AggieMike88
Touchdown! Greaser!
- Joined
- Jan 13, 2010
- Messages
- 20,804
- Location
- Denton, TX
- Display Name
Display name:
The original "I don't know it all" of aviation.
Question 1107 from the Instrument Ground Instructor Prep
When making an airborne VOR check, what is the maximum allowable tolerance between the two indicators of a dual VOR system (units independent of each other except the antenna)?
A) 6° between the two indicated radials of a VOR
B) 4° between the two indicated bearings of a VOR.
C) Plus or minus 4° when set to identical radials of a VOR
B) 4° between the two indicated bearings of a VOR.
C) Plus or minus 4° when set to identical radials of a VOR
Sheppard Air has the correct answer as (b), citing FAR 91.171(c)
"If dual system VOR (units independent of each other except for the antenna) is installed on the aircraft, the person checking the equipment my check one system against the other in place of the check procedures specified in paragraph (b) of this section. Both systems shall be tuned to the same VOR ground facility and note the indicated bearings to that station. The maximum permissible variation between the two indicated bearings is 4°"
And Sheppard Air's explanation does include the comment that this question often confuses the test takers.
Is this regulation and question not talking about the common "dual CDI" setup that the majority of us have in our aircraft? If that is correct, can someone supply a photo or image of what this instrument looks like?
I accept the answer to the question to be correct (essentially the question is a rephrase of the regulation). But I'm stumbling on visualizing what this would look like on an instrument panel.