Unit 1 Flashcards

1
Q

Translates air pressure into height above sea level and is not a good indicator of aircraft altitude when flying over land

A

Aneroid altimeter

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2
Q

This uses transmitted radio waves to measure aircraft height above the earths terrain

A

Radar altimeter

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3
Q

Formula used for radar altimeter

A

Distance = Time x Constant

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4
Q

What is the frequency range of CARA

A

4.3 GHz +/- 50 MHz

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5
Q

Ground speed of CARA

A

1800 knotts

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6
Q

Maneuver angle for fixed wing at 50,000 feet and 5000 feet

A

+/- 30° at 50,000 ft

+/- 60° at 5000 ft

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7
Q

Maneuver angle for rotary wing at 50,000 feet and 5000 feet

A

+/- 10° at 50,000 ft

+/- 30° at 5000 ft

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8
Q

Power requirement of CARA

A

28 VDC

26 VAC at interface adapter

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9
Q

What are the components of the Major component group #1

A

Receiver transmitter and height indicator

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10
Q

What are the additional components group #2

A

Antennas, interface adapter, cable adapter, mounting adapter, voice warning generator

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11
Q

What component of the CARA is responsible for generating the transmitted frequency and processing the reflective signal representing the terrain below

A

Receiver/transmitter RT

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12
Q

What provides analog and digital data for display on the CARA

A

Receiver/transmitter RT

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13
Q

What is used to compensate for height of antennas above ground and length of cables from the RT to the antennas and is installed in the RT

A

Aircraft installation delay AID

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14
Q

What component on the CARA displays both analog and digital info provided from the RT and supplies a warning signal when altitude falls below

A

CARA Height Indicator

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15
Q

What component of the CARA contains all the operating controls for the system/circuitry

A

CARA height indicator

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16
Q

What range is the analog and digital on the CARA height indicator

A

Analog : 0-5000 ft

Digital : 0-50,000 ft

17
Q

What gives altitude warning in the CARA height indicator

A

VALI setting indicator

18
Q

Radiates/receives

19
Q

What converts analog altitude data for used by other aircraft systems

A

Interface adapter

20
Q

What contains the circuitry that provides for isolation to the SRU level within the RT unit in the CARA

A

BIT processor

21
Q

Which self test is activated on power on and is undetectable
Occurs 2 to 3 times per second

A

Automatic self test AST

22
Q

What self test is a manual check of the RTN antennas and is a two-step process

A

Manual push to test PTT

23
Q

What is the two-step process in the manual push to test

A
Step 1 : Analog pointer = 500 ft
              Digital display = 88888
              R/T Lamp lit for 1.5 secs
Step 2 : Analog pointer = 300 ft
              Digital display = 300 ft
              R/T Lamp lit is out
24
Q

What self test is during back shop and is activated by doing PTT with a jumper in the maintenance test harness

A

Maintenance built in test MBIT

25
What will happen when there is a failure indication
“FAIL” on digital display, RT status light will be illuminated, analog pointer will indicate below zero
26
System Integration on CARA uses what?
Analog altitude, low altitude warning, radar altimeter valid signal
27
What system is a passive system and warns of impending danger to avoid ground impact it has audio and visual warning
Ground proximity warning systems GPWS
28
What outputs does GPWS use
Analog altitude and low altitude warning
29
What is an active system and digital system that integrates with autopilot to avoid impact? This initiates fly up commands and executed windshear functions
Ground collision avoidance system GCAS
30
What outputs does the GCAS utilize
Analog altitude, low altitude warning, radar altimeter valid signal
31
What integrates flight instruments, navigation systems, warning and caution information, and other aircraft systems
Control display system CDS
32
What is used for pilot relief during flight and derives altitude right information
Automatic flight control systems AFCS
33
What outputs does the CDS utilize
Analog altitude, low altitude warning, and radar altimeter valid signals
34
What outputs does the AFCS utilize
Analog altitude and radar altimeter valid signals