N111AX

Service difficulty reports · 39

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 = 'N111AX' AND registry_match = 'registration'
  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 YADA20210303001Fire Loop · brokenON VISUAL APPROACH TO LANDING ANC, LEFT ENGINE FIRE WARNING "T" HANDLE INTERMITTENTLY FLICKERED AND THEN CAME ON STEADY THEN EXTINGUISHED (NO OTHER EVIDENCE OF FIRE) AND THEN CAME ON AGAIN ON FINAL (NO OTHER EVIDENCE OF FIRE) - AIRCRAFT LANDED WITHOUT INCIDENTMar 2, 2021 · N111AX · Beech 1900C · Fire DetectionSDR YADA201912170001Landing Gear · malfunctionedGEAR DOWN UNCOMMANDED WITH HANDLE IN UP POSITION. NO RED LIGHTS IN HANDLE. 3 GREEN INDICATORS.Dec 13, 2019 · N111AX · Beech 1900C · Landing Gear Retraction/Extension SystemSDR YADA20190118001Squat Switch · intermittentPILOT REPORTED CABIN PRESSURIZATION DUMPED AT 10,500 FEET, O2 MASKS WERE DEPLOYED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED TROUBLESHOOTING AND FOUND THAT THE LANDING GEAR SQUAT SWITCH WAS INTERMITTENT AND CAUSING FALSE READINGS.Jan 18, 2019 · N111AX · Beech 1900C · Landing Gear Position and WarningSDR YADA20190116001Controller · malfunctionedPILOT REPORTED HE EXPERIENCED RAPID DECOMPRESSION AT 17,600 FEET. DEPLOYED O2 MASKS AND RETURNED TO ANCHORAGE AND LANDED WITHOUT ANY INCIDENTS OR PROBLEMS. MAINTENANCE PERFORMED TROUBLESHOOTING, REPLACED PRESSURIZATION CONTROLLER, PERFORMED PRESSURE CHECKS ON Jan 16, 2019 · N111AX · Beech 1900C · Cabin Pressure ControllerSDR YADA20180709001Doubler · corrodedDOUBLER FOUND CRACKED AT NUT-PLATE DURING DETAILED FUSELAGE CAMP INSPECTION. REMOVAL OF DOUBLER FOR REPAIR/REPLACEMENT DISCLOSED ADDITIONAL CORROSION DAMAGE TO THE DOUBLER. REPLACEMENT OF DOUBLER REQUIRED.Jul 9, 2018 · N111AX · Beech 1900C · Fuselage Miscellaneous StructureSDR YADA20180426001Lens · detachedLEFT WING TIP NAV STROBE LENS COVER LOST INFLIGHT.Apr 25, 2018 · N111AX · Beech 1900C · Exterior LightingSDR YADA20180102001Actuator · failedPILOT REPORTED THAT THE LANDING GEAR FAILED TO FULLY RETRACT, AIRCRAFT RETURNED TO HOME STATION. MAINTENANCE REMOVED AND REPLACED RIGHT MAIN LANDING GEAR ACTUATOR, OPERATIONAL CHECK SUCCESSFUL.Jan 2, 2018 · N111AX · Beech 1900C · Landing Gear ActuatorSDR YADA20171226001Actuator · crackedWHILE PERFORMING HEAVY MAINTENANCE INSPECTION AND SCHEDULED X-RAY OF NLG ACTUATOR CAP, TEST RESULTS SHOWED NOSE LANDING GEAR ACTUATOR CAP TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR ACTUATOR WITH SERVICEABLE.Dec 24, 2017 · N111AX · Beech 1900C · Landing Gear ActuatorSDR YADA20171018001Door Frame · crackedDURING MAINTENANCE VISUAL INSPECTION OF AIRSTAIR DOOR, FOUND A CRACK ON AIRSTAIR DOOR FRAME TO BE OUT OF LIMITS IAW SRM 53-90-08. AIRSTAIR DOOR FRAME WAS REPLACED.Oct 18, 2017 · N111AX · Beech 1900C · Fuselage Main, StructureSDR YADA20170621001Sensor · failedPILOT REPORTED THE LEFT ENVIRONMENTAL FAIL DURING CLIMB OUT, PILOT CYCLED ENVIROMENTAL SYS OFF THEN OPEN AND RECEIVED THE RIGHT ENVIROMENTAL FAIL LIGHT. MAINTENANCE REMOVED AND REPLACED CENTER TEMPATURE SENSOR AND OPERATIONAL CHECKS WERE SUCCESSFUL.Jun 21, 2017 · N111AX · Beech 1900C · Cabin Temperature Control SystemSDR YADA20170515001Fcu · unresponsivePILOT REPORTED THAT THE LEFT HAND ENGINE WAS UNRESPONSIVE TO POWER LEVER INPUT AND WOULD NOT COME OUT OF IDLE. MAINTENANCE PERSONAL REMOVED AND REPLACED THE LEFT HAND ENGINE FUEL CONTROL UNIT, PERFORMED RIGGING, OPERATIONAL AND LEAK CHECKS OF THE LEFT HAND ENGMay 15, 2017 · N111AX · Beech 1900C · Fuel Control/Turbine EnginesSDR YADA20170308002Frame · crackedWHILE AIRCRAFT WAS IN SCHEDULED HEAVY MAINTENANCE, MECHANIC WAS PERFORMING VISUAL C-CHECK AND FOUND A CRACK IN FRAME AT FS 509.50, WL 96 APPROXIMATELY (JUST AFT OF CARGO DOOR). P/N:114-430125-5Mar 6, 2017 · N111AX · Beech 1900C · Fuselage Main, FrameSDR YADA20170308001Frame · crackedWHILE AIRCRAFT WAS IN SCHEDULED HEAVY MAINTENANCE, MECHANIC WAS PERFORMING VISUAL C-CHECK AND FOUND A CRACK IN FRAME P/N:114-430121-33 AT FS 456.00 APPROXIMATELY WL 96(JUST FORWARD OF CARGO DOOR).Mar 6, 2017 · N111AX · Beech 1900C · Fuselage Main, FrameSDR YADA20160629001Circuit Breaker · burnedCIRCUIT BREAKER PANEL STARTED SMOKING AFTER LANDING. FLIGHT CREW SHUTDOWN ACFT AND EVACUATED SAFELY. MAINTENANCE LOCATED AND REPLACED OVERHEATED 5 AMP CIRCUIT BREAKER FOR ENGINE INSTRUMENT LIGHTING.Jun 27, 2016 · N111AX · Beech 1900C · Flight Compartment LightingSDR YADA20141223001Cable · brokenATTEMPTING TO DEPLANE, AIR STAIR DOOR WOULD NOT OPEN. FOUND ONE DOOR CAM OPERATING CABLE HAD BROKEN.Dec 23, 2014 · N111AX · Beech 1900C · Passenger/Crew DoorsSDR YADA20141129001Light · intermittentNOSE GEAR GREEN LIGHTS INTERMITTENT ON LANDING, NO OTHER WARNING INDICATION. DECLARED AN EMER FOR PRECAUTION. ACFT LANDED WITHOUT INCIDENT. CAUSE OF INTERMITTENT GREEN LIGHT NOT YET DETERMINED.Nov 29, 2014 · N111AX · Beech 1900C · Landing Gear Position and WarningSDR YADA20140721001Handle · missingPILOT REPORTED CARGO DOOR EXTERIOR HANDLE MISSING AFTER LANDING.Jul 21, 2014 · N111AX · Beech 1900C · Cargo/Baggage DoorsSDR 2013F00122Plunger · out of adjustWHEN THE ACFT REACHED ALTITUDE OF 22,000 FT. THE AFT CARGO DOOR WARNING LIGHT CAME ON. WHEN ACFT DROPPED IN ALTITUDE BELOW 20,000 FT. THE CARGO DOOR WARNING LIGHT EXTINGUISHED. FLIGHT CREW RETURNED TO DEPARTURE AND CALL MX. MX HAD FLIGHT CREW INSPECT CARGO May 30, 2013 · N111AX · Beech 1900C · Door Warning SystemSDR 2011FA0000813Socket · unsecureON APPROACH WITH THE LANDING GEAR SELECTED DOWN, THE RT MAIN GEAR DID NOT INDICATE DOWN AND LOCKED. THE PILOT CYCLED THE GEAR AGAIN AND STILL DID NOT GET A RT MAIN GEAR DOWN AND LOCKED INDICATION. THE LANDING WAS ABORTED. THE PILOT TAPPED ON THE LIGHT AND Dec 30, 2011 · N111AX · Beech 1900C · Landing Gear Position and WarningSDR YADA111709Exhaust Stack · crackedPILOT REPORTED OCCASIONAL EXHAUST FUMES IN CABIN. CONFIRMED THAT THE CREW SMELLED EXHAUST ON ROLLOUT WITH PROPS IN BETA AND HAD SMELLED IT AT AN ENGINE START (AS IS COMMON WHEN STARTING WITH A TAIL WIND). MX LOCATED A CRACKED HEATED INTAKE LIP STUB PIPE ON TNov 17, 2009 · N111AX · Beech 1900C · Engine Collector/Tailpipe/NozzleSDR YADA080509Cable · separatedPILOT REPORTED THAT PITCH TRIM SEEMED TO SLIP - RETURNED TO AIRPORT. MAINTENANCE REPLACED A BROKEN ELEVATOR TRIM CABLE.Aug 5, 2009 · N111AX · Beech 1900C · Elevator Tab Control SystemSDR YADA120108Windshield · crackedLT WINDSHIELD BROKE IN CRUISE - RED GLOW FROM HEATER ELEMENTS UNTIL WINDSHIELD HEAT TURNED OFF. UNEVENTFUL LANDING MADE AT ORIGINAL DESTINATION. MX REPLACED THE LT WINDSHIELD DUE TO OUTER PANE FAILURE.Dec 1, 2008 · N111AX · Beech 1900C · Flight Compartment WindowsSDR YADA111708Skin · corrodedDURING INSP, THE MECHANIC NOTICED THE BELLY BEACON FRONT FASTENER WAS LOOSE. UPON INSP, THE MECHANIC DETERMINED THAT THERE WAS CORROSION UNDER THE BEACON MOUNT. THE BELLY SKIN REQUIRED A PATCH REPAIR TO REMOVE THE DAMAGED AREA.Nov 10, 2008 · N111AX · Beech 1900C · Fuselage Main, Plate/SkinSDR ACE0519080Nipple · crackedPILOT REPORTED LOSS OF OIL PRESSURE, NR1 ENGINE. ENGINE SECURED IN FLIGHT AND AC RETURNED TO DEPARTURE AIRPORT AND MADE AN UNEVENTFUL LANDING. MAINT REPLACED THE NR1 ENGINE TORQUE PRESSURE LINE DUE CRACKED NIPPLE IN HOSE END. INSPECTION OF CRACKED HOSE NIPPMay 19, 2008 · N111AX · Beech 1900C · Turbine Engine Oil SystemSDR ACE011208Tube · leakingPILOT REPORTED NOSE TIRE FLAT ON LANDING. REPLACED TIRE ASSEMBLY DUE FAILED INNER TUBE. WE ARE EXPERIENCING MULTIPLE FAILURES, BURST TUBES FROM THIS MFG. MFG PREVIOUSLY NOTIFIED.Jan 12, 2008 · N111AX · Beech 1900C · Tire TubeSDR ACE011108Tube · blownPILOT REPORTED NOSE TIRE FLAT ON LANDING. REPLACED TIRE ASSY DUE FAILED INNER TUBE. WE ARE EXPERIENCING MULTIPLE FAILURES / BURST TUBES FROM THIS MFG. MFG PREVIOUSLY NOTIFIED.Jan 11, 2008 · N111AX · Beech 1900C · Tire TubeSDR ACE122407Tube · failedPILOT STOPPED AIRCRAFT ON TAXIWAY DUE NOSE TIE VIBRATION. REPLACED FLAT NOSE TIRE. TEARDOWN INSPECTION OF TIRE INDICATED A BURST TUBE AT A INSTALLATION FOLD. INSPECTION OF TUBE MATERIAL AT BURST AREA APPEARED TO RESEMBLE A CRACK MORE THAN A TEAR. THIS IS TDec 24, 2007 · N111AX · Beech 1900C · Tire TubeSDR ACE052607Wire · shortedPILOT REPORTED (CAN NOT TURN ON BATTERY POWER), LOCATED BLOWN 60 AMP. CURRENT LIMITER CAUSED BY SHORT TO GROUND ON NR 6 GAUGE WIRE (WIRE NR P30A6) AT BLEED AIR DUCT PN. 114-550159-1. REPAIRED WIRE AND DUCT (HOLE IN DUCT), REMOVED 1 FOOT OF EXCESS LENGTH OF WMay 26, 2007 · N111AX · Beech 1900C · Electrical Power System WiringSDR ACE010507Windshield · crackedPILOT REPORTED LT WINDSHIELD CRACKED AT 400 FT ON DEPARTURE. PILOT BURNED OFF FUEL AND RETURNED TO DEPARTURE FOR WINDSHIELD REPLACEMENT.Jan 5, 2007 · N111AX · Beech 1900C · Flight Compartment WindowsSDR ACE092706Pulley · frozenPILOT REPORTED, THOUGHT THAT THE RUDDER HAD EXPERIENCED A -FREEZING- CONDITION WHILE IN FLIGHT (PROBLEM HAD RESOLVED ITSELF PRIOR TO LANDING). MAINTENANCE INSPECTED A KNOWN PROBLEM AREA UNDER THE CARGO FLOOR INSIDE THE CARGO DOOR (FS 505 WL 88) AT THE RUDDER Sep 27, 2006 · N111AX · Beech 1900C · Rudder Control SystemSDR ACE012406Stringer · corrodedFOUND CORROSION ON STRINGER 15 LH AT FUSELAGE STATION 210. THE REPAIR REQUIRED DER. ENGINEERING ASSISTANCE DUE NO OEM DOCUMENT COVERING THE REQUIRED REPAIR.Jan 24, 2006 · N111AX · Beech 1900C · Fuselage Main, Longeron/StringerSDR 072405Smoke · detectedODOR OF SMOKE IN COCKPIT - SHUT OFF BLEED AIR AND EVIRONMENTAL AIR, ODOR WENT AWAY - MAINTENANCE COULD NOT LOCATE ANY SOURCE OF THE ODOR - OPS CHECK FLIGHT SCHEDULED.Jul 24, 2005 · N111AX · Beech 1900C · Air Distribution SystemSDR ACE051805Windshield · crackedPILOT REPORTED LT WINDSHIELD CRACKED OUTER PLY VERIFIED CRACKED - REPLACED WINDSHIELD (WITHIN MFG. WARRANTY PERIOD).May 18, 2005 · N111AX · Beech 1900C · Flight Compartment WindowsSDR ACE050705Safety Switch · intermittentPIREP - LANDING GEAR WOULD NOT RETRACT. MAINTENANCE REPLACED INTERMITTENT RT LANDING GEAR SAFETY SWITCH.May 7, 2005 · N111AX · Beech 1900C · Landing Gear Position and WarningSDR ACE122403Exhaust Duct · disconnectedPILOT REPORTED EXHAUST SMELL IN CABIN ON TAKEOFF AND CLIMB. MAINTENANCE LOCATED A DISCONNECTED NR 1 ENGINE INTAKE HEATED LIP (EXHAUST DUCT) TUBE. EXHAUST COULD HAVE BEEN INGESTED BY THE ENGINE AND THEN MIXED WITH THE BLEED AIR. NO PART FAILURE WAS OBSERVED.Dec 24, 2003 · N111AX · Beech 1900C · Engine Collector/Tailpipe/NozzleSDR 040503Switch · wornPILOT REPORTED HAVING TO CYCLE THE LANDING GEAR TO GET THE LEFT MAIN TO INDICATE DOWN AND LOCKED (GREEN) - MAINTENANCE REPLACED THE LEFT MAIN GEAR DOWN AND LOCK SWITCH.Apr 5, 2003 · N111AX · Beech 1900C · Landing Gear Position and WarningSDR YAD2003F00000Pump · failedIN CRUISE FLIGHT, RT ENGINE LOW FUEL PRESSURE ANNUNCIATOR CAME ON AND THE ENGINE SHUT DOWN (FLAMEOUT)-THE AIRCRAFT MADE AN UNEVENTFUL LANDING AT AN ALTERNATE AIRPORT. POST LANDING VISUAL INSPECTION AND GROUND RUNS DID NOT IDENTIFY ANY ABNORMALITIES. ENGINE ADec 26, 2002 · N111AX · Beech 1900C · Engine Fuel PumpSDR ACE0118021Yoke · crackedWHILE PERFORMING A SCHEDULED AILERON YOKE INSPECTION, FOUND THE RT AND LT AILERON YOKES CRACKED ON TWO SIDES (TOP AND BOTTOM) OF THE TAPER PIN HOLES, ALONG THE GRAIN OF THE METAL. THE CAUSE OF THE FAILURES WAS NOT EVIDENT.(K)Jan 25, 2002 · N111AX · Beech 1900C · AileronsSDR ACE1116011Control Cable · frozenPILOT REPORTED RUDDER FROZEN IN FLIGHT, UNEVENTFUL LANDING MADE. PILOT REPORTED THE RUDDER BROKE FREE WHILE TAXING REMOVED CARGO COMPARTMENT FLOOR AT CARGO DOOR AND OBSERVED WATER FROZEN AROUND RUDDER CABLE PULLEYS AT FUSELAGE STATION 495. REMOVED WATER AFTENov 16, 2001 · N111AX · Beech 1900C · Rudder Control System
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