1.
What is the purpose of VOR?
A. 
Determine bearing to a stations
B. 
Indicate distances along the approach
C. 
Determine left/right guidance
D. 
Determine up/down guidance
2.
The basic operating principle of VOR is phase comparing the
A. 
90 and 150 Hz modulated signals
B. 
30 Hz reference and 9,960 Hz FM signals
C. 
30 Hz variable and 9,960 Hz FM signals
D. 
30 Hz reference and 30 Hz variable signals
3.
If the magnetic bearing to a VOR station is 225 degrees, the phase difference between the 30 Hz reference and 30 Hz variable signal is
A. 
B. 
C. 
D. 
4.
VOR identification (audible) signals are transmitted
A. 
B. 
At specified time intervals
C. 
D. 
5.
The ILS localizer course width at a distance of 10 miles from the transmitter is normally
A. 
B. 
C. 
D. 
6.
What frequency is used to transmit ILS glide slope information?
A. 
B. 
C. 
D. 
7.
The ILS marker beacon carrier frequency is
A. 
B. 
C. 
D. 
8.
What MLS outputs are provided to the pilot's and copilot's HSIs for approach and takeoff?
A. 
Ground station indications
B. 
C. 
D. 
9.
What is not an MLS output?
A. 
B. 
C. 
Glide slope correction flag
D. 
10.
On how many channels are the MLS receivers capable of operating?
A. 
B. 
C. 
D. 
11.
What is the frequency range of the MLS receivers?
A. 
B. 
C. 
D. 
12.
Which antennas are shared by MLS numbers 1 and 2?
A. 
B. 
C. 
D. 
13.
Which MLS landing system component allows for selection of system status?
A. 
B. 
Integrated display computer unit
C. 
Flight director mode selector
D. 
14.
When an ILS frequency is selected, the ARN-127 VOR receiver parks the HSI bearing pointer at the
A. 
B. 
C. 
D. 
15.
Which radial will the aircraft be positioned on if the aircraft is located north of the VOR station?
A. 
B. 
C. 
D. 
16.
To get a FROM flag in view on the HSI when the magnetic bearing to the VOR station is 75 degrees, the selected course should be manually set to
A. 
B. 
C. 
D. 
17.
During ILS operation, a full-scale deflection of the HSI vertical needle indicates the aircraft is off course from the runway centerline by
A. 
B. 
C. 
D. 
18.
In ILS operation, a deflection of two dots on the attitude director indicator glide slope deviation scale indicates the aircraft is
A. 
2.5 degrees off glide path
B. 
6.0 degrees off glide path
C. 
0.6 degrees off glide path
D. 
0.25 degrees off glide path
19.
When the ILS marker beacon amber (orange) lamp illuminates, the pilot hears a
A. 
B. 
C. 
D. 
20.
The total number of VOR/ILS channels that can be selected by the AN/ARN-147 control box is
A. 
B. 
C. 
D. 
21.
If the VOR station signal is lost or the receiver malfunctions, the ARN-147 system parks the bearing pointer at the
A. 
B. 
C. 
D. 
22.
In VOR mode, what information is sent to the HSI by the ARN-147 VOR/localizer receiver?
A. 
TO/FROM, heading, and relative bearing
B. 
Left/right deviation, flag alarm, and TO/FROM
C. 
Relative bearing, flag alarm, and heading
D. 
Flag alarm, distance, and left/right deviation
23.
What glide slope information is provided to the attitude director indicator when the AN/ARN-127 is oeprating in the ILS mode?
A. 
B. 
C. 
D. 
24.
The main reference burst is transmitted when the main lobe of the TACAN surface beacon radiation pattern is due
A. 
B. 
C. 
D. 
25.
A TACAN beacon provides a station identification code every
A. 
B. 
C. 
D.