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 AALA20140907008Hydraulic Line · defectiveLEFT HYD QTY WENT TO ZERO. FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED NOSE GEAR DOOR ACTUATOR PRESS HOSE. SYS GND CHECKED NORMAL OPERATION CLOSED.SDR YENA20140907185Pressure Switch · faultedFLIGHT DIVERTED DUE TO BLUE HYDRAULIC PUMP HAD A LOSS OF PRESSURE. PERFORMED TSM TASK 29-12-00-810A AND FOUND BLUE ELECTRIC PUMP PRESSURE SWITCH FIN 2074GJ AT FAULT. R & R PRESSURE SWITCH IAW AMM 29-12-17. OPS CHECK AND LEAK CHECK OK. FAULT NO LONER IN VIESDR CA140905001Clamp · damaged(CAN) NR 1 HYDRAULIC SYS FAILED IN FLIGHT. BEYOND 30 MIN, SYSTEM DEPLETED INVESTIGATION FOUND THE NR 1 HYDRAULIC SYS CASE DRAIN LINE, PN: 82974216-003, AIPC REF: 29-00-01, FIG 5, ITEM 60, WAS FOUND CHAFED THROUGH BY A LOOP P, CLAMP, THE CUSHION MATERIAL WAS SDR AALA20140904011O-Ring · splitRIGHT HYD SYS QTY LOSS. EMER DECLARED FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED SPLIT O RING ON SPOILER SOV. SYS GND CHECKED NORMAL OPERATION CLOSED.SDR CA140910004Hydraulic Line · failed(CAN) SLOW DEPLETION OF GREEN HYDRAULIC FLUID IN CRUISE ABOUT 1 HOUR FROM DESTINATION. ECAM ACTIONS COMPLETED. ARRIVAL AND LANDING UNEVENTFUL. MAINTENANCE MET FLIGHT AT GATE. RESOLUTION REPAIRED GREEN SYSTEM PX SUPPLY LINE P/N : D2904004809601OUTBD OF RIB 5SDR CA140902004O-Ring · leaking(CAN) NR 1 HYDRAULIC QUANTITY SHOWING 0, SOURCE OF LEAK WAS FROM HYDRAULIC FILTER MANIFOLD COUPLING P/N AE99116H. 1. DAMAGED PACKING REPLACED. 2. CASE DRAIN FILTER REPLACED 3. PRESSURE FILTER REPLACED. 4. RETURN FILTER REPLACED. 5. EDP REPLACCED DUE DRY RUN 6SDR JIKA2014090101Hydraulic Line · puncturedDURING APPROACH PILOT NOTICED A LOSS OF HYD PRESS. PILOT PERFORMED EMER CHECKLIST PROCEDURE ITEMS & MANUALLY EXTENDED LG. PILOT LANDED WITHOUT FURTHER INCIDENT. TROUBLESHOOTING REVEALED A PIN HOLE IN THE FLAP UP LINE AT HYD POWER PACK. REPLACED THE FLAP UPSDR USAA2014090200008B-Nut · looseON DESCENT CREW REPORTED GREEN HYD SYS FAILURE, LOSS OF FLUID & PRESS. DECLARED AN EMER & LOWERED THE GEAR MANUALLY. FLIGHT LANDED WITHOUT INCIDENT BUT WAS TOWED TO THE GATE. MX FOUND HYD PRESS LINE B NUT TO GREEN PTU MANIFOLD 1113GM LOOSE. TIGHTENED B NUTSDR CA140918001Ptu · leaking(CAN) LOST ALL HYD SYSTEM NR 2 FLUID AT GATE, FLIGHT CANCELLED, PTU FOUND LEAKING, PTU REPLACED, AC RETURNED TO SERVICE. A FAILURE IN FLIGHT WOULD HAVE HAD A MUCH BIGGER SAFETY IMPACT.SDR FDEA201408252309Hydraulic Line · failedUPON TOUCHDOWN WITH FLAPS 35 & MEDIUM BRAKES SELECTED, EXPERIENCED COMPLETE LOSS OF NR 2 HYD SYS FLUID RESERVOIR WAS ZERO & PUMPS OFF. ALL THESE HAPPENED BETWEEN TOUCHDOWN & TAXI SPEED. NR 2 LT FAN COWL OPENED, FOUND PRESS LINE GOING INTO THE HYD CONTROL UNISDR FDEA201408242304Hydraulic System · overservicedHYD YELLOW RSVR OVERHEAT LIGHT AFTER TAKEOFF. LIGHT STAYED ON. FOUND YELLOW SYS OVER SERVICED. DRAINED BETWEEN 1.5 & 2.0 GALLONS OUT OF YELLOW SYS. THIS COULD POSSIBLY REMEDY PROBLEM, BUT NO TIME TO LET SYS RUN. NEEDS TESTING & POSSIBLY MORE TROUBLESHOOTSDR CA140826028Packing · leaking(CAN) FOUND ALTERNATE NOSE LANDING GEAR EXTENSION RESERVOIR TO BE LEAKING FROM DIPSTICK TUBE AND THE RESERVOIR LID. WE WERE ABLE TO DUPLICATE THE LEAKAGE BY SIMULATING INFLIGHT AIRFLOW ACROSS THE RESERVOIR VENT OUTLET ON THE FUSELAGE SKIN WITH SHOP AIR. THIS WSDR YENA20140820164Hose · leakingCREW DECLARED AN EMERGENCY AND ACFT DIVERTED DUE TO ECAM HYD G RESVOIR LOW LEVEL. FOUND RT OTBD HOSE ON LOCKSTAY ACTUATOR OF RT MLG SNAPPED OFF. R & R RT OTBD HOSE IAW AMM 32-11-22. SERVICED GREEN HYDRAULICS IAW AMM 12-12-29. ACCOMPLISHED LEAK CHECK OF RT MLSDR CA140825007Line · leaking(CAN) LINE HAD CHAFFED THROUGH AT TWO SPOTS. A PINHOLE LEAK DEVELOPED WHERE IT CHAFFED ON THE EMERGENCY PRESSURIZATION UPPER CHECK VALVE COUPLING.SDR CA140821009Swivel · leaking(CAN) DURING WALKAROUND, A HYDRAULIC LEAK WAS NOTICED IN THE AREA OF THE NLG. UPON INSPECTION, IT WAS DISCOVERED THAT THE STEERING MANIFOLD PRESSURE LINE SWIVEL JOINT WAS LOOSE. THE MANIFOLD HAD BEEN IN PLACE SINCE DELIVERY. THE SWIVEL JOINTS WERE RETORQUED ASDR IPXA2014082084023O-Ring · leakingC HYD QTY EICAS MESSAGE FOLLOWED BY A C HYD PRESSURE EICAS MESSAGE. PERFORMED CHECKLIST AND RETURNED TO DEPARTURE FOR A FLAPS 20 LANDING. EMERGENCY DECLARED. SERVICED CTR SYS HYD. PERFORMED LEAK CHECK ON CTR SYS HYD. FOUND LEAKING AT THE LCCA FILTER COVER.SDR CA140818008Tee Fitting · broken(CAN) APPROXIMATELY 5 HOURS INTO THE FLIGHT THE CREW REPORTED A RIGHT HYDRAULIC LOW QUANTITY INDICATION. FOUND THE RT HYD SYS TEE BROKEN. REPLACED THE TEE AND RT EDP.SDR GTIA2014081401405Line · failedLOST ALL HYD G FLUID AFTER GEAR RETRACTION AFTER TAKEOFF. REPLACED LT MAIN GEAR DOWNLOCK ACTUATOR LINES DUE TO OTBD LINE LEAKING, IAW AMM 52-11-22-400-004A. NO LEAKS NOTED. DUE TO LOSS OF GREEN SYS REMOVE AND INSPECTED NR 1 ENGINE CASE DRAIN FILTER. REMOVESDR DALA2014081104423B-Nut · leakingAFTER LANDING, THE CREW CONTACTED MAINTENANCE AND ADVISED THAT THEY HAD DONNED THEIR OXYGEN MASKS DUE TO AN OIL ODOR. REPORTED PASSENGERS WERE GETTING SICK DUE TO THE ODOR. MAINTENANCE FOUND HYDRUALIC FLUID IN INTAKE DUCT AND PLENUM OF APU. ALSO FOUND LT GEASDR HNAA2014081100227Line · leakingHYDRAULIC LEAK IN NOSE WHEEL WELL. INSTALLED NLG DRAG STRUT ACTUATOR BLUE FLEX LINE. CYCLED GEAR. NO LEAKS NOTED. CHECKED GOOD.SDR CA140811003Hose · leaking(CAN) FLIGHT CREW NOTICED HYDRAULIC FLUID LOSS AT THE ELEVATOR AND CARRIED OUT A REJECTED TAKE-OFF. THE A/C TAXIED BACK TO THE GATE WITHOUT INCIDENT. INVESTIGATION BY MAINTENANCE PERSONNEL REVEALED A PUNCTURE AT THE NR 1 ELEVATOR PCU HYDRAULIC HOSE. THE HOSE WSDR 9EKA20140809009Hydraulic Line · rupturedINFLIGHT CREW NOTED NR 1 HYD SYS FAIL LIGHT ILLUMINATED & PROCEEDED TO SHUT DOWN NR 1 SYS. EXECUTED UNEVENTFUL LANDING. VISUALLY FOUND NR 1 HYD SYS PRESSURE LINE PN 70-060T000Y4B4 TO LT CYCLIC SERVO RUPTURED.SDR FXGA20140808001Hydraulic Line · looseHYDRAULIC FAILURE ON DECENT, EMER DECLARED & 0 DEGREE FLAP LANDING PERFORMED.SDR CA140809002Line · leaking(CAN) DURING FLIGHT, NR2 HYD ISOLATION VALVE CAUTION LIGHT ILLUMINATED. FOLLOWED BY FLUID LOSS INDICATION ON THE NR 2 SYSTEM HYDRAULIC QUANTITY GAUGE. MAINTENANCE FOUND HYDRAULIC LINE TO NOSE GEAR DRAG STRUT ACTUATOR LEAKING. LINE WAS REPLACED AND AIRCRAFT RSDR IPXA201408083914Hose · brokenAT BLOCK IN MX INFORMED CREW THAT NR 8 TIRE WAS SHOWING A FIRE. BRAKE TEMP NORMAL, FOUND BROKEN HOSE OF HYD BRAKE AFT PORT OF NR 8 BRAKE. NO OTHER EVIDENCE OF DAMAGE NOTED. R & R HOSE MM32-43-20-4, REV 80.00, DATE 07/22/14, PN OFF: ILLEG, PN ON: AE1014098SDR 6CBA20140806132Circuit Breaker · poppedAFTER DEPARTING, THE FLIGHT CREW REPORTED HYD CAWS IN FLIGHT. HYD CB POPPED SHORTLY AFTER GEAR SELECTED UP. THE LG WAS VISUALLY INSPECTED, FUNCTIONAL TEST COMPLETED OF NORMAL & EMERGENCY EXTENSION & RETRACTION SYSTEMS IAW AMM 12-A-32-30-00-00A-903A-A. NO DESDR DALA2014080604323O-Ring · leakingLOSS OF GREEN SYS HYDRAULIC FLUID. ALTERNATE GEAR EXTENDED. REPLACED GREEN SYS BRAKE MANIFOLD O-RING SEAL.SDR 2014FA0000459Line · chafedTHE ACFT EXPERIENCED A HIGH TEMP NR 1 HYDRAULIC SYSTEM LEADING TO A LOSS OF HYDRAULIC FLUID RESULTING IN A DECLARED EMERGENCY LANDING. AFTER INVESTIGATING THE CAUSE OF THE FLUID LOSS WE DISCOVERED THE NR 1 HYDRAULIC SYSTEM PRESSURE LINE, PN 604-75238-3 WAS CHSDR SWAA2014080630615O-Ring · damagedDIVERSION A SYS HYD FLUID LOSS IN FLIGHT. R & R NR 1 ENG TO PRESS MODULE UNION O RING IAW MM.SDR NI6R201408040015Hydraulic System · malfunctionedDURING CRUISE FLIGHT, EXPERIENCED MAIN HYDRAULIC SYSTEM PRESSURE LOSS. HYDRAULIC QUANTITY REMAINED AT NORMAL. AN EMERGENCY WAS DECLARED AND INITIATED EMERGENCY CHECKLIST ITEMS. HYDRAULIC SYSTEM WAS PLACED INTO BYPASS AND SYSTEM PRESSURE RETURNED TO NORMAL. SDR SWAA2014080130551Valve · leakingDECLARED EMER, A SYS HYD FAILURE. R & R VLV IAW MM.SDR 2017FA0000069Transmitter · intermittentPILOT REPORTED INTERMITTENT FAILURE OF THE NR 2 HYDRAULIC QUANTITY INDICATION. INSTALLED A NEW TANK QUANTITY TRANSMITTERSDR FDEA201407241939Line · leakingAFTER LOWERING THE MLG & GETTING ALL DOWN & LOCKED, ALL GREEN, RECEIVED AN ECAM ALERT OF LOSS OF GREEN SYS HYD. SECURED GREEN PUMPS PRIOR TO RED DOT. ACCOMPLISHED ALL ECAM PROCEDURES. R & R GREEN SYSTEM CASE DRAIN FILTER IAW MM 29-11-15 LEAK CHECKED OK. LISDR FDEA201407241955Line · leakingAFTER DEPARTURE, ECAM & OVERHEAD SHOWED LOSS OF GREEN HYD PRESSURE & QTY. COMPLIED WITH ECAM & QRH. CONFIGURED FOR LANDING WITH GRAVITY EXTENSION. DURING APPROACH, GREEN HYD QTY SHOWED SOME FLUID REMAINING. PUMPS OFF LESS THAN ONE MINUTE AFTER ECAM. CONSDR JIKA2014072301Hydraulic Line · leakingDURING CLIMB OUT PILOT NOTICED A DROP IN HYD PRESS ON GAUGE NEAR ZERO, ALSO NOTICED BOTH HYD FAIL ANNUNCIATOR LIGHT ILLUMINATED. PILOT DECIDED TO RETURN, PILOT PERFORMED EMER CHECKLIST ITEM THAT INCLUDED MANUALLY EXTENDING LG. PILOT LANDED WITHOUT FURTHER INSDR SWAA2014072430270Drain Line · leakingB SYS HYD LEAK, TURN OFF ALL HYD PUMPS. TIGHTENED HYD B SYS DRAIN FITTING LINE IAW SIP.SDR USAA2014072400001Hydraulic Line · leakingEN ROUTE THE GREEN HYD QTY WENT TO ZERO IN FLIGHT. DECLARED AN EMER & DIVERTED & LANDED WITHOUT INCIDENT. ACFT WAS TOWED TO THE GATE. CREW USED THE GRAVITY GEAR EXTENSION HANDLE TO EXTEND GEAR. R & R TWO HYD LINES IN THE NR 1 ENG PYLON IAW IPC 29-11-06 ITESDR SWIA201438832Hose · failedNR 2 EDP HYDRAULIC CAUTION MESSAGE. NO QUANITY OR PRESSURE. REPLACED HYD SYSTEM 2 HYDRAULIC DAMPENER HOSE.SDR F3LA2014072401049Hydraulic Line · leakingAFTER TAKEOFF GREEN HYD SYS FAILURE LOW RES & LOW HYD PRESS MESSAGES. EMER DECLARED. REPLACED FLEXIBLE HOSE FOR RT GEAR DOOR ACTUATOR, AFT HOSE IAW AMM 32-31-39 PAGE BLOCK 401.SDR MTNA201407180001Line · failedAFTER BLOCK OUT OF FLIGHT THE COPILOTS BRAKE WAS FOUND TO BE INOPERATIVE. REPLACED HYDRAULIC LINES. CHECKED GOOD & ACFT RETURN TO SERVICE.SDR 2014FA0000445Case · crackedFILTER CASE CRACKED AT THREADS.SDR CA140716015Accumulator · leaking(CAN) SHORTLY AFTER TAKEOFF THE CREW NOTICED BOTH RED HYDRAULIC ANNUNCIATORS ON SO RETURNED BACK TO THE AIRPORT. ON INITIAL CHECK THE FLIGHT CREW DISCOVERED HYDRAULIC FLUID DRIPPING FROM THE L/H NACELLE IN THE AREA OF THE HYDRAULIC POWER PACK. A MAINTENANCE CHSDR CA140717013Reservoir · leaking(CAN) DURING SERVICE, HYDRAULIC LEAK WAS DISCOVERED. IT WAS DISCOVERED THAT THE HYDRAULIC LEAK WAS COMING FROM THE DIPSTICK TUBE OF THE ALTERNATE GEAR EXTENSION RESERVOIR. THE RESERVOIR WAS ALMOST EMPTY. THIS AREA IS ALREADY SUBJECT TO SB 84-29-34 & SUBSEQUSDR CA140909005Hose · ruptured(CAN) DURING A FIRE FIGHTING MISSION, CREW EXPERIENCED AN HYDRAULIC FAILURE AND DECIDED TO ABORT THE MISSION. CREW PERFORMED THE ABNORMAL PROCEDURE "HYDRAULIC LOW PRESSURE OR LOW QTY" AND INFORMED THE TOWER DECLARING EMERGENCY. 3 MINUTES LATER, LANDING WAS PESDR NACA201407120001O-Ring · deterioratedNR 2 HYDRAULIC LOW PRESSURE LIGHT FLICKERED ON & OFF ALONG WITH MASTER CAUTION LIGHT DURING DEPARTURE. SYSTEM "A" INDICATED .5 GALLONS DURING CLIMB AND VISUAL APPROACH. FOUND O-RINGS ON ELEVATOR FEEL COMPUTER FILTER CAPS DETERIORATED. REPLACED O-RINGS ON BOSDR CA140711001Line · leaking(CAN) APPROXIMATELY 40 MINUTES AFTER TAKEOFF THE CREW REPORTED A LOSS OF THE YELLOW HYDRAULIC SYSTEM PRESSURE. AFTER DISCUSSION WITH MOC AND SOC. THE DECISION WAS MADE TO RETURN. AIRCRAFT WAS BELOW MAXIMUM LANDING WEIGHT AT TOUCHDOWN. AN EMERGENCY WAS DECLAREDSDR DXTA2014071405816Line · brokenWHEN GEAR HANDLE WAS SELECTED TO UP POSITION, AMBER HYD QTY LOW MESSAGE ILLUMINATED FOLLOWED BY THE A PUMP FAIL & PTU FAIL MESSAGES. FOLLOWED EMERGENCY CHECKLIST & RETURNED TO DEPARTURE. GEAR DID NOT RETRACT & THREE GREEN & UNSAFE LIGHTS REMAINED ON. ON PSDR SWAA2014071029841Hydraulic Line · failedB HYD QTY GAUGE SHOWED 1/2 FULL. ON APPROACH ENG 2 LOW PRESS LIGHT FLICKERED TWICE. R & R B SYS ELEC HYD PUMP PRESS LINE IAW MM.SDR MTNA070920140001Line · leakingDURING BRAKE CHECK FOR TAXI, THE LT BRAKE PEDAL ON THE COPILOTS SIDE WAS INOPERATIVE. TROUBLESHOT & A HYD LEAK WAS FOUND. THE LINE WAS REPAIRED IAW AMM 20-23-13. LEAK & OPERATIONS CHECKED GOOD IAW JIC 32-42-00 OPT 10000.SDR SWIA201438621Line · failedACFT LOST ALL FLUID IN NR 1 HYDRAULIC SYSTEM. REPLACED HYDRAULIC LINE AND NR 1 EDP IAW AMM.
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