N184UX

Service difficulty reports · 81

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 = 'N184UX' 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 GLBA20090530AAltimeter · intermittentUPON CLIMBING OUT, THE PILOTS REPORTED THAT THE CAPTAINS ALTIMETER FAILED, HOWEVER, IT WAS NORMAL AFTER FIVE MINUTES. MX REMOVED AND REPLACED THE CAPTAINS ENCODING ALTIMTER IAW GMM 9.7.0, FAR 43 APPENDIX (E)AND(C)(A). MX PERFORMED PITOT STATIC CHECKS IAW BMM 2May 30, 2009 · N184UX · Beech 1900D · Altimeter, Barometric/EncoderSDR GLBA2009020503Cowling · looseAT 1000FT WITH TORQUE AT 1000'S PROP AT 1550 THE LT ENGINE JUMPED SEVERAL TIMES FROM 50 TO 2000 POUNDS OF TORQUE. MAINTENANCE PERFORMED ENGINE RUNS AND FOUND NO TORQUE SURGE PER BEECH MM 76-10-00. UPON FURTHER INVESTIGATION MAINTENANCE DISCOVERED THE COWLINGFeb 5, 2009 · N184UX · Beech 1900D · Nacelle/Pylon, Main FrameSDR GLBA200812111Terminal · arcedSMOKE SMELL - FLIGHT NR 7195 - UPON DEPARTURE FROM MKE IN FLIGHT - PILOTS REPORTED SPARKS NEAR THE BOTTOM OF THE RT CORNER OF THE FIRST OFFICERS WINDSHIELD INSIDE OF COCKPIT AND SMELLED A SLIGHT BURNING SCENT. MX REMOVED PAPER CLIP FROM FIRST OFFICERS WINDSHIDec 10, 2008 · N184UX · Beech 1900D · Windshield/Door Rain/Ice RemovalSDR GLBA20061073Stringer · debondedSTRINGER 9L DISBONDED AT FS 243.25 TO FS 258.25. MAINT REPAIRED DISBONDED STRINGER 9L AT FS 243.25 TO FS 258.25 IAW SRM 53-90. REPAIR APPROX 10.5 INCH. 2024 T3. RII INSP C/W IAW TASKCARD 8.2.1.Feb 19, 2008 · N184UX · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA20061072Skin · crackedFUSELAGE SKIN CRACK IN/AT PREVIOUS REPAIR CRACK APPROX 1 INCH LENGTH AT FS 248.0 ABOVE STR 9L. MAINT REPAIRED FUSELAGE SKIN AT FS 248.0 IAW SRM 51-70. REPAIR DIMENSIONS APPROXIMATELY 14 FT BY 12.5 FT, 2024 T3 .040. RII INSP C/W IAW TASKCARD 8.2.1.Feb 19, 2008 · N184UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20061070Frame · cracked02/18/08, FRAME CRACKED AT STR 9R CUTOUT. CRACK APPROX .500 IN LENGTH AT FS 177.35. MAINT REPAIRED FRAME CRACK AT STR RELIEF HOLE AT FS 177.35 AND STR 9R IAW SRM 51-70. REPAIR APPROX 5 INCH X 2.5 INCH 2024 T-3 .071. RII INSP C/W IAW TASKCARD 8.2.1.Feb 19, 2008 · N184UX · Beech 1900D · Fuselage Main, FrameSDR GLBA20061059Angle · crackedLT WING TO FUSELAGE HEAVY ANGLE CRACKED APPROX 1.750 AT FWD BEND RADIUS AT FS 288.0. MAINT REPAIRED THE LT TO FUSELAGE HEAVY ANGLE IAW. SRM 53-90. REPAIR APPROX 13.5 INCH. RII INSP COMPLIED IAW TASKCARD 8.2.1.Feb 18, 2008 · N184UX · Beech 1900D · Fuselage Miscellaneous StructureSDR GLBA20061060Angle · crackedRT WING TO FUSELAGE HEAVY ANGLE CRACKED APPROX 2.125 INCH AT FWD BEND RADIUS AT FS 288.0. MAINT REPAIRED THE LT TO FUSELAGE HEAVY ANGLE IAW SRM 53-90. REPAIR APPROX 13.5 INCH. RII INSP COMPLIED WITH IAW TASKCARD 8.2.1.Feb 18, 2008 · N184UX · Beech 1900D · Fuselage Miscellaneous StructureSDR GLBA20061022Cable · brokenEES SYSTEM - PILOTS REPORTED DIFFICULTY WITH THE AIRSTAIR DOOR NOT LOCKING PROPERLY. MAINTENANCE DISCOVERED THE DOOR CABLE WAS BROKEN ON THE INSIDE. MAINTENANCE REMOVED AND REPLACED THE AIRSTAIR DOOR CABLE IAW MM 52-10. OPERATIONAL CHECK GOOD. RII INSPECTION CNov 4, 2007 · N184UX · Beech 1900D · Entrance StairsSDR 20030825Window · crackedDURING ROUTINE INSPECTION, EMERGENCY EXIT 4C WINDOW PAN FOUND CRACKED AT RADIUS. REPLACED WINDOW PAN IAW EO. AIRCRAFT RETURNED TO SERVICE.Mar 11, 2005 · N184UX · Beech 1900D · Door WindowsSDR 20030824Bulkhead · crackedDURING ROUTINE INSPECTION, BULKHEAD AT FRAME STATION 492.75 FOUND TO BE CRACKED WHERE IT ATTACHES TO TOP OF CARGO DOOR FRAME. REPAIRED IAW EO. AIRCRAFT RETURNED TO SERVICE.Mar 10, 2005 · N184UX · Beech 1900D · Fuselage Main, BulkheadSDR 20030823Structure · corrodedDURING ROUTINE INSPECTION, CORROSION DISCOVERED AROUND AIRSTAIR DOOR HANDLE APPROX 2 INCH IN DIA AREA REPAIRED IAW EO. AIRCRAFT RETURNED TO SERVICE.Mar 10, 2005 · N184UX · Beech 1900D · Entrance StairsSDR 20030822Frame · crackedDURING ROUTINE INSPECTION, FOUND WEB CRACK ON FRAME FS 466.0 STRINGER 10R. REPAIRED CRACK IAW WITH EO. AIRCRAFT RETURNED TO SERVICE.Mar 10, 2005 · N184UX · Beech 1900D · Fuselage Main, FrameSDR GLAB20030698Receptacle · damagedRT NACELLE POWER CABLE OPENING AT WHEEL WELL IS DAMAGED, REPAIRED.Aug 2, 2004 · N184UX · Beech 1900D · Electrical Power SystemSDR GLBA2003125Indicator · inoperativeRT ITT INDICATOR NOT WORKING, REMOVED AND REPLACED INDICATOR.Aug 27, 2003 · N184UX · Beech 1900D · Engine EGT/TIT Indicating SystemSDR GLBA2003054Transmitter · malfunctionedRADAR WILL NOT PAINT, R & R WX RADAR OPS CHECK GOOD.Apr 23, 2003 · N184UX · Beech 1900D · Weather Radar SystemSDR GLBA2003011Pump · failedRIGHT FUEL LOW PRESS LIGHT ILLUM. REMOVED AND REPLACED LP FUEL PUMP, OPS CHECK GOOD.Jan 20, 2003 · N184UX · Beech 1900D · Aircraft Fuel Distribution SystemSDR GLBA2002205Connector · defectiveRT FUEL INDICATOR READS ZERO. REMOVED AND REPLACED RT FUEL FLOW TRANSMITTER CONNECTOR, OPS CHECK GOOD.Dec 16, 2002 · N184UX · Beech 1900D · Fuel Flow IndicatingSDR GLBA2002181Warning Light · illuminatedRT PITOT HEAT ANNUNCIATOR ILLUMINATED IN FLIGHT, OPS CHECK GOODNov 10, 2002 · N184UX · Beech 1900D · Pitot/Static Anti-Ice SystemSDR GLBA2002163Bulb · burned outLANDING GEAR LIGHT RIGHT SIDE WILL NOT ILLUMINATE, REPLACED BULBOct 14, 2002 · N184UX · Beech 1900D · Landing Gear Position and WarningSDR GLBA2002121Warning System · false activationDUAL ENVIRO FAIL ON TAKEOFF ROLL, PERFORMED GROUND RUNS AND P-TEST AND OPS CHECK GOOD.Aug 13, 2002 · N184UX · Beech 1900D · Central WarningSDR GLBA2002061Seal · tornCABIN DOOR SEAL LEAKING, REPLACED SEAL OPS CHECKED SATISFACTORYMay 14, 2002 · N184UX · Beech 1900D · DoorsSDR GLBA2002057Shutoff Valve · failedDUAL ENVIRONMENTAL FAILURE ON CLIMBOUT. REPLACED PRSOV VALVE.May 6, 2002 · N184UX · Beech 1900D · Cabin Pressure Control SystemSDR GLBA2002037Encoder · inaccurate#2 ENCODER REPORTED HIGH BY ATC, REPLACED ENCODING ALTIMETER OPS CHECKED SYSTEM SATISFACTORYMar 18, 2002 · N184UX · Beech 1900D · Altimeter, Barometric/EncoderSDR GLBA2002038Altimeter · malfunctionedALTIMETER SPLIT. COULD NOT DUPLICATE, OPS CHECKED SATISFACTORY.Mar 18, 2002 · N184UX · Beech 1900D · Altimeter, Barometric/EncoderSDR GLBA2002018Elt · malfunctionedELT WOULD NOT SILENCE. REPLACE ELT, OPS CHECKED SYSTEM SATISFACTORY.Feb 8, 2002 · N184UX · Beech 1900D · Emergency Locator BeaconSDR GLBA2002009Warning System · malfunctionedLANDING GEAR INTRANSIT LIGHT FAILED TO EXTINGUISH, CYCLED GEAR AGAIN LIGHT REMAINED ON FOR APPROX 1 MINUTE. INSPECTED GEAR INDICATION SYSTEM AND PERFORMED TEST FLIGHT. COULD NOT DUPLICATE PROBLEM.Jan 22, 2002 · N184UX · Beech 1900D · Landing Gear Position and WarningSDR GLBA2001101A/C Pack · failedRIGHT ENVIROMENTAL FAIL ON T/O ROLL. INSPECTED, COULD NOT DUPLICATE.May 15, 2001 · N184UX · Beech 1900D · Cabin Cooling SystemSDR 20000508SH028Gyro · failedPILOT WRITE-UP WAS ''HDG WON''T MOVE WITH AIRCRAFT MOVEMENT''. THIS GYRO IS LOCKED UP. (X)Mar 24, 2000 · N184UX · Beech 1900D · Directional Gyro and Indicating SystemSDR 99ZZZX4085Altimeter · malfunctionedCAPTAIN'S ALTIMETER READS 80 FEET - 100 FEET HIGH AT ALL ALTITUDES AND ENCODER TRANSITION POINTS ARE OUT OF TOLERANCE. REMOVED AND REPLACED ALTIMETER. BENCH TEST VERIFIED ALTIMETER TO BE INDICATING 80 FEET HIGH AT 1,500 FEET AND 110 FEET HIGH AT 10,000 FEET. Sep 17, 1999 · N184UX · Beech 1900D · Altimeter, Barometric/EncoderSDR 99ZZZX3498Altimeter · bindingKOLLSMAN KNOB FOUND BINDING WHEN REMOVED FROM STOCK. RETURNED.Jul 22, 1999 · N184UX · Beech 1900D · Altimeter, Barometric/Encoder
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