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How to establish forward CG limit
Aviatordan created the topic: How to establish forward CG limit
How's life treating you? It's good to be back on the forum, it's been a while.
I have a question regarding finding the forward CG limit on a C182Q.
The Flight Manual states:
- 1005 mm aft of the datum at 2950 lbs; and
- 839 mm aft of the datum at 2249 lbs.
- Linear variation applies between 2249 and 2950 lbs.
How do I establish a formula to establish the CG limit? I remember for the Echo it was (present weight - 2360) X.27 + 2400.