Extra EA 400 - Conversion to U.S. Units

Section 1 Pilot’s Operating Handbook
General EXTRA 500
Unusable Fuel Fuel remaining after a runout test has been completed in
accordance with certification basis.
Standard
Empty Weight
Weight of a standard airplane including unusable fuel, full
opera ting fluids and full oil.
Basic Empty
Weight
Standard empty weight plus optional equipment.
Payload Weight of occupants, cargo and baggage.
Useful Load Difference between takeoff weight, or ramp weight i
f
applicable, and basic empty weight.
Zero Fuel
Weight
Basic empty weight plus payload but no usable fuel.
Maximum
Ramp Weight
Maximum weight approved for ground maneuver. (It includes
weight of start, taxi and run up fuel.)
Maximum
Takeoff
Weight
Maximum weight approved for the start of the takeoff run.
Maximum
Landing
Weight
Maximum weight approved for the landing touchdown.
Minimum
Weight
Standard empty weight plus minimum crew (1 pilot) and fuel
for half an hour operating the airplane at maximum continuous
power.
Maximum
Empty Weight
Maximum approved empty weight of airplane including
unusable fuel, full operating fluids and full oil.
1.6 Conversion to U.S. Units
Multiply kg by 2.2 to obtain lbs.
Multiply m by 39.37 to obtain in.
Multiply kgm by 0.866 to obtain in.lbs./100
1-18 26. January 2011