14 Cfr

Question 1

The positive limit maneuvering load factor (n) for normal category airplanes:

A. 4.4
B. 2
C. 6.4
D. 3.8

Answer 1

D . 3.8

Question 2

The design airspeeds selected for 14 CFR Part 23 airplanes are at which value

A. True Airspeeed
B. indicated airspeed
C. equivalent airspeed
D. Ground speed

Answer 2

C. equivalent as

Question 3

For all single-engine airplanes under acrobatic category with a VSO of more than 61 knots at maximum weight, the upward ultimate load factor need not exceed:

A. 6.0 g
B. 2.1 g
C. 3.8 g
D. 5.0g

Answer 3

D. 5.0 G

Question 4

For normal category airplanes with two engines, during takeoff with one engine inoperative, the steady gradient of climb at an altitude of 400 ft above surface with gears retracted must be?
A.Greater than 1.25%
B. Greater than 2 %
C. Greater than 3 %
D. Less than 2 %

Answer 4

B. G than 2%

Question 5

Under Part 23, what minimum structural requirement must aircraft meet?

A. Must withstand extreme weather
B. Must withstand loads during intended operations
C. Only needs to pass one load test
D. Must meet passenger comfort requirements

Answer 5

B. Must withstand loads during intended operations

Question 6

What is the primary purpose of Part 25?

A. Standards for small aircraft
B. Standards for rotorcraft
C. Standards for transport category airplanes
D. Standards for ultralight aircraf

Answer 6

C. Standards for transport category airplanes

Question 7

ATA Chapter for Wings
A. 53
B. 56
C. 57
D. 58

Answer 7

C. 57

Question 8

For FAR Part 23 airplanes, each engine mount and its supporting structure must be designed for a limit load factor in a lateral direction, for the side load on the engine mount, of not less than
A. 1.33
B. 1.31
C. 1.25
D. 2.25

Answer 8

A. 1.33

Question 9

Which of the following is NOT a major repair
A. Changing the wing’s original design to include winglets
B. Calibration of radio equipment.
C. Repairing a cracked wing spar
D. Replacing damaged rivets on the wing’s primary structure

Answer 9

A. Changing the wing’s original design to include winglets

Question 10

Which of the following is NOT considered a major alteration to the wing structure?
A. Adding a non-original fairing to the wingtip
B. Changing the primary wing material from aluminum to composite
C. Modifying the aileron attachment points
D. Replacing worn-out rivets with identical replacements

Answer 10

D. Replacing worn-out rivets with identical replacements

Question 11

Under FAR Part 23, which of the following is not considered as limited acrobatic operation?
A. Turns less than 60 deg
B. Cuban eights
C. Spins
D. No specific

Answer 11

A. 60 deg

Question 12

This means a type certificate including the amended and supplemental type certificate
A. interface component
B. design approval
C. production approval
D. state of design

Answer 12

B. design approval

Question 13

If a new safety belt is to be installed in an aircraft, the belt must conform to the strength requirements in what document?
A. AC 43.13B
B. STC 1282
C. TSO C22
D. 14 CFR PART 43

Answer 13

C. TSO C22

Question 14

A type of Certificate issued when an applicant has received FAA approval to modify an aeronautical product from its original design
A. TSO
B. STC
C. JAR
D. AC

Answer 14

B. STC ( supplemental type cert)

Question 15

For transport category airplanes, the negative maneuvering load factor at VC may not be less than:
A. -1
B. -2.5
C. -6
D. -0.5

Answer 15

A. -1

Question 16

For levels 1 and 2 low-speed airplanes, a climb gradient of ____ percent for landplanes and _____ percent for seaplanes and amphibians
A. 8.3 and 6.7
B. 3.8 and 6.0
C. 1.2 and 3.9
D. 6.9 and 4.2

Answer 16

A. 8.3 and 6.7