DMS Check On Learnings Flashcards

1
Q

Are armament loading selections available on the LMP?

A

YES

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2
Q

What Indications are available to the crew that the load maintenance panel (LMP) Squat Override is in the AIR MODE?

A

There are no indications

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3
Q

What component provides the voice messages for the WCA subsystem?

A

Communications Interface Unit

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4
Q

Which component controls the operation of the DMS?

A

Mission Processor (MP)

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5
Q

How is data on the maintenance data recorder downloaded?

A

Maintenance Support Device (MSD)

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6
Q

The DMS page can only be accessed from which page?

A

Menu Page (M)

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7
Q

Faults are detected through which three types of Built in Tests (BITS)?

A

PBIT, CBIT, and IBIT

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8
Q

What page can you safely shutdown the TADS and PNVS systems?

A

INIT, SHUTDOWN, and MASTER OFF

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9
Q

When versions mismatch occurs, how can you tell what the mismatch is?

A

The software version is displayed in white

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10
Q

When will components run PBIT?

A

When power is applied

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11
Q

Which crewmember(s) can disable the DMS auto page function?

A

CPG Only

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12
Q

On what MPD page does the crew enter the helicopter tail number?

A

DMS Utility

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13
Q

In order for the crew to upload all subsystem initialization files and AMPS data at one time, what selection should be chosen from the DTU Page?

A

MASTER LOAD

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14
Q

When you push the MASTER LOAD button on the DTU page, what mission is loaded?

A

MSN 1

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15
Q

What page will display the status and type of ERMM’s installed in the ESSRD?

A

DTU

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16
Q

The DMS fault page will default to which data type?

A

Active

17
Q

Aircraft logbook write ups should be made from information obtained from which page?

A

DMS/FAULT Page

18
Q

When is a BUCS IBIT required?

A

Prior to each flight and before starting engines

19
Q

What is the purpose of performing an IBIT on a system?

A

Allows crew members to test specific subsystems for status and fault isolation

20
Q

What is the purpose of the WCA subsystem?

A

Alert crew members Warnings, Cautions, and Advisories associated with aircraft systems and subsystems

21
Q

Digitized Voice messages are provided to alert crew members to… (BLANK)

A

Warnings

22
Q

What happens when a Caution condition is no longer detected?

A

All indications (visual/audio) will be canceled without crewmember intervention

23
Q

How are Advisories indicated?

A

Advisory tone, EUFD message in the advisory column, and the DMS Page

24
Q

What is the indication on the MPD to alert the crew that they are operating in single MP Mode?

A

White bold lines are displayed on the MPD’s

25
Q

Who can reset a MP in the event of a failure?

A

Pilot, on the Processor Select Panel

26
Q

In the event of a dual MP failure, what is the indication on the MPD’s?

Land…

A

Red X’s will be superimposed across all MPD’s
“LAND AS SOON AS POSSIBLE”

27
Q

Can a Manual AIU reset be performed in the air?

A

Yes (recommended to be performed on the ground, CH.9)

28
Q

If an AIU fails can you run a IBIT on that AIU in air?

A

NO

29
Q

How many digitized voice warnings?

A

15

30
Q

What three functions does the Data Management System (DMS) have?

A

(1) Data Transfer (DT)
(2) Warning/ Caution/ Advisory (WCA)
(3) Fault Detection and Isolation (FDI)