The history of the Boeing L-15 reconnaissance aircraft

The L-15 reconnaissance aircraft was a light and small observation liaison aircraft produced by Boeing Aircraft Company after World War II in limited quantities - only 12 were produced, with the US Army as its main operator. The first flight took place on July 13, 1947, with production spanning from 1947 to 1949.

The L-15 reconnaissance plane represents a new direction for Boeing in a postwar world that no longer needs the high productivity and cutting-edge design of piston-engine fighter jets. The all-metal construction L-15 is designed for short take-off and landing (STOL) operations - any terrain that could have an impact on other large aircraft - and is designed for light reconnaissance aircraft observation missions (where the aircraft provides all-round visibility), Boeing is trying to Diversify its products in the post-war economy.

The L-15 was developed at Boeing's Wichita, Kansas facility.

The L-15 Scout features a unique exterior configuration. The aircraft features high-mounted monoplane wing assemblies fitted with "flaperons," which double as ailerons and flaps. Two crew members, including the pilot and observer, sat in a glass pod fuselage under the main wing of the wing. The engine is mounted at the very forward end of the fuselage, and the tail extends to the rear of the aircraft.

The rear is clearly decorated with two vertical rear fins. The landing gear is a traditional "trailer" with two main gears and a tail wheel. All parts are fixed (units are not retracted), the tail wheel is located under the rear of the fuselage nacelle. The size of the aircraft makes it suitable for transport on a C-97 aircraft, once disassembled for travel.

If the mission requires, the L-15 can also be equipped with twin pontoons for water landings.

Power comes from a single 125 hp Lycoming O-290-7 series flat-four, air-cooled. Top speed is 112 mph and 16,400 feet per hour. The plane can climb at 628 feet per minute, and the power handling is reported to be excellent.

As fate would have it, the L-15 was not a financial success and became Boeing's last single-engine product for the light aircraft market. As can be seen from the text, no fixed L-15 reconnaissance contract was signed.

Specification

Basic

Year:
1947
Status:
Retired, out of service
Staff:
2

Production

[12 units] :
Boeing Wichita - USA

Roles

- Naval/Navigation

- Reconnaissance (RECCE)

Dimensions

Length:

25.00 ft (7.62 m)

Width:

12.19m

Height:

2.65m

Weight

Curb Weight:

686 kg

MTOW:

932 kg

(Difference: +542lb)

Performance

1 x Lycoming 0-290-7 125hp piston engine driving a two-bladed propeller unit in the nose.

Performance

Maximum Speed:

180 km/h (97 knots)

Service Limit:

16,398 ft (4,998 m; 3.11 mi)

Rate of climb:

628 ft/min (191 m/min)

Armor

No.

Changes

L-15 - Base Series Name

YL-15

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