Construction Specifications

The TIG welded fuselage is faricated from aircraft grade 4130 chrome moly steel tubing. The wings, wing struts, and cross members are fabricated from anodized, 6061 T-6 aluminum. There are eleven ribs per wing assembled on tubular spars. Each wing houses a 9 gallon, fabricated aluminum fuel tank.

The aircraft is covered with treated and painted 3.6oz (90-120g) aircraft grade fabric. The fabric is hand stitched to the wings and horizontal tail surfaces. Flap adjustment can be set to three different positions with a 35 degree maximum.

The Savage features the classic "Taildragger" arrangement. Full swivel tail-wheel enhances ground handling. The main landing gear is fitted with a typical bungee configuration that includes safety cables to prevent over extension. Hydraulic toe brakes are provided for both front and rear.

The two-piece engine cowl provides easy engine access. The large, swing-up door can be opened in flight for greater access and visibility for sight seeing and taking pictures.

Performance & Specifications

VNE:
Top Speed:
Cruise Speed:
Rate of Climb:
Stall Speed:
Max Ceiling:
Cruise Range:
Take-Off Roll:
Landing:
Landing (50ft Obstacle):
MTOW:
Payload:
127mph
117mph
104mph
864ft/min
38mph
14,500ft
380mi
360ft
295ft

623ft
1,235lbs
562lbs
Engine:

Fuel Capacity:
Propeller:
Wing Span:
Fuselage Length:
Overall Height:
Wing Area:
Cabin Width:
Wheelbase:
Max Cross Wind:
Empty Weight:
G-Load Factor:
Rotax 912ULS (100HP)
18 Gallons
Wood, 2-Blade
30ft 6in

21ft
6ft 2in
153sq ft
2ft 6in
5ft 11in
18mph
673lbs
+6/-3

Zlin Aviation, S.R.O.