Bendix 51

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In 1944, Bendix Corporation CEO Ernst Breech ordered the creation of the Bendix Personal Airplane Div. The first aircraft developed by this department was the light multipurpose Bendix 51, released in 1945. Engineer Vern Biasell, who previously worked for Stinson, led the design.

Table of Contents

Design and Concept

The Bendix 51 was a four-seater, twin-boom, high-wing monoplane. It was powered by a 100 hp Franklin 6AC engine, featuring a distinctive pusher propeller configuration.

Variants and Fate

The single prototype (NX34106) underwent testing but did not enter series production. In the same year, an amphibious variant, the Bendix 51A (NX40051), was released. This version differed only in its redesigned lower section, adapted for takeoff and landing from water surfaces. Unfortunately, this amphibious model also failed to attract buyers.

Technical Specifications

Modification	Bendix 51
Wingspan, m	12.19
Length, m	8.60
Wing area, m2	20.25
Empty weight	703
Maximum takeoff weight	1157
Engine type	1 Piston engine Franklin 6AC
Power, hp	1 x 100
Maximum speed, km/h	270
Cruising speed, km/h	252
Crew, crew	1
Payload:	3 passengers

Image and diagram gallery of the Bendix 51

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ArchivoAéreo Editorial Team

A group of aviation researchers and enthusiasts dedicated to documenting and preserving global aeronautical history. All articles are reviewed to ensure historical accuracy.

Sources & Accuracy

The information presented in this technical sheet has been compiled from declassified flight manuals, historical archives, and specialized literature. While we strive for maximum accuracy, some performance data may vary depending on the specific variant or operational conditions.

Bendix 51	Bendix 51
Bendix 51