Variants
The United States Navy and Marine Corps utilized the type under the designation of "OY-1". The later-production OY-2, missing out on service in World War II, was a refinement of the line by way of a 24-volt-based electrical system over the original 12-volt installation. The British acquired exactly 100 L-5 Sentinels for their part in the war and this stock encompassed both L-5 and L-5B models (variants detailed below). The British redesignated these American aircraft by naming them simply as "Sentinel I" and "Sentinel II", respectively. Many L-5 aircraft were used in the post-war period across civilian industries and sold to American allies abroad.
The line began with the "O-62" with its Lycoming O-435 piston engine of which 275 were built to the standard. The first L-5 totaled 1,538 aircraft and were known to the USN and USMC services as the OY-1 (the OY-1 designation encompassed the L-5, L-5B, L-5C, and L-5E production types).
The L-5A was a cancelled version intended to carry a "Ranger" engine of 200 horsepower as well as 24 volt electrical system. The L-5B made it to production and numbered 712 examples - these differentiated by having an easy-access rear fuselage door and they could furthermore accept a float undercarriage for water landings. The L-5C was finished with a camera mount accommodating the K20 reconnaissance camera for photographic work. The L-5D designation was skipped which led to the L-5E produced in 500 examples with drooping ailerons providing better low-speed control. 200 L-5E-1 Sentinels were equipped with larger tires and heavy duty brakes, featured a 24 volt electrical system and SCR-274 radio package. It was powered by a revised Lycoming O-435-11 engine. 115 of this mark were produced.
The United States Army Air Forces (USAAF) then became the United States Air Force (USAF) and, in 1962, the aircraft were redesignated. The few Sentinels remaining in inventory became the U-19A (12 volt models) and the U-19B (24 volt models). The L-5/235 is a variant fitted with a 235 horsepower Lycoming O-540 engine. These aircraft were modified for Italy for glider towing. The XL-5F was an L-5B modified with a 24 volt electrical system and radios that served as the prototype for the L-5G. In 1948, this airplane was fitted with a geared Lycoming GO-435 engine and an experimental 5-bladed propeller. It was used in "Quiet Airplane" experiments at Langley Research Center (Virginia) and became an early American attempt at designing a "stealth" aircraft.
L-5 Stinson Walk-Around
The L-5 had a crew of two seated in tandem. Overall length of the aircraft was 24 feet with a wingspan reaching 34 feet and a height of nearly 8 feet. Empty weight was just 1,550lb with a possible MTOW of 2,050lb. Power was from a single Lycoming O-435-1 engine of 185 horsepower driving a two-bladed propeller at the nose. The military never-exceed speed was 200 mph in a dive but limited to 163 mph for civil certification. The maximum range was out to 375 miles with no fuel reserves. Its service ceiling reached 15,800 feet and rate-of-climb was 900 feet-per-minute at sea level.
Note
Special Thanks to James H. Gray / Sentinel Owners & Pilots Association for his insightful contributions to this entry.
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