N115AX

Service difficulty reports · 18

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 n_number = 'N115AX'
  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.

SDR YADA20230313002Bellcrank · crackedWHILE PERFORMING A COMPANY FLEET CAMPAIGN DISCOVERED FORWARD ELEVATOR BELLCRANK CRACKED WEB.Mar 4, 2023 · N115AX · Beech 1900C · Elevator Control SystemSDR YADA20210817201Housing · erodedPILOT REPORTED "OIL LEAKING FROM RIGHT ENGINE" - MAINTENANCE FOUND OIL LEAK TO BE COMING FROM THE ENGINE OIL SCAVENGE PUMP HOUSING. REPLACED HOUSING. FOUND CAVITATION EROSION THROUGH CASTING.Aug 12, 2021 · N115AX · Beech 1900C · Turbine Engine Oil SystemSDR YADA2019043029002Actuator · failedMAINTENANCE REPORTED: WHILE HAND PUMP CYCLING LANDING GEAR AFTER R/H MAIN LANDING GEAR ACTUATOR REPLACEMENT, R/H MAIN GEAR WILL NOT COME DOWN.Apr 29, 2019 · N115AX · Beech 1900C · Landing Gear ActuatorSDR YADA2019043029001Actuator · malfunctionedPILOT REPORTED: ON APPROACH PUT LANDING GEAR DOWN. LEFT MAIN AND NOSE GEAR CAME DOWN. PUMP STOPPED WORKING HAD AN INTRANSIT LIGHT AND RIGHT MAIN NEVER CAME DOWN. 20 SECONDS LATER PUMP STARTED WORKING INTRANSIT LIGHT WENT OUT AND RIGHT MAIN CAME DOWN. MAINTENANApr 29, 2019 · N115AX · Beech 1900C · Landing Gear ActuatorSDR YADA20180105001Scavenge Pump · leakingMAINTENANCE DISCOVERED THAT THE NR 1 ENGINE HAD AN OIL LEAK AT THE SCAVENGE PUMP HOUSING– THE PUMP WAS LEAKING THROUGH THE CASTING. THIS IS THE THIRD SUCH FAILURE OF THIS PART IN ONE YEAR FOR US.Jan 5, 2019 · N115AX · Beech 1900C · Turbine Engine Oil SystemSDR YADA2018111409011Bearing · seizedCOMPONENT TEAR DOWN FINDINGS: BLOWER MOTOR END CAP BEARING P/N:M4000AC-3, FAILED INTERNALLY, CAUSING HIGH MOTOR DRAG AND HEAT BUILDUP. HEAT SINK RESISITORS, WIRE TERMINALS AND NOISE SUPPRESSORS SHOWED HIGH HEAT AREAS (MOST LIKELY DUE TO HIGH CURRENT DRAW FROM Nov 7, 2018 · N115AX · Beech 1900C · Air Distribution FanSDR YADA20181109001Blower Motor · seizedPILOTS REPORTED A STRONG SMELL OF ELECTRICAL FUMES IN THE COCKPIT AND THAT O2 MASKS WERE USED. AIRCRAFT LANDED AS SCHEDULED IN DILLINGHAM. MAINTENANCE WAS DISPATCHED TO (DLG) AND FOUND THAT THE AFT VENT BLOWER BEARING SEIZED. THE VENT BLOWER WAS REMOVED AND RENov 7, 2018 · N115AX · Beech 1900C · Air Distribution FanSDR YADA20161014001Seal · debondedPILOT REPORTED WITH ENG BLEEDS OFF AND VENT ON HIGH, THE ODOR OF BURNING OIL/FUMES FILLED THE COCKPIT. PILOT HAD PREVIOUSLY REPORTED THAT THE AIRCRAFT WOULD NOT PRESSURIZE WITH BLEEDS ON UNLESS TEMPERATURE SWITCH WAS HELD IN INCREASE & COCKPIT WAS EXTREMELY WAOct 14, 2016 · N115AX · Beech 1900C · Emergency ExitsSDR YADA20160809001Rudder Pedal · frozenPILOT REPORT RUDDER PEDALS FROZEN AT ALTITUDE WITH YAW DAMP OFF. MAINTENANCE DISCOVERED AND REMOVED ICE AND WATER UNDER FLOOR BOARDS, CLEANED AND INSPECTED, OPS CHECKED GOOD.Aug 9, 2016 · N115AX · Beech 1900C · Rudder Control SystemSDR YADA20160504001Skin Panel · debondedPOST LANDING INSPECTION REVEALED THAT THE NR 1 ENG HAD A SEPARATION OF PN 114-980077-17 SKIN FROM THE PN 114-980077-5 BOND ASSEMBLY & WAS NO LONGER ATTACHED TO THE ACFT. MX VERIFIED THAT ALL BOND ASSEMBLY FASTENERS WERE IN PLACE & THAT THE FAILURE WAS THE BONMay 4, 2016 · N115AX · Beech 1900C · Nacelle/Pylon, Plate/SkinSDR YADA20160422001Printed Ckt Board · failedIN FLIGHT, AFTER LG HAD BEEN RETRACTED & STOWED, THE LG RELAY CB POPPED. THE LG HANDLE WAS SELECTED DOWN & CB PUSHED IN, CB POPPED AGAIN. MANUAL GEAR EXTENSION WAS THEN ACHIEVED. FOUND THE LG PUMP MOTOR BURNED. THE MOTOR WAS REPLACED AS WELL AS THE SUSPECTApr 22, 2016 · N115AX · Beech 1900C · Landing Gear Retraction/Extension SystemSDR YADA2015122201Connector · corrodedHAD TO PUMP GEAR DOWN TO GET THREE GREEN, NOSE GEAR HAD NOT INDICATED GREEN. NO IN-TRANSIT LIGHT. FERRY GEAR DOWN. MX COULD NOT DUPLICATE. GEAR RETRACT & EXTEND, OPERATIONS CHECKED GOOD MULTIPLE TIMES. REPLACED NOSE GEAR DRAG BRACE DOWN LOCK SWITCH FOR CODec 22, 2015 · N115AX · Beech 1900C · Landing Gear System WiringSDR YADA20150819001Turbine Blades · damagedWHILE INVESTIGATING RISING ENG ITT TREND, FOUND SIGNIFICANT DAMAGE TO COMPRESSOR SHROUD SEGMENTS & CT BLADES. CAUSE OF DAMAGE APPEARS TO BE FROM EXCESSIVE CARBON BUILD UP ON THE COMBUSTION LINER COMING LOOSE & ABRADING SEGMENTS & CT BLADES TO THE POINT THE SEAug 19, 2015 · N115AX · Beech 1900C · Turbine SectionSDR YADA20140819001Vsi · failedWHILE TAXIING TO REPOSITION ACFT, FLIGHT CREW REPORTED SMELLING & SEEING SMOKE FROM THE INSTRUMENT PANEL. THE ACFT RETURNED TO THE RAMP WITHOUT INCIDENT. PERFORMED A GND RUN ON THE ACFT & OBSERVED THE COPILOTS ELECTRONIC VSI INDICATOR SCREEN FLICKER & THEN WAug 19, 2014 · N115AX · Beech 1900C · Rate of Climb IndicatorSDR YADA20140312001Downlock Switch · inoperativePIREP, RED GEAR HANDLE LIGHT ILLUMINATES WITH GEAR DOWN & HANDLE DOWN. REPLACED NOSE GEAR DOWN LOCK SWITCH AFTER UNEVENTFUL LANDING AT ORIGINATING AIRPORT.Mar 10, 2014 · N115AX · Beech 1900C · Landing Gear Position and WarningSDR YADA201201170001Wire Harness · corrodedON CLIMB OUT, THE PILOT RETRACTED THE LANDING GEAR BUT THE RED "GEAR INTRANSIT LIGHT" IN THE LANDING GEAR SELECTOR HANDLE NEVER EXTINGUISHED. THE GEAR WAS EXTENDED AND THE ACFT WAS LANDED AND RETURNED TO BASE. MX PERSONNEL FOUND THE A CONNECTOR PLUG AND WIRIJan 17, 2012 · N115AX · Beech 1900C · Landing Gear System WiringSDR YADA100708Line · rupturedPILOT REPORTED LEFT BRAKE "FLAT". REPLACED SEEPING FLEXIBLE BRAKE LINE - DATE CODE 2Q06.Oct 7, 2008 · N115AX · Beech 1900C · Landing Gear Brake SystemSDR YAD2008F00003Brake Sys · weakPILOT REPORTED LT BRAKE FLAT ON TAXI AND LANDING. MX BLEED BRAKES.Sep 20, 2008 · N115AX · Beech 1900C · Landing Gear Brake System
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