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 DHL2004765007Filter · dirtyRIGHT MAIN GEAR BRAKES ARE CHATTERING WITH BRAKE APPLICATIONS WHEN RELEASE BRAKE APPLICATION NOTICE BRAKES STICKING. CHECK FOR FREE WHEEL ROTATION IS GOOD SERVICED BRAKE SYSTEM. REMOVED AND REPLACED RETURN "B" SYSTEM FILTER, NO LEAKS NOTED, OPS GOOD PER MM SDR MALA040578Isolation Valve · malfunctionedEN ROUTE TO ATL, YELLOW HYD SYSTEM HI TEMP LIGHT ILLUMINATED. FOLLOWED QRH AND RETURNED TO MEM. MAINTENANCE REMOVED & REPLACED NR 2 ISOLATION VALVE P/N HTE9531-3 IAW RJ MM CH 29-10-14 201. RAN A/C ON GROUND 30 MINUTES, ACTUATING ALL HYDRAULICALLY ACTUATED CSDR CA041013007Fitting · cracked(CAN) BRASS OUTLET ANGLE FITTING ON FUEL PUMP CRACKED CAUSING FUEL TO LEAK OUT IN FLIGHT.SDR DAT2004F00006Line · leakingDURING CLIMB OUT, WHEN GEAR WAS RAISED, FLIGHT CREW HEARD A HIGH PITCH WHINE. IT WAS NOTICED THE HYD L AND HYD R LIGHTS WERE ILLUMINATED ON THE CWP WITH THE CONTENTS GAUGE AT ZERO THUS ALL HYDRAULIC FLUID WAS LOST. EMERGENCY CRUISE AND DESCENT CHECKLISTS WERSDR 2004F00403Line · leakingDURING THE CLIMB-OUT WHEN THE GEAR WAS RAISED, THE FLIGHT CREW HEARD A HIGH PITCH WHINE. IT WAS NOTICED THE HYD L AND HYD R ILGHTS WERE ILLUMINATED ON THE CWP WITH THE CONTENTS GAUGE AT ZERO THUS ALL HYDRAULIC FLUID WAS LOST. THE EMERGENCY, CRUISE AND DESCENSDR DLM88040860Line · chafedLT HYD QTY BEGAN TO DECREASE IN CLIMBOUT FOLLOWED BY DECREASE IN PRESSURE. AFTER FOLLOWING QRH LT SIDE WENT BACK UP FROM 2 TO 17 QUARTS, PRESS REMAINED AT ZERO, PUMPS TURNED BACK OFF. FOUND HYD LINE CHAFED IN AIR CONDITION COMPARTMENT BEHIND P-DOME, LEFT SIDSDR A6WA200440129Manifold · malfunctionedHYDRAULIC 3B RUNS CONTINUOUSLY EVEN WITH SWITCH IN OFF POSITION AND CIRCUIT BREAKER PULLED HYDRAULIC QUANTITY DURING FLT WAS 95 PERCENT. REMOVED AND REPLACED PRESSURE MANIFOLD ASSEMBLY FOR ACMP HYD SYSTEM NR 3 A/B IAW AMM 29-12-05. (M)SDR QXEA200400671Line · leakingFLIGHT RETURNED TO FIELD AFTER THE NR 1 HYDRAULIC SYSTEM FAILED. MAINTENANCE INSPECTED THE AIRCRAFT AND REPLACED THE FLEX LINE FROM THE ANTI SKID VALVE TO THE PRESSURE MANIFOLD. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR 2004FA0000704Hydraulic System · contaminatedDURING THE INITIAL PHASE 1 AND 2 INSPECTION BEING COMPLETED ON AC, ROUTINE INSPECTION OF HYDRAULIC SYS COMPONENTS REVEALED THAT THE HYDRAULIC SYS FILTER HAD RETAINED A LARGE AMOUNT OF RED PLASTIC MATERIAL AND THE (GEAR DOWN) PORT SCREEN WAS FOUND TO BE ALMOST SDR P5CA0401190Line · dentedAFTER T/O NOSE GEAR WOULD NOT RETRACT. STATUS MESSAGE -GEAR DISAGREE-, -GEAR MONITOR-, -GEAR DOOR-. REPLACED DENTED HYDRAULIC LINE & BROKEN STOP BRACKET IN NOSE WHEEL WELL, PERFORMED INSPECTION OF NOSE WHEEL WELL & NO FURTHER DAMAGE. GEAR SWING ACCOMPLISHEDSDR 04251625Tube · leakingEVENT SUMMARY STATED EMERGENCY DECLARED FOR HYD 2 LOW PSI MSG. A/C LANDED SAFELY AT GATE. REMOVED AND REPLACED RT LOWER FAIRING. REMOVED AND REPLACED RETURN TUBE ASSY, RESERVOIR TUBE ASSY, FILL TUBE ASSY FOR NR 2 HYD. INSTALLED SCREWS ON RT ENGINE PYLON.SDR WRNA200400010Nut · looseCOMPLETE LOSS OF GREEN SYSTEM HYD QUANTITY. PERFORMED ABNORMAL CHECKLIST. RETURNED TO AIRPORT, PERFORMED MANUAL GEAR EXTENSION. LANDING NORMAL. MAINTENANCE FOUND JAMNUT LOOSE ON GREEN PRESSURE MANIFOLD. TORQUED NUT AND LEAK CHECK GOOD I/A/W A300 MM 20-21-SDR MALA040561Line · leakingDURING TAXI OUT, CAPT HEARD A LOUD POP, A LONG, STRONG LOW PITCH HISSING SOUND COMING FROM REAR OF AIRCRAFT. HYDRAULIC PANEL QUANTITY AND PRESSURE FOR GREEN SYS QUICKLY BLED TO ZERO AND ASSOCIATED QUANTITY, LOW PRESSURE AIR TO PRESSURE LIGHT ILLUMINATED. CABSDR HNAA0400118Line · crackedFLIGHT NR 3955, REPORTED THE NR 1 HYDRAULIC CONTENTS DROPPING ON LANDING. RUDDER ISO VALVE LIGHT ILLUMINATED THEN WENT OUT. FLIGHT LANDED WITHOUT INCIDENT. FLUID WAS NOTED AS LEAKING FROM THE LT FLAP AREA. MAINTENANCE FOUND THE SPOILER LIFT DUMP PRESSURE LINESDR A6WA200460033Line · rupturedFOUND RIGHT MLG FAILED TO RETRACT AFTER TAKEOFF, REV UNSAFE LIGHT ILLUMINATED, CYCLED MLG DOWN, RETUREND TO RDU FOR FERRY FLIGHT BACK TO ATW. INSPECTED AND FOUND RT MLG FLEX LINE FOR RETRACTOR BRAKES RUPTURED WITH HYDRAULIC FUSE BLOWN, REPLACED LINE. RESET HSDR SWAA042535Line · leakingAIR TURNBACK, NR 1 ENGINE HYDRAULIC A-SYSTEM LOW PRESSURE LIGHT ILLUMINATED. REMOVED AND REPLACED NR 1 ENGINE A-SYSTEM HYDRAULIC PRESSURE LINE PER MM.SDR CA040831013Line · leaking(CAN) LOST (A) SYSTEM HYDRAULICS. FOUND RT MLG UPLOCK HYDRAULIC LINE LEAKING AT ACTUATOR. LINE REPLACED IAW AMM 32-32-11 P/N BACH8A0LEE0260T. RT MLG UPLOCK LINE PRESSURIZED AND LEAK CHECKED SERVICEABLE. NR 1,2 ENG PRESS FILTERS CHECK OK IAW MM 29-11-71 NR 1SDR P5CA0401182Line · leakingVIA PHONE PATCH, CREW REPORTS 0 PSI/0 QTY ON NR 1 HYDRAULIC SYSTEM. INSTALLED TEMP FLEX LINE PER MM 20-11-18 & GMM 3-17-1, PLACED ITEM ON COI 921-163. LINE IS LOCATED AFT OF STATION 23600 ON LT SIDE.SDR RU3A0411Hose · rupturedLOST ALL HYDRAULIC PRESSURE ON NR 3 HYDRAULIC SYSTEM, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE DISCOVERED HYDRAULIC PRESSURE HOSE, P/N 600-75123-107 RUPTURED. RU3A (M)SDR I05R098769Pressure Switch · failedPRESSURE SWITCH FAILED IN 3 HRS OF OPERATION. REPLACED PART.SDR GNB2004F00000Line · crackedPILOT PRE-FLIGHT, HYDRAULIC RESERVOIR LOW. MAINTENANCE PRESSURE CHECKED SYSTEM, FOUND NR 6 PRESSURE LINE CRACKED AT BEND RADIUS.SDR 04FDEA02561Hydraulic System · malfunctionedREJECTED T/O AT APPROXIMATLEY 80 KIAS STANDARD POWER SET AT 109 N1 ON BOTH ENGINES. ECAM WARNING OF LOW HYDRAULIC PRESSURE ON NR 2 PUMP. RETURNED TO RAMP FOR INSPECTION. INSPECTED ALL AIRCRAFT EXTERIOR FOR OBVIOUS LEAKS, NONE FOUND. SUSPECT RIGHT HAND SIDESDR CA040910002Hose · burstBEFORE FIRST FLIGHT DURING HYDRAULIC TESTING, PILOT SWITCHED 'OFF' NR 2 HYDRAULIC SYSTEM. AFTER THE SYSTEM WAS SWITCHED BACK 'ON' PRESSURE INDICATION FELL OFF TOZERO. A/C WAS SHUTDOWN. SUBSEQUENT INSPECTION REVEALED THAT THE BRAIDED NR 2 HYDRAULIC HOSE FROMSDR 04FDEA02559O-Ring · tornAT 100 NM FROM GDL, LOST GREEN HYDRAULIC SYSTEM, GRAVITY GEAR EXTENSION AND LANDING NORMAL. PUMPS OFF AT 2300 PSI. FOUND EVIDENCE OF LEAKAGE ON ENGINE NR 1 PYLON. AFTER CLEANANCE AND INSPECTION FOUND GREEN PRESSURE SW LEAKING HYD DUE TO O-RING FAILURE, REPSDR DLM88040804Line · leakingLEFT SYSTEM HYD QTY WENT TO 3 QTS. TURNED OFF LEFT ENG DRIVEN PUMP PER POM. RE-ENGAGED LEFT ENG HYD PUMP DURING FINAL APPROACH. LEFT HYD QTY EVENTUALLY WENT TO ZERO. FOUND BLUE FLEXIBLE PRESSURE LINE LEAKING IN TAIL CONE AREA. REPLACED FLEX LINE, LT ENG DSDR MALA040538Isolation Valve · failedYELLOW HYD SYSTEM OVERTEMP ANNUNCIATOR ILLUMINATED IN FLT. AIR RETURN TO MSP. MAINTENANCE REPLACED NR 3 EDP P/N 521449, S/N ON F9932438, OFF MX653033 IAW 29-10-17, DID NOT FIX. REPLACED NR 3 ENGINE HYD ISOLATION VALVE P/N HTE9531-3, S/N ON 1190UB1/5, S/N OFSDR CA040825010Line · ruptured(CAN) HYDRAULIC QUANTITY INDICATOR SHOWED RAPID DEPLETION TO 1 GAL AFTER TAKEOFF. FOUND RUPTURED HYDRAULIC LINE P/N BACH8B04NN0214T IN NOSE LANDING GEAR WHEEL WELL.LINE REPLACED IAW 20-10-52. ENGINE HYDRAULIC CASE DRAIN FILTERS CHECKED FOR METAL CONTAMINATION,SDR CA040823001Line · cracked(CAN) DURING FINAL APPROACH, PILOT REPORTED SMOKE IN COCKPIT AND PERFORMED AN UNEVENTFUL EMERGENCY LANDING. THE 'SMOKE' REVEALED TO BE HYDRAULIC FLUID MIST, WHICH SPREAD ALL OVER IN THE COCKPIT. ON GROUND WE FOUND A HYDRAULIC LINE BELOW THE COCKPIT CRACKED NEASDR 2004UALA00779B-Nut · looseLANDED UNDER AMBER ALERT DUE TO LOSS OF HYDRAULIC SYSTEM. *S/D* AIRCRAFT EXPERIENCED GREEN HYDRAULIC QUANTITY LOSS INFLIGHT. FOUND B-NUT LOOSE AT BRAKE PRESSURE ACCUMULATOR. TIGHTENED B-NUT, NO LEAKS.SDR HNAA0400115O-Ring · leakingFLIGHT NR 3818 REPORTED TOTAL LOSS OF NR 2 HYDRAULIC SYSTEM CONTENTS. PRESSURE LOSS WAS FOR APPROX. 7 MINUTES, WITH NR 2 ENGINE RUNNING. MAINTENANCE FOUND UNION ON THE ASSOCIATED HYDRAULIC PRESSURE MANIFOLD TO HAVE A BAD O-RING. O-RING WAS REPLACED AND THE SYSSDR 2004FA0000757Pressure Switch · leakingAPPROX 5-10 MINUTES AFTER TAKEOFF, PILOTS NOTED NR 2 HYDRAULIC SYSTEM LOSING FLUID. SYSTEM CONTINUED TO LOSE FLUID SO NR 2 ENGINE WAS SHUT DOWN AND AIRCRAFT LANDED. MAINTENANCE FOUND NR 2 HYDRAULIC SYSTEM PRESSURE SWITCH LEAKING. INSTALLED NEW PRESSURE SWITSDR 2004UALA00776Hydraulic System · lowFLT EXPERIENCED LOSS OF ALL QTY GREEN HYDRAULIC SYSTEM. DECLARED EMERGENCY & CONTINUED TO PLANNED DESTINATION. AIRCRAFT LOST GREEN HYDRAULIC QUANTITY INFLIGHT. LANDING GEAR EXTENDED VIA GRAVITY. OAKLAND SERVICED GREEN SYSTEM TO FULL. RAN ALL SYSTEMS, VERISDR CA040819013Line · ruptured(CAN) AC WAS ORBITING OVER FIRE. A LOUD SURGING SOUND WAS HEARD. A CHECK OF HYDRAULIC RESERVOIR INDICATED THAT NO HYDRAULIC FLUID WAS REMAINING. FLAPS WERE SELECTED FROM 15 TO 0 DEGREES. HYD BYPASS WAS SELECTED UP. RETARDANT LOAD WAS JETTISONED. AC RETURNED SDR C2XA04IA102Hose · brokenBPT - FLIGHT 2409, DURING CLIMB THE CREW REPORTED THE LOSS OF ALL HYDRAULIC FLUID FROM THE NUMBER ONE SYSTEM. THE AIRCRAFT RETURNED TO BPT WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE INBOARD HOSE ASDR CA040819011Rccb · inoperative(CAN) THE NR 2 STANDBY HYD PUMP WOULD NOT COME ON LINE WHEN SELECTED. THE CAUSE WAS DETERMINED TO BE A FAILED REMOTE CONTROL CIRCUIT BREAKER. THE UNIT HAD ONLY 24.7 HOURS.SDR CA040813001Line · cracked(CAN) A/C WAS UNABLE TO EXTEND GEAR. FOUND HYDRAULIC HAND PUMP PRESSURE LINE WAS CRACKED JUST ABOVE FIRST CHECK VALVE. ALL HYDRAULIC FUEL LEAKED OUT.SDR AALA20040850Hose · damagedAFTER FEAR UP RECEIVED LT HYDRAULIC QUANTITY STATUS MESSAGE WITH HYDRAULIC LIGHT. SECURED LT HYDRAULIC PUMPS WITH FLUID IN SYSTEM AND LOWERED GEAR AND FLAPS PRIOR TO SYSTEM LOSS. RETURNED AND LANDED WITHOUT INCIDENT. FOUND IB RT MAIN GEAR EXTENSION AND REFRACSDR 04FDEA02462Hose · leakingON GEAR RETRACTION, HYD SYSTEM A QUANTITY WENT TO ZERO. NUMEROUS SAFETY WIRES BROKEN IAW EMERG PROC. BOTH A PUMPS OFF IMMEDIATELY, HYD FLUID SHUTOFFS CLOSED 5 MINUTES LATER, NR 1 AND NR 2 ENGINES SHUT DOWN APPROX 45 MINUTES AFTER THAT. FOUND LEAKING RT GESDR 0401325803Line · crackedIN CRUISE AT FL 37,000 FT RECEIVED R HYD SYS PRESS AND R HYD SYS QTY MESSAGES. QUANTITY SHOWED ZERO IN RT SYSTEM. DECISION WAS MADE TO DIVERT TO DTW. LANDING UNEVENTFUL, MAINTENANCE FOUND THE RETURN LINE FROM THE RT (ALTERNATING CURRENT MOTOR PUMP (ACMP) CRACKSDR 2004UALA00735Hydraulic System · inoperativeRETURNED TO FIELD DUE TO LOSS OF BLUE SYSTEM HYDRAULICS. FOUND BLUE HYDRAULIC SYSTEM ELECTRIC PUMP PRESSURE FLEX LINE CHAFED. REPLACED CHAFED LINE AE707414-2. OPERATIONS CHECK NORMAL.SDR 0401319919Line · rupturedFLIGHT CREW NOTICED THE LOSS OF HYDRAULIC FLUID FROM THE RT SYSTEM WHEN THE (RUDDER CONTROL MANUAL) LIGHT ILLUMINATED. COM PROCEDURES WERE COMPLIED WITH AND THE FLIGHT CONTINUED TO SCHEDULED DESTINATION. LANDING AT MSP WAS UNEVENTFUL. MAINTENANCE FOUND A RUPTUSDR IXXA0400103OB-Nut · looseDURING TAKEOFF FROM PGUA, HYDRAULIC FLUID DROPPED TO STAND PIPE LEVEL. HYDRAULIC FLUID WAS LEAKING FROM NR 2 ENGINE. AIRCRAFT RETURNED TO PGUA AND LANDED WITH INCIDENT. AN INSPECTION IS ON GOING. INFORMATION WILL BE PROVIDED AS SOON AS IT IS AVAILABLE. MASDR ASMF200408008Servo Valve · leakingDURING TRANSIT CHECK, HYDRAULIC LEAKAGE WAS DETECTED IN INTERIOR DOUBLE SERVO VALVE. IT WAS REPLACED IAW MM32-43-02, TEST WERE CORRECT.SDR CA040810003O-Ring · failed(CAN) ENROUTE, (GREEN SYS) LOW LEVEL PRESS INDICATION OBSERVED. THE CREW ACCOMPLISHED THE CHECK LIST AND CONTINUED TO YZF. THE AIRCRAFT LANDED WITHOUT INCIDENT AND WAS TOWED FROM THE RUNWAY. THE O-RING AND BACK-UP RING AT THE ACCUMULATOR FITTING WERE REPLACEDSDR DLM88040717Line · failedLOST COMPLETE RIGHT HYD SYS. PERFORMED EMERGENCY PROC AND RET TO ATL. FOUND NR 2 ENGINE HYDRAULIC PRESSURE LINE BLOWN. REPLACED SAME.SDR 2005FA0000265Line · unserviceableHAD 3 HYDRAULIC LINE FAILURES CAUSING LOSS OF LANDING GEAR OPERATION WITHIN 70 HOURS. 2 FAILURES WERE DUE TO LOOSE B-NUTS, 1 WAS FAILURE OF LINE AT FLARE. LINES ARE SOFT ALUMINUM, THIN WALL TUBING WITH NO SPEC NUMBER APPEARS TO BE 3003-0 USED FOR AIR AND VACSDR 2004UALA00708Warning Light · illuminatedGREEN RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN. EMERGENCY DECLARED. LOST NOSE WHEEL STEERING. TOWED TO GATE. FOUND GREEN SYSTEM YAW DAMPER SERVO ACTUATOR LEAKING. YAW DAMPER SERVO ACTUATOR WAS REPLACED.SDR 2004UALA00707Hydraulic System · lowRETURN TO FIELD WITH YELLOW HYDRAULIC SYSTEM LEVEL LOW. FOUND GREEN SYSTEM CHECK VALVE AT MANIFOLD LEAKING, REPLACED O-RING. OPERATIONS CHECK NORMAL.SDR AWXA200400842Tube · leakingPHX - DIVERSION - FLT 0058 - AFTER TAKEOFF FROM LAS EN ROUTE FOR JFK RECEIVED EICAS MESSAGE M56 LT HYDRAULIC SYSTEM PRESSURE, HYDRAULIC QUANTITY DECREASED TO ZERO AND SYSTEM PRESSURE WARNING LIGHT ILLUMINATED, DIVERTED TO PHX FOR REPAIR. MAINTENANCE FOUND LT SDR CA040812001B-Nut · cracked(CAN) CREW REPORTED 'A' SYSTEM HYDRAULIC FLUID LOSS IN FLIGHT. MAINTENANCE FOUND LEAK AT B-NUT END FITTING AT 'A' SYSTEM MODULE. LINE REPLACED.
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