Master Caution & Warning

Question 1

Take off Inhibit system activates at ( ) knots and normally deactivates at 400 feet AGL.

Answer 1

40 knots. PTM Pg. 4-7

Question 2

The Landing Inhibit system activates at () feet AGL with the gear down and deactivates at 40
knots upon landing roll-out.

Answer 2

400 feet. PTM Pg. 4-8

Question 3

A Take Off Configuration Warning will activate for the following conditions: a () not stowed, () extended, () not at 8 or 20 degrees, parking brake “ON,” take off trim not set in
all three axis’, a pitch trim mis-compare or Pitch Trim Bias not at zero.

Answer 3

Thrust Reverser, spoilers extended, flaps. PTM Pg. 4-10

Question 4

The Crew Warning Panel (CWP) is a redundant system providing the primary () warnings.

Answer 4

The primary red warnings.

PTM Pg. 4-1

Question 5

Holding the Rotary System Test button down for more than () seconds during the LTS test will activate the voice warnings.

Answer 5

15 seconds. PTM Pg. 4-4

Question 6

The Crew Warning Panel (CWP) provides ( ) and () warnings.

Answer 6

Voice & aural. PTM Pg. 4-1

Question 7

Switch indicators and WARN/CAUT lights are dimmed using the ( ) light switch. PTM Pg. 4-5

Answer 7

NAV light switch. PTM Pg. 4-5

Question 8

The Stall, Configuration Warning, Overspeed and Gear aural warnings cannot be ( ) .

Answer 8

Muted.

PTM Pg. 4-9