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ATA 22

Authored by Ahmad Zhafri

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Professional Development

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ATA 22
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8 questions

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1.

MULTIPLE CHOICE QUESTION

1 min • 20 pts

Stability Augmentation System (SAS) mode ONLY is engaged when…

ATT mode is disengaged, advisory P/R TRIM OFF and caution ATT OFF are displayed in CAS window

ATT mode is engaged,

advisory P/R TRIM OFF and C/Y TRIM OFF are displayed in CAS window

ATT mode is disengaged, caution 1-2 APP OFF and ATT OFF are displayed in CAS window

2.

MULTIPLE CHOICE QUESTION

1 min • 20 pts

The AW189 AFCS consists of:

Fight Control Computer (FCC), two pitch and two roll linear actuator, Stability Control Augmentation System (SCAS) actuator, three trim actuators and control panel

Fight Control Computer (FCC), one pitch ,one roll linear actuator, one yaw linear actuator, three trim actuators and control panel

Fight Control Computer (FCC), two pitch and two roll linear actuator, Stability Control Augmentation System (SCAS) actuator, four trim actuators and control panel

3.

MULTIPLE CHOICE QUESTION

1 min • 20 pts

The AFCS is to provide the following main functions: -

Primary Modes, Secondary Modes and Self-test Function

Primary Modes, Upper Modes and Self-test function

Upper Modes, Lower Modes and Self-Test function

4.

MULTIPLE CHOICE QUESTION

1 min • 20 pts

Where is the pitch and roll trim actuator located?

Below cockpit floor underneath the co-pilot’s seat

At the top of cockpit ceiling on pilot side

At the top of left side cabin ceiling

5.

MULTIPLE CHOICE QUESTION

1 min • 20 pts

Linear actuator received input in _______ with pilot command input

series

parallel

Series- parallel

6.

MULTIPLE CHOICE QUESTION

1 min • 20 pts

Autopilot (AP) can be turn off by means of

AP OFF on ECDU or thru switch on AFCS panel

AP OFF push button on collective or thru switch on AFCS panel

AP OFF push button on cyclic or thru switch on AFCS panel

7.

MULTIPLE CHOICE QUESTION

1 min • 20 pts

ALTA mode will disengage automatically during

Target altitude is acquired and below 200 feet

Speed below 90 knots and below 200 feet

Target altitude is required and speed below 90 knots

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