We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type data
Airframe
Manufacturer
Beechcraft
Model
A45
Year
1952
Serial number
G-39
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
2
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
A3BC18
Engine
Make and model
Cont Motor O-470 Series
Type
Reciprocating
Power
230 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records
2021 – nowN34MR LLCOrlando, FL · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 2026 · SDRs · Oct 16, 2026
NTSB events (1)
Accident · substantial damage
Feb 21, 2003 · Merritt Island, FL
The separation of both propeller blades in-flight for undetermined reasons and the failure of the pilot to attain the proper touchdown during the forced landing resulting in overrun during landing and subsequent collapse of the nose landing gear. A contributing factor in the accident was the reduced visibility due to grease on the windscreen following separation of both propeller blades.
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (1)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
Landing gear · idler arm · frozenAug 26, 1997
WHILE TAXIING, A SQUEAK WAS HEARD FROM THE NOSE WHEEL AREA. WITH THE AIRCRAFT ON JACKS, THE NOISE WAS ISOLATED TO THE STEERING ROD IDLER ARM, P/N 35-825052-2. THE ONLY WAY TO INSPECT THIS PART IS TO REMOVE THE ENTIRE COLLAR AND SHAFT. THE IDLER ARM SHOULD BE FREELY MOVABLE ON THE SHAFT. IN THIS…
From FAA Service Difficulty Reports; matched by N-number and serial number.