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 2001F00022Hydraulic Line · chafedDCA - FLT 2299 - AFTER TAKEOFF FROM \, AS CREW RETRACTED THE LANDING GEAR, THEY RECEIVED A RED LIGHT FOR THE RT MLG. SHORTLY AFTER, THEY RECEIVED A RED LIGHT FOR THE 'A' SYSTEM HYDRAULIC. CREW CONTINUED THEIR CLIMB TO FL190 AND THEN PERFORMED PROCEDURES FOR SDR USAASB01156Hydraulic Line · leakingDCA - FLT 2299 - AFTER T/O , AS THE LANDING GEAR RETRACTED, RECEIVED A RED LIGHT FOR THE RT MLG. THEN RECEIVED A RED LIGHT FOR THE A SYS HYDRAULIC. CONTINUED TO CLIMB TO FL190 THEN PERFORMED PROCEDURES FOR A SYS HYDRAULIC FAILURE. DECLARED AN EMERGENCY AND RETSDR AUS20010703Pipe · leaking(AUS) UTILITY HYDRAULIC SYSTEM SUCTION PIPE CONTAINED A PIN HOLE LEAK.LOSS OF HYDRAULIC FLUID.SDR UPS01536014Hydraulic Line · leakingINSPECTION TYPE:N/A ATB-LOSS OF HYD FLUID. *S/D* INSTALLED TEMP FLEX LINE HOSE ON LT MLG SIDE STRUT ACTUATOR LEAK CHECKS OK. REMOVED AND REPLACED HYD PUMP AND FILTERS IAW MM 29-11-05, OPS AND LEAKS CHECK GOOD.SDR DL757010856Hydraulic Line · leakingAFTER TAKEOFF GEAR DOORS LIGHT AND ADVISORY MESSAGE ON WHEN GEAR RAISED. GEAR RECYCLED, LIGHT STILL ON. FLT ATTN REPORTS VIBRATION IN FLOOR NEAR GEAR DOOR AREA. FOUND FLEX HYD LINE LEAKING ABOVE RT MLG. MADE APPROVED HYD REPAIR. INSTALLED TEMP HYD LINE PESDR CA010628042Hose · ruptured(CAN) HYDRAULIC HOSE RUPTURE AT FITTING P/N MS24590-4. FITTING M524590-4 HAD WORN INTERNAL THREADS WHEN HOSE WAS MANUFACTURED. HOSE AND FITTING SEPARATED ON GEAR CYCLE.SDR AUS20010568Manifold · cracked(AUS) HYDRAULIC POWER TRANSFER UNIT (PTU) MANIFOLD CRACKED AND LEAKING IN AREA OF CHECK VALVE MOUNTING FLANGE.SDR CA010621035Line · leaking(CAN) MAINTENANCE INVESTIGATION OF A HYDRAULIC FLUID LEAK IN THE NR 1 MLG BAY RESULTED IN THE REPLACEMENT OF THE DOOR OPEN LINE TO THE SEQUENCE VALVE. THE LINE WAS LEAKING FROM A PINHOLE AT A FACTORY BEND. TTAF 23453, TCAF 34772.SDR ARWA0010503O-Ring · failedON APPROACH TO TNCC (CURAZAO) LOSS OF HYDRAULIC FLUID. PERFORMED EMERGENCY CHECKLIST AS PER ARROW AIR PROCEDURE. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED O-RING FROM NR 3 ENGINE DRIVEN HYDRAULIC PUMP PRESSURE LINE ELBOW IAW MM 29-10-12, LEAK CKD OK, OPERASDR SIMA20011428Hydraulic System · lack of lubeRIC - FLT 4944 - CREW REPORTED THE NR 1 HYDRAULICS SYSTEM LOW LIGHT CAME ON FOLLOWED BY A NR 1 ENGINE HYDRAULIC SYSTEM FAILURE. SYSTEM PRESSURE DROPPED TO ZERO AND WAS REGAINED UPON LANDING GEAR EXTENSION. MAINTENANCE SERVICED THE NR 1 HYDRAULIC SYSTEM IAW ESDR 2001F00016Hydraulic Line · leakingAEROQUIP HOSE, STEEL BRAIDED G01, THAT GOES TO THE NOSE GEAR ACTUATOR DEVELOPED A LEAK IN THE MIDDLE OF THE HOSE ASSEMBLY, RESULTING IN LOSS OF HYDRAULIC FLUID. AIRCRAFT WAS UNABLE TO LOWER THE RIGHT MAIN GEAR, DAMAGE TO THE AIRCRAFT WAS MINOR.SDR DLM88010791Hydraulic Line · leakingLEFT HYD QTY 4 COMPLIED W/POM, WHEN SYS REPRESSURIZED ON APPROACH GOT ZERO PRESSURE INDICATION. FOUND T/R LINE LEAKING IN 48 SECTION. REMOVED AND REPLACED SAME, SERV HYD. OK FOR SERVICE.SDR 01FDEA00372Line · leakingAFT T/O FLT CONTROL LIGHTS CAME ON AND B-SYS QUANTITY WENT TO ZERO. *S/D* REMOVED AND REPLACED FLEX LINE IN 727-200 MM 20-10-012. OK FOR SERVICE.SDR DLM88010788Line · looseLEFT HYD QTY DECREASED TO 3 QTS CLIMBING THRU 17K. TURNED OFF LEFT ENG HYD PUMP AND QTY INCREASED TO 15 QTS. ON FINAL W/ LEFT ENG PUMP AND XFER PUMP ON LEFT HYD QTY AND PRESS WENT TO 0. MTC NOTED EMPTY RESERVOIR. FOUND T/R CNTRL VLV LINE LEAKING. SECURESDR AUS20010501Elbow · cracked(AUS) HYDRAULIC SYSTEM LEAKING FROM CRACKED PRESSURE LINE ELBOW LOCATED UNDER NO3 STRUT REAR SAILBOAT. LOSS OF HYDRAULIC FLUID.SDR 0101835501Hydraulic Line · rupturedDURING APPROACH AFTER GEAR EXTENSION, THE LEFT HYDRAULIC SYSTEM LOST ALL FLUID. AN EMERGENCY WAS DECLARED WITH DFR EQUIPMENT CALLED OUT. LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE RUPTURED NOSE GEAR STEERING HYDRAULIC LINE AND SERVICED THE LEFT HYDRAUSDR F3LA200100065B-Nut · looseDURING TRAINING FLIGHT, FLIGHT CREW REPORTED LOSS OF GREEN HYDRAULIC SYSTEM. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED IN PHX WITHOUT INCIDENT. AIRCRAFT WAS TOWED OFF THE RUNWAY DUE TO THE LOSS OF THE NOSE WHEEL STEERING. THE B-NUT ON THE HYDRAULIC PRESSDR HEEA073093Elbow · chafedON FINAL APPROACH, THE OIL COOLER LIGHT ILLUMINATED. FOUND THE UTILITY HYDRAULIC SYSTEM LOST FLUID. MAINTENANCE FOUND LEAK AT ELBOW WHERE THE SUPPORT HAD CHAFED THROUGH DUE TO JAM NUT BEING LOOSE.SDR C2XA01CL105O-Ring · damagedCLE FLIGHT 3812 THE CREW REPORTED THE GREEN AND BLUE HYDRAULIC LOW LEVEL WARNING CAME ON INFLIGHT. THE CREW DECLARED A EMERGENCY AND LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND A O-RING LEAKING ON A UNION ON THE BLUE SYSTEMSDR 20010605CW009Cover · crackedCOVER FOUND TO BE CRACKED IN TWO PLACED DURING NDI. PROBABLE CAUSE: FATIGUE.SDR ASOA01051Hydraulic Line · chafedFLT 4456 - INBOUND TO DFW FROM LBB, AIRCRAFT LOST GREEN SIDE HYDRAULICS AND HAD TO MANUALLY EXTEND THE GEAR. CREW DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY IN DFW. MAINTENANCE REPLACED LEFT ENGINE HYDRAULIC PUMP, HYDRAULIC RESERVOIR FILTERS ON LEFT SIDESDR HEEA073103Pressure Switch · inaccurateINACCURATE READINGS.SDR CA010509012Line · leaking(CAN) RT LIFT DUMP PRESSURE HYDRAULIC LINE FOUND LEAKING FROM A BEND IN THE LINE LOCATED APPROXIMATELY 6 INCHES FROM THE FITTING IN THE RIGHT NACELLE. THE HYDRAULIC LINE WAS REPLACED AND ALL CHECKS COMPLETED.SDR CA010529003Line · broken(CAN) ON LANDING THE PILOT PUMPED THE FLAPS DOWN, WHEN THE FLAPS REACHED THE DOWN POSITION THE HYDRAULIC LINE TO THE FLAP SELECTOR BROKE, LEAKING HYDRAULIC FLUID ON TO THE FLOOR. THE PILOT LANDED THE AIRCRAFT WITHOUT INCIDENT. UPON INVESTIGATION THE AME FOUND SDR AWXA0001693O-Ring · damagedSJC - EMERGENCY LANDING - 4/27/01 - FLT 285 - EN ROUTE FROM PHX TO SJC THE CREW REC''D AN ECAM MSG HYD Y RSVR LO LVL FOLLOWED BY HYD Y ENG 2 PUMP LO PR. PERFORMED ECAM ACTIONS AND CONTINUED TO LANDING IN SJC. IN SJC MAINTENANCE FOUND THE CENTER FITTING ON AUSDR CA010522006Case · cracked(CAN) AFTER TAKEOFF TRAILING EDGE FLAPS WOULD NOT RETRACT. AFTER SEVERAL ATTEMPTS FLAPS RETRACTED. FLIGHT CONTINUED, LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTION REVEALED TRAILING EDGE FLAP BYPASS VALVE MALFUNCTIONING. VALVE REPLACED. SUBSEQUENT VALSDR GAIA01156OPHydraulic Line · leakingFLT 1850 - PDX-SEA - UPON LANDING GEAR EXTENSION, LOST A SYSTEM HYDRAULICS QUANTITY WENT TO ZERO. AIRCRAFT MADE AN UNEVENTFUL LANDING IN SEA. INSPECTION OF AIRCRAFT FOUND LEAKING LEFT GEAR DOOR ACTUATOR RETURN HOSE. REMOVED AND LEFT ACTUATOR RETURN HOSE. REMSDR HEEA072898Motor · seizedTHE UTILITY HYDRAULIC SYSTEM FAILED IN FLIGHT. MAINTENANCE REPLACED SEIZED HYDRAULIC MOTOR.SDR HEEA072897O-Ring · leakingTHE UTILITY HYDRAULIC SYSTEM FAILED IN FLIGHT. MAINTENANCE REPLACED LEAKING O-RINGS ON HYDRAULIC MOTOR.SDR HEEA072896O-Ring · leakingTHE UTILITY HYDRAULIC SYSTEM FAILED IN FLIGHT. MAINTENANCE REPLACED LEAKING O-RINGS ON HYDRAULIC MOTOR.SDR HEEA072895Tube · crackedDURING CRUISE FLIGHT THE NR 1 HYDRAULIC SYSTEM LIGHT CAME ON. MAINTENANCE FOUND A CRACKED TUBE.SDR ABXA010215Relief Valve · leakingTHE RIGHT HYDRAULIC QUANTITY DECREASED TO .67. THE ENGINE DRIVEN PUMP DE-PRESSURIZED AND THE ALTERNATING CURRENT MOTOR PUMP WAS SELECTED OFF. MAINTENANCE INSPECTED AND REPLACED THE FILTER MODULE RELIEF VALVE IAW B767 29-11-17. OPS AND LEAK CHECKS WERE COMPLSDR AALA20010888Hose · leakingJFK - FLT 1152 - EN ROUTE MIA-JFK, ON SHORT FINAL GREEN HYDRAULIC SYSTEM DECREASED TO ZERO. HYDRAULIC PUMPS WERE IMMEDIATELY SHUT OFF. LANDED JFK WITHOUT FURTHER INCIDENT. REPLACED LEFT SIDE MAIN LANDING GEAR PRESSURE FLEXIBLE HOSE. SERVICED GREEN SYSTEM. SDR 20010605CW006Housing · damagedHOUSING HAS A PINHOLE LEAK OUTSIDE OF PORT NR 1.SDR AALA20010886Plug · looseDFW - FLT 1104 - EN ROUTE LAS-DFW - DETECTED DECREASE RIGHT SIDE HYDRAULIC QUANTITY. RIGHT SIDE HYDRAUILC SYSTEM SHUT OFF WITH A QUANTITY OF FOUR QUARTS. LANDED WITHOUT FURTHER INCIDENT. RE-SECURED PLUG AT RIGHT SIDE RUDDER SHUTOFF VALVE. NO LEAKS NOTED. SSDR 0101533208O-Ring · leakingDURING CRUISE, RECEIVED HYD Y RSVR LO LVL MESSAGE. PERFORMED COM PROCEDURES AND CONTINUED TO FINAL DESTINATION WITH A NORMAL LANDING. MAINTENANCE REPLACED O-RING AT ENGINE NR 2 PYLON CHECK VALVE. LEAK CHECK OK.SDR DL757010684Hydraulic Line · rupturedLEFT HYD QTY LOSS IN FLIGHT. UNABLE TO STOP LOSS WITH POM PROCEDURES. FOUND RIGHT GEAR TRUCK TILT PRESSURE LINE RUPTURED. REPLACED LINE.SDR CA010529006Manifold · leaking(CAN) YELLOW SYSTEM LOW LEVEL ECAM ON DESCENT INTO YYC - MAJOR HYDRAULIC LEAK EVIDENT AT BLOCK IN ON RAMP. FOUND YELLOW LEAK MEASUREMENT MANIFOLD LEAKING. REPLACED HYDRAULIC LEAK MEASUREMENT MANIFOLD. SYSTEM CHECKS SERVICEABLE IAW 29-19-41-401.. . . .SDR DLM88010670Hydraulic Line · leakingLOSS OF HYD FLUID ON RT SIDE. STOPPED AT 1 QT. MTC FOUND LINE TO RT HYD FILTER MODULE LEAKING. LINE WAS REPLACED.SDR CA010529022Tube · leaking(CAN) DURING A WALK-AROUND, THE FLIGHT CREW NOTED FLUID LEAKING FROM THE R/H WING. MAINTENANCE FOUND THE HYDRAULIC TUBE (PRESSURE) TO THE R/H INBOARD ROLL SPOILER ACTUATOR LEAKING (PIN HOLE). THE HYDRAULIC TUBE WAS REPLACED AND ALL CHECKS COMPLETED. . . . .SDR DL72S010655Hydraulic Line · damagedTOTAL LOSS OF A SYSTEM HYDRAULICS ON DEPTATURE. LOST BOTH PRESSURE AND QUANTITY WHEN FLAPS WERE RETRACTED FROM 15 TO 5 FOUND LINE TO RIGHT MLG DOOR WITH HOLE IN LINE REPLACED LINE.SDR SIMA20011101Hydraulic Line · rupturedLAX - FLT 3035 - CREW REPORTED A LOSS OF HYDRAULIC FLUID. AOM PROCEDURES WERE FOLLOWED, GEAR WAS BLOWN DOWN AND AIRCRAFT WAS LANDED SAFELY. MAINTENANCE FOUND A HYDRAULIC LINE IN THE NOSE WHEEL WELL RUPTURED. LINE WAS REPLACED, LEAK CHECK WAS GOOD AND AIRCRASDR AU010375Hydraulic System · low(AUS) HYDRAULIC A SYSTEM QUANTITY AND PRESSURE LOST.SDR AU010373Hose · failed(AUS) NR 1 HYDRAULIC PUMP PRESSURE HOSE FAILED. LOSS OF HYDRAULIC FLUID.SDR UPS01535632Switch · failedENG START MAIN CARGO SMOKE DETECTION INDICATED SMOKE ALONG WITH ACRI D ODOR IN COCKPIT T/S TO LEFT HYDRAULIC ACMP SWITCH FAILED R&R SWITCHSDR CA010515008Solenoid Valve · failed(CAN) HYD BLOCK LIGHT CAME ON IN FLIGHT. PILOT RETURNED TO BASE AND CALLED OUT RESCUE CREW. LANDED WITHOUT DIFFICULTY. SOLENOID VALVE REPLACED AND AIRCRAFT RETURNED TO SERVICE ON APRIL 20. AIRCRAFT TEST FLOWN FOR 30 MINUTES AND NO FURTHER LIGHT REPORTS.SDR CA010511008Line · chafed(CAN) UPON CLIMBING, CREW RECEIVED A HYDRAULIC NR 1 LOW PRESSURE MESSAGE, ASSOCIATED WITH A NR 1 SYSTEM, QUANTITY INDICATING ZERO PERCENT. AIRCRAFT DIVERTED TO BIRMINGHAM. MAINTENANCE FOUND A CHAFED STEEL BRAIDE HYDRAULIC LINE IN AFT FUSE. THE LINE IS THE PESSSDR USAASB01103Hydraulic Line · leakingLGA-JAX - FLT 2650 - DURING CRUISE, THE ''A'' SYSTEM HYDRAULIC QUANTITY DECREASED TO ZERO. AN EMERGENCY WAS DECLARED AND THE FLIGHT DIVERTED TO CLT. EN ROUTE TO CLT, BOTH ''A'' SYSTEM LOW PRESSURE LIGHTS ILLUMINATED. FLIGHT LANDED WITHOUT FURTHER INCIDENT ASDR AC2A072829Hose · chafedPART IS CHAFED. LINE CHAFED ON TRANSMISSION COWLING. INSTALLED NEW LINE. REPOSITIONED ELBOW FOR NEW LINE TO CLEAR TRANSMISSION COWLING.SDR IXXA0100016Swivel · leakingAFTER TAKEOFF FROM TOL, THE FLIGHT CREW NOTICE A DECLINED IN THE MAIN HYDRAULIC QUANTITY SYSTEM. THE FLIGHT RETURNED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT LOCATING A RUPTURED LEFT AILERON SWIVEL GLAND. MAINTENANCE REPACKED THE
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