EGI Flashcards

1
Q

What two things make up HNAV

A

GPS+ INAV

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2
Q

Describe INS / What does it provide / What’s a weakness

A

Passive, worldwide, self contatined // Att, HDG, Postion, Velocity, Accleration / Only accurate for a short period of time.

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3
Q

Describe GPS / What does it provide/ What’s a weakness

A

Passive, worldwide // GPS is worldwide precise and regular position // Not self contained and is vilnerable to jamming and spoofing, no heading and attitude

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4
Q

What do P codes give me access to?

A

Military GPS

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5
Q

What is SAASM

A

Full selective availability/ anti-spoofing

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6
Q

GAS-1 stands for what?

A

GPS antenna System

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7
Q

Which EGIs are connected to GAS-1

A

Both

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8
Q

EGI 2 automatically connects to what if GAS-1 Fails / what about EGI 1

A

SATCOM/GPS

There is no backup

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9
Q

What are the four EGI Alignment Types

A

(1) GPS/INS
(2) Gyrocompass (GC)
(3) Stored Heading (SH)
(4) Directional Gyro (DG)

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10
Q

HNAV ( ATT/ HDG Valid / Where/ Align Time )

A

10 Seconds/ 7 minutes/shore&Shipboard / 15 minutes

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11
Q

Directional Gyro ( ATT/ HDG Valid / Where/ Align Time )

A

10 Secs/ -/Shore&Shipboard/ 2 minutes

It will take like 2 minutes to get off deck

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12
Q

Store Heading ( ATT/ HDG Valid / Where/ Align Time )

A

10 Seconds/ 30 seconds / Shore/ 3 minutes

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13
Q

Gyro Compass ( ATT/ HDG Valid / Where/ Align Time )

A

10 Secs/ 90 Seconds/ shore / 4 mins

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14
Q

Which EGIs are required for full AFCS Function

A

Both

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15
Q

EGI #2 provides what for AFCS

A

Pitch+Roll+ +ATT+ HDG + Vel

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16
Q

What does a DG aligment not provide, thus effecting which two functions?

A

Valid Velocity/ Hover coupler and autp Approach

17
Q

What is a normal Display for FOM

A

2 or less

18
Q

What is a normal display for EHE

A

Less than 25 ft

19
Q

What information do the ADCs supply after processing data?

A
  • Barometric altitude and local barometric pressure
  • Vertical speed
  • Indicated Airspeed (IAS)
  • OAT
20
Q

What does the Airspeed Transducer (AST) do?

A

Receives analog airspeed data from the pitot-static system and retransmits it digitally to the AFCC

21
Q

What configurations can the EGI support?

A
  • Two current legacy EGIs
  • A current legacy EGI and a SAASM EGI
  • Two SAASM EGIs
22
Q

What are the two navigation modes of the EGI?

A
  • Hybrid navigation (HNAV)
  • Inertial navigation (INAV)
23
Q

When is the Gyrocompass (GC) alignment type used?

A

When the helicopter is not in motion on the ground

24
Q

What does the Directional Gyro (DG) alignment provide?

A

Attitude and true heading outputs to support a quick launch capability

25
Q

What does the EGI require for coupled approach and hover function?

A

Valid heading and velocity data from EGI 2

26
Q

What is the purpose of manual entry of latitude and longitude in EGI?

A

Aids in alignment aboard ship or ashore and satellite acquisition

27
Q

What is required for GPS alignment to begin?

A

The GPS must acquire and track at least four satellites.

28
Q

What indicates that aircraft heading has become valid after alignment start?

A

A heading display on the HSI and ‘HDGV-G’ displayed in Display Area 1 of the MD.

29
Q

What is the maximum time for a complete GPS alignment?

A

15 minutes.

30
Q

What is a Gyro Compass (GC) alignment designed for?

A

To align an EGI when the aircraft is on the ground.

31
Q

What is required for Stored Heading (SH) alignment to occur?

A

A GC alignment must be completed prior to the last shutdown.

32
Q

What is the main purpose of a Directional Gyro (DG) alignment?

A

To provide a quick launch capability.

33
Q

What must be entered by the operator during DG alignment?

A

Magnetic heading.