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 PAI2004F00001Line · chafedFOUND RT GROUND SPOILER HYD LINE CHAFED THROUGH BY AILERON CABLE, AFTER SEEING EVIDENCE OF HYDRAULIC FLUID DRIPPING OFF OF WING SKID. IT IS IN THE WING T/E AREA AT STA WS85. INSIDE THE FLAP ACTUATOR/TRACK MOUNT. IMPOSSIBLE TO SEE WITHOUT AID OF MIRROR AND MOSDR SWAA041067Line · looseAIR TURNBACK, A-SYSTEM HYDRAULIC QUANTITY WENT TO ZERO. RETORQUED A-SYSTEM HYDRAULIC RESERVOIR RETURN LINE PER MM.SDR P5CA0401070Tube · leakingSTATUS MESSAGE, "HYD PRESSURE ENG 2." INSTALLED FLEX LINE IN PLACE OF RIGID LINE AND SECURED, OPS AND LEAK CHECK OK IAW MM 29-00-00 AND SERVICED HYD LEVEL TO FULL.SDR 2004UALA00346Hydraulic System · leakingRETURNED TO THE FIELD DUE TO HYDRAULIC FLUID LOSS AND UNSUITABLE WEATHER. ACTUAL FLUID LOSS UNDETERMINED, NO SIGNIFICANT LEAKS FOUND AND NO FURTHER LOSS OF FLUID.SDR ASMF200404009Line · leakingDURING TRANSIT CHECK HYDRAULIC FLUID LEAK WAS DETECTED IN A LINE LOCATED AT THE UPPER SECTION OF THE AFT CARGO DOOR. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE THE LEAK WAS DETECTED IN THE RIGHT HYDRAULIC PUMP RETURN LINE, IT WAS ADJUSTED INSDR 2004UALA00325Pressure Switch · malfunctionedGREEN HYDRAULIC SYSTEM RSVR LO LVL ECAM DISPLAYED. GREEN HYDRAULIC SYSTEM LOW LEVEL SWITCH FAILED, REPLACED GREEN HYDRAULIC SYSTEM LOW LEVEL SWITCH, OPERATIONS CHECK NORMAL.SDR DL76S040323O-Ring · damagedLOSS OF CENTER HYD FLUID. FOUND O-RING ON RUDDER PCA DAMAGED. REPLACED O-RING.SDR CA040407009Housing · cracked(CAN) DURING TESTING THE ACTUATOR SHOWED HIGH INTERNAL LEAKAGE. AFTER INVESTIGATION IT WAS DISCOVERED THAT THE HOUSING WAS CRACKED INTERNALLY. THE CRACK IS IN THE SERVO VALVE AXIS OF THE HOUSING AND APPEARS TO ORIGINATE FROM A DRILLED PASSAGE. THIS ASSEMBLYSDR BAQA093191Module · leakingUNIT LEAKING HYRO FLUID. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 04/23/2004SDR WRLA200415Line · brokenACCORDING TO THE CAPTAIN'S REPORT: AFTER THE TAKEOFF FROM SBEG, DURING CLIMB AND AFTER SLAT RETRACTION,THE (HYD 3 FAIL)ALERT WAS ANNUNCIATED, AND COMPLETE LOSS OF SYSTEM 3 HYD. FLUID WAS NOTED,NO ACTION WAS POSSIBLE,PROCEEDED TO KFLL AND FOLLOWED CKECKLIST FORSDR RAIA00404005Line · crackedLOST HYDRAULIC PRESSURE AFTER TAKEOFF. MAINTENANCE FOUND BRAKE IN HYDRAULIC TUBE AND SWAGED TUBE.SDR UIA9312Line · brokenIN FLIGHT (NR 2 HYD PUMP CAUTION LIGHT COME ON AND ROLL SPLR OB HYD CAUTION LIGHT COME ON AND NR 2 PRESS IND. (0) AND QTY IND (0) AFTER A/C LANDED CHECK NR 2 HYD SYS FOUND RT OB SPLR PRESSURE TUBE BROKEN. IAW AMM 20-50-52 REPLACED FLEXIBLE HOSE FOR TEMPOSDR HEEA094230Guide · defectiveIN CRUISE FLIGHT, HYDRAULIC BLOCK LIGHT CAME ON, FOLLOWED BY NR 1 HYDRAULIC LIGHT ILLUMINATION. RETURNED TO BASE. FOUND DEFECTIVE SWITCH ON GUIDE ASSEMBLY. REPLACED HYDRAULIC GUIDE ASSEMBLY.SDR SIMA200409903Line · leakingDURING CLIMB-OUT, CREW HEARD A POP IN THE NOSE GEAR AREA FOLLOWED BY MAIN ACCUMULATOR DROPPING TO ZERO. PERFORMED EMERGENCY EXTENSION OF LANDING EAR. LANDED WITH ZERO FLAPS. FOUND NLG ACTUATOR LINE BROKEN. REPLACED ACTUATOR LINE IAW AMM 29-11. AIRCRAFT RETSDR AWXA200400344Hydraulic Line · rupturedSAT - AIR TURNBACK - FLT 0679 - ON CLIMBOUT OF SAT EN ROUTE FOR PHX LOST A-HYDRAULIC SYSTEM, FOLLOWED QRH AND TURNED BACK TO SAT. MAINTENANCE REMOVED AND REPLACED RUPTURED HYDRAULIC PRESSURE LINE BETWEEN A-SYSTEM MODULE AND LT MAIN LANDING GEAR ACTUATOR. REMSDR CA040403001Hydraulic Line · punctured(CAN) ON TAXI OFF THE RUNWAY HYD 2 LOW PRESSURE CAUTION POSTED ON EICAS. PRESSURE SHOWED BETWEEN 100-300 PSI. MAINTENANCE FOUND THE RT IB GROUND SPOILER EXTENSION FLEX LINE P/N AE2464218E0164 IN THE GEAR WELL RUPTURED. THE LINE WAS FOUND TO BE CHAFFING ON TSDR AUS20040242Hose · failed(AUS) RT MAIN LANDING GEAR RADIUS ROD UP HYDRAULIC HOSE FAILED. LOSS OF HYDRAULIC FLUID.SDR COMA0460237Hydraulic Line · leakingFLIGHT 5291 NR 1 HYDRAULIC SYSTEM LOW PRESSURE WARNING, RESERVOIR INDICATED EMPTY. REPLACED HYDRAULIC SUCTION LINE IN AFT EQUIP BAY.SDR C8GA20040003B-Nut · looseFLT 1724 FROM KROC TO KPHL. ON APPROACH TO KPHL OBSERVED A COMPLETE LOSS OF B-SYSTEM HYDRAULIC FLUID. ACCOMPLISHED ABNORMAL CCIA AIRCRAFT OPERATIONS MANUAL A-05-3, ADVISED ATC AND DECLARED EMERGENCY AS A PRECAUTIONARY. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFSDR DXTA200400283Line · leakingUPON GEAR RETRACTION SEVERAL LOUD BANGS WERE HEARD AND FELT, GEAR LIGHTS EXTINGUISHED, HYDRAULIC PRESSURE LIGHT STARTED FLASHING. PULLED C/B AND ANOTHER BANG HEARD AND FELT ALONG WITH RED GEAR UNSAFE LIGHT, RESET C/B AND GEAR EXTENDED NORMALLY. - PERFORMED 15 SDR CLS2004F00000Hose · leakingDURING 100 HOUR, INSPECTION FOUND LT MAIN LANDING GEAR HYDRAULIC ACTUATOR HOSE LEAKING HOSE WAS HARD AND NOT FLEXIBLE HOSE TAG SHOWS MFG DATE 3Q77 AND APPEARS TO BE ORIGNAL HOSE INSTALLED. AC MFG DATE 1978 WITH 7221.9 HOURS TT. RECOMMEND TO REPLACE FLEX HOSESDR S642004F00000Powerpack · inoperativeSMOKING AT LT WING FAIRING EDGES. FAIRING PULLED, FOUND HYD PKG SOFT START RESISTOR SMOKED AS WELL AS LARGE BLACK AREA ON FUSELAGE BLACK. INSIDE OF WING FAIRING BURNED AND BUBBLED ON OUTSIDE. INSTALLED NEW RESISTOR AND NEW HYD UNIT SELECT RELAY. PULLED NR SDR CALA0400281Line · leakingTHE RIGHT HYDRAULIC SYSTEM QUANTITY AND PRESSURE DROPPED WHILE EN ROUTE FROM SFO TO IAH. THE LOSS WAS ACCOMPANIED BY HYDRAULIC FLUID FUMES AND HAZE IN THE CABIN WHEN THE HYDRAULIC FLUID WAS INJESTED INTO THE PACK SYSTEM. THE AIRCRAFT LANDED AT IAH AND PASSENSDR C2XA04BT039Control Unit · leakingCREW REPORTED NR 1 HYDRAULIC QUANTITY LOW LEVEL INFLIGHT. AIRCRAFT DECLARED AN EMERGENCY AND DIVERTED TO EWR. EWR MAINTENANCE REMOVED AND REPLACED NR 1 ICU IAW EMB135 AMM 78-33-01. SERVICED HYDRAULICS, OPS CHECKED AND LEAK CHECKED GOOD. PERFORMED OPERATIONSDR SWAA040870Hose · leakingDIVERSION, HYD B-SYSTEM LOW PRESSURE LIGHT ILLUMINATED, QUANTITY ALMOST ZERO. REMOVED AND REPLACED HYD-B SYSTEM PRESSURE HOSE PER MM.SDR 0400483230Priority Valve · leakingJUST PRIOR TO APPROACH, RECEIVED ECAM MESSAGE 'HYD Y RSVR LO LVL'. FOLLOWED COM AND LANDED UNEVENTFULLY. ECAM INDICATED NEAR TOTAL LOSS OF FLUID. FOUND PRIORITY VALVE AT PTU MANIFOLD LEAKING. REPLACED PRIORITY VALVE AND SERVICED YELLOW HYDRAULIC RESERVOIR. LEASDR CA040329005Tube · leaking(CAN) HYDRAULIC SYSTEM FAILURE (NR 1 ISO VALVE AND ROLL SPOILER INBOARD HYDRAULIC CAUTION LIGHTS) HYDRAULIC TUBE FOR LT INBOARD FLIGHT SPOILER ACTUATOR (UNLOAD) FOUND WITH PINHOLES. TUBE REPLACED, FUNCTION AND LEAK CHECKS COMPLETED. NR 1 HYDRAULIC EDP WAS NOSDR MASA200400156Line · crackedASH NR 7062. EGE-DEN. A/C LOST ALL HYD FLUID ON THE NR 2 HYD SYSTEM AND LANDED IN DEN. MX FOUND THE NR 2 STANDBY LINE OFF OF THE NR 2 PUMP CRACKED. MX REPLACED THE LINE, PUMP, AND INSPECTED THE EDP, AND FILTERS FOR CONTAMINATION.SDR CA040331002Line · leaking(CAN) DURING WALK AROUND BEFORE DEPARTURE PILOT NOTED SUBSTANTIAL HYDRAULIC LEAK FROM NR 2 NACELLE. MAINTENANCE FOUND NR 1 SYSTEM LIFT DUMP PRESSURE LINE WITH A PIN HOLE LEAK. LINE REPLACED LEAK AND FUNCTION CHECK CARRIED OUT, AND AIRCRAFT RETURNEDTO SERVICE.SDR AUS20040322Ptu · seized(AUS) HYDRAULIC POWER TRANSFER UNIT (PTU) SEIZED.SDR HNAA0400025Line · leakingNR 2 HYD. QTY, LOST QTY IN TAKEOFF AND LANDING PHASE OF FLT. HYD PRESS STAYED AT 3000 PSI AT ALL TIMES. FOUND HYD LINE TO NLG DOOR SEQUENCE VALVE SOLENOID LEAKING, INSTALLED TFL AT THIS TIME.SDR AWXA200400294Hydraulic Line · chafedLAS - AIR TURNBACK - FLT 0116 - ON CLIMBOUT OF LAS EN ROUTE FOR LAX B-SYSTEM HYDRAULICS FAILED, TURNED BACK TO LAS AND LANDED WITHOUT FURTHER DIFFICULTY. MAINTENANCE FOUND HYDRAULIC LINE LEAKING BETWEEN B-SYSTEM PRESSURE MODULE AND A/C DRIVEN PUMP. REMOVED ASDR AMTA200400318Line · leakingLEFT HYDRAULIC QUANTITY EICAS MESSAGE FOLLOWED BY 'RSVR' ON OVERHEAD PANEL. REPLACED LEFT ENGINE HYD PUMP CASE DRAIN LINE WITH SERVICEABLE PREFABRICATED HIGH PRESSURE HOSE PER GMM CH 3, P46. NO LEAKS NOTED. (M)SDR AALA20040363Hose · leakingEN ROUTE DFW TOTAL LOSS OF HYDRAULIC QUANTITY ON LEFT HAND SYSTEM. RETURNED MCO AND LANDED WITHOUT INCIDENT. REPLACED PRESSURE LINE TO RETRACT SIDE OF NOSE GEAR DOOR CYLINDER WITH 3000 PSI FLEX LINE DUE TO RUPTURE. SERVICED HYDRAULIC QUANTITY TO FULL. SYSTSDR C8GA20040002Line · rupturedFLT 202 FROM MDSD TO KMIA. ENROUTE TO KMIA OBSERVED A COMPLETE LOSS OF "B" SYSTEM HYDRAULIC FLUID FOLLOWED BY BOTH "B" SYSTEM LOW-PRESSURE LIGHTS ILLUMINATING. BRAKE PRESSURE BEGAN A SLOW DROP TO 1400 POUNDS. A PHONE PATCH WAS MADE TO COMPANY, ADVISED ATC IN MSDR P5CA0401059Hose · looseLOSS OF HYD FLUID, SYSTEM NR 1 ENG PUMP SELECTED OFF. SYSTEM NR 1 PRESS NORMAL TO COMPLETION OF FLIGHT. FOUND PRESS HOSE AT EDP LOOSE. TIGHTENED HOSE/LINE PER MM 29-11-08. NO LEAKS NOTED PER MM 71-00-00.SDR USAASB04030Tube · leakingAFTER TAKEOFF FROM CLT, THE RIGHT MLG WOULD NOT RETRACT. THE RT ENGINE DRIVEN HYDRAULIC PUMP LOW PRESURE LIGHT WAS ALSO ILLUMINATED. CREW ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES, SELECTED THE HYDRAULIC PUMP TO OFF AND DECLARED AN EMERGENCY. FLIGHT RETURNSDR 2004F00170Line · leakingDURING CRUISE FROM GSO-ACY, EXPERIENCED A LOSS OF THE A-SYSTEM HYDRAULICS. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED AT ACY WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC FEED LINE. CONDUCTED 'A' SYSTEM TROUBLESHOOTING PROCEDURES FOR PUMP SDR DL75K040236Line · rupturedON TOUCHDOWN GOT LEFT HYDRAULIC SYSTEM FAILURE, QUANTITY IS AT .07RF. THE AIRCRAFT WAS TOWED BACK TO THE GATE, INSPECTED THE LEFT LANDING GEAR AND FOUND THE DOWNLOCK ACTUATOR FWD HYDRAULIC LINE LEAKING. THE LINE WAS REPLACED AND THE HYDRAULIC SYSTEM WAS REFISDR COMA0460195Hydraulic Line · leakingFLIGHT 5588 HYDRAULIC SYSTEM 2 LOW PRESSURE CAUTION. REPLACED DEFECTIVE HYDRAULIC LINE IN LEFT WHEEL WELL.SDR USAASB04027Valve · crackedCREW REPORTED LOSING SYSTEM A-HYDRAULICS ON TAKEOFF AS LOW PRESSURE LIGHT ILLUMINATED AND QUANTITY INDICATED ZERO. FLT LEVELED OFF AT 5,000 FEET TO COMPLETE QUICK REFERENCE HANDBOOK PROCEDURES, THEN THE FLIGHT RETURNED TO FIELD AT BNA. UPON LANDING, THE LANDSDR DLM88040227Line · unserviceableON CLIMBOUT, RIGHT HYDRAULIC QTY WENT TO -0- FOLLOWED BY LOSS OF HYDRAULIC PRESSURE. REPLACED RIGHT ENGINE PRESSURE LINE.SDR AUS20040183Pipe · cracked(AUS) HYDRAULIC PIPE CRACKED AND LEAKING. LOSS OF HYDRAULIC FLUID. PIPE IS LOCATED IN RT WING LEADING EDGE. INVESTIGATION FOUND TOOLING MARKS ON THE PIPE IN THE AREA OF THE PIPE BEND.SDR EKL2004F00000Hose · leakingAFTER START, WHILE AT FLIGHT IDLE, PRIOR TO TAKE OFF, THE PILOT RECEIVED THE HYD LIGHT ON THE WARNING PANEL. PILOT SHUT DOWN AC WITHOUT INCIDENT. UPON FURTHER INVESTIGATION, IT WAS DETERMINED THAT A SMALL PIN HOLE SIZE LEAK HAD DEVELOPED IN THE PRESSURE LINESDR HNAA0400021Line · leakingAFTER TAKEOFF NR 2 HYD IOS C/L ILLUMINATED AND NR 2 HYD PRESSURE AND QTY DROPPED TO ZERO, FOLLOWED BY ILLUMINATION OF NR 2 ENG HYD PUMP, RUDDER PRESS, RUDDER FULL PRESS & OUTBD ROLL SPLR. C/L ILLUMINATED. LOST PRESSURE AT 0958 ENGINE SHUTDOWN AT 1040. INSTALSDR CA040311004Line · cracked(CAN) ON DEPARTURE LT HYD PRESSURE LIGHT ILLUMINATED IN FLIGHT WITH HYD PRESS. READING ZERO. AIRCRAFT LANDED. MAINTENANCE FOUND LT EDP INOPERATIVE. LT EDP SWAPPED WITH RT EDP AND AIRCRAFT DISPATCHED IAW MEL 29-5.EDP P/N AS666411-L-5666 S/N MX134145-4M. THE SDR 2004F00239Line · leakingWHILE IN CRUISE FLIGHT FROM SUX SYSTEM 'A' HYD SHOWED A SLOW FLUID LOSS. ACCOMPLISHED ABNORMAL PROCEDURES THEN DIVERTED TO ATL AND LANDED WITHOUT INCIDENT. FLUID QTY AND LANDING 2 GALLONS. FOND NR 1 ENGINE CASE DRAIN LINE IN SECITON 48 LEAKING. INSTALLED TSDR AUS20040157O-Ring · failed(AUS) HYDRAULIC SYSTEM A PRESSURE MODULE SUPPLY LINE O-RING SEAL FAILED. LOSS OF HYDRAULIC FLUID.SDR CA040304011Maxaret · broken(CAN) AFTER A FLIGHT THE AIRCRAFT WAS BEING PULLED INTO THE HANGAR. AN AME WAS WALKING PAST THE AIRCRAFT AND NOTICED THE LT ANTI-SKID COVER WAS MISSING THE THREE RIVETS ON THE CASE. ON REMOVAL OF THE COVER THE COMPOSITE BLOCKS DESIGNED TO HOLD THE DRIVE PORTSDR CA040304001Pilot Valve · seized(CAN) IN ORDER TO COMPLY WITH AIRWORHTINESS DIRECTIVE CF-2003-002R1, THE FLIGHT CONTROL RODS WERE DISCONNECTED AND THE PILOT VALVE WAS FOUND TO BE SEIZED ON THE FORE AND AFT SERVO.
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