N231YV

Service difficulty reports · 90

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 = 'N231YV' 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 GLBA2017110300689Cable · brokenMAINTENANCE REPORTED THAT THE LOWER FORWARD AIRSTAIR DOOR HANDRAIL CABLE WAS BROKEN INTERNALLY. REMOVED AND REPLACED THE FORWARD LOWER DOOR CABLE, P/N OFF/ON: 1440-43GLA, IAW B1900D MM 52-10-02.Nov 2, 2017 · N231YV · Beech 1900D · Passenger/Crew DoorsSDR GLBA2017072100676Cover · wornMAINTENANCE REPORTED THAT THE AFT BOTTOM CABLE SHEATH WAS WORN ON THE PAX DOOR. REPLACED THE CABLE IAW MM 52-10-02.Jul 18, 2017 · N231YV · Beech 1900D · Passenger/Crew DoorsSDR GLBA2017031300641Brake Sys · contaminatedTHE CREW REPORTED THE LEFT HAND BRAKE HAS TO BE PUMPED TO WORK, IT'S SPONGY. BOTH CAPTAIN AND COPILOT BRAKES ARE SPONGY ON LT SIDE. MAINTENANCE BLED THE LT BRAKE SYSTEM IAW BEECH MM 32-40-05. VERIFIED PILOT AND CO-PILOT OPERATION. OPS CHECK GOOD.Mar 11, 2017 · N231YV · Beech 1900D · Landing Gear Brake SystemSDR GLBA2017030900639Brake Sys · contaminatedCAPTAIN'S AND FIRST OFFICER'S LEFT BRAKE PEDALS WERE EXTREMELY SPONGY AND WENT TO FLOOR WITH VERY LITTLE TO NO BRAKING ABILITY. MAINTENANCE BLED THE LT BRAKE SYSTEM IAW MM 32-40-05. FLUSHED WITH 2 QUARTS OF 5606. TAXIED AIRCRAFT AND VERIFIED OPERATION. OPS CHEMar 7, 2017 · N231YV · Beech 1900D · Landing Gear Brake SystemSDR GLBA2017030700638Master Cylinder · contaminatedSIG EVENT - THE CREW REPORTED THAT THE CAPTAIN'S LEFT HAND BRAKE WAS SPONGY AND INEFFECTIVE. MAINTENANCE BLED THE CAPTAIN'S LEFT HAND BRAKE IAW BEECH 32-40-05. OPS CHECK GOOD.Mar 5, 2017 · N231YV · Beech 1900D · Master Cylinder/Brake ValveSDR GLBA2016060600591Master Cylinder · wornPILOT REPORTED THAT THE CAPTAINS SIDE LT BRAKE PEDAL IS NOT HOLDING & WENT TO THE FLOOR. REPLACED THE CAPTAINS LT BRAKE CYLINDER IAW 32-40-06, PN 90-380001-33 & SN 2912 OFF, SN 3549 ON, BRAKE BLEED & OPERATIONS CHECKED GOOD.Jun 3, 2016 · N231YV · Beech 1900D · Master Cylinder/Brake ValveSDR GLBA2016042500583Pcb · faultyPILOT REPORTED THAT THE AUTOFEATHER ARMED WITH N1 ABOUT 95%, AFX DISABLE ILLUMINATED & RT AUTOFEATHER FAILED TO ARM. REPLACED PCB A123, PN ON & OFF 129-364091-9, SN OFF 446C95, SN ON 925I94, IAW AIM 10-24-01. VERIFIED RIGGING OF ARMING SWITCHES IAW MM 61-21-Apr 24, 2016 · N231YV · Beech 1900D · Propeller Feathering/ReversingSDR GLBA2016042500582Unknown · malfunctionedPILOT REPORTED THAT AFTER TAKEOFF, POWER WAS APPLIED, AFX DISABLE ANNUNCIATOR ILLUMINATED & RT AUTOFEATHER DISARMED, THEN REARMED. THEN AFTER ROTATION, RT AUTOFEATHER DISARMED. ON CLIMB OUT SYS REARMED FOR THE REMAINDER OF THE FLIGHT. SUPPLEMENTAL INFORMATIApr 23, 2016 · N231YV · Beech 1900D · Propeller Feathering/ReversingSDR GLBA2016020900565Control Handle · brokenPILOT REPORTED THAT THE LG FAILED TO EXTEND NORMALLY, FOLLOWED CHECKLIST. PERFORMED MANUAL EXTENSION, DOWN WITH 3 GREENS. JACKED ACFT RETRACTED GEAR 10 TIMES, NO DEFECTS NOTED. CHECKED CONTINUITY OF WIRES IAW WDM 32-31-01-01 & 32-31-0202, FROM A316 TO P532,Feb 8, 2016 · N231YV · Beech 1900D · Landing Gear SelectorSDR GLBA2015110900557Spar Cap · corrodedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THE RT REAR LOWER WING SPAR CAP FROM WING STATION 215.08 - 310. CORROSION ON THE AFT FLANGE GOING UP ON THE TEE. REPAIRED IAW EO 15-1900-57-003.Nov 9, 2015 · N231YV · Beech 1900D · Wing SparSDR GLBA2015110900556Spar · corrodedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THE RT REAR WING SPAR OTBD WEB CORRODED. REPAIRED IAW EO 15-1900-57-003.Nov 9, 2015 · N231YV · Beech 1900D · Wing SparSDR GLBA2014101600456Skin · crackedDURING A SCHEDULED INSPECTION FOUND CRACK IN THE LT AFT FUSELAGE SKIN AT BS 549.25 BETWEEN STRINGERS 12 - 13L, 1.1 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-043. MAJOR REPAIR.Oct 16, 2014 · N231YV · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2014101600455Structure · damagedDURING A SCHEDULED INSPECTION FOUND MULTIPLE FASTENER HOLES ELONGATED BETWEEN BS 531 - 557.5. ELONGATION RANGING FROM .20 INCHES TO .30 INCHES, FASTENER HOLES ARE FOR THE LT FWD VENTRAL FIND, INBD & OTBD OF STRINGER 12L. REPAIRED IAW EO 14-1900-52-043. MAOct 16, 2014 · N231YV · Beech 1900D · Fuselage Miscellaneous StructureSDR GLBA2014101400454Skin · crackedDURING A SCHEDULED INSPECTION FOUND A CRACK IN THE EMERGENCY EXIT DOOR 6C RT AFT INSIDE SKIN 0.875 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-52-005. MAJOR REPAIR.Oct 14, 2014 · N231YV · Beech 1900D · Emergency ExitsSDR GLBA2014101000453Skin · crackedDURING A SCHEDULED INSPECTION FOUND A CRACK IN THE FUSELAGE SKIN AT FS 249.25 & STRINGER 12L UNDER LT VORTEX GEN 1.75 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-042. MATERIALS UTILIZED ARE INCLUDEDOct 10, 2014 · N231YV · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2014100900451Bulkhead · crackedDURING A SCHEDULED INSPECTION FOUND A CRACK IN THE CANTED BULKHEAD AT FS 588.10 & STRINGER 8L .65 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-041. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING Oct 9, 2014 · N231YV · Beech 1900D · Fuselage Main, BulkheadSDR GLBA2014100900452Skin · crackedDURING A SCHEDULED INSPECTION FOUND A CRACK IN THE UPPER FWD CORNER OF A/S DOOR CUT OUT FS 150.6 PROTRUDING UPWARD .75 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-040. MATERIALS UTILIZED ARE INCLUDEOct 9, 2014 · N231YV · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2014100800450Spar · crackedDURING A SCHEDULED INSPECTION FOUND A CRACK IN THE AFT CTR HORIZONTAL STAB SPAR WEB, .125 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-55-011. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.Oct 8, 2014 · N231YV · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA2014100800449Bulkhead · buckledDURING A SCHEDULED INSPECTION FOUND THE CANTED BULKHEAD AT FS 588.10 BUCKLED FROM STRINGER 12R TO STRINGER 11L. PREVIOUS REPAIR DOUBLER BETWEEN STRINGER 11L & 13L BUCKLED. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-Oct 8, 2014 · N231YV · Beech 1900D · Fuselage Main, BulkheadSDR GLBA2014100700448Frame · crackedDURING A SCHEDULED INSPECTION FOUND 2 CRACKS IN THE FUSELAGE FRAME AT FS 183.25 AT 2 LOCATIONS. 1ST AT INBD CORNER AREA AT ENVIRONMENTAL DUCT CUT OUT, ONE CRACK IS FROM CUT OUT ALL THE WAY THROUGH THE BEND RADIUS TO THE EDGE FRAME. SECOND IS FROM FASTENER INOct 7, 2014 · N231YV · Beech 1900D · Fuselage Main, FrameSDR GLBA2014092600446Skin · damagedDURING A SCHEDULED INSPECTION FOUND A LIGHTNING STRIKE ON THE OTBD TE LT ELEVATOR JUST OTBD OF THE MOST OTBD STATIC WICK. SKIN HAS .5 INCH X .25 INCH DAMAGE STARTING INBD OF THE FIBERGLASS END CAP & TRAVELING OUTWARD UNDER THE END CAP, DAMAGING THE END CAP. Sep 26, 2014 · N231YV · Beech 1900D · Elevator, Plate/SkinSDR GLBA2014082900435Skin · damagedDURING A SCHEDULED INSPECTION MAINTENANCE, FOUND WING SKIN BENT UPWARDS ON TRAILING EDGE BETWEEN WS 114.25 & 124.25. REPAIRED IAW EO 14-1900-57-006.Aug 29, 2014 · N231YV · Beech 1900D · Wing, Plate/SkinSDR GLBA2013013000166Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK AT FS 107 AND STRINGER 8R, FRAME CRACK PROTRUDING OUT OF RIVET, .5 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-007.Jan 30, 2013 · N231YV · Beech 1900D · Fuselage Main, FrameSDR GLBA2013013000165Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND TWO CRACKS AT FS 107 AND STRINGER 8L IN THE BEND RADIUS, CRACK PROTRUDING OUT OF RIVET, 1.25 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-008.Jan 30, 2013 · N231YV · Beech 1900D · Fuselage Main, FrameSDR GLBA2013013000164Frame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FUSELAGE FRAME AT FS 456 AT THE GAS STRUT UPPER INBD NUTPLATE BETWEEN STRINGERS 3L AND 4L, .75" IN LENGTH. REPAIRED IAW EO 13-1900-53-002.Jan 30, 2013 · N231YV · Beech 1900D · Fuselage Main, FrameSDR GLBA2012030901Rib · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK AT THE LT CENTER WING L/E INBD RIB AND REINFORCEMENT STRAP 1.5" FWD OF SPAR, 1" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-57-002. MAJOR REPAIR.Mar 8, 2012 · N231YV · Beech 1900D · Wing, Rib/BulkheadSDR GLBA2012030101Spar Cap · chafedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CHAFE ON THE LT WING FWD LOWER SPAR CAP AT BL 29.5, APPROX 1" BY .312" AT WIDEST POINT, .125" TO .187" DEEP AT DEEPEST POINT. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONSMar 1, 2012 · N231YV · Beech 1900D · Wing SparSDR GLBA20111111FCable · frayedPILOT REPORTED THAT THE TOP AFT AIRSTAIR DOOR CABLE IS FRAYED. MX REPLACED THE TOP AFT DOOR CABLE, OPS CHECKED GOOD.Nov 10, 2011 · N231YV · Beech 1900D · Passenger/Crew DoorsSDR GLBA20110823HSkin · debondedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP MX FOUND THE RT WINGLET DEBONDED AT THE INBD EDGES AND A HOLE IN THE L/E NEXT TO THE UNDER LIGHT DAM. MX REPLACED, AND REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-57-009.Aug 23, 2011 · N231YV · Beech 1900D · Wing, Plate/SkinSDR GLBA20110818KRail · wornAIRSTAIR DOOR AFT UPPER HAND RAIL WORN. MX REPLACED THE RAIL IAW BMM 52-10-02, OPS CK GOOD.Aug 17, 2011 · N231YV · Beech 1900D · Passenger/Crew DoorsSDR GLBA20110810FScrew · missingPILOT REPORTED THAT A SCREW WAS MISSING FROM THE CABIN DOOR. MX REPLACED THE SCREW.Aug 9, 2011 · N231YV · Beech 1900D · Passenger/Crew DoorsSDR GLBA20110808HGovernor · inoperativePILOT REPORTED THAT DURING THE AFX TEST, RT PROP DID NOT FEATHER. MX RESEATED A173 PCB IAW MI 24-01 AND REPLACED THE RT OVERSPEED GOV IAW BMM 61-20-01, PN: 210961C SN:11403305, OPS CK GOOD.Aug 5, 2011 · N231YV · Beech 1900D · Propeller GovernorSDR GLBA20110803HCap · damagedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND THE RT STABILON END CAP DAMAGED FROM TE FWD 10.7" AND FROM T/E OTBD TIP 7" GOING 2.5" PAST SPLICE. MX REPLACED, REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW. EO 11-1900-55Aug 3, 2011 · N231YV · Beech 1900D · Empennage StructureSDR GLBA20110801JSwitch · inoperativePILOT REPORTED THAT THE LT AUTOFEATHER INTERMITTENT AFX REPEATER AND LT AUTOFEATHER ANNC WENT OFF DURING TAKEOFF ROLL, ABORTED AND EXITED RUNWAY. MX REPLACE THE LT POWER LEVER AFX ARMING MICRO SWITCH, PN: 15M1 IAW BMM 61-21-02, OPS AND RIG CK GOOD.Jul 30, 2011 · N231YV · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20110727JPcb · inoperativePILOT REPORTED THAT ON DECENT THE RT AUTOFEATHER DID NOT ARM. MX REPLACED PCB A123 PN: 129-304091-9 SN: 735599 IAW AIM MI 24-01, OPS CK GOOD.Jul 26, 2011 · N231YV · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20110727HPcb · inoperativePILOT REPORTED THAT THE LT AUTOFEATHER SYS DID NOT ARM ON TAKEOFF ROLL. MX REPLACED PCB A123 IAW AIM MI 24-01.Jul 26, 2011 · N231YV · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20110711NPcb · inoperativePILOT REPORTED THAT THE LT AUTOFEATHER DISARMED ON TAKEOFF ROLL AT 65 KNOTS, ABORTED TAKEOFF. MX WAS ABLE TO DUPLICATE BY MOVING J2 CONNECTOR OF A123PCB, R & R CONNECTOR J2 PH: 3-582151-1, REF BMM 61-05-01 AND R & R A123 PCB REF AIM MI24-01 PN 129-3640919, PEJul 10, 2011 · N231YV · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20110711HConnector · groundedPILOT REPORTED THAT WITH THE GEAR HANDLE IN THE UP POSITION "AUTOFEATHER OFF" ANNUNCIATOR ILLUMINATED WITH THE AUTOFEATHER SWITCH IN THE ARM AND OFF POSITION. MX T'S FOUND THE SOCKET INSIDE THE UPLOCK PLUG SHORTING TOGETHER, REPAIRED SOCKET AND PLUG PN MS3126Jul 8, 2011 · N231YV · Beech 1900D · Propeller/Propulsor System WiringSDR GLBA20110629FSkin · debondedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND THE AIRSTAIR DOOR EXTERIOR SKIN DEBONDING IN A 7" X 7" AREA AROUND THE PRESSURE LOCK. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-52-003. MATERIALS UTILIZED Jun 29, 2011 · N231YV · Beech 1900D · Passenger/Crew DoorsSDR GLBA20110627JFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP MX FOUND A CRACK IN THE AIR STAIR DOOR LOWER FRAME AT THE LOWER AFT CORNER, .75" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-043 MATERIALS UTIJun 27, 2011 · N231YV · Beech 1900D · Passenger/Crew DoorsSDR GLBA20110627HFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND A CRACK IN THE FUSELAGE FRAME AT FS 456 AND STRINGER 10R, .2" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-042 MATERIALS UTILIZED ARE INCLUDED IJun 27, 2011 · N231YV · Beech 1900D · Fuselage Main, FrameSDR GLBA20110627GSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND A CRACK IN THE INNER SKIN OF THE EMERGENCY EXIT AT 6A, VERT LENGTH 3.25"M ABD HORZ 3". MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-52-007. MATERIALS UTILIZEJun 27, 2011 · N231YV · Beech 1900D · Emergency ExitsSDR GLBA20100826FValve · inoperativePILOT REPORTED THAT THE LANDING GEAR DID NOT EXTEND ON FINAL APPROACH, GEAR FAILED TO EXTEND AND LANDING GEAR RELAY TRIPPED, GEAR WAS MANUALLY EXTENDED SUCCESSFULLY WITH 3 GREEN LIGHTS INDICATED. MX REMOVED LANDING GEAR SERVICE VALVE PN 101-388008-3, SN 2206 Aug 25, 2010 · N231YV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA201008231Powerpack · failedPILOT REPORTED THAT THE LANDING GEAR DID NOT EXTEND ON FINAL APPROACH, INTRANSIT LIGHT WAS ON AND NOTICED THAT THE GEAR RELAY CB POPPED, EXTENDED THE LANDING GEAR MANUALLY, LANDED SAFELY. MAINTENANCE CONFIRMED DISCREPANCY, TROUBLESHOT SYSTEM TO HYDRAULIC POWERAug 23, 2010 · N231YV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA201005301Bulb · burned outPILOT REPORTED AFTER LANDING THAT THE EMERGENCY INSTRUMENT LIGHT SECOND FROM THE LEFT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT IAW 1900 AMM 33-10-00, PART NUMBER D165-100-2, OPERATIONAL TEST OF THE SUBSEQUENT SYSTEM CHECKS GOOD.May 30, 2010 · N231YV · Beech 1900D · Emergency LightingSDR GLBA20100112FSkin · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND BETWEEN 2 RIVETS AT FS 290 AND BL 30L ON THE BOTTOM OF THE LT LOWER FUSELAGE AFT OF THE FWD WING SPAR, CRACK APPROX .4" IN LENGTH. MAINT REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSJan 12, 2010 · N231YV · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20100107FSkin · crackedDURING ROUTINE SCHEDULED MX, A SMALL CRACK IN THE SKIN WAS FOUND AT FS 265 2.5" OTBD OF STR 13R. CRACK APPROX .250" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTIONS IAW EO 09-120-53-004. MATERIALS UTLIZED ARE LISTED IN THE Jan 7, 2010 · N231YV · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20100104JFrame · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MX 2 CRACKS WERE FOUND AT THE AIRSTAIR DOOR FUSELAGE FRAME AT FS 150 AT THE LWR STRUT MOUNT AREA. CRACKS MEASURE 1" AND 1.25" RESPECTIVELY. MX REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTIONS IAW Jan 4, 2010 · N231YV · Beech 1900D · Fuselage Main, FrameSDR GLBA20100104HStringer · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND AT STRINGER 4R CUTOUT AT FS 288. IT EXTENDS OUTWARD AND DOWNWARD AT A 45 DEG ANGLE. CRACK IS APPROX .4" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED REQUIRED RII INSPECTIONS IAW EO 09-120Jan 4, 2010 · N231YV · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA20100104GFrame · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MX CRACK WAS FOUND IN THE RT SIDEWALL FRAME AT TS 164 AND STRINGER 9AR CUTOUT. CRACK IS APPROX 1.75" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTIONS IAW EO 09-120-53-001. MATERIALS Jan 4, 2010 · N231YV · Beech 1900D · Fuselage Main, Frame
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