Fouga CM-170 Magister / CM-170-II Super Magister
| Specifications | |
|---|---|
| Country of Origin | France |
| Builder | |
| Role | Armed Trainer, Secondary attack role |
| Similar Aircraft | |
| Wingspan | 40 feet |
| Length | 33 feet |
| Height | 6.5 feet |
| Weight | 4200 pounds empty, 7600 pounds maximum takeoff weight |
| Engine | two 1150 pound thrust Turbomeca Marbore VI Turbojets |
| Maximum speed | 400 KIAS, 0.82 Mach |
| Cruising speed | |
| Range | 575 miles |
| Service Ceiling | 37,000 feet |
| Armament | |
| Crew | one Student and one Instructor |
| Cost | |
| User Countries | |
| Operational | 1956 |
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