DA20-C1 Flight Manual
Supplement 4
Doc # DA202-C1 April 16, 2009 Page S4 - 15
DA 20 (Example) Your DA 20
Calculation of the Load Limits
Weight [lbs]
(Weight [kg])
Moment
[in.lbs]
([kgm])
Weight [lbs]
(Weight [kg])
Moment
[in.lbs]
([kgm])
1. Empty Weight (use the data for your
airplane recorded in the equipment
list, including unusable fuel and
lubricant).
1153
(523)
12562
(144.740)
2. Pilot and Passenger:
Lever Arm: 0.143 m (5.63 in)
359
(163)
2021
(23.286)
3. Baggage:
Max. Wt. 44 lbs (20 kg)
Lever Arm: 0.824 m (32.44 in)
--
(--)
--
(--)
4. Baggage Compartment Extension:
Max. Wt. 44 lbs (20 kg)
Lever Arm: 1.575 m (62.0 in)
--
(--)
--
(--)
5. *Combined Baggage
Max. Wt. 44 lbs (20 kg)
Lever Arm: 1.20 m (47.22 in)
--
(--)
--
(--)
6. Total Weight and Total Moment with
empty fuel tank (sum of 1. - 3.)
1512
(686)
14583
(168.026)
7. Usable Fuel Load
(6.01 lbs. per US gal./0.72 kg per liter)
Lever Arm (32.44 in)
(0.824 m)
93
(42)
3017
(34.762)
8. Total Weight and Total Moment, taking
fuel into account (sum of 6. and 7.)
1605
(728)
17600
(202.788)
9. Find the values for the total weight (1512 lbs and 1605 lbs) and the total moment (14583 in lbs and 17600
in. lbs) in the center of gravity diagram. Since they are within the limitation range, the loading is
permissible.
* Combined Baggage: For convenience of calculation use this line if baggage is to be located in
both the baggage compartment and the baggage extension. The combined total of the baggage
must not exceed 44 lbs (20 kg).
Figure 6.6. Calculation of Loading Condition
Revision 24 DOT Approved
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