ENSTROM 280FX OPERATOR’S MANUAL 6-11
Rev. 11
Report No. 28-AC-020 Sep 20/17
Figure 6-5. Gross Weight vs. Longitudinal Moment
NOTE
Figures 6-6 through 6-10 are an adaptation
of Enstrom Form F-168A, which is used for
current production aircraft as of the date
of this revision. Refer to the actual weight
and balance records for the aircraft.
This electronic document is not linked to a subscription for revision control or distribution. Refer to theTechnical
Publications Status link under the Technical Support Page of the Enstrom Helicopter website for the current revision
level of the 280FX Rotorcraft Flight Manual.
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