C
IRRUS
D
ESIGN
S
ECTION
6: W
EIGHT
AND
B
ALANCE
SR20
W
EIGHT
AND
B
ALANCE
L
OADING
F
ORM
P/N 11934-005
6-5
Weight and Balance Loading Form
• N
OTE
•
The Takeoff Condition Weight must not exceed 3150 lb.
The Takeoff Condition Moment must be within the Minimum
Moment to Maximum Moment range at the Takeoff Condition
Weight. (Refer to Moment Limits).
R
ELATED
T
ABLE
/F
IGURE
:
For Center of Gravity Envelope, refer to
.
Serial Num:............................................................................................................
Date:........................................................................................................................
Reg. Num: ..............................................................................................................
Initials:....................................................................................................................
Figure 6-2:
Weight & Balance Loading Form
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 items 5 and 6
8.
Fuel for start, taxi, and run-up
Normally 9 lb at average moment of
922.8
9.
Takeoff Condition Weight
Subtract item 8 from item 7
Reissue A
