What is the ultimate positive load before structural failure for the following aircraft? | Cheap Nursing Papers
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What is the ultimate positive load before structural failure for the following aircraft?

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What is the ultimate positive load before structural failure for the following aircraft?

Aircraft weight 20000lbs

aerobatic catagory aircraft = (+6g, -3g) EXPLAIN ANSWER

-9000lbs

-30000lbs

-120,000lbs

-180,000lbs

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