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You are here: home->amg->C02->C.8.1.7.2.A.1
8172
Improper loading of a helicopter which results in exceeding either the fore or aft CG limits is hazardous due to the
| | A) Coriolis effect being translated to the fuselage. |
| | B) reduction or loss of effective collective pitch control. |
| | C) reduction or loss of effective cyclic pitch control. |
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