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 RAIA00309246Line · leaking5471-PIA- AFTER ARRIVAL AND PARKING AT STL LOST HYD PRESSURE. MAINTENANCE REMOVED AND REPLACED PRESSURE LINE IN RIGHT ENGINE BAY AREA.SDR 03FDEA01596Line · leakingHYD SYSTEM NR 1 FAILED. NOTE: DUE TO LOSS OF HYD FLUID. FOUND HYD LINES CHAFED TOGETHER JUST AFT OF 1-3 REVERSIBLE MOTOR PUMP IN CENTER W/W CHANGED LINE, LEAK CHECK OK.SDR IU62003F00038Housing · crackedCRACKED INNER DIAMETER OF MOUNT HOLE. OVER TORQUE, OVER PRESSURE OF POOR DESIGN. ENGINEER NEW DESIGN OF MATERIAL TYPE.SDR 505091703B-Nut · looseENROUTE TO DESTINATION, AIRPORT CREW NOTICED THE ILLUMINATION OF THE LOW HYDRALIC PRESSURE ANNUNCIATORS FOLLOWED BY A DECREASE IN HYDRAULIC SYSTEM PRESSURE ON THE PRESSURE GAUGE. CREW RETURNED TO THE DEPARTURE AIRPORT AND PERFORMED MANUAL GEAR EXTENSION AND LSDR RYN2004F00027Module · failedAFTER TAKEOFF, RETRACTED FLAPS AND RECEIVED AN A-HYDRAULIC LOW PRESSURE INDICATION AT FLIGHT ENGINEER PANEL AND PILOTS FWD PANEL. FOLLOWED HYDRAULIC LOSS PROCEDURES. AIRCRAFT RETURNED TO DEPARTURE AIRPORT WITHOUT INCIDENT. REMOVED AND REPLACED (A) SYSTEM HYSDR UPS03841227Line · leakingEMERGENCY LANDING FOR LOSS OF HYD QTY. REMOVED AND REPLACED BOGIE TRIM CYLINDER FLEX LINE, LT GEAR SERVICED HYD FLUID & OPERA TED ALL SYSTEMS CHECKS GOOD NO LEAKS.SDR CA031030005Line · failed(CAN) DURING ILS APPROACH, CAPT CALLED FOR LANDING GEAR TO BE LOWERED 'NR 2 HYD PRESSCAUTION LIGHT CAME ON FOLLOWED BY LANDING GEAR UNSAFE LIGHTS. APPROACH DISCONTI NUED, A/C ORBITED UNDER RADAR CONTROL TO EAST OF AIRFIELD. EMERGENCY CHECK LISTCONSULTED. NR 2 SDR RAIA00309239Line · chafedHYDRAULIC FAILURE. MAINTENANCE REPAIRED CHAFED HYD PRESSURE LINE IN RIGHT NACELLE.SDR C1HA200385008Hydraulic Line · rupturedON DESCENT HAD HYD A ENG 1 PUMP LOW PRES LITE ON A QUANTITY -0- RAN PRECEDURE 2.29.2- AFTER A PUMP AND FLUID SHUT OFF TURNED OFF, QUANTITY CAME UP TO 1.5 GAL. FLT ATTENDANT REPORTED GRINDING NOISE FROM ENG 1 WHEN QTY INDICATED 1.5- PUMPS AND SHUTOFFS WERE TURNSDR CA030926001Line · cracked(CAN) DURING THIS FLIGHT WE EXPERIENCED A HYDRAULIC FAILURE OF THE NR 2 HYDRAULIC SYSTEM NUMBER . AFTER THE LANDING, THE INSPECTION REVEALED A CRACKED ENGINE DRIVEN PUMP FEED PRESSURE TUBE.MOD 8Q100820 WAS INTRODUCED TO IMPROVE THE RELIABILITY OF THE TUBES BY SDR CA030911002Servo · damaged(CAN) PILOT CONDUCTED PREFLIGHT CHECK AND ON AIRCRAFT RUN UP COMPLIED WITH THE INTENT OF AD CF 200315R1. DURING THE TEST UPON DEPLETION OF THE HYDRAULIC SYSTEM ACCUMULATORS, CYCLIC MOVED TO THE LT FWD QUADRANT UNCOMMANDED. THE TEST WAS REPEATED 12 TIMES AT BOTSDR MWEA030369Hydraulic Line · inoperativeHYRAULIC RIGHT AND LEFT LOW ALERT APPEARED. REMOVED AND REPLACED PRESSURE LINE AT HYDRAULIC PUMP.SDR QXEA200301114Line · rupturedON FLIGHT 2060 SEA TO YVR AIRCRAFT RETURNED TO FIELD DUE TO: AFTER GEAR RETRACTION NR 1 ENGINE HYDRAULIC PUMP CAUTION WARNING LIGHT ILLUMINATED. AT THE SAME TIME QUANTITY AND PRESSURE WENT TO ZERO. THE SYSTEM WAS WITHOUT PRESSURE FOR 25 MINUTES. WHEN STANDBY PSDR NP0002Line · crackedFOUND HYDRAULIC FLUID AROUND AFT END OF LT HYDRAULIC RESERVOIR. CLEANED AREA AND FOUND NOTHING. PRESSURIZED THE NR 1 HYDRAULIC SYST AND FOUND NO LEAK. AFTER SEVERAL FLIGHTS, FOUND SIMILAR HYDR FLUID TRACES AROUND HYD RESERVOIR BUT FOUND NO CRACK. CLEANED AREASDR SIMA200325308Valve · inoperativeDURING TAKEOFF AT ABOUT 110 KNOTS THE AIRCRAFT VEERED HARD TO THE LEFT. TAKEOFF WAS ABORTED AND AIRCRAFT WAS RETUREND TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE POWER BRAKE CONTROL VALVE IAW SAAB MM. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND SDR AWXA200301027Hydraulic System · lowAIR TURN BACK-FLT 0459-AFTER T/O, EN ROUTE, RECD ECAM YELLOW AND GREEN HYD SYS LOW PRESS IND, TURNED BACK AND LANDED. MAINT PWR UP YELLOW, GREEN HYD SYS, NO ECAM WARNING PRESENT, FOUND QTY LEVELS OF BOTH SYS LOW, BUT ABOVE MIN GAUGE LEVEL (GAUGE AND ECAM QTY LSDR SIMA200325101Shutoff Valve · crackedCREW REPORTED HYDRAULIC SYSTEM NR 2 ZERO PERCENT QUANTITY AND ZERO PRESSURE. RAMP REPORTED A LARGE QUANTITY OF FLUID UNDER AFT FUSELAGE. MAINTENANCE FOUND THE NR 2 HYDRAULIC SHUTOFF VALVE LEAKING DUE TO THE VALVE BODY SPLIT. MAINTENANCE REMOVED AND REPLACEDSDR 2003F00559Flex Line · damagedDURING CRUISE FLIGHT, AN ECAM WARNING MSG 'HYD YELLOW RESERVOIR LOW LEVEL' WAS DISPLAYED, ALSO A YELLOW HYDRAULIC SYSTEM LOW PRESS MESSAGE CAME, THE AIRCRAFT DEVIATED ITS SCHEDULE FLIGHT TO EL SALVADOR STATION FOR MAINTENANCE. AFTER LANDING AT SAL STATION, TESDR P5CA0300937Hose · chafedON MECHANIC PREFLIGHT FOUND HYD FLUID LEAKING FROM NR 1 ENG. REPAIRED PRESSURE LINE IAW 20-11-05 PERFORMED LEAK CHECK IAW 29-11-00.SDR CA030925002Line · ruptured(CAN) DURING TAXI-OUT, FUSELAGE HYD LINE RUPTURED AT A POINT OVERHEAD ROW 4 - 5 (CA. FS X 407.7 + 2) JUST FORWARD OF THE PRESSURE FITTING AND BELOW THE 90 DEGREE BEND ROUTING THE LINE DOWNWARD. 7 PASSENGERS WERE ON BOARD (1 PASSENGER AND 1 FA WERE TAKEN TO HOSDR PCAA0309105Line · brokenWHILE ON DEICING PAD CREW REPORTED THAT A HYDRAULIC LINE WAS LEAKING IN THE CABIN AT SEATS 5DF AND 6DF. EMERGENCY WAS DECLARED. FLIGHT ATTENDANT AND ONE PASSENGER WERE TAKEN TO HOSPITAL DUE TO AFFECT OF HYDRAULIC FLUID IN THE CABIN. MAINTENANCE REPLACED A HSDR DL757030812Hydraulic Line · leakingLT HYD QTY WENT TO 00-HAD PRESURE ON LT SIDE GOOD AT 3100. RETURNED TO CVG AFTER COORDINATING WITH MTC. EICAS MSGS LT HYD SYS PRESS, RUDDER RATIO, LT HYD QTY. REPLACED FLEX LINE AT LEFT SIDE ELECTRIC PUMP.SDR 2003FA0001043Shuttle Valve · leakingOXYGEN ACCESS PANEL ON RIGHT SIDE OF FUSELAGE HAD A NOTICEABLE AMOUNT OF SKYDROL-500 ACCUMALATED INSIDE THE ACCESS DOOR OF THE O-2 SERVICE PANEL. IT WAS DETERMINED THAT THE FLUID WAS COMING FROM THE EMERGENCY LANDING GEAR AIR RELEASE VALVE VENT PORT DUE TO A SDR AUS20031331Shutoff Valve · faulty(AUS) LT ENGINE FIREWALL MOUNTED HYDRAULIC FIREWALL SHUTOFF VALVE FAULTY. VALVE WOULD NOT FULLY CLOSE WHEN THE FIRE SWITCH WAS OPERATED WHICH ALLOWED HYDRAULIC FLUID TO LEAK PAST THE VALVE.SDR CA030908002Line · chafed(CAN) AFTER TAXIIING THE AIRCRAFT FOR MAINTENANCE WE NOTICED HYDRAULIC FLUID ON THE FLOOR UNDER THE RT WING ROOT. AFTER REMOVING THE BELLY PANEL FOR INSPECTION THE LEAK WAS FOUND TO BE LOCATED ABOUT 20 INCHES AFT OF THE LEADING EDGE OF THE RT WING WHERE THE LSDR GAIA03080OPHose · leakingAFTER TAKEOFF FROM ATL AT 1000 FT AGL THE FLIGHT CREW NOTICED THAT THE 'A' SYSTEM HYDRAULIC FLUID WAS LOST. THE CREW RETURNED TO ATL MANUALLY EXTENDING THE LANDING GEAR AND FLAPS. AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED NR 1 ENGINE DRIVEN PUMP SDR CA030903002Manifold · failed(CAN) THE INDICATOR LIGHT FOR THE NR 1 HYD SYS WILL NOT EXTINGUISH WHEN POWERED BY THE HYDRAULIC CART NOR WILL THE RESERVOIR DRAIN INTO THE HYDRAULIC CART. (SUSPECT THE TEST SCREW ORIFICE IN THE VALVE BODY IS PLUGGED). THE HYDRAULIC POWER PACK ASSEMBLY WAS REPSDR AUS20030971Line · cracked(AUS) HYDRAULIC LINE LOCATED IN LT WING ADJACENT TO RESERVOIR CRACKED AND LEAKING.SDR 2003F00609Line · wornAFTER TAKEOFF, AIRCRAFT LOST SYSTEM 'A' HYDRAULICS. AIRCRAFT DIVERTED BACK TO MMUN AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED RIGHT MAIN ACTUATOR GEAR HYDRAULIC LINE WITH TEMPORARY FLEX LINE IAW MM 20-10-5, OPS CHECK AND LEAK CHECKSDR DXTA200300106Manifold · damagedDESCENDING THRU FL180 AN UNCOMMANDED EXTENSION OF GEAR WAS EXPERIENCED (GEAR DID NOT FULLY EXTEND) GOT UNLOCKED LIGHT THEN GEAR RETRACTED. - TROUBLESHOT AND FOUND HYDRAULIC MANIFOLD DOES NOT HOLD PRESSURE. REMOVED AND REPLACED LANDING GEAR HYDRAULIC MANIFOLD ASDR 2003FA0000898Line · corrodedDURING GEAR RETRACTION AND GEAR EXTENSION, HYDRAULIC FLUID LEAKED UNDER PRESSURE. FOUND THIS LINE CORRODED SO BADLY THAT A HOLE HAD BEEN FORMED IN THE LINE. THE CORROSION WAS DUE TO PREVIOUS ROUTING OF AIR CONDITIONING DUCT TY-WRAPPED TO THE FOUR LANDING GEASDR AUS20030884Line · leaking(AUS) HYDRAULIC PRESSURE LINE LOCATED IN AREA BELOW PILOTS RUDDER PEDALS CRACKED AND LEAKING. LOSS OF HYDRAULIC FLUID.SDR AALA20030906O-Ring · leakingDURING DESCENT, THE NR 1 HYD SYSTEM WENT TO 36 PERCENT AND THE HYD SYSTEM NR 1 LOW LIGHT ILLUMINATED. THE ALTERNATE FLAP AND LANDING GEAR EXTENSION PROCEDURES WAS USED. CREW DECLARED AN EMERGENCY AND LANDED AT YYZ WITHOUT FURTHER INCIDENT. REPLACED THE NR 1SDR MALA030388Selector Valve · leakingAIR RETURN TO OKC DUE TO GREEN HYD SYSTEM LOW ON FLUID. FERRIED TO MSP. FOUND STBY GEN SELECTOR VALVE LEAKING HYD FLUID. FROM LOG SHEET DISC 17: RESEALED RIGHT WING ROOT PER EOA57042 LEAK CHECK GOOD REMOVED AND REPLACED STBY GEN SELECTOR VALVE PN 71149-3 SSDR AELLCDG001Hydraulic System · misoverhauledSEVERAL COMPONENTS OF THIS TANDEM HYDRAULIC UNIT RECENTLY OVERHAULED, SEEM TO HAVE BEEN TREATED IN A WAY THAT NEITHER CORRESPONDS TO THE ORIGINAL DRAWINGS/SPECIFICATIONS OF THE UNIT NOR THE MBB-BK 117 REPAIR MANUAL (REM, CHAPTER 401)SDR XNOA01148Hose · brokenDURING TAXI LOW LEVEL LIGHT ON BLUE SYSTEM HYDRAULICS. FOUND INBOARD AILERON BLUE SYSTEM ACTUATOR HOSE BROKEN. REPLACE THE HOSE. NO LEAK FOUND. OPERATION NORMAL IAW A300 MM 27-11-00.SDR P5CA0300924Hydraulic Line · rupturedNR 1 HYDRAULIC SYS QUANITITY AND PRESSURE DROPPED TO ZERO AT STARTUP. SWAPPED PRESSURE LINE FROM NR 2 TO NR 1. CAPPED NR 2 ADP LINE FITTINGS. PERFORMED LEAK CHECKS, OPERATIONAL CHECK PER 29-11-00. SYS OPERATIONAL CHECK AND LEAK CHECK NORMAL.SDR AALA20030901O-Ring · leakingAFTER TAKEOFF DURING GEAR RETRACT, RT HYDRAULIC PRESSURE LOW LIGHT CAME ON, GEAR DOOR OPEN LIGHT CAME ON AND HYDRAULIC QUANTITY DROPPED TO ZERO. CREW DECLARED AN EMERGENCY AND RETURNED WITHOUT FURTHER INCIDENT. REPLACED RUDDER SHUTOFF VALVE O-RING AND PLUG ASDR AALA20030893O-Ring · cutAFT APPROX 1 HOUR OF FLIGHT CENTER HYD QTY EICAS MSG DISPLAYED. PUMPS SELECTED OFF IAW PROCEDURE STOPPED FLUID LOSS AT .40. UPON INSPECTION, FOUND DPI FOR ADP PRESS MODULE LOOSE WITH A CUT O-RING. REPLACED O-RING, NO LEAKS NOTED. SERVICED CTR HYDRAULIC QUASDR CA030828001Hose · ruptured(CAN) DURING FLIGHT THE PILOT NOTICED A LOSS OF HYD PRESSURE ON NR 1 HYDRAULIC SYSTEM. THE SYSTEM WAS DEACTIVATED AND THE PILOT RETURNED TO BASE. AFTER LANDING, SYSTEM NR 1 WAS INSPECTED AND A HYD PRESSURE HOSE WAS FOUND RUPTURED. THE HOSE ASSEMBLY WAS REPLACSDR A6WA20030124Hydraulic Line · leakingON TAKEOFF, NR 2 HYDRAULIC SYSTEM QUANTITY DECREASED TO 0 PERCENT, NR 2 EDP, RAN 11 MINUTES AT 0 PERCENT RETURNED TO LNK. REMOVED AND REPLACED NR 2 SYSTEM HYD FILL LINE. (M)SDR UPS03M41133Hydraulic System · failedLT HYD SYS FAILED. (RT HYD CNTRL C/B POPPED) PER A/C STATUS IN IMPACTS THIS OCCURED IN CRUISE. R&R HYD SYS CONTROLLER PER 29-08-01 OP TEST DUE FOR REPLACEMENT OF CONTROLLER (A/P NO. ILLEGIBLE) RAN ENGS AND TESTED PUMPS & HSC PER 29-11-20 & 29-11-21 NO FAULTS.SDR CA030910007Servo · unserviceable(CAN) DURING GRD CHECKS AT IDLE & FLIGHT IDLE, CYCLIC CONTROL MOVING UNCOMMANDED LT & FORWARD. CYCLIC CONTROL WOULD CONTACT STOP, AFTER 1-2 SECONDS IT COULD BE BROUGHT BACK TO CENTER POSITION & APPEARED NORMAL. MOVEMENT COULD BE DUPLICATED ON SUBSEQUENT RUSDR 0301583226Line · chafedIN MODERATE TURBULENCE, AUTOPILOT KICKED OUT AND RECEIVED YELLOW HYDRAULIC SYSTEM RESERVOIR LOW LEVEL MESSAGE ON ECAM. FOLLOWED COM PROCEDURE AND LANDED AT DTW UNEVENTFULLY. FOUND YELLOW SYSTEM COMPLETELY EMPTY. FOUND SPOILER HYDRAULIC PRESSURE LINE CHAFED ON SDR UPS03841118Fitting · leakingCREW REPORTED LOSING HYD SYSTEMS. DECLARED EMERGENCY. A/C LANDED W/O INCIDENT. HYD QTY DROPPED TO STANDPIPE LEVEL FOLLOWED BY RUDDER & AILERON CONTROL MANUAL LIGHTS COMING ON, (FL 390 & 150 NM FROM DESTINATION). REMOVED AND REPLACED RESERVOIR AIR PRESS REGSDR RYN2004F00022Line · chafedON CLIMB OUT, LOST HYDRAULIC A-SYSTEM. ACCOMPLISHED APPROPRIATE CHECK LIST AND MANUALLY EXTENDED THE LANDING GEAR. EMERGENCY DECLARED AND AIRCRAFT RETURNED. AIRCRAFT LANDED MDT WITHOUT INCIDENT. REPLACED NR 2 ENGINE HYDRAULIC PUMP FLEX PRESSURE LINE. LEAKSDR 2003FA0000912Line · corrodedBRAKE LINE IS MADE FROM -4 ALUMINUM LINE. CRACK STARTS .2500 INCH FROM FLARED END, AND RUNS APPROX. .3750 INCH LONG LENGTH OF LINE. PROBABLE CAUSE IS FATIGUE OR LINE STRESSED, OR CORROSION.SDR ERAA097529Guide · shortedGUIDE ASSY IS SHORTED, HAS BROKEN SOCKET. DISASSEMBLED, CLEANED, INSPECTED, INSTALLED NEW SOCKET, POTTED AND TESTED. INSPECTED AND REPAIRED IAW MBB BO105 REM 405.SDR 00104Line · leakingON APPROACH, ATTEMPTED NORMAL GEAR EXTENSION BUT HYDRAULIC PRESSURE WAS TO LOW TO EXTEND THE GEAR. EXTENDED GEAR USING EMERGENCY GEAR PROCEDURE AND LANDED WITH NO PROBLEM. FOUND RT ENGINE DRIVEN HYDRAULIC PUMP PRESSURE LINE LEAKING. REMOVED AND REPLACED HOSE ASDR CWQ2004F00003Line · chafedREPORT 110840, INSPECTED WHEEL WELL AREAS LT AND RT, FOUND THE LT WHEEL WELL LINES TO BE OK AT THIS TIME. RT WHEEL WELL BRAKE LINE ASSY , PN 6627100-34 AND THE FLAP RETRACT LINE ASSY PN 6627000-68, TO BE CHAFED BEYOND ALLOWABLE LIMITS STATED IN MM. REMOVED A
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