Pilot Operating Handbook
Section 6
TL-2000
Sting
Weight & Balance Information
Notice! The information contained in this document is for reference and information only.
The pilot is the final and only responsible party for the safe operation of this aircraft.
31 December 09 / Chg 5
6-10
Copyright © 2009 Reproduction of this document or any of its parts is forbidden.
An aircraft log book entry should be made whenever a Weight Balance calculation is
performed, indicating date, and nature of change, results and name of person
performing the calculation. (An entry moment arm is included in the sample should
any changes be made to the instrument panel.) This document, in its entirety,
becomes a part of the Aircraft Legal Documents. It must be kept aboard the aircraft
and made available for inspection upon request.
WEIGHT & BALANCE DATA WORKSHEET NOTES
1.
Datum Plane:
Forward tip of nose cone at propeller.(prevents neg calcs)
2.
Maximum Forward CG Limit:
80.2 inches aft of Datum
3.
Maximum Aft CG Limit:
86.7 inches aft of Datum
4.
Maximum Gross Weight:
1320 pounds
5.
Maximum Seat Load:
250 pounds
6.
Minimum Pilot Weight:
100 pounds
7.
Maximum Main Fuel:
120 pounds
8.
Maximum Wing Fuel:
72 pounds
9.
Maximum Baggage Weight:
60 pounds (25 pounds used in example)
