Data Management System (DMS)

Question 1

DMS primary functions (three)

Answer 1

Data Transfer (DF)
Warning, Caution, Advisory (WCA)
Fault Detection and Isolation (FDI)

Question 2

What monitors fault detection and health of aircraft

Answer 2

PBIT, CBIT, IBIT

Question 3

DMS Components

Answer 3

Processor select panel, mission processors, AIU, MSPU, SSRD

Question 4

Mission processor

Answer 4

Digital computer informs DMS of aircraft configuration

Question 5

Processor select panel

Answer 5

three position which controls and relays status of the MP’s

Question 6

Aircraft Interface Units

Answer 6

six analog to digital converters reducing the workload of the mp’s

Question 7

Solid State Recording Device

Answer 7

located on the top shelf in the right Aft Avionics Bay

Question 8

two major ESSRD functions

Answer 8

Video Recording and Data Transfer

Question 9

Maintenance Data Recorder

Answer 9

automatic operation located in CPG station stores in three sections

Question 10

Enhanced Removable Memory Modules

Answer 10

Three 100GB capacity ERMMS used for data transfer and video recording

Question 11

Maintenanace Support Device

Answer 11

Access to data stored on MDR via the 1553 Multiplex Interface panel

Question 12

Modernized Signal Processor Unit

Answer 12

permanently installed rotor smoothing and machinery health monitoring system

Question 13

Quick Access Recorder

Answer 13

used to record the maintenance data generated by the MSPU

Question 14

Communications Interface Unit

Answer 14

Digital signal processing for all audio: ICS, Radios, IDM

Question 15

What cues do the CIU provide Aural for

Answer 15

Voice warnings, audio from ADF and ESSRD, Caution/Advisory/IFF Tones, ASE related messages

Question 16

Multi Select FIll Panel

Answer 16

Uploading of communications data for

Question 17

what cues do warnings have

Answer 17

Aural (talks to you)

Question 18

DMS Control Recommended Standard

Answer 18

RS-422, -485 Serial Links

Question 19

DMS functions within the aircraft

Answer 19

Information Data Sharing, Maintenance data recording, Crew Notification of WCA, Subsystem monitoring and system activation, crash and/or accident, subsystem activation

Question 20

IBIT, CBIT, PBIT

Answer 20

Interfaced (Interactive), Continuous, and Power BIT

Question 21

Version mismatched in advisories section requires

Answer 21

Check versions page it will be displayed in white

Question 22

what station is capable of disabling DMS Autopage

Answer 22

CPG

Question 23

what indicates single mp mode

Answer 23

white lines top and/or bottom on both mp stations

Question 24

main purpose to check UTIL page daily

Answer 24

check aircraft tail number

Question 25

aircrew text messages are given as

Answer 25

degraded fault or fail

Question 26

dms page only accessed from which page

Answer 26

menu page

Question 27

faults are detected through which built in test

Answer 27

PBIT, CBIT, IBIT

Question 28

Type of DMS fault message is defined as the direct cause of anomaly is known and intended functionality of the system is partially removed

Answer 28

degraded

Question 29

following ERMM combinatins should be avoided

Answer 29

No mission ERMM,

Question 30

DMS Fault Page 5 Data Types

Answer 30

Active Data, Historical, Exceedance, AIU, and Mp Data

Question 31

What IBIT cannot be ran in the air

Answer 31

MP1, MP2, AIU

Question 32

when is a bucs ibit required

Answer 32

prior to each flight and before starting engines

Question 33

purpose of an IBIT on a system

Answer 33

allows crewmembers to test specific subsystems for status and fault isloation

Question 34

what form is used to record the weapons sighting data?

Answer 34

DA Form 2408-4-4

Question 35

what page contains unique selections for shutdown/farp controls

Answer 35

INIT

Question 36

Prior to shutting down APU, what page can safely shut down TADS and PNVS?

Answer 36

INNIT, Shutdown, Master OFF

Question 37

What does selecting REARM/REFUEL on INIT FARP Page

Answer 37

Disables all systems posing safety risks during rearm/refuel operations

Question 38

purpose of WCA subsystem is to

Answer 38

alerts crew to Warnings, cautions, and advisories associated with

Question 39

indication on MOD to alert crew in single MP mode

Answer 39

white bold lines are displayed on the MPDs

Question 40

Who can reset MP in event of failure

Answer 40

Pilot, on processor select panel

Question 41

indication of dual mp failure

Answer 41

red X's superimposed across all MPD's "Land ASAPossible"

Question 42

Can an AIU be performed in Air

Answer 42

Yes, but not recommended