N100UX

Service difficulty reports · 94

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 = 'N100UX' 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 GLBA2017110900691Hose · leakingPILOTS REPORTED THAT THERE WAS A FUEL LEAK FROM LEFT WHEEL WELL ONTO THE LEFT OUTBOARD MAIN TIRE, A DROP EVERY 5 SECONDS. R & R THE HOSE WITH SERVICEABLE ONE IAW 28-20-00, LEAK CHECKED GOOD.Nov 6, 2017 · N100UX · Beech 1900D · Fuel StorageSDR GLBA2017100300685Cable · tornMAINTENANCE REPORTED THAT THE UPPER AFT AIRSTAIR DOOR CABLE WAS TORN. REMOVED AND REPLACED THE UPPER AFT AIRSTAIR DOOR CABLE IAW 52-10-02. P/N OFF/ON: 1440-40GLA, NSN.Oct 2, 2017 · N100UX · Beech 1900D · Passenger/Crew DoorsSDR GLBA2016011900564Cable · brokenPILOT REPORTED THAT THE FWD DOOR SNUBBER WAS INOPERATIVE. MX FOUND THE COUNTER BALANCE CABLE BROKEN, DISCONNECTED & REMOVED BOTH ENDS. INSTALLED NEW CABLE ASSEMBLY. OPS CHECKED GOOD.Jan 16, 2016 · N100UX · Beech 1900D · Passenger/Crew DoorsSDR GLBA2014071400420Tire · failedPILOT STATED THAT THE TOWER CALLED & SAID THEY SAW DEBRIS AFTER TAKEOFF. GROUND OPS CONFIRMED PIECES OF A TIRE ON THE RUNWAY. DECLARED AN EMERGENCY & RETURNED TO THE FIELD, RT INBD TIRE HAD SEPARATED. MAINTENANCE REPLACED BOTH RT TIRES.Jul 13, 2014 · N100UX · Beech 1900D · TireSDR GLBA2014031000400Skin · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE SKIN AT THE RT FWD SPAR CAP AREA, FS 288.0, 1.5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-021.Mar 9, 2014 · N100UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2014022800397Frame · corrodedDURING A SCHEDULED INSPECTION MX FOUND CORROSION AT FS 288.000 ON THE FRAME WHERE THE STRINGERS 16, 15R, 15L, 14R, & 14L ATTACHED, AREA OF 3 INCHES WIDE BY 2 INCHES. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-014.Feb 28, 2014 · N100UX · Beech 1900D · Fuselage Main, FrameSDR GLBA2014022800396Stringer · corrodedDURING A SCHEDULED INSPECTION MX FOUND CORROSION AT FS 258.250 TO FS 288.000 ON STRINGER 14L AT FAYING SURFACE. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-013.Feb 28, 2014 · N100UX · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2014022800395Stringer · corrodedDURING A SCHEDULED INSPECTION MX FOUND CORROSION AT FS 258.250 TO FS 288.000 ON STRINGER 15L AT FAYING SURFACE. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-015.Feb 28, 2014 · N100UX · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2014022800394Stringer · corrodedDURING A SCHEDULED INSPECTION MX CORROSION AT FS 258.250 TO FS 288.000 AT STRINGER 16 ON FAYING SURFACE. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-016.Feb 28, 2014 · N100UX · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2014022800393Stringer · corrodedDURING A SCHEDULED INSPECTION MX FOUND CORROSION AT FS 258.250 TO FS 288.000 ON STRINGER 15R AT FAYING SURFACE. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-017.Feb 28, 2014 · N100UX · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2014022800392Stringer · corrodedDURING A SCHEDULED INSPECTION MX FOUND CORROSION AT FS 258.250 TO 288.000, STRINGER 14R AT FAYING SURFACE. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-018.Feb 28, 2014 · N100UX · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2014022800390Skin · tornDURING A SCHEDULED INSPECTION MX FOUND THE SKIN TORN ON THE BELLY AT FS 265.750 & STRINGER 14L, APPROXIMATELY 5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-020.Feb 28, 2014 · N100UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2014021700385Frame · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE FUSELAGE FRAME AT FS 183.250, BETWEEN STRINGERS 2R & 3R WHERE THE DUCT PASSES THROUGH THE FRAME, .5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 14-1900Feb 17, 2014 · N100UX · Beech 1900D · Fuselage Main, FrameSDR GLBA2014021300382Frame · crackedDURING A SCHEDULED INSPECTION MX FOUND 2 CRACKS IN THE RT SIDE OF FS 107 & STRINGER 8R, FRAME ANGLE & LONGERON, FRAME CRACKED AT UPPER END OF FRAME IN BEND RADIUS. LONGERON CRACKED FROM LOWER EDGE TO LONGERON UPWARD THROUGH BEND RADIUS, 1.5 INCHES IN LENGTH.Feb 13, 2014 · N100UX · Beech 1900D · Fuselage Main, FrameSDR GLBA2014021300381Skin · corrodedDURING A SCHEDULED INSPECTION MX FOUND BELLY SKIN CORROSION AT FS 270 & STRINGER 16, 1.2 INCHES FWD & AFT DIRECTION BETWEEN STRINGER 16 FASTENERS. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-010.Feb 13, 2014 · N100UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2014021300380Frame · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE LT FUSELAGE AT FS 107 & STRINGER 8L FRAME AT THE UPPER END AT FRAME IN BEND RADIUS, .75 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-009.Feb 13, 2014 · N100UX · Beech 1900D · Fuselage Main, FrameSDR GLBA2014021200379Rib · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE RT WING INBD RIB FLANGE & DOUBLER AT JUNCTION WITH THE WING SPAR, RADIATES FROM THE OTBD EDGE OF THE FLANGE & DOUBLER INWARD TOWARD THE FLANGE BEND RADIUS, 1 INCH IN LENGTH. REPAIRED THE AFFECTED AREA AND Feb 11, 2014 · N100UX · Beech 1900D · Wing, Rib/BulkheadSDR GLBA2014021000378Skin · crackedDURING A SCHEDULED INSPECTION MX FOUND 2 CRACKS IN THE FUSELAGE SKIN AT FS 150 & STRINGER 1, JUST TO THE RT OF STRINGER 1 LOCATION, CRACK RADIATES INBD & OTBD FROM FASTENER .55 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECFeb 10, 2014 · N100UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2013103000346Door Frame · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE AFT LOWER CARGO DOOR FRAME AT FS 509.50 AND BETWEEN STRINGERS 10 - 11L, 2.5 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-077.Oct 30, 2013 · N100UX · Beech 1900D · Fuselage Main, StructureSDR GLBA2013070100267Relay · inoperativePILOT REPORTED THAT THE LANDING GEAR WOULD NOT EXTEND NORMALLY ON APPROACH, RAN CHECKLIST AND NOT HELP, MANUALLY PUMPED GEAR DOWN, ALL INDICATIONS NORMAL, AFTER LANDING FOUND LANDING GEAR RELAY CB POPPED. MX R & R TIME DELAY PCB, R & R GEAR MOTOR RELAY, R & RJun 28, 2013 · N100UX · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA2013062800265Relay · malfunctionedLANDING GEAR WOULD NOT EXTEND NORMALLY ON APPROACH. RAN CHECKLISTS AND NO HELP, MANUALLY PUMPED GEAR DOWN. ALL INDICATIONS NORMAL. AFTER LANDING, FOUND LANDING GEAR RELAY CIRCUIT BREAKER TRIPPED. R & R LANDING GEAR MOTOR RELAY IAW AIM 12-15.0. R & R LANDINJun 27, 2013 · N100UX · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA2013030600198Diode · failedPILOT REPORTED THAT THERE WAS ELECTRICAL SMOKE COMING FROM THE FUEL GAUGE PANEL, RT FIRE WALL CIRCUIT BREAKER TRIPPED. MX REPLACED THE CR3 DIODE ON THE FUEL PANEL.Mar 5, 2013 · N100UX · Beech 1900D · DC Power Distribution SystemSDR GLBA2013021300175Bulb · inoperativePILOT REPORTED THAT THE INSTRUMENTS EMERGENCY LIGHTS ON CAPS SIDE WILL NOT ILLUMINATE. MX REPLACED THE BULB, OPS CHECKED GOOD.Feb 12, 2013 · N100UX · Beech 1900D · Emergency LightingSDR GLBA2013011400151Bulb · burned outPILOT REPORTED THAT THE CAPTAIN'S SIDE EMERGENCY LIGHT WILL NOT ILLUMINATE. MX REPLACED THE BULB, OPS CHECKED GOOD.Jan 11, 2013 · N100UX · Beech 1900D · Emergency LightingSDR GLBA2012081400032Bulkhead · debondedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION FOUND THE FWD UPPER PRESSURE BULKHEAD AT FS 34.0 THE 2ND & 3RD BONDED STRAP FROM THE RT OTBD EDGE OF BULKHEAD HAS DEBONDED AREAS AT THE BOTTOM AREA OF STRAPS, THE 2ND STRAP DEBONDED AREA 2.3" X 1.3", 3RD STRAug 14, 2012 · N100UX · Beech 1900D · Fuselage Main, BulkheadSDR GLBA2012081400031Bulkhead · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND LT UPPER FWD PRESSURE BULKHEAD AT FS 84.0 CRACKED AT FASTENER HOLE ALONG BOTTOM EDGE OF PRESSURE BULKHEAD, 5.75" FROM THE LT OTBD PRESS BULKHEAD EDGE, CRACK RADIATES UPWARD FROM FASTENER HOLE, .1875" IN LENGTH. REPAug 13, 2012 · N100UX · Beech 1900D · Fuselage Main, BulkheadSDR GLBA2012080800029Elevator · damagedDURING A SCHEDULED ROUTINE INSPECTION FOUND THE LT ELEVATOR HAS DAMAGE ON THE T/E, .37" BY .15". REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-27-001. MATERIALS UTILIZED ARE INCLUDED IN THE EO.Aug 8, 2012 · N100UX · Beech 1900D · Elevator Tab Control SystemSDR GLBA2012080700028Spar Cap · crackedDURING A SCHEDULED INSPECTION, FOUND TWO CRACKS IN THE RT SIDE OF THE VERTICAL STAB, RT FWD SPAR CAP ANGLE AT APPROX AREA VSS 84.10, 20 PERCENT. REPAIRED AFFECTED AREA IAW EO 12-1900-55-022. MAJOR REPAIR.Aug 7, 2012 · N100UX · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA2012080600027Spar Cap · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE LT VERTICAL STAB, LT FWD SPAR CAP ANGLE AT APPROX FSS 84.10, 20 PERCENT CHORD VISIBLE, 1.25" IN LENGTH. REPAIRED AFFECTED AREA IAW EO 12-1900-55-021. MAJOR REPAIR.Aug 6, 2012 · N100UX · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2012080300025Stringer · corrodedDURING A SCHEDULED ROUTINE INSPECTION FOUND CORROSION BETWEEN STRINGER 16 AT FS 243.25 AND 258.25, IN A 2.25" AREA. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-042. MATERIALS UTILIZED ARE INCLUDED IN THE EO.Aug 3, 2012 · N100UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2012080300026Rib · crackedDURING A SCHEDULED ROUTINE INSP FOUND A CRACK ON THE LT WING INBD AUX RIB FLANGE & ANGLE AT JUNCTION WITH LT WING FWD WING SPAR AT FS 288, 1.3" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-57-008. MATERIALSAug 3, 2012 · N100UX · Beech 1900D · Wing, Rib/BulkheadSDR GLBA201208030024Skin · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND THE CENTER BELLY SKIN AT FS 303, 2" IB FROM RT EDGE, SKIN CRACKED, 1.25" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-041. MATERIALS UTILIZED ARE INCLUDED IN THAug 2, 2012 · N100UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA201208020023Bulkhead · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND 9 CRACKS IN THE LT LOWER PRESSURE BULKHEAD RADIATING FROM THE DOUBLE ROW OF FASTENERS AT THE INBD EDGE OF THE BULKHEAD, 3" IN LENGTH. REPAIRED AFFECTED AREA IAW EO 12-1900-53-040. MAJOR REPAIR.Aug 2, 2012 · N100UX · Beech 1900D · Fuselage Main, BulkheadSDR GLBA201208020022Bulkhead · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND CRACKS IN THE RT LOWER PRESSURE BULKHEAD RADIATING FROM FASTENERS AT THE INBD EDGE OF THE BULKHEAD, 8 CRACKS, 3.1" IN TOTAL LENGTH. REPAIRED AFFECTED AREA IAW EO 12-1900-53-040. MAJOR REPAIR.Aug 2, 2012 · N100UX · Beech 1900D · Fuselage Main, BulkheadSDR GLBA2012080100021Skin · corrodedDURING A SCHEDULED ROUTINE INSPECTION, FOUND BELLY SKIN CORROSION AT FS 243.25, AT JUNCTION OF FRAME & STRINGER 16, AND AT FS 243.25, AT JUNCTION OF FRAME & STRINGER 15L. REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-039.Aug 1, 2012 · N100UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2012061801Web · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE HORIZONTAL STAB AFT WEB AT HSS 0.00 IN THE LIGHTNING HOLE AT 2 O'CLOCK POSITION LOOKING FWD, .125" IN LENGTH. REPAIRED AFFECTED AREA IAW EO 12-1900-55-016. MAJOR REPAIR.Jun 16, 2012 · N100UX · Beech 1900D · Horizontal Stabilizer StructureSDR GLBA2012052201Diaphragm · damagedPILOT REPORTED THAT DURING CLIMB OUT AND PASSING THROUGH 21,500" CABIN HIGH ANNC ILLUMINATED, DECLARED EMERGENCY, MASKS DEPLOYED, RETURNED TO DEPARTURE. MX R & R LT OUTFLOW VALUE DUE TO DAMAGE TO THE DIAPHRAM IAW BMM 21-30-01, OPS CHECKED GOOD IAW BMM 21-30-0May 20, 2012 · N100UX · Beech 1900D · Pressure Regulator/Outflow ValveSDR GLBA20111212GCable · brokenPILOT REPORTED THAT THE DOOR SNUBBER CABLE IS BROKEN. MX REPLACED THE CABLE IAW MM 52-10-01, OPS CHECKED GOOD.Dec 10, 2011 · N100UX · Beech 1900D · Passenger/Crew DoorsSDR GLBA20110516FCheck Valve · failedSIG EVENT - THE PILOT REPORTED THAT 600 LBS OF FUEL DRAINED FROM THE MAIN TANK TO THE AUX TANK (LT). MX REPAIRED BY REPLACING THE LT AUX FUEL LINE CHECK VALVE.May 14, 2011 · N100UX · Beech 1900D · Aircraft Fuel Distribution SystemSDR GLBA20110307GSpar · wornMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE LH WING REAR SPAR BOTTOM LEADING EDGE CHAFFED AT 2 LOCATIONS BY EXT PWR CABLE, OB CHAFF .4" IN LENGTH .1" DEEP, IB CHAFFR .3" IN LENGTH .05" DEEP. MAINTENANCE REPAIRED THE AFFECTED AREMar 7, 2011 · N100UX · Beech 1900D · Wing SparSDR GLBA20110308GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE CARGO DOOR AFT FUSELAGE FRAME CRACKED 1.5" IN LENGTH AT THE GAS STRUT MOUNT UPPER IB NUT PLATE, FS 509 BETWEEN STRINGERS 4L & 5L. REF SDR 20110308F. MAINTENANCE REPAIRED THE AFFECTED AMar 4, 2011 · N100UX · Beech 1900D · Fuselage Main, FrameSDR GLBA20110308HFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE CARGO DOOR FRAME AT THE FWD GAS STRUT MOUNT CRACKED IN TWO PLACES 1.5" IN LENGTH AT FS 456 BETWEEN STRINGERS 3L & 4L. REF SDR 20110308F. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFMar 4, 2011 · N100UX · Beech 1900D · Fuselage Main, FrameSDR GLBA20110304FStructure · damagedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE RT OB WHEEL WELL KEEL ATTACHING HOLES FOR OB FENDER BRACKET HAS ELONGATED HOLES. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-54Mar 4, 2011 · N100UX · Beech 1900D · Wing Main, Frame StructureSDR GLBA20110304JSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE UPPER FUSELAGE SKIN AT F.S. 288 AND STRINGER 1 IS CRACKED, CRACK RADIATES FORWARD FROM FASTENER .4" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSMar 4, 2011 · N100UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20110304KSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE UPPER SKIN CRACKED AROUND (7) FASTENERS AT FS 273 BETWEEN STRINGER 1 AND 2R, CRACKS RANGE FROM .4" TO .2" IN LENGTH. SOME FOUND WITH EDDY CURRENT. MAINTENANCE REPAIRED THE AFFECTED AREMar 4, 2011 · N100UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20110304HFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE RH FUSELAGE FRAME CRACKED .3" IN LENGTH AT STRINGER 9AR CUTOUT AT F.S. 177. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-014. MATMar 4, 2011 · N100UX · Beech 1900D · Fuselage Main, FrameSDR GLBA20110304GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE RH FUSELAGE FRAME CRACKED AT STRINGER CUTOUT F.S. 183 STRINGER 9AR, .4" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-0Mar 4, 2011 · N100UX · Beech 1900D · Fuselage Main, FrameSDR GLBA20110308FMount · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE CARGO DOOR GAS STRUT FWD MOUNT HAS 2 CRACKS APPROX 1.3" IN LENGTH, THE AFT GAS STRUT MOUNT HAS 1 CRACK APPROX .6" IN LENGTH.Mar 4, 2011 · N100UX · Beech 1900D · Cargo/Baggage DoorsSDR GLBA20110303HFrame · crackedDURING A SCHEDULED ROUNTINE INSP MX FOUND THE RT SIDE WALL HEAVY ANGLE AT FS 303, CRACKED IN THE BEND RADIUS, APPROX 1" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-010. MATERIALS UTILIZED ARE INCLUDED IN Mar 3, 2011 · N100UX · Beech 1900D · Fuselage Main, FrameSDR GLBA20110303GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND THE LT HEAVY ANGLE CRACKED AT FS 303 APPROX 1" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-009. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEEMar 3, 2011 · N100UX · Beech 1900D · Fuselage Main, Frame
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