Fouga CM.175 Zéphyr

· Fouga · 2 × Turbomeca Marboré

Airplanes

Length

10.06 m

Flat Wing Span

12.15 m

Height

2.8 m

Flat Wing Area

17.3 m²

Max Speed

715 km/h

Max Ceiling

11000 m

Number of Engines

Aircraft Engine

First Flight

1956-07-31

Entry Into service

1959-01-01

Number Built

Maximum Take-Off Weight

3.2 t (paragliders: kg)

Maximum Range

925 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Fouga CM.175 Zéphyr	3.2	925

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Fouga CM.170 Magister	Turbomeca Marboré	10.06	12.15		Compare
Beechcraft Duke		10.0584	11.8872	5	Compare
Cessna 411	Continental IO-520	10.0584	11.8872		Compare
Piper PA-31 Navajo	Lycoming O-540	9.7536	12.192	5	Compare
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PZL-230 Skorpion		10	12.1		Compare

All data (22 fields)

Name: Fouga CM.175 Zéphyr
Manufacturer: Fouga
Description: The Fouga Zéphyr (company designation CM.175) was a 1950s French two-seat carrier-capable jet trainer for the French Navy.
First Flight: 1956-07-31
Entry Into service: 1959-01-01
Service End: 1994-01-01
Designer: Fouga
Length (m): 10.06
Height (m): 2.8
Cockpit Crew: 2
Max Speed (km/h): 715
Max Ceiling (m): 11000
Armament: 2 x 7.5 mm or 7.62 mm machine guns (seldom carried); Up to 100 kg (220 lb) of weapons on two underwing hardpoints.
National Origin: France
Number Built: 32
Powerplant Description: 2 × Turbomeca Marboré IIA turbojets
Primary Users: French Navy
Wikipedia Article (URL): en.wikipedia.org/wiki/Fouga_CM.175_Z%C3%A9phyr
Flat Wing Span (m): 12.15
Flat Wing Area (m²): 17.3
Aircraft Engine: Turbomeca Marboré
Number of Engines: 2