LANDING GEAR

Question 1

. The landing gear is

Answer 1

electrically actuated and hydraulically operated

Question 2

Where is the landing gear emergency handle located?

Answer 2

Under the cockpit floor between the pilot seats.

Question 3

What holds the landing gear in the up position?

Answer 3

An uplock box on each gear.

Question 4

Explain the Emergency Extension process

Answer 4

Pull out the free-fall handle that activates the free-fall selector valve and releases
all residual hydraulic pressure from the landing gear lines to the return line, and
mechanically releases the landing gear uplocks. Gravitational and aerodynamic
forces extend the landing gear (the gear free fall). The downlock mechanism then
locks the gear in its fully extended position.

Question 5

When the flap lever is set to either 0, 1, or 2 position, when would the landing
gear aural warning sound?

Answer 5

Difference between pressure altitude and LFE is less than 700’, or radio
altimeter indication less than 700’ AGL; and
*Airspeed is below 160kts; and
*Either thrust lever is set below 40 degrees for two operative engines; and
*Thrust lever of operative engine is set below 40 degrees for a one-engine
inoperative condition

Question 6

When would the landing gear aural warning sound at flap lever 3 position or
FULL?

Answer 6

Regardless of thrust lever position, airspeed and altitude, the landing gear aural
warning cannot be silenced by pushing the WRN INHIB button.

Question 7

When would the landing gear aural warning sound if flaps failed?

Answer 7

The landing gear aural warning will sound when the difference between pressure
altitude and LFE is less than 700’ while descending.

Question 8

What is the primary input to the Air/Ground System?

Answer 8

Weight-on-Wheels (WOW)

Question 9

Name some of the aircraft systems that utilize the WOW signals:

Answer 9

‣ Brake Control System
‣ Landing Gear Control Lever
‣ FADEC (Full Authority Digital Engine Control)
‣ Electrical System
‣ Lights (Baggage Compartment)
‣ Air Conditioning and Pressurization
‣ Fuel System (Fuel Indication)
‣ Flight Controls (Flaps and Spoilers);
‣ Avionics (Data Concentrator Unit and GEA (Garmin Engine/Airframe unit) 3).

Question 10

What is the maximum turning radius?

Answer 10

Rudder pedals give up to 20 degrees of steering authority with another 23 degrees
thru differential braking and thrust.

Question 11

What would a “LG WOW SYS FAIL” CAS message indicate?

Answer 11

There is disagreement between the signals from right and left WOW sensors
for more than 3 seconds.