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 2010FA0001169Line · misinstalled(EBVR) FOUND NR 2 BRAKE SYSTEM CROSS CONNECTED, LT PEDAL OPERATES RT BRAKE, RT PEDAL OPERATES LT BRAKE. FOUND PLUMBING IN NOSE WHEEL SWAPPED. REF IPC 32-40-40-10, ITEMS 210 AND 290. CORREDTED PROBLEM BY CONNECTING LINES TO CORRECT LOCATIONS, FUNCTION CHECKSDR SIMA201030601Hydraulic Line · leakingON FLIGHT 4649 DURING CRUISE THE CREW REPORTED AT FLIGHT LEVEL 320 EICAS INDICATED HYDRAULIC 3 LOW PRESSURE AND BRAKE PRESSURE CAUTION MESSAGES. HYDRAULIC PAGE INDICATED HYDRAULIC 3 FLUID QUANTITY 5 PERCENT ONLY AND NO PRESSURE IN THE LINES PSI BELOW 1800 PSISDR CA101103002Hose · leaking(CAN) FLUID SQUIRTED FROM NOSE WHEEL AT END OF PUSHBACK, AIRCRAFT HAD PUSHED BACK FROM STAND. AT END OF PUSH AND WHILE DISCONNECTING TOW-BAR WHAT APPEARED TO BE HYDRAULIC FLUID SQUIRTED FROM NOSE-WHEEL AND HIT 2 RAMP OPERATIVES IN THE FACE AND EYES. FLEXIBLESDR ASOA201001680Hydraulic System · lowHYD 3 LOW PRESS CAUTION MESSAGE IN FLIGHT. RAN CHECKLIST AND HAD TO MANUALLY EXTEND GEAR. DECLARED EMERGENCY. (EMERGENCY DECLARED -- EMERGENCY EQUIPMENT REQUESTED TO BE STANDING BY) (CLOSED)SDR VQI2010F00002Tube · wornHAD AN UNEVENTFUL FLIGHT UNTIL AT 0327Z, AIRMAN INDICATED 2 ECAM WARNINGS - HYD Y ENG2 PUMP LO PR AND HYD RSVR LO LVL AT APPROX FL180. AIRMAN THEN INDICATED AN ADDITIONAL ECAM WARNING AT 0328Z OF HYD Y SYS LO PR. THE CREW DECLARED AN EMERGENCY, FOLLOWED APPRSDR AALA20101023LAX01Flex Line · leakingLAX - CREW REPORTED CENTER HYDRAULIC QUANTITY LOSS. EMERGENCY DECLARED LANDED LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND HORIZONTAL STAB SECONDARY BRAKE LINE LEAKING. INSTALLED FLEX LINE. SYSTEM GROUND CHECK NORMAL OPERATION.SDR UALA2010102203905Packing · leakingON WALK AROUND FOUND RT WELL LEAKING HYDRAULIC FLUID. FOUND RT SYS RELIEF VALVE LEAKING FROM LOWER UNION. REPLACED PACKING AND SERVICED HYDRAULICS, OPS CHECKS GOOD.SDR UALA2010102103897Pressure Switch · faultyRUDDER RATIO LIGHT ILLUMINATED IN FLIGHT. EICAS MESSAGE RUDDER RATIO DISPLAYED. REPLACED LEFT ELEC. HYD PRESSURE SWITCH S27 PER MM. ACP OPS CHECKED PER MM. CHECKS OKAY, NO FAULTS & NO MESSAGES.SDR CALA2010102000489O-Ring · deterioratedLEFT HYDRAULIC SYSTEM QUANTITY AND PRESSURE WERE LOST. FLT ATTENDANTS REPORTED HEARING A LOUD THUMP TOWARD THE FRONT OF CABIN AROUND THE TIME THE SYSTEM WAS LOST. QTY=.11 PRESS=40-5- PSI PTU STATUS MSG. REPLACED PTU O-RING PACKING ON THE FLAP/SLAT DEPRESSURSDR SWAA106533Hydraulic Line · leakingAIR TURNBACK, HYDRAULIC A-SYSTEM LOSS. REMOVED AND REPLACED LT MLG ACTUATOR HYDRAULIC LINE.SDR UALA2010101803856Line · leakingHYD HOSE LINE LEAKING ABOVE RH MAIN LANDING GEAR. REPLACED HYDRAULIC LINE. PRESSURIZED HYDRAULICS AND NO LEAKS FOUND.SDR FDEA201010164085Line · leakingHYD 1 OFF ALERT IN CRUISE 2.7 G REMAINING IN TANK 1. ON FINAL HYD 1 FAIL ALERT 0.5 REMAINING IN TANK 1. ON FINAL HYD 1 FAIL ALERT 0.5 REMAINING IN TANK 1. FOLLOWED QRH PROCEDURES LANDED WITHOUT INCIDENT. REPLACED LT INBD FLAP ACTUATOR PRESSURE LINE IAW ASDR GLBA20101014FHose · failedPILOT REPORTED THAT WHILE ON A TRAINING FLIGHT THE GREEN HYD SYS LOW AND ELEC PUMP LIGHT ILLUMINATED, DECLARED AN EMERGENCY AND LANDED WITH NO OTHER INCIDENT. MX FOUND A PIN HOLE IN THE RT FWD NLG DOOR ACTUATOR SUPPLY LINE, REPLACED FWD NOSE GEAR ACTUATOR SUPPSDR FDEA201010124015Line · leakingHYD QTY LOW CTR (LOST ALL HYD FLUID IN CTR) SVC'D HYD FLUID TO CTR HYD SYS TO PROPER LEVEL IAW AMM 12-12-01-3-0, PERF CTR HYD SYS LEAKS FOUND. NO EXTERIOR LEAKS CAN BE FOUND. SUMP DRAINED LT FUEL TK & RT FUEL TK, FOUND HYD CONTAMINATED IN RT FUEL TK FUEL SAMSDR NSVA2010180Unknown · malfunctionedDURING MAINTENANCE TAXI/RUN THE AIRCRAFT VEERED RIGHT INTO A DITCH ON TAXIWAY ZULU. THE CAUSE IS UNKNOWN AT THIS TIME. IAD FIRE DEPARTMENT AND LAW ENFORCEMENT PERSONNEL WAS DISPATCHED TO ASSIST. THERE IS NO FIRE OR INJURIES REPORTED. THE FULL EXTENT OF THESDR UALA2010100803741Fitting · leakingNR2 HYD QTY READS XXRF. RT HYD QUAN AT .74RF AT 4.5 HOURS FLT TIME. FOUND FITTING LEAKING STEADY ON VALVE ASSY FUSE. JUST OTBD OF LT MAIN GEAR. SECURED FITTING NO LEAKS.SDR CA101008001Hose · leakingAFTER DEPARTURE, DURING THE INITIAL CLIMB, THE ACFT GREEN HYD SYS FAILED. THE QRH WAS FOLLOWED AND AN EMERGENCY WAS DECLARED WITH ATC. THE FLIGHT RETURNED TO POINT OF DEPARTURE WHERE AN OVERWEIGHT LANDING OF 69.0 KGS WAS CARRIED OUT WITHOUT FURTHER INCIDENT. SDR USAA2010100192174Packing · failedFLT 5 -EMERGENCY LANDING- CREW REPORTED YELLOW HYDRAULIC RESERVOIR LOW LEVEL WARNING - FOLLOWED ECAM PROCEDURES AND TURNED OFF YELLOW ENGINE 2 HYDRAULIC PUMP - YELLOW SYSTEM SHOWED ZERO. SHORTLY THEREAFTER, CREW REPORTED GREEN SYSTEM WAS OVERHEATING - DECLARESDR UALA2010100503692O-Ring · leakingNR 6 SPOILER HAS RUNNING HYD LEAK WITH PRESSURE ON AND SPOILERS STOWED. LEAK IS RUNNING FROM CAP 550 AND O-RING 555. REPLACED NR 6 SPOILER PCA IAW MM.SDR CA101004006Hose · leakingTHE ACFT DEVELOPED LOW CTR HYD PRESSURE AFTER TAKEOFF. WITH NO INDICATIONS OF IMPROVEMENT, THE FLIGHT DIVERTED. AS A PRECAUTION, CFR WAS CALLED OUT TO MEET THE FLIGHT, HOWEVER THE ACFT WAS ABLE TO TAXI INTO THE GATE WITHOUT ASSISTANCE. THERE WAS NO ADVERSE PSDR UALA2010100403656Pressure Switch · faultyLEFT ELEC DEMAND HYD PRESS LIGHT ON WITH SWITCH IN AUTO. REPLACED PRESSURE SWITCH. ACCOMPLISHED LEAK CHK. NO LEAKS NOTED. NO HELP, NEEDS MORE TROUBLESHOOTING. REPLACED EDP PRESSURE SWITCH S26 IAW AMM.SDR CA101004004Valve · failedAFTER TAKEOFF POWER WAS APPLIED THE CREW REJECTED TAKEOFF DUE TO A LOSS OF THE YELLOW HYD SYS PRESSURE. THE ACFT RETURNED TO THE GATE. EMERG BRAKE DUAL DISTRIBUTION VALVE REPLACED IAW AMM 32-43-14-400 CHECKS SERV.SDR AALA20100930DFW01Hydraulic System · lowDFW - CREW REPORTED ON DESCENT LEFT HYDRAULIC QUANTITY DECREASED. EMERGENCY DECLARED LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. SERVICED LEFT AND RIGHT HYDRAULIC SYSTEMS PER MM 12-13-01-3. SYSTEM GROUND CHECK NORMAL OPERATION.SDR HNAA2010093000222Line · leakingNR2 HYD ISOLATION VALVE CAUTION LIGHT ILLUMINATED WITH JUST BELOW E QUARTS ON QTY INDICATOR. INSPECTED AND FOUND HYD LEAK OF NOSE GEAR DOWN BLUE LINE, R & R LINE AS REQUIRED, SERVICED NR2 HYDR SYS UP TO FULL, GROUND RAN NR2 ENGINE WITH BOTH STANDBY PUMPS ON, SDR FDEA201009303819Filter · leakingDURING DESCENT RECEIVED ECAM GREEN HYD SYS LOW LEVEL WARNING. HYD QTY ON OVERHEAD PANEL INDICATED ZERO. CONSULTED THE QRH AND MANUALLY EXTENDED THE LANDING GEAR. FOUND HYD LEAKAGE CAME FROM THE GREEN SERVO CONTRO FILTER. REMOVED AND REPLACED THE PUMP DELIVSDR COMA2010100450214Hydraulic Line · leakingON DESCENT INTO DCA RECEIVED HYD 2 LOW PRESS CAUTION MSG, 0 FLUID AND 0 PSI ON EICAS. EMERGENCY DECLARED, A/C DIVERTED TO BWI LANDED SAFELY. REMOVED AND REPLACED NR 2 EDP PRESSURE HOSE IN RT PYLON.SDR FDEA201009303821Filter · leakingDURING DESCENT RECEIVED ECAM GREEN HYD SYS LOW LEVEL WARNING. HYD QUANTITY ON OVERHEAD PANEL INDICATED ZERO. CONSULTED THE QRH AND MANUALLY EXTENDED THE LANDING GEAR. PERFORMED GREEN HYD SYS LEAK CHECK FOUND HYD LEAKAGE CAME FROM THE FILTER 1049 WHICH ON GSDR CA100930001Actuator · leakingAPPROX 45 MINUTES TO DESTINATION THE CREW REPORTED GREEN HYD LOW PRESSURE INDICATION AND DECLARED AN EMERGENCY.SDR UALA2010100103633Valve · faultyON TAXI OUT, HAD INTERMITTENT C FLT CONT HYD EICAS MESSAGE. SECURED VALVE OPEN IAW MEL. OFF LIGHT ON C FLT CONTROL SWITCH LIGHT INOP. REPLACED CENTER VALVE. OPS NORMAL.SDR CA100929003Check Valve · failedSHORTLY AFTER TAKEOFF, THE CREW REPORTED A YELLOW HYD SYS OVERHEAT AND AFTER DISCUSSION WITH MX AND SOC IT WAS DECIDED TO RETURN THE ACFT TO AIRPORT OF DEPARTURE.SDR CA100928015Flex Hose · burstBURST IN FLEX NEAR QUICK DISSCONNECT FITTING END, LOSS OF HYD PRESSURE AND FLUID.SDR ASOA201001471Line · leakingHYD SYS 2 FAILURE IN FLIGHT PRESSURE AND QTY INDICATE 0. (EMERGENCY DECLARED -- ENROUTE TO IAD ACFT DIVERTED DUE TO MX) FOUND HYD SYS NR 2 PRESSURE LINE ON BRAKE CONTROL VALVE LEAKING. R & R HYD LINE IAW AMM 20-22-01 LEAK CHECK GOOD. (CLOSED)SDR DJFA2010026Hydraulic System · warning messageIN CRUISE FLIGHT, CREW NOTED HYDRAULIC QUANTITY LOW CAS MESSAGE AND CONFIRMED THE A-SYSTEM HYDRAULIC FLUID QUANTITY INDICATED 15 PERCENT. CREW NOTED ALSO THAT THE HYDRALIC FLUID TEMPERATURE WAS RISING. CREW BEGAN PREPARATIONS TO DIVERT, AS HYDRAULIC TEMPERATSDR NOCA06510Packing · damagedPLEASE BE ADVISED N764NA (FLT 7018 LEJ-KWI) PHONE PATCHED MCC AND ADVISED "L HYD QUANTITY" DECREASING. THE FLIGHT CREW FOLLOWED QRH. A/C WENT BACK TO LEJ. NO OVER WEIGHT LANDING CONDITION. FOUND PRESSURE LINE UNION PACKING DAMAGED ON THE CENTER ACTUATOR. RSDR UALA2010092403549Seal · leakingCENTER HYD QTY LOW SHOWS RF. TOPPED UP 8 QTS OF HYDRAULIC. FOUND PRESSURE AND CASE DRAIN MODULE ELECTRIC C2 PUMP LEAKING AT POPOUT. DEFERRED C2 ELECTRIC PUMP IAW MEL 2911C. REPLACED SEALS ON C2 PUMP PRESS AND CASE DRAIN MODULE FWD DPI SWITCH. LEAK CK'D GOOD.SDR AALA20100923MCO01Hydraulic Line · leakingMCO - INFLIGHT JFK-MIA. APPROX 1.5 HRS INTO FLIGHT EXPERIENCED CENTER SYSTEM HYDRAULIC LOW INDICATION CENTER SYSTEM FLUID LEVEL DECREASED DOWN TO 0.30. AFTER GEAR AND FLAP EXTENSION FLUID DROPPED TO 0.11. EMERGENCY DECLARED DIVERTED MCO LANDED WITHOUT INCIDSDR UALA2010092103505Circuit Card · malfunctionedLT AND RT ELEC HYD DEMAND PUMPS RUN CONTINUOUSLY AT CRUISE. LT & RT HYD IM CARD REPLACED AND OPS SOFTWARE (297A-BCE-00-27) LOADED IAW AMM & TESTS OK. W-U GENERATED FOR TEST FLIGHT.SDR ABXA201009220124Hydraulic Line · defectiveLOST ALL CENTER HYDRAULIC QUANTITY. DEFERRED: 66591. REMOVED & INSTALLED HYD FLEX LINE IN RT W/W AT MAIN LANDING SELECTOR VALVE IAW AMMM 29-20-00 & 20-40-09-8. OPS & LEAK CHECK NORMAL. DEFERRED FOR TRACKING PER GMM CHAPTER 1 SECT 07.04 & MM 20-10-09-8. PSDR UALA2010092003490Seal · leakingNR 2 ENG HOC. ACCOMPLISHED HIGH POWER RUN, WAS GOOD, NO NEW OIL ON GROUND, ENG NOT WET. FOUND DAMAGE TO HYDRAULIC LINES & BLANKET. AGGED DRAIN LINES AND ACP'D HIGH PWR RUN. NO LEAKAGE FROM LINES. ACPD MM GEARBOX PRESS CK, NO LEAKS NOTED. REPLACED DEOILER CARSDR SWIA201024917Hydraulic Line · crackedEN ROUTE, LOW LEVEL GREEN HYDRAULIC FOLLOWED BY MAIN PUMP OFF. (FLT 6965) REPAIRED HYDRAULIC LINE AT ENGINE DRIVEN PUMP LINE AT ABOVE LEFT ENGINE OIL COOLER PER AMM.SDR UALA2010092103513Line · chafedNR 2 ENGINE HYDRAULIC SUPPLY LINE HAS EVIDENCE OF WEAR ON SILICONE HEATSHIELD UP NEAR THE FIREWALL DISCONNECT. AREA OF DEFECT IS APPROX 1. 5 INCH IN DIAMETER EXPOSING THE BRAIDED STAINLESS STEEL CORE. THERE IS NO VISIBLE DAMAGE TO BRAIDED CORE. WILL ACP INTESDR DXTA2010092004247Line · leakingDURING FLIGHT - HYD PERCENT QTY A 15, 'HYD VOL LOW A' CAS, 'HYD O'TEMP A' CAS, A TEMP DEG C 101. COMPLIED WITH PILOTS ABBREVIATED CHECKLIST ABNORMAL PROCEDURED N2 "A" HYD SYS FLUID APPEARS TO BE LEAKING FROM CTR BELLY OF ACFT FWD OF MLG AT AFT PORTION OF SKID SDR CLCA092020101Hydraulic Line · leakingHYDRAULIC SYSTEM FAILURE DURING CRUISE, ALT LANDING GEAR EXTENSION REQUIRED, DIVERTED TO (SVMI/CCS). FOUND DEFECTED HYD HOSE NR 3 ENGINE DRIVEN PUMP, LOWER HOSE ASSY. REPLACED HOSE WITH SERVICEABLE HOSE IAW MD-11 MM 20-40-01, PERFORMED LEAK CHECK IAW MM 71SDR CALA2010091700440Hydraulic Line · damagedAFTER T/O LOSS OF L HYD QTY. DEPLOYED FLAPS AND GEAR NORMALLY - LEFT HYD PRESS LOW ANNUNCIATED. MADE FLAPS 20 DEG LANDING LG.W 198,480 NORMAL TOUCHDOWN FOUND NOSE GEAR DOOR ACTUATOR UP PRESS LINE DAMAGED. REMOVED AND REPLACED NOSE GEAR DOOR ACT UP PRESS LISDR 2010FA0001060Regulator Valve · worn(NI6R) ON APPROACH FOR LANDING, THE AIRCREW DISCOVERED THE MAIN HYD SYS WOULD NOT BUILD PRESSURE ABOVE 1,000 PSI. NORMAL IN-FLIGHT OPERATING RANGE IS 1,400 - 1,725 PSI. AN IN-FLIGHT EMERGENCY WAS DECLARED, THE ACFT LANDED SAFELY, AND WAS TOWED FROM THE ACTIVE SDR CHQA201000180Hydraulic Line · looseDURING CRUISE THE FLIGHT CREW RECEIVED A HYD 1 QTY LOW ADVISORY MESSAGE. THE QRH WAS FOLLOWED AND THE AIRCRAFT RETURNED TO FIELD. WHILE RETURNING TO CMH, THE HYDRAULIC SYSTEM 1 PRESSURE WENT TO ZERO AND THE HYD 1 SYS FAIL MESSAGE WAS DISPLAYED. THE QRH ITEMSDR AALA20100910JFK01O-Ring · brokenJFK - CREW REPORTED AIRCRAFT HAD LOST MOST OF THE CENTER HYDRAULIC SYSTEM FLUID. EMERGENCY DECLARED LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED O-RINGS ON AIR DRIVEN PUMP FILTER MODULE DIFFERENTIAL PRESSURE INDICATOR. SYSTEM GROUNDSDR UALA2010090903335O-Ring · leakingHYDRAULIC FLUID LEAKING FROM LT STABILIZER AREA RUNNING DOWN BELLY OF AIRCRAFT. LEAK APPEARS TO BE FROM A RUDDER AUTOPILOT SERVO. FOUND LEFT RUDDER RATIO CHANGER LEAKING AT SUPPLY AND RETURN B-NUTS. CHANGED OUT BOTH O RINGS NO LEAKS NOTED DURING OPS CHECK.SDR 2010FA0001138Line · separatedLANDING GEAR WOULD NOT EXTEND DUE TO FAILURE OF NOSE GEAR DOWN PRESSURE HYD HOSE ASSY. GEAR HYD HOSE ASSY (ALL) SHOULD BE CHANGED EVERY 10 YRS OR 1000 HRS TIS BETWEEN CHANGES.SDR UALA2010090703290Hose · leakingNR 1 ENG EVIDENCE OF HYD LEAK RT SIDE OF ENGINE. REPLACED HYD PRESS HOSE AND BLANKET. LEAKED CHECK GOOD.
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