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 2016F00174Pressure Switch · leakingON DESCENT THE CREW RECEIVED A HYDRAULIC QUANTITY LOW CAS MESSAGE AND THE AIRCRAFT LANDED WITHOUT INCIDENT. UPON A POST FLIGHT INSPECTION THE CREW NOTICED HYDRAULIC FLUID RESIDUE ON THE LOWER FUSELAGE AND FLUID LEAKING FROM UNDER THE BAGGAGE AREA. FURTHER INVESDR QXEA2016082800560Hydraulic Line · chafedNR 1 HYD ISO VALVE CAUTION, ROLL SPOILER INBD CAUTION, NR 1 HYD QTY 0. AFTER LANDING NR 1 ENGINE HYD PUMP CAUTION. AFTER INITIAL INVESTIGATION REPORTS NR 1 LT SIDE WHEEL WELL COVERED IN FLUID. PERFORMED GVI OF LT NACELLE AND LT GEAR WELL. ISOLATED FLUID LEASDR FDEA201608273055Control Valve · leakingAT TOP OF DESCENT RECEIVED A LEVEL ONE HYD 3 ELEVATOR OFF ALERT. FLUID DECREASED TO 1.2 AT SHUTDOWN. USED NORMAL GEAR EXTENSION, NORMAL TAXI IN AND NORMAL HYDRAULIC TEMPERTURE OF 37 DEGREES C. FOUND O-RING EXTENDED OUT OF NR 3 STABILIZER TRIM CONTROL UPPER SDR NI6R201608270037B-Nut · crackedNR 2 RADIAL ENGINE HYDRAULIC PUMP PRESSURE LINE INTERNAL TO THE FUSELAGE BEGAN LEAKING IN FLIGHT. UPON IDENTIFICATION OF THE LEAK, THE NR 2 ENGINE WAS SHUTDOWN AND AN IFE WAS DECLARED. LANDING WAS UNEVENTFUL. UPON INVESTIGATION OF THE LEAK, IT WAS DISCOVERESDR DALA2016082906238Hydraulic Line · leakingNR 2 HYDRAULIC PRESSURE WENT TO ZERO IN FLIGHT WITH HIGH HYDRAULIC QTY. HYDRAULIC PRESSURE REGAINED WITH THE AUXILIARY PUMP ON IAW CHECKLIST, QTY RETURNED TO NORMAL. MAINTENANCE FOUND EXCESSIVE AIR IN RT HYDRAULIC SYSTEM AND ALSO NOTED GROUND CONTROL ACTUATOSDR C77A20160829005Line · leakingCREW REPORTED LOSS OF NR 1 HYDRAULIC SYSTEM INBOUND. EMERGENCY DECLARED AND LANDED NORMALLY AND TAXIED TO GATE UNDER OWN POWER. NO PASSENGER ISSUES REPORTED. COMPLETE LOSS OF HYD SYS 1. VERIFIED NR 1 HYD SYS AT 16%. R & R HYD PRESSURE PIPE IAW AMM. ACCSDR 2020FA0000460Hydraulic System · failedHYDRAULIC PRESSURE WENT TO 0 PSI DURING FLIGHT. EMERGENCY EXTENSION OF THE LANDING GEAR WAS PERFORMED. BRAKING WAS LIMITED DURING LANDING.SDR CALA2016082695686Line · failedHYD PRESSURE SYS C LOW, LESS THAN 1200 PSI. EMERGENCY DECLARED AFTER TOUCHDOWN. REPLACED NOSE GEAR HYD LINE.SDR SWAA2016082455082Shutoff Valve · inoperativeTOTAL LOSS OF SYSTEM "A" HYDRAULICS. EMERGENCY DECLARED AND RETURNED TO DEPARTURE. R & R THE SHUTOFF VALVE IAW AMM.SDR ASMF201610011Actuator · leakingDURING TRANSIT CHECK, IT WAS DETECTED A HYDRAULIC LEAK IN THE RIGHT MAIN LANDING GEAR RETRACT ACTUATOR OUT OF LIMIT IAW DMC B787A-A-29-11-00-00C-364-A. AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERSONNEL REPLACED THE RIGHT MAIN LANDING GEAR RETRACT ACTUASDR FDEA201608182927Hydraulic System · malfunctionedDURING CRUISE AT FL 340, RECEIVED A HYD BLUE SYS LOW PRESSURE ECAM. HYD PAGE OF ECAM SHOWED 2950 PSI IN THE BLUE SYSTEM, NO OTHER INDICATIONS ON OVERHEAD PANEL AND SYSTEM QUANTITY WAS NORMAL. NO OTHER INDICATION ON HYD BLUE SYSTEM, PRESSURE REMAINED CONSTSDR DALA2016081906144Fluid · lowRT HYDRAULIC QUANTITY LOW LIGHT CAME ON IN CRUISE, SHOWED .38 WHEN STABILIZED W/ RT PUMPS OFF. SERVICED HYD SYS TO FULL. PRESSURIZED LT AND RT HYD AND CYCLED BRAKES AND CONTROL SURFACES. HYDRAULIC QUANTITY STEADY, NO FLUID MOVEMENT INDICATED. OK FOR SERVICSDR SIMA20160816005Quick Disconnect · looseAFTER TOUCHDOWN AND ROLLOUT, NOTICED THAT I HAD TO APPLY MORE BRAKING THAN USUAL. DURING TAXI IN, LT OTBD BRAKING, REGISTER 00, LT INBD BRAKE 08. THE RT INBD BRAKES REGISTERED 05, RT OTBD BRAKES 07. ACFT, DURING ROLLOUT AND BRAKING, PULLS TO THE RIGHT. FOUSDR AWKA2016081700815O-Ring · failedTURNING ON FINAL & LOWERING THE MLG, RECEIVED A HYD VOLUME LOW A CAS MESSAGE, NOTED THE HYD A VOLUME WAS 15%. ELECTED TO DIVERT, DECLARED AN EMERGENCY, & LANDED WITHOUT INCIDENT. ON LANDING, HYDRAULIC A VOLUME HAD DECREASED TO 7%. FOUND A FAULTY SYSTEM A HYSDR AALA201608169002Packing · leakingTHE FLIGHT CREW REPORTED A GREEN SYSTEM HYDRAULIC FAILURE DUE TO FLUID LOSS DURING DESCENT. THE FLIGHT CREW DECLARED AN EMERGENCY AND DIVERTED, LANDED SAFELY WITH NO FURHTER INCIDENT. AIRCRAFT GROUNDED. MAINTENANCE FOUND THE RIGHT AILERON SERVO INBOARD HYDRASDR CALA2016081200526Flex Line · brokenHYD PRESSURE SYS C EICAS CAUTION LOW CENTER HYDRAULIC SYSTEM PRESSURE . SYSTEM PRESSURE LESS THAN 1200 PSI. MM 29-10150. ASM 29-11 TASK 894 C HYD SYS RESERVOIR LOWER SIGHT GLASS INDICATION NORMAL. IAW AMM 29-11-00-200-804 EXTERNAL LEAK CHECK ACCOMPLISHED, NOSSDR SIMA20160810001B-Nut · looseHYD SYS 1 FLUID LEAK UPON LANDING TRANSFER TO NRWC 817, DFW-02039, REF NRWC 817, DFW-02039. NOSE WHEEL STEERING B-NUT WAS TIGHTENED. HYD SYS NR 1 SERVICED. HYD SYS NR 1 PRESSURIZED AND BLEAD, NO LEAKS NOTED.SDR HNAA2016081100245Circuit Breaker · trippedNR 1 STANDBY PUMP CIRCUIT BREAKER TRIPPED. RESET THE CIRCUIT BREAKER. GROUND RAN ACFT AND OPERATED SYSTEMS. SYSTEMS OPS NORMAL.SDR HYIA20160810001Line · crackedPILOT REPORTED LEFT BRAKE INOPERATIVE AND STEERING NOT AVAILABLE. MAINTENANCE INSPECTED AND FOUND THE BRAKE LINE FROM THE PARKING BRAKE VALVE ELBOW, TO MASTER CYLINDER FLEX HOSE LEAKING. REMOVED AND REPLACED THE LINE.SDR FDEA201608092846Hydraulic Line · leakingGREEN HYDRAULIC LOW LEVEL ECAM WARNING DURING FLT. DROPPED TO BELOW RED DOT. IMMEDIATELY ON ALERT WITH SOME FLUID INDICATION, TURNED OFF BOTH GREEN HYD PUMPS. EVENTUALLY FLUID DROPPED TO ALMOST ZERO. REMOVAL, INSTALLATION OF NR 2 ENGINE CASE DRAIN HYD TUSDR CALA2016080900514Hose · failedAT 1000 FEET DURING FINAL, EXPERIENCED A COMLETE LOSS OF LT HYD SYS FLUID AND PSI FOUND DOWNLOCK ACTUATOR FLEX LINE WITH HOLE, REPLACED LINE AND RAN ENGINETO VERIFY CORRECT OPERATION OF ENGINE PUMP, ADP AND PTU. ALL FUNCTIONS NORMAL, NO FURTHER ACTION REQUIRESDR AALA20160806001Filter · leakingDURING DESCENT "B" HYDRAULIC SYSTEM QUANTITY DECREASED TO UNUSEABLE LEVEL. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. MAINTENANCE FOUND "B" SYSTEM HYDRAULIC ACOUSTIC FILTER LEAKING. REMOVED AND REPLACED THE FILTER IAW AMM 29-11-27. OPS AND SDR MASA2016080612897Hydraulic System · failedHYD 2 SYSTEM FAILURE. HYD SYS 2 SHOWING ZERO QUANTITYSDR E0YA201608090001Hose · leakingAFTER INITIAL CLIMB OUT, THE CREW NOTED A STEADY DEPLETION OF THE "A" HYDRAULIC SYSTEM. AFTER ASCERTAINING THE FLIGHT COULD CONTINUE SAFELY, THE CONTINUED ON AND LANDED. THE AIRCRAFT WAS SHUT DOWN ON THE RUNWAY AND TOWED TO THE HANGAR DUE TO NO BRAKES AVAILABSDR DXTA2016080406275Circuit Board · unserviceableFOUL ODOR FOLLOWED BY HYD NR 2 ISOLATION LIGHT. RETURNED TO DEPARTURE. R & R PCB'S 413JE-421JE WITH SUPPLIED PARTS IAW AMM 24-00-00-910-801. PERFORMED ENGINE RUN UP AND FOUND NO FOUL ODOR AT THIS TIME. NO ISOL LIGHT AT THIS TIME. PARTS REPLACED: CIRCUIT BSDR QXEA2016080300519Hydraulic Line · failedENROUTE EXPERIENCED A HYD FAILURE ON THE NR 2 ENGINE. FOLLOWED THE GUIDANCE IN THE E & A CHECKLIST INCLUDING MANUAL GEAR EXTENSION. DIVERTED AND LANDING UNEVENTFUL. GEAR PINS INSTALLED UPON LANDING. REF HYD PRESSURE BETWEEN 0-2000 PSI, QTY 0. VERIFIED NR SDR UIEA2016080300665Hydraulic System · malfunctionedLOW SPEED (40KTS) TAKEOFF REJECTION DUE TO STAB GREEN BAND DISAGREE WITH NOSE GEAR PRESSURE SWITCH. NO BRAKE TEMP HIGHER THAN 1.2. ACCOMPLISHED HIGH ENERGY STOP INSPECTION IAW AMM 5-51-10 ALL CHECKS NORMAL.SDR 2016F00162Elbow · brokenAT DEPARTURE. AIRCRAFT STARTED ROLLING ON TAXIWAY AND BRAKE TEST PERFORMED. BRAKE PRESSURE LOW AND ANTISKID FAIL ALARM WARNING ON. FLIGHT CREW NOTICE THAT THE NORMAL BRAKING IS INOPERATIVE, THE CBD ACTIVATES THE EMERGENCY BRAKING, RETURN TO BLOCKS. AIRCRAFT SDR CALA2016080300492Control Panel · overheatedSLIGHT MOMENTARY ELECTRICAL ODOR IN COCKPIT. COMPLIED WITH SMOKE INSPECTION, FOUND M10050 P5 OVERHEAD PANEL EXTREAMLY HOT AND WITH A SLIGHT BURNED ODOR. REMOVED AND REPLACED THE PANEL IAW AMM 29-11-00. NO OTHER DEFECTS OR ODORS NOTED.SDR IPXA2016090207767Seal · leakingINSPECTION TYPE:3C, CABIN PRESSURIZATION LEAK AT AFT PRESSURE BULKHEAD HYD PIPING SEAL, RT SIDE REPAIRED, NOTED SEALS IAW EA 011-2900-01-A6416, REV IR AND EO MD11-2920-61734-A.SDR 2016FA0000385Dump Valve · bypassingINTERNAL FAILURE OF THE DUMP VALVE IN THE HYDRAULIC SYSTEM PREVENTED THE NOSE LANDING GEAR FROM PROPERLY EXTENDING AND LOCKING EVEN AFTER THE EMERGENCY GEAR EXTENSION LEVER WAS ACTUATED.SDR AALA20160730005B-Nut · looseDURING FLIGHT THE LEFT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED. TRANSFER PUMP WAS TURNED OFF. QUANTITY IN LEFT SYSTEM 3 QUARTS, PUMP PRESSURE WENT TO 3000 PSI FOR 5 SECONDS THEN DROPPED TO 1000 PSI. PUMP TURNED OFF. EMERGENCY DECLARED. LANDING UNEVENTFUL. SDR EBVR20160816001Fitting · looseDURING CRUISE FLIGHT, CREW RECEIVED A CAS MESSAGE FOR LOW HYDRAULIC FLUID LEVEL ON NR 1 SYSTEM. AIRCRAFT LANDED. ON ARRIVAL AT AIRCRAFT MAINTENANCE CREW FOUND A LEAKING MS FITTING. NO PRIOR MAINTENANCE WAS DONE TO OR AROUND THAT FITTING OR LINE AT OUR FACILSDR AALA20160729007Module · leakingDURING CRUISE RIGHT HYDRAULIC QUANTITIY STATUS MESSAGE DISPLAYED. QUANTITY DROPPED TO ZERO, RIGHT PRIMARY HYDRAULIC PUMP WARNING ILLUMINATED. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. MAINTENANCE FOUND LEAK AT RIGHT PUMP FILTER MODULE. RSDR HALA2016072700306Packing · damagedAIR DIVERSION, RT HYD QTY, EICAS DISPLAYED. RIGHT QTY WAS .49 WITH, RF DISPLAYED. TROUBLESHOT, FOUND LEAK CAME FROM MODULE STRUT ENGINE DRIVE PUMP PRESSURE AND CASE DRAIN FILTER DUE TO PACKING DAMAGED. REPLACED PACKING IAW AMM TASK 29-11-17-004-001. LEAK CSDR AALA201607279006Line · leakingFLIGHT CREW REPORTED THE LOSS OF THE GREEN SYSTEM HYDRAULIC PUMP AND HYDRAULIC FLUID WHILE RETRACTING THE GEAR DURING CLIMB. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY. AIRCRAFT GROUNDED. MAINTENANCE FOUND THE RIGHT MAIN LANDING GEAR SIDE STAYSDR AALA201607269002Pressure Switch · faultedFLIGHT CREW REPORTED DURING CLIMBING OUT THE ENG DRIVEN GREEN HYDRAULIC SYSTEM PUMP FAILED AND A LOW PRESSURE WARNING ECAM MESSAGE. THE FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. AIRCRAFT GROUNDED. MAINTENANCE ACCOMPLISHED TSM 29-11-00-810-SDR HALA2016072400299Plunger · lack of lubeRAT WILL NOT STOW. LUBRICATED TURBINE LOCK PLUNGER CABLE. OPS CHECKED GOOD.SDR SIMA20160724001Manifold · failedHYD 3 LOW PRESSURE. REMOVED PANEL 293BR AND 1 AFT OF 233BR, AMM 53-52-32. INSPECTED AND FOUND RT PRESSURE TRANSDUCER LEAKING. ITEM 3 OF THIS LOG PAGE. REAPPLIED PANEL 195EV AND 196 EV IAW 53-52-72 AMM. FOUND SIGNIFICANT LEAK FROM NR 3 HYDRAULIC PRESSURE TSDR CALA2016072595585Line · damagedHYD EDP 1 LO PR WITH HYD G RESERVOIR LOW LEVEL AND LOW PRESSURE ECAM MESSAGES DISPLAYED. CREW REPORT FLUID LEVEL AT ZERO, TURNED ENG 1 HYD PUMP IAW QRH AS SOON AS ECAM DISPLAYED. FOUND THE ENG 1 PRESSURE LINE IN THE PYLON DAMAGED. REMOVED AND REPLACED THESDR AALA201607259003Line · chafedFLIGHT CREW REPORTED THAT ON TAXI OUT AND PRIOR TO TAKING THE ACTIVE RUNWAY, A MIST AND HYDRAULIC FUMES WERE NOTED IN THE CABIN FOLLOWED BY A HYDRAULIC FAILURE. THE FLIGHT CREW DEPLOYED ALL OF THE EVACUATION SLIDES AND EVACUATED THE AIRCRAFT. AIRCRAFT GROUNDSDR AALA20160723003O-Ring · leakingDURING CRUISE THE "A" SYSYTEM HYDRAULIC LOW PRESSURE WARNING ILLUMINATED. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. MAINTENANCE FOUND THE "A" SYSTEM FLOW LIMITER TO BE LEAKING AT ITS O-RING. REMOVED AND REPLACED THE O-RING AND ACCOMPLISHEDSDR SIMA20160722001Hydraulic Line · chafedHYD SYS 1 QTY WENT TO ZERO. HYD SYS 1 FAIL, RAN LIST, EMERGENCY LANDING GEAR EXTENSION. FOUND NR 1 HYDRAULIC PUMP PRESSURE LINE CHAFED.
R & R PRESSURE HOSE IAW MM 29-10-03. NO LEAKS NOTED AT THIS TIME.SDR QXEA2016072100459Hose · leakingNR 2 HYD ISOLATION VALVE ILLUMINATED IN CRUISE FLIGHT. OBSERVED THAT THE NR 2 HYD QTY WAS DECREASING TO 10%. HYD PRESSURE REMAINED NORMAL FOR REMAINDER OF FLIGHT. IAW CHECKLIST, PERFORMED MANUAL GEAR EXTENSION. RETURNED TO FIELD. LANDING UNEVENTFUL. FOUND SDR FDEA201607212593Hydraulic Line · leakingDURING CLIMBOUT, RECEIVED LT HYD SYS LOW QUANTITY MESSAGE. SHORTLY, RECEIVED LT HYD SYS PRESSURE MESSAGE. COMPLIED WITH QRH EXTEND FLAPS ALTERNATELY AND ALTERNATELY EXTEND LANDING GEAR. FOUND LEFT MAIN GEAR DOWN LOCK ACTUATOR PRESSURE LINE LEAKING. REPLASDR JJBA20160720004Hydraulic System · lowPOSSIBLE HYD LEAK NR 1 HYD SYS. QTY DROPPED FROM 1.9 TO 0.9 IN FLIGHT. SERVICED NR 1 HYD SYSTEM TO 2 QUARTS. PERFORMED ENGINE RUNS IAW 71-00-00 PERFORMED CYCLING TEST OF HYDRAULIC SYSTEM NO LEAKS NOTED. OPS CHECK SAT.SDR CALA2016072295577Fitting · leakingGREEN SYS HYD LOSS DURING CLIMB, QTY TO ZERO, NO PRESSURE, EMERGENCY DECLARED FOUND HYDRAULIC FITTING LEAKING AT GREEN ACCUMULATOR DDP POSITION, R & R ACCUMULATOR, LEAK CHECKED OKSDR CALA2016072195571Control Valve · failedLEVEL CRUISE FLIGHT AT FL360, HYD RESERVOIR LOW LEVEL ECAM DISPLAYED. SECURED THE HYD SYSTEM, DECLARED EMERGENCY AND DIVERTED. R & R THE NR 2 THRUST REVERSER HYDRAULIC CONTROL VALVE AND ENGINE HYDRAULIC PUMP. CHANGED CASE DRAIN FILTER WITH NO DEBRI NOTEDSDR VQIA201607290029Accumulator · failedEXPERIENCED LOW BLUE HYDRAULIC SYSTEM PRESSURE DURING INITIAL TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AT 70 KNOTS AND THE AIRCRAFT RETURNED TO THE GATE. LOCAL MAINTENANCE CONTRACTOR ACCOMPLISHED TSM 29-12-00-810-805-A AND DISCOVERED A FAILED BLUE HYDRAULIC SYSSDR AALA201607229001Line · chafedDURING APROACH, THE FLIGHT CREW REPORTED THE GREEN HYDRAULIC SYSTEM PRESSURE WAS LOW AND DECLARED AN EMERGENCY. A FLAPS FAULT WAS RECIEVED AFTER LOWERING THE GEARS AND ATTEMPTING TO LOWER THE FLAPS. THE AIRCRAFT LANDED WITH THE FLAPS AT 0 SAFELY. THE TOWER RE
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