NAV Flashcards

1
Q

How many routes (RTEs) can be stored in the Apache?

A

10

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2
Q

What are the (5) major components of the NAV system?

A
Embedded GPS Inertial (EGI) x2
Doppler Radar Velocity Sensor (DRVS)
Air Data System (ADS)
Radar Altimeter (RAD ALT)
Automatic Direction Finder (ADF)
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3
Q

Where is the GPS antenna which provides signals to the EGIs located?

A

On top of the vertical fin

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4
Q

Where are the two EGI units installed?

A

Behind PNVS, in front of CPG

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5
Q

What does the GPS provide the EGI?

A

Position

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6
Q

What does the Doppler Radar Velocity Sensor (DRVS) provide the EGIs?

A

Velocity only

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7
Q

What does the Helicopter Air Data System (HADS) provide the EGIs?

A

latitudinal and longitudinal true airspeed and pressure altitude

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8
Q

What does the System Processor (SP) provide the EGIs?

A

manual updates

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9
Q

What does the Inertial Navigation Unit (INU) provide the EGIs?

A

horizontal and vertical linear accelerations and angular rates

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10
Q

What does the Kalman Filter (computer algorithm) within the EGI do?

A

combines all NAV and raw sensor data IOT provide an optimal estimate of Attitude, Position, HDG, Velocity, Acceleration, and Angular Rate

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11
Q

Where is the DRVS mounted and what does it provide?

A

In the bottom fairing

Velocity only

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12
Q

On power-up, the DRVS is defaulted to the ON position. To reduce radar detectability, can the crew turn off the DRVS?

A

YES

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13
Q

When will the Kalman Filter reject DRVS returns?

A

Flight over a smooth/glass type surface
ALT > 10,000 feet
Excessive bank angle

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14
Q

The High Integrated Air Data Computer (HIADC) accepts pneumatic inputs and process all of the Airspeed and Direction Sensors (AADS) IOT provide the FMC with:

A
Indicated Airspeed (LAT / LONG)
True Airspeed (TAS)
Altitude Rate, Static Pressure, Static Air Temperature
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15
Q

RAD ALT is located ______ and provides AGL information to the _______.

A

in the bottom fairing

SPs, DPs, WP, and the FMC

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16
Q

When is the audio ALTITUDE LO presented:
< 10’ AGL
11’-999’ AGL
1000’-1428’ AGL

A

ALT = LO BUG
ALT is 10% below LO BUG
ALT is 100’ below LO BUG

17
Q

LO and HI bug entry can be made within the ranges of ________.

A

0’ - 1420’ with a resolution of 1 foot

18
Q

How man satellites can each EGI track?

A

5

19
Q

From which page is the manual primary EGI selection made?

A

TSD UTIL

20
Q

What is the function of the DRVS in the NAV system?

A

Provide velocity

Doppler Radar Velocity Sensor

21
Q

Which page should you select IOT set the HI and LO altitude?

A

FLT SET

22
Q

Which MPD page controls NAV subsystem moding?

A

TSD page

23
Q

What is the maximum number of lines that can be placed on the LINE page?

A
15 lines (boundaries, phase line coordinates, etc.)
..must be built in AMPS..
24
Q

What is the maximum number of areas that can be placed on the AREA page?

A

12 Engagement Areas

..must be built in AMPS..