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The SECAT RG-75 (sometimes designated SECAT 75T) was a light utility biplane built in France shortly after World War Two. It was a conventional cabin monoplane with two seats side-by-side. The wing was mounted high and was of fully cantilever design. The conventional undercarriage consisted of two fixed divided main units plus a fixed tailskid. Power was supplied by a tractor-mounted piston engine that drove a two-bladed propeller. Construction was of wood throughout covered in plywood.

The SECAT RG-75 (sometimes designated SECAT 75T) was a light utility biplane built in France shortly after World War II. It was a conventional cabin monoplane with two seats side-by-side.1

Made by SECAT.

Empty Weight Lb
617
Wing Area Sqm
14
Designer
Rémy Gaucher
Eng 1 Type
Regnier 4D2
Ceiling Ft
16400
Eng 1 Kw
52
Span In
10
Gross Weight Lb
1100
Capacity
one passenger
Span Ft
32
Number Built
2
Crew
one pilot
Climb Rate Ftmin
639
Empty Weight Kg
280
Gross Weight Kg
500
Height In
3
Range Km
800
Climb Rate Ms
4
Manufacturer
SECAT
Range Miles
500
Max Speed Mph
112
Max Speed Kmh
180
Height Ft
6
Origin
France
National Origin
France
Wing Area Sqft
151
Met Or Eng
met
Span M
10
Length Ft
23
Height M
2
Ceiling M
5000
Eng 1 Hp
70
Eng 1 Number
1
Length M
7
Category
French civil utility aircraft 1940-1949
SECAT aircraft

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