817
Federal Aviation Administration, DOT
§ 171.109
Back course sector
means the course
sector on the opposite end of the run-
way from the front course sector.
Course line
means the locus of points
along the final approach course at
which the DDM is zero.
Course sector
means a sector in a hori-
zontal plane containing the course line
and limited by the loci of points near-
est to the course line at which the
DDM is 0.155.
Displacement sensitivity
means the
ratio of measured DDM to the cor-
responding lateral displacement from
the appropriate reference line.
Front course sector
means the course
sector centered on the course line in
the direction from the runway in which
a normal final approach is made.
Half course sector
means the sector in
a horizontal plane containing the
course line and limited by the loci of
points nearest to the course line, at
which the DDM is 0.0775.
Point A
means a point on the front
course in the approach direction a dis-
tance of 4 nautical miles from the
threshold.
Point A1
means a point on the front
course in the approach direction a dis-
tance of 1 statute mile from the thresh-
old.
Point A2
means a point on the front
course at the threshold.
Reference datum
means a point at a
specified height located vertically
above the intersection of the course
and the threshold.
Missed approach point
means the
point on the final approach course, not
farther from the final approach fix
than Point ‘‘A2’’, at which the ap-
proach must be abandoned, if the ap-
proach and subsequent landing cannot
be safely completed by visual ref-
erence, whether or not the aircraft has
descended to the minimum descent al-
titude.
§ 171.109
Performance requirements.
(a) The Simplified Directional Facil-
ity must perform in accordance with
the following standards and practices:
(1) The radiation from the SDF an-
tenna system must produce a com-
posite field pattern which is amplitude
modulated by a 90 Hz and a 150 Hz tone.
The radiation field pattern must
produce a course sector with the 90 Hz
tone predominating on one side of the
course and with the 150 Hz tone pre-
dominating on the opposite side.
(2) When an observer faces the SDF
from the approach end of runway, the
depth of modulation of the radio fre-
quency carrier due to the 150 Hz tone
must predominate on his right hand
and that due to the 90 Hz tone must
predominate on his left hand.
(3) All horizontal angles employed in
specifying the SDF field patterns must
originate from the center of the an-
tenna system which provides the sig-
nals used in the front course sector.
(4) The SDF must operate on odd
tenths or odd tenths plus a twentieth
MHz within the frequency band 108.1
MHz to 111.95 MHz. The frequency tol-
erance of the radio frequency carrier
must not exceed plus or minus 0.002
percent.
(5) The radiated emission from the
SDF must be horizontally polarized.
The vertically polarized component of
the radiation on the course line must
not exceed that which corresponds to
an error one-twentieth of the course
sector width when an aircraft is posi-
tioned on the course line and is in a
roll attitude of 20
°
from the horizontal.
(6) The SDF must provide signals suf-
ficient to allow satisfactory operation
of a typical aircraft installation within
the sector which extends from the cen-
ter of the SDF antenna system to dis-
tances of 18 nautical miles within a
plus or minus 10
°
sector and 10 nautical
miles within the remainder of the cov-
erage when alternative navigational fa-
cilities provide satisfactory coverage
within the intermediate approach area.
SDF signals must be receivable at the
distances specified at and above a
height of 1,000 feet above the elevation
of the threshold, or the lowest altitude
authorized for transition, whichever is
higher. Such signals must be receiv-
able, to the distances specified, up to a
surface extending outward from the
SDF antenna and inclined at 7
°
above
the horizontal.
(7) The modulation tones must be
phase-locked so that within the half
course sector, the demodulated 90 Hz
and 150 Hz wave forms pass through
zero in the same direction within 20
°
of
phase relative to the 150 Hz component,
every half cycle of the combined 90 Hz
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