AWR 13.2 Flashcards

1
Q

Operation of the NVGs in both crew stations _________.

A

is authorized.

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2
Q

When using the ITT NVGs and the low-battery voltage light is constantly lit:
Blinking:

A
  • NVGs exposed to certain electromagnetic emitters

- low battery voltage

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3
Q

Prior to flight with the Air Warrior Over-Water Cold Weather ensemble, a ______ shall be performed. If it fails, the kit is not authorized.

A

control-sweep

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4
Q

NOTE: MODE 4 CAUTION indications may be generated every 2-3 minutes when __________. Care should be taken to ____.

A

the MODE 4 selection on XPNDR is OFF

avoid complacency when canceling audio tone

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5
Q

Deselecting XPNDR on the EMER PANEL will _______ code. (contrary to user’s manual)

A

reset MODE 3/A from 7700 to it’s previous

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6
Q

The MAYDAY message (BFT) generated from selecting XPNDR on the EMER panel contains _________, although it may be inaccurate (____).

A

aircraft fault data (W/C/A)

stale information

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7
Q

A private net (PN) failure advisory may be displayed on the EUFD when performing PN ___________.

A

digital messaging and voice traffic on the same radio

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8
Q

QTM targeting solutions are dependent on the aircraft _________. Differences in ____ when transmitting may cause inaccurate firing solutions.

A

altimeter setting

altimeter settings

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9
Q

A laser WARNING message may be intermittently displayed (in error) during ________.

A

internal boresight

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10
Q

Sight selecting FCR after receiving a RFHO does not correctly display the _____. Sight selecting HMD or TADS will give the correct _____.

A
radar range (R?.?)
Nav Range (Nx.x) to the target
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11
Q

WARNING: The TADS/PNVS has exhibited susceptibility to certain _______ (___) which may cause _________. If encountered, proceed IAW ______.

A
electromagnetic fields (HIRTA) which may cause the turret to slew to the hard stops
EP in Ch.9, "TADS/PNVS FAILURE"
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12
Q

NOTE: The ADF does not support direction finding in areas of _______ and may provide inaccurate bearing. Recommend cross checking with other sources.

A

NDB congestion

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13
Q

WARNING: The BFT has not been qualified as the sole source for _____ or for ___.

A

targeting information

Identification Friend or Foe (IFF)

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14
Q

WARNING: The BFT SA picture may have latencies of up to ______ and possible inaccuracies. ______ shall not be performed over the BFT.

A

two minutes

Time sensitive functions

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15
Q

The C2 and SA data provided over the BFT system shall not be used as ________.

A

the primary source of navigation or to determine location of other platforms

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16
Q

The BFT transceiver may occasionally lose satellite lock without automatically regaining it. If it does not regain lock for several minutes, _______.

A

power cycle the BFT transceiver

17
Q

A “FMC PREFLIGHT TEST SERVER CMD FAIL” fault may be displayed during power-up after running aircraft on external power. How do you clear the fault?

A

Perform a BUCS IBIT

18
Q

WARNING: A generator power interrupt will result in ________ for approx. _____.

A

single DP operation

21 seconds

19
Q

If a power interrupt occurs during NVS flight, ____________. What do you do?

A

CPG HDU video will change to PLT FORMAT.

The PLT shall immediately assume control of the aircraft.

20
Q

The STAB icon on the flight page (during manual mode) and nominal airspeed will be _______ when current airspeed is below ____.

A

incorrectly displayed as RED

the low airspeed setting on the FLT SET pg

21
Q

NOTE: ENG 1 and 2 TQ color representations on the ______ do not change from GREEN regardless of the value. The values however are correct.

A

PERF HIT PAGE

22
Q

IPAC software version 2.3.0: SE Max TQ available can be optimistic by as much as ___ because ____.

A

3%

IPAC only accounts for 1/2 of total bleed air losses associated with IPAS and ECS heating.

23
Q

Use of the PERF PAGE is ________.

A

not authorized for performance planning (v13.2 only… v13.3 IS AUTHORIZED)

24
Q

WARNING: In the event of a GUN EL MISTRACK fault, _________ and may not provide proper ______.

A

the gun is frozen in azimuth and stored in elevation

wire strike protection due to wire cutter angle

25
Q

Dual HADS probe failure may occur when the aircraft is subjected to wind or wind gusts of _______.

A

45 knots or greater

26
Q

If HADS data is invalid, the airspeed data will come exclusively from the ____ and, depending on airspeed, will be ______.

A

FMC

inertial ground speed (

27
Q

How can Dual HADS Failure be detected?

How can the HADS be brought back online?

A

Compare STBY instruments with indications, confirm by checking FAULT PAGE.
Only after the aircraft is shutdown.

28
Q

WARNING: A dual HADS probe failure may cause degraded _____. IOT prevent _____, the crew should check ______ after being subjected to >45 knot winds.

A

ballistic solutions

fratricide / FAULT PAGE

29
Q

The standalone VNSight mode is _______. The only authorized mode is ______ or ____.

A

not authorized for flight

FUSED or FLIR

30
Q

Due to the VNSight upgrade, _________ followed by _______ 30 seconds later is typical, even if the fault page depicts ____.

A

BORESIGHT FAIL

BORESIGHT COMPLETE / BORESIGHT FAIL

31
Q

Flares can cause ground fires when launched from altitudes of ______ and below.

A

200’ AGL

32
Q

Flares launched from low altitude (___) may bounce off the ground, potentially striking the aircraft.

A

50-100’ AGL

33
Q

CMWS will not detect sequencer or dispenser failures. How do you get the indication?

A

Select BYPASS and then return to AUTO mode. Updated inventory will also provide updated status.

34
Q

Perform a system start-up or ASE/UTIL page re-inventory to detect _______.

A

dispenser / sequencer failures

35
Q

CMDS INV LOW is depicted when the selected flare category is below ___.

A

20%

36
Q

If flares are ignited (hangfire / ignited by SAF) and lodged in the dispenser, what is the EP?

A

1) CMDS JETT

2) Land as soon as POSSIBLE

37
Q

For TRC to be engaged, what conditions must be met? (6)

A

ATT / ALT HOLD, 5’, Force Trim released and SCAS engaged