Cirrus SR20 User Manual Page 22

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P - 7 P/N 11935-003
CIRRUS PILOT CHECKLIST MODEL SR20
Weight and Balance
Loading Calculations
For Moment/1000, refer to Loading Data table on following page.
Calculation Instructions
1. Enter the current basic empty weight and moment from the aircraft’s
Weight and Balance Record.
2. Enter the total weight and moment/1000 for the front seat occupants from
the adjacent Loading Data Table.
3. Enter the total weight and moment/1000 for the rear seat occupants from
the adjacent Loading Data Table.
4. Enter the total weight and moment/1000 for the baggage from the
adjacent Loading Data Table.
5. If desired, subtotal the weight and moment/1000 entries from steps 1 - 4.
6. Enter the weight and moment/1000 of usable fuel loaded on the airplane.
7. Subtotal the weight and moment/1000.
8. Enter values for typical start, taxi, and run-up operations of 6 pounds at an
average moment\1000 of 0.922.
9. Subtract step 8 weight and moment/1000 from the Ramp Weight to
determine the Takeoff Weight and moment/1000.
a. Verify Takeoff Weight does not exceed the 3000 pounds.
b. Verify Moment/1000 does falls between the interpolated minimum
and maximum values listed on the adjacent Moment Limits Table.
Description Weight Moment/1000
1. Empty Weight
Includes unusable fuel and full oil
2. Front Seats Occupants
Pilot and Passenger
3. Rear Seats Occupants
4. Baggage
130 lb maximum
5. Zero Fuel Condition
Subtotal items 1 thru 4
6. Fuel Load
56 Gallon @6.0 lb/gal. maximum
7. Ramp Weight
Subtotal items 5 and 6
8. Fuel for start, taxi, and runup
Normally 6 lb at avg. mmnt of 922.8
- -
9. Takeoff Weight
Subtract Item 8 from item 7
July 2011
PERFORMANCE
WEIGHT AND BALANCE
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