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 FDEA201506141800Priority Valve · leakingREJECTED TAKEOFF AT 70 KIAS DUE TO ECAM YELLOW SYS HYD LOW QTY WARNING. RAN QRH, TURNED PUMPS OFF AS DIRECTED WITH ZERO QTY READING ON THE GAUGE AS THE QTY WENT TO ZERO UPON THE INITIAL FAILURE. R & R PRIORITY VLV 273179 IAW AMM 27-14-16-04. LEAK & OPERATIOSDR YENA20150610188Control Servo · leakingFLIGHT DIVERTED. DURING CRUISE FLIGHT RECEIVED ECAM: HYD Y RESERVOIR LOW LEVEL QUANTITY INDICATED ZERO. INSPECTED AND FOUND RT SPOILER NR 4 SERVO CONTROL LEAKING. R & R RT NR 4 SPOILER SERVO CONTROL REF AMM 27-64-51, OPS CHECK AND LEAK CHECK GOOD. "Y" HYD SYSSDR CA150610002Schrader Valve · leaking(CAN) APPROXIMATELY 2HRS INTO FLIGHT CREW CONTACTED MOC THROUGH DISPATCH TO DISCUSS MIGRATION OF HYD FLUID FROM RT SIDE TO CENTER. AFTER DISCUSSION IT WAS DECIDED NOT TO CROSS THE OCEAN & DIVERT BACK FOR MX TO INVESTIGATE FURTHER. RESOLUTION FOUND SCHRADER VSDR VNAA2015060900008Line · chafedCREW REPORTED THE NR 1 HYDRAULIC SYS HAD A LOW PRESSURE MESSAGE IN FLIGHT. DIVERTED AND LANDED WITHOUT INCIDENT. TROUBLESHOT THE NR 1 HYD SYS, INSPECTED AND FOUND HYDRAULIC PRESSURE LINE IN AFT EQUIPMENT BAY TO BE CHAFED. R & R THE HYDRAULIC LINE AND PERFORSDR CALA2015061000496Hydraulic System · lowHYDRAULIC QTY 0.57 RF LT SIDE. EICAS HYD QTY ON APPROACH. SERVICED LT HYD SYS IAW AMM 12-12-01-301. PRESSURIZED LT HYD SYS IAW AMM 29-00-00, NO LEAKS NOTED.SDR CA150618006Hydraulic Line · leaking(CAN) CREW REPORTED IN FLIGHT THAT THEY LOST HYD PRESS ON THE RT SIDE & THE QTY WAS AT 18%. NOTE RECENT HISTORY OF WORK ON HYD SYS. ALSO RECENT RT ENG CHANGE. ONCE ON GROUND CREW REPORTED THAT THE FIRST INDICATION WAS A CYAN SPOILER FAULT CAS MSG FOLLOWED ISDR MASA2015060512137Hose · failedHYDRAULIC SYS 3 ZERO PSI AND QTY, RETURNED TO FIELD, DECLARED AN EMERGENCY. MAINTENANCE TROUBLESHOT TO HOSE ON NLG RETRACT ACTUATOR.SDR CA150605001O-Ring · failed(CAN) YELLOW HYDRAULIC SYSTEM FAILURE ENROUTE. PACKING REPLACED ON CHECK VALVE OF YELLOW PTU MANIFOLD IAW AMM 29-13-15. LEAK CHECK C/O, NO LEAKS FOUND.SDR 9SUA2015060401Hydraulic System · contaminatedUPON GEAR EXTENSION, ON APPROACH, THE CREW DID NOT GET A GREEN SAFE RT MLG INDICATION. THE CREW DID A LOW APPROACH TO SEE IF THE TOWER COULD CONFIRM. THE CREW MISSED THE APPROACH, RAN THE APPROPRIATE CHECKLIST & DIVERTED. AFTER ACCOMPLISHING THE APPROPRIATESDR FDEA201506041694Hydraulic Line · blownCLIMBING THROUGH 13000 FT, EICA LT HYD QTY ON STATUS PAGE. LT HYD QTY WAS BELOW .48 & WAS CONTINUING TO GO LOWER. RETURNED & LOWERED LG WHILE WE STILL HAD FLUID. ALT LE & TE FLAP EXTENSION. UNEVENTFUL LANDING, NO NWS SO TOW IN TO GATE OF RUNWAY. NOTE, HYDSDR CA150603007Line · loose(CAN) ACFT HAD LT HYDRAULIC LOW PRESSURE MESSAGE IN FLIGHT AND DIVERTED. LT HYDRAULICS LOST DUE TO A LOOSE PRESSURE LINE FROM THE ENGINE DRIVEN HYD PUMP. ENGINE HYDR DRIVEN PUMP, LT HYD MAINFOLD, INTERNAL CHECK VALVE DEFECT AND CONTAMINATED WITH CHIPS FROM THSDR AALA201506019006Hydraulic Line · leakingFLIGHT 828, EN-ROUTE THE CREW RECEIVED A GREEN SYS HYD FAILURE MSG & ENG 1 GREEN HYD PUMP LOW PRESS LIGHT. OPERATIONAL DECISION WAS MADE TO RETURN. AFTER AN UNEVENTFUL LANDING, THE ACFT HAD TO BE TOWED TO THE GATE. REPLACED A GREEN SYS HYD PRESS LINE.SDR 2CCA2015060100066Piston · out of adjustDURING POST MAINTENANCE VISIT ACCEPTANCE FLIGHT, DURING FLIGHT CONTROL CHECK IN EXCESS OF 250 KTS, FOUND LT RUDDER HAD NO EFFECT WHEN DEPRESSED FULLY - EITHER WITH POWER ON OR OFF. FULL RUDDER TRIM HAD NO EFFECT DEFLECTED LEFT. RIGHT RUDDER CHECK AND TRIM OSDR CALA2015060193845Flex Line · leakingLOSS OF BLUE SYS HYD WITH ASSOCIATED LOW LEVEL & LOW PRESS EVIDENCE OF HYD FLUID AROUND BLUE SYS HYD BAY. R & R FLEX LINE IAW IPC 29-12-03-09 ITEM 330 & CLAMP ITEM 380. ALSO R & R BLUE ELEC PUMP IAW AMM 29-12-51-400-001A & BLUE SYS FILTERS IAW AMM 29-12-43 &SDR CA150602020Line · leaking(CAN) HYDRAULIC LINES, PN 704A34-412- 264 & -266 AFTER LANDING THE PILOT PERFORMED A QUICK CHECK OF THE SYS ON THE TRANSMISSION SYSTEMS AND FOUND HYDRAULIC FLUID ON THE DECK. DURING THE INSPECTION, 2 HYDRAULIC LINES, PRESSURE SIDE, WERE FOUND LEAKING. THESE TYSDR CA150601014Valve · broken(CAN) DURING FLIGHT TRAINING, TWO PILOTS WERE FLYING FOR A PPC. THE ACFT WAS JUST COMING OUT OF A TURN WHEN THE FLIGHT INSTRUCTOR SWITCHED THE HYDRAULICS OFF, AT THIS POINT THE CYCLIC IMMEDIATELY WENT HARD LT WITH BOTH PILOTS BEING UNABLE TO RESIST THE MOVEMENSDR CA150526007Hose · leaking(CAN) AUTO BRAKE FAIL ON APPROACH, GREEN HYD FAIL ON TAXI, ACFT STOPPED ON TAXIWAY FOR TOW IN TO GATE. FOUND DAMAGED HYD FLEX HOSE ON RT MLG GEAR CONNECTING TO RT MLG NORMAL BRAKE MANIFOLD. REPLACED HYD FLEX HOSE IAW AMM 32-11-12 PB 401. NO LEAKS NOTED AT TSDR E0YA2015060800001Pressure Switch · failedDURING FLIGHT, THE CREW NOTICED THE HYDRAULIC QUANTITY LOW MESSAGE ILLUMINATE. SHORTLY THEREAFTER THE HYDRAULIC PRESSURE FROM THE MAIN ENGINE HYDRAULIC PUMPS STARTED TO DROP FOLLOWED BY THE LT MAIN PRESSURE LOW WARNING LIGHT ILLUMINATE. THE MAIN PRESSURE DROSDR CA150526003Canister · damaged(CAN) DURING DESCENT THE GEAR WAS SELECTED DOWN & DID NOT RESPOND. EMER EXTENSION WAS USED TO DEPLOY THE GEAR. THE LT HYD CANISTER THREADS WERE FOUND SHEARED. THE LAST TIME THE CANISTER WAS REMOVED WAS APPROX 100 HRS PRIOR DURING INSPECTION. THIS IS THE SESDR FDEA201505251633Hydraulic Line · wornDURING ROLL OUT AFTER LANDING, LEVEL 2 HYD 1 FAIL ILLUMINATED. HYD QTY INDICATED 0.1 PRESS REMAINED ABOVE 2700 PSI WITH 1 - 3 RMP'S CLOSED. SELECTED HYD SYS MANUAL FOR TAXI IN. COMPLETED QRH PROCEDURES. 1/3 RMP HYD FLEX LINE BAD, ON ORDER.SDR CA150521002Motor · failed(CAN) ON DEPARTURE, THE LANDING GEAR WAS SELECTED UP BUT DID NOT MOVE FROM THE EXTENDED POSITION. TROUBLESHOOTING IDENTIFIED THE HYDRAULIC PUMP DC MOTOR WAS INOPERATIVE.SDR CA150520006Hose · ruptured(CAN) DURING APPROACH, WHEN GEAR SELECTED DOWN, NO FLUID INDICATING IN NR 2, ALSO ASSOCIATED CAUTIONS AFTER TROUBLESHOOTING MAINTENANCE FOUND THE NR 2 EDP SUCTION LINE RUPTURED. REPLACED IAW AMM 29-11-01. ENGINE RUNS CARRIED OUT WITH NO LEAKS FOUND. AFH 295SDR CA150519025Hose · broken(CAN) LOSS OF NR 2 HYD CONTENTS DURING GEAR RETRACTION. AFTER TAKEOFF ON GEAR UP SELECTION NR 2 SYS HYD CONTENTS DROPPED TO ZERO AND THE RT MLG DID NOT FULLY RETRACT. CREW REQUESTED A DIVERSION, ALTERNATE EXTENTION COMPLETED AND ACFT LANDED SAFELY FLEXIBLE HSDR CA150515008Hydraulic Line · defective(CAN) ENGINE HYD & FUEL HOSE FIRE PROOF PROPERTIES, RECEIVED FROM SUPPLIER HOSE ASSEMBLIES FOR NACELLES WITH THE SILICON FIRE SLEEVES MOLDED OR EXTRUDED ON SUBJECT PART NUMBERS HAVE NOT DEMONSTRATED, THROUGH ANNUAL TESTING REQUIRED BY AS150. FIRE PROOF PROPERSDR CA150520004Line · damaged(CAN) FLARE ON HYDRAULIC LINE FAILED AT THE CONNECTION TO THE GEAR SELECTOR ASSY. FAILURE CAUSED LOSS OF HYDRAULIC FLUID AND SUBSEQUENT EMERGENCY LANDING ON A GRASS FIELD. INSPECTION DETERMINED THAT THE FLARE HAD SUBSTANDARD MANUFACTURING QUALITIES. UPON INSPSDR SWAA2015051239597Hydraulic Line · damagedAIR TURN BACK, NR 1 ENG HYD PUMP LOW PRESS LIGHT SWITCH OFF IAW QRH. FOUND NR 1 ENG HYD PUMP PRESS LINE DAMAGED AT BULKHEAD. R & R PRESS LINE NR 1 ENG DRIVEN HYD PUMP IAW MM.SDR ESPA2015FA0000183Line · rupturedNORMAL TAKEOFF, ABOUT HALFWAY TO DESTINATION STARTED HEARING A LOW RUMBLE IN THE BELLY OF THE PLANE. HAVING BEEN THROUGH THIS BEFORE, HAD THE CO-PILOT CHECK THE HYDRAULIC PRESSURE WHICH WAS NORMAL. ABOUT 15 SECONDS LATER, HE SAID THE HYDRAULIC PRESSURE GUAGE SSDR PCSA2015050801Hydraulic Line · looseHYDRAULIC SYS A FAILURE. DECLARED AN EMER. FOUND NR 1 ENG HYD PUMP PRESS LINE LOOSE IN NR 1 ENG PYLON. THE LINE WAS SECURED, THE HYD SYS SERVICED, ENG OPERATED, FLIGHT CONTROLS CYCLED & LEAK CHECKS PERFORMED IAW THE AMM.SDR CALA2015050600375Compensator · damagedAFTER AUTOPILOT WAS ENGAGED, ACFT PITCHED DOWN. AUTOPILOT WAS MANUALLY DISCONNECTED. MOMENTARY FEEL DIFF PRESS LIGHT CAME ON. HYD SYS QTY SLOWLY DROPPED TO ZERO FOLLOWED BY A TOTAL LOSS OF HYD SYS A PRESS. PERFORMED FIM TASK 29-30-00-810-803 FOR FLUID & PRSDR AALA201505059007Tube · leakingAT CRUISE, THE ACFT HAD A GREEN SYS HYD FAILURE, WITH PRESS & QTY LOSS. THE CREW BURNED OFF THE PUMP IMMEDIATELY. THE FLIGHT DECLARED AN EMER & RETURNED. ON APPROACH, THE GEAR WAS MANUALLY EXTENDED. AFTER LANDING, THE ACFT NEEDED TO BE TOWED TO THE GATE. SDR CA150504008O-Ring · leaking(CAN) AFTER DEPARTING, THE FLIGHT EXPERIENCED A YELLOW HYD FAILURE. THE CREW IN CONSULTATION WITH FLIGHT DISPATCH, MTC CONTROL & SOC ELECTED TO DIVERT THE FLIGHT BACK WHERE & OVER WEIGHT LANDING BY 9000 KGS WILL BE CARRIED OUT. THE CREW WILL DECLARE A PAN WISDR CALA2015050493651Hydraulic Line · unknownG RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN AT FL 360. EMER DECLARED & DIVERTED. REPLACED NR 1 ENG HYD PRESS LINE.SDR MASA2015050212043Valve · leakingNM 3 HYDRAULIC QTY AT ZERO IN FLT. REPLACED FLOW LIMITER VALVE.SDR SWAA2015050439283Hydraulic Line · faultyDIVERSION, DECLARED EMER, SYS B HYD SYS FAILURE. SYS B QTY & PRESS WENT TO 0. R & R HYD LINE IAW MM.SDR 9EKA2015050416Pipe · looseLEFT HYD LOW LEVEL LIGHTS CAME ON IN FLIGHT. LT SERVO TOP PIPE LEAKING. LT SERVO TOP PIPE WAS TIGHTENED & NO FURTHER LEAKS DETECTED. NO LIGHTS AFTER RESERVOIR WAS RE-FILLED.SDR CA150430006Line · leaking(CAN) ACFT JUST CAME OUT OF INSPECTION. IT HAD ALL HYDRAULIC LINES REPLACED FOR 6 YEAR REPLACEMENT. ACFT WAS GROUND RUN AND LEAK CHECKED SERVICEABLE. ACFT DEPARTED A DAY LATER, AFTER ARRIVING PILOT DID A POST FLIGHT INSPECTION AND FOUND HYDRAULIC FLUID LEAKSDR UHLA201504290333Hydraulic System · lowTHE CREW REPORTED THAT THEY RECEIVED A "HYDRAULIC SYSTEM 1 LOW QUANTITY" MESSAGE AFTER TAKEOFF. THE ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED HYDRAULIC SYSTEM 1. OPS AND LEAK CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CA150501008Line · cracked(CAN) WHILE FIXING THE HYDRAULIC PUMP ON NR 2 ENGINE, THE PRESSURE LINE FLARE FITTING FROM PUMP TO THE FIRE WALL WAS FOUND CRACKED. NR 2 ENGINE AT FLARE ON LINE.SDR CA150429010Hose · leaking(CAN) AFTER REPLACEMENT OF ANOTHER NLG HYDRAULIC LINE WHO NEEDED TO BE REPLACED DUE TO SEEPING, WE PROCEEDED TO CARRY OUT A GEAR SWING FOR PROPER OPERATION AND LEAK CHECK. AFTER SELECTING GEAR UP AND HOLD FOR 5 MINUTES AT 3000 PSI, HYDRAULIC FLUID STARTED COMSDR WX0A2015050172563Hydraulic Line · looseDURING APPROACH RECEIVED RT HYD PRESS LOW ANNUNCIATOR. RT HYD QTY INDICATES 2 QTS, FOUND FLUID LEAKING FROM TAIL SECTION OF THE ACFT. FOUND HYD LINE RT SIDE TAIL SECTION B NUT LINE TO RUDDER PRESS GAUGE VIBRATED LOOSE. TIGHTENED HYD LINE RT SIDE RUDDER PRESSDR CA150427003Line · leaking(CAN) CREW REPORTED LT HYD SYSTEM FLUID LOSS AND RETURNED. RESOLUTION RT FLAPER ON POWER CONTROL UNIT RETURN LINE, LT HYD SYS, TIGHTENED IAW DMC B787-A-20-11-00-00A-030A-A.SDR HALA2015042600065Packing · leaking"HYD RT QTY LO" SYS FAILURE. R & R LT MLG BUNGEE CYLINDER B-NUT LINE FITTING PACKING IAW AMM 32-33-02 STEP 2, D, 1, H AND STEP 3, E, P. LEAK CHECK GOOD.SDR CA150428006Pressure Switch · intermittent(CAN) HYDRAULIC PRESSURE SWITCH INTERMITENT, FOUND DIRTY, LOCATED IN LT WHEEL WELL AREA, CLEANED AND TESTED, RE-INSTALLED AND PERFORMED 18 GEAR CYLCES THROUGHOUT THE DAY, RESPECTING MOTOR COOL DOWN TIMES, IAW SERVICE MANUAL, NO PROBLEMS FOUND.SDR CA150423004Line · melted(CAN) DURING MAINTENANCE INSPECTION, IT HAD BEEN FOUND THAT A HYDRAULIC LINE LOCATED FORWARD OF THE RT WING, INBD FLAP HAD MELTED FAIRLEADS. THE ITEMS ARE AS IDENTIFIED IN IPC 29-00-00, FIGURES 60 AND 70. HYDRAULIC LINE, PN: 82950010-185 AND FAIR LEAD, P/N`S:SDR VQI2015F00016Line · brokenACFT LANDED SAFELY AFTER LOSING GREEN HYDRAULIC SYSTEM QUANTITY AND DECLARING AN EMERGENCY. THE CREW ENTRIES: "HYD GREEN RSRV LO LEVEL IN FLIGHT" AND " HYD GREEN ENG 1 PUMP LO PR IN FLIGHT". MAINTENANCE FOUND PRESSURE RELIEF LINE BROKEN AND PROCEEDED TO REPLSDR AWKA20150428001O-Ring · damagedWHILE HOLDING SHORT OF THE RUNWAY, THE FLIGHT CREW RECEIVED THE MASTER CAUTION WARNING & A HYD VOLUME LOW A CAS MSG. THEY NOTICED THE A SIDE HYD QTY INDICATING 16 PERCENT & DECREASING AT A RATE OF APPROX 1 PERCENT EVERY 2 - 5 SECONDS. THE APPROPRIATE CHECKLISDR E07A20150424001Hydraulic Line · chafedAT APPROX 19:30Z N609LS LANDED WITH LT HYD FAILURE. HAD TO MANUALLY EXTEND THE GEAR, THEN MADE A UNEVENTFUL LANDING. DETERMINED A HYD LINE GOING TO LT HYD POWER PACK HAD A HOLE CHAFED IN IT.SDR SIMA20150419001O-Ring · failedJUST PRIOR TO LEVEL OFF, HYD 2 LOW PRESSURE CAUTION MESSAGE FOLLOWED BY, IB FLT SPOILERS, IB SPOILERONS, ON EDI. R & R O-RINGS ON HYD 2 DAMPENER & AFT HOSE ASSEMBLY ON HYD 2 DAMPENER IAW AMM 29-11-60.SDR CA150422001Hose · leaking(CAN) DURING THE CLIMB THE CREW RECEIVED A NR 2 ISOLATION VALVE CAUTION LIGHT AND NOTED THAT THEIR NR 2 HYDRAULIC FLUID WAS DEPLETED. MAINTENANCE FOUND THE LT OTBD ROLLER SPOILER ACTUATOR HOUSING FRACTURED. THE ROLL SPOILER ACTUATOR AND THE NR 2 EDP WERE REPSDR CA150421001Line · chafed(CAN) UPON INSPECTION OF THE ACFT IT WAS FOUND THAT THE LT SKI UP LINE ON THE LT MLG LEG WAS CHAFED THROUGH WHERE THE LEG EXIT THE FUSELAGE ON AFT FUSELAGE GEAR FAIRING. ONCE SKIS WERE SELECTED UP ALL PRESSURE WAS LOST WAS LOST AFTER IT RAN OUT OF HYDRAULIC F
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