Pitot Static System 1-44

Question 1

The aircraft has how many independent pitot static systems, and what does it provide?

Answer 1

Two. Provide mach/airspeed, altitude, and vertical speed

indications.

Question 2

The primary pitot system probe near the ______ and two static ports on the upper _______ port and lower _______ port) provide the required pressures
to the air data computer.

Answer 2

right wing tip; rightside; left-side

Question 3

The engine data manager (EDM), standby altimeter, and
standby airspeed indicators in each cockpit receive static
pressures from the which pitot system?

Answer 3

The secondary

Question 4

How is the pitot probes are protected from icing

Answer 4

By electrical heating elements

Question 5

Pitot heat for both pitot probes is provided through the probes anti-ice switch, located where?

Answer 5

PROBES ANTI-ICE, on the engine/electrical switch panel in the front cockpit

Question 6

Which annunciator will illuminate whenever the probes anti-ice switch is used?

Answer 6

A green ANTI ICE annunciator

Question 7

No heating is provided for the static ports as the port, how are they protected?

Answer 7

the ports are protected from

icing by airframe location.