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 JJBA20130510008Line · leakingDURING GEAR RETRACTION, THE CREW REPORTED THE NOSE GEAR DOOR CYCLED AND GEAR RETRACTION WAS SLOW TO COME UP. MX CREW REPLACED A HYD FLUID LINE IN THE NOSE WHEEL WELL.SDR BSYR2012047Unknown · malfunctionedAPPROXIMATELY 60 MILES OUT FROM SUS, PILOT NOTICED COMPLETE LOSS OF HYDRAULIC PRESSURE. PILOT NOTIFIED ATC OF SITUATION, PILOT COMPLETED EMERGENCY GEAR EXTENSION AND LANDED SAFELY WITHOUT INCIDENT. MAINTENANCE HAS BEEN NOTIFIED AND INSPECTING AIRCRAFT.SDR CA130606001Line · chafed(CAN) HYDRAULIC LINE SUPPORT ASSY AT LEFT HAND WING STATION 27.1 CHAFFED INTO THE TUBE ASSEMBLY CAUSING A HYDRAULIC LEAK. LINE MANUFACTURED AS PER MAINTENANCE TABLE 201 AND REPLACED AND SUPPORT ASSEMBLY CLEANED. AIRCRAFT RETURNED TO SERVICE. (TC# 20130606001)SDR UALA2013051303302Valve · leakingLONG TERM HYDRAULIC LEAK FROM DRAIN HOLES AFT OF FWD CARGO DOOR ACTUATOR. INSTALLED CARGO BAY DOOR SELECTOR VALVE ON FWD DOOR. LEAK CHECKED, OKAY.SDR FDEA201305090943Flex Line · leakingDURING ACFT BLOCK IN, FOUND NR 4 BRAKE SMOKING AND LEAKING HYD ON THE GROUND. FURTHER TROUBLESHOOTING FOUND NR 4 BRAKE FLEX LINE LEAKING. NO RESTRICTION. INSTALLED NEW BRAKE LINE AS REQUIRED. LEAK CHECKED GOOD. IAW MM 20-10-10-4.SDR 2013FA0000273Packing · leakingDURING LOW LEVEL TRACK, LEVEL FLIGHT, NOSE GEAR UNSAFE LIGHT CAME ON FOR ABOUT 2 MINUTES. DURING RTB AT ALTITUDE OF 12K, LIGHT CAME ON AGAIN AND HYDRAULIC PRESSURE DROPPED. WENT TO 0 PSI IN ABOUT A MINUTE. PILOT EXECUTED EMERGENCY PROCEDURES FOR GEAR EXTENSSDR CA130521004Hose · failed(CAN) CREW REPORTED COMPLETE LOSS OF FLUID IN HYDRAULIC SYS NR 3 DURING DESCENT. THEY PERFORMED QRH ABNORMAL 10-8 LANDING FLAPS 20, MANUAL GEAR EXTENSION, NOSE WHEEL STEERING OFF, ACFT LANDED WITHOUT INCIDENT.SDR UALA2013051003284Hydraulic Line · damagedHYD QTY DISPLAY IS BLANK. POS 2 (01=L,02=R,03=C). FRM CODE 29-33-04-XX. CREW COMMENTS: RIGHT QTY IND .49RF ALSO SATUS MSG R HYD SYS MAINT COMPLIED WQRH. FOUND HYDRAULIC TUBE AT RT ENGINE PYLON DAMAGED, REF IPC 29-11-00-002A INDEX 386. REPLACED HYD TUBE ANDSDR SWIA201333432Hydraulic Line · chafedCOMPLETE LOSS OF FLUID IN HYDRAULIC SYSTEM 3. LANDING WAS NORMAL. (FLT 6225) PERFORMED OPS CHECK OF NORMAL MLG EXTENSION AND RETRACTION. GEAR SWINGS GOOD. SERVICED 3 HYD SYSTEM. FOUND CHAFED 3 SYSTEM HYD LINE, REPLACED IAW AMM.SDR JIKA2013050801Hydraulic Line · crackedTHE PILOT REPORTED THAT ON CLIMBOUT FROM KMIA BOTH HYDRAULIC FAIL ANNUNCIATOR’S ILLUMINATED. THE PILOT IMMEDIATELY TRIED TO LOWER THE LANDING GEAR WITHOUT SUCCESS. THE PILOT DIVERTED BACK TO KMIA, DECLARED AN EMERGENCY, PUMPED THE LANDING GEAR DOWN AND LANDSDR UALA2013050803232Hydraulic Line · looseTAIL SKID DRIPPING HYD FLUID. LARGE PATCH OF FLUID UNDER SKID. CLEANED AND CHECKED ALL HYD LINE IN FWD STABILIZER COMPARTMENT, FOUND TWO LINES LOOSE, TIGHTENED BOTH LINES ABOUT 1-2 TURN AND SECURED. RAN ALL THREE HYD SYSTEMS AGAIN AND CHECKED FOR ANY ACTIVESDR FDEA201305070931Selector Valve · malfunctionedAT LEVEL OFF RECEIVED YELLOW HYD LOW PRESS THEN LOW QUANTITY. FOLLOWED QRH SECURED YELLOW SYSTEM AND CONTINUED TO DESTINATION. REPLACED MCD SELECTOR VALVE IAW MM 52-33-53-04. OPS AND LEAKS CHECKS NORMAL ACFT OK FOR SERVICE.SDR JJBA20130506002Hydraulic System · lowAFTER TAKEOFF, CREW REPORTED THAT THE NR 2 ENGINE HYD PUMP LIGHT ILLUMINATED AND THE SPOILER LIGHT ILLUMINATED WITH VIBRATION EXPERIENCED. THE CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. THE MX CREW BLED AND SERVICED THE HYD SYS AND ALL CHECKS WERESDR CA130506004Check Valve · leaking(CAN) ACFT SUSTAINED A LEAK IN THE YELLOW HYD SYSTEM. DUE TO LOW LEVEL OF HYD FLUID, CREW SHUTDOWN PUMP RENDERING YELLOW HYD SYSTEM UNSERVICEABLE. CRF WAS REQUESTED FOR LANDING, FLIGHT DID NOT DECLARE AN EMERGENCY. YELLOW HP MANIFOLD CHECK VALVE LEAKING, CHESDR UALA2013050703181B-Nut · leakingHYDRAULIC FLUID LEAKING FROM LEFT MLG. PUDDLE UNDER THE GEAR. FOUND B-NUT LOOSE ON LOWER BRAKE SERVO VALVE. SECURED B-NUT, NO LEAKS NOTED.SDR UALA2013050703176Hydraulic System · leakingFLUID DRIPPING FROM BOTTOM OF FSLG. REPLACED PTU, OP AND LEAK CHECKED GOOD.SDR A6WA201305064202Hydraulic Line · chafedNR 1 HYD LOW PRESS IN FLIGHT, PRESSURE + QTY WENT TO ZERO, C/W QRH AT ZERO QTY FOR 18 MINUTES. REMOVED AND REPLACED CHAFED LINE IN AFT EQUIPMENT BAY AND LEAKING LINE IN PYLON. OPS AND LEAK CHECK GOOD AT THIS TIME IAW AMM 20-22-00.SDR CA130506007Line · chafed(CAN) CREW ADVISED LOW NR 1 HYDRAULIC QTY AND WHEN THEY SELECTED FLAPS DOWN, THEY RECEIVED A NR 1 HYD ISO VALVE CAUTION AND THE FLAPS STAYED AT 0. CREW CONDUCTED A FLAPLESS LANDING. MAINTENANCE FOUND THE NR 1 ENGINE EDP PRESSURE LINE, PN 82970410-119, AND CSDR UALA2013050603159O-Ring · damagedHYD LEAK IN 'C' SYS. REPLACED O-RING OTBD SPOILER RIGHT SIDE, OPS CHECKED. LEAK CHECK NORMAL NR 12 SPOILER.SDR DXTA201305060571O-Ring · tornLOST A SYS HYD SYS. QUANITY DROPPED BELOW 14 PERCENT FOLLOWED BY ASSOCIATED CAS MSG. "A" PRESSURE WENT TO ZERO. FOLLOWED CHECKLIST, BLEW GEAR DOWN. HYD FLUID LEAKING UNDER ACFT CENTER DRAIN MAST. TROUBLESHOT "A" HYD SYS. FOUND LT HYD PRESSURE TRANSDUCER SDR CA130506003Manifold · leaking(CAN) DURING WALKAROUND MAINTENANCE FOUND HYD LEAK AT GREEN GROUND SERVICE MANIFOLD, 2 SCREW HEAD BROKEN. MACHINE SCREWS WERE REPLACED AND ACFT RETURNED TO SERVICE.SDR UALA2013050303124Line · leakingNR 2 ENGINE HAS A MASSIVE HYDRAULIC LEAK. REPLACED HYDRAULIC LINE IN NR 2 ENGINE PYLON FOR THRUST REVERSER DEPLOYMENT. OPS AND LEAK CHECKED GOOD.SDR 2013FA0000323Switch · inoperativeDURING FLIGHT, THE "HYD POWER" ANNUNICATOR AND WARNING HORNS WERE ACTIVATED. THE PILOT FOLLOWED THE PUBLISHED EMERGENCY PROCEDURE AND DEACTIVATED THE HYD POWER. AN EMERGENCY WAS DECLARED AND THE PILOT EXECUTED A RUN-ON LANDING. DURING THE MX INVESTIGATION, ISDR HALA2013050200052Filter · failedON CLIMBOUT, LT HYD QTY EICAS MESSAGE DISPLAYED. STATUS PAGE SHOWED ZERO QTY. RAN QRH PROCEDURE AND RETURNED TO DEPARTURE. FOUND DPI FOR PRESSURE FILTER ON EDP (L) MODULE BLOWN. REPLACED DPI IAW AMM 29-11-17. REPLACED CASE DRAIN AND PRESSURE FILTERS ON EDP SDR UALA2013050303122Line · leakingHYDRAULIC FLUID DRIPPING FROM AFT OF AFT CARGO DOOR. REPLACED LEAKING TUBE ASSY AT AFT CARGO DOOR SELECTOR VALVE IAW MM 20-23-11-300-001-A. OPS AND LEAK CHECKED GOOD. OK FOR SERVICE.SDR MTNA20130501001Accumulator · lowON LANDING, NOSE WHEEL STEERING FAILED TO RESPOND TO INPUT AND ACFT VEERED TO LEFT. APPLICATION OF NORMAL BRAKE ON PILOT AND CO-PILOT SIDE FAILED TO SLOW AND EMERGENCY BRAKES REQUIRED TO STOP. ONCE TAXI ATTEMPT WAS RESUMED, NOSE WHEEL STEERING AND NORMAL BRASDR UALA2013050103051Hose · leakingRIGHT MLG OTBD FRONT BRAKE HOSE LEAKING HYDRAUIC FLUID. REPLACED HOSE ASSY, CHECKED OKAY.SDR UALA2013043003039Line · leakingHYDRAULIC LEAK FROM LEFT AILERON. FOUND HYDRAULIC SUPPLY LINE FOR INBD SERVO CONTROL, PIN HOLE LEAK AT ELBOW BULKHEAD FITTING. REPAIRED LINE.SDR CLCA20130430002Unknown · malfunctionedAFTER DEPARTING MIA, AND DURING CRUISE FLIGHT, LEVEL 1 ALERT 1, 2, 3 LHEDF OFF. ENGINE HYD PUMP CONTROL CIRCUIT BREAKER OUT. RETURNED TO MIA WITHOUT INCIDENT.SDR UALA2013043003038Line · unsecureTHREE INCH ROUND PUDDLE OF FLUID ON GROUND BETWEEN AFT TIRES RIGHT SIDE. SECURED HYD LINE TO TILT ACTUATOR ON RIGHT MAIN GEAR. PRESSURIZED HYD SYS NO ACTIVE LEAKS FOUND. ALL THREE HYD QTY'S FULL.SDR SWIA201333357Line · leakingFLT 4808. LOST ALL NR 1 HYDRAULIC FLUID. REPLACED CHAFED LINE IN THE AFT EQUIPMENT BAY, NR 1 ENGINE DRIVEN PUMP, PRESSURE SWITCH AND BLED NR 1 HYDRAULIC SYSTEM.SDR UALA2013043003020Pressure Switch · faultyAFTER SHUTDOWN AT GATE, RT ENGINE HYDRAULIC SWITCH PRESSURE LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED RIGHT ENGINE EDP PRESSURE SWITCH REF AMM. LEAK AND OPS CHECKED.SDR QXEA2013042900819Warning Light · multiple failNR 2 HYD PRESSURE AT 0. NR 2 HYD ISO, ROLL SPOILER HYD SPOILER OTBD. NR 2 RUDDER HYD CAUTION LIGHTS ILLUMINATED, CIRCUIT BREAKERS ALL IN. COMPLIED WITH FIM TASK 29-10-00-810-804, STEPS 1 THRU 4A (1) FOUND LARGE AMOUNT OF AIR IN NR 2 HYD SYSTEM, BLEED HYD SYSDR V6NA20130426001Tube · leakingENROUTE, HYD SYS INDICATED ZERO SYS PRESSURE. DIVERTED, PERFORMED A MANUAL GEAR EXTENSION IAW CHECKLIST. RAN CHECKLIST FOR, "FAILED HYD LANDING". LANDED WITHOUT INCIDENT. HYD PRESSURE WAS AVAILABLE FROM THE AUX PUMP FOR USE WITH BRAKING. DETERMINED TO BE SDR V6NA20130429001Tube · leakingENROUTE, HYDRAULIC SYSTEM INDICATED ZERO SYSTEM PRESSURE. DIVERTED, PERFORMED A MANUAL GEAR EXTENSION IAW CHECKLIST. RAN CHECKLIST FOR, "FAILED HYD LANDING". LANDED WITHOUT INCIDENT. HYD PRESSURE WAS AVAILABLE FROM THE AUX PUMP FOR USE WITH BRAKING. DETERSDR CA130429012Line · leaking(CAN) HYDRAULIC HOSE REPLACED WITH NEW HOSE AT 972.8 HRS. HELICOPTER LANDED AFTER TRAINING FLIGHT. THE PILOT NOTICED HYDRAULIC FLUID ON THE RT SIDE OF THE ACFT. ENGINEER CHECKED AND THE DECK WAS COVERED WITH HYDRAULIC FLUID. ACFT WAS GROUNDED WAITING ON REPSDR CA130424006Hose · leaking(CAN) NOUS AVONS INSTALLER UNE DEUXIEME HOSE A 3458. 6HRES ET A 3472.2 HRES LA HOSE A COMMENCER A FUIRE. VOIR LES DERNIERS RAPPORT RDS (TC# 20130424006)SDR AALA20130425001B-Nut · looseLAX - CREW REPORTED DURING FLAP EXTENSION, "B" SYSTEM HYDRAULIC SYSTEM QUANTITY DROPPED TO ZERO. EMERGENCY DECLARED FLIGHT LANDED LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. TIGHTENED "B" SYSTEM SUPPLY TUBE IN RIGHT WING B NUT THAT WAS FOUND LOOSE. SDR CA130425002Line · split(CAN) HYDRAULIC LINE HAS SMALL SPLIT, NOT VISIBLE TO NAKED EYE, BUT SHOWS UP WHEN UNDER PRESSURE.SDR CA130424003Hose · leaking(CAN) NEW STYLE LINES WERE INSTALLED LESS THAN 3 HRS PRIOR TO FAILURE. PILOT NOTICED HYD FLUID UNDER THE ACFT AND FOUND A MASSIVE LEAK ON THE MGB DECK. THERE HAVE BEEN REPORTED ISSUES WITH THESE "NEW" LINES AND WE ARE AWARE OF SEVERAL OPERATORS WHO HAVE HAD SDR UALA2013042302829Fuse · leakingAFTER LANDING HAD LOSS OF HYDRAULIC FLUID IN RIGHT SYSTEM. REPLACED NORMAL ANTISKID MODULE HYDRAULIC FUSE IN LEFT WHEEL WELL, BOTTOM FUSE. BRAKES OPS NORMAL, NO LEAKS NOTED.SDR UALA2013042302820Line · leakingRIGHT HYD SYSTEM LEAK AT PYLON. REMOVED NR 2 ENGINE THRUST REVERSER ISOLATION VALVE HYD PRESSURE LINE. REPLACED LINE WITH A FLEXIBLE LINE IAW GPM 1-0-13-003 PG 10. OPS AND LEAK CHECKED OK.SDR CLCA20130422001Hydraulic Line · looseDURING CRUISE, LEVEL 1 HYD PUMPS 1L, 2L, 3L OFF APPEAR ON SD AND ENG HYD PUMP CONTROL RIGTH CB POPPED OUT. LEVEL 1 SEL HYD SYS MAIN DURING FLIGHT. PRIOR TO LANDING MIA, LEVEL 2, HYD 3 FAIL DUE TO LOSS OF ALL HYD FLUID. MANUALLY EXTENDED LG, LANDED WITHOUT ISDR UALA2013042202782Unknown · leakingHYDRAULIC FLUID STREAMING DOWN APU COMPARTMENT, LEAK IS COMING FROM RUDDER AREA, SUSPECT PCU OR BROKE LINE. INSPECTED AREA FOUND NO LEAKS.SDR QMLA2013042013060Line · leakingPILOT REPORTED HYD FLUID ON THE M/R TRANSMISSION AND DECK POST FLIGHT. CLEANED THESE AREAS, RETIGHTENED ALL THE HYD LINE FITTINGS THEN PERFORMED A GROUND RUN OF THE ACFT. UPON VISUAL INSPECTION, DURING THE GROUND RUN HYD FLUID BEGAN SEEPING OUT FROM UNDER THSDR QMLA2013042013059Line · leakingPILOT REPORTED HYD FLUID ON THE M/R TRANSMISSION AND DECK POST FLIGHT. CLEANED THESE AREAS, RETIGHTENED ALL THE HYD LINE FITTINGS, THEN PERFORMED A GROUND RUN OF THE ACFT. UPON VISUAL INSPECTION DURING THE GROUND RUN HYD FLUID BEGAN SEEPING OUT FROM UNDER THSDR QMLA2013042013058Line · leakingPILOT REPORTED HYD FLUID ON THE M/R TRANSMISSION AND DECK POST FLIGHT. CLEANED THESE AREAS, RETIGHTENED ALL THE HYD LINE FITTINGS THEN PERFORMED A GROUND RUN OF THE ACFT. UPON VISUAL INSPECTION DURING THE GROUND RUN HYD FLUID BEGAN SEEPING OUT FROM UNDER THESDR UALA2013041902713Line · leakingNR 2 ENGINE COWLING SHOWS EVIDENCE OF OIL LEAK. FOUND NR 2 THRUST REVERSER HYD LINE LEAKING. REPLACED NR 2 THRUST REVERSER CROSSOVER FLEXSHAFT HYD LINE PER MM. CYCLED REVERSER SEVERAL TIMES. NO LEAKS. OK FOR SERVICE.SDR USAA2013041900020Line · leakingON CLIMBOUT FROM PHX, CREW REPORTED TO DISPATCH THEY LOST THE YELLOW HYDRAULIC SYSTEM. CREW DECLARED AN EMERGENCY AND RETURNED TO PHX. FLIGHT LANDED WITHOUT INCIDENT. FOUND NR 2 PYLON HYD PRESSURE LINE CHAFED. R & R HYD LINE, LEAK CHECKED GOOD. CHECK OF SDR CA130417002Hose · failed(CAN) 1000 PRIOR TO LANDING CREW REPORTED HYDRAULIC FLUID LOSS ON GREEN SYS. QRH PROCEDURE APPLIED AND ACFT LANDED UNEVENTFULLY. ACFT HAD TO BE TOWED OFF THE RUNWAY DUE TO LOSS OF STEERING CAPABILITY. AFTER INVESTIGATION, IT WAS FOUND THAT THE RT MLG DOOR UPL
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