CESSNA 172试题集--20131104.pdfVIP

1 The Theory Course for Cessna 172R NAV III ITEM BANK 2 Chapter 1 Aircraft Structure and Systems 1、The wingspan of C172 is A.36’1’’ B.8’11’’ C.27’2’’ 2、The max height of C172 is A.36’1’’ B.8’11’’ C.27’2’’/3 3、The wing area of C172 is square feet. A. 174 B. 175 C. 176/4 4、The propeller diameter and type of C172 is A. 75inches, fixed pitch B. 75inches, constant speed C. 75inches, fixed pitch or constant speed 5、The length of C172 is A. 36’1’’ B. 8’11’’ C. 27’2’’ 6、The minimum turning radius of C172 is A. 36’1’’ B. 11’1/4’’ C. 27’-5 1/2’’ 7、C172 is an all metal, , single engine airplane. A. four-place B. five-place C. two-place 8、The type of fuselage of C172 is A. monocoque structure B. semimonocoque structure C. frame structure 9、The fuselage of C172 is consisted of A. Bulkhead, ribs, skin 3 B. Bulkhead, stringers, skin C. Bulkhead, ribs, stringers 10、The wing of C172 is A. high wing B. low wing C. middle wing 11、The wings of C172 are consisted of A. Spar, ribs, stringers, skin B. Spar, bulkhead, stringers, skin C. Spar, bulkhead, ribs, stringers, skin 12、The empennage of C172 consists of A. vertical stabilizer and rudder B. horizontal stabilizer and elevator C. vertical stabilizer, rudder, horizontal stabilizer and elevator 13、The ground adjustable trim tab on rudder can control by pilot. A. True B. False 14、The control surface are operated by hand through A. cables and mechanical linkage B. rods C. electric wires 15、C172’s main flight control surfaces consist of A. aileron, elevator, rudder B. aileron, flaps, trim tab C. aileron, flaps, rudder 16、With C172, depressing rudder pedals will cause the movement of A. Nose wheel only. B. Rudder only C. Nose wheel and rudd