JASC 2910
Service difficulty reports · 11,292
Reports filed under 2910 · Hydraulic System, Main, newest first.
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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"
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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 CA020726002Line · punctured(CAN) IN FLIGHT, LOST NUMBER ONE HYDRAULIC PRESSUE AND QUANTITY. FOUND NUMBER ONE PUMP PRESSURE LINE PUNCTURED. LINE REPLACED AND PUMP MPN 887055,OPERATION CHECKED NORMALSDR AWXA200200522Fitting · stuckPHX- AIR TURNBACK- FLT 0663- ON DEPARTURE OUT OF PHOENIX EN ROUTE TO SNA, THE REPORT BY THE PILOT STATED THAT A LOSS OF -B- SYSTEM HYDRAULICS HAD OCCURRED AND THAT THE AIRCRAFT WAS RETURNING TO PHOENIX. MAINTENANCE INSPECTED THE HYDRAULIC SYSTEM AND FOUND THESDR AALA20020875Relief Valve · malfunctionedDFW - FLT 389 - EN ROUTE SAT-DFW - DURING DESCENT, LEFT HYDRAULIC QUANTITY EICAS MESSAGE CAME ON. LEFT RESERVOIR LIGHT ALSO CAME WITH ZERO PRESSURE SHOWING. AIRCRAFT LANDED AT DFW WITHOUT INCIDENT. INSPECTION OF AIRCRAFT FOUND NO LEAKS. REPLACED LEFT RESERSDR CNQ2002F00000Line · chafedTHE ORANGE FRESH AIR DUCT IN THE TAILCONE IS CHAFING AGAINST THE SPEED BRAKE LINES. THIS RESULTED IN A FAILURE IN THE SPEED BRAKE LINE. THE CREW AND PASSENGERS OF THE AIRCRAFT REPORTED A HYD FLUID MIST COMING OUT OF THE WEMACS IN THE CABIN. REPLACED DUCT ASDR HEEA080063Tube · corrodedHYDRAULIC TUBE PITTED.SDR HEEA079892Module · malfunctionedOVERBOARD DRAIN WILL NOT PASS FLUID OR AIR. REPLACED HYDRAULIC MODULE.SDR GXP2002F00004Packing · leakingLOSING HYDRAULIC FLUID FROM SYSTEM 2. REMOVED AND REPLACED PACKING ON NR 2 ENGINE HYDRAULIC PUMP. SAFETIED ALL CONNECTIONS AND FILLED HYDRAULIC SYSTEM RESERVOIR NR 1 AND NR 2. STARTED NR 2 ENGINE AND LET STABILIZE. HYDRAULIC PRESSURE GOOD AND RESERVOIR NR SDR ASOA02327Hose · leakingDURING FLIGHT, AIRCRAFT LOST ALL HYDRAULIC FLUID IN THE NR 1 SYSTEM. AIRCRAFT DIVERTED AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE ENGINE DRIVEN PUMP PRESSURE LINE AND ALSO REMOVED AND REPLACED THE ENGINE DRIVEN HYDRAULIC PUMP ITSELF. OPERATIONASDR DLM88020647Hydraulic System · leakingCREW REPORTED ON FINAL APPROACH WITH PACKS IN FULL COLD GOT SMOKE IN THE CABIN. FOUND HYDRAULIC LEAK IN RIGHT WHEEL WELL. FLUID HAD TRANSITIONED TO APU INLET CONTAMINATING A/C SYSTEM. COMPLIED WITH OPERATIONS 5088 AND 5089 DUCT BURN OUT PROCEDURE. CLEANED SDR RAIA00206174Pump · overheated5493-STL- RIGHT HYDRAULIC HIGH TEMP CAPTION ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE RIGHT HYDRAULIC PUMP.SDR COMA0260361Hydraulic Line · leakingFLIGHT 6657 #1 HYDRAULIC SYSTEM INDICATING ZERO PRESSURE AND ZERO QUANTITY.REPLACED THE HYDRAULIC LINES AT THE LT ENGINE TO PYLON INTERFACE.SDR R7MR340235216Pressure Switch · intermittentPRESSURE SWITCH OPERATES INTERMITTENTLY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR SWAA021273Line · leakingDECLARED EMERGENCY, HYDRAULIC SYSTEM A FAILED DURING CLIMB-OUT. REMOVED AND REPLACED SYSTEM AILERON PCU LINE PER MM.SDR C2XA02TY096Manifold · overheatedTYS WHILE EN ROUTE FROM IAH TO TYS THE A/C WAS OUT APPROXIMATELY THIRTY MINUTES WHEN THE EICAS GAVE A NR 1 HYD, SYSTEM OVERHEAT MESSAGE FOLLOWED BY 0 PRESSURE INDICATION ON NR 1 SYSTEM. THE CREW FOLLOWED THE QRH PROCEDURE AND LANDED THE A/C AT TYS. MAINTENASDR 2002UALA00960Hydraulic Line · rupturedLEFT HYDRAULIC QUANTITY DROPPED TO ZERO. RIGHT MAIN GEAR DOWNLOCK HOSE RUPTURED. REPLACED HYDRAULIC HOSE.SDR 920WA0003Hydraulic SystemDuring descent into CUN master caution hydrualics - both A system low pressure lights on. "A" system pressure gauge almost 0. QRH accomplished. Declared emergency. - Inspected system, ground ran and performed test flight. No defects noted.SDR CA020612002Hose · chafed(CAN) HYDRAULIC FLUID LEAK, FROM BELLY THE MAIN LANDING GEAR RETRACTION LINE WAS RUBBING AGAINST A SCREW, THAT WAS HOLDING TWO CLAMPS AROUND TWO OTHER HYDRAULIC LINES UNDER THE RELAY BOX IN THE BELLY.SDR DLM88020613Hydraulic Line · rupturedRT ENG PRESSURE LINE IN AFT COMPARTMENT RUPTURED CAUSING RT SYS FAILURE AND LT GEAR DOOR DAMAGE ON LANDING. FOUND NR 2 ENG HIGH PRESSURE FLEX LINE BURST JUST BEFORE HIGH PRESSURE FILTER MODULE AND ADEL CLAMP BROKEN ON HYDRAULIC LINE WHERE IT MEETS THE FLEX LISDR HNAA020043Hydraulic Line · leakingCREW REPORTED LOSS OF HYDRAULIC FLUID FROM NR 2 HYD SYSTEM AND SUBSEQUENT ILLUMINATION OF ISO VALVE CAUTION LIGHT. CREW DECLARED AN EMERGENCY AND RETURNED TO MIA. FOUND 2 HYDRAULIC LINES AT NR 1 MLG FWD DOOR ACTUATOR WITH PIN HOLES. INSTALLED TEMPORARY FLEXSDR HNAA0200043Hydraulic Line · leakingCREW REPORTED LOSS OF HYDRAULIC FLUID FROM NR 2 HYD SYSTEM AND SUBSEQUENT ILLUMINATION OF ISO VALVE CAUTION LIGHT. CREW DECLARED AN EMERGENCY AND RETURNED TO MIA. FOUND 2 HYDRAULIC LINES (P/N'S 82970010-399 & 82970010-401) AT NR 1 MLG FWD DOOR ACTUATOR WITH SDR HEEA079749Ferrule · looseHYD LINE LEAKING AT FITTING FERRULE LOOSE ON LINE. SCRAPPED.SDR HEEA079748Line · leakingHOLE IN HYDRAULIC LINE. SCRAPPED.SDR MALA020309Switch · failedDURING FLIGHT 2824, HYDRAULIC SYSTEM WARNING INBOUND TO MSP. CREW PERFORMED EMERGENCY GEAR EXTENSION AND USED HYDRAULIC PUMP IN OVERRIDE TO GET RT MLG DOWN AND LOCKED. FROM LOG PAGE 1078212, HYDRAULIC CAUTION LIGHT ON INFLIGHT, PUMP INOP IN AUTO. EMERGENCY SDR IU62002F00011Housing · crackedHOUSING IS CRACKED AT THE RETRACT PORT. PROBABLY CAUSED BY OVER PRESSURIZATION AND WEAKENED METAL. REPLACE WITH UPGRADED HOUSING ASSEMBLY. (OCN: 168497 / MECH. CB4)SDR HNAA0200042Hydraulic System · malfunctionedDURING SINGLE ENGINE TAXI, CREW REPORTED LOST NR 1 STANDBY HYDRAULIC SYSTEM PRESSURE AND THE USE OF THE NORMAL BRAKE SYSTEM. CREW USED THE PARKING BRAKE TO STOP THE A/C. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY.SDR CA020725002Line · failed(CAN) LOSS OF SYS 1 HYDRAULIC FLUID DURING FLIGHT. PIN HOLE FOUND ON PUMP RETURN LINE. RETURN LINE REPLACEDSDR CA020604004Line · failed(CAN) HYDRAULIC NR 1 LOW PRESSURE AND QUANTITY "0". HYDRAULIC PUMP RAN DRY FOR 3 MIN. HYDRAULIC RETURN LINE FOR PRESSURE MANIFOLD FOUND LEAKING. NR 1 ENGINE HYDRAULIC PUMP CHANGED AS PER 29-11-01-400-801, HYDRAULIC LINE REPLACED PER STANDARD PRACTICES 20-22-0SDR DLM88020605Hydraulic Line · chafedDURING DESCENT THROUGH 15,000 FT RECEIVED LOW RT HYD PRESS AND QUANTITY MESSAGES, HAD NOT USED FLAPS OR SPOILERS AT THAT POINT. HYD PRESSURE WAS ALREADY 0 AND HYD QTY WAS 1 QUART. RT PUMP WAS UNFEATHERED FOR 2 MINUTES BEFORE COMING TO THAT POINT IN CKLIST. SDR HEEA079470Tube · chafedHYDRAULIC TUBE CHAFED ON BOTTOM SIDE. REPLACED WITH SERVICEABLE PART.SDR HEEA079440Pressure Switch · intermittentPRESSURE SWITCH INTERMITTENTLY CAUSES LIGHT TO COME ON WITH PRESSURE APPLIED. REPLACED WITH SERVICEABLE PART.SDR MALA020306O-Ring · failedDURING FLIGHT 3512, GREEN HYDRAULIC SYSTEM FAILURE INDICATION. EMERGENCY DECLARED. CREW MADE AN EMERGENCY LANDING. HYDRAULIC QTY ANNUNCIATOR ON GREEN SYSTEM INDICATED 1/4, QRH PERFORMED EMERGENCY LANDING. MAINTENANCE REMOVED AND REPLACED O-RING, SERVICED HSDR QXEA0200843Hydraulic System · lowSEA - DURING FLIGHT THE FLIGHT CONTROL HYDRAULIC QUANTITY DROPPED TO ZERO. LANDING AT SEA WAS UNEVENTFUL. MAINTENANCE INSPECTED THE AIRCRAFT AND SERVICED THE FLIGHT CONTROL HYDRAULIC SYSTEM TO FULL. THE SYSTEM WAS PRESSURIZED FOR 45 MINUTES WITH NO LEAKS OR MISDR 2002FA0000678Hydraulic Line · crackedLINE WAS CRACKED BEHIND AN ADEL CLAMP. MINOR PITTING AND CORROSION WAS EVIDENT ONCE CLAMP WAS REMOVED FROM LINE. LINE HAD BEEN PREVIOUSLY REPLACED ON 01/02. TWO OTHER HYDRAULIC LINES, P/N 6207023-154 AND 6207021-152 WERE REMOVED AND FOUND TO HAVE SIMILAR COSDR HNAA0200044O-Ring · deterioratedCREW REPORTED LOSS OF NR 1 HYDRAULIC SYSTEM FLUID. PRESSURE DID NOT GO TO ZERO. SYSTEM QUANTITY WAS AT ZERO FOR LESS THAN 10 MINUTES. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. FOUND LEAKING O-RING ON NR 1 HYD SYSTEM PRESSURE MANIFOLD. REPLACSDR CA020530003Check Valve · leaking(CAN) ECAM MESSAGE "Y SYST LO PR" AND 10 MIN LATER "LO LVL" ECAM ACTIONS COMPLETED. YELLOW HYDRAULIC SYSTEM PTU MANIFOLD CHECK VALVE FOUND LEAKING AND SAME REPLACED AS PER AMM. 29-13-15.SDR CA020530007Seal · failed(CAN) GREEN HYDRAULIC FLUID LEVEL FELL IN YELLOW RANGE. AIRCRAFT DIVERTED TO YYZ RESULTING IN AN OVERWEIGHT LANDING. SEAL FOUND LEAKING ON LANDING GEAR DOOR MANIFOLD ASSY. SEAL REPLACED AND SYSTEM LEAK CHECKED SERVICEABLE. OVERWEIGHT LANDING CHECK COMPLETED, SDR 0201715524Hydraulic Line · leakingLEFT HYDRAULIC SYSTEM FAILURE AT 80 KNOTS DURING LANDING ROLLOUT. LOSS OF STEERING RESULTED IN AIRCRAFT BEING TOWED FROM RUNWAY TO GATE. MAINTENANCE DISCOVERED HYDRAULIC LINE TO LEFT DOWNLOCK ACTUATOR LEAKING. REPLACED THE HYDRAULIC LINE PER MM 32-32-581. LSDR AALA20020764Hydraulic Line · broken(LINE) EN ROUTE, MIA-BOG LOSS OF LEFT SYSTEM HYDRAULIC FLUID INDICATION. DECLARED EMERGENCY AND LANDED AT MBJ WITHOUT INCIDENT. CHECKED AND FOUND BROKEN HYDRAULIC LINE ON NOSE GEAR DOOR ACTUATOR. REPLACED HYDRAULIC LINE. REPLENISHED SYSTEM. SYSTEM GROUND SDR JEM2002F00001Line · chafedTHIS LINE ASSEMBLY WAS CHAFING AGAINST AN ENGINE POWER CONTROL CABLE LOCATED BEHIND THE REMOVEABLE LEFT HAND INBOARD LEADING EDGE PANEL. VIBRATION CAUSED THE OUTER SHEATH OF THE CONTROL CABLE TO CHAFE DEEP SERRATIONS INTO THIS LANDING GEAR HYDRAULIC LINE. ITSDR UG82002F00003B-Nut · looseTOTAL LOSS OF (A) HYDRAULIC SYSTEM FLUID. B-NUT ON LINE ASSEMBLY LOOSENED AND BACKED OFF DUE TO INCORPORATION OF SB. FURTHER INSTALLATIONS OF THIS BULLETIN HAVE BEEN TEMPORARILY TERMINATED BY MFG. SECURED B-NUT, SERVICED (A) HYDRAULIC SYSTEM. SERVICED EMESDR IXXA0200026OFlex Line · rupturedENROUTE FROM PDX TO TOL, DURING CLIMB OUT THE FLIGHT CREW NOTICED THE MAIN HYDRAULIC QUANTITY SYSTEM DECLINING. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND RETURN TO PDX FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED AND LOCATED A RUPTURED HYDRAULIC LINESDR ARWA20020506Hydraulic Line · leakingAT 2225Z IN CLIMBING, HYDRAULIC QUANTITY DROPPED TO STAND PIPE PRESSURE DROPPED TO ZERO RETURNED TO KMIA. PERFORMED LOSS HYDRAULIC PRESSURE EMERGENCY CHECKLIST ON HYDRAULIC FLUID; PERFORMED EMERGENCY CHECKLIST ON HYDRAULIC CHECK, NO FURTHER LOSS OF FLUID. USSDR AWXA200200439O-Ring · deterioratedLAS - DIVERSION - FLT 0470 - EN ROUTE FROM PHX TO BUR ECAM INDICATED YELLOW HYDRAULIC SYSTEM LOW QUANTITY, AIRCRAFT DIVERTED TO LAS. MAINTENANCE FOUND HYDRAULIC LEAK AT QUICK DISCONNECT (3701GM) ON YELLOW HYDRAULIC SYSTEM MAIN POWER MODULE, REMOVED AND REPLACESDR ASM2002F00005Fuse · leakingAIRCRAFT RETURN TO PLATFORM AS A CONSEQUENCE OF HYDRAULIC LEAK AND LOW PRESSURE INDICATION. DURING REVISION WAS DETECTED A CRACK ON THE LEFT FUSE ASSEMBLY HYDRAULIC QUANTITY MEASURE. IT WAS CHANGED IAW MM, TEST OK.SDR UPS02538278Hydraulic Line · rupturedINSPECTION TYPE:N/A ATB- LOSS OF LEFT SYSTEM HYD PRESSURE. FOUND LT MAIN GEAR DOWNLOCK PRESS LINE LEAKING. REMOVED AND REPLACED DOWNLOCK ACT RETRACT PRESS LINE. LEAKS CHECK GOOD PER MM 32-32-02.SDR AUS20020875Hose · failed(AUS) HYDRAULIC HOSE FAILED IN AN AREA APPROXIMATELY 200MM (8IN) ALONGTHE LENGTH ALONG THE HOSE. LOSS OF HYDRAULIC FLUID. SUSPECT HOSEHAD SUFFERED SOME DISTRESS DURING ITS LIFE.SDR CA020522004Hydraulic Line · split(CAN) AFTER LANDING PILOT WAS COMPLETING POST FLIGHT/PRE FLIGHT WALK AROUND INSPECTION AND FOUND THE NR 3 BRAKE LINE LEAKING HYDRAULIC FLUID. MAINTENANCE DISPATCHED WITH FLEXIBLE BRAKE LINE, HYDRAULIC FLUID AND TOOLING REQUIRED. NR 3 BRAKE FLEXIBLE LINE REPLACSDR AALA20020706Hydraulic Line · leaking(HYDRAULIC LINE) ENROUTE, LEFT HAND HYDRAULIC SYSTEM LOSS OF ALL FLUID IN FLIGHT. RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. REPLACED HYDRAULIC LINE TO DOWNLOCK ACTUATOR, ENGINE DRIVEN PUMP AND ENGINE DRIVEN PUMP FILTERS. SYSTEM GROUND CHECKED NORMAL SDR CA020521009Line · cracked(CAN) PILOT FOUND DURING WALK AROUND BEFORE DEPARTURE FROM YAD A SMALL QUANTITY OF HYD. FLUID UNDER NR 3 BRAKE ASSY. MAINT ADVISED AND REQUEST THE PILOT TO APPLIED THE PARKING BRAKE TO CONFIRM THE LEAK. PILOT CONFIRM THAT LEAK IS FROM HYD. FLEX LINE CONNECTED SDR HEEA078991Tube · corrodedMLG TUBE PITTING UNDER SLEEVES AND FLARE IS DAMAGED.
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