Transformer-coupled
Direct-coupled
Basic-coupled
Fiber-optic
1 Mbps
10 Mbps
15 Mbps
25 Mbps
Weather radar (WXR) overlay
Enhanced traffic alert collision avoidance system (ETCAS) overlay
MAP arc overlay
Ground proximity warning system (GPWS) terrain overlay
Radar altitude
Auto-throttle speed
Display mode commands
Flight director commands
Monitor
Combiner
Controller
Transmitter
OFF
DAY
AUTO
NIGHT
Flight display system
Navigation computer
Control display unit
Data transfer unit
Ram air pressure
Tactical air navigation
Aircraft performance data
Ethernet local area network (LAN) data
Transferred to the maintenance management system
Classified as a caution or warning
Detected on the ground
Not recorded
Flight management system control display units
CITS control and display (CCD) panel
CITS maintenance recorder (CMR)
CITS maintenance codes (CMC)
29.92″ Hg and the temperature is +15° C
29.92″ Hg and the temperature is +40° C
30.92″ Hg and the temperature is +15° C
30.92″ Hg and the temperature is +40° C
Less at low radar altitudes and greater at higher radar altitudes
Less at low attack angles and greater at higher attack angles
Greater at low airspeeds and less at higher airspeeds
Greater at low altitudes and less at higher altitudes
Time and distance
Power and ground
Altitude and airspeed
Commands and displays
Ambient pressure
Impact pressure
High altitude
Full pressure
Six
Three
One
Zero
True airspeed
Mach number
Indicated airspeed
Maximum safe Mach number
Altitude and instrument
Altitude and installation
Temperature and altitude
Temperature and installation
Two variable resistance-type sensing elements
Three variable resistance-type sensing elements
Two variable capacitance-type sensing elements
Three variable capacitance-type sensing elements
Flight recorder switch
Water immersion
Aircraft power
Gravity
Black
Green
White
Yellow
Depressing the master caution light
Reset by the associated system
Test switch activation
Audible warnings
Remote terminal
Bus controller
Stub coupler
Bus monitor
MIL–STD–3910B
MIL–STD–1553B
Optic transceiver
Star coupler
Bus monitor
Data transfer unit
Digital switching module
Integrated processing center
Multifunctional display (MFD) control panel
Electronic horizontal situation indicator (EHSI)
Electronic attitude director indicator (EADI)
Multifunctional display
Data transfer unit
Control display unit
Navigation computer
Flight display system
1553A Fuel Savings Advisory Bus (FSB)
1553B Fuel Savings Advisory System Bus (FSB)
1553A Flight Management Bus (FMB)
1553B Flight Management Bus (FMB)
Preflight initialization
Airspeed calculations
Total air temperature
Vertical navigation
Navigation subsystem only
Navigation, flight controls, electronic warfare, and weapons subsystems
Navigation, electronic warfare, weapons, and avionics subsystems
Avionics subsystem only
Pitot pressure
Mach number
Static pressure
Total air temperature
1 hour
8 hours
10 minutes
30 minutes
Inches of methyl chloride
Inches of mercury
Thousands of feet
Hundreds of feet
Pitot
Static
Barometric
Atmospheric
Density error
Instrument error
Installation error
Differential error
One-degree increments from –70° C to +80° C
One-degree increments from –50° C to +60° C
Two-degree increments from –70° C to +80° C
Two-degree increments from –50° C to +60° C
Red
Black
White
Yellow
Check for proper aircraft system operation
Check for proper light bulb operation
Extinguish the master caution light
Extinguish the audible warning
0 – 2,450 feet
50 – 2,450 feet
0 – 12,450 feet
50 – 12,450 feet
Mode 1, Excessive Sink Rate
Mode 3, Descent after Takeoff
Mode 4, Proximity to Terrain
Mode 5, Descent below Glideslope
Physically interconnecting the two shakers
Allowing only one shaker to operate at a time
Having the copilot’s shaker run slower than the pilot’s
Alternating between the two shakers on a one-second interval
20 bits long with a 3-bit sync character, 16 information bits, and 1 parity bit
16 bits long with a 3-bit sync character, 12 information bits, and 1 parity bit
10 bits long with a 2-bit sync character, 16 information bits, and 1 parity bit
8 bits long with a 2-bit sync character, 12 information bits, and 1 parity bit
Weather radar (WXR)
Auto-detect timing data (ADTD)
Ground proximity warning system (GPWS)
Tactical collision avoidance system (TCAS)
1553A data bus
1553B data bus
Ethernet local area network (LAN)
Aeronautical Radio, incorporated (ARINC) 429
Vertical navigation
Preflight initialization
Data bus management
Aircraft performance data
Atmospheric pressure to enter the static chamber
Atmospheric pressure to enter the pitot chamber
Impact pressure to enter the static chamber
Impact pressure to enter the pitot chamber
Red
Blue
Green
White
Red
Blue
Green
Yellow
“Glideslope.”
“Don’t Sink.”
“Too Low, Gear.”
“Too Low, Flaps.”
Quiz Review Timeline (Updated): Mar 20, 2022 +
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