# Service difficulty reports: N115AX A list on [N115AX](https://openairdocs.org/aircraft/N115AX.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR YADA20230313002](https://openairdocs.org/sdr/YADA20230313002.md): Bellcrank · cracked · Mar 4, 2023 · N115AX · Beech 1900C · Elevator Control System > WHILE PERFORMING A COMPANY FLEET CAMPAIGN DISCOVERED FORWARD ELEVATOR BELLCRANK CRACKED WEB. - [SDR YADA20210817201](https://openairdocs.org/sdr/YADA20210817201.md): Housing · eroded · Aug 12, 2021 · N115AX · Beech 1900C · Turbine Engine Oil System > PILOT 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. - [SDR YADA2019043029002](https://openairdocs.org/sdr/YADA2019043029002.md): Actuator · failed · Apr 29, 2019 · N115AX · Beech 1900C · Landing Gear Actuator > MAINTENANCE REPORTED: WHILE HAND PUMP CYCLING LANDING GEAR AFTER R/H MAIN LANDING GEAR ACTUATOR REPLACEMENT, R/H MAIN GEAR WILL NOT COME DOWN. - [SDR YADA2019043029001](https://openairdocs.org/sdr/YADA2019043029001.md): Actuator · malfunctioned · Apr 29, 2019 · N115AX · Beech 1900C · Landing Gear Actuator > PILOT 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. MAINTENAN - [SDR YADA20180105001](https://openairdocs.org/sdr/YADA20180105001.md): Scavenge Pump · leaking · Jan 5, 2019 · N115AX · Beech 1900C · Turbine Engine Oil System > MAINTENANCE 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. - [SDR YADA2018111409011](https://openairdocs.org/sdr/YADA2018111409011.md): Bearing · seized · Nov 7, 2018 · N115AX · Beech 1900C · Air Distribution Fan > COMPONENT 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 - [SDR YADA20181109001](https://openairdocs.org/sdr/YADA20181109001.md): Blower Motor · seized · Nov 7, 2018 · N115AX · Beech 1900C · Air Distribution Fan > PILOTS 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 RE - [SDR YADA20161014001](https://openairdocs.org/sdr/YADA20161014001.md): Seal · debonded · Oct 14, 2016 · N115AX · Beech 1900C · Emergency Exits > PILOT 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 WA - [SDR YADA20160809001](https://openairdocs.org/sdr/YADA20160809001.md): Rudder Pedal · frozen · Aug 9, 2016 · N115AX · Beech 1900C · Rudder Control System > PILOT 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. - [SDR YADA20160504001](https://openairdocs.org/sdr/YADA20160504001.md): Skin Panel · debonded · May 4, 2016 · N115AX · Beech 1900C · Nacelle/Pylon, Plate/Skin > POST 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 BON - [SDR YADA20160422001](https://openairdocs.org/sdr/YADA20160422001.md): Printed Ckt Board · failed · Apr 22, 2016 · N115AX · Beech 1900C · Landing Gear Retraction/Extension System > IN 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 SUSPECT - [SDR YADA2015122201](https://openairdocs.org/sdr/YADA2015122201.md): Connector · corroded · Dec 22, 2015 · N115AX · Beech 1900C · Landing Gear System Wiring > HAD 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 CO - [SDR YADA20150819001](https://openairdocs.org/sdr/YADA20150819001.md): Turbine Blades · damaged · Aug 19, 2015 · N115AX · Beech 1900C · Turbine Section > WHILE 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 SE - [SDR YADA20140819001](https://openairdocs.org/sdr/YADA20140819001.md): Vsi · failed · Aug 19, 2014 · N115AX · Beech 1900C · Rate of Climb Indicator > WHILE 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 W - [SDR YADA20140312001](https://openairdocs.org/sdr/YADA20140312001.md): Downlock Switch · inoperative · Mar 10, 2014 · N115AX · Beech 1900C · Landing Gear Position and Warning > PIREP, RED GEAR HANDLE LIGHT ILLUMINATES WITH GEAR DOWN & HANDLE DOWN. REPLACED NOSE GEAR DOWN LOCK SWITCH AFTER UNEVENTFUL LANDING AT ORIGINATING AIRPORT. - [SDR YADA201201170001](https://openairdocs.org/sdr/YADA201201170001.md): Wire Harness · corroded · Jan 17, 2012 · N115AX · Beech 1900C · Landing Gear System Wiring > ON 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 WIRI - [SDR YADA100708](https://openairdocs.org/sdr/YADA100708.md): Line · ruptured · Oct 7, 2008 · N115AX · Beech 1900C · Landing Gear Brake System > PILOT REPORTED LEFT BRAKE "FLAT". REPLACED SEEPING FLEXIBLE BRAKE LINE - DATE CODE 2Q06. - [SDR YAD2008F00003](https://openairdocs.org/sdr/YAD2008F00003.md): Brake Sys · weak · Sep 20, 2008 · N115AX · Beech 1900C · Landing Gear Brake System > PILOT REPORTED LT BRAKE FLAT ON TAXI AND LANDING. MX BLEED BRAKES. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N115AX/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.