N202UX

Service difficulty reports · 77

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 = 'N202UX' 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 GLBA20110111FSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A .5" CRACK IN THE FUSELAGE BELLY SKIN, 5" RT OF FS 228.25. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-003. MATERIALS UTILIZED ARE INCLUDED IN THE EO.Jan 10, 2011 · N202UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20110107FDoor Frame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND A CRACK IN THE AIRSTAIR DOOR ENTRANCE LOWER FRAME AT THE AFT CORNER AT F.S. 173, 1.1" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-Jan 7, 2011 · N202UX · Beech 1900D · Fuselage Main, StructureSDR GLBA20100823FSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP A, 2" CRACK WAS FOUND BETWEEN FS 300 TO 302, 28.5" OTBD OF THE CTR LINE ON THE RT SIDE AT WATER LINE 75.00. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP IAW EO 10-1900-53-051. MATERIALS UTIAug 23, 2010 · N202UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20100816GClamp · looseSIG EVENT - PILOT REPORTED THAT THE ACFT WOULD NOT PRESSURIZE IN FLIGHT. MX INSPECTED THE ACFT AND RESEATED A LOOSE CLAMP ON THE ACM TO THE HEAT EXCHANGER, OPS CHECKS OK, REF 71-51-01.Aug 15, 2010 · N202UX · Beech 1900D · Cabin Pressure Control SystemSDR GLBA20091031AConnector · disconnectedPILOTS REPORTED THAT UPON APPROACH NEITHER THE LETTER "R" OR THE LETTER "H" GREEN LIGHTS ILLUMINATED ON THE RT SIDE UPON GEAR EXTENSION NOR WITH THE MANUAL EXTENSION PROCEDURE. MX FOUND THE RT MLG ACTUATOR DOWNLOCK SWITCH CONNECTOR NOT CONNECTED PROPERLY. MX Oct 30, 2009 · N202UX · Beech 1900D · Landing Gear System WiringSDR GLBA20091030AIndicator · inoperativeNEITHER R OR H GREEN LIGHTS ILLUMINATED ON THE RT SIDE ON EXTENSION OR WITH MANUAL EXTENSION PROCEDURE.Oct 30, 2009 · N202UX · Beech 1900D · Landing Gear Position and WarningSDR GLBA200905121Line · overheatedPILOTS REPORTED THAT WHEN FULL POWERE WAS SET THE RT TORQUE WAS AT APPROX 3100 LBS BEFORE ITT LIMIT WAS EXCEEDED. TAKEOFF TORQUE SHOULD HAVE BEEN 3572 AT FLAPS 17 DEGREE AND BLEEDS CLOSED. ITT WAS EXCEEDED FOR APPROXIMATELY 1 SECOND. MAINTENANCE FOUND THE P3 LMay 12, 2009 · N202UX · Beech 1900D · Engine (Turbine/Turboprop)SDR GLBA2009031309ACircuit Board · malfunctionedON EXENED BASE POWER AT 1200 FT. LBS. ENGINES WERE GOING IN AND OUT OF FEATHER. MAINTENANCE RE-RACKED THE AUTOFEATHER PRINTED CIRCUIT BOARD AND THEY SYSTEM OPERATIONALLY CHECKED GOOD PER BMM 61-21-00-0001. OPERATION CHECK OF AUTOFEATHER SYSTEM GOOD PER 61-21-0Mar 13, 2009 · N202UX · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20090214BFrame · crackedDURING SCHEDULED STRUCTURAL INSP, A FRAME WAS FOUND CRACKED AROUND 2 RIVETS AT APPROX FS 544.75 AT STRINGERS 1R AND 13R. TWO CRACKS TOTALING .625". MX MANUFACTURED DOUBLER AND REPAIRED AFFECTED AREA IAW EO 09-UE202-05. OUT OF .040 INCH, 2024 T3 AL ALCLAD. MS2Feb 14, 2009 · N202UX · Beech 1900D · Fuselage Main, FrameSDR GLBA20090214DFrame · buckledDURING SCHEDULED STRUCTURAL INSP A FRAME ANGLE WAS FOUND BUCKLED AT THE INTERSECTION OF FS 544.75 AND STRINGER 12R. MX INSTALLED DOUBLER APPROXIMATELY 6" X 4" MADE FROM .040" 2024 T3 AL ALCLAD AND INSTALLED USING MS20470AD RIVETS ANS SEALED WITH AC240 B 1/2. RFeb 13, 2009 · N202UX · Beech 1900D · Fuselage Main, FrameSDR GLBA20090214CFrame · crackedDURING SCHEDULED STRUCTURAL INSP A FRAME CRACK WAS FOUND AROUND ONE RIVET AT FS 544.75 BETWEEN STRINGER 12L AND 13L. ONE CRACK .500" LONG. MX REPAIRED FRAME AT F.S. 544.75 INBD OF STRINGER 12L IAW EO-09-UE202-04. REPAIR ANGLE 4.125" X 2.750", 2024 T3, .040", Feb 13, 2009 · N202UX · Beech 1900D · Fuselage Main, FrameSDR GLBA20090213CFrame · crackedDURING SCHEDULED STRUCTURAL INSPECTION A FRAME WAS FOUND CRACKED ON THE LEFT SIDE OF STRINGER 1 AT FS 150.60. MAINTENANCE REPAIRED FRAME IAW EO 09-UE202-03.Feb 13, 2009 · N202UX · Beech 1900D · Fuselage Main, FrameSDR GLBA20090213BSkin · crackedMAJOR REPAIR - DURING SCHEDULED STRUCTURAL INSPECTION A SKIN CRACK AT INSERTION OF STRINGER 1 AND FS 150.60 WAS DISCOVERED. MAINTENANCE REPAIRED SKIN CRACK IAW EO 09-UE202-01.Feb 12, 2009 · N202UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20090213AFrame · crackedMAJOR REPAIR - DURING SCHEDULED STRUCTURAL INSPECTION A FRAME WAS FOUND CRACKED AT STRINGER 9R AT RELIEF CUTOUT AT FS 163.975. MAINTENANCE REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE IAW EO 09-UE202-02 AT FS 163.975 AND STRINGER 9R, REPAIR APPROXIMATELY 5" Feb 12, 2009 · N202UX · Beech 1900D · Fuselage Main, FrameSDR GLBA200901051Autofeather Sys · malfunctionedSUSPECTED AUTOFEATHER - ACFT.202UX SIGNIFICANT EVENT FLT NR 5028 "DEN" 01/04/08 UPON FINAL APPROACH THE PILOTS REPORTED THAT THE LT ENGINE BEGAN CYCLING IN/OUT OF AUTOFEATHER AS PWR WAS ADDED FROM 500 TO 1000 LBS. MX INSPECTED SECURITY OF MICROSWITCHES AND Jan 4, 2009 · N202UX · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20060941Hinge · lack of lubeFLIGHT 5067, PILOT REPORTED THAT THE ELEVATOR TRIM STUCK TWICE DURING FLIGHT AND WAS UNABLE TO ADVANCE TRIM PAST 1/2 NOTCH NOSE DOWN POSITION. MAINTENANCE CLEANED AND LUBED AFFECTED HINGE AREAS, AND AN OPERATIONAL CHECK FLIGHT WAS PERFORMED WHICH WAS FOUND SATApr 24, 2007 · N202UX · Beech 1900D · Elevator Tab Control SystemSDR GLBA20060907Skin · crackedUPON ROUTINE INSPECTION- MAINTENANCE FOUND A CRACK APPROXIMATELY 7.750 INCHES LONG AT APPROXIMATELY FS 352, APPROXIMATELY 27.5 INCHES LT OF THE BELLY CENTERLINE. MAINTENANCE REPAIRED THE AFFECTED AREA IAW SRM 51-70 FROM FS 298 TO 305.75. PATCH DIMENSION 14 INCFeb 19, 2007 · N202UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20060660Anti-Ice System · smokeCAPTAINS WINDSHIELD HEAT CYCLED ON AND OFF WITH SWITCH OFF, DESCENDING INTO DENVER HAD ELECTRICAL ODOR AND SMOKE STARTED COMING OUT FROM CAPTAINS CONTROL COLUMN, TURNED OFF ALL ICE PROTECTION SMOKE DISSAPATED, LANDED WITHOUT INCIDENT, PENDING REPAIRSFeb 1, 2006 · N202UX · Beech 1900D · Ice/Rain Protection SystemSDR 20030846Spar · crackedDURING ROUTINE INSPECTION, FOUR CRACKS APPROX .5 INCH LONG FOUND EXTENDING FROM THE DE-ICE LINE HOLE IN THE HORIZONTAL MAIN SPAR WEB. REPAIRED IAW WITH COMPANY EO. AIRCRAFT RETURNED TO SERVICE.May 17, 2005 · N202UX · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA20030629Structure · corrodedCABIN DOOR HAS CORRODED AREA BY BUTTON, REPAIRED.May 19, 2004 · N202UX · Beech 1900D · Passenger/Crew DoorsSDR GLBA20030579Warning System · illuminatedCARGO DOOR ANNUNCIATOR ILLUMINATED IN FLT, ADJUSTED DOOR AJAR SW.Mar 1, 2004 · N202UX · Beech 1900D · Door Warning SystemSDR GLBA20030522Switch · out of adjustCARGO DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT, ADJUSTED DOOR AJAR SWITCH OPS CK GOODDec 30, 2003 · N202UX · Beech 1900D · Door Warning SystemSDR GLBA2002013Indicator · malfunctionedNR 1 ITT INDICATOR FAILED ON T/O ROLL. RESET C/B, OPS CHECKED SYSTEM SATISFACTORY.Jan 26, 2002 · N202UX · Beech 1900D · Engine EGT/TIT Indicating SystemSDR GLBA2001232Indicator · erratic#2 VSI FLUX, REPLACED INDICATOR OPS CHECKED SYSTEM SATISFACTORYNov 24, 2001 · N202UX · Beech 1900D · Indicating/Recording SystemSDR GLBA2001133Altimeter · inoperativeCAPTAINS ALTIMETER FLAGGED, REPLACED ALTIMETER OPS CHECKED SATISFACTORYJun 24, 2001 · N202UX · Beech 1900D · Navigation SystemSDR GLBA2001006Warning Light · illuminatedRETURN TO BLOCK - RIGHT BLEED AIR ANNUCIATOR ILLUMINATED ON CLIMBOUT. REPAIRED EVA TUBING.Jan 12, 2001 · N202UX · Beech 1900D · Bleed Air Indicating SystemSDR 0001024AP005Strap · chafedAVIONICS ANNUNCIATOR CIRCUIT BREAKER POPPED CONCURRENT WITH SMOKE SMELL IN COCKPIT. AVIONICS ANNUNCIATOR WOULD NOT ILUMINATE AND PA AND CO-PILOTS PHONE CIRCUIT BREAKER WOULD NOT RESET. FOUND BONDING STRAP CHAFING ON GPWS WIRING. REPAIRED WIRING AND BONDING Jul 6, 2000 · N202UX · Beech 1900D · Electrical Power System
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