Question: Match the load condition to the structural component where it is most likely to cause a critical load condition. Upper wing skin ( compression )

Match the load condition to the structural component where it is most likely to cause a critical load condition.
Upper wing skin (compression)
Elevator support structures
Rotation for takeoff
Manoeuvres for a twin engine aircraft with a single engine failure
Vertical tail
Undercarriage
Cabin pressurisation
Crabbed landing
Pull up from a dive
Fuselage skin
Match the load condition to the structural

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