.

Piper AE- NE- HE- Cup

.
.
.
 

Development

Entwicklung

     
.
 

Variants

Versionen

 

HE-1
AE-1

-

HE-1
AE-1

-

 

NE-1

-

NE-1

-

 

NE-2

-

NE-2

-

.
 

Operational history

Einsatzgeschichte

 

The HE-1 was an ambulance version of the Piper Cub and 100 were ordered. The rear fuselage hinged up to permit loading of a single patient on a stretcher. In 1943 the remaining HE-1s were redesignated as AE-1.
A training version with dual controls, 230 were ordered as NE-1 and 20 as NE-2.
In February 1944 two NE-1s were used to test the use drone aircraft in combination with M type airships to bomb submarines.

Bestellt

.
 

Drawings

Zeichnungen

  ..

..

   
 

-

   
.
 

Specifications

Technische Daten

Specifications

Piper L-4J

Wingspan

Spannweite

10.76 m

Length

Länge

6.88 m

Height

Höhe

2.02 m

Wing area

Flügelfläche

16.54 m2

Engine

Motor

Lycoming 0-290-D2 C
flat four 125 hp

Maximum speed

Höchstgeschwindigkeit

201 Km/h

Empty weight

Leergewicht

474 Kg

Loaded weight

Startgewicht

710 Kg

Climb Rate

Steigrate

4.4 m/s

Service ceiling

Gipfelhöhe

5'215 m

Range

Reichweite

400 Km

Armament

Bewaffnung

none
Capacity Zuladung 1 Pilot, 1 Passenger
.
Serial, Piper NE HE- Cup

NE-1

26196 - 26425

230

NE2

29669 - 29688

20

NE2

29689 - 29698

(10)

AE-1

30197 - 30296

100

Total

350


-

last update 27. June 2015

written 27. June 2015

-

-
- Corrections, additions and remarks please send to the Web master Michael E. Fader -
- If information from this site is used as source material please credit www.wings-aviation.ch  -
- If this page does not have a navigational frame on the left, click HERE to see the rest of the website. -