ASE Flashcards

1
Q

What does CUI stand for?

A

Controlled Unclassified Information

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2
Q

What is the purpose of the OT-228/U Common Infrared Counter Measure (CIRCM) for CH-47F Aircraft?

A

Employs infrared countermeasures to protect the aircraft from missile threats.

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3
Q

What are the conditions for employing OT-228/U CIRCM?

A

Given classroom instruction, hands-on demonstration, a CH-47F Aircraft with CIRCM installed, operational Missile Warning System (MWS), and applicable tools.

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4
Q

What does SOP stand for in the context of survivability?

A

Standard Operating Procedure

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5
Q

Identify the components involved in employing the OT-228/U CIRCM.

A
  • CIRCM
  • Line Replaceable Units (LRUs)
  • Platform Components
  • Modes of Operation
  • Maintenance Procedures
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6
Q

True or False: All system operational and maintenance procedures are for instructional purposes only.

A

True

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7
Q

What must be referred to before operating and/or performing any maintenance procedures?

A

Applicable system/platform technical manuals

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8
Q

What does Advanced Threat Infrared Countermeasure (ATIRCM) refer to on the Multifunction Display (MFD)?

A

It refers to CIRCM.

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9
Q

Fill in the blank: LASER stands for _______.

A

Light Amplification by Stimulated Emission of Radiation

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10
Q

What are the types of LASERs?

A
  • Continuous Wave (CW)
  • Single-pulse
  • Multiple-pulse
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11
Q

How is LASER radiation characterized compared to ordinary light?

A
  • More directional
  • Limited to a single or a limited number of wavelengths
  • Coherent
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12
Q

What is the definition of Class 1 LASER?

A

Considered to be incapable of producing damaging radiation levels during operation.

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13
Q

What distinguishes Class 2 LASERs?

A

Emits in the visible portion of the spectrum (0.4 to 0.7 µM) and eye protection is normally afforded by the aversion response.

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14
Q

Class 4 LASERs are hazardous to which parts of the body?

A

Eye or skin from the direct beam.

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15
Q

What is the nominal hazard zone (NHZ) distance for CIRCM LASERs?

A

82 feet (25 meters) from any single LASER.

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16
Q

What is the purpose of the CIRCM system?

A

Provides near spherical coverage of the host platform by interfacing with the Missile Warning System.

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17
Q

What are the major components of the CIRCM system?

A
  • 2 LASERs
  • 2 Pointer Trackers (P/T)
  • 1 System Processor Unit (SPU)
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18
Q

What does the System Processor Unit (SPU) do?

A
  • Generates computational, control, and communications resources
  • Provides power to P/T LRUs
  • Processes incoming signals from MWS
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19
Q

What is the operational temperature range for the CIRCM system?

A

-65°F (-54°C) to +160°F (71°C)

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20
Q

What is the non-operation (long-term storage) temperature range for the CIRCM system?

A

-80°F (-62°C) to +85°F (29°C)

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21
Q

What does the CIRCM system automatically do when it detects a missile threat?

A

Tracks and actively counters IR guided missile threats with directable LASER energy.

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22
Q

What is the function of the Pointer Tracker (P/T) in the CIRCM system?

A

Directs the mid-infrared LASER beam onto the threat and disrupts the missile’s guidance system.

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23
Q

What type of energy does the CIRCM system’s LASER utilize?

A

Mid-infrared (IR) signal.

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24
Q

What is the MIL-STD standard mentioned?

A

MIL-STD-1553B

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25
Q

What is the power input for the SPU?

A

+28V

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26
Q

Where is the SPU installed on the aircraft?

A

On the left side above the P/TL 1

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27
Q

What does the P/T LRU do?

A

Points and stabilizes the energy in response to azimuth and elevation messages

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28
Q

What are the components contained in the P/T?

A

Motors, motor drivers, camera, cryogenic cooler, electronics hardware, operational applications software, optical components, interfaces

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29
Q

What is the output of the P/T?

A

The IR beam exits through the P/T output dome

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30
Q

What is the weight of P/T 1?

A

24.7 lbs

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31
Q

Where is P/T 1 installed on the aircraft?

A

On the left side attached to Laser 1 under the SPU

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32
Q

What is the function of the LASER LRU?

A

Contains electronic components and optical elements to modulate mid-infrared LASER energy

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33
Q

What does the ASE Panel control?

A

CIRCM ON and OFF state

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34
Q

What does the Proximity Switch do?

A

Disarms CIRCM from firing the LASER when the aircraft lands

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35
Q

What must be checked before operating CIRCM?

A

Refer to platform/system specific technical manuals and checklist

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36
Q

What are the operational modes of the CIRCM?

A
  • OPERATE * BIT
37
Q

What is the nominal hazard zone (NHZ) for CIRCM LASERs?

A

82 feet (25 meters) from any single LASER, 118 feet (36 meters) where two LASERs are visible

38
Q

What does BIT mode determine?

A

Health of the CIRCM system

39
Q

What is the Power-up BIT (PBIT)?

A

Executes automatically at system power on to establish LRU operational status

40
Q

What is the purpose of Continuous BIT (CBIT)?

A

Performs periodic tests evaluating operational status in a non-interference basis

41
Q

How can an Initiated BIT (IBIT) be requested?

A

Manually by the aircrew to verify operational status of CIRCM

42
Q

What safety precautions are advised when operating LASERs?

A
  • Avoid eye or skin exposure * Use approved LASER protective eyewear * Wear long-sleeved clothing
43
Q

What is the default state of CIRCM when power is applied to the aircraft?

44
Q

What does the Safe/Arm switch do?

A

Enables or disables the CIRCM system LASER

45
Q

What happens if CIRCM is not powered on concurrently with the MWS?

A

CAAS will display a CIRCM system failure

46
Q

What is required for CIRCM LASER response to threat stimulus?

A
  • CIRCM system is powered ON * Weight-Off-Wheels is indicated * CIRCM Safe/Arm switch is in ARM position
47
Q

What should be established during the Confidence Test?

A

Constant communication between the cockpit and ground personnel

48
Q

What does the CIRCM utilize?

A

A Class IV LASER

49
Q

What should aircrews do before flight regarding flares in chaff module positions?

A

Visually inspect the dispensers for proper loading

Ensures correct identification in ASE equipped aircraft.

50
Q

What is the consequence of loading flares into chaff dispensers?

A

Flares will not be correctly detected and could damage rotor blades

Flares could be dispensed unintentionally.

51
Q

What happens if CIRCM is not powered-on within 30 seconds after CMWS is powered-on?

A

CIRCM will not complete startup built-in test (SBIT)

This leads to an ATIRCM system failure indication.

52
Q

What does the threat system status display provide to the pilot?

A

Visibility into the threat detection system operational state

Includes failed, degraded, or normal status indicators.

53
Q

What does the threat detector fault arcs indicate?

A

Visibility on the compass rose to areas where threat detection coverage is degraded

Due to failure of threat detectors.

54
Q

What type of notification does the crew receive if the entire CIRCM system fails in flight?

A

Aural notification for ‘Jamming Countermeasure Failed’

Indicates a complete system failure.

55
Q

What are the potential causes of CIRCM system failures?

A

SPU failure and conditions making both left and right Pointer/Tracker (PT) and/or Lasers inoperable

Example: Left laser fail and Right PT fail.

56
Q

What information is available on the Navigation Display page regarding CIRCM status?

A

Additional CIRCM status information

Similar to CMWS.

57
Q

What is the recommended action when using isopropyl alcohol?

A

Avoid contact with eyes, skin, and clothing; use with adequate ventilation

Direct eye contact can cause irritation.

58
Q

What should be done if damage is detected during optics cleaning?

A

The LRU exhibiting the condition shall be replaced

Includes scratches, digs, chips, fractures, or cracks.

59
Q

What is required for ESD precautions while handling Electrostatic Sensitive assemblies?

A

Perform ESD precautions

Necessary for maintenance personnel.

60
Q

What is the first step in the Pre-Maintenance procedure for CIRCM?

A

Set SAFE/ARM switch to SAFE

Ensures safety before maintenance actions.

61
Q

What is the procedure for removing the Laser Pointer Tracker (LP/T)?

A

Disconnect electrical connectors, loosen captive screws, and carefully remove LP/T

Follow specific steps to avoid damage.

62
Q

What is the allowable action for a damaged P/T connector receptacle?

A

Replace P/T

No repairs allowed.

63
Q

What should be done if corrosion is found on the Pointer/Tracker?

A

Repair if light; replace if severe

Follow TM 1-1500-344-23 for cleaning and corrosion control.

64
Q

What should be inspected before installing the LP/T?

A

Chemical coated surfaces

Ensures proper maintenance procedures.

65
Q

What is the final step in the LP/T installation procedure?

A

Secure Access Panel with two bottom latches

Completes the installation process.

66
Q

What is the first step in securing LP/T1 to the Bracket Assembly?

A

Position LP/T1 onto Bracket Assembly.

67
Q

How is LP/T1 secured to the Bracket Assembly?

A

Using four captive screws.

68
Q

What must be performed after securing LP/T1?

A

Perform resistance check.

69
Q

What is the first action when removing LP/T2?

A

Open Access Panel by disconnecting two bottom latches.

70
Q

What should be used to clean the area around mounting surfaces?

A

Cheesecloth dampened with isopropyl alcohol.

71
Q

What is the warning associated with the LASER and P/T components?

A

They contain Chromium, Nickel, or Cadmium plating.

72
Q

What should you do if dust contacts your eyes during maintenance?

A

Flush them thoroughly with water.

73
Q

What is the allowable action for a damaged P/T connector receptacle?

A

Replace P/T.

74
Q

What must be done if there are cracks on the P/T dome?

A

Replace P/T.

75
Q

What is the action for light corrosion found on P/T?

A

Repair IAW TM 1-1500-344-23, Cleaning and Corrosion Control.

76
Q

Fill in the blank: The acronym ‘SPU’ stands for _______.

A

System Processor Unit.

77
Q

What must be done if a damaged optical input port is found?

A

Replace P/T.

78
Q

What is the action required for loose or missing hardware on LASER?

A

Replace LASER.

79
Q

What is the procedure to secure SPU to the Mounting Plate?

A

Using four captive screws.

80
Q

What is required to be worn when using a power grinding wheel?

A

Approved respirator and goggles or face shield.

81
Q

What does the acronym ‘TM’ stand for in maintenance procedures?

A

Technical Manual.

82
Q

What is the allowable action if severe corrosion is found on SPU?

A

Replace SPU.

83
Q

What should be done if coughing or wheezing persists after dust inhalation?

A

Get immediate medical attention.

84
Q

What is the first step to install LP/T2?

A

Position LP/T2 onto Bracket Assembly.

85
Q

How should the Access Panel be secured after maintenance?

A

With two bottom latches.

86
Q

What is the action for a damaged mounting bolt on LASER?

A

Replace LASER.

87
Q

What is the purpose of torqueing captive screws?

A

To ensure secure attachment IAW applicable TM.

88
Q

What must be done before sanding or grinding LASER components?

A

Refer to TM 1-1500-344-23.

89
Q

What does ‘IAW’ stand for?

A

In Accordance With.