JASC 2910
Service difficulty reports · 11,291
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 7SJA2017120400619Hydraulic System · leakingHYDRAULIC NR 1 SYSTEM, 'HYD 1 LO QTY' CAS MESSAGE ON MFD. WITH VISUAL VERIFICATION OF HYDRAULIC FLUID AFTER LANDING.SDR CALA2017120204290Sdac · leakingECAM WARNING "G RSVR LO LVL". EMERGENCY DECLARED. REF TSM 29-11-00-810-803, POSSIBLE SDAC ISSUE. RMVD AND RPLD SDAC 1 (1WV1) PER AMM 31-55-34-000-001-A AND 400- 001-A. OPS CHKD OK PER AMM 31-50-00-710-001-A.SDR VQIA2018F00004Control Unit · failedTHE FLIGHT CREW REPORTED AN ABORTED TAKEOFF DUE TO A NR 2 THRUST REVERSER FAULT. THE ACFT RETURNED TO THE GATE. R & R HYDRAULIC CONTROL UNIT IAW AMM 78-31-51.SDR 2017FA0000609Hydraulic System · leakingWHILE TAXING OUT FOR DEPARTURE, RECEIVED A HYDRAULIC SYSTEM 2 LOW CAS MESSAGE, WHICH WAS VERIFIED ON THE MFD PAGE, RETURNED TO THE FBO AND VISUALLY CONFIRMED HYDRAULIC FLUID LEAKING.SDR G1IA201711230001Filter · not reportedATTEMPTED TO PUT THE GEAR DOWN AND ONLY RECEIVED A NOSE GEAR GREEN LIGHT AND GEAR HANDLE RED LIGHT. CYCLED THE GEAR BUT HAD THE SAME RESULTS. EXECUTED THE EMERGENCY GEAR EXTENSION CHECK LIST. CONFIRMED 3 GREEN LIGHTS, HANDLE EXTINGUISHED. LANDED WITHOUT INCSDR HNAA2017112100377Line · contaminatedRIGHT MLG, AFTER GEAR RETRACTION, WOULD CONTINUE TO UNLOCK AND LOCK. SELECTED GEAR DOWN, ALL NORMAL WITH THE GEAR DOWN. R & R NOSE GEAR DOOR SOLINOID VALVE IAW MM 32-22-02. BLED HYDRAULIC LINE IAW MM 29-10-00-860-803-A. OPS CHECKED IAW MM 32-30-00-700-801-A. SDR CALA2017111704067Tube · leakingLEFT HYD QTY EICAS PUMPS OFF, QTY SHOWED .47 NOW .43 AND DECREASING. EMERGENCY DECLARED. REMOVED AND REPLACED A CHAFED HYDRAULIC LINE AND ADEL CLAMP. SECURED. SERVICED HYDRAULIC SYSTEM AND LEAK CHECKED, NO LEAKS NOTED.SDR 2020FA0000465Hydraulic System · failedHYDRAULIC PRESSURE FELL TO 0 PSI DURING FLIGHT. EMERGENCY EXTENSION OF LANDING GEAR PERFORMED. LIMITED BRAKING UPON LANDING.SDR VQIA2017F00061Hydraulic System · lowON 11/15/2017 THE FLIGHT CREW OF AIRCRAFT N523VA AN A319-112 WITH 33336 FH AND 12557 FC OPERATING VX HAD THE FOLLOWING WRITE-UP INBOUND INTO SFO: HYD B SYS LO PR IN FLIGHT. THE FLIGHT CREW DECLARED A PRECAUTIONARY EMERGENCY AND LANDED WITHOUT INCIDENT. UPONSDR 2017F00200Hydraulic Line · damagedHYDRAULICS, SYSTEM 1 INOPERATIVE. REPLACED OF FLEXIBLE HOSE OF LINE PRESSURE IAW/AMM 29-11-03 , IN OPERATIONAL TEST IS NORMAL.SDR IPXA2017111623653Tee Fitting · leakingHYDRAULIC LEAK IN THE TAIL SECTION, JUST AFT OF APU INTAKE INSIDE DOUBLE DOOR ACCESS. AFTER SELECTING APU AIR ON, SMOKE BEGAN TO FILL THE COCKPIT. SELECTED APU AIR OFF AND THE SMOKE QUIT. IDENTIFIED THE LEAK COMING FORM SWEDGE TEE FITTING AT THE MAIN NR 2SDR CALA2017111704065Actuator · leakingC HYD QTY EICAS MESSAGE, C QTY STABLE AT .48, WITH ALL CENTER PUMPS OFF. EMERGENCY DECLARED. FOUND THE RT MLG POSITIONER TILT ACTUATOR LEAKING . REMOVED AND REPLACED THE ACTUATOR IAW MM 32-32-18, OPS AND LEAK CHECKED WITH NO DEFECTS NOTED.SDR IPXA2017111423583Valve · stuckHYD PUMP AND ADP SHOW NO HYD PRESSURE WHILE RUNNING. FOUND ISOLATED ACMP PRESSURE VALVE STUCK. R & R THE VALVE IAW MM 29-11-08 AND RELAY K1 PANEL M1216. IAW STANDARD WIRE PRACTICES MANUAL 20-81-22. CLOSED THE VALVE PREVENTED PRESSURE TO GET TO PRESSURE SWISDR SWAA2017111317706Line · leakingA SYSTEM HYDRAULIC LEAKING FROM SPOILER ACTUATOR LINE. RETURNED TO DEPARTURE. REPAIRED THE NR 12 SPOILER PRESSURE LINE IAW MM.SDR UIEA2017121102387Control Unit · leakingLEFT STCM INPUT SHAFT SEAL HAS HYDRAULIC LEAK.(<P>REMOVED AND REPLACED LEFT STCM. OPS CHECK NORMAL IAW AMM 27-41-00-715-014 TASK .</P>)SDR ASMF20180116002Unknown · leakingDURING TRANSIT CHECK, DETECTED A HYDRAULIC LEAK IN THE LEFT MAIN LANDING GEAR RETRACT ACTUATOR. MAINTENANCE PERFORM A PRESSURIZATION OF THE SYSTEM TO VERIFY THE LEAKS, DID NOT CONFIRM THE HYDRAULIC LEAK. AS A PRECAUTION, THE LEFT MAIN LANDING GEAR RETRACT ASDR AALA201711129004O-Ring · damagedYELLOW SYSTEM LOW PRESSURE FAULT RESULTED IN THE AIRCRAFT DIVERTED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REPLACED DAMAGED O-RING ON PTU MODULE FITTING AND ACCOMPISHED A SATISFACTORY LEAK CHECK IAW AMM 20-29-00 AND AMM 29-SDR AALA20171108006Seal · leakingCENTER HYDRAULIC SYSTEM QUANTITY LOSS INDICATION, APU LOW DUCT PSI. CHECKED AND FOUND CENTER HYDRAULIC MODULE SEAL LEAKING. THE SEAL WAS REPLACED. SYSTEM PRESSURIZED, NO LEAKS FOUND IAW 29-11-13 & 12-12-01. AIRCRAFT WAS GROUNDED.SDR AALA20171108007Hydraulic Line · leakingFLT 288 PVG - ORD. THE AIRCRAFT WAS GROUNDED. DURING CRUISE EICAS MSG HYDRO QTY LOW C ILLUMINATED. THE FLIGHT CONTINUED AND DECLARED AN EMERGENCY FOR LANDING. ON FINAL APPROACH, AFTER GEAR DOWN SELECTED, EICAS MESSAGE HYDRO PRESS SYS C DISPLAYED. AFTER LANSDR DALA2017110708007B-Nut · leakingFLIGHT ATTENDANTS REPORTED FUMES IN CABIN AFTER TAKEOFF. FOUND THE LT A/C COMPARTMENT B-NUT ON A HYD FUSE LEAKING NEAR FILTER PACK. TIGHTENED THE B-NUT.SDR V6NA20171117001Packing · leakingDURING CRUISE AT FL410, OBSERVED THE AMBER LEFT LOW HYDRAULIC ANNUNCIATOR FLICKER FOLLOWED BY THE RIGHT. FLICKERED AGAIN A FEW TIMES THEN TURNED SOLID ON. THE HYDRAULIC PRESSURE GAUGE SHOWED NORMAL 1550 PSI. DETERMINED THAT THE HYDRAULIC PRESSURE GAUGE WAS VSDR REXA2017110301152Hydraulic System · leakingNR 1 HYDRAULIC LEAK. REPLACED THE EDP, PRESSURE MANIFOLD AND PRESSURE CHECK VALVE. ALL PARTS ACCOUNTED FOR IN WORK PACKAGE. YELLOW TAGS RECEIVED FOR CHECK VALVE REMOTE RECEIVING INSPECTION.SDR SIMA20171103003Line · leaking30 SECONDS AFTER GEAR HANDLE UP. LOST HYD 3 WITH A LOW PRESSURE GEAR DISAGREE. NOSE DOWN. BOTH MLG UP. RAN CHECKLIST FOR HYD 3. MANUALLY EXTENED GEAR, HYD 3 WAS 25%. HYD 3 35% BEFORE FLT, SERVICED BACK UP 48% HYD 3 NORMAL AT TAXI OUT. FOUND NOSE GEARSDR SWIA201743939O-Ring · failedHYD SYSTEM 3 FAILED DURING CRUISE FLIGHT. ZERO PSI. COMPLIED WITH QRH. DECLARED EMERGENCY. PERFORMED A FREEFALL EXTENSION OF LANDING GEAR. R & R THE HYD PUMP 3A AND 3B IAW AMM. R & R THE O-RING BETWEEN THE PUMP AND THE BALL ATTENUATOR. LEAK CHECKED GOOD.SDR F3LA2017110200244Line · chafedDIVERT DUE TO A GREEN HYD SYSTEM LOW LEVEL, NR 1 ENGINE PUMP PRODUCED LOW PRESSURE. REMOVED AND REPLACED THE LEFT ENGINE HYDRAULIC CONTROL UNIT PIPE IAW AMM 29-11-49-400-049-A. OPS AND LEAK CHECKED GOOD.SDR CALA2017102703791Line · leakingTHE NR 1 LE SLAT TRANSIT LIGHT IS ON WITH OVERHEAD LE DEVICE PANEL SHOWING NORMAL. EMERGENCY DECLARED. REPLACED L/E SLAT, B SYSTEM PRESSURE LINE. SERVICED THE HYD SYS IAW MM 12-12-00. OPS CHECKED IAW MM 27-81-00. NO FAULTS NOTED. NO FURTHER LEAKS NOTED. OK SDR UIEA2017102702128Line · leakingEXTREME ODOR OF JET ENGINE EXHAUST IN THE COCKPIT AND UPPER DECK DURING DESCENT. PERFORMED FIM 21-00, TASK 810. FOUND RT WING GEAR DOOR RETURN HYD FITTING LEAKING. PERFORMED APU BLEED FOR OIL CONTAMINATION. PERFORMED ENGINE BLEED AIR OIL CONTAMINATION CHECK,SDR AALA201710259017Power Unit · leakingFLIGHT ATTENDANT NOTED ODOR IN CABIN DURING FLIGHT AND GROUND OPERATIONS. FOUND A LEAKING POWER TRANSFER UNIT. REMOVED AND REPLACED GREEN/YELLOW POWER TRANSFER UNIT IAW AMM.SDR BSYR20171024264ALine · chafedAT LANDING GEAR EXTENSION DURING APPROACH, GEAR EXTENDED WITH THREE GREEN DOWN INDICATIONS, THE MAIN INBOARD GEAR DOORS DID NOT CLOSE AS INDICATED BY THE RED WARNING LIGHTS. LOSS OF HYDRAULIC PRESSURE AND ELECTED TO DIVERT TO A NEARBY AIRPORT. WHILE ENROUTESDR DALA2017102407754Line · looseDURING CRUISE, SYS B HYD SYSTEM LOW PRESSURE LIGHT CYCLED ON AND OFF EVERY 10 SECONDS. CHECKED MFD SYS PAGE AND NOTED THE B SYS QTY AT 0. TURNED OFF B SYS PUMP. B SYS PRESSURE REMAIND AT 2900. NO M/C LOW PRESS LIGHT. DECLARED EMERGENCY, LANDED NORMAL. MASDR FDEA201710233030Line · leakingAPPROACHING 50 FT CALL, DURING LANDING HYD QTY LOW C ANNUNCIATED. LANDED, STOPPED AT HIGH SPEED. FOUND HYD LEAKS FROM THE PRESSURE LINE OF THE LT PCU. R & R THE FLEX HOSE IAW MM 32-53-03-4. CHECKED CTR HYD SYS ALL DPI FOUND NORMAL AND INSPECTED CTR HSDR AALA20171022002Hydraulic Line · leakingAIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. CENTER HYDRAULIC SYSTEM PRESSURE CAUTION LIGHT ILLUMINATED. LANDING UNEVENTFUL. REMOVED AND REPLACED LEFT MAIN LANDING GEAR HYDRAULIC HOSE ASSEMBLY (LINE) PER AMM 20-10-10. LEAK AND OPERATIONAL CHECK GOOD.SDR SWAA2017102317320Hydraulic Line · damagedDIVERSION/DECLARED EMERGENCY, SUSPECTED BIRD STRIKE ON TAKEOFF. HYDRAULIC QUANTITY LOSS IN-FLIGHT. INSTALLED HYDRAULIC LINE PER AMM.SDR AALA20171020001B-Nut · leakingRETURNED TO FIELD AND AN EMERGENCY LANDING WAS ACCOMPLISHED DUE TO A GREEN SYSTEM HYDRAULIC LOSS. MAINTENANCE FOUND LANDING GEAR DOOR SELECTOR VALVE CONNECTOR LEAKING. PERFORMED RESET PROCEDURE ON GRAVITY EXTENSION TO MAKE THE LANDING GEAR AND THE DOOR SAFE ASDR IPXA2017101822754Shutoff Valve · malfunctionedEMERGENCY DECLARED, C HYD QTY, ENROUTE THE HYD SYS PRESSURE HYD C . 45 - .1 FLAPS EXTENDED ALTERNATE GEAR EXTENDED ALTERNATE RESERVE BRAKES AND STEERING ON.FOUND FLAP / SLAT SHUTOFF VALVE MODULE LEAKING. R/R FLAP / SLAT SHUTOFF VALVE MODULE WITH REF TO 767 ASDR AALA201710189017Line · brokenHYDRAULIC A SYSTEM FAILURE. EMERGENCY DECLARED, AND FLIGHT DIVERTED. LANDING UNEVENTFUL. REMOVED AND REPLACED A BROKEN HYDRAULIC LINE ON THE NR 1 ENGINE PYLON IAW AMM 20-50-11. LEAK AND OPS CHECKED GOOD. AIRCRAFT WAS GROUNDED.SDR DXTA201710160001Line · leakingA SIDE HYD FAILURE. REMOVED AND REPLACED BOTH HYDRAULIC LINES TO THE NLG RETRACT ACTUATOR. SERVICED THE HYDAULIC SYSTEM AND JACKED AIRCRAFT. RESET THE EMERGENCY GEAR BLOWDOWN SYSTEM AND BLED THE HYDRAULIC ACTUATOR SYSTEM. COMPLETED MULTIPLE OPS CHECK ( GEARSDR DALA2017101607532Accumulator · leakingDURING TAXI IN, AFTER STARTING THE APU AND TURNING ON APU AIR. THE CABIN FILLED WITH A THIN HAZE AND A SLIGHT BURNING ODOR WHEN AWAY WHEN APU AIR WAS REMOVED. PULLED AND COLLARED APU CIRCUIT BREAKERS. FOUND RT ELEVATOR ACCUMULATOR LEAKING IN TAIL COMPARTMSDR FDEA201710092885Line · chafedHYD QTY LOW C IN FLIGHT. TROUBLESHOT AND FOUND HYD FLUID LEAKING FROM RT MLG STEERING PCU PRESSURE HOSE. FOUND A HOLE ON IT DUE TO CHAFING WITH ITS GUIDE. R & R THE STEERING ACTUATOR PRESSURE HOSE IAW AMM 32-53-03-4. LEAK AND OPS CHECKED NORMAL. ACFT OK FSDR F3LA2017101000230Line · leakingYELLOW HYD SYSTEM FAILURE, NO FLUID LOSS OF ACCUMULATOR PRESSURE. PUMP RAN 20 SECONDS, PTU RAN 30 SECONDS, FOUND HYD LINE LEAKING. REMOVED AND REPLACED HYDRAULIC LINE IAW AMM 20-23-11-911-001, AND 20-23-11-917-001. PERFORMED NR 2 ENGINE IDLE AND LEAK CHESDR DXTAT2PL6D005ETFYHydraulic Line · leakingHYDRAULIC VOLUME LOW A CAS MESSAGE IN FLIGHT. EMERGENCY GEAR EXTENTION USED AS WELL AS EMERGENCY BRAKE SYSTEM. HYDRAULIC FLUID LEAKING REAR OF AIRCRAFT AS WELL AS NOSE GEAR AREA. TROUBLESHOOTING FOUND THE A SIDE PRESSURE LINE WITH A PIN HOLE, LEAKING. RESDR YENA201710050816Line · failedEMERGENCY DECLARED. CREW OBSERVED A HYD G RSVR LOW LEVEL ECAM. FOLLOWED THE QRH 10-9, TURNED OFF THE GREEN SYSTEM HYDRAULICS. AIRCRAFT LANDED UNEVENTFULLY AND WAS TOWED TO THE GATE. REPAIRED THE CASE DRAIN HYD LINE ON NR 1 ENGINE PYLON IAW 20-23-11. PERFORSDR TIMA20171004014Powerpack · failedLANDING GEAR DID NOT EXTEND WHEN SELECTED. PUMPED GEAR DOWN MANUALLY. LANDED WITHOUT INCIDENT. FURTHER INVESTIGATION REVEALED THAT THE PROBLEM WAS WITH THE HYDRAULIC POWER PACK.SDR HALA2017100400250O-Ring · leakingATB, RIGHT HYDRAULIC QUANTITY LEAK. REPLACED LT BUNGEE CYLINDER ACTUATOR O-RING.SDR CALA2017100603431Valve · faultedECAM CAUTION MESSAGE FOR G RSVR LOW LEVEL MESSAGE INOPERATIVE. EMERGENCY DECLARED. REMOVED AND REPLACED GREEN LEAKAGE MEASUREMENT SOLENOID VALVE, LEAK AND OPS CHECKED GOOD IAW AMM 29-19-51SDR AALA201710029024O-Ring · leakingAIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. JFK-ZRH FLIGHT DIVERTED TO LHR ACCOUNT CENTER HYDRAULICS QUANTITY LOSS. LANDING UNEVENTFUL. MAINTENANCE FOUND AIR DRIVEN PUMP CASE DRAIN FILTER MODULE DIFFERENTIAL PRESSURE INDICATOR LEAKING. REMOVED AND REPLACEDSDR RAIA201709280002Hydraulic System · malfunctionedHYD 1 LOW ON EICAS. BLED NR 1 HYD SYSTEM, SERVICED THE SYSTEM, OPS CHECKED GOOD.SDR 2017FA0000642Hose · burstUPON LANDING GEAR RETRACTION ON DEPARTURE THE CREW NOTED THAT THE NOSE GEAR DID NOT RETRACT. THE HYDRAULIC LOW PRESSURE ECAS MESSAGE APPEARED ALONG WITH HYDRAULIC VOLUME LOW MESSAGE. PER THE CHECKLIST THE HYDRAULIC PUMPS WERE BOTH UNLOADED AND THE LANDING GESDR TIMA20170926013Powerpack · failedLANDING GEAR STARTED COMING DOWN IN FLIGHT, HAD TO MANUALLY PUMPED DOWN. FURTHER INVESTIGATION REVEALED THAT THE PROBLEM WAS WITH THE HYDRAULIC POWER PACK.SDR CALA2017092503324Tube · leakingLEFT HYD SYS LEAK. EMERGENCY DECLARED. FOUND HYD FLUID PUDDLING UNDER #1 ENG. REF IPC 29-11-05-03, FOUND THE TUBE ASSY LEAKING FROM LOWER END OF RIGID LINE AT THE B-NUT. TIGHTENED B-NUT APPROX 1/4 TURN. STILL LEAKING. R & R THE TUBE ASSY.
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