AW 139 Instruments

Question 1

The pilot´s Attitude Stand-by

Answer 1

b. Provides an output to the MAU’s

Question 2

When the PUSH SYNC button is pressed

Answer 2

c. The Heading Bug aligns with current aircraft heading

Question 3

The Emergency Locator Transmitter automatically activates during a crash or an emergency landing

Answer 3

c. And transmit on the 121,500 Mhz (civil), the 243,000 Mhz (military) and the 406,025 Mhz (SAR SAT)

Question 4

The test of Emergency Locator Transmitter

Answer 4

a. Must be done according to the international authority rules

Question 5

When the HDG mode is engaged

Answer 5

b. Any lateral beep operation modifies the input on that mode

Question 6

With any mode engaged, the PFD different selection on the Guidance Controller causes

Answer 6

c. The disengagement of the mode(s)

Question 7

The Flight Director modes can be engaged

Answer 7

c. When the air-speed is equal or greater the 60 Kts

Question 8

The VOR 1 bearing pointer is displayed on the HSI

Answer 8

c. Under pilots selection through the Display Controller with the system valid

Question 9

The ADF 2 bearing pointer is displayed on the HSI

Answer 9

c. Under pilots selection through the display Controller

Question 10

On the HSI the pilots can display the on-side/cross side VOR/LOC

Answer 10

a. Under pilots selection through the Display Controller

Question 11

The DH can be set through the DH knob on the pilot´s Remote Instrument Controller and

Answer 11

c. The new value is displayed on the pilot´s PFD only

Question 12

The MAU #2 transmit serial data on the ASBC-D identified as:

Answer 12

c. Right primary and right backup

Question 13

The MAU #2 receives serial data on the ASCB-D identified as:

Answer 13

a. Left primary, right primary and right backup

Question 14

Which MAU is considered “Master” between the two

Answer 14

c. Always the MAU #2

Question 15

The Decision Height (DH) is entered via the:

Answer 15

Remote instrument controller (RIC)

Question 16

What does the PUSH TEST button on the DH knob test?

Answer 16

The radio altimeters

Question 17

When is the automatic direction finder (ADF) bearing pointer displayed on the horizontal situation indicator (HSI)?

Answer 17

When signal is valid and the pointer is selected on the display controller.

Question 18

How is an active caution displayed?

Answer 18

Displayed in reverse video and then displayed in amber text after MCL acknowledgement.

Question 19

The Air Data Module (ADM) #1 provides data to the Modular Avionics Unit (MAU) #1 only, and in case of malfunction, form where is the copilot’s data on the primary flight display (PFD) provided?

Answer 19

The ADM #2 after pilot intervention.

Question 20

Which statement is true with reference to the ATT mode?

Answer 20

It is the default mode when the autopilot is engaged.