CHAPTER 2 - Airworthiness of Aircraft

Question 1

1. The State of Design is to ensure that a continuing structural integrity programme, including information concerning corrosion control, is maintained in respect of aeroplanes:

a. with maximum certificated take-off mass less than 5700 kg
b. with maximum certificated take-off mass greater than 5700 kg
c. with maximum certificated take-off mass equal to 5700 kg
d. with maximum certificated take-off mass not more than 5700 kg

Answer 1

b. with maximum certificated take-off mass greater than 5700 kg

Question 2

2. The continuing validity of a Certificate of Airworthiness of an aircraft is subject to the laws of:

a. the State of Registration
b. the State of Registration or the State of the Operator
c. the State of the Operator
d. the State of Registration and the State of Design

Answer 2

a. the State of Registration

Question 3

3. When a Contracting State first enters on its register an aircraft and issues or validates a Certificate of Airworthiness, it shall inform:

a. The State of Registry
b. The State of Manufacture
c. The State of Design
d. The State of the Operator

Answer 3

c. The State of Design

Question 4

4. Which document contains information concerning the flight limitations of the aircraft ?

a. The C of A
b. The C of R
c. The C of L
d. The aircraft Flight Manual

Answer 4

d. The aircraft Flight Manual