JASC 2910
Service difficulty reports · 11,292
Reports filed under 2910 · Hydraulic System, Main, newest first.
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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"
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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 QXEA0201591Hydraulic System · lowSEA - AIRCRAFT RETURNED TO FIELD WHEN HYDRAULIC PRESSURE INDICATED 0 AND QUANTITY INDICATED LOW. MAINTENANCE INSPECTED THE AIRCRAFT AND SERVICED THE NR 1 AND 2 HYDRAULIC SYSTEMS. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR PCAA0210116Line · leakingROC-DCA FLIGHT#3793. CREW REPORTED WHILE AT 17,000 FEET #2 HYDRAULIC ISOLATION VALVE LIGHT ILLUMINATED WITH .5 QUARTS INDICATED ON #2 SYSTEM. FLIGHT DIVERTED TO MDT, EMERGENCY DECLARED, AIRCRAFT LANDED WITH OUT INCIDENT. MAINTENANCE FOUND HYDRAULIC LINE TO GEASDR AUS20021091Pipe · loose(AUS) HYDRAULIC SYSTEM PIPE FROM FIREWALL DISCONNECTED. LOSS OF HYDRAULIC FLUID. PERSONNEL/MAINTENANCE ERROR.SDR AUS20021090Pipe · chafed(AUS) LT ENGINE DRIVEN HYDRAULIC PUMP ALUMINIUM SUPPLY LINE CHAFING ON A STAINLESS STEEL FUEL LINE. THE HYDRAULIC LINE CHAFED THROUGH RESULTING IN LOSS OF HYDRAULIC FLUID.SDR DHL2002747006Solenoid Valve1) IN FLIGHT, HYDRAULIC SYSTEM "A" DECREASED TO 0.2. ENGINE #1 LOW PRESSURE LIGHT ILLUMINATED INTERMITTENTLY. PERFORMED ABNORMAL PROCEDURES. "A" HYDRAULIC SYSTEM FLUID SHUTOFF SWITCHED CLOSED FOR 7 MINUTES. (NOTE: DHL INSPECTION AND SURVEILLANCE REPORT DATED SDR 043682Motor · failedON AN ATTEMPT TO LAND, THE CREW TRIED TO EXTEND LANDING GEAR, BUT THE CIRCUIT BREAKER POPPED. THEY RESET CIRCUIT BEAKER ND LANDING GEAR STILL WOULD NOT EXTEND. THE CREW PERFORMED AN EMERGENCY EXTENSION. RECEIVED 3 GREEN GEAR DOWN INDICATORS. THE CREW DECLARED SDR IU62002F00034Housing · crackedTHE HOUSING IS CRACKED THROUGH INTERNALLY FROM ONE VALVE TO ANOTHER. PROBABLE CAUSE COULD BE WEAK MATERIAL OR OVER PRESSURIZATION.SDR MALA020589Connector · looseDURING FLIGHT 2991 FLIGHT CREW BLEW LANDING GEAR DOWN AFTER HYDRAULIC CAUTION LIGHT ILLUMINATED. EMERGENCY AND MAIN ACC INDICATED LOW. LOWERED GEAR HANDLE AND PULLED EMERGENCY EXTENSION HANDLE PER MEMORY ITEM. GEAR LOCKED IN DOWN POSITION OK. MAINTENANCE ASDR DLM88021147Fitting · looseLT HYDRAULIC SYSTEM QUANTITY INDICATES 1 QUART. PRESSURE 3100 PSI. PER CREW COMMENT PUMPS SHUT DOWN-0 PSI WHEN PUMPS REAPPLIED. TIGHTENED LOOSE LT THRUST REVERSER CONTROL VALVE HYDRAULIC LINE. A/C DUE DUCT BURNOUT.SDR CA021115003Hose · leaking(CAN) HYDRAULIC PRESSURE HOSE WAS LEAKING.SDR ALG2003F00042Switch · failedDURING CRUISE FLIGHT, NR 2 SERVO SYSTEM CAUTION LIGHT ILLUMINATED, AIRCRAFT WAS DIVERTED TO INTRACOASTAL, PILOT FOLLOWED EMERGENCY CHECKLIST AND LANDED AT INTRACOASTAL. UPON LANDING, THE MECHANIC REMOVED AND REPLACED REARWARD PRESSURE SWITCH ON LEFT FORWARD SSDR AUS20021110Line · cracked(AUS) FLAP "UP" HYDRAULIC LINE FLARED END CRACKED. LINE IS LOCATED INBOARD OF THE REAR LT NACELLE.SDR 2003F00054Coupling · looseTHE FLIGHT CREW NOTED A COMBINED HYDRAULIC SYSTEM FAILURE MESSAGE. THE SYSTEM LOST PRESSURE DUE TO FLUID STARVATION AT THE SUPPLY LINE TO THE HYDRAULIC PUMP ON THE LEFT ENGINE. THE QUICK DISCONNECT COUPLING APPARENTLY HAD NOT BEEN LOCKED INTO PLACE. THE QUISDR AALA20021350Hydraulic Line · looseMIA - FLT 1193 - EN ROUTE JFK-MBJ, PASSENGER REPORTED WHITE STREAK COMING OFF LEFT WING DURING CRUISE. CREW INVESTIGATED SHUTDOWN LEFT ENGINE PER FUEL LEAK CHECK LIST. LANDED AT MIA WITHOUT INCIDENT. INSPECTED AND FOUND HYDRAULIC LINE LEAKING. TIGHTENED LESDR 2002UALA01485Manifold · damagedRETURNED TO FIELD DUE TO A YELLOW HYDRAULIC LOW LEVEL INDICATION. FOUND TOP CENTER PLUG OF YELLOW SYSTEM LEAKAGE MEASUREMENT VALVE BLOWN OUT. REPLACED GROUND LEAKAGE-MEASUREMENT MANIFOLD OF THE YELLOW SYSTEM, SERVICE YELLOW SYSTEM TO FULL.SDR CA020926005Line · cracked(CAN) HYDRAULIC LINE FOUND CRACKED FROM DRAIN ON LOWER BELLY AND RT WING FAIRING. LIFT DUMP PRESSURE TUBE ASSY IN RT WING REPLACED. LINE CRACKED AT FIRST ELBOW FROM I/B END OF LINE. IPC REF 29-00-00 FIG 60 ITEM 140.SDR DLM88021112B-Nut · looseAIRCRAFT RETURNED TO RAMP DUE TO SMOKE IN CABIN. FOUND HYD LINE B-NUT LOOSE AND LEAKING AT LT THRUST REVERSER CONT VALVE. TIGHTENED LINE AND LEAK CHECKS GOOD. REPLACED RT AND LT COALESCER BAGS. LEAK CHECKS OK. PERFORMED OP 5089 DUCT BURNOUT. CHECKS OK.SDR ARWA20020915Hydraulic Line · leakingLOSS OF HYDRAULIC FLUID IN FLIGHT, PERFORMED EMERGENCY CHECKLIST AND LANDED IN MIA WITHOUT FURTHER INCIDENT. FOUND NR 2 ENGINE HYDRAULIC CASE DRAIN LINE LEAKING. REMOVED & REPLACED LINE IAW MM 20-12-0. SERVICED HYDRAULIC FLUID IAW MM 12-30-1, PREFORMED LEAKSDR 02FDEA00669B-Nut · looseIN CRUISE GOT HYD 3 ELEV OFF THEN 3-2 NRMP INOPERATIVE LOSS OF NR 3 HYD FLUID, THEN HYD NR 3 FAILED. DUMPED APPROX 50000 LBS OF FUEL AND LANDED AT ORD, DECLARED EMERGENCY AND PULLED CVR. FOUND LOOSE B-NUT AT CHECK VALVE IN AFT ACCESSORY COMP RT SIDE. TIGHTESDR CA021007012Line · cracked(CAN) ON A TURN AROUND IN THE MECHANIC FOUND AN HYDRAULIC LEAK IN THE WHEEL WELL. HE DECIDED TO REPLACE THE RIGID LINE WITH A TEMPORARY FLEX HYDRAULIC LINE AS PER M.M. 20-12-04. THE MECHANIC CHOOSE THE WRONG TYPE OF LINE (MEDIUM PRESS LINE INSTEAD OF HIGH PRESSDR AUS20021069Powerpack · contaminated(AUS) HYDRAULIC POWER PACK CONTAMINATED BY UNKNOWN BIOLOGICAL GROWTH.SDR PNSA020904Hydraulic Line · crackedAfter selecting gear down on arrival to ANC (flaps were set to 1/2) LH hydraulic warning came on, 2 seconds later RH hyd warning came on. Performed required checklists and declared emergency. Landing was normal without nosewheel steering and flaps at 1/2. MainSDR CA020918005Actuator · failed(CAN) YELLOW HYDRAULIC SYSTEM LOST FLUID AND CABIN FILLED WITH SMOKE. YELLOW SYSTEM YAW DAMPER ACTUATOR FOUND LEAKING. YAW DAMPER CHANGED AS PER AMM. YAW DAMPER OPERATION CHECK CARRIED OUT AS PER AMM.SDR USAABB02160Hydraulic Line · leakingCLT - FLT 1892 - ON GEAR EXTENSION FOR LANDING, CREW NOTED LOSS OF HYDRAULIC QUANTITY ON THE LEFT SYSTEM. CREW PERFORMED A TOWER FLYBY TO ENSURE THE GEAR DOWN AND LOCKED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEASDR COMA0260531Hydraulic LineHYDRAULIC NUMBER ONE LOW PRESSURE CAUTION.TIGHTENED LOOSE QUICK DISCONNECT FITTING ON HYDRAULIC PRESSURE LINE AT PYLON FIRE WALL.SDR ESUA116360Line · loosePILOT DECLARED AN EMERGENCY ON APPROACH, IT WAS DISCOVERED THAT THE HYDRAULIC PRESSURE INDICATED (0). THE GEAR WAS ABLE TO BE PLACED IN THE DOWN AND LOCKED POSITION WITH NO EMERGENCY PROCEDURES. AIRCRAFT LANDED ON 13L. THE AIRCRAFT WAS STOPPED ON THE RUNWAYSDR CA021003007Hose · leaking(CAN) HOSE ASSEMBLY FAILED RESULTING IN LOSS OF HYDRAULIC FLUID. THE LOSS OF FLUID RESULTED IN LOSS OF HYDRAULIC BOOST TO FLIGHT CONTROLS. AIRCRAFT WAS LANDED UNEVENTFULLY WITHOUT HYDRAULIC BOOST. THE HYDRAULIC LINE EXHIBITED NO SIGNS OF LEAKAGE PRIOR TO FAILUSDR MEX2002297Hydraulic Line · leakingFLT 405 - JFK - AIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF AN HYDRAULIC LEAKAGE IN THE RIGHT SYSTEM. TECHNICIAN REVIEWED SUCH SYSTEM AND FOUND LEAKAGE IN A PIPELINE FROM THE FILTERS TO THE WHEELS. PIPELINE WAS REPLACED IAW MM 29-11-17, TESTS OK. (M)SDR 091302Hydraulic Line · loosePILOT DECLARED AN EMERGENCY ON APPROACH INTO DALLAS LOVE FIELD. IT WAS DISCOVERED THAT THE HYDRAULIC PRESSURE INDICATED O. THE GEAR WAS ABLE TO BE PLACED IN THE DOWN AND LOCKED POSITION WITH NO EMERGENCY PROCEDURES. THE AIRCRAFT WAS STOPPED ON THE RUNWAY BYSDR UO22002F00017Line · chafedHYDRAULIC NR 1 PRESSURE LINE AND NR 1RETURN LINE CHAFING IN PYLON.SDR ARWA20020912Line · leakingAFTER LANDING, LOSS HYDRAULIC FLUID TO STANDPIPE. REMOVED AND REPLACED HYDRAULIC BRAKE LINE WITH A FLEX LINE (TEMP) IAW MM 32-42-1 AND GMM 6-6-1 OPS AND LEAK OK IAW MM 32-42-1 SERVICED HYDRAULIC SYSTEM IAW MM 12-03-0. CARRIED OVER ITEM NR 05938 WAS CLOSED ON SDR CA020926002Manifold · bypassing(CAN) AIR TURNBACK DUE TO NR 2 HYDRAULIC FLUID HOT CAUTION LIGHT ON IN FLIGHT. HYDRAULIC PIPES ARE HOT TO TOUCH ON GROUND. NR 2 HYDRAULIC PRESSURE MANIFOLD REPLACED.SDR 2002UALA01435Hydraulic Line · rupturedABORTED TAKEOFF DUE TO ECAM HYDRAULIC GREEN RESERVOIR LOW LEVEL WARNING. FOUND RIGHT HAND MLG DOOR RETRACT ACTUATOR AFT FLEX LINE RUPTURED. REPLACED FLEX LINE.SDR PCAA0209102Hydraulic Line · leakingROC-LGA FLIGHT#3905. CREW REPORTED #2 HYDRAULIC ISOLATION VALVE CAUTION LIGHT ILLUMINATED IN FLIGHT DURING CLIMBOUT. AIRCRAFT DIVERTED TO SYR WITHOUT INCIDENCE. MAINTENANCE REPLACED A HYDRAULIC LINE IN NOSE GEAR AREA, AND SERVICED #2 HYDRAULIC SYSTEM. OPERATIOSDR DLM88021046Line · leakingAPPROCH FLT.615 AT 1329 - RT SYS HYD FLUID LOSS, HYD RETURN LINE WORN THRU RT SIDE AFT ACCESSORY BAY. FLEX LINE PN 299201301 REPLACED. REPLACED RT ENGINE DRIVEN HYD PUMP. REPLACED HYD FILTERS, WASHED APU INLET. REPLACED COALESCER BAGS & PERFORMED PNEUMATIC SDR CA020910005Line · cracked(CAN) CREW REPORTED COMPLETE LOSS OF NR 2 HYDRAULIC SYSTEM AFTER SELECTING GEAR DOWN ON APPROACH. AIRCRAFT LANDED WITHOUT INCIDENT . INSPECTION FOUND NR 2 HYD SYTEM LOSS OF FLUID, LT OUTBOARD ROLL SPOILER RETURN LINE CRACKED & LEAKING. TEMP LINE INSTALLED, ESDR RW82002F00000Line · failedTHE HYDRAULIC PRESSURE LINE FROM THE PUMP HAD FAILED. THE CLAMP THAT SECURES THE HOSE TO THE PYLON DECK HAD CHAFED INTO THE STEEL BRAIDING OF THE LINE, CAUSING A WEAK POINT IN THE LINE, AND THE WALL OF THE HOSE TO RUPTURE THROUGH THE BRAIDING. THUS CAUSING ASDR MALA020549Pressure Switch · failedDURING CLIMBOUT OF FLIGHT 2971 MAIN AND EMERGENCY HYDRAULIC PRESSURE LIGHT ILLUMINATED. FOLLOWED MEMORY ITEMS AND NOTED MAIN AND EMERGENCY ACCUMULATORS AROUND 200 PSI. THEREFORE, CREW PLACED MAIN GEAR HANDLE DOWN AND PULLED EMERGENCY GEAR HANDLE. AIR RETURNSDR AUS20021002Pipe · cracked(AUS) LH HYDRAULIC SYSTEM HYDRAULIC PIPE TO HEAT EXCHANGER LOCATEDUNDER THE SAILBAOT FAIRING CRACKED. LOSS OF LH HYDRAULIC SYSTEM FLUID. LH HYDRAULIC CASE DRAIN FILTER CONTAMINATED.SDR CED2002F00000Regulator · crackedAIRCRAFT WAS ENROUTE, LOST HYDRAULIC PRESSURE. AIRCRAFT DIVERTED, MAINTENANCE FOUND HYDRAULIC PRESSURE REGULATOR LEAKING. THE VALVE BODY WAS CRACKED AT ONE OF THE BORES. THE TIME ON THE VALVE WAS APPROX 3 HOURS SINCE REPAIR.SDR 2002FA0001161Line · crackedHYDRAULIC LINE FAILED DURING FLIGHT AND AIRCRAFT LOST ALL HYDRAULIC PRESSURE. LANDING GEAR WAS EXTENDED BY EMERGENCY BLOW DOWN BOTTLE. LINE IS ON LEFT SIDE, AFT OF FIREWALL BETWEEN FILTER AND FLOW VALVE. FAILURE APPEARS TO BE MANUFACTURER DEFECT.SDR MWEA020539Hydraulic Line · leakingLOST ALL HYDRAULIC QUANTITY ON RIGHT SIDE. -- REMOVED LINES REPLACED WITH TEMPORARY FLEX LINE AND PLACED ON MAINTENACE CARRY OVER FOR REPLACEMENT OF TEMPORARY FLEX LINE.SDR XNOA01067Hydraulic System · dirtyNR 1 EDP INOP (GREEN SYSTEM). CLEANED AND RESECURED CONNECTION AT BYPASS. SOL SYS CHECKED GOOD PER A300 MM 29-11-32.SDR DLM88021033Tube · leakingON CLIMB OUT HYD QTY ON LEFT SIDE ENGINE DROPS TO 3/4 QT FOLLOWED POM PROCEDURES AND SHUT OFF HYD PUMPS ON LEFT SIDE UNTI CONFIGURING FOR LANDING. CORR ACT. FOUND LINE LEAKING AT LEFT THRUST REVERSER MODULE. REPLACED LINSDR AALA20021258Hydraulic Line · leakingORD - FLT 1451 - RIGHT MAIN LANDING UNSAFE MESSAGE ON MFDU. USED ALTERNATE GEAR EXTENSION. LANDED ORD WITHOUT INCIDENT. REPLACED RIGHT UPLOCK ACTUATOR LINE. JACKED AND CYCLED GEAR, NO FAULTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR 2002FA0001036Hydraulic Line · separatedHOSE ASSEMBLY SEPARATED AT SWEDGED END/ AT ACTUATOR NO CHAFFING OR OTHER APPARENT WEAR ON HOSE.SDR CA020903010Line · chafed(CAN) PILOT NOTICED HYDRAULIC FLUID LEAKING FROM LT REAR SPAR I/B OF ENGINE. LIFT DUMP PRESSURE LINE FOUND LEAKING. LINE REPLACED.SDR 2002FA0001068Line · brokenDURING LANDING APPROACH, LANDING GEAR FAILED TO EXTEND EITHER NORMALLY OR BY USING HAND PUMP. LANDING GEAR WAS EXTENDED BY USING BLOW DOWN BOTTLE, NOSE AND RIGHT REAR DID NOT EXTEND AND AIRCRAFT WAS SUBTANTIALLY DAMAGED DURING LANDING. INSPECTION REVEALED THSDR SWIA200211184Hydraulic Line · crackedDURING APPROACH, EXPERIENCED LOSS OF HYDRAULIC FLUID IN BLUE SYSTEM. FOLLOWED QRH, LANDED UNEVENTFULLY. FOUND CRACKED LINE IN RIGHT NACELLE. REMOVED AND REPLACED LINE. RAN ENGINES. LEAK CHECK GOOD.SDR AUS20021118Line · leaking(AUS) LT MAIN LANDING GEAR DOWN' HYDRAULIC LINE LEAKING.
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