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 2007UALA03804Hydraulic System · leakingEVIDENCE OF HYD LEAK AFT FUSELAGE GREEN SYSTEM. LOST 1 US GAL IN 1.5 HRS.SDR 2007UALA03797Unknown · malfunctionedMADE A GO-AROUND AND LANDED UNDER AMBER ALERT DUE TO FLAP INDICATION PROBLEMS ON APPROACH. 10-16-07 ACCOMPLISHED VISUAL CHK OF FLAPS AND SLATS. ACCOMPLISHED BITE OF BOTH FSEU, AND FSPM CARDS BOTH CHECKED OK. NO FAULTS, OK LIGHTS AND MESSAGES CLEARED. CYCSDR AALA20071766Hose · leakingDFW INFLIGHT T1866/19SEP - DURING CLIMB CREW RECEIVED LEFT HYDRAULIC QUANTITY INDICATION FOLLOWED BY LOSS OF LEFT HYDRAULIC SYSTEM PRESSURE. USED ALTERNATE FLAP EXTENSION AND GEAR PROCEDURES. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND LEFT HYDRAULICSDR NWAA073253201Hydraulic System · leakingLOST ALL GREEN HYDRAULIC PRESSURE AND FLUID AS GEAR RETRACTED AFTER TAKEOFF. CREW FOLLOWED COM PROCEDURES. AIRCRAFT TURNED BACK TO MSP. ALTERNATE EXTENSION OF GEAR AND LANDING ACCOMPLISHED UNEVENTFULLY. AIRCRAFT TOWED OFF OF RUNWAY TO GATE. REPLACED GREENSDR AALA20071756Valve · inoperativeAUA INFLIGHT T929/16SEP MIA TO GRU - CENTER HYDRAULIC SYSTEM QUANTITY DECREASING. DIVERTED TO AUA AND LANDED WITHOUT INCIDENT. REPLACED VALVE FOR CENTER HYDRAULIC SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR AALA20071749B-Nut · looseMSY INFLIGHT T9404/15SEP DFW TO FLL - LEFT HYDRAULIC QUANTITY LOSS IN FLIGHT. DIVERTED TO MSY AND LANDED WITHOUT INCIDENT. TIGHTENED LOOSE B NUT ON PYLON HYDRAULIC LINE. SERVICED LEFT HYDRAULIC SYSTEM. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. SYSTEM GRSDR DL76L071211Line · crackedRT HYD QTY ZERO AFTER TAKEOFF AT 5000 FT. FOUND HYD PRESS LINE AT RT A/C PUMP CRACKED AT B NUT. REPLACED HYD LINE. RESERVICED SYS AND OPERATED SYS. NO LEAKS RAN ENG AND OPS CHECK ENG PUMP OK.SDR COMA0760568Hydraulic Line · leakingFLIGHT 9456 - RECEIVED -HYD 2 LOW PRESS- CAUTION. HYD 2 QTY IS 0%. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED LEAKING HYDRAULIC LINE. NO FURTHER DEFECTS.SDR AWXA200701109Priority Valve · leakingCMH - EL - LOG 7781043 - DURING CRUISE, CREW RECEIVED A YELLOW SYSTEM LOW LEVEL MESSAGE. CREW DECLARED AN EMERGENCY. THE LANDING WAS UNEVENTFUL AND THE A/C TAXIED TO THE GATE. MX DISCOVERED THE YELLOW SYSTEM PRIORITY VALVE LEAKING. MX REPLACED THE YELLOW SSDR 2007FA0000805Line · leakingPILOT NOTED LOSE HYDRAULIC LINE. DECLARED EMERGENCY AND LANDED. NO NOSE WHEEL STEERING ON GROUND. INSPECTED ALL HYDRAULIC LINES AND FITTINGS. NOTED EDP LINE GOING TO PRESSURE MANIFOLD B NUT WAS ABLE TO GET HALF A TURN. SYSTEM SERVICED AND FUNCTIONAL CHECKED SSDR 2007UALA03652Hydraulic System · leakingLANDED UNDER AMBER ALERT DUE TO LOSS OF CENTER SYSTEM HYDRAULIC PRESSURE. 10-11-07 CREW SECURED CENTER SYSTEM AC PUMPS AT 0.70. CENTER HYDRAULIC SYSTEM SERVICED TO FULL.SDR DXTA200702456Line · rupturedON TAKEOFF AT GEAR RETRACTION, A POP WAS HEARD FOLLOWED BY (L) HYD, LOW CAS( L), HYD PUMP FAIL, PTU FAIL, AND RT HYD OVERTEMP. CHECKLIST FOLLOWED. GEAR BLOWN DOWN AND LANDED UNEVENTFULLY. ALL CAS OCCURED WITHIN 3 MINS. FOUND NOSE RETRACT LINE RUPTURED. REPLSDR QXEA200701411Pressure Switch · malfunctionedSEA - SHORTLY AFTER TAKEOFF 3 MASTER CAUTIONS APPEARED, RUD PRESS, RUD FULL PRESS, NR 2 RUD HYD CREW RUN APPROPRIATE CHECKLISTS. BLED RUDDER HYDRAULIC SYSTEM AND REPLACED RUD HYD PRESSURE SWITCHES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR CA070910003Line · ruptured(CAN) 10 MINUTES PRIOR TO LANDING, THE PORT AND STARBOARD HYDRAULIC PUMP LIGHTS ILLUMINATED WITH MAIN PRESSURE DEPLETING AND STOPPING AT ACCUMULATOR PRESSURE. THE CREW CARRIED OUT THE APPROPRIATE PROCEDURES AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUNSDR AALA20071696Hose · damagedJFK TEST FLIGHT T9640/06SEP - AFTER TAKEOFF CREW REPORTED MAIN LANDING GEAR UNSAFE LIGHT. FOLLOWED BY LEFT SYSTEM HYDRAULIC LOSS. LANDED JFK WITHOUT INCIDENT. AFTER LANDING RIGHT GEAR DOOR WAS EXTENDED AND WHEEL WELL WAS SATURATED WITH HYDRAULIC FLUID. FOSDR RAIA00709005Tube · leakingFLT 7897 - LIT - HYDRAULIC SYSTEM LOW QUANTITY MESSAGE IN FLIGHT AND READING -0- QUANTITY ON THE GROUND. MAINTENANCE REMOVED AND REPLACED A-HYDRAULIC TUBE AT THE WING STUB. LEAK CHECKED GOOD.SDR 224297Housing · crackedBODY IS CRACKED BELOW THREADS.SDR SIMA200725005Shuttle Valve · failedHYDRAULIC SYSTEM ONE FAILURE MESSAGE, CFR CALLED. RETURNED TO DFW. REMOVED AND REPLACED NUMBER FOUR BRAKE SHUTTLE VALVE AND TIGHTENED RESERVOIR REFILL CHECK VALVE AND LINE IAW EMB AMM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR NSVA20070220Unknown · unknownHYD LIGHTS ON IN FLIGHT. MAIN AND EMERGENCY ACCUM LOW, EMERGENCY LANDING DECLARED. INSPECTED FOR EXTERNAL LEAKS. NONE NOTED. FOUND MAIN SYSTEM OVERSERVICED, AND AUX SYSTEM REQUIRED SERVICING. RESERVICED, PERFORMED HYD SYSTEM CHECK, NO FAULTS FOUND.SDR CA070905010Pipe · cut(CAN) DURING ROUTINE A CHECK INSPECTION A CUT APPROXIMATELY 1 CM LONG WAS NOTICED ON THE ENGINE HYDRAULIC PUMP SUPPLY PIPE. THIS CUT WAS APPROXIMATELY .050 DEEP AND WAS THE RESULT OF CHAFFING WHEN THE COWLS WERE CLOSED. (TC NR 20070905010)SDR SWIA200718665Line · leakingFLT 3819 - LOST HYDRAULIC FLUID ON NR 2 SYSTEM. REPLACED THE NR 2 HYDRAULIC SYSTEM PRESSURE LINE AND THE CASE DRAIN LINE IN THE AFT EQUIPMENT BAY IAW CRJ MM 29-11-01.SDR DLM8K071173B-Nut · looseUPON CONFIGURING A/C FOR LANDING, LEFT HYD QUANTITY WENT TO 3 QUARTS AND REMAINED THERE. RAN QRH AND LANDED NORMALLY. DID NOT START APU AS PER QRH CHECKLIST. FOUND HYD LINE B NUT LOOSE ON LT ENG HYD CASE DRAIN FILTER OUTBOARD SIDE. RETORQUED SAME PER AMM. SDR DL757071166Hose · leakingON FINAL APPROACH AFTER SELECTING LANDING FLAPS LEFT HYD QTY STATUS MSG AND QTY LEVEL ZERO. FOUND OUTBOARD NOSE STEERING FLEX HYD LINE LEAKING IN AFT RT SIDE OF NOSE WHEEL WELL. INSTALLED TEMP HYD LINE TO FOM. REMOVED TEMP HYD LINE AND INSTALLED NEW FLEX HYSDR KNNA200700041Hose · leakingWHILE EN ROUTE TO ATLANTA HARTSFIELD AIRPORT (KATL) FROM TUNICA, MISSISSIPPI (KUTA) AS SKY KING FLT (SGB332) THE CREW NOTICED A SLOW LOSS OF SYSTEM “A” HYDRAULIC FLUID. AFTER DECLARING AN IN-FLIGHT EMERGENCY, AN UNEVENTFUL LANDING WAS MADE, THE CREW TAXI THE SDR DLM88071145B-Nut · looseHYD LOSS ON TOP OF DESCENT DURING FLAP EXTENSION. TIGHTENED B-NUT IN RT WHEEL WELL. SERVICED HYD FAN MOTORS A HYD PUMPS LK CKS GOOD. CYCLED FLIGHT CONTROLS CKS OK.SDR DJFA2007101Line · bentDURING PREFLIGHT, CREW NOTED CHAFFING ON THE HYDRAULIC BRAKE LINE IN THE LT MLG WHEEL WELL. MAINTENANCE DISCOVERED THE LINE BENT AND MIS-SHAPEN FROM AN UNKNOWN CAUSE. THE LINE APPEARED TO BE ROUTED CORRECTLY BUT AS A RESULT OF THE CONTORTION, THE LINE WAS CHSDR CA070828003Line · chafed(CAN) DURING A C-CHECK INSPECTION IN THE RT MAIN LANDING GEAR WHEEL WELL, THE HDRAULIC SUCTION TUBE ASSY(P/N 601R75239-463) OF HYDRAULIC PUMP 3B WAS FOUND WITH CHAFING DAMAGE. THIS TUBE WAS RUBBING AGAINST THE HYDRAULIC LINE(P/N 601R75239-273),WHICH IS THE UPLSDR CA070828002Line · chafed(CAN) DURING C-CHECK INSPECTION, CHAFING DAMAGE WAS NOTED ON THE HYDRAULIC PUMP 3B SUCTION LINE P/N 601R75239-463. THIS HYDRAULIC TUBE LINE WAS RUBBING AGAINST THE UPLOCK NR 3 HYDRAULIC TUBE LINE (P/N 601R75239-273) THAT FEEDS INTO THE EXTEND LINE FOR THE RHS SDR AALA20071601Hose · leakingMIA INFLIGHT T1818/22AUG - ON SHORT FINAL, LOST LEFT HYDRAULIC QUANTITY DOWN TO .22. LANDED MIA WITHOUT INCIDENT. REPLACED MAIN LANDING GEAR DOWN LOCK ACTUATOR HOSE. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR DXTA200702401Motor · inoperativeAFTER CLEARING RUNWAY ON TAXI IN, LO BRAKE PRESSURE LIGHT CAME ON, AND HAD NO BRAKES SO PULLED EMERGENCY BRAKE LEVER TO STOP THE A/C. FOUND BRAKE HYDRAULIC PUMP "ELECTRIC MOTOR" BAD. REPLACED WITH OVERHAULED UNIT IAW CE560XLS MM CH 32-42-00 AND ANTISKID BLEESDR 2007FA0000780Line · rupturedTHE NOSE WHEEL STEERING CENTERING FLEXIBLE HYDRAULIC HOSE RUPTURED WHERE THE HOSE BODY IS SWEDGED TO A 45 DEGREE FITTING WHICH ATTACHES TO A BULKHEAD FITTING IN THE NOSE WHEEL WELL. THIS CONDITION ALLOWED THE LOSS OF HYDRAULIC FLUID IN THE (A SYSTEM). AIRCRASDR DXTA200702397Hose · faultyUPON DEPARTURE, UPON GEAR RETRACTION, OBSERVED A LOUD SINGLE (THUD), FOLLOWED BY A HIGH PRESSURE (HISSING) SOUND, THEN A STRONG ODOR OF HYDRAULIC FLUID. WITHIN 2-5 SECONDS, MASTER CAUTION ILLUMINATED ALONG WITH THE FOLLOWING CAS MESSAGES: AMBER - HYD PTU. RESDR QXEA200701272Hose · leakingPDX - RECEIVED A HYDRAULIC LOW PRESSURE CAUTION FOR SYSTEM 2. PER THE CHECKLIST CLOSED THE RIGHT SHUTOFF VALVE AND CONTINUED TO PDX (35 MINUTES). MAINTENANCE FOUND THE PRESSURE OUTPUT LINE FOR THE DAMPER TO BE LEAKING. REPLACED LINE. OPERATIONAL CHECKS GOSDR ASMF200708003Shutoff Valve · leakingAIRCRAFT RETURN TO PLATFORM DURING TAXI, CREW SELECTED SLATS EXTEND AND THE HYDRAULIC QUANTITY LIGHT TURNED ON. MAINTENANCE DETECTED HYDRAULIC LEAK IN RT SYSTEM AND QUANTITY ZERO, SO THE SYSTEM WAS SERVICED AND HYDRAULIC PRESSURE WAS APPLIED AND THE LEAK WAS SDR SWAA074032Check Valve · faultyDURING FLIGHT WITH RT PACK RUNNING, BAD HYDRAULIC FLUID SMELL IN CABIN. REMOVED AND REPLACED HYDRAULIC CHECK VALVES ON RESERVOIR PRESSURIZATION MODULE PER MM.SDR 07FDEA02833Shutoff Valve · malfunctionedLOSS OF HYD SYS 3, COMPLETED QRH EMERGENCY PROCEDURES. RETURNED TO ANC. RESEALED PRIMARY TRIM CONTROL SOLENOID OPERATED SHUT-OFF VALVE. REF MM 27-43-41-4. OPS AND LK CK GOOD.SDR BB07063Module · leakingFLIGHT 707, MUC-PHL: FLIGHT DIVERTED TO LGW DUE TO CENTER HYDRAULIC SYSTEM QUANTITY DROPPING. MAINTENANCE REPLACED THE FLAP/SLAT HYDRAULIC SHUTOFF VALVE MODULE.SDR A6WA200740445O-Ring · failedDURING CLIMB AT 25,000 FT, LT ENGINE LOW OIL PRESSURE WARNING ILLUMINATED 23 PSI 2-3 SECONDS AS PER QRH REDUCED THRUST LEVER, OIL PRESSURE STAYED BETWEEN 30-40 PSI LOW OIL PRESSURE ILLUMINATED. REMOVED AND REPLACED ENGINE NR 1 HYD ENGINE DRIVEN PUMP O-RINGS ASDR 07FDEA02911B-Nut · leakingAFTER ENGINE START CREW REPORTED SMOKE IN THE COCKPIT COMING FROM THE CASPER VENTS. FOUND HYDRAULIC RETURN LINE B NUT LEAKING AT PYLON ON NR 1 ENGINE. SECURED AND OPERATED ENGINE WITH NO LEAKS REMOVED AND REPLACED NR 1 PACK COALESCER BAG PER MM 21-51-16-3. SDR 2007UALA03086O-Ring · failedFLIGHT DIVERTED DUE TO YELLOW HYDRAULIC SYSTEM INOPERATIVE MESSAGE. 09-07-07 REPLACED FAILED O-RINGS AT FLIGHT CONTROL PRESSURE SWITCH.SDR DJFA2007090Line · failedDURING PREFLIGHT, CREW NOTED HYDRAULIC FLUID AT THE LT TR AREA. MAINTENANCE FOUND THE HYDRAULIC LINE FOR THE TR ACTUATOR STOW PRESSURE TO HAVE BURST. THE LINE WAS REPLACEDSDR 07FDEA02805Line · rupturedPDIS: AT ROTATION LOSS OF HYD "SYS 1", 0.0. FOUND INLET HOSE ON LOWER HYDRAULIC PUMP RUPTURED. NEEDS NEW HOSE, PUMPS, FILTERS. FOUND HYD LINE NR 1 ENGINE DRIVEN PUMP LINE RUPTURED, REPLACED LINE,BOTH ENG DRIVEN PUMPS, ALL RELATED FILTERS AND LEAK CHECKED PESDR 2007FA0000715Accumulator · rupturedDURING TRAINING FLIGHT IN PREP FOR COMMERCIAL/AMEL, PILOT PERFORMED INTENTIONAL SHUTDOWN OF LT ENGINE (FEATHERED). WAS UNABLE TO RESTART WITH ACCUMULATOR AND BEGAN PROCEDURE TO RESTART WITHOUT ACCUMULATOR WHICH WAS UNSUCCESSFUL. PILOT RETURNED TO DEPARTURE ASDR 2007UALA03065Swivel · leakingRTFL DUE TO GREEN HYDRAULIC SYSTEM FAILURE. 09-07-07 BROKEN HYD SWIVEL FITTING ON GEAR. REPLACED BROKEN SWIVEL FITTING. RESET ALL SYSTEMS.SDR DLM88071041Line · leakingNUMBER 2 ENGINE HYDRAULIC PRESSURE LINE LEAK AND CAUSE TO LOSE MOST OF THE HYDRAULIC FLUID. REPLACED FLEX LINE FROM NR 2 ENGINE TO PYLON LEAK CHECKS NORMAL.SDR F3LA200700195Line · leakingFLIGHT CREW REPORTED GREEN HYD QTY LOW IN CRUISE. PERFORMED LANDING GRAVITY EXTENSION PER FOM VOL II. REPLACED NR 1 ENGINE T/R ISOLATION VALVE PRESSURE HYDRAULIC LINE. PERFORMED OPS AND LEAK CHECK IAW 8-37-51-PB-401. CHECKED GOOD. RESET FREE FALL EXTENSIOSDR DLM88071037Hose · leakingFLT 456 ATL-DCA DIVERTING TO IAD DUE TO RT SYSTEM HYD QTY LOSS AT CRUISE. RT SYSTEM QTY DECREASING AT CRUISE FL 330 AT APPROX 2 QUARTS QTY NOTICED RT SYSTEM PRESSURE DECREASING AS WELL. SHUTDOWN RT SYSTEM HYD PER NNC.13.12 AND REVIEWED PROCEDURES. DUE TO POSDR DJFA2007089Line · looseON LANDING CREW REPORTED HYD LOW LEVEL LIGHT WITH 0 QTY INDICATED. BRAKES FAILED AND EMERGENCY BRAKING WAS USED. MAINTENANCE FOUND A LOOSE HYDRAULIC LINE AT THE PYLON. THE LINE WAS TIGHTENEDSDR 2007UALA03031Line · failedC-HYD FAILURE AFTER FINAL APPROACH. 08-31-07 REPLACED INBOARD. NOSE STEERING HYDRAULIC LINE. PRESSURE CHECKED SYSTEM. CHECKED OK FOR SERVICE.SDR CA070822003Hose · damaged(CAN) AIRCRAFT WAS ONE HOUR OUT OF DEPARTURE PLACE AND ON ROUTE TO ENGLAND WHEN EICAS ILLUMINATED WITH THE FOLLOWING MESSAGES: C HYD SYS FLUID LOSS - C HYD SYS PRESS AIRCRAFT DIVERTED TO NEAREST AIRPORT WHERE IT WAS FOUND THAT THE LT MAIN LANDING GEAR TRUCK TI
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