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.

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 Jun 2, 2001 · N389US · Boeing 7373B7SDR 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 RETJun 2, 2001 · N389US · Boeing 7373B7SDR AUS20010703Pipe · leaking(AUS) UTILITY HYDRAULIC SYSTEM SUCTION PIPE CONTAINED A PIN HOLE LEAK.LOSS OF HYDRAULIC FLUID.Jun 1, 2001 · Fokker F28MK1000SDR 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.May 30, 2001 · N406UP · Boeing 75724APFSDR 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 PEMay 28, 2001 · N647DL · Boeing 757232SDR 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.May 27, 2001 · Piper PA31SDR AUS20010568Manifold · cracked(AUS) HYDRAULIC POWER TRANSFER UNIT (PTU) MANIFOLD CRACKED AND LEAKING IN AREA OF CHECK VALVE MOUNTING FLANGE.May 25, 2001 · Airbus A320*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.May 25, 2001 · Dhav DHC8311SDR 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, OPERAMay 25, 2001 · N8969U · Doug DC862SDR 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 EMay 22, 2001 · N736DT · Emb EMB135LRSDR 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.May 22, 2001 · N4DU · Cessna P337HSDR 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.May 18, 2001 · N989DL · Doug MD88SDR 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.May 18, 2001 · N278FE · Boeing 727233SDR 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. SECUREMay 17, 2001 · N918DL · Doug MD88SDR AUS20010501Elbow · cracked(AUS) HYDRAULIC SYSTEM LEAKING FROM CRACKED PRESSURE LINE ELBOW LOCATED UNDER NO3 STRUT REAR SAILBOAT. LOSS OF HYDRAULIC FLUID.May 16, 2001 · Boeing 747SP38SDR 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 HYDRAUMay 16, 2001 · N501US · Boeing 757251SDR 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 PRESMay 16, 2001 · N901FR · Airbus A319111SDR 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.May 14, 2001 · N59806 · Bell 214STSDR 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 SYSTEMMay 13, 2001 · N17831 · Aerosp ATR42320SDR 20010605CW009Cover · crackedCOVER FOUND TO BE CRACKED IN TWO PLACED DURING NDI. PROBABLE CAUSE: FATIGUE.May 11, 2001 · Boeing 737SDR 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 SIDEMay 10, 2001 · N232AS · Emb EMB120RTSDR HEEA073103Pressure Switch · inaccurateINACCURATE READINGS.May 10, 2001 · N4000L · Snias AS350B2SDR 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.May 9, 2001 · Dhav DHC8102SDR 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 May 5, 2001 · Dhav DHC3SDR 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 AUMay 3, 2001 · N658AW · Airbus A319132SDR 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 VALMay 1, 2001 · Boeing 737275SDR 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. REMMay 1, 2001 · N79748 · Boeing 727224SDR HEEA072898Motor · seizedTHE UTILITY HYDRAULIC SYSTEM FAILED IN FLIGHT. MAINTENANCE REPLACED SEIZED HYDRAULIC MOTOR.May 1, 2001 · N59806 · Bell 214STSDR HEEA072897O-Ring · leakingTHE UTILITY HYDRAULIC SYSTEM FAILED IN FLIGHT. MAINTENANCE REPLACED LEAKING O-RINGS ON HYDRAULIC MOTOR.May 1, 2001 · N59806 · Bell 214STSDR HEEA072896O-Ring · leakingTHE UTILITY HYDRAULIC SYSTEM FAILED IN FLIGHT. MAINTENANCE REPLACED LEAKING O-RINGS ON HYDRAULIC MOTOR.May 1, 2001 · N59806 · Bell 214STSDR HEEA072895Tube · crackedDURING CRUISE FLIGHT THE NR 1 HYDRAULIC SYSTEM LIGHT CAME ON. MAINTENANCE FOUND A CRACKED TUBE.May 1, 2001 · N3911L · Bell 412SDR 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 COMPLMay 1, 2001 · N775AX · Boeing 767281SDR 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. Apr 30, 2001 · N14061 · Airbus A300B4605RSDR 20010605CW006Housing · damagedHOUSING HAS A PINHOLE LEAK OUTSIDE OF PORT NR 1.Apr 30, 2001 · Boeing 737SDR 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. SApr 30, 2001 · N427AA · Doug DC982SDR 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.Apr 28, 2001 · N308US · Airbus A320211SDR 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.Apr 27, 2001 · N648DL · Boeing 757232SDR 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.. . . .Apr 26, 2001 · Airbus A320232SDR 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.Apr 24, 2001 · N968DL · Doug MD88SDR 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. . . . .Apr 23, 2001 · Dhav DHC8102SDR 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.Apr 21, 2001 · N540DA · Boeing 727232SDR 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 AIRCRAApr 20, 2001 · N349SB · Saab 340BSDR AU010375Hydraulic System · low(AUS) HYDRAULIC A SYSTEM QUANTITY AND PRESSURE LOST.Apr 20, 2001 · Boeing 737377SDR AU010373Hose · failed(AUS) NR 1 HYDRAULIC PUMP PRESSURE HOSE FAILED. LOSS OF HYDRAULIC FLUID.Apr 20, 2001 · Boeing 747438SDR 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 SWITCHApr 20, 2001 · N451UP · Boeing 75724APFSDR 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.Apr 19, 2001 · Bolkms BO105CSDR 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 PESSApr 19, 2001 · Cndair CL6002B19SDR 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 AApr 19, 2001 · N283AU · Boeing 7372B7SDR AC2A072829Hose · chafedPART IS CHAFED. LINE CHAFED ON TRANSMISSION COWLING. INSTALLED NEW LINE. REPOSITIONED ELBOW FOR NEW LINE TO CLEAR TRANSMISSION COWLING.Apr 19, 2001 · N430CV · Bell 430SDR 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 THEApr 18, 2001 · N824BX · Doug DC871F
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