81-06. Limitations
All questions: 58
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1. Which of the following statements is true?
2. An aircraft is flown at 20% below its normal weight. Because of this, VA will be:
3. Which statement regarding the gust load factor on an aeroplane is correct (all other factors of importance being constant)?
1) Increasing the aspect-ratio of the wing will increase the gust load factor.
2) Increasing the speed will increase the gust load factor.
4. Aileron reversal at high CL results from:
5. Load factor is:
