Day 9 - Landing Gear and Brakes

Question 1

Normally the Landing Gear is __ actuated and __ operated

Answer 1

Electrically, hydraulically

Question 2

The landing gear extension cycle requires approximately __ seconds

Answer 2

7

Question 3

The landing gear retraction cycle requires approximately __ seconds

Answer 3

7

Question 4

For emergency gear extension, the EMER L/G Down handle must be pulled out approximately __ inches

Answer 4

10

Question 5

During emergency gear extension it takes approximately __ seconds for the gear to be down and locked

Answer 5

30

Question 6

During emergency gear extension, pulling the LDG GEAR circuit breaker does what

Answer 6

Removes electrical power from the gear system eliminating gear sequencing

Question 7

T/F - Once the gear has been extended using the emergency method, do not recycle the landing gear handle

Answer 7

TRUE

Question 8

The landing gear warning tone is initiated when

Answer 8

The landing gear are not down/locked and flaps are at the 0 or 10 degree position with one or both throttles retarded below 70% N2 OR the landing gear are not down/locked and flaps are extended beyond the 10 degree position

Question 9

An illuminated red UNLOCKED gear indicator means

Answer 9

Landing gear is in transit, one or more gear not locked, main gear fuselage doors not closed and locked

Question 10

Maximum rudder pedal deflection steers the nose wheel __ degrees either side of center

Answer 10

25

Question 11

Use of differential power or braking will result in castering the nose wheel up to __

Answer 11

45 degrees

Question 12

If both pilot and copilot are attempting to operate the brakes, which one will control the brakes

Answer 12

The person applying the most toe brake force

Question 13

Name the four modes of braking operation

Answer 13

Manual, power, anti-skid, and emergency

Question 14

T/F - The anti-skid system is fully functional during manual braking

Answer 14

FALSE

Question 15

The brake accumulator is pressurized at __ psi of nitrogen

Answer 15

900 +/- 50

Question 16

Anti-skid control is only activated above __ knots tire speed

Answer 16

14

Question 17

When is anti-skid braking available upon landing

Answer 17

Wheels spin at 37 knots or weight on wheels more than approximately 2.5 sec

Question 18

T/F - It is permissible to test the anti-skid in congested areas

Answer 18

FALSE

Question 19

If an ANTISKID FAIL annunciator is illuminated, the anti-skid should be placed to __ to assure full power braking

Answer 19

OFF

Question 20

The nitrogen emergency system provides sufficient pressure for at least __ to __ brake applications

Answer 20

7, 10

Question 21

If nitrogen pressure has been used to close the main gear doors enough pressure remains for __ to __ emergency brake applications

Answer 21

7, 9

Question 22

T/F - Normal braking should be used in conjunction with emergency braking to increase braking effectiveness

Answer 22

FALSE

Question 23

State the three conditions that the parking brakes should not be set

Answer 23

Hot brakes, low temperatures with visible moisture, or from the copilot’s side

Question 24

If landing with one main gear up or unsafe, you should touchdown where

Answer 24

On the same side of the runway as the extended gear