Cirrus DESIGN SR20 Information Manual

6-14 P/N 13999-002 Info Manual
Section 6 Cirrus Design
Weight & Balance SR20
Figure 6-6
Weight & Balance Loading Form
Serial Num:_________________Date: _________________________
Reg. Num: _________________Initials: _______________________
• Note •
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).
Item Description
Weight
LB
Moment/
1000
1.
Basic Empty Weight
Includes unusable fuel & full oil
2.
Front Seat Occupants
Pilot & Passenger (total)
3. Rear Seat Occupants
4.
Baggage Area
130 lb maximum
5.
Zero Fuel Condition Weight
Sub total item 1 thru 4
6.
Fuel Loading
56 Gallon @ 6.0 lb/gal. Maximum
7.
Ramp Condition Weight
Sub total item 5 and 6
8.
Fuel for start, taxi, and runup
Normally 6 lb at average moment of 922.8
––
9.
Takeoff Condition Weight
Subtract item 8 from item 7
Weight and Balance Loading Form
September 2011

Cirrus DESIGN SR20 Specifications

General

Brand	Cirrus
Model	DESIGN SR20
Category	Aircrafts
Language	English