Weight & Balance Loading Form - Cirrus DESIGN SR20 Information Manual

Section 6
Weight & Balance
Weight & Balance Loading Form
Serial Num:_________________Date: _________________________
Reg. Num: _________________Initials: _______________________
Item
Basic Empty Weight
1.
Includes unusable fuel & full oil
Front Seat Occupants
2.
Pilot & Passenger (total)
3. Rear Seat Occupants
Baggage Area
4.
130 lb maximum
Zero Fuel Condition Weight
5.
Sub total item 1 thru 4
Fuel Loading
6.
56 Gallon @ 6.0 lb/gal. Maximum
Ramp Condition Weight
7.
Sub total item 5 and 6
Fuel for start, taxi, and runup
8.
Normally 6 lb at average moment of 922.8
Takeoff Condition Weight
9.
Subtract item 8 from item 7
The Takeoff Condition Weight must not exceed 3000 lb. All weights above 2900 lb
must consist of fuel.
The Takeoff Condition Moment must be within the Minimum Moment to Maximum
Moment range at the Takeoff Condition Weight. (Refer to Figure 6-8, Moment
Limits).
6-14
Description
Figure 6-6
Weight and Balance Loading Form
• Note •
Cirrus Design
Weight Moment/
LB
–
P/N 13999-002 Info Manual
September 2011
SR20
1000
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