(a) No person may operate a civil aircraft under IFR using the VOR
system of radio navigation unless the VOR equipment of that aircraft --
(1) Is maintained, checked, and inspected under an approved procedure;
or
(2) Has been operationally checked within the preceding 30 days, and
was found to be within the limits of the permissible indicated bearing
error set forth in paragraph (b) or (c) of this section.
(b) Except as provided in paragraph (c) of this section, each person
conducting a VOR check under paragraph (a)(2) of this section shall --
(1) Use, at the airport of intended departure, an FAA-operated or
approved test signal or a test signal radiated by a certificated and
appropriately rated radio repair station or, outside the United States, a
test signal operated or approved by an appropriate authority to check the
VOR equipment (the maximum permissible indicated bearing error is plus or
minus 4 degrees); or
(2) Use, at the airport of intended departure, a point on the airport
surface designated as a VOR system checkpoint by the Administrator, or,
outside the United States, by an appropriate authority (the maximum
permissible bearing error is plus or minus 4 degrees);
(3) If neither a test signal nor a designated checkpoint on the surface
is available, use an airborne checkpoint designated by the Adninistrator
or, outside the United States, by an appropriate authority (the maximum
permissible bearing error is plus or minus 6 degrees); or
(4) If no check signal or point is available, while in flight --
(i) Select a VOR radial that lies along the centerline of an
established VOR airway;
(ii) Select a prominent ground point along the selected radial
preferably more than 20 nautical miles from the VOR ground facility and
maneuver the aircraft directly over the point at a reasonably low
altitude; and
(iii) Note the VOR bearing indicated by the receiver when over the
ground point (the maximum permissible variation between the published
radial and the indicated bearing is 6 degrees).
(c) If dual system VOR (units independent of each other except for the
antenna) is installed in the aircraft, the person checking the equipment
may 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 degrees.
(d) Each person making the VOR operational check, as specified in
paragraph (b) or (c) of this section, shall enter the date, place, bearing
error, and sign the aircraft log or other record. In addition, if a test
signal radiated by a repair station, as specified in paragraph (b)(1) of
this section, is used, an entry must be made in the aircraft log or other
record by the repair station certificate holder or the certificate
holder's representative certifying to the bearing transmitted by the
repair station for the check and the date of transmission.
(Approved by the Office of Management and Budget under control
number 2120-0005)