DIAMOND AIRCRAFT
DA 20/100 Flight Manual
Weight & Balance
Doc # 202-100-VLA
20 December, 2000
Page
DOT-Approved
6 - 2
1.
INTRODUCTION
To obtain the performance, flight characteristics and safe operation described in this Flight Manual, the
airplane must be operated within the permissible weight and balance envelope as described in Chapter 2.
It is the pilot's responsibility to adhere to the weight and balance limitations and to take into consideration
the change of the CG position due to fuel consumption.
The procedure for weighing the airplane and calculating the empty weight CG position are given in this
Chapter.
The aircraft is weighed when new and should be reweighed in accordance with applicable air regulations.
Empty weight and the center of gravity are recorded in a Weighing Report and Weight and Balance
Report as illustrated in the samples in figure 6.1 and 6.2. The actual report for the aircraft is at the end of
this chapter.
In case of equipment changes, the new weight and empty weight CG position must be determined by
calculation or by weighing and must be entered in the Weight & Balance Report. The following pages are
sample forms which can be used for airplane weighing, calculation of the empty weight CG position, and
for the determination of the useful load.
NOTE
After every repair, painting or change of equipment the new empty weight must be
determined as required by applicable air regulations. Weight, empty weight CG position
and useful load must be entered in the Weight & Balance Report by an authorized
person.