Pilot Operating Handbook - Ecoflight.ch

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Rev. 02 – July 16 th , 2009 4 Weight-and-Balance-Information Table of Contents Paragr. Description Page 4.1 Installed Equipment List 4-2 4.2 Weight and Balance Form 4-2 4.3 Center of Gravity (CG) Range and Determination 4-3 4.4 CG-Calculation 4-4 4.5 Calculation Example 4-5 4.6 CG-Diagram 4-6 4.7 Aircraft Specific Weights 4-6 Weight and Balance Information 4 - 1
Rev. 02 – July 16 th , 2009 4 Weight-and-Balance-Information 4.1 Installed Equipment List To meet the requirements of the LSA airworthiness standard, the listed minimum instrumentation is provided as basic equipment. • Airspeed indicator • Altimeter • Compass • RPM gauge • Oil -pressure and -temperature gauge • Position- and tail lights • Anti Collision Light • Master-, avionics and engine kill (ignition) swit<strong>ch</strong> • Electrical system including circuit breakers • 4-point safety belts for pilot and passenger If the aircraft shall be operated N-VFR an altitude indicator must be installed. 4.2 Weight and Balance Form The equipment list including all additional and optional equipment is to be listed in the provided weight and balance form. The CG determination shall refer to the valid weight and balance form. Weight and Balance Information 4 - 2
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