Langley NL-
Aircraft of the U.S. Navy
Entwicklung
The XNL-1 was a twin engined basic trainer with a Vidal plastic-bonded mahogany plywood construction. One was built by Langley Aviation.
Versionen
XNL-1
-
XNL-1
-
Zeichnungen
-
| 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 |
| Serial, Langley NL- | ||
|
XNL-1 |
39056 |
1 |
|
Total |
1 |
|
