N7232R

Cancelled 2024

Deregistered aircraft · 1984 Beech B200C · Pratt & Whitney Canada PT6A-42

Cancelled
June 4, 2024
Exported to
Netherlands
Status when cancelled
Valid registration
Serial number
BL-69
Year built
1984
Type
Fixed wing multi engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
March 17, 2006
Certificate issued
July 7, 2021
Last registry action
May 14, 2023
Mode S code
A9B15F
Owner when cancelled
Eastern Stearman Inc Trustee
Location
Leesburg, VA
Owner type
Corporation

From the FAA registry file of October 29, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

Service difficulty reports · 9

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR 2011FA0000112Display · malfunctionedTHE PILOT REPORTED THE EX600 MFD DISPLAY REMAINED DIM AND NOT LEGIBLE FOR APPROX 10 TO 15 MINUTES DURING THE ACFT GROUND RUN-UP CHECKS PRIOR TO TAXI. WHEN THE DISPLAY ACHIEVED 'NORMAL' BRIGHTNESS AND WAS READABLE IN DAYLIGHT CONDITIONS, ALL THE ASSOCIATED FUNFeb 15, 2011 · N7232R · Beech B200C · Central DisplaySDR 2011FA0000111Display · malfunctionedON THE EX600 MFD WHICH HAD JUST BEEN INSTALLED IN AUGUST OF 2010, THE PILOT REPORTED THE FOLLOWING MESSAGES WERE DISPLAYED: BROADCAST RECEIVER NOT COMMUNICATING, BROADCAST DATA NOT YET RECEIVED. THE MFD WOULD NOT DISPLAY THE WEATHER DATA FROM THE WSI-301. MDec 16, 2010 · N7232R · Beech B200C · Central DisplaySDR 2009FA0000079Duct · crackedDURING REPLACE OF THE RT ENGINE, AFT LOWER COWLING FWD BULKHEAD P/N 101-910038-3, CRACKS WERE DISCOVERED IN THE LT AND RT COWLING AFT DUCTS P/N 101-910049-11 AND 101-910049-12 UPPER MOUNTING FLANGES. THIS AREA IS ONLY ACCESSIBLE BY REMOVING THE PANEL (DOOR) PFeb 3, 2009 · N7232R · Beech 200CBEECH · Powerplant SystemSDR 2008FA0000377Skin · crackedDURING A PREFLIGHT INSPECTION, MAINTENANCE TECH NOTED A 3.75 INCH LONG CRACK IN THE RT WING LOWER WING SKIN JUST FWD OF THE IB SECTION OF THE OB FLAP. ADDITIONALLY A SUPPORT/ ANCHOR TAB THAT ATTACHES THE LOWER WING SKIN TO THE IB MOST FLAP WELL RIB OF THE OB WJul 1, 2008 · N7232R · Beech B200C · Wing, Plate/SkinSDR 2005FA0000034Relay · failedWHILE THE AIRCRAFT WAS IN FLIGHT, THE FLAPS FAILED TO EXTEND TO THE SELELCTED APPROACH POSITION. THE PILOT CYCLED THE FLAP SELECT SWITCH TO UP AD BACK TO APPROACH AND THE FLAPS EXTENDED. MAINTENANCE INVESTIGATED THE REPORTED PROBLEM AND WAS ABLE TO DUPLICATEOct 19, 2004 · N7232R · Beech B200C · Trailing Edge Flap Control SystemSDR 2004FA0000524Torque Tube · looseDURING AN INSPECTION, THE LT ELEVATOR CORNTOL TORQUE TUBE THAT ATTACHES TO IB END RIB OF THE LT ELEVATOR WAS FOUND TO HAVE PLAY BETWEEN THE ACTUATING HORN AND THE TORQUE TUBE ITSELF. THE COLLAR WITH THE FLANGE AND THE 4 MOUNTING BOLTS ATTACHING THE TORQUE TUBJul 1, 2004 · N7232R · Beech B200C · Elevator Control SystemSDR 2004FA0000523Torque Tube · looseDURING PHASE INSPECTION, THE RT ELEVATOR CONTROL TORQUE TUBE THAT ATTACHES TO THE IB END RIB OF THE RT ELEVATOR WAS FOUND TO HAVE PLAY BETWEEN THE COLLAR WITH THE FLANGE THAT BOLTS TO THE END RIB AND THE TORQUE TUBE ITSELF. THE 4 MOUNTING BOLTS WERE TIGHT TO Jun 1, 2004 · N7232R · Beech B200C · Elevator StructureSDR BN001Strap · crackedUPON REMOVAL OF AIRCRAFT INTERIOR TO TROUBLESHOOT WIRING PROBLEMS, TWO STRAP ASSEMBLIES ON THE RT SIDE OF THE FUSELAGE AT F.S. 227.0 AND 246.0, BUTTOCK LINE 119.0 WERE FOUND COMPLETELY CRACKED THROUGH. THE STRAP ASSEMBLY AT F.S. 246.0. THESE AREAS WOULD NOTOct 17, 2002 · N7232R · Beech B200C · Fuselage Main, FrameSDR 2001F00087Bracket · crackedCRACK WAS DISCOVERED DURING ROUTINE MAINTENANCE. THIS IS THE SECOND BRACKET REPLACED IN THE LAS 400 FLIGHT HOURS, IN BOTH INSTANCES THE CRACK WAS LOCATED AT THE LOWER LEFT CORNER. (M)Oct 30, 2000 · N7232R · Beech B200C · Fuselage Miscellaneous Structure