Weight And Balance Loading Form - Cirrus SR22 Pilot Operating Handbook

C D
IRRUS ESIGN
SR22

Weight and Balance Loading Form

The Takeoff Condition Weight must not exceed 3600 lb.
The Takeoff Condition Moment must be within the Minimum
Moment to Maximum Moment range at the Takeoff Condition
R T
ELATED ABLE
For Center of Gravity Envelope, refer to
Serial Num:............................................................................................................
Date:........................................................................................................................
Reg. Num: ..............................................................................................................
Initials:....................................................................................................................
Figure 6-2: Weight & Balance Loading Form
Item
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
3400 lb maximum
6. Fuel Loading
92 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 1394
9. Takeoff Condition Weight
Subtract item 8 from item 7
P/N 13772-006
Reissue A
Weight. (Refer to Moment Limits).
/F :
IGURE
Description
S
ECTION
W
EIGHT AND
• N •
OTE
Section 2:
Weight
6: W
EIGHT AND
B L
ALANCE OADING
Limitations.
LB Moment/1000
B
ALANCE
F
ORM
6-5