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 CA010322005Line · leaking(CAN) AIRCRAFT WAS CLIMBING THROUGH 8000 FEET WHEN NR 1 A SYSTEM HYDRAULIC PUMP FAILED, FOLLOWED SHORTLY BY THE NR 2 PUMP FAILURE. QUANTITY WAS DECREASING RAPIDLY. AIRCRAFT RETURNED. INSPECTION FOUND A SYSTEM FLEX LINE, LOCATED FORWARD OF L/H GEAR LEAKING. REPMar 14, 2001 · Boeing 7372L9SDR SWIA972428Hydraulic Line · leakingDURING CLIMBOUT, LOST HYDRAULIC SYSTEM ONE PRESSURE AND QUANTITY. RETURNED TO SLC. FOUND HYDRAULIC LINE FOR ENGINE DRIVEN HYDRAULIC PUMP PSI LINE IN PYLON TO BE LEAKING. REMOVED AND REPLACED LINE. OPS CHECK AND LEAK CHECKED GOOD.Mar 14, 2001 · N408SW · Cndair CL6002B19SDR 951141Hose · burstDURING FLIGHT BOTH THE HYDRAULIC FLOW LIGHTS AND THE HYDRAULIC RESERVEOIR LOW LEVEL LIGHT ILLUMNINATED. FOUND THE PRESSURE LINE FROM THE NR 1 HYDRAULIC PUMP BURST APPROX. 18 INCHES FROM THE PUMP. THERE WERE NO CHAFF MARKS ON THE HOSE, SUSPECT INTERNAL FAILURE Mar 14, 2001 · N3262M · Cessna 550SDR SWAA010761Hydraulic Line · leakingAIR TURNBACK, NLG RED WARNING LIGHT ILLUMINATED AFTER TAKEOFF/GEAR RETRACTION. LOUD NOISE FROM DRAG CONTINUED UNTIL GEAR HANDLE PLACED IN DOWN POSITION. ALL INDICATIONS THEN APPEARED NORMAL. FOUND NLG UPLOCK HYDRAULIC LINE LEAKING. REMOVED AND REPLACED HYDMar 13, 2001 · N658SW · Boeing 7373L9SDR RRXA010022O-Ring · leakingLOST HYDRAULICS DOWN TO THE STAND-PIPE. PERFORMED PROCEDURES PER QRH ABNORMAL CHECKLIST. REPLACED O-RINGS ON SLOT VALVE PER DC8 MM 29-10-20, LK AND OPS CK GOOD AT THIS TIME.Mar 13, 2001 · N996CF · Doug DC862FSDR 0100983203Hydraulic Line · leakingDURING CRUISE, RECEIVED HYD G RSVR LO LVL AND HYD G SYS LO PR MESSAGES. SELECTED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP AND PTU OFF PER COM PROCEDURES. DURING APPROACH AT FINAL DESTINATION, SELECTED PTU ON RESTORING GREEN SYSTEM PRESSURE TO EXTEND LANDING GEAMar 12, 2001 · N303US · Airbus A320211SDR DL72W010399Module · failedLOSS OF SYSTEM A FLUID AND PRESSURE SHORTLY AFTER LDG GEAR WAS SELECTED DN. ALL 3 GREEN DN LOCK LGTS ILLUM AND RED DR LGT REMAINED ILLUM. THE L/R GEAR DR AND TAIL SKID AMBER ANNUNCIATORS ON S/O PNL REMAINED ILLUM. FOLLOWED HYD LOSS PRO CEDURES PER POM. UNMar 11, 2001 · N2816W · Boeing 727247SDR CALA0100218Hydraulic Line · leakingTHE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM EWR. OVERRIDE WAS USED AND THE GEAR RETRACTED. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MAIN GEAR TRUCK PRESSURE LINE LEAKING. THE LINE WAS REPLACED USMar 11, 2001 · N17126 · Boeing 757224SDR 20010420CW011Hydraulic Line · brokenNOSE GEAR UP HOSE PNS217840105 CAME OUT OF SWEDGE FITTING.Mar 9, 2001 · N9864B · Cessna 172RGSDR AU010208Hose · failed(AUS) NR 4 BRAKE HYDRAULIC HOSE FAILED.Mar 9, 2001 · Boeing 767338SDR MWEA010299Fitting · leakingGATE CREW REPORTED HAZE/SMOKE WITH ODOR IN CABIN. MAINTENANCE FOUND HYDRAULIC LEAK AT PRESSURE TRANSMITTER FITTING LOOSE CAUSING FLUID TO BE SUCKED INTO APU INLET. TIGHTENED LOOSE FITTING, PRESSURIZED SYSTEM AND NO LEAKS NOTED.Mar 9, 2001 · N810ME · Doug DC982SDR GAIA01107OPHydraulic Line · crackedFLT 7359 - OAK-MHR - DURING CLIMB, THE SYSTEM A HYDRAULIC QUANTITY STARTED TO DECREASE. THE CREW DECLARED AN EMERGENCY AND LANDED SAFELY IN MHR WITH NO FURTHER PROBLEMS. MAINTENANCE FOUND A CRACKED HYDRAULIC PRESSURE LINE TO THE RIGHT WING LEADING EDGE DEVICMar 8, 2001 · N6810 · Boeing 727223SDR CA010706015Line · leaking(CAN) PILOT REPORT: HYDRAULIC SYSTEM NR 2 LOW PRESSURE MESSAGE DURING CRUISE. FOUND HYDRAULIC SYSTEM NR 2 EMPTY OF FLUID. MAINTENANCE FINDING: FOUND FITTING OF FILL LINE LEAKING (REF IPC 29-11-00-5-270). FOUND FITTING ADAPTER WRONG INSTALLED ON FILL LINE. INSTMar 5, 2001 · Cndair CL6002B19SDR AALA20010377Hydraulic Line · leakingLAX - FLT 364 - EN ROUTE FLL-LAX, DETECTED LEFT SIDE HYDRAULIC SYSTEM DECREASE TO ZERO. LANDED LAX WITHOUT FURTHER INCIDENT. REPLACED LEFT GEAR DOWN LOCK LINE. SERVICED HYDRAULIC SYSTEM. LEAKS CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Mar 5, 2001 · N696AN · Boeing 757223SDR RRXA010015Hydraulic Line · rupturedON TAXI IN A/C LOST ALL HYD FLUID. FOUND FLEX LINE ON STOW PUMP RUPTURED. REMOVED AND REPLACED FLEX LINE. LEAK AND OP CK''S GOOD. A/C RETURNED TO SERVICE.Mar 2, 2001 · N997CF · Doug DC862FSDR HALA0100062Shutoff Valve · leakingHNL - FLT 152 - NR 2 ENGINE BOTH HYD PRESS LOW LIGHTS CAME ON AS FLUID QUANTITY DECREASED TO ZERO. REPLACED 1-3 NON-REVERSIBLE SHUTOFF VALVES. LEAK AND OPS CHECK OK. (M)Feb 28, 2001 · N152AA · Doug DC1010SDR AALA20010361Line · leakingDFW - FLT 1881 - EN ROUTE AUS-SJC - LEFT HYDRAULIC SYSTEM QUANTITY DECREASED TO ZERO. DIVERTED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED RIGHT MAIN GEAR DOOR ACTUATOR HYDRAULIC FLEX LINE. SERVICED HYDRAULIC SYSTEM. PERFORMED LEAK CHECK. NO LEAKS NFeb 28, 2001 · N670AA · Boeing 757223SDR DL757010339Hydraulic Line · leakingAIRCRAFT DIVERTED TO MCO WITH GEAR DOOR LIGHT AND EICAS MSG WITH GEAR RETRACTED OR EXTENDED. FOUND HYD LINE LEAKING RT GEAR TRUCK POSITION LINE AT TOP OF RT GEAR FLEX LINE. PER MM 20-10-09 INSTALLED TEMP HYD LINE LEAK AND OPN CKS NORMAL. FWD TEMP LINE TO MCFeb 28, 2001 · N660DL · Boeing 757232SDR 2001UALA00163Module · leakingSTRONG ODOR DETECTED IN COCKPIT DURING CRUISE WHEN UPPER RECIRCULATING FAN IS TURNED OFF. ODOR GOES AWAY QUICKLY WHEN FAN IS TURNED BACK ON. LOWER FAN OK. SUPPLEMENTAL DATA UPDATE THE PROBLEM WAS DUE TO FAULTY RT HYDRAULIC PNEUMATIC PRESSURIZATION MODULE. Feb 27, 2001 · N797UA · Boeing 777222SDR AU010199Line · leaking(AUS) HYDRAULIC B SYSTEM RESERVOIR TO STANDBY SYSTEM SUPPLY LINE LEAKING. LOSS OF HYDRAULIC FLUID.Feb 27, 2001 · Boeing 737376SDR ARWA1000204O-Ring · tornHYDRAULIC SYSTEM LOSS DOWN TO STADPIPE, EMERGENCY CHECK, LIST C/W. RETURNED TO STATION. FOUND O-RING FROM RT AILERON ACTUATOR TUBING FITTING LEAKING. REPLACED O-RING IAW MM 20-60-0, OPS CHECK NORMAL. NO LEAKS NOTED, SYSTEM CHECK SATISFACTORY.Feb 25, 2001 · N802BN · Doug DC862SDR AALA20010336O-Ring · leakingEWR - FLT 1704 - EN ROUTE ORD-EWR, DURING TAXI AIRCRAFT CABIN FILLED WITH SMOKE. DETECTED HYDRAULIC FLUID EMPTY. REPLACED O-RING AT RUDDER SHUTOFF VALVE PLUG. ACCOMPLISHED LEAK CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Feb 24, 2001 · N582AA · Doug DC982SDR AU010238Pipe · chafed(AUS) HYDRAULIC PIPES LOCATED IN LT WHEEL WELL RUBBING ON LANDING GEARDOOR PREVENTING REAR UPLOCK SWITCH FROM ACTIVATING.Feb 23, 2001 · Fokker F28MK1000SDR GAIA01073BOPLine · rupturedFLT 1805 - FWA-LAX - AT FL310, HYDRAULIC SYSTEM ''A'' PRESSURE AND QUANTITY WENT TO ZERO. AIRCRAFT MADE AN UNEVENTFUL LANDING IN DEN. TROUBLESHOOT AND FOUND RUPTURED HYDRAULIC LINE IN RIGHT SIDE OF AFT AIRSTAIR. REMOVED AND REPLACED THE HYDRAULIC LINE PER BFeb 23, 2001 · N79748 · Boeing 727224SDR USAASB01055Hydraulic Line · leakingPIT - FLT 2622 - EN ROUTE FROM BWI TO MDW, AT FL280, FLIGHT EXPERIENCED A LOSS OF SYSTEM A HYDRAULIC QUANTITY FOLLOWED BY A LOSS OF HYDRAUIC PRESSURE. CREW DECLARED AN EMERGENCY AND DIVERTED TO PIT. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND WAS TOWED TO THEFeb 23, 2001 · N253AU · Boeing 737201SDR AU010239Hydraulic System · low(AUS) NR 2 HYDRAULIC SYSTEM LOW QUANTITY. INVESTIGATION COULD FIND NOEVIDENCE OF LEAKS. SUSPECT SYSTEM NOT REPLENISHED.Feb 22, 2001 · Fokker F28MK1000SDR MALA010211Reservoir · lowON TAKEOFF FLIGHT 2822 GEAR WAS RETRACTED, THE 3 GREEN LIGHTS WENT OUT BUT THE INTRANSIT LIGHT REMAINED ILLUMINATED AND THE HYDRAULIC PUMP KEPT RUNNING. AIR RETURN TO DTW. MAINTENANCE SERVICED HYDRAULIC SYSTEM UP TO LIMIT, CYCLED THE GEAR SEVERAL TIMES, ALL Feb 22, 2001 · N414XJ · Saab 340BSDR USAASB01054Hydraulic Line · rupturedCLT - FLT 1507 - ON CLIMB-OUT, AT FL100, THE B HYDRAULIC SYSTEM LOW PRESSURE LIGHT ILLUMINATED WITH HYDRAULIC QUANTITY INDICATING ZERO. CAPTAIN DECLARED AN EMERGENCY AND THE FLIGHT RETURED TO FIELD AT CLT. ON RETURN TO CLT, CREW SUSPECTS THE STANDBY HYDRAULIFeb 21, 2001 · N511AU · Boeing 7373B7SDR AC2A072815Hose · leakingAT CRUISE TO LEEVILLE (LA) HELIPORT, THE PILOT HEARD A LOUD GRINDING NOISE FOLLOWED BY COMPLETE HYDRAULIC FAILURE. THE PILOT PERFORMED THE EMERGENCY PROCEDURE THEN CONFIRMED IT WITH THE BOOK WITH NO CORRECTION TO THE EMERGENCY. PILOT PERFORMED A SHALLOW APPFeb 20, 2001 · N17592 · Bell 206L3SDR P2EA01003Line · wornFLT 650 - MYR - DURING FLIGHT INBOUND TO MYR A SYSTEM HYDRAULIC QUANTITY WHEN TO 0, FOLLOWED BY A SYSTEM PRESSURE. DURING INSPECTION FOUND A SYSTEM WITH HYDRAULIC LINE LEAKING. REMOVED AND REPLACED TUBE ASSEMBLY. OPS CHECKED AND LEAK CHECKED IAW BOEING MM 2Feb 17, 2001 · N125NJ · Boeing 7372B7SDR AU010148Pipe · leaking(AUS) HYDRAULIC LINE LOCATED IN RH WHEEL BAY CONTAINED A PINHOLE LEAK.Feb 17, 2001 · Dhav DHC8102SDR CA010301011Tube · leaking(CAN) THE FLIGHT CREW OBSERVED HYDRAULIC FLUID LEAKING FROM THE L/H NACELLE DURING WALKAROUND. MAINTENANCE INVESTIGATION RESULTED IN REPLACEMENT OF THE NR 2 FLIGHT SPOILER UNLOADING LINE.Feb 17, 2001 · Dhav DHC8102SDR 2001UALA00120Filter · leakingLOSS OF THE B-SYSTEM HYDRAULICS. *S/D* REPLACED B-SYSTEM ACOUSTIC FILTER AND ASSOCIATED O-RING, AND SERVICED B-SYSTEM HYDRAULICS. NO FURTHER LEAKS EVIDENT.Feb 17, 2001 · N384UA · Boeing 737322SDR CA010305015Selector Valve · failed(CAN) THE PILOT REPORTED THE HYDRAULIC LIGHT WAS ILLUMINATED ON THE CAWS PANEL. THE ACCUMULATOR PRESSURE WAS VERIFIED, AND FOUND CORRECT. THE SERVICE SLECTOR WAS REPLACED.Feb 16, 2001 · Pilats PC1245SDR 0100523207Hydraulic Line · leakingDURING CRUISE, RECEIVED HYD Y RSVR LO LVL MESSAGE. FOLLOWED COM PROCEDURES, CONTINUED TO FINAL DESTINATION, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED HYDRAULIC LINE BETWEEN THE AUTO BRAKE SELECTOR AND PARK BRAKE VALVE. NO OTHER LEAK NOTED.Feb 16, 2001 · N307US · Airbus A320211SDR AUS20011127Pipe · worn(AUS) HYDRAULIC PRESSURE LINE WORN. LINE WAS INADEQUATELY SECURED.PERSONNEL/MAINTENANCE ERROR.Feb 15, 2001 · Cessna 172RGSDR AUS20010768Hose · ruptured(AUS) LT MAIN LANDING GEAR ACTUATOR UP HOSE BURST. LOSS OF SYSTEM A' HYDRAULIC FLUID.Feb 15, 2001 · Boeing 737377SDR CA010320021Line · loose(CAN) PILOT OBSERVED GREEN SYSTEM HYDRAULICS WAS LOOSING FLUID. AIRCRAFT DIVERTED TO YYT. HYDRAULIC LINE IN NR 1 ENGINE PYLONFOUND LOOSE. LINE TIGHTENED AND LEAK CHECK CARRIED OUT SERVICEABLE.Feb 14, 2001 · Airbus A310304SDR JDMA648BLine · crackedHYDRAULIC TRANSFER LINE IN AUXILARY SYSTEM, LINE WAS FOUND BROKEN AT FLAIR CAUSING LOSS OF HYDRAULIC FLUID AND HYDRAULIC SYSTEM FAILURE. AIRCRAFT WAS REPAIRED AND RETURNED TO SERVICE.Feb 14, 2001 · N28AY · Lear 28SDR AWXA0001340Hydraulic System · lowSEA - EMERGENCY LANDING - 2/10/01 - ON DESCENT INTO SEA THE GREEN HYDRAULIC SYSTEM WENT TO LOW LEVEL. IN SEA THE AIRCRAFT WAS INSPECTED AND NO LEAKS FOUND. THE GREEN SYSTEM HYDRAULIC SYSTEM WAS SERVICED TO FULL AND NO FURTHER PROBLEMS REPORTED. THIS WAS THEFeb 14, 2001 · N627AW · Airbus A320231SDR UPS01235000Module · failedINSPECTION TYPE:N/A ON CLIMBOUT OF WAW A-SYS HYD PRESS DROPPED TO ZERO. NO FLUID LOSS. INADVERTANT DEPLOYMENT OF NR 1 THRUST REVERSER ON TOUCH DOWN. REPLACED A-HYD SYS PRESSURE MODULE DEACTIVATED NR1 T-R PER MEL. SUSPECT OUT OF RIG.Feb 13, 2001 · N922UP · Boeing 72731CSDR CA010308010Line · chafed(CAN) DURING A 60 MONTH/2400 HOUR INSPECTION, THE FLEXIBLE HYDRAULIC LINE (SUCTION TO THE ENGINE DRIVEN PUMP) OF THE NR 1 SYSTEM WAS FOUND TO HAVE CHAFED A HOLE THROUGH FUEL SHROUD SUPPLY LINE TO THE EDP.HYDRAULIC LINE P/N: AE3660010K0270FUEL SHROUD P/N: 601R6Feb 12, 2001 · Cndair CL6002B16SDR SWIA972370Hydraulic Line · chafedON APPROACH RECIEVED A GREEN (LEFT) SYTEM LOW LEVEL LIGHT GAUGE SHOWED TOP OF YELLOW ARC. A FEW MINUTES LATER RECEIVED A LOW PRESSURE LIGHT. THEN A FEW MINUTES LATER RECEIVED A MAIN PUMP LOW PRESSURE LIGHT WITH THE ELEC HYDRAULIC PUMP ON LIGHT. THE HYDRAULIFeb 12, 2001 · N583SW · Emb EMB120ERSDR JBXA000243Hydraulic Line · crackedNR 1 HYDRAULIC SYSTEM INDICATED ZERO PERCENT AT FL290 EN ROUTE TO BUF. RAN QRH AND DIVERTED TO PHL. FOUND PRESSURE LINE FROM EDP NR 1 TO PRESSURE FILTER CRACKED AT PRESSURE FILTER CONNECTION. REMOVED AND REPLACED PRESSURE LINE, REMOVED AND REPLACED EDP NR 1Feb 11, 2001 · N575ML · Cndair CL6002B19SDR 20010409SG008Hydraulic Line · damagedCCS - FLT TA610 - DURING CRUISE, THE HYDRAUIC SYSTEM ''A'' WAS LOSS, DUE TO THIS SITUATION, THE AIRCRAFT RETURNED TO CARACAS AIRPORT. AFTER LANDING, MAINTENANCE TECHNICIANS PERFORMED INSPECTION AND FOUND IN NR 1 ENGINE THE PRESSURE HOSE DAMAGED, IT WAS REMOVEFeb 9, 2001 · N235TA · Boeing 7372H6SDR 20010320CW012Line · failedLOST ALL HYDRAULIC PRESSURE GOING INTO AIRPORT. BLEW GEAR DOWN, LANDED, NO PROBLEMS. FOUND NOSE GEAR RETRACT LINE BURST, CAUSING LOSS OF ALL HYDRAULIC FLUID. REMOVED AND REPLACED HYDRAULIC LINE AND BOTH HYDRAULIC PUMPS.Feb 9, 2001 · N64CP · Lear 35LEARSDR CA010301031Shutoff Valve · leaking(CAN) ON START UP THE NR 1 SERVO JAM WARNING LIGHT WOULD NOT EXTINGUISH WHEN NORMAL HYDRAULIC PRESSURE WAS REACHED. THE FLIGHT CREW SHUT DOWN AND UPON EXITING THE AIRCRAFT SAW HYDRAULIC FLUID UNDER THE AIRCRAFT. THE ENGINEER FOUND THE NR 1 HYDRAULIC SYSTEM FLUFeb 9, 2001 · Skrsky S76ASDR 2001UALA00102B-Nut · leakingTHE AIRCRAFT EXPERIENCED A SYSTEM A-HYDRAULIC FLUID LOSS DURING CRUISE. AIRCRAFT DIVERTED TO CLE. *S/D* FOUND LOOSE B-NUT ON ELEVATOR FEEL COMPUTER FILTER HOUSING LINE. TIGHTENED APPROX 1 FULL TURN. STATIC LEAK STOPPED. SERVICED A-HYD SYSTEM TO FULL. RAFeb 9, 2001 · N7461U · Boeing 727222SDR AU010089Fitting · leaking(AUS) HYDRAULIC FITTING LOCATED IN LT OUTBOARD NACELLE LEAKING UNDERPRESSURE.Feb 5, 2001 · Emb EMB120SDR ARWA0010202O-Ring · damagedCLIMBOUT A LOSS OF HYDRAULIC FLUID DOWN TO STAND PIPE. AFTER LANDING MIA, FOUND HEAVY HYDRAULIC LEAK COMING FROM RT WING AILERON SWIVEL. INSPECTED SWIVEL AND FOUND BOTH O-RINGS DAMAGED. REMOVED AND REPLACED O-RINGS AS REQUIRED. FOUND NORMAL, NO LEAKS IAW DFeb 4, 2001 · N661AV · Doug DC863F
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