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 CA140521005Gauge · failed(CAN) AFTER REPLACEMENT OF A NR 3 BRAKE ACCUMULATOR FOR A PARK BRAKE PRESSURE DECAY DEFECT, THE ASSOCIATED PRESSURE GAUGE FAILED, CATASTROPHICALLY. THE ACCUMULATOR AND GAUGE WERE REPLACED WITH SERVICEABLE UNITS AND THE AC RETURNED TO SERVICE. AC HOURS:23865SDR DXTA2014052005775Filter · contaminatedAFTER TAKEOFF, GEAR WOULD NOT RETRACT. WITH THE GEAR HANDLE IN THE UP POSITION THE RED UNLOCK LIGHT ILLUMINATED & THE GREEN NO LIGHT & GREEN RT LIGHT REMAINED ILLUMINATED. AUDIBLE GEAR NOISE WAS OBSERVED. GEAR HANDLE WAS PLACED BACK TO THE DOWN POSITION & NSDR AALA20140519012Hydraulic Line · leakingTPA CREW REPORTED ON CLIMB OUT MASTER CAUTION LIGHT & LT HYD LOW PRESS LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED TPA LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LT HYD SYS RETURN LINE.SDR CALA2014052291112Hydraulic System · malfunctionedC HYD SYS PRESSURE MESSAGE ON EICAS. PERFORMED QRH PROCEDURE. YAW DAMPER KICKED OFF & NOTICED DIFFERENCE IN FLIGHT CONTROL PERFORMANCE. PRESSURE WENT TO ZERO ON BOTH CENTER ELECTRIC PUMPS. RECEIVED CTR HYD EICAS MESSAGE & IAW QRH SHUT OFF CTR PUMPS. DURINGSDR CA140520003B-Nut · loose(CAN) THE ACFT ENCOUNTERED A YELLOW HYDRAULIC SYS PRESSURE MESSAGE DURING CRUISE AFTER DEPARTURE. AS A PRECAUTION, THE FLIGHT CREW DECLARED A PAN PAN FOR PRIORITY WITH ATC. ONCE STABILIZED, THE FLIGHT CREW IN CONJUNCTION WITH MAINTENENCE AND FLIGHT DISPATCH,SDR CA140520004Pressure Switch · failed(CAN) LEFT HYD PRESS LOW AMBER CAS MESSAGE DURING DESCENT. LEFT HYD PRESSURE SWITCH WAS REPLACED. FUNCTION TESTS CARRIED OUT AND TESTED SERVICEABLE.SDR CA140517002O-Ring · cut(CAN) DURING DESCENT EMERGENCY DECLARED DUE TO NR 1 HYDRAULIC SYSTEM FLUID LOSS. UNEVENTFUL LANDING PERFORMED. MAINTENANCE FOUND A CUT O-RING NEAR THE GROUND-HYD SERVICE PORT. O-RING REPLACED AND ACFT RETURNED TO SERVICE.SDR CALA2014051691029O-Ring · damagedYELLOW HYD ECAM MSG LOW QTY. REPLACED BAD O RING ON BOTTOM OF YELLOW SYS FILTER MODULE ASSEMBLY, NR 2 ENG DRIVEN PUMP & CASE DRAIN FILTER. ALSO REPLACED REF ITEM 4192001 CHECKED ASSOCIATED FILTERS FOR METAL DEBRIS, NONE FOUND. SYS OPERATIONS CHECKED & LEAKSDR ASAA2014051407812O-Ring · leakingLIQUID DRIPPING UNDERNEATH RT ENGINE. ACFT GROUNDED. FOUND HYD FLUID FROM NR 2 ENGINE EDP CASE DRAIN. R & R EDP FILTER AND TEFLON RINGS IAW AMM 29-11-51-400-801. RAN ENGINE LEAK CHECK GOOD.SDR SWAA2014051427919O-Ring · failedDIVERSION, SYS A HYD FAILURE INFLIGHT. FOUND FAILED O RING ON A SYS MODULE. R & R O RING ON A SYS MODULE IAW SIP.SDR AWKA2014051419512Hydraulic Line · rupturedAFTER TAKEOFF & DURING GEAR RETRACTION, THE FLIGHT CREW HEARD A THUMP FOLLOWED BY INCREASED WIND NOISE. IT WAS NOTED THE GEAR INDICATING DOWN WITH THE GEAR HANDLE IN THE UP POSITION, THREE GREEN GEAR LIGHTS WITH A RED DISAGREE LIGHT WAS INDICATED. ON THE EICSDR CA140604001Line · ruptured(CAN) DURING CRUISE THE NR 1 MAIN HYDRAULIC SYS LOST ALL FLUID. ACFT DIVERTED TO BASE. AFTER LANDING, SMOKE WAS NOTICED COMING FROM THE LT ENGINE AND AIRFIELD SERVICES WAS REQUESTED. THE HYDRAULIC PRESSURE LINE RUNNING FROM PRESSURE MANIFOLD IN THE NACELLE, OSDR 9JLA2014052904789Filter Housing · defectiveTHE HYD FILTER BYPASS PIN WAS FOUND TRIPPED DURING A POST FLIGHT CHECK. THE HYD FILTER WAS REMOVED & NO CONTAMINATION WAS FOUND. THE FILTER WAS REINSTALLED & THE BYPASS PIN WAS RESET. LEAK & FUNCTIONAL CHECKS WERE SATISFACTORY, NO DEFECTS WERE FOUND. BEFORSDR CA140522018Line · failed(CAN) DURING WALK AROUND FOUND HYD FLUID LEAKING FROM AFT BELLY DRAIN NEAR POTABLE WATER SERV PANEL. UPON FUTHER INSPECTION BULK CARGO, RT SIDE BEHIND WATER TANKS, FOUND HYD SYS RETURN LINE LEAKING. PN 272W4690-56. BS 2150 PIN HOLE IN RADIUS NEAR UNION RESOSDR HNAA2014052900166Line · leakingWITH NR 2 ENGINE RUNNING AT FLT IDLE AND START FEATHER BLEEDS ON IN AUTO SET AT MAX AFTER 3-4 MINS STRONG ODOR IN MID TO AFT CABIN. PAX COMPLAINED AND DEPLANED ACFT. INSPECTED AND FOUND HYD LEAK AT NOSE GEAR DOWN LINE IN CABIN. CAPPED AND PLUGGED LINE OUTSIDSDR WVBA201405090090Housing · crackedAFTER SUCCESSFUL LANDING, PILOT REPORTED THAT THE LANDING GEAR WOULD NOT EXTEND AND HE HAD TO MANUALLY PUMP DOWN THE GEAR. MAINTENANCE EXAMINATION REVEALED THAT THE RT HYDRAULIC FILTER BOWL HAD RUPTURED IN THE THREADED PORTION APPROXIMATELY 0.25" ABOVE THE O-SDR IPXA2014050782891Packing · leakingHYDRAULIC QTY 3 LOW FAIL, REPLACED NR 3 SYS SPOILER SERVO AND ACTUATOR PACKING. PERFORMED HYD TEST NO MORE LEAK ALL SYS OK. PERFORMED NR 3 HYD SYS BLEEDING IAW 29 -03-00. ALL SYS OK.SDR R61A201405020626Valve · leakingCREW RECEIVED A NR 1 HYD PRESSURE CAUTION LIGHT ALONG WITH INTERMITTENT HYD PRESSURE AND QTY INDICATION. CREW RAN QRH, CONTACTED MAINTENANCE CONTROL AND DIVERTED TO PIT. CREW DECLARED AN EMERGENCY AND REQUESTED THAT EMERGENCY VEHICLES BE ROLLED. CREW MADE ASDR USAA2014050200001Hydraulic Line · leakingAT CRUISE ALTITUDE RECEIVED GREEN HYD RESERVOIR LOW LEVEL ECAM MSG. PERFORMED ECAM & QRH PROCEDURES. DIVERTED TO CLT RUNWAY 18C AFTER MANUAL GEAR EXTENSION. FOUND GREEN HCU HYD LINE LEAK. REPLACED GREEN HCU HYD LINE IAW AMM 29-11-49-000-049-A6. AS A PRECASDR DUFA20140502001Hydraulic Line · chafedAPPROX 200 FT AGL, THE PILOT BEGAN TO SEE & SMELL SMOKE IN THE COCKPIT. CONTACTED ATC & DECLARED AN EMER, MADE A SAFE LANDING. WHILE EXITING THE ACFT, NOTICED THE SMOKE WAS MUCH THICKER IN THE MID CABIN AREA. AN INSPECTION OF THE ENGS REVEALED NO EVIDENCE OFSDR FDEA201404260862Flex Line · leakingLEFT HYD SYS FAILURE AFTER LANDING. FOUND LT GEAR DOWN LOCK ACTUATOR FLEX HYD LINE LEAKING, ITEM 275 IAW IPC 32-32-51-15, MPN 271N6119-1. R & R FLEX LINE IAW SMP. FOR INFO BEFORE TO SERVICE HYD FLUID FOR LEAK CHECK, NOTED THAT LEVEL WAS 0.25, IAW MM 29-11-0SDR HALA2014042500055Hose · leakingDURING FLIGHT, RIGHT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED. PERFORMED ALTERNATE GEAR EXTENSION PROCEDURE. R & R RT MAIN GEAR ACTUATOR HOSE ASSY SERVICED HYDRAULICS. LEAK TESTED GOOD. OK FOR SERVICE. HYDRAULIC PRESSURE GOOD.SDR R61A201404250598B-Nut · brokenDURING SHORT FINAL, CREW REPORTED LOSS OF NR 2 HYDRAULIC FLUID TO ABOUT 10 PERCENT REMAINING. ACFT WAS ALREADY CONFIGURED FOR LANDING, CREW COMPLETED QRH PROCEDURES AND LANDED WITHOUT INCIDENT. AN EMERGENCY WAS NOT DECLARED. MAINTENANCE FOUND NR 2 WHEEL SDR FDEA201404250855Flex Line · crackedTAKEOFF PLUS TEN MINUTES EICAS LT HYD QTY, CREW NOTED QTY AT .60 & DECREASING AT A RATE OF APPROX .10 MINUTE. 5 - 6 MINUTES LATER LT HYD QTY WAS 0.00. EICAS LT HYD SYS PRESS FOLLOWED. LT HYD PUMP ELEC & ENG SHUTOFF AS DIRECTED BY QRH. HYD QTY WAS NEAR 0 SDR CA140428001Hose · leaking(CAN) ON A DAILY INSPECTION THE HYDRAULIC OIL LEVEL WAS FOUND TO BE LOW. IT WAS FOUND THAT THE TAIL ROTOR PRESSURE HOSE TO THE T/R SERVO HAD A SMALL LEAK IN IT. CHANGED THE HOSE OUT OUT AT THIS TIME WHICH FIXED THIS PROBLEM.SDR AWKA2014042453424O-Ring · leakingWHILE EN ROUTE, THE FLIGHT CREW REPORTED THE B HYD SYS DROPPED TO 17 PERCENT. THE CREW FOLLOWED THE CHECK LIST & SHUTDOWN & UNLOADED THE B HYD SYS. THE A SYS CONTINUED TO FUNCTION NORMALLY. IT WAS DISCOVERED THAT THE LT ELEVATOR PCU PRESS SWIVEL FITTING WASSDR 2A6R2014042297801Roll Pin · missingTANDEM HYDRAULIC PN 117-45020V002, SN 05-0198, TT 9205 4 FAILED AMC BK117 AAIP A-1641 TEST. THE LATERAL 1 SERVO VLV PN 105-46682 WAS FOUND MISSING ROLL PIN & SPRING.SDR CA140422002Line · ruptured(CAN) HYDRAULIC "UP" HOSE RUPTURED. FLUID LOSS. NR 2 SERVO LIGHT AND ZERO PRESSURE WITH RED UNLOCKED LIGHT. EMERGENCY GEAR EXTENSION SYS ACTUATED WITH NO EFFECT. PILOT REPORTED THAT WHEN MAINS TOUCHED DOWN NOSE GEAR THEN LOCKED INTO PLACE. LANDING COMPLETED.SDR UHLA2014042000327O-Ring · failedDURING DESCENT, RECEIVED HYD 2 LOW QTY MESSAGE FOLLOWED BY HYD 2 LOW PRESSURE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R & R HYD SYS 2 MANIFOLD PRESSURE O-RING, HYD SYS 2 EDP, AND HYD 2 PRESSURE RETURN EDP CASE DRAIN FILTERS.SDR 2014FA0000311Line · chafedWHILE TAXING INTO RAMP AREA, FOLLOWING AN UNSCHEDULED ENGINE CHANGE RUN-UP. THE AUXILIARY HYDRAULIC PUMP WAS ACTIVATED TO SET THE PARKING BRAKE. THIS PRESSURIZED THE BACKUP PRESSURE SUPPLY TO THE RT ROLL SPOILER. A CLOUD OF HYDRAULIC FLUID WAS OBSERVED BY TSDR QXEA2014041300300Hydraulic System · malfunctionedAFTER LIFT OFF, APPROX 200 AGL, ELEV PRESS CAUTION LIGHT ILLUMINATED. ALL 3 HYD SYSTEMS READ 3000 PSI. NR 3 HYD ISO VALVE WAS OUT AND DARK. CAUTION LIGHT STAYED ILLUMINATED THROUGHOUT FLIGHT. CAUTION LIGHT WENT OUT AND NR 3 HYD DROPPED AFTER LANDING. RETURSDR USAA2014041400013Circuit Breaker · failedENROUTE FROM PVD TO CLT, CREW RECEIVED A HYD SYS B LOW PRESS ECAM. DECLARED AN EMERGENCY & LANDED WITHOUT INCIDENT. ACCOMPLISHED TSM TASK 29-12-00-810-804-A, LOSS OF PRESS OF BLUE ELEC PUMP. FOUND PROBABLE MECHANICAL FAILURE OF CB 2701GJ. R & R CB IAW SPM SDR CA140414002Filter · dirty(CAN) DURING THE OPS-1 INSPECTION AND FOLLOWING THE "SCHEDULED INSPECTION PROGRAM", PHASE 1, MAINTENANCE PRACTICES, LJ-1063 AND AFTER, ITEM F.11.A. PERFORM THE GEAR-UP AND GEAR-DOWN PORT FINGER SCREEN CLEANING PROCEDURE. WHEN THE TECH PULLED THE SCREENS FOR CSDR JIKA2014041001Bowl · crackedSHORTLY AFTER TAKEOFF, TOWER NOTICE SOMETHING STREAMING FROM ACFT. AS A PRECAUTION PILOT CHECKED BOTH WINGS, ALL FOUR FUEL CAPS, FOR SUBSTANCE STREAMING FROM ACFT, NO VISIBLE SIGNS OF ANY SUBSTANCE STREAMING FROM ACFT. RETURNED TO DEPARTURE, AFTER PILOT SELSDR 2014FA0000246Line · chafedLOSS OF NR 1 HYD SYS, AFTER LANDING WITH ENGINES STILL RUNNING, NR 1 HYD LOW PRESSURE EICAS MESSAGE WITH ASSOCIATED MASTER CAUTION. ALSO, VISIBLE LIQUID IN AFT EQUIPMENT BAY. FOUND AN ADEL CLAMP CUSHION BECAME WORN TO THE POINT THAT THE METAL STRAP PORTION OSDR CALA2014041090799Control Unit · faultyNUMBER 2 CTR ELEC HYD PUMP DOES NOT LOAD SHED WITH ALL HYD PUMPS ON. REPLACED ELCU C1 IAW MM 29-11- 67, OPERATIONS CHECKED NORMAL. NR 2 CTR PUMP LOAD SHEDS WITH ALL PUMPS RUNNING.SDR IPXA2014050282841Structure · corrodedDURING 4C INSPECTION, DISCOVERED CORROSION ON CENTER WING TANK UPPER FWD AND CENTER SKIN BETWEEN XCW=-81 AND XCW=-100 AT STRINGER 15. ACCOMPLISHED REPAIR ON CENTER WING TANK UPPER SKIN BETWEEN XCW=-81-XCW=-100 AT STRINGER 15 IAW EA 011-5730-01-A5292 AND EO 57SDR CA140409001Valve · failed(CAN) CREW REQUESTED R33R PRIOR TO LANDING DUE TO A "10 MINS GREEN HYD LOW" MSG BEING ILLUMINATED. ECAM MSG DID NOT APPEAR DURING LANDING. THERE IS A REPORTED HISTORY OF THIS EVENT WITH THIS FIN. ACFT TAXIIED NORMALLY TO THE GATE AFTER LANDING. GREEN HYD SYSDR CA140409004Line · failed(CAN) THROUGH APPROXIMATELY 500, HAD THE MASTER CAUTION ILLUMINATE AND AN ASSOCIATED "OTBD SPOILER" CAUTION LIGHT. CAPTAIN ACKNOWLEDGED AND ASKED FOR "CALL TOP OF SECOND". FOLLOWING THE AFTER TAKEOFF CHECKS WE NOTED THE LANDING GEAR APPEARED TO NOT HAVE TRAVSDR YENA20140407071Line · leakingDECLARED AN EMERGENCY AND ACFT DIVERTED DUE TO NR 2 HYD LOW QTY IN FLIGHT. AT 22 PERCENT DROPPED DOWN TO 6 PERCENT DOWN WITH A 2 PERCENT DROP EACH 6 TO 10 MINUTES. LANDED WITH 6 PERCENT AFTER LANDING PRESSURE WENT TO 8 PERCENT THEN 10 PERCENT AT GATE. ALL FLSDR PRIA20140409001Hydraulic Line · misinstalledNLG DID NOT RETRACT WHEN GEAR HANDLE SELECTED UP. EMER & ABNORMAL PROCEDURES CHECKLIST FOLLOWED & GEAR WAS SELECTED DOWN. MLG EXTENDED & GREEN BUT NLG RETRACTED & HAD RED UNLOCKED LIGHT. TOWER VERIFIED MAINS DOWN & NOSE GEAR UP. EMER LG WILL NOT EXTEND PROSDR HALA2014040500044Line · damagedAIR DIVERSION, RT HYD QTY INDICATOR ILLUMINATED. FOLLOWED QRH. NOTED QTY ON RT TO 0.48. HYD TUBE ASSY ON LT ANTI SKID SHUTTLE VALVE DAMAGED. FLEX LINE INSTALLED.SDR DALA14020550992Fitting · shearedFLIGHT DIVERTED DUE TO RT HYDRAULIC SYS QUANTITY LOSS. CREW MANUALLY EXTENDED LANDING GEAR DUE TO ZERO HYD PRESSURE INDICATING DURING APPROACH. MAINTENANCE FOUND EVIDENCE OF HYD LEAKAGE IN RT WHEELWELL AND NOTED A FITTING SHEARED FROM THE DUAL BRAKE CONTROL VASDR USAA2014040100006Switch · faultyCREW REPORTED AN ECAM WARNING, HYD G RSVR LOW LEVEL. DECLARED AN EMERGENCY & LANDED WITHOUT INCIDENT AT CLT. FLIGHT TAXIED TO THE GATE UNDER ITS OWN POWER. R & R GREEN RESERVOIR LOW LEVEL SWITCH IAW AMM 29-11-41-400-003-A. OPERATIONS CHECK & LEAK CHECKED NSDR 9MTA2014040200001Hose · leakingPILOT REPORTED LOSS OF BRAKING. INSPECTION REVEALED HYD FLUID ON RT FLAP & IN RT GEAR WELL.SDR CHQA20140329098Hydraulic System · low pressureCREW REPORTED THAT AFTER TAKEOFF, RECEIVED A HYD SYS 1 LOW QTY MSG DURING GEAR RETRACTION. RETURNED TO FIELD & LANDED WITHOUT INCIDENT.. SERVICED HYD SYS 1. FURTHER, INSPECTIONS WERE COMPLETED ON THE FLIGHT CONTROLS, THE BRAKE SYS, THE HYD SYS, THE SPOILERSDR SWAA2014040126742Packing · failedNR 1 ENGINE A SYS HYD FAILURE A SYS ZERO HYD QTY. R & R HYD A SYS MODULE PACKING SEAL IAW MM.SDR SWIA201436917Hose · leakingHYD 1 LOW PRESSURE ON ED1. REPLACED INBD SPOILER RETRACT HOSE ASSY AND OTBD SPOILER HOSE ASSY.SDR CA140326025Motor · failed(CAN) THE PILOTS SELECTED GEAR DOWN AND THE LANDING GEAR MOTOR CB POPPED. THEY MANUALLY EXTENDED THE GEAR AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CAME TO TROUBLESHOOT THE PROBLEM AND FOUND POWER TO THE MOTOR. WHEN GEAR WAS SELECTED DOWN THEY HIT THESDR FDEA201403230548Transmitter · leakingHAD A TOTAL LOSS OF SYS GREEN HYDRALIC FLUID IN FLIGHT. MANUALLY EXTENDED GEAR. INSPECTED MAIN WHEEL AREA, FOUND PRESSURE TRANSMITTER LEAKING, HYD RESERVIOR NEVER WENT COMPLETELY EMPTY. REPLACED GREEN HYDRAULIC PRESSURE TRANSMITTER IAW AMM 29-32-13-04, OPS
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