FA-62B 10.2cc 4-stroke Methanol engine

Saito FS-62B 10.2cc 4-Stroke Methanol Engine

This engine is designed and manufactured based on high efficiency and durability of the first AAC method in the world. AAC: Aluminum Piston, Aluminum Cylinder - Hardchrome Plated. SAITO FA-62B engines have been designed placting emphasis on the lightweight and compact.

Features:

• Cylinder: By the monolithic structure of cylinder head and cylinder with direct hard chrome plated inner surface without using cylinder liner, this engine emphasizes durability while it also offers lightweight and distortion-free structure with improved cooling efficiency.
• Piston: High silicon content aluminum is used in the piston construction. It also has a compression ring that increases the engine’s efficiency.
• Crankshaft: Made of solid chrome molybdenum steel, and supported by two ball bearings.
• Combustion chamber: Increased combustion efficiency with improved hemispherical shape.
• Exhaust sound: Real-plane-like exciting exhaust sound.
• Weight: Lightest level in the class.
• Mounting dimensions: The same with those of FA-50 & 56.

Specs:

• Application: 4-stroke .50 or 2-stroke .30-.40 class airplanes
• Displacement: 10.24 cc
• Stroke: 19.0 mm
• Bore: Ø26.2 mm
• Motor weight: 420 g (Approx. 470 g with muffler)
• Practical RPM Range: 2000-11.500
• Max RPM on the ground (stationary): 9500-10.500
• Propeller size: APC 12x6"-12x8" & 13x5"-13x6"
• Propeller Static thrust APC 12x6": 2.3 kg / APC 13x6": 2.5 kg
• Fuel: Good quality modelfuel with synthetic oil and 10-20% nitro content
• Fuel consumption: Aprox. 20 cc/min (At full throttle 10.200 rpm)

Thrust info:

• Engine: FA-62B
• Propeller: 13x6
• Static Thrust: 2.6kg
• Max weight for hover capability: 2.6kg
• Rec. Max weight for sportsman flying: 3.7kg
• Max weight for possible take-off: 5.2kg