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827 

Federal Aviation Administration, DOT 

§ 171.107 

§ 171.101 Scope. 

This subpart sets forth minimum re-

quirements for the approval and oper-
ation of non-Federal Simplified Direc-
tional Facilities (SDF) that are to be 
involved in the approval of instrument 
flight rules and air traffic control pro-
cedures related to those facilities. 

§ 171.103 Requests for IFR procedure. 

(a) Each person who requests an IFR 

procedure based on an SDF that he 
owns must submit the following infor-
mation with that request: 

(1) A description of the facility and 

evidence that the equipment meets the 
performance requirements of § 171.109 
and the standards and tolerances of 
§ 171.111, and is installed in accordance 
with § 171.113. 

(2) A proposed procedure for oper-

ating the facility. 

(3) A proposed maintenance organiza-

tion and a maintenance manual that 
meets the requirements of § 171.115. 

(4) A statement of intent to meet the 

requirements of this subpart. 

(5) A showing that the facility has an 

acceptable level of operational reli-
ability as prescribed in § 171.111(k), and 
an acceptable standard of performance. 
Previous equivalent operational experi-
ence with a facility with identical de-
sign and operational characteristics 
will be considered in showing compli-
ance with this paragraph. 

(b) After the Federal Aviation Ad-

ministration inspects and evaluates 
the facility, it advises the owner of the 
results and of any required changes in 
the facility or the maintenance manual 
or maintenance organization. The 
owner must then correct the defi-
ciencies, if any, and operate the facil-
ity for an in-service evaluation by the 
Federal Aviation Administration. 

§ 171.105 Minimum requirements for 

approval. 

(a) The following are the minimum 

requirements that must be met before 
the Federal Aviation Administration 
will approve an IFR procedure for a 
non-Federal Simplified Directional Fa-
cility: 

(1) A suitable frequency channel 

must be available. 

(2) The facility’s performance, as de-

termined by air and ground inspection, 

must meet the requirements of 
§§ 171.109 and 171.111. 

(3) The installation of the equipment 

must meet the requirements of 
§ 171.113. 

(4) The owner must agree to operate 

and maintain the facility in accord-
ance with § 171.115. 

(5) The owner must agree to furnish 

periodic reports as set forth in § 171.117, 
and agree to allow the FAA to inspect 
the facility and its operation whenever 
necessary. 

(6) The owner must assure the FAA 

that he will not withdraw the facility 
from service without the permission of 
the FAA. 

(7) The owner must bear all costs of 

meeting the requirements of this sec-
tion and of any flight or ground inspec-
tions made before the facility is com-
missioned, except that the FAA may 
bear certain of these costs subject to 
budgetary limitations and policy estab-
lished by the Administrator. 

(b) If the applicant for approval 

meets the requirements of paragraph 
(a) of this section, the FAA commis-
sions the facility as a prerequisite to 
its approval for use in an IFR proce-
dure. The approval is withdrawn at any 
time the facility does not continue to 
meet those requirements. In addition, 
the facility is licensed by the Federal 
Communications Commission. The 
Federal Aviation Administration rec-
ommends cancellation or nonrenewal 
of the Federal Communications Com-
mission license whenever the frequency 
channel is needed for higher priority 
common system service. 

§ 171.107 Definition. 

As used in this subpart: 

SDF 

(simplified directional facility) 

means a directional aid facility pro-
viding only lateral guidance (front or 
back course) for approach from a final 
approach fix. 

DDM 

(difference in depth of modula-

tion) means the percentage modulation 
depth of the larger signal minus the 
percentage modulation depth of the 
smaller signal, divided by 100. 

Angular displacement sensitivity 

means 

the ratio of measured DDM to the cor-
responding angular displacement from 
the appropriate reference line. 

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828 

14 CFR Ch. I (1–1–24 Edition) 

§ 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