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
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
