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0041
An aircraft is loaded with the CG aft of the aft limit. What effect will this have on controllability?
| * | A) Stall and spin recovery may be difficult or impossible. |
| | B) A stall will occur at a lower airspeed, but recovery will be easier because of reduced wing loading. |
| | C) A stall will occur at a higher indicated airspeed due to the greater downloading on the elevator. |
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