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 AU981238Pipe · worn(AUS) FLAP SYSTEM HYDRAULIC PIPE WORN THROUGH AND LEAKING DUE TO RUBBING ON AN AIR CONDITIONING DUCT MARMON CLAMP. PIPE IS LOCATED IN THE WING ROOT AREA. PART TC: 10,846SDR DLM88981968Hose · leakingA/C LOST RT HYD PRESSURE AND FLUID, USED EMERGENCY PROCEDURES. REPLACED RT ENGINE HYD PUMP MAIN PRESSURE LINE.SDR C2XA98IA372Pump · failedIAH - FLT 3828 - THE CREW REPORTED THAT THE NOSE LANDING GEAR WAS SLOW TO RETRACT. THE AIRCRAFT RETURNED TO IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE GREEN SYSTEM A/C WILD HYDRAULIC PUMP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVISDR CALA9801831Line · leakingTHE A-SYSTEM HYDRAULIC QUANTITY AND PRESSURE WAS LOST AFTER TAKEOFF. A MANUAL GEAR EXTENSION WAS ATTEMPTED. THE NOSE GEAR DID NOT EXTEND ON FIRST PULL OF HANDLE. THE HANDLE WAS PULLED AGAIN AND THE GEAR EXTENDED BUT NOSE EXTENSION CABLE WOULD NOT RETRACT FUSDR 98ZZZX4041Valve · leakingHNL/NAN - DURING CRUISE, NR 3 SYSTEM HYDRAULIC QUANTITY DECREASED IN-FLIGHT. ON ARRIVAL NAN, NR 3 SYSTEM FLIGHT CONTROL SOV FOUND UNSERVICEABLE. PART REPLACED AND AIRCRAFT RELEASED TO SERVICE.SDR DLM88981928Line · leakingLEFT HYD SYS QTY WENT TO ZERO. PRESS WENT TO ZERO. FOUND LT SYSTEM SUPPLY LINE LEAKING. PERMASWAGED LINE.SDR DL73K981927Line · leakingHYD LEAK A-SYS TOTAL LOSS. FOUND LEAK NR 1 ENG. REPLACED HYD PUMP PRESS AND CASE DRAIN LINES. REPLACED HYD PUMP AS PRECAUTION. CHECKED CASE DRAIN FILTER FOR CONTAMINATION, NONE FOUND. REPLACED SAME. SERVICED SYS RAN ENGS AND FLT CONTROLS TO BLEED. ALL CKSDR CA980928014Line · chafed(CAN) DURING FLIGHT, THE PORT HYDRAULIC FLOW LIGHT CAME ON FOLLOWED BY THE STANDBY LIGHT. EMERGENCY DECLARED AND A SAFE LANDING CARRIED OUT. PORT HYDRAULIC PUMP LINE CHAFED THROUGH ON THE EDGE OF THE GENERATOR BRUSH COVER ALLOWING A MASSIVE HYDRAULIC LEAK. SDR 98FDEA00577Line · splitSYS-A HYD FAILURE 5 MIN AFTER T/O QUAN AND PRESS ZERO. FLUID SHUTOFF SWITCH CLOSED. FOUND HYD LINE SPLIT ON A-SYS PRESS TRANSMITTER. REMOVED AND REPLACED SAME. NOTED 1 GAL FLUID IN A-SYS SERVICE TO FULL, RAN BOTH NR 1 AND NR 2 ENG. ALL SYS OPER CK NORM. SDR CA980928013Plug · cracked(CAN) AFTER TAKEOFF, THE LANDING GEAR FAILED TO RETRACT WHEN SELECTED UP. AFTER THE UP SELECTION THE HYDRAULIC PRESSURE WAS SEEN TO FAIL. AIRCRAFT RETURNED TO BLOCKS. INVESTIGATION REVEALED THAT A MANIFOLD BLANKING PLUG HAD CRACKED UNDER THE HEAD AND ALLOWSDR 98ZZZX3605Tube · leakingFOLLOWING LANDING, PILOT NOTED HYDRAULIC LEAK FROM NOSE BAY AREA. DEFECT REPORTED. EXAMINATION REVEALED LEAK TO ORIGINATE FROM TUBE ASSY. SUBMITTER STATED CAUSE WAS CHAFING OF PIPE BY NOSE WHEEL DOOR ACTUATING ROD. DIFFICULT TO LOCATE DUE TO PROXIMITY OF SSDR USAASB98236Hydraulic System · req'd serviceMCO - FLT 2299 - APPROXIMATELY 20 MINUTES OUT FROM MCO, THE 'A' SYSTEM HYDRAULIC PUMP LOW PRESSURE LIGHT AND THE 'A' SYSTEM FLIGHT CONTROL LOW PRESSURE LIGHT ILLUMINATED WITH ZERO QUANTITY ON GAUGE. FLIGHT LANDED WITHOUT INCIDENT AT MCO AND TAXIED TO THE GATESDR CALA9801671Hyd Line · puncturedTHE NR 2 HYDRAULIC SYSTEM QUANTITY AND PRESSURE WAS LOST ON APPROACH TO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A HOLE IN HYDRAULIC PRESSURE LINE TO LEFT HYDRAULIC PUMP AND THE RIGHT PUMP WAS LEAKING HYDRAULIC FLUID OUT DRAIN MAST. THE SDR CALA9801670Hyd Line · leakingTHE A HYDRAULIC SYSTEM WAS LOST ON FINAL APPROACH TO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE A SYSTEM HYDRAULIC PRESSURE LINE IN AFT AIRSTAIRS TO FIREWALL LEAKING. THE HYDRAULIC PRESSURE LINE WAS REMOVED AND REPLACED. TSDR DLL17981855Hyd Line · leakingHYDRAULIC SYSTEM-B LOW QTY LIGHT CAME ON IN FLIGHT. QUANTITY INDICATED LESS THAN QUARTER FULL. FOUND RT O/B AILERON ACTUATOR PRESSURE LINE LEAKING AT ANGULAR SEAL PLATE (P/N 277203191). REPLACED SEAL, SERVICED HYDRAULICS AND LEAK CHECKS SATISFACTORY.SDR AU981142Pipe · leaking(AUS) LANDING GEAR EMERGENCY VALVE FORWARD PIPE LEAKING FLUID FROM A PIN HOLE IN A CURVED SECTION OF THE PIPE. LOSS OF HYDRAULIC FLUID. PART TC: 3,439.SDR MASA98179Connector · failedFLT 4446 - MTJ-PHX - DURING CLIMB-OUT FROM MTJ, THE MASTER CAUTION ILLUMINATED, AND THE CAUTION PANEL INDICATED NR 2 ENGINE HYDRAULICS. CREW DECLARED AN EMERGENCY AND DIVERTED TO GTJ. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND REMOVED ANDSDR VTZA98282Line · chaffedFLT 6548 - CLE-IAD - DURING LANDING, AIRCRAFT MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS ALL HYDRAULIC PRESSURE DROPPED TO ZERO. MAINTENANCE INSPECTED AND REMOVED AND REPLACED TWO HYDRAULIC LINES IN LEFT LEADING EDGE OF WING, OPS CHECK OK. AIRCRSDR TAOA099803Modular Unit · leakingLGA-DCA - FLT 6451 - 'A' HYDRAULIC SYSTEM FAILURE IN FIGHT AFTER FLAP RETRACTION. FOUND 'A' SYSTEM MODULAR UNIT LEAKING DUE TO CRACKED FITTING REPLACED MODULE. REPLACED 1 AND 2 HYDRAULIC PUMPS, CASE DRAIN RETURN AND PRESSURE FILTERS. SERVICED HYDRAULIC SYSTSDR HEEA0015965Valve · stickingHYDRAULIC VALVE STICKS.SDR 98ZZZM807Line · chaffedFLT 6548 - CLE-IAD - DURING LANDING, AIRCRAFT MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS ALL HYDRAULIC PRESSURE DROPPED TO ZERO. MAINTENANCE INSPECTED AND REMOVED AND REPLACED TWO HYDRAULIC LINES IN LEFT LEADING EDGE OF WING, OPS CHECK OK. AIRCRSDR PNSA980906Line · splitON PREFLIGHT FOR NEXT LEG, FOUND HYDRAULIC FLUID LEAKING FROM RT ENGINE. FOUND SPLIT HYDRAULIC LINE IN RT NACELLE. REPLACED LINE.SDR CALA9801616Flex Line · failedTHE A HYDRAULIC SYSTEM WAS LOST AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A HOLE IN ELEVATOR LEFT PCU PRESSURE FLEX LINE. THE FLEX LINE WAS REMOVED AND REPLACED. IN ADDITION, THE NR 2 ENGINSDR TWAA9814102Fuse · failedTHE RT HYD SYSTEM FAILED DURING GEAR RETRACTION AFTER TAKEOFF. COMPLETE FLUID LOSS FROM RT SIDE. RT HYD PUMP LATER FAILED. FLT RETURNED TO STL. REPLACED NR 3 BRAKE HYD FUSE LIMITER AS INITIAL CAUSE. CHECK-C 3-16-98 MCI.SDR CALA9801598Hyd Line · leakingTHE RT HYDRAULIC PRESSURE LOW LIGHT AND MANUAL RUDDER CONTROL LIGHT ILLUMINATED DURING CLIMB OUT OF ANC. THE RT HYDRAULIC PUMP PRESSURE WAS ZERO WITH QUANTITY DECREASING. THE HYDRAULIC QUANTITY LOSS CHECKLIST WAS ACCOMPLISHED AND THE AIRCRAFT LANDED AT SEA WSDR AALA981599Valve · malfunctionedLHR - FLT 67 - AFTER TAKEOFF LHR EN ROUTE TO ORD WITH GEAR HANDLE UP, CENTER PRESSURE DROPPED TO 690 PSI. GEAR WOULD NOT RETRACT, GOT GEAR DOORS AND TAIL SKID LIGHTS. RETUREND AND LANDED LHR OVERWEIGHT AT 346,000 LBS. LANDED WITHOTU INCIDENT. FOUND HYDRAULSDR CALA9801588Hyd Line · leakedSMOKE APPEARED IN THE CABIN AFTER TAKEOFF AND BEGAN CLEARING WITHIN 2-3 MINUTES. THE SMOKE HAD COMPLETELY DISSIPATED WITHIN 10-15 MINUTES. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A HYDRAULIC LINE IN THE AFT CARGO COSDR CA980916012Hydraulic Sys · contaminated(CAN) AFTER TAKEOFF, THE LANDING GEAR SYSTEM WOULD NOT RETRACT. AIRCRAFT RETURNED OK. INSPECTION FOUND AIR IN BOTH HYDRAULIC SYSTEMS. POSSIBLY FLIGHT DECK INHIBIT HANDLE NOT COMPLETELY CLOSED.SDR VTZA98276Hose · looseFLT 6348 - IAD-GSO - DURING LANDING, MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH LT HYDRAULIC PRESSURE INTERMITTENT. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND TIGHTENED DOWN LINE TO RADIUS ROD. OPS CHECK OK. AIRCRAFSDR 98UAL900431Line · leakingDIVERTED TO JFK WHEN THE HYDRAULIC SYSTEM-B FAILED. *S/D* REMOVED AND REPLACED LEAKING HYD SYSTEM-B LINE AND FILTERS. LEAK CHECKS GOOD.SDR HEEA0015810Line · dentedDENT IN LINE.SDR AU981089Hose · deteriorated(AUS) LEFT MAIN LANDING GEAR EXTENSION HYDRAULIC HOSE DETERIORATED AND HOLED. LOSS OF HYDRAULIC FLUID. PART TC: 7.941.SDR 98ZZZX4015Hose · failedTHE LEFT ENGINE NR 6 HIGH PRESSURE TEFLON HOSE SPLIT CAUSING AIRCRAFT TO LOSE HYDRAULIC PRESSURE. SUBMITTER SUGGESTED FAULTY HOSE AS CAUSE OF FAILURE.SDR 98ZZZX3553Hose · failedTHE AIRCRAFT EXPERIENCED A TOTAL HYDRAULIC FAILURE IN-FLIGHT. THE PILOT MADE AN EMERGENCY LANDING WITHOUT INCIDENT. THE HYDRAULIC SYSTEM WAS INSPECTED AND IT WAS DETERMINED THAT THE SUCTION LINE FROM THE RESERVOIR TO THE HYDRAULIC PUMP HAD FAILED INTERNALLY.SDR K3HA980099Line · leakingNO A-HYDRAULIC SYSTEM PRESSURE DUE TO NR 1 AND NR 2 ENGINE HYDRAULIC PUMP FAILURE. NO FLUID LOSS. GEARS MANUALLY EXTENDED. LUGGAGE RACK INHIBITED MANUAL GEAR EXTENSION. FOUND LEAKING NR 1 ENGINE HYDRAULIC PUMP PRESSURE LINE AND FIRE WALL COUPLING. REPLACESDR DL733981732Line · puncturedEN ROUTE EXPERIENCED TOTAL HYD SYS-B FAILURE CONTACTED ATL. MTC AND DISPATCH ADVISED LANDING IN LAS. T/S B-HYD SYS FOUND PIN HOLE IN FLEX HOSE FROM PUMP TO PRESS MODULE. INSTALLED APPROVED INTERIM HYD HOSE.SDR COA9860245Line · leakingNR 3 HYDRAULIC SYSTEM FAILED DURING FLIGHT. REPLACED LEAKING BALL ATTENUATOR LINE ON PUMP 3A.SDR 99ZZZX2702Bracket · crackedLEFT WING TE HYDRAULIC LINE CLAMP BRACKET CRACKED AT RIB 5. REPLACED BRACKET.SDR 99ZZZM560Bracket · crackedLEFT WING TE HYD LINE CLAMP BRACKET CRACKED AT RIB 5. REPLACED BRACKET. (M)SDR CALA9801488Hyd Line · leakingTHE AIRCRAFT HAD ASSYMETRIC LOCKOUT BETWEEN FLAPS 2 AND 5 ON APPROACH TO IAH. THE ALTERNATE FLAP SYSTEM WAS USED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FLAP HYDRAULIC LINE LEAKING IN LT FORWARD AIR CONDITIONING BAY. THE HYDRAULIC LINE WASDR SCNA98090Line · rupturedAFTER DEPARTURE LOSS OF A SYSTEM HYDRAULIC QUANTITY UPON GEAR RETRACTION. PERFORMED ALL COM PROCEDURES AND DUMPED FUEL. RETURNED TO MSP. FOUND RUPTURED LINE ON ELEVATOR ACCESSORY. REMOVED AND REPLACED LINE WITH FOLLOWING LEAK AND OPERATIONAL CHECKS GOOD.SDR 99ZZZM484Bracket · crackedRIGHT WING TE TOP HYDRAULIC LINE CLAMP BRACKET CRACKED RIB NR 6. REMOVED AND REPLACED BRACKET. (M)SDR 99ZZZM475Bracket · crackedRIGHT WING TE LOWER HYDRAULIC LINE BRACKET CRACKED AT RIB NR 5. REMOVED BRACKET AND FABRICATED NEW BRACKET PER DRAWING HC9 32H0211. INSTALLED BRACKET AND ATTACHED LINES TO BRACKET. (M)SDR 98ZZZX3849Hose · rupturedAIRCRAFT LOST HYDRAULIC POWER TO FLIGHT CONTROLS DUE TO RUPTURED RT CYCLIC SERVO FLEX LINE. LINE SUPPLIES HYDRAULIC FLUID TO AFT END OF SERVO. IMPROPER ASSY OF FITTING TO HOSE IS SUSPECTED.SDR 98ZZZX3826Hose · rupturedAIRCRAFT LOST HYDRAULIC POWER TO FLIGHT CONTROLS DUE TO RUPTURED RIGHT HAND CYCLIC SERVO FLEX LINE. LINE SUPPLIES HYDRAULIC FLUID TO AFT END OF SERVO. IMPROPER ASSEMBLY OF FITTING TO HOSE IS SUSPECTED. REF: QUALITY AVIATION SERVICES, R/S QS7R937J.SDR 98FDEA00501Hydraulic Line · ruptured98-202 - LOST 'B' SYS HYD QUANTITY AND PRESSURE ON TAKEOFF. INSPECTED AND FOUND NR 1 'B' PUMP PRESS LINE RUPTURED. REMOVED AND REPLACED LINE WITH NEW ALT LINE PER ENG AUTH 7-2914-38376. OPERATION AND LEAK CHK GOOD PER B-727 M/M 29-12-0.SDR UPS98227394Hose · rupturedIN FLIGHT, 'B' HYD SYS QUANTITY SHOWED 0, AND NR 2 PUMP LOW PRESS LIGHT ILLUMINATED, AOM PROCEDURES ACCOMPLISHED, 10 MIN LATER, NR 1 B PUMP LOW PRESS LITE ILLUMINATED ALONG WITH 'B' SYS RUDDER AND ELEVETOR LIGHTS AND ELEV FEEL DRIFT LIGHT, AOM ACCOMPLISHED, AFSDR ABXA9800734Hyd Hose · rupturedON TAKEOFF FROM ILN, LOST ALL HYDRAULIC PRESSURE. UNABLE TO RAISE FLAPS. RETURNED TO ILN. REPLACED RIGHT BOGIE TRIM HYDRAULIC LINE. LEAK CHECKED GOOD IAW DC8 MM.SDR SWIA971229Filter · dirtyGREEN HYDRAULIC FILTER LIGHT CAME ON AFTER TAKEOFF. RETURNED TO SLC. REPLACED GREEN SYSTEM PRESSURE AND RETURN FILTERS. NO VISIBLE CONTAMINATION FOUND (RETURN PIN WAS POPPED). RAN BOTH HYDRAULIC SYSTEMS 15 MINUTES AND ALL CHECKS GOOD.SDR CALA9801416B Nut · leakingTHE RT HYDRAULIC SYSTEM FLUID QUANTITY DROPPED TO 1.5 QUARTS ON CLIMB-OUT OF DCA EN ROUTE TO EWR. THE RIGHT PUMP AND AUX PUMP WERE TURNED OFF. THE GEAR WAS MANUALLY EXTENDED AND THE AIRCRAFT LANDED AT EWR WITH GEAR DOORS OPEN. THE RIGHT GEAR DOOR SUSTAINED
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