SERVICE MANUAL & ICA
WIPLINE 2100 & 2350 FLOATS
P/N 1002549
Revision N
Page 61
Level the aircraft as per the weight and balance section of the landplane handbook or draw a pencil mark on the
top of the stub gear, 10 3/16” from the front face of the front lift strut attach lug. Drop a plumb bob from the wing
leading edge and lift the tail until the plumb reaches this mark. Plane is now level.
Place the scales under all 4 wheels. Place whatever blocking is required under the main gears to level the aircraft.
Drop the plumb bob from the leading edge to the floor and mark with a line. This line is the datum, 0.0.
Measure the distance from 0.0 to each nose wheel center. This is X1 and X2.
Measure the distance from 0.0 to each main wheel center. This is Y1 and Y2.
If the floats are seaplane floats, the scales go under the step point in the rear and a point towards the front of the
float. These distances are measured and become the same X and Y as for the amphibian.
Use this table for the calculations:
11.7 WEIGHING PROCEDURE FOR 8GCBC SCOUT FLOATPLANE
Totals
Notes:
1. Zero out or deduct tare weights at the Y arms.
2. If using overhead hoist and weight load cell, pick up aircraft at centerline of front spar wing butt fittings. The
centerline of the front spar is +9.0” from the datum. Level the aircraft by placing weight on the float deck to
balance. Record tare weight and arm.
Содержание Wipline 2100
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