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SYSTEMS > ASE > Flashcards

ASE Flashcards

1
Q

Where is the AN/APR-39 Radar Warning Receiver (RWR) digital processor located in the aircraft?

A

Left Aft Avionics Bay

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2
Q

Which component provides Radar, Laser and Missile threat audio to the crewmembers?

A

Communication Interface Unit (CIU)

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3
Q

Where are RWR, LWR and MWS detected threats displayed on the ASE and TSD pages of the Multi-Purpose Display (MPD)?

A

ASE threat symbols are always displayed on the inside of the ASE footprint.

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4
Q

When will an ASE footprint be displayed on the TSD page?

A

When ASE threats are selected for presentation from the TSD-THRT/SHOW page and at least one threat exists for display.

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5
Q

How may the AN/APR39A Radar Warning Receiver (RWR) be declassified?

A

Remove the User Data Module (UDM)

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6
Q

What is the purpose of the blade antenna within the RWR System?

A

Receives C/D band Radio Frequency (RF) energy and routes it to the digital processor.

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7
Q

What indication does the AN/APR-39 RWR provide if the received threat detection does not match a stored threat in the EID file?

A

A “U” will be displayed

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8
Q

How can the crew identify the system’s #1 priority ASE emitter when looking at the ASE or TSD pages?

A

The emitter will have a home plate symbol surrounding it.

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9
Q

Which component contains the classified operational software required for tactical operation of the Laser Detecting Set (LDS) / LWR?

A

The User Data Module (UDM)

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10
Q

What three threats are detected by the LDS /LWR?

A

Beam Rider, Designator, and Range Finder

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11
Q

How many degrees of detection are provided by the LDS / LWR in elevation?

A

± 45

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12
Q

How many degrees of detection are provided by the LDS / LWR in azimuth?

A

360

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13
Q

The AN/AVR-2B Laser Detector Set (LDS) / LWR is designed to operate in conjunction with which other ASE system?

A

APR-39 RSDS / RWR

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14
Q

The RFI gives the crew 360 degrees of coverage. What numeric values define the fine area?

A

90 degrees, with 45 degrees each side of the FCR centerline.

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15
Q

What is the primary difference between the fine and coarse areas of coverage?

A

Azimuth accuracy is much better in the fine area of coverage.

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16
Q

What three types of radar systems can the RFI detect?

A
  1. Pulse
  2. Pulse Doppler
  3. Continuous Wave
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17
Q

What is the primary function of the RFI system?

A

It functions primarily as an offensive system that provides NFOV target cueing for onboard and off board sights/sensors for employment of weapons.

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18
Q

What identifies an emitter that has been detected in the fine area of coverage of the RFI antenna array?

A

A triangle at the bottom center of the symbol

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19
Q

On what three FCR operational modes will RFI icons be displayed?

A
  1. GTM
  2. RMAP
  3. ATM
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20
Q

How can you differentiate between a priority emitter that is tracking/missile guidance another platform and an emitter that is signal lost, lock broken, or undetermined?

A

Homeplate intensity

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21
Q

How many RFI emitters can be displayed on the FCR, ASE and TSD pages?

A

10

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22
Q

What symbology indicates an MRFI interim solution?

A

A line with increasing/decreasing chevrons

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23
Q

What 2 configurations can MRFI be installed?

A

FCR (pinned) and URX

24
Q

How many ASE emitters (RWR/LDS/MWS) can be displayed on the FCR page?

A

None

25
Q

RFI detected threat/emitter symbols will not be selectable via the CAQ function on either the ASE or TSD pages when the _______ is the selected sight.

A

FCR

26
Q

What two pages are used to enable the RFI system if it is installed on the aircraft?

A

FCR UTIL or WEAPON UTIL (CPG or PLT)

27
Q

How can the crew select a non priority Radar Frequency Interferometer (RFI) threat to conduct a cued search on?

A

Reselect the cued search button and/or use the Cursor Select Function to choose an emitter.

28
Q

What four functions are performed when the CUED search button is selected?

A
  1. FCR centerline slews in azimuth to the RFI #1 emitter
  2. FCR is placed in the proper mode, unless already there
  3. Sets the appropriate Scan size as determined by how the threat was detected
  4. Scan will be automatically initiated.
29
Q

How is a manual cued search performed?

A
  1. An emitter is selected from the FCR page
  2. A single scan is initiated
30
Q

What indication does the crew receive if an emitter has been merged?

A

The RFI icon will appear within the FCR footprint as the NTS

31
Q

When performing an automatic CUED search utilizing the LHG, what will the FCR mode to if it is an airborne type emitter and the FCR is in the TPM mode?

A

ATM mode with a narrow field of view scan

32
Q

In order for the crew to perform a manual cued search when the FCR is the LOS, the RFI threat emitter must be selected from the ______ page utilizing the cursor select method

A

FCR

33
Q

What is the function of the CMWS system?

A

Used to detect and, in conjunction with the ICMD, counteract IR missile Threats

34
Q

What component serves as the primary processing center for LWR, RWR and CMWS systems?

A

Aircraft Gateway Processor (AGP)

35
Q

What component houses the User Data Module for CMWS?

A

ECU

36
Q

How can the AN/AAR-57 (V) CMWS be safed in addition to selecting the SAFE/ARM button on the ASE, WPN or INIT page?

A

By installing the safety pin in the safety switch

37
Q

Where are the HFI detects displayed on the ASE page?

A

Inner ring of the ASE footprint

38
Q

Sights and weapons can immediately be cued to the azimuth of the HFI threat. True or False?

A

True

39
Q

What are the two CMWS declared hostile fire threats?

A

Gunfire, RPG

40
Q

The ASE auto store only applies to which type ASE points?

A

MWS geolocated points and MRFI points

41
Q

Which page are ASE geo-located stored points displayed on?

A

TSD

42
Q

In order to auto transmit a geo-located ASE point the CMDS system must be ______.

A

Armed

43
Q

How many ASE geo-located points can be stored in the COORD file?

A

60, but can be indexed to 99

44
Q

What do bearing lines indicate?

A

Pairs a geolocated ASE threat with the detecting platform at the time of detection. Altitude of detecting platform is displayed in MSL (truncated)

45
Q

What capabilities are lost in an “ASE BACKUP” condition?

A

No ASE threat displays or audio. No inventory / fault status.

46
Q

What conditions will cause the jettison feature to be inhibited?

A

Engaging either of the two system safeties, CMDS safety pin or weight on wheel switch (SQUAT)

47
Q

What capabilities are lost in a “CMDS BYPASS” condition?

A

No automatic dispense.
Limited manual dispense.
No inventory / fault status.
No display/audio if MWS fails.

48
Q

During an automatic dispense of Flares, is the aircrew required to provide inputs to CMWS?

A

No

49
Q

What three CMDS status indications are displayed in the CM inhibit status windows (ASE, INIT, and WPN pages)?

A

ARM, SAFE, or PIN

50
Q

What three CMDS status indications are displayed in the HMD HAD?

A

Current manual program, SAFE, or PIN

51
Q

When arming the CMDS system utilizing the stores jettison panel, who can perform the jettison function?

A

PLT or CPG

52
Q

Where are the manual dispense controls located for the CMWS?

A

Cyclic stick

53
Q

CIRCM may lase missile regardless if CMWS declares the threat. True or False?

A

True

54
Q

How does the crewmember arm the laser for the CIRCM system?

A

Selecting R JAM button on ASE page

55
Q

What indication will you see when CIRCM is lasing a threat?

A

Lightning bolt in center of ownship

56
Q

How can M206 and M211 munitions be identified?

A

The M206 has a red end cap with the letter “F” on it.
The M211 has a gray sealant on the end.

57
Q
A

SYSTEMS (13 decks)

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