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FOUGA CM-175 Zephyr

From SKYbrary Wiki

FOUG
Aircraft
Name CM-175 Zephyr
Manufacturer FOUGA
Body Narrow
Wing Fixed Wing
WTC Light
Type code L2J
Engine Jet
Engine count Multi
Mass group 2


Manufacturered as:

AEROSPATIALE Magister
AEROSPATIALE CM-170R Magister
AIR-FOUGA CM-170R Magister
AIR-FOUGA Magister
FOUGA Magister
FOUGA CM-170R Magister
IAI Tzukit
IAI CM-170R Magister
IAI CM-170R Tzukit
IAI Magister
POTEZ Zephyr
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
SUD CM-170R Magister
SUD Magister
SUDFLUG CM-170R Magister
SUDFLUG Magister
VALMET CM-170R Magister
VALMET Magister


FOUGA CM-175 Zephyr

FOUGA CM-175 Zephyr

Description

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 m39.862 ft <br />
Length 10.06 m33.005 ft <br />
Height 2.80 m9.186 ft <br />
Powerplant 2 x Turbomeca Marboré IIA turbojets, 3.92 kN each
Engine model Turboméca Marboré

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
Descent
(to FL100)
Descent (FL100
& below)
Approach
V2 (IAS) kts IAS kts IAS kts IAS kts MACH TAS 240 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance 930 m ROC ft/min ROC ft/min ROC ft/min ROC ft/min MACH 0.41 ROD ft/min ROD ft/min MCS kts Distance 1100 m
MTOW 40004,000 kg <br />4 tonnes <br /> kg Ceiling FL400 ROD ft/min APC
WTC L Range 880880 nm <br />1,629,760 m <br />1,629.76 km <br />5,346,981.631 ft <br /> NM

Accidents & Serious Incidents involving FOUG

None on SKYbrary