FOUGA CM-175 Zephyr

Aircraft
Name: 
CM-175 Zephyr
Manufacturer: 
Body: 
Narrow
Wing: 
Fixed Wing
WTC
L
Type Code: 
L2J
Engine: 
Jet
Engine Count: 
Multi
Manufacturered as
AEROSPATIALE CM-170R Magister
AEROSPATIALE Magister
IAI CM-170R Magister
IAI CM-170R Tzukit
IAI Magister
IAI Tzukit
SUD CM-170R Magister
SUD Magister
VALMET CM-170R Magister
VALMET Magister
AIR-FOUGA CM-170R Magister
AIR-FOUGA Magister
FOUGA CM-170R Magister
FOUGA Magister
POTEZ CM-170R Magister
POTEZ CM-175 Zephyr
POTEZ Magister
POTEZ Zephyr
POTEZ AIR-FOUGA CM-170R Magister
POTEZ AIR-FOUGA CM-175 Zephyr

FOUG

The Fouga Zéphyr (company designation CM.175) was a 1950s French two-seat carrier-capable jet trainer for the French Navy. It was developed from the land-based CM.170 Magister.

Technical Data
Wing span: 
12.15 m
Length: 
10.06 m
Height: 
2.80 m
Powerplant: 

2 x Turbomeca Marboré IIA turbojets, 3.92 kN each

Engine Model: 
Turboméca Marboré
Indicative Performance Data
Take-Off
V2: 
n/a
Distance: 
930 m
MTOW: 
4000 kg
Initial Climb (to 5000 ft)
IAS: 
n/a
ROC: 
n/a
Initial Climb (to FL150)
IAS: 
n/a
ROC: 
n/a
Initial Climb (to FL240)
IAS: 
n/a
ROC: 
n/a
MACH Climb
MACH: 
n/a
ROC: 
n/a
Cruise
TAS: 
240 kts
MACH: 
0.41
Ceiling: 
400
Range: 
880 NM
Initial Descent (to FL240)
MACH: 
n/a
ROD: 
n/a
Descent (to FL100)
IAS: 
n/a
ROD: 
n/a
Descent (FL100 & below)
IAS: 
n/a
MCS: 
n/a
ROD: 
n/a
Approach
Vapp (IAS): 
n/a
Distance: 
1100 m

SKYbrary Partners:

Safety knowledge contributed by: