SELF-CHECK 1 / Aircraft Overview (Ch. 8)

Question 1

What is the overall height of the tail of G200?

Answer 1

21 feet 5 inches

Question 2

What are the weight and volume capacities of the baggage compartment?

Answer 2

1,980 lbs, 125 cubic feet, approximately 126 lbs/sq. in

Question 3

What is the wing span of the G200?

Answer 3

58 feet, 1 inch

Question 4

At 45,000 feet flight altitude, what will the cabin altitude be?

Answer 4

Approx. 8,000 feet

Question 5

What is the sea-level static thrust rating of the PW306A engine?

Answer 5

6,040 lbs

Question 6

What is the minimum runway width on which the aircraft can turn around?

Answer 6

Approx. 50 feet (48 feet 11 inches)

Question 7

What is the purpose of the tail strakes?

Answer 7

To add stability at lower speeds & dampen the dutch-roll tendencies.

Question 8

In degrees, what are the turning limits of rudder-pedal steering, hand-tiller steering, and tow-steering (torque link connected)?

Answer 8

In degrees, what are the turning limits of rudder-pedal steering, hand-
tiller steering, and tow-steering (torque link connected)?

3° L and R 60° L and R 100° L and R

Question 9

What are the max airspeed/Mach numbers?

Answer 9

What are the max airspeed/Mach numbers?

310 KTS SL to 10,000 feet: 330 KTS 10,000 feet to FL200: & 360 KIAS/.85 Mach above FL200

Question 10

What are the approximate dimensions of the baggage compartment and its door?

Answer 10

What are the approximate dimensions of the baggage compartment
and its door?

5 feet X 5 feet X 5 feet & the door is approximately 3 feet X 3 feet.