POH section 7- Pitot static system

Question 1

where are the 2 pitot heads?

Answer 1

on top of the nose

Question 2

where are the 2 pairs of balanced static ports?

Answer 2

on both sides of the fuselage

Question 3

what does the left pitot static system supply?

Answer 3

pilots instruments

Question 4

what does the right pitot static system supply?

Answer 4

co-pilots instruments

Question 5

what will we not recieve if the pitot drain valves are eft open?

Answer 5

airspeed indication

Question 6

where are the pitot drain valves located?

Answer 6

underneath the nose

Question 7

what does putting the alternate static pressure selector valve to ALTERNATE SOURCE do?

Answer 7

uses static pressure from the cabin- selected in the event of the normal stick system becoming clogged

Question 8

which instruments functions will be maintained when switching to alternate static?

Answer 8

• altimeter
• ASI
• VSI

Question 9

what should we do to the autopilot prior to switching on the alternate static?

Answer 9

switch it off

Question 10

what protects the pitot heat?

Answer 10

PITOT LH/BUS 1 on overhead breaker panel

PITOT RH/BUS 2 on AC/DC breaker panel