AWR 13.2 Flashcards

(37 cards)

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
Dual HADS probe failure may occur when the aircraft is subjected to wind or wind gusts of _______.
45 knots or greater
26
If HADS data is invalid, the airspeed data will come exclusively from the ____ and, depending on airspeed, will be ______.
FMC | inertial ground speed (
27
How can Dual HADS Failure be detected? | How can the HADS be brought back online?
Compare STBY instruments with indications, confirm by checking FAULT PAGE. Only after the aircraft is shutdown.
28
WARNING: A dual HADS probe failure may cause degraded _____. IOT prevent _____, the crew should check ______ after being subjected to >45 knot winds.
ballistic solutions | fratricide / FAULT PAGE
29
The standalone VNSight mode is _______. The only authorized mode is ______ or ____.
not authorized for flight | FUSED or FLIR
30
Due to the VNSight upgrade, _________ followed by _______ 30 seconds later is typical, even if the fault page depicts ____.
BORESIGHT FAIL | BORESIGHT COMPLETE / BORESIGHT FAIL
31
Flares can cause ground fires when launched from altitudes of ______ and below.
200' AGL
32
Flares launched from low altitude (___) may bounce off the ground, potentially striking the aircraft.
50-100' AGL
33
CMWS will not detect sequencer or dispenser failures. How do you get the indication?
Select BYPASS and then return to AUTO mode. Updated inventory will also provide updated status.
34
Perform a system start-up or ASE/UTIL page re-inventory to detect _______.
dispenser / sequencer failures
35
CMDS INV LOW is depicted when the selected flare category is below ___.
20%
36
If flares are ignited (hangfire / ignited by SAF) and lodged in the dispenser, what is the EP?
1) CMDS JETT | 2) Land as soon as POSSIBLE
37
For TRC to be engaged, what conditions must be met? (6)
ATT / ALT HOLD, 5', Force Trim released and SCAS engaged