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 COMA0660292Line · leakingFLIGHT 5662- EN ROUTE MCO-RDU, RECEIVED A NR 1 HYDRAULIC SYSTEM LOW PRESSURE CAUTION, FLIGHT DIVERTED TO SAV. REPLACED LEAKING BRAIDED HYDRAULIC LINE.SDR SWAA061164Hydraulic Line · leakingAIR TURNBACK, ENGINE DRIVEN "A" SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. "A" SYSTEM QUANTITY DROPPED TO 1/4 FULL. R&R "A" SYSTEM HYDRAULIC ELECTRIC DRIVEN PUMP PRESSURE LINE PER MM.SDR 0600683201Line · leakingAFTER TAKEOFF RECEIVED MULTIPLE ECAM MESSAGES ON THE GREEN HYDRAULIC AND THEN YELLOW SYSTEM OVERHEAT AND MASTER WARNING "LAND ASAP". DECLARED AND EMERGENCY AND RETURNED TO MCO AND LANDING WAS UNEVENTFUL. FOUND SEVERED LINE 32-3200-4-0141 MFG NR AE707879-4 ANSDR CA060403026B-Nut · leakingHYDRAULIC FLUID LEAKING FROM FITTING. BACKUP NUT ON FITTING FOUND UNDER TORQUED. FACTORY TORQUE SEAL AND PAL NUT WERE FOUND UNDISTURBED. BACKUP NUT RETORQUED AND NO FURTHER DEFECTS FOUND.SDR CA060403020Elbow · split45 DEGREE UNIVERSAL ELBOW FITTING FOUND SPLIT WITH HYDRAULIC FLUID LEAKAGE ON THE NR 2 HYDRAULIC SYSTEM, IPC 29-11-00, FIG 20, VIEW K, ITEM NR 45. FITTING REPLACED WITH THE SYSTEM CHECKED SERVICEABLE.SDR DLM88060232Unknown · unknownDURING DESCENT WHEN SPEED BRAKE/ SPOILER HANDLE WAS MOVED AFT RT HYD SYS PRESS DROPPED TO 0 AND QTY EVENTUALLY INCREASED FROM 13 TO 18. LATER WHEN SLAT HANDLE MOVED TO EXTEND LEFT HYD PRESS DROPPED TO 0 AND LEFT QTY INSP AND REPLACED SYS PRESS RETURN CASE DRASDR COMA0660286Hydraulic System · contaminatedFLIGHT 5256 - DURING CLIMB-OUT OF CAK FLIGHT RETURNED TO THE FIELD DUE TO A LOUD NOISE FROM THE LANDING GEAR. PURGED AIR FROM THE NR 3 HYDRAULIC SYSTEM.SDR 0600669868Line · failedFOLLOWING TAKEOFF, THE CREW NOTED THAT THE LEFT HYDRAULIC SYSTEM QUANTITY DROPPED TO ZERO. NO MENTION OF EITHER SYSTEM PRESSURE INDICATIONS. COM PROCEDURES WERE COMPLIED WITH AND THE FLIGHT CONTINUED TO SCHEDULED DESTINATION. LANDING AT DTW WAS UNEVENTFUL ASDR BJ6A200612902Check Valve · leakingFLIGHT CREW REPORTED AFTER A FLIGHT FROM EGGW TO KEWR THAT THE A SYSTEM HYDRAULIC QUANTITY DECREASED FROM 92% TO 63%. THERE IS EVIDENCE OF FLUID IN THE RIGHT MAIN LANDING GEAR WELL AND ON THE AFT LOWER FUSELAGE. MAINTENANCE HAS DETERMINED THE SOURCE OF THE HSDR UIEA200600061Union · wornATB:LOSS NR 4 HYD SYSTEM AFTER GEAR UP. SYSTEM LEAKING. FOUND UNION ON HYD RETURN LINE WORN, REPLACED OPS AND LEAK CHECKED NORMAL AS PER MM 29-00-00.SDR ASMF200603015Hydraulic Line · leakingAIRCRAFT RETURNED FLIGHT, AFTER TAKEOFF AND LANDING GEARS UP, THE RIGHT HYDRAULIC FLUID QUANTITY WENT DOWN TO 2 QUARTS. AFTER LANDING, THE BRAKES TEMPERATURE REACHED 350 °C AND GOT STUCK. DURING MAINTENANCE REVISION A RIGHT HYDRAULIC SYSTEM LEAK WAS DETECTEDSDR DLM88060224B-Nut · looseNORMAL LANDING AND TAXI WHILE APPROACHING GATE. APU STARTED, FLT ATTENDANT REPORTED CABIN FILLING WITH SMOKE. APU/PNEUMATICS SHUTDOWN. CABIN DOORS AND EMERGENCY EXITS OPENED TO VENT. SMOKE DISSIPATED. L2 DOOR SLIDE WAS INADVERTANTLY DEPLOYED. MTC DISCOVESDR TAMF20060017OFilter · leakingDURING CLIMB, FLIGHT 850 (MDE-VCP), LEFT HYD QTY DECREASED TO ZERO AND SYSTEM PRESS & QTY LIGHTS ILLUM EICAS MSG L HYD SYS PRESS & LEFT HYD QTY DISPLAYED. RETURNED TO MEDELLIN. FOUND HYDRAULIC LEAK BY PCA SPOILER CAP FILTER. RIGHT NOW THE AIRPLANE IS OUT OFSDR SWAA061044Line · leakingDECLARED EMERGENCY, LOST B-SYSTEM HYDRAULIC PRESSURE. B-SYSTEM HYDRAULIC QUANTITY DROPPED TO 1/4 FULL. REMOVED AND REPLACED B-SYSTEM HYDRAULIC ELECTRIC DRIVEN PUMP LINE PER MM.SDR 2006FA0000442Hydraulic Line · chafedCOMPLETE INTERIOR REFURBISHING WAS DONE. 100 HRS AFTER AC WAS RETURNED TO SERV, NOSE AND LT MAIN GEAR WOULD NOT LOCK DOWN, PILOT LANDED WITH ONLY RT GEAR EXTENDED. HYD FLUID WAS DRIPPING FROM BELLY, UPON INVESTIGATION, ALUMINUM HYD LINE WAS CHAFED THROUGH BSDR NOZ2006F00000Shutoff Valve · failedON FINAL APPROACH, AFTER SELECTING LANDING GEAR AND FLAPS TO DOWN, THE CHECK HYD QUANTITY LIGHT CAME ON. QUANTITY READ ZERO. CREW PERFORMED A MISSED APPROACH AND LEFT THE AC IN LANDING CONFIGURATION. CREW FOLLOWED THE (COMBINED HYD SYSTEM FAILURE) CHECK LISSDR CA060322006Valve · stuckLANDING GEAR DID NOT COME UP ON CLIMB. PILOT FOUND COMPLETE FAILURE OF ALL HYDRAULIC SYSTEM. ON TROUBLESHOOTING, FOUND SOLENOID LANDING VALVE SCREEN STUCK ON VALVE SEAT CAUSING COMPLETE BYPASS OF THE HYDRAULIC FLUID. THIS VALVE WAS PLANNED TO BE REPLACED ATSDR CA060317011Hydraulic System · leakingON INVESTIGATING A HYDRAULIC LEAK IN THE NR 1 GEAR WELL AREA, CRACKS WERE NOTED IN THE CHANNELS P/N 101-120025-57 AND P/N 101-120025-55 AS WELL AS THE ANGLE'S P/N 101-120025-67 AND 101-120025-68. THE A/C HAD A HYDRAULIC GEAR INSTALLED IN 1988 (REPLACING THE MSDR CA060316007Manifold · malfunctionedDURING PILOT TRAINING AIRCRAFT COMPLETED A HYDRAULICS OFF LANDING. HYDRAULIC SWITCH WAS THEN TURNED BACK ON AND THE FORE AND AFT MOVEMENTS CAME BACK HOWEVER THE LATERAL MOVEMENTS DID NOT COME BACK TO NORMAL HYDRAULIC ON. AIRCRAFT WAS THEN SHUT DOWN AND HYDRASDR HNAA0600020Hose · leakingLOST NUMBER 2 HYDRAULIC FLUID AFTER GEAR RETRACTION, SYSTEM WENT INTO ISOLATION, ONE QUART LEFT IN SYSTEM, PRESSURE NORMAL. REMOVED AND REPLACED THE BLUE FLEXIBLE UP LINE TO NOSE GEAR DRAG STRUT ACTUATOR, SERVICED AND BLED SYSTEM.SDR KPVA20066Packing · leaking(PIREP) NR 1 HYDRAULIC LEAK. MX CONFIRMED HYDRAULIC LEAK NR 1 NACELLE, RIGHT SIDE BULKHEAD BEHIND FLAP POST COVER. REPLACED BAD PACKING STA Y163.40 LT. RAN ENGINE FOR LEAK CHECK GOOD. SERVICED HYDRAULIC RESERVOIR PER DHC-8 MM 29-00-00 PG 201-202.SDR 2006FA0000361Flex Line · rupturedDURING FLIGHT, LOST NR 1 HYDRAULIC PRESSURE, DIVERTED INTO AIRPORT AND LANDED WITHOUT INCIDENT. TROUBLESHOOT AND FOUND RUPTURED HYDRAULIC FLEX LINE, PN 605700311 WHICH IS MOUNTED ON THE PRESSURE SIDE OF THE HYDRAULIC EDP. INSTALLED NEW HYDRAULIC FLEX LINE WISDR CA060313004Line · chafedHYD FLUID LEAKING FROM LEFT ENGINE COMPARTMENT. PRESSURE LINE FROM HYD PUMP TO FIREWALL FOUND CHAFED AND LEAKING. LINE WAS CHAFED ON A UNION FITTING ON THE OIL TANK IN A "OUT OF VIEW" AREA. LINE REPLACED, GEAR SWINGS CARRIED OUT, HYD RESEVOIR TOPPED UP AND SDR 0600493238Priority Valve · leakingEN ROUTE ECAM HYD Y ENG 2 PUMP TO RR APPEARED. NO YELLOW FLUID REMAINING. FLIGHT CONTINUED TO DESTINATION DELCLARING A YELLOW EMERGENCY WITH AN UNEVENTFUL LANDING. REMOVED AND REPLACED YELLOW SYSTEM LOW AND HIGH PRESSURE FILTERS (NO CONTAMINATION NOTED). FSDR 2006UALA00369Screw · shearedRETURN TO FIELD DUE TO A LOSS OF GREEN HYDRAULIC SYSTEM. LOSS GREEN HYD FLUID LEVEL. YELLOW AND BLUE SYS APPEARS OK. SECURED GREEN HYD SYS PER IRREG PROCEDURES. INSTALL GROUND SAFETY LOCKS PER AMM 32-00-00 AND TROUBLESHOOT. SOURCE OF GREEN HYD QTY LOSS. SDR QXEA200600599Power Unit · malfunctionedPDX FLIGHT 2242: AFTER PUSHBACK AND AFTER START CHECKLIST (ENGINES 1 AND 2 BOTH UNFEATHERED) STANDBY PRESS INDICATED ZERO PSI STBY HYD PRESSURE SWITCH LIGHT WAS ON AND NO CAUTION/WARNING LIGHTS ILLUMINATED. NO C/B'S POPPED. CONDUCTED MEL PROCEDURE 29-30-2. SDR CA060228008Line · chafedFLUID LEAK ON RT GEAR "UP" HYDRAULIC RETURN LINE NOTICED DURING OVERNIGHT CHECK. LINE WAS CHAFED THROUGH DUE TO RUBBING ON A BRACKET. LINE REPLACED,GEAR SWING CARRIED OUT AND AIRCRAFT RETURNED TO SERVICE. TT-37255:17 TC-22887.SDR DXTA200601270Line · leakingAFTER SELECTING GEAR DOWN POWER BRAKE LOW PRESS AND ANTI SKID INOP ANNUNCIATOR LIGHTS WOULD NOT EXTINGUISH. USED EMERGENCY BRAKING, BRAKE RESERVOIR IS EMPTY. FOUND LT HYDRAULIC BRAKE LINE LEAKING. REMOVED AND REPLACED HYDRAULIC BRAKE LINE. BLEED LT AND RT SDR P5CA0601450Module · failedCREW REPORTED ON TAKEOFF ROLL, ANTI-SKID LIGHT CAME ON F/E PANEL, HAD R/F, R/R, L/F, AND L/R LIGHTS ON FOR R/H BODY GEAR. TAKEOFF ABORTED AT 60 KTS. REPLACED ANTI-SKID CONTROL MODULE PER MM 32-42-02, PERFORMED HIGH ENERGY STOP INSPECTION.SDR QXEA200600498Line · failedSEA FLIGHT NR 2133 AFTER PUSHBACK WHEN RELEASED EMERGENCY BRAKE NR 1 HYDRAULIC QUANTITY'S PRESSURE DROPPED TO 0. FOLLOWED BY NR 1 ENGINE HYDRAULIC PUMP AND ASSOCIATED CAUTION LIGHT. APPROXIMATELY 2-3 MINUTES NR 1 ENGINE RAN PRIOR TO SHUTDOWN. MAINTENANCE FOUSDR 06FDEA0812Hydraulic Line · chafedPDIS 671 29-11 0007374 22FEB06 OAK OPEN R LOGPAGES: 01086620 ECAM ALERT AT FL320 GREEN HYD SYS QNT LOW ALERT. MANUAL GEAR EXTENSION ACCOMPLISHED. FLUID DRIPPING FROM NR1 ENG RESEARCHING. FOUND 2 HYDR LINES LEAKING THAT HAD BEEN CHAFED THROUGH AT A CLAMP INSDR DL76L060145Hydraulic Line · splitAFTER TAKEOFF RIGHT GEAR DID NOT COME UP. INDICATIONS WERE GREEN RIGHT GEAR LIGHT, AMBER DOOR AND GEAR DISAGREE LIGHT, EICAS MESSAGE OF GEAR DISAGREE GEAR DOOR. FOUND GEAR UP PRESSURE LINE SPLIT AT I/B ATTACH HOSE REPLACED. P/N AS115-10K0324.SDR DLM88060129Hydraulic System · lowRIGHT HYD SYSTEMS QUANTITY DECREASED TO 5 QTS INFLIGHT. ACCOMPLISHED HYD QUANTITY DECREASING CHECKLIST. QUANTITY SHOWED 19 QTS INFLIGHT AND 7 QTS AFTER LANDING OPERATIONS NORMAL. INSP AIRCRAFT FOR HYD LEAKS, NONE FOUND. SERVICED HYD TO CORRECT LEVEL PER M/SDR MALA060066Hydraulic System · malfunctionedON APPROACH INTO DTW THE CREW EXPERIENCED AN ABNORMAL GEAR INDICATION AND HYD CAUTION LIGHT. FLAPS FAILED TO EXTEND BEYOND 15 DEG THE CREW DECLARED AN EMERGENCY AND DID AN EMERGENCY EXTENSION OF THE GEAR. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAIN ACCSDR HEEA108083Tube · looseNR 1 SERVO LIGHT CAME ON. SLOWED AIRCRAFT BELOW 125 KTS. EXPERIENCED NO BINDING OF LOSS OF HYDRAULIC PRESSURE. RECYCLED SERVO JAM CIRCUIT BREAKER, LIGHT STAYED ON. LIGHT WENT OUT UPON LANDING. MAINTENANCE FOUND THE B-NUT ON THE FORWARD END OF TUBE HAD BACSDR 2006UALA00268Hydraulic System · leakingLANDED UNDER AMBER ALERT DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. A/C TOWED TO GATE. GREEN SYS HYD QTY WENT TO ZERO. TROUBLESHOT GREEN SYS HYD LEAK. FOUND NR 2 ENG EDP PUMP LEAKING. FOUND PUMP HOUSING CRACKED. REPLCD PUMP. REPLACED LFT ENG HYD FILTER ASSY ANSDR CA060213004Line · cracked(CAN) TOTAL LOSS OF NR 2 HYDRAULIC FLUID, FROM A RUPTURE ON THE PRESSURE MANIFOLD LINE P/N MM670-75294-009. NR 2 HYDRAULIC LINES P/N MM670-75294-009, MM670-75294-005 AND SUPPORT CLAMPS P/N MM670-75800-041, MM670-75800-029 ALL REPLACED. ENGINE DRIVEN PUMP FAILESDR HEEA107983Tube · chafedDURING CRUISE THE NR 1 HYDRAULIC LIGHT ILLUMINATED. SWITCHES CHECKED AND JAM CIRCUIT BREAKER RESET. RETURNED TO HOUMA. FOUND NR 1 HYDRAULIC PUMP PRESSURE TUBE ASSEMBLY CHAFED BY ADJACENT TUBES. REPLACED AFFECTED TUBES.SDR CA060208009O-Ring · swollen(CAN) SHORTLY AFTER TAKEOFF, CREW NOTICED SYS (A) HYDR INDICATED ZERO QTY. CREW DECLARED AN EMERGENCY, ASKED FOR A RETURN TO AIRPORT. CREW REQUESTED A FUEL DUMP, THIS WAS APPROVED BY ATC. AFTER FUEL DUMPING WAS COMPLETED AC RETURNED AIRPORT FOR ARRIVALS ILS 29SDR CA060209001Hose · burst(CAN) LANDING THE CREW DEPLOYED THE THRUST REVERSERS AND GOT 6 LIGHTS FOLLOWED BY (HYD LOW LEVEL) AND (HYD LOW FLOW) LIGHTS. MAINTENANCE FOUND ONE LINE P/N CM3574D460B000S ON THE LT SIDE HAD BURST. REPLACED LINE WITH NEW. INSPECTED BOTH PRESSURE FILTERS AND NOSDR CA060202003Hydraulic Line · chafedHYDRAULIC LEAK DISCOVERED ON STOW LINE TO LT INBOARD THRUST REVERSER SYNC ACTUATOR ON NR 2 ENGINE, CAUSED FROM RUBBING ON AN ANGLE EDGE SUPPORT. LINE REMOVED AND FITTINGS CAPPED. A FLEET CAMPAIGN IS NOW IN PROGRESS TO CHECK ALL SYNC ACTUATOR LINES FOR DAMAGESDR 06FDEA0419Line · leakingHYD "B" LOW PRESS LT PUMP 1 CAME ON IN FLT PRESSURE STARTED DROPPING AND PUMP 2 LOW PRESSURE LT CAME FOLLOWED QRH TO LANDING SHGN. FOUND FLEX LINE CHAFED AGAINST HARD LINE IN "B" PUMP AREA CREATING SIGNIFICANT HYDRAULIC LEAK. NEEDS BOTH THE FLEX LINE AND SDR DL757060083Hose · rupturedATB ON DEPARTURE LOST ALL LEFT HYD SYS FLUID. RETURNED TO AIRPORT. REPLACED RUPTURED HOSE.SDR DL764060082Switch · inoperativeCENTER RIGHT HYD PUMP SWITCH INOP. REPLACED SWITCH PANEL.SDR 06FDEA0401Solenoid · unknownAFTER T/O GOT YELLOW HYD SYSTEM LO PRESS ECAM, QUANTITY WAS FINE, PRESSURE READ 50 PSI. REMOVED AND REPLACED YELLOW HYD SYSTEM SOLENOID, OPERATED DEPRESSURIZING VALVE. REF: 29-11-32-4. RAN ENGINE, SYSTEM OPS CHECKS GOOD. RUN PERFORMED.SDR 012206N401CS1Line · brokenON APPROACH INTO PHX ,THE CREW SELECTED FLAPS AND NOTICED A HYD FLOW LOW ANNUNCIATOR. THE APPROACH WAS ABORTED AND AN EMERGENCY WAS DECLARED. ATC CLEARED AIRCRAFT TO EXTENDED DOWNWIND APPROACH AND THE CREW EXTENDED THE LANDING GEAR WITH THE EMERGENCY BLOWDOWSDR CA060120003Connector · cracked(CAN) RT ENGINE HYDRAULIC SHUTOFF VALVE FOUND LEAKING. FAULT TRACED TO CRACKED CONNECTOR - IPC REF 29-11-81-01, ITEM 50. CONNECTOR REPLACED. (TC NR 20060120003)SDR R61A20060003Line · chafedDURING INBOUND FLIGHT 3345 PITTSBURG TO INDIANAPOLIS, HYDRAULIC SYSTEM 2 QUANTITY WENT TO 0. CREW DECLARED AN EMERGENCY LANDED WITHOUT INCIDENT.SDR DLM88060049Hydraulic Line · damagedAFTER TAKEOFF DURING CLEAN UP NOTICED RT HYD SYS PRESS AND QTY AT ZERO. FOUND PRESSURE LINE TO HYDRAULIC CONTROL MODULE IN SECTION 48 RT SIDE DAMAGE. REMOVED AND REPLACED SAME, RAN RT ENGINE, LEAK CHECK OK.SDR RAIA00601036Hydraulic System · failedFLT 8000 - STL- HYDRAULIC SYSTEM 2 FAILURE. MAINTENANCE PLACED BRAKE PRESSURE TRANSDUCER ON MEL. NO LEAKS NOTED.
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