SA.321G Super Frelon
The Super Frelon first flew in 1962. The Super Frelon was produced in a civilian transport version and military transport, anti-submarine, and anti-ship versions.
The six-blade main rotor is mounted above center of fuselage. Of the three turboshaft engines, two are mounted side-by-side atop the fuselage forward of main rotor; the third is behind the main rotor. Round air intakes are located above and behind cockpit. Boat-hull type fuselage mounts stabilizing floats on either side of the body, which has fixed landing gear and an upswept rear section. The nose is round with glassed-in cockpit. The tail boom tapers from the main body to the swept-back, tapered fin with a rotor on the left. The single flat is tapered and and flat-mounted on the right side of the fin
Eén uitvoering mogelijk;
Aerospatiale SA.321G Super Frelon - Aéronavale, Flotille 32F, Marine Nationale BAN, Lancéoc-Poulmic 2003.
Aantal onderdelen; 340.
- Lengte: 658 mm.
- Hoogte; 190 mm.
- Rotordiameter; 540 mm.
Humbrol verf kleur nr.'s; 11 / 14 / 19 / 21 / 22 / 24 / 27 / 30 / 33 / 34 / 53 / 56 / 61 / 65 / 79 / 85 / 96 / 102 / 103 / 126 / 127 / 132 / 1321.
Released by Heller in 2004