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Which consequence results when hydraulic retraction failure occurs during aircraft landing sequence?

A)Asymmetric thrust or lift develops
B)Inadequate strut compression ensues, damaging fuselage
C)The gear door fails to close
D)Increased roll moment occurs inflight

💡 Explanation

Incomplete hydraulic extension leads to inadequate strut compression during ground impact; therefore, the energy absorption capacity is reduced causing structural damage to the fuselage during landing impact, rather than distributed load mitigation because the oleo strut mechanism requires proper function.

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