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BE A36 Weight and Balance Calculator (serial numbers E1371-2110)

A weight and balance calculator for the Beech Bonanza A36

A weight and balance calculator for the Beech Bonanza A36

BE A36 Weight and Balance Calculator (serial numbers E1371-2110)

by Alicia Sikes
BE A36 Weight and Balance Calculator (serial numbers E1371-2110)
BE A36 Weight and Balance Calculator (serial numbers E1371-2110)
BE A36 Weight and Balance Calculator (serial numbers E1371-2110)

What is it about?

A weight and balance calculator for the Beech Bonanza A36. This calculator is for serial numbers E1371-2110 (1979-1983). If your aircraft has tip tanks, please use the tip tank version of this app. Enter the weight (in pounds) for each position in the aircraft, and the amount of fuel (in gallons), and the calculator will let you know if you are out of limits on weight or CG. The forward and aft CG limits are calculated using formula derived from the aircraft limit chart. You can move the arm positions for the forward two rows of seats, the aft row is locked per the POH. Correct cargo and bag loading is verified.

BE A36 Weight and Balance Calculator (serial numbers E1371-2110)

App Details

Version
2.0
Rating
NA
Size
1Mb
Genre
Utilities Lifestyle
Last updated
July 16, 2015
Release date
November 10, 2010
More info

App Screenshots

BE A36 Weight and Balance Calculator (serial numbers E1371-2110) screenshot-0
BE A36 Weight and Balance Calculator (serial numbers E1371-2110) screenshot-1
BE A36 Weight and Balance Calculator (serial numbers E1371-2110) screenshot-2
BE A36 Weight and Balance Calculator (serial numbers E1371-2110) screenshot-3

App Store Description

A weight and balance calculator for the Beech Bonanza A36. This calculator is for serial numbers E1371-2110 (1979-1983). If your aircraft has tip tanks, please use the tip tank version of this app. Enter the weight (in pounds) for each position in the aircraft, and the amount of fuel (in gallons), and the calculator will let you know if you are out of limits on weight or CG. The forward and aft CG limits are calculated using formula derived from the aircraft limit chart. You can move the arm positions for the forward two rows of seats, the aft row is locked per the POH. Correct cargo and bag loading is verified.

If proposed fuel burn is entered (in gallons), a landing CG check is performed. Proper cargo loading positions are also checked- an invalid loading configuration will not add the cargo weight and moment to the aircraft calculations.
Bonus material! A quick reference for the aircraft V-speeds and other interesting aircraft specific numbers.

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