Trago Mills SAH-1 Aircraft

Sprint 160, RV Smith from British Built Aircraft

Production Details

Design Company:

Trago Mills Ltd (Aircraft Division)

First Flight:

23 August 1983

SAH-1:

1 - Trago Mills

Sprint 160:

5 - FLS Aerospace

Club Sprint:

1 - FLS Aerospace

Type Specification

Applies to:

Orca SAH-1

Type:

Two-seat fully-aerobatic light aircraft

Wing:

Cantilever low-wing monoplane. Tapered, non-swept aluminium alloy wings

Fuselage:

Aluminium alloy stressed skin structure

Tail Unit:

Aluminium alloy cantilever structure. Tailplane attached to fuselage, with horn balanced elevator. Sweptback fin and horn balanced rudder

Landing Gear:

Non-retractable tricycle type with single wheel on each unit

Power Plant:

One 118 hp Textron Lycoming O-235-L2A flat four engine driving a two blade propeller

Accommodation:

Two seats side-by-side in enclosed cockpit

Span:

30 ft 8.5 in

Length:

21 ft 7 in

Height:

7 ft 7.5 in

Wing Area:

120 sq ft

Empty:

1,100 lb

Max Take-off:

1,750 lb

Max Speed:

140 mph

Max Rate of Climb:

915 ft/min

Service Ceiling:

16,400 ft

Range:

714 miles

Preserved in British Museums

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