The Vigilant was designed in response to a 1938
United States Army Air Corps design competition for a two-seat light observation aircraft. After the German-manufactured
Fieseler Storch was demonstrated at the 4th International Air Meet in Zurich, Switzerland in 1937, the Air Corps Material Division at Wright Field initiated a feasibility study for the creation of a similar aircraft. The development program was approved in January 1938, design and performance specifications were determined in April 1938, and a Circular Proposal for a formal design competition was released to manufacturers in August 1938, just twelve days before a Storch was demonstrated at the Cleveland Air Races by German aviator Emil Kropf. Stinson (later a division of
Vultee), won the $1.5 million contract over 11 competitors, including the
Bellanca YO-50 and
Ryan YO-51 Dragonfly. Stinson won the $1.5 million contract with an initial order for 100 aircraft. Eleven competing designs included the
Bellanca YO-50 and
Ryan YO-51 Dragonfly that were each runners-up and garnered 3-plane contracts for further evaluation. The Stinson Model 74 was a radial-engined, high-wing monoplane with large trailing-edge slotted flaps and full-span leading-edge automatic slats for low-speed, high-lift, short-field performance. The Model 74 prototype was given the Army designation
YO-49 for evaluation, with the first flight by test pilot Al Schramm on 15 July 1940. The aircraft was built of chrome-molybdenum steel tubing and covered with doped cotton fabric; the engine cowling and the fuselage, forward of the wing, was fully enclosed in aluminum. Control surfaces and the
empennage were fabric-covered
stainless steel. The Lycoming power plant was hand-cranked with an inertial starter and was fitted with a
Hamilton Standard constant speed propeller. At least 12 ambulance conversions were fitted with
Edo 49-4000 floats (4,000-pound
displacement) for amphibious landings and takeoffs. The Vigilant could maintain stable, level flight at 31 miles per hour and in a 20 mph breeze it was capable of stopping in less than its own length. Given an adequate headwind, it gave the illusion of "hovering" and sometimes surprised onlookers by drifting backward. Under calm conditions the L-1 could land and take off again inside a 200 foot diameter circle, and landing over a 50-foot obstacle it could stop on dry sod within 300 feet with a ground roll of approximately 100 feet. ==Operational history==