Interceptor I400M
Model Specifications
3.1.4 Areas. The following descriptive information is not to be used for inspection purposes.
| Wing | ||
| Wing area, total, including ailerons, flaps and fuselage projections | 160.0 sq ft | |
| Wing flap area, total | 22.4 sq ft | |
| Aileron area | 10.8 sq ft | |
| Horizontal Tail Surface | ||
| Horizontal tail area, total | 38.0 sq ft | |
| Elevator, aft of hinge line | 12.96 sq ft | |
| Vertical Tail Surface | Vertical tail area, total | 20.4 sq ft |
| Rudder, aft of hinge line, including tab area | 10.3 sq ft |
3.1.5 Dimensions and General Data. The following dimensions and data are for descriptive purposes and not to be used for inspection.
| Wing | ||
| Span, maximum | 30.5 ft | |
| At root | 85.0 in | |
| At tip | 40.0 in | |
| Mean aerodynamic chord | 65.55 in | |
| Airfoil section designation and thickness (percent chord) | ||
|
At root |
NACA 23015 | |
| At Sta 62.0 | NACA 23012 | |
| At tip | NACA 4412 | |
| Incidence | ||
| At root | 3.0 deg | |
| At Sta 62.0 | 3.0 deg | |
| At tip | -2.0 deg |
I400M Intro - Top & Side View - Front & Armament View - Mission Profiles
Paul M. Whetstone, President
Email pwhetstone@meyersaircraft.com
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