ESIS SFD Flashcards

1
Q

Where is the ESIS SFD ADC located?

A

Nose compartment (ADC 4000)

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2
Q

What causes the VMO bar to be displayed on the SFD?

A

Anytime 170 KCAS is displayed on the airspeed tape
(Max Operational Speed)
tied to Vne of aircraft

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3
Q

Under what circumstances is there a need to initiate a FAST ERECT action from the menu list on the SFD?

A

Extended maneuver error;
DG indication continues-loss of magnetometer heading source

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4
Q

What is the maximum that pitch trim can be adjusted on the SFDs?

A

7 degrees

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5
Q

What are the components that make up the ESIS system for the SFDs

A

x2 Detachable Config Modules, x2 SFD, the ADC-4000, and a Magnetometer

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6
Q

What are the four selectable menu items on the SFD?

A

-fast erect
- set pitch trim
- set brightness
-Baro Type

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7
Q

A loss of heading information on the SFD indicates a possible failure of the?

A

Magnetometer

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8
Q

Where does the ESIS system receive electrical power from?

A

No. 1 Essential DC BUS for SFD 1
No. 2 Essential DC Bus for SFD 2

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9
Q

Define ESIS

A

Electronic Standby Instrument System

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10
Q

What information does the magnetometer provide to the SFDs?

A

Computes magnetic heading with pitch and roll data

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11
Q

Where is the magnetometer located?

A

AFT Pylon

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12
Q

A failure indication on the sides of the SFD indicate a failure of what ESIS component?

A

ADC-4000

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13
Q

What conditions must the aircraft be in to perform a Fast Erect on the SFD?

A

On the ground or straight and level non accelerated flight

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14
Q

What type of information does the ADC-4000 provide to the SFDs?

A

-Airspeed
- vertical speed
- altitude

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15
Q

DCM

A

Detachable Configuration Module (DCM-3000)

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16
Q

How long is SFD blank when going through power-on self test

A

15 seconds

17
Q

What 2 errors can you have

A

Error Code
Error Message

18
Q

What constitutes an extended maneuver

A

maneuver exceeding 6 minutes at a roll angle > 7° from level

19
Q

What indicates a failure on the SFC

A

Red X’s

20
Q

What indicates Attitude Failurex

A

“ATT FAIL”

21
Q

How is power reset to the SFD

A

pulling circuit breaker

22
Q

When is the DG (Directional Gyro) displayed within the SFD’s display area

A

With a temporary loss of magnetometer heading source

23
Q

What type of failure stops the start-up process

A

System Failures

24
Q

What does the ADC provide to the SFD’s

A

Airspeed, Vertical Speed, Altitude Data

25
Q

What is the corrective action if “WARNING Power Reset Needed” appears on the SFD display

A

Bring aircraft to straight and level non-accelerating flight and then reset/recycle power to GH-3001

26
Q

When does the menu listing automatically terminate with no mode activity on the SFD’s

A

15-20 seconds