Let’s consider we need to design avionics system for general aviation aircraft. If empty weight of aircraft is 100 unit then what will be the approximate range of required avionics weight.(a) 1 unit to 3 unit(b) 0.3 to 0.5 units(c) 0.58 units(d) 4 to 5 unitsThe question was posed to me in an international level competition.This intriguing question comes from Subsystems topic in division Landing Gear and Subsystems of Aircraft Design

Let’s consider we need to design avionics system for general aviatio

1.	Let’s consider we need to design avionics system for general aviation aircraft. If empty weight of aircraft is 100 unit then what will be the approximate range of required avionics weight.(a) 1 unit to 3 unit(b) 0.3 to 0.5 units(c) 0.58 units(d) 4 to 5 unitsThe question was posed to me in an international level competition.This intriguing question comes from Subsystems topic in division Landing Gear and Subsystems of Aircraft Design
Answer» The correct answer is (a) 1 unit to 3 unit For EXPLANATION: Given, empty WEIGHT, W = 100 unit. Typically, RANGE of avionics weight can be ESTIMATED as follows. Avionics weight range = 0.01W to 0.03W = 0.01100 to 0.03100 = 1 unit – 3 unit.

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