Flight Instruments

Question 1

LIMITATION:
Can you use VNAV during the intermediate segment of an approach that includes a teardrop course reversal?

Answer 1

No.

Question 2

LIMITATION:
When is Dead Reckoning Mode available:

Answer 2

Dead Reckoning mode is only available
1. Enroute (ENR)
2. Oceanic (OCN) phase of flight

Question 3

What Flight Instruments are on the Emergency BUS:

Answer 3

“PAT-AI”
P: PFD 1
A: AHRS 1
T: Transponder 1
A: AFCS
I: IESI
(Think: During emergency situations with Tim.. PAT was full of Artificial Intel.)

Question 4

What does IESI stand for?

Answer 4

Integrated Electronic Standby Instrument

Question 5

What is the HEADING source of the IESI?

Answer 5

AHRS 1

Question 6

How long does IESI take to align?

Answer 6

90 seconds after power up, the airplane must not be moved.
(It can be identified by an Aligning flag)

Question 7

The IESI primary electrical bus is?
What’s its back up electrical bus?

Answer 7

The IESI is primarily powered by the Emergency Bus and it will continue to operate powered by the batteries BUT in case the Emergency Bus fails, it will automatically switch to DC BUS 1.

(Don’t get confused with FADEC: powered by 28 volt DC system or the PMA, whichever is higher.)

Question 8

What does IASP stand for and what does it supply information to?

Answer 8

Integrated Air/Stall probe.

Question 9

What are the Primary source of air data information for the 3 ADS systems (ADS 1, ADS 2 and Standby)

Answer 9

IASP 1 = ADS1
IASP 2 = ADS2
Pitot Static = ADS Stanby

Question 10

Normal operations where are the PFD 1, MFD, PFD 2 and IESI getting its information.

Answer 10

PFD 1 & MFD are from ADS 1/ (AHRS 1).
PFD 2 is from ADS 2 / (AHRS 2)

Question 11

Your ADS system provides primary air data information to:

Answer 11

PFDs, MFD and IESI.

Question 12

Name the Probe locations.

Answer 12

Question 13

REVERSION:
If ADS 1 fails, what happens to PFD1? What happens if ADS 2 fails?

Answer 13

Question 14

1. What is the primary source of air data information for the the Air Data system 1 and 2?
2. What is the primary source of ATTITUDE, and HEADING information in the Phenom?
3. What is the source of HEADING information for the IESI?

Answer 14

1. IASP 1 &2
2. AHRS 1&2
3. AHRS 1

Question 15

What does the GREEN CIRCLE indication on your airspeed tape indicate?

Answer 15

1.3 Vs : 130% of stall speed.

Question 16

When will takeoff V speeds automatically go away on your airspeed tape?

Answer 16

Passing through 160 knots

Question 17

What is the GOLDEN CAS message

Answer 17

Root of all evil

Question 18

If PFD 2 fails, what happens to the other displays?

Answer 18

Question 19

Answer 19

Question 20

Answer 20

Question 21

Answer 21

Question 22

SWITCH:
Explain the PUSHER CUTOUT button

Answer 22

The SWPS provides one cutout button for both channels. The Button disconnects the channels when pushed in and disarms your Stick Pusher.

Question 23

REVERSION:
In case that a single ADS or AHRS fails, and automatic reversion does not occur… what can the pilot do?

Answer 23

Press the soft key, LOCATED ON THE MFD to manually revert the to the operating ADS/AHRS.

Question 24

OVERVIEW:

Answer 24

Note: Heading info for IESI is from AHRS 1.
Note: If ADS 1 fails, PFD 1 goes to ADS 2, than Standby ADS.
If ADS 2 fails, PFD 2, goes to ADS 1, than Standby ADS.

Question 25

LIMITATIONS: Review the Card

Answer 25