95FDEA00106Hyd Syst · reqd serviceTPE - LOST NR 3 HYDRO SYSTEM, FLUID QUANTITY WENT DOWN TO 2.8. SERVICED NR 3 HYDRO SYSTEM TO 8.5 GALLONS. TROUBLESHOT AND RAN ENGINES. NO LEAK NOTED. (SUSPECT AIR BLEED VALVE PLUNGER MAY HAVE STUCK OPEN.) EXCERISED PLUNGER AND OPS. CHECK NORMAL.SDR 95FDEA00105O-Ring · failedHYD NR 1 OFF ALERT AFTER 50 MINUTES OF FLIGHT AT FLT LEVEL 320. QUANTITY FELL TO 2.8, PRESS DROPPED TO 40 PSI, NR 2, NR 3 NORMAL. HYD TEMP NR 1 - 48C TEMP ROSE TO 92C, THEN CAME BACK DOWN. FOUND HYD LEAK FROM LINE FITTING ON FILTER HEAD TO NR 1L HYD PUMP PRSDR CAL950074Hyd Line · leakingEWR - FLT 518 - THE ACFT LOST 'A' SYSTEM HYDRAULICS ON APPROACH WITH THE NR 1 PUMP LOW PRESSURE LIGHT FLICKERING ON AND OFF. THE GEAR AND FLAPS WERE EXTENDED USING ALTERNATE MEANS AND THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE HYDRAUSDR COM11754Tube Assy · leakingHYDRAULIC FLUID LEAK IN NLG AREA. REPLACED NLG UPLOCK HOOK HYDRAULIC TUBING.SDR CAL950073Hyd Line · leakingMIA - FLT 334 - THE 'A' SYSTEM HYDRAULIC QUANTITY DECREASED TO .1250 GALLON WHILE IN FLIGHT. 'ABNORMAL' PROCEDURES WERE COMPLIED WITH AND THE ACFT WAS DIVERTED TO MIA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP PSDR UF6A950116Hyd Fluid · reqd serviceORD - FLT 5106 - LOW HYDRAULIC LEVEL LIGHT ILLUMINATED. MAINTENANCE SERVICED HYDRAULIC SYSTEM WITH FLUID. (W)SDR USAA950024Nut · loosePIT - FLT 1025 - AFTER TAKEOFF, THE CREW GOT A 'HYD SYS 2 LO QTY' ALERT. ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PRESSURE LINE 'B' NUT ON UPPER PUMP LOOSE AT QUICK DISCONNECT. MAINTENANCE TIGHTENED FITTING. SERVICED, RAN ENGINSDR 95ZZZZ95B-Nuts · looseFLT 3057 - BWI-HPN - NR 1 HYDRAULIC SYSTEMS CONTENTS WENT TO ZERO IN FLIGHT. AIRCRAFT DIVERTED TO PHL AND LANDED WITHOUT INCIDENT. RETORQUED SEVERAL 'B' NUTS ON HYDRAULIC LINES TOP OF NR 1 NACELLE ABOVE JET PIPE. SERVICED SYSTEM AND BLED, PERFORMED SEVERAL SDR 95ZZZX735Line · leakAT AROUND 8:20 A.M. FLIGHT 296 FROM BILLINGS TO MISSOULA, HYDRAULIC POWER PACK CIRCUIT BREAKER TRIPPED AND LANDING GEAR EXTENDED PREMATURELY. THE PILOT USED HIS HAND PUMP TO LOCK THE GEAR DOWN AND DECLARED AN EMERGENCY LANDING. THE PLANE LANDED WITHOUT INCIDSDR LOSA9504Hyd Power Pack · malfunctionedLAS - CREW RPORTED RT ENGINE HYDRAULIC LIGHT REMAINED LIT, AFTER START-UP AND RT HYDRAULIC PRESSURE GAUGE INDICATED ZERO. MAINTENANCE FOUND HYDRAULIC PRESSURE NORMAL AFTER BYPASSING FLAP SYSTEM BY PULLING 'FLAP CONTROL' C/B. RT ENGINE HYDRAULIC PUMP AND FILTSDR 95ZZZW53Hyd Hose · failedSLOW LEAK IN 'A' SYSTEM, HYD 1.5 GALLONS REMAIN IN RESERVOIR 'B' SYSTEM RESERVOIR FULL. ENGINE NR 2 HYDRAULIC LOW PRESS LIGHT CYCLES ON AND OFF APPROX 1 CYCLE PER MINUTE WITH ENGINE NR 1 'A' HYDRAULIC PUMP SWITCH ASSOCIATED FLUID SHUTOFF SWITCH CLOSED. STANDSDR CAL950039Hyd Line · leakingEWR - FLT 0398 - THE BLUE SYSTEM HYDRAULIC QUANTITY DECREASED TO TOP OF YELLOW ARC WHILE IN FLIGHT. THE SERVOS WERE TURNED OFF PER THE 'ABNORMAL' CHECK LIST AND THE HYDRAULIC FLUID LOSS CEASED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A BLUE SDR 95ZZZW124Hydraulic Line · defectiveFLT 4133 - DURING CRUISE, 11,000 MSL FLIGHT CREW HEARD AN UNUSUAL NOISE FROM THE ENGINE NACELLES. BOTH HYDRAULIC PRESSURE GAUGES WERE AT NEAR '0' PSI INDICATION. ACFT DIVERTED TO HARRISBURG, PA WHERE IT MADE AN EMERGENCY LANDING WITHOUT INCIDENT. MAINTENANCSDR USAA950027Hyd Fitting · leakingPHL - FLT 8610 - FLIGHT EN ROUTE BUT TO ACY WHEN AIRCRAFT LOST 'A' SYSTEM HYDRAULICS. FLIGHT DIVERTED TO PHL WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENACNE REPLACED BROKEN FITTING AT LEFT MAIN GEAR DOWN LINE RESTRICTOR. ALSO, REPLACED NR 1 AND NR 2SDR UPS201953Hyd Syst · overservicedPILOT REPORTED, AIR CONDITIONING FUMES STILL EVIDENT ESPECIALLY AT HIGH POWER SETTING. FOUND HYDRAULIC SYSTEM OVERSERVICED. DRAINED HYD FLUID TO PROPER LEVEL.SDR DLM88950177Hyd Hose · leakingDURING CLIMBOUT, ON FLAP SLAT RETRACTION HAD TOTAL LOSS OF RIGHT SYSTEM HYDRAULIC PRESSURE AND FLUID. RETURNED TO DFW. FOUND LEAKING LINE AT RIGHT FWD FILTER MODULE IN TAIL COMAPARTMENT. REPLACED LINE OPERATION NORMAL.SDR 95ZZZX487Switch · intermittentTHIS SWITCH WAS CHANGED 183 HOURS AGO PER SB 964A, PART I. NEVER HAD ANY PROBLEMS UNTIL NEW SWITCH WAS INSTALLED, THEN, SWITCH INTERMITTENT. HAVE TO TAP SWITCH AT TIMES TO MAKE HYDRAULIC PUMP WORK, GIVES NO WARNING WHEN IT FAILS, PIPER PN 765-457. PARKER HASDR 95ZZZX557Line · leakingPILOT REPORTED DURING GEAR EXTENSION, HYDRAULIC QUANTITY AND MAIN ACCUMULATOR PRESSURE DROPPED TO ZERO. MAINTENANCE INSPECTED AND FOUND HYDRAULIC LINE FROM THE PUMP TO THE FILTER LEAKING. THE LINE WAS REPLACED AND A FUNCTIONAL CHECK OF THE SYSTEM PERFORMED WSDR USAA950013Hyd Line · failedCLT - FLT 1243 - FLIGHT EN ROUTE PHL TO ATL WHEN 'A' SYSTEM HYDRAULIC QUANTITY INDICATED ZERO. FLIGHT DIVERTED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED HYDRAULIC PRESSURE LINE ABOVE LEFT MAIN GEAR AND 'A' SYSTEM PRESSURE FILTERSDR COM60379Valve · inopTASK NR 002-05-900-991, RT ENGINE HYDRAULIC SHUT OFF VALVE DOES NOT CLOSE DURING RT FIREX PUSH TEST. REPLACED S.O.V.SDR COM11719Hyd Syst · frozenGREEN SYSTEM HYDRAULIC RESEVOIR LOW PRESSURE INDICATOR ON. RESERVOIR PRESSURIZATION SYSTEM CONTAINED MOISTURE WHICH FROZE. PURGED MOISTURE FROM SYSTEM.SDR 95ZZZX544Hyd System · required serviceNAS/FLL - FLT 424 - PILOT REPORT: 1) HYDRAULIC FLUID LEAK LEFT SIDE. 2) LEFT MAIN GEAR DOWN LIGHT DOES NOT COME ON WITH GEAR EXTENDED. MAINTENANCE: FERRIED AIRCRAFT TO MIA. FOUND HYDRAULIC SYSTEM LOW ON FLUID, BLED HYDRAULIC SYSTEM, PERFORMED GEAR RETRASDR 95UAL737001Hyd Fluid · low qty'A' SYSTEM HYDRAULIC QUANTITY DROPPED TO ONE FOURTH FULL AFTER TAKEOFF. 'A' SYSTEM EMPTY, LOW PRESSURE LIGHTS ON.SDR CAL950001Hyd Line · chafedFLT NR 1680 - ORD - THE 'A' SYSTEM HYDRAULIC QUANTITY INDICATION SLOWLY DROPPED TO ZERO WHILE EN ROUTE FROM MCI TO MKE. THE AIRCRAFT WAS DIVERTED TO ORD. THE 'A' SYSTEM LOW PRESSURE LIGHTS BEGAN TO FLICKER ON AND OFF WHILE ON FINAL APPROACH. THE AIRCRAFT LASDR 95ZZZX674Tube · rupturedAFTER DEPARTURE FROM FXE, ONE HOUR INTO FLIGHT, A/C LOST HYDRAULIC PRESSURE AND LT MAIN GEAR EXTENDED AT 410. PILOT REDIRECTED FLIGHT TO FLL FOR LANDING FOLLOWING EMERGENCY PROCEDURES. EXTENDED GEAR USING BLOW-DOWN PROCEDURES. GEAR EXTENDED AND AIRCRAFT LAN
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