Avionics

Question 1

FC 530 - the static ports for flight instrument operation are located:

Answer 1

In the pitot static heads

Question 2

FC 530 - The pilot controls the static pressure source for the pilot
Flight instrument operation:

Answer 2

Electrically with the STATIC PORT switch

Question 3

FC 530 - The Air data unit receives pitot information from:

Answer 3

The right pitot static head

Question 4

FC 530 - The Air data unit receives static information from:

Answer 4

Both pitot-static heads with static source switch in BOTH

Question 5

During flight director only operation, depressing the pilot SYNC switch:

Answer 5

Disengages any pitch mode except G/S ARM AND ALT SEL ARM (FC 530)

Question 6

The ADIs and HSIs are energized when:

Answer 6

An inverter is turned on

Question 7

To control the aircraft in the pitch axis, the autopilot uses:

Answer 7

Pitch servo and secondary pitch trim motor

Question 8

If the stick nudger or puller engages during autopilot operation: (3)

Answer 8

• Selected pitch modes will be cancelled
• The autopilot maintains a synchronous standby mode in the pitch axis until the nudger or puller releases
• Selected roll modes remain engaged

Question 9

When using the flight director REV (or BC) mode during a localized Back course approach, the:

Answer 9

Published inbound (front) course must be set in the HSI course window

Question 10

When using the autopilot, the following limitation applies:

Answer 10

The pilot or copilot must be in his respective seat with the seat belt fastened