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
Boeing
Model
E75N1
Year
1943
Serial number
75-8520
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
A0D867
Engine
Make and model
Cont Motor W670 Series
Type
Reciprocating
Power
250 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records
2017 – nowLegacy Biplane LLCStanley, NC · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 2026 · SDRs · Oct 16, 2026
NTSB events (2)
Accident · substantial damage
Nov 4, 1995 · Wauchula, FL
A TOTAL LOSS OF ENGINE POWER DUE TO WORN SERRATED TEETH ON THE VALVE TIMING GEAR AND INTERMEDIATE CAMSHAFT DRIVE GEAR WHICH PREVENTED THE VALVE TRAIN AND GENERATOR FROM OPERATING. A FACTOR WAS THE LACK OF SUITABLE TERRAIN FOR THE FORCED LANDING.
FAILURE OF THE PILOT TO MAINTAIN DIRECTIONAL CONTROL WHICH RESULTED IN AN INADVERTENT GROUND SWERVE. THE CROSSWIND AND THE PILOT'S IMPROPER USE OF BRAKES WERE CONTRIBUTING FACTORS.
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.
No ADs published since 1998 matched this airframe or engine model.
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.
Reciprocating engine · gear · wornJan 16, 1995
WEAR FOUND ON VALVE TIMING SERRATED GEARS ON REAR CRANKSHAFT AND STARTER GEAR. SUBMITTER RECOMMENDS REMOVING TACHOMETER DRIVE AND INSPECT REAR CRANKSHAFT NUT FOR PROPER TORQUE AT EVERY ANNUAL INSPECTION.
From FAA Service Difficulty Reports; matched by N-number and serial number.