FOUG
FOUGA CM-175 Zephyr
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
Manufactured as
VALMET CM-170R Magister
VALMET Magister
SUD CM-170R Magister
SUD Magister
SUDFLUG CM-170R Magister
SUDFLUG Magister
POTEZ Magister
POTEZ CM-175 Zephyr
POTEZ CM-170R Magister
POTEZ AIR-FOUGA CM-170R Magister
POTEZ AIR-FOUGA Zephyr
POTEZ AIR-FOUGA CM-175 Zephyr
POTEZ AIR-FOUGA Magister
POTEZ Zephyr
IAI Tzukit
IAI CM-170R Magister
IAI CM-170R Tzukit
IAI Magister
FOUGA Magister
FOUGA CM-170R Magister
AIR-FOUGA CM-170R Magister
AIR-FOUGA Magister
AEROSPATIALE Magister
AEROSPATIALE CM-170R Magister
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 (metric)
12.15 m
Length (metric)
10.06 m
Height (metric)
2.80 m
Powerplant
2 x Turbomeca Marboré IIA turbojets, 3.92 kN each
Engine Model(s)
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
