Vision Indicating And Recording Flashcards

1
Q

How many displays

A

4 in total

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2
Q

Are pilots/copilots side panels identical

A

Yes, include 1 electrical management system control display unit, one stall protection panel EMS CDU, one clock, one air con gasper

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3
Q

Where is RAT release handle located

A

Center pedant Le, l/h side next to LG manual release handle

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4
Q

Where is gear select handle

A

Center instrument panel

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5
Q

Where are fuel/hydraulic/elt/air con/pressurisation/engine panels located

A

Center o/h panel

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6
Q

Where are fire handles locate

A

Center o/h panel

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7
Q

Difference with flight deck refuel panel behind captain

A

Has provision for aft tank

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8
Q

Where is oil replenishment panel

A

Behind captain

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9
Q

What time does clock supply

A

Local or GMT, transmits time related info to all other systems requiring time related issues when gps is not available via ARINC 429 to the data bus concentrator modular cabinet DMC

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10
Q

Where is clock powered from

A

Secondary power distribution assy #1 batt bus to captain, clock 2 powered by #1 dc bus

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11
Q

Where does FDR get its parameters from

A

DMC 1data concentrator modular cabinet 1 and has pilot event marker,solid state, ult,Pilot event PEM, trialling accelerometer, download connector, stored max 25hrs ARINC 717 BUS

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12
Q

Where id fdr located

A

Aft unpressurised b/h sloping b/h and PEM pilots event marker on pedestal below du 4

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13
Q

Does fdr system have Force transducers

A

Yes, rudder and control wheel and is an optional FDR system called CFMS crew force monitoring

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14
Q

What CAS messages for FDR

A

FDR ACC FAIL // FDR FAIL

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15
Q

Where is data concentrator cabinet

A

Behind f/o in flight deck

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16
Q

What does EICAS DO

A

Engine instrument display, various aircraft and avionics systems, on a continuous basis for crew alerting, master warning and caution, flight data acquisition, aural warning, lamp driver, checklist function

17
Q

What software does the EICAS use

A

Resides in virtual machine no 2, VM2, on the DCM6000 within each channel in each DMU. EICAS has no hardware interfaces and make use of the system services and common input/output concentrators IOC,s
FDR info comes from DCU 1

18
Q

Where are the DCM,s kept data concentrator modular cabinet

A

2 cabinets in system, both kept in underfloor avionic compartment on the 6000, fwd avionic rack on 5000

19
Q

Does the DCM have a power producing module

A

Yes, single channel unit within the DMC 6000, 4 function , power conditioning, temp control,discrete to transistor logic, TTL conversion, includes fan and fault if fan below 75o/o speed

20
Q

What is aircraft personality module APM

A

Loc Stn 240r, on 6000 and Stn 240+32r on global 5000, non volatile external , remain on aircraft even r paren storage devices have been replaced

21
Q

On DCM what is strapping

A

Uses a number of signals to determine its position within the aircraft can be set externally by discreet or internally to DCM

22
Q

What is crew alerting system

A

CAS

23
Q

What is TAWS

A

Terrain aural warning system

24
Q

Where are checklist function stored

A

DCU

25
Q

What is CPS

A

Central processing system, cos its of set of cabinets for the hosting of avionics modules, modules are developed for the CPS and provide combinations of aircraft signal inputs and outputs that vary in number and type.

26
Q

What is ARINC 818

A

Avionics digital video bus, used in part by the enhanced video systems EVS, include, ;infra red sensors, Radar,Synthetic vision, Head up displays, primary and multifunction displays

27
Q

What is ARIC 708 data bus

A

Specific to weather radar systems, 1 megabit data rate