81-06. Limitations
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1. On JAR-23 airplane, the limit load factor in normal category is:
2. VA is:
3. By what percentage does VA (EAS) alter when the aero plane’s weight decreases by 10%?
4. Which of the following are the gust values used in the V-n diagram?
5. An aircraft is flown at 20% below its normal weight. Because of this, VA will be:
