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Langley NL-

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Aircraft of the U.S. Navy

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Development

Entwicklung

The XNL-1 was a twin engined basic trainer with a Vidal plastic-bonded mahogany plywood construction. One was built by Langley Aviation.

 

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Variants

Versionen

 

XNL-1

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XNL-1

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Drawings

Zeichnungen

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Specifications

XNL-1

Wingspan

Spannweite

10.72 m

Length

Länge

6.30 m

Height

Höhe

2.15 m

Wing area

Flügelfläche

?

Engine

Motor

2 x Franklin 4-AC-199-F3  engine, 90 hp each

Maximum speed

Höchstgeschwindigkeit

217 km/h

Empty weight

Leergewicht

639 Kg

Loaded weight

Startgewicht

1'043 Kg

Climb Rate

Steigrate

?

Service ceiling

Gipfelhöhe

4,100 m

Range

Reichweite

640 km

Armament

Bewaffnung

none

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Serial, Langley NL-

XNL-1

39056

1

Total

1


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last update 1. December 2015

written 13. Oktober 2015

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