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 ARWA20011104Hydraulic Line · leakingAFTER T/O LOST HYDRAULIC FLUID TO STAND PIPE AND PRESS 0, PERFORMED LOSS OF HYDRAULIC FLUID AND PRESS CHECKLIST AND RETURNED TO MIAMI. LANDED IN MIAMI OVERWEIGHT AT 272,600 WITHOUT INCIDENT. FOUND LT MLG BUNGEE CYLINDER PRESSURE LINE LEAKING. REMOVED AND RESDR CA011120004Control Unit · leaking(CAN) RETURNED TO YHM DUE TO LOSS OF 'A' SYS HYDRAULIC FLUID. SHORTLY AFTER TAKEOFF OUT OF YHM CREW NOTICED HYD MASTER CAUTION LIGHT HAD ILLUMIINATED, THE 'A' SYS HYDRAULIC FLUID HAD DEPLETED & THE HYDRAULIC LOW PRESSURE WARNING LIGHTS HAD ILLUMINATED. CREW SDR SABA011065Hydraulic System · contaminatedAIRCRAFT 961 ON FLIGHT 5103 FROM HICKORY TO CHARLOTTE: JUST AFTER TAKE-OFF, PILOT REPORTED THE RETRACTION OF RIGHT MAIN GEAR WAS SLOW. UPLOCK INDICATED NORMAL. AIRCRAFT LANDED IN CHARLOTTE WITH NO OTHER PROBLEM. NO EMERGENCY PROCEDURES WERE USED. MAINTENANSDR CA011116012Line · leaking(CAN) THE FLIGHT CREW NOTICED FLUID LEAKING FROM THE LEFT NACELLE DURING THEIR WALK-AROUND INSPECTION.MAINTENANCE FOUND THE "MLG DOWN PRESSURE" HYDRAULIC TUBE LEAKING FROM A PIN HOLE UNDER THE EXHAUST SHROUD. THE RIGID TUBE WAS TEMPORARILY REPLACED WITH TWO FLSDR 2003F00021Hydraulic Line · chafedSJU - FLT 7100 - BLUE SYSTEM HYDRAULIC FLUID LOSS. BLUE SYSTEM HYDRAULIC LINE CHAFED THROUGH. REPAIRED LINE WITH PERMASWEDGE IAW EMB-120 MM 20-10-0 AND A SUCCESSFUL LEAK CHECK WAS PERFORMED. (M)SDR 2001FA0000690Hydraulic Line · chafedBLUE HYDRAULIC FLUID LOSS. BLUE SYSTEM HYDRAULIC LINE CHAFFED THROUGH. REPAIRED LINE WITH PERMISSIVE IAW EMB-120 MM 20-10-01 AND A SUCCESSFUL LEAK CHECK WAS PERFORMED. (M)SDR 2001UALA02266Hydraulic Line · rupturedAIRCRAFT ARRIVED AT GATE WITH RIGHT MLG DOOR OPEN AND LEFT HYDRAULIC SYSTEM INOP. RIGHT DOWN LOCK ACTUATOR LINE LEAKING. REPLACED HOSE.SDR TSAA0129152Hydraulic Line · leakingFLT 62, HNL-OGG, THE HYDRAULIC ANNUNCIATOR CAME ON AFTER TAKEOFF. BOTH 'A' SYSTEM HYDRAULIC LOW PRESSURE LIGHTS ILLUMINATED. THE 'A' SYSTEM QUANTITY READ '0'. DECLARED EMERGENCY AND RETURNED TO HNL FOR AN UNEVENTFUL LANDING. REPLACED THE RIGHT LANDING GEARSDR CA011113003Line · severed(CAN) AFTER TAKE-OFF ONCE THE CREW SELECTED GEAR UP THEY NOTICED THAT THE NR 2 HYDRAULIC QUANTITY WAS AT O. THE A/C RETURNED TO THE DEPARTURE AIRPORT.INVESTIGATION REVEALED THAT THE MAIN PRESSURE LINE TO THE NR 2 PRESSURE MANIFOLD HAD COMPLETLY RUPTURED. A TEMSDR GAIA01313OPHydraulic Line · crackedFLT 3850 - MSP-FWA - DURING CRUISE, THE FLIGHT CREW NOTICED THAT THE 'A' SYSTEM HYDRAULIC SYSTEM WAS ISOLATED THE AIRCRAFT CONTINUED TO FWA. THE AIRCRAFT MADE AN UNEVENTFUL LANDING. INSPECTION REVEALED A CRACKED HYDRAULIC LINE AT FUSELAGE STATION 1303. THE SDR CA011211007Fitting · cracked(CAN) ELBOW HYDRAULIC FITTING CRACKED AT OUTLET PORT OF LT ELECTRICAL HYDRAULIC PUMP.SDR DHL2001364027Hydraulic Line · leakingDURING CRUISE, GREEN SYS HYD LEVEL LOW LIGHT ILLUM. MAGNETIC INDICATORS & GREEN SYS PRESS INDICATED NORM. DURING DESCENT, GREEN SYS MAGNETIC INDICATOR WENT AMBER WITH PRESS FLUCTUATING. PUMP PRESS LIGHT ILLUM. GREEN SYS PUMPS WERE TURNED ON. BLUE SYS PUMP WENSDR AUS20011178Line · damaged(AUS) HYDRAULIC LINE DAMAGED BY CONTACT FROM THE RT WING LANDING GEAR RETRACTION ACTUATOR. LOSS OF NR 4 HYDRAULIC SYSTEM FLUID.SDR AUS20011173Nut · loose(AUS) NR 1 ENGINE DRIVEN HYDRAULIC PUMP PRESSURE LINE UNION JAM NUT LOOSE AND LEAKING. INVESTIGATION FOUND THAT IT WAS CHAFED THROUGH FOR 50 PERCENT OF THE CIRCUMFERENCE ON THE JAM NUT SIDE WITH A CORRESPONDING RIDGE (FRACTURE) ON THE INSIDE. UNION IS LOCATED SDR RAIA00111003O-Ring · leaking7137-STL-GREEN HYDRAULIC SYSTEM WENT TO ZERO PSI. MAINTENANCE INSPECTED, REMOVED AND REPLACED LEAKING PRESSURE TRANSMITTER O-RING. LEAK CK OK IAW ATR MAINTENANCE MANUAL.SDR SWAA013017Hydraulic Line · cracked(AIR TURNBACK) A-SYSTEM HYDRAULIC FAILURE, PRESSURE TO ZERO, LOW PRESS LIGHT AND FEEL DIFFERENTIAL PRESSURE LIGHT ILLUMINATED. FOUND A-SYSTEM HYD PRESSURE SPOILER LINE CRACKED. REMOVED AND REPLACED LINE PER MM.SDR SWAA013009Hydraulic Line · damaged(AIR TURNBACK) A-SYSTEM HYDRAULIC FAILURE AFTER TAKEOFF AND GEAR RETRACTION. FOUND HOLE IN LT MLG RETRACT LINE. REMOVED AND REPLACED LINE, OPS AND LEAK CHECK GOOD PER MM.SDR AWXA200100564Hose · rupturedLAS - AIR TURNBACK - FLT 870 - "C" - DURING CLIMB OUT OF LAS THE # 2 ENG "B" SYSTEM HYD PRESS. LIGHT STARTED FLICKERING AND THE "B" SYSTEM HYD QUANTITY DECREASED TO 1/4 FULL. THE CREW SHUT OF THE "B" SYSTEM HYDRAULICS AND RETURNED TO LAS MAKING AN UNEVENTFUL LSDR ACE1029011Fitting · leakingON DEPARTURE, THE GEAR WARNING LIGHTS (HANDLE) CAME ON. THE GEAR WOULD NOT CYCLE WITH THE ELECTRIC PUMP. THE GEAR WAS EXTENDED WITH THE HAND PUMP. THE CREW CONTINUED THE FLIGHT AS REQUIRED TO BURN FUEL DOWN TO LANDING WEIGHT AND THE AIRCRAFT MADE AN UNEVENTSDR SWAA012945Hydraulic Line · rupturedDECLARED EMERGENCY, B SYSTEM HYDRAULIC FLUID QUANTITY STARTED DECREASING FOLLOWED BY NR 2 ENG LOW PRESSURE LIGHT ILLUMINATING. QRH FOLLOWED & LANDING ACCOMPLISHED. FOUND HYD FLEX LINE BETWEEN ACOUSTIC FILTER & MODULAR PACKAGE RUPTURED. R&R LINE, HYD PUMP & FILSDR 01FDEA00931Hydraulic System · leakingA-SYS QUANTITY DECREASING. SERVICED A-HYD SYS, NO LEAKS NOTED. OK FOR SERVICE.SDR 00005Hydraulic Line · leakingLEAK AT THE RETURN LINE TO ENGINE DRIVEN HYDRAULIC PUMP IN HELL HOLE OF AIRCRAFT.SDR AUS20011141Pipe · leaking(AUS) RT HYDRAULIC SYSTEM PRESSURE PIPE FAILED AT A BRAZED FITTING LOCATED INBOARD OF THE RT PRESSURE BULKHEAD TO PYLON.SDR PNSA11004Hydraulic Line · chafedRT HYDRAULIC LIGHT ILLUMINATED DURING CRUISE. AIRCRAFT RETURNED TO MAINTENANCE BASE WHERE HYDRAULIC PRESSURE LINE IN RT ENGINE FOR PUMP WAS FOUND CHAFED.SDR UG82001F00009Power Unit · failedVIBRATION FELT ON CABIN FLOOR AS WELL AS HUM. LT HYD (A) SYSTEM FLUCTUATED BETWEEN 2400-3300 PSI. WHEN GEAR WAS SELECTED DOWN LT HYD PRES WAS 2100 AND RT HAD AN OT (AMBER) LIGHT. UPON LANDING THEY GOT A (B) SYSTEM FAIL MESSAGE, BOTH SYSTEM PRESSURES WERE 180SDR UPS01237092Hydraulic Line · crackedINSPECTION TYPE:N/A SYSTEM A-HYDRAULIC FAILURE, QTY ZERO. FOUND NR 13 SPOILER ACTUATOR RETURN LINE CRACKED. PER GMM INSTALLED A FLEX HOSE. CHECKED CASE DRAIN FILTERS, REPLACED NR 2 HYD EDP. SERVICED SYSTEM AND OPS CHK'D GOOD. PUMPED CHANGED DUE TO BYPASS SSDR CA011031020Cylinder · cracked(CAN) DURING PRE-FLIGHT INSPECTION HYDRAULIC FLUID WAS FOUND TO BE WEEPING FROM THE NOSE GEAR TRANSFER CYLINDER. THE AREA WAS CLEANED AND DRIED. THE VISUAL INSPECTION DETERMINED THAT THE NOSE GEAR TRANSFER CYLINDER END CAP WAS CRACKED. THE SUSPECT COMPONENT WASDR CA011031009Tube · leaking(CAN) DURING TAXI TO TAKEOFF, THE FLIGHT CREW NOTICED A STRONG ACID ODOUR IN THE COCKPIT. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE DISCOVERED A LEAKING HYDRAULIC LINE IN THE NLG WHEEL WELL. THE LEAKING HYDRAULIC TUBE WAS THE "CLOSE" PRESSURE LINE TOSDR 2001F00643Hydraulic Line · leakingFLT 523 - ARRIVING FROM SVMI, AFTER LANDING INTO MIA, HYDRAULIC SYSTEM 'A' PRESSURE AND QUANTITY INDICATION DROPPED TO 0. AIRCRAFT CONTINUED TO GATE WITHOUT INCIDENT. MAINTENANCE T/S AND FOUND THE HYDRAULIC SYSTEM 'A' RETURN LINE FROM THE ENGINE NR 2 HYDRAULSDR ABXA010534Fluid · lowGEAR WOULD NOT RETRACT AFTER TAKEOFF. HYDRAULIC PRESSURE WAS 0 PSI. HYDRAULIC QUANTITY WAS NORMAL. ACCOMPLISHED LOSS OF HYDRAULICS CHECKLIST. SYSTEM OPERATED NORMALLY ON AUX PUMP. FOUND AIRCRAFT WAS BELOW STANDPIPE LEVEL. SUSPECT AIRCRAFT HYDRAULIC QUANTSDR AALA20011895Fuse · faultyDFW - FLT 1241 - AFTER TAKEOFF DFW-LAS, LEFT HYDRAULIC QUANTITY DROPPED TO .38 WITH ACCOMPANYING HYDRAULIC QUANTITY MESSAGE. RETURNED TO DFW LANDED WITHOUT INCIDENT USING ALTERNATE GEAR AND FLAP PROCEDURE. SYSTEM EXPERIENCED REPEAT OCCURRENCE OCTOBER 15, 2001SDR 2001UALA02127Hydraulic Line · shearedON LANDING ROLLOUT EICAS C HYD SYSTEM PRESSURE AND RES QTY LIGHT ILLUMINATED, LOST CENTER SYSTEM COMPLETELY, NOSEWHEEL TILLER AND FLAPS WOULD NOT RESPOND. FOUND ADP PRESSURE SUPPLY LINE IN LEFT WHEEL SHEARED OFF AT PRESSURE MODULE REF IPC 29-11-76 ITEM 592. SDR CA011101003Line · leaking(CAN) PILOTS REPORTED HYD 1 LO PRESS CAUTION MESSAGE ON IN FLIGHT. PRESSURE AND QUANTITY AT ZERO. EXECUTED APPROPRIATE CHECK LISTS. ENGINE DRIVEN PUMP RAN DRY FOR 37 MINS. REMOVED AND REPLACED NR 1 EDP IAW 29-13-00 DUE TO BEING RAN DRY. REMOVED AND REPLACED NRSDR HEEA076590Tube · crackedTUBE ASSY CRACKED. REPLACED WITH SERVICEABLE PART.SDR HEEA076565Line · crackedWHILE IN CRUISE FLIGHT, NR 1 HYDRAULIC SYSTEM FAILED. MAINTENANCE REPLACED HYDRAULIC TUBE ASSY DUE TO CRACK IN ONE OF THE CURVES.SDR UPS01837003Control Unit · failedINSPECTION TYPE:NA DEPLOYED REVERSERS IN FLIGHT (280 KIAS) TO MEET CROSSING RESTRICTION, NR 2 WOULD NOT STOW. RAN CHECKLISTS THROUGH INFLIGHT SHUTDOWN. SLOWING THROUGH 200 KIAS, REVERSER STOWED. THREE ENGINE LANDING. INFLIGHT WINDMILLING. REMOVED NR 2 ENGISDR CA011031008Line · ruptured(CAN) DURING CLIMB (4,000 FT) NR 1 ENGINE HYDRAULIC PUMP CAUTION LIGHT AFTER 10 SECONDS FURUTHER NR 1 HYD ISO VLV AND THEN ROLL SPLR AND NR 1 RUD HYD CAUTION LIGHT. FLAP PWR FAILURE. QRH APPLIED. SYSTEM NR 1 AND STANDBY INDICATING ZERO RETURNED FOR FLAPLESS LASDR CA011031010Tube · leaking(CAN) THE FLIGHT CREW REPORTED THAT THE NR 2 ENGINE DRIVEN PUMP CAUTION LIGHT CAME ON DURING LANDING GEAR EXTENSION. MAINTENANCE DISCOVERED THE NR 2 HYDRAULIC SYSTEM HAD AIR IN IT AND ALSO THE NR 2 SPOILER LIFT DUMP PRESSURE LINE BETWEEN THE LIFT DUMP VALVES WSDR ABXA010529Hydraulic System · lowTHE GENERAL HYDRAULIC SYSTEM NEEDED SERVICED. THE SYSTEM INDICATED ZERO DURING APPROACH AND LANDING. MAINTENANCE SERVICED THE GENERAL HYDRAULIC SYSTEM IAW DC-8 MAINTENANCE MANUAL.SDR AWXA200100516O-Ring · failedPHX - AIR TURNBACK - FLT 882 - 30 MIN INTO FLT. CREW RECEIVED CLASS 1 ECAM YELLOW HYD LOW LEVEL, WITH ASSOCIATED ECAM INDICATION OF NO RESERVOIR FLUID IN YELLOW SYSTEM. CREW FOLLOWED ECAM PROCEDURES AND RETURNED TO PHX MAKING AN UNEVENTFUL LANDING. EMERGENCY ESDR UG82001F00008Hydraulic System · malfunctionedVIBRATION FELT ON CABIN FLOOR AS WELL AS HUM. LEFT HYDRAULIC (A) SYSTEM FLUCTUATED BETWEEN 2400-3300 PSI. WHEN GEAR WAS SELECTED DOWN LEFT HYDRAULIC PRESSURE WAS 2100 AND RIGHT HAD AN OT(AMBER) LIGHT. UPON LANDING THEY GOT A (B) SYSTEM FALL MESSAGE, BOTH SYSSDR CA011003017Line · cracked(CAN) A/C MADE NORMAL APPROACH & LDG. DURING 180 DEG TURN TO CLEAR RWY, CREW NOTED FLUX IN HYDRAULIC NOSEWHEEL STEERING SYS, BUT TAXIIED IN & SHUTDOWN WITH NO PROBLEMS. ON EXITING A/C, CREW NOTICED SMALL AMOUNT HYDRAULIC FLUID ON GROUND UNDER LT ENGINE FIREWALSDR AUS20011044Line · cracked(AUS) LANDING GEAR HYDRAULIC DOWNLINE, PRESSURE SIGNAL LINE FLARE IS CRACKED AT ATTACHMENT TO PRESSURE GAUGE.SDR SWIA200110205Hydraulic Line · leakingHYD 1 LO PRESS MESSAGE ON INFLIGHT. QUANTITY AND PRESSURE AT 0. EXECUTED APPROPRIATE CHECK LISTS. DIVERTED TO GJT. ENGINE DRIVEN PUMP RAN DRY FOR 37 MINUTES. REMOVED AND REPLACED NR 1 HYDRAULIC ENGINE DRIVEN PUMP IAW 29-13-00 DUE TO BEING RAN DRY. REMOVED SDR SWIA200110219Manifold · leakingHYDRAULIC SYSTEM NR 3 LOST ALL FLUID. FOUND NR 3 PRESSURE MANIFOLD ASSEMBLY LEAKING. REMOVED AND REPLACED NR 3 HYDRAULIC PRESSURE MANIFOLD ASSEMBLY IAW CRJ MM 29-11-05. OPS CHECK GOOD, LEAK CHECK GOOD. P/N OFF: ADA686-301 S/N OFF: 1580SDR 2001FA0000343Line · failedLEFT HYDRAULIC PRESSURE LINE FROM ENGINE TO HYDRAULIC MANIFOLD BROKE AT FLARE. 3 MILE FINAL EMPTIED HYDRAULIC RES INTO EQUIPMENT BAY/BAGGAGE COMPT. LINE REMOVED AND SENT TO MFG FOR EVALUATION. NOTE: RIGHT HYDRAULIC PRESSURE LINE REMOVED AND REPLACED AS WELSDR AWXA200100476Packing · brokenLAX - ABORTED APPROACH - FLT 37 - "C" - ON FINAL APPROACH ECAM INDICATED YELLOW HYDRAULIC SYSTEM LOW PRESSURE, SYSTEM FLUID DEPLETED AND THE CREW PERFORMED A GO AROUND. THE SUBSEQUENT APPROACH AND LANDING WAS UNEVENTFUL. MAINTENANCE INSPECTED THE AIRCRAFT ANDSDR WD42002F00001Tube · corrodedSHORTLY AFTER AIRCRAFT DEPARTURE, THE PILOT SMELLED HYDRAULIC FLUID IN COCKPIT. DECISION WAS MADE TO DIVERT BACK TO AIRPORT. WHEN CYCLING GEAR DOWN, AN UNSAFE CONDITION WAS INDICATED AND GEAR WAS PLACED IN DOWN POSITION BY EMERGENCY PROCEDURES AND LANDED WITSDR CA011105003Line · leaking(CAN) DURING RUN UP THE SUBJECT LINE STARTED LEAKING, THIS WAS REPORTED BY PASSENGERS IN AIRCRAFT WHO NOTICED HYDRULIC FLUID LEAKING INTO CABIN FROM OVERHEAD.AIRCRAFT WAS SHUT DOWN AND THE AME LOCATED THE LEAKING LINE ON NR 2 HYDRAULIC SYSTEM. THIS LINE WAS LASDR CA011004006Line · leaking(CAN) AFTER A MAINTENANCE RUN, THE ENGINEER NOTICED A HYDRAULIC LEAK FROM THE LEFT WHEEL WELL. UPON FURTHER INVESTIGATION, IT WAS DETERMINED THAT THE LEAK WAS COMING FROM THE MLG DOWN PRESSURE LINE (RIGID TUBE) IN THE LEFT NACELLE DUE TO A PIN HOLE IN THE TUBE
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