Fire Protection

Question 1

During the Fire Detect test, the crew should see the ( ) Leak, ( ) Leak and ( ) Leak lights illuminate on the Crew Warning Panel.

Answer 1

Left Bleed Air Leak, Right Bleed Air Leak and

Wing/Stab Leak lights. PTM Pg. 8-10

Question 2

During the Fire Detect test, the crew should see the red LR BLEED AIR LEAK and WING/STAB LEAK ( ) messages.

Answer 2

CAS messages. PTM Pg. 8-10

Question 3

Pushing the FIRE PUSH button shuts off:

Answer 3

Fuel, hydraulic fluid to the hydraulic pumps, hydraulic fluid to the thrust reversers and bleed air. PTM Pg. 8-4

Question 4

Pushing the FIRE PUSH button disconnects the:

Answer 4

Generator, alternator, disables the on-side windshield

heat system, and deactivates the engine ignition system. PTM Pg. 8-4

Question 5

The FIRE PUSH buttons will arm the fire extinguishing system even with electrical power turned off main ship batteries off, emergency battery off, generators off so long as one of the: ( ) is connected.

Answer 5

Batteries is connected. PTM Pg. 8-2

Question 6

If the ( ) disc on the aft right fuselage is ruptured, one or both Halon bottles have thermally discharged.

Answer 6

Red colored. PTM Pg. 8-6

Question 7

If the ( ) disc on the aft right fuselage is ruptured, one or both Halon bottles were discharged by the FIRE PUSH and fire extinguisher ARMED switches.

Answer 7

Yellow colored. PTM Pg. 8-6

Question 8

During preflight, the Halon bottles should read approximately ( ) psi at ( ) degrees F.

Answer 8

600 psi at 70 degrees F. PTM Pg. 8-6

Question 9

FIRE indications are available on the ( ) page of the RMUs.

Answer 9

Engine page. PTM Pg. 8-3