# N7232R: 1984 Beech B200C, registration cancelled 2024-06-04

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 4, 2024
- Exported to: Netherlands
- Status when cancelled: Valid registration
- Airframe: [Beech B200C](https://openairdocs.org/model/beech-b200c) (registry code 1152924)
- Engine: [Pratt & Whitney Canada PT6A-42](https://openairdocs.org/engine/pratt-whitney-canada-pt6a-42) (registry code 52062)
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE), [TCDS E4EA](https://openairdocs.org/tcds/E4EA) (OpenAirDocs)
- Serial number: BL-69
- Year built: 1984
- Type of aircraft: Fixed wing multi engine
- Engine type: 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](https://openairdocs.org/faa-owner/EASTERN%20STEARMAN%20INC%20TRUSTEE)
- Location: [Leesburg, VA](https://openairdocs.org/faa-place/VA/Leesburg)
- Owner type: Corporation
- Owner's area on the map: 39.1803° N, 77.5335° W: Placed by OpenAirDocs at the center of ZIP code 20176, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N7232R
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=7232R
- Page: https://openairdocs.org/deregistered/N7232R-2024-06-04

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.

ADs and bulletins for the Beech B200C: https://openairdocs.org/model/beech-b200c.md

## Service difficulty reports (9)

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

- [SDR 2011FA0000112](https://openairdocs.org/sdr/2011FA0000112), Feb 15, 2011: DISPLAY. MALFUNCTIONED. THE 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 D
- [SDR 2011FA0000111](https://openairdocs.org/sdr/2011FA0000111), Dec 16, 2010: DISPLAY. MALFUNCTIONED. ON THE EX600 MFD WHICH HAD JUST BEEN INSTALLED IN AUGUST OF 2010, THE PILOT REPORTED THE FOLLOWING MESSAGES WERE DISPLAYED: BROADCAST RECEIVER NOT COMMUNICATING
- [SDR 2009FA0000079](https://openairdocs.org/sdr/2009FA0000079), Feb 3, 2009: DUCT. CRACKED. DURING 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 AN
- [SDR 2008FA0000377](https://openairdocs.org/sdr/2008FA0000377), Jul 1, 2008: SKIN. CRACKED. DURING 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. ADDITIONA
- [SDR 2005FA0000034](https://openairdocs.org/sdr/2005FA0000034), Oct 19, 2004: RELAY. FAILED. WHILE 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 APPROA
- [SDR 2004FA0000524](https://openairdocs.org/sdr/2004FA0000524), Jul 1, 2004: TORQUE TUBE. LOOSE. DURING 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 T
- [SDR 2004FA0000523](https://openairdocs.org/sdr/2004FA0000523), Jun 1, 2004: TORQUE TUBE. LOOSE. DURING 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 T
- [SDR BN001](https://openairdocs.org/sdr/BN001), Oct 17, 2002: STRAP. CRACKED. UPON 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
- [SDR 2001F00087](https://openairdocs.org/sdr/2001F00087), Oct 30, 2000: BRACKET. CRACKED. CRACK 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

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