659
Federal Aviation Administration, DOT
§ 77.25
a slope of 7 to 1 from the sides of the
primary surface and from the sides of
the approach surfaces. Transitional
surfaces for those portions of the preci-
sion approach surface which project
through and beyond the limits of the
conical surface, extend a distance of
5,000 feet measured horizontally from
the edge of the approach surface and at
right angles to the runway centerline.
§ 77.21
Department of Defense (DOD)
airport imaginary surfaces.
(a)
Related to airport reference points.
These surfaces apply to all military
airports. For the purposes of this sec-
tion, a military airport is any airport
operated by the DOD.
(1)
Inner horizontal surface. A plane
that is oval in shape at a height of 150
feet above the established airfield ele-
vation. The plane is constructed by
scribing an arc with a radius of 7,500
feet about the centerline at the end of
each runway and interconnecting these
arcs with tangents.
(2)
Conical surface. A surface extend-
ing from the periphery of the inner
horizontal surface outward and upward
at a slope of 20 to 1 for a horizontal dis-
tance of 7,000 feet to a height of 500 feet
above the established airfield ele-
vation.
(3)
Outer horizontal surface. A plane,
located 500 feet above the established
airfield elevation, extending outward
from the outer periphery of the conical
surface for a horizontal distance of
30,000 feet.
(b)
Related to runways. These surfaces
apply to all military airports.
(1)
Primary surface. A surface located
on the ground or water longitudinally
centered on each runway with the same
length as the runway. The width of the
primary surface for runways is 2,000
feet. However, at established bases
where substantial construction has
taken place in accordance with a pre-
vious lateral clearance criteria, the
2,000-foot width may be reduced to the
former criteria.
(2)
Clear zone surface. A surface lo-
cated on the ground or water at each
end of the primary surface, with a
length of 1,000 feet and the same width
as the primary surface.
(3)
Approach clearance surface. An in-
clined plane, symmetrical about the
runway centerline extended, beginning
200 feet beyond each end of the primary
surface at the centerline elevation of
the runway end and extending for 50,000
feet. The slope of the approach clear-
ance surface is 50 to 1 along the runway
centerline extended until it reaches an
elevation of 500 feet above the estab-
lished airport elevation. It then con-
tinues horizontally at this elevation to
a point 50,000 feet from the point of be-
ginning. The width of this surface at
the runway end is the same as the pri-
mary surface, it flares uniformly, and
the width at 50,000 is 16,000 feet.
(4)
Transitional surfaces. These sur-
faces connect the primary surfaces, the
first 200 feet of the clear zone surfaces,
and the approach clearance surfaces to
the inner horizontal surface, conical
surface, outer horizontal surface or
other transitional surfaces. The slope
of the transitional surface is 7 to 1 out-
ward and upward at right angles to the
runway centerline.
§ 77.23
Heliport imaginary surfaces.
(a)
Primary surface. The area of the
primary surface coincides in size and
shape with the designated take-off and
landing area. This surface is a hori-
zontal plane at the elevation of the es-
tablished heliport elevation.
(b)
Approach surface. The approach
surface begins at each end of the heli-
port primary surface with the same
width as the primary surface, and ex-
tends outward and upward for a hori-
zontal distance of 4,000 feet where its
width is 500 feet. The slope of the ap-
proach surface is 8 to 1 for civil heli-
ports and 10 to 1 for military heliports.
(c)
Transitional surfaces. These sur-
faces extend outward and upward from
the lateral boundaries of the primary
surface and from the approach surfaces
at a slope of 2 to 1 for a distance of 250
feet measured horizontally from the
centerline of the primary and approach
surfaces.
Subpart D—Aeronautical Studies
and Determinations
§ 77.25
Applicability.
(a) This subpart applies to any aero-
nautical study of a proposed construc-
tion or alteration for which notice to
the FAA is required under § 77.9.
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660
14 CFR Ch. I (1–1–24 Edition)
§ 77.27
(b) The purpose of an aeronautical
study is to determine whether the
aeronautical effects of the specific pro-
posal and, where appropriate, the cu-
mulative impact resulting from the
proposed construction or alteration
when combined with the effects of
other existing or proposed structures,
would constitute a hazard to air navi-
gation.
(c) The obstruction standards in sub-
part C of this part are supplemented by
other manuals and directives used in
determining the effect on the navigable
airspace of a proposed construction or
alteration. When the FAA needs addi-
tional information, it may circulate a
study to interested parties for com-
ment.
§ 77.27
Initiation of studies.
The FAA will conduct an aero-
nautical study when:
(a) Requested by the sponsor of any
proposed construction or alteration for
which a notice is submitted; or
(b) The FAA determines a study is
necessary.
§ 77.29
Evaluating aeronautical effect.
(a) The FAA conducts an aero-
nautical study to determine the impact
of a proposed structure, an existing
structure that has not yet been studied
by the FAA, or an alteration of an ex-
isting structure on aeronautical oper-
ations, procedures, and the safety of
flight. These studies include evalu-
ating:
(1) The impact on arrival, departure,
and en route procedures for aircraft op-
erating under visual flight rules;
(2) The impact on arrival, departure,
and en route procedures for aircraft op-
erating under instrument flight rules;
(3) The impact on existing and
planned public use airports;
(4) Airport traffic capacity of exist-
ing public use airports and public use
airport development plans received be-
fore the issuance of the final deter-
mination;
(5) Minimum obstacle clearance alti-
tudes, minimum instrument flight
rules altitudes, approved or planned in-
strument approach procedures, and de-
parture procedures;
(6) The potential effect on ATC radar,
direction finders, ATC tower line-of-
sight visibility, and physical or elec-
tromagnetic effects on air navigation,
communication facilities, and other
surveillance systems;
(7) The aeronautical effects resulting
from the cumulative impact of a pro-
posed construction or alteration of a
structure when combined with the ef-
fects of other existing or proposed
structures.
(b) If you withdraw the proposed con-
struction or alteration or revise it so
that it is no longer identified as an ob-
struction, or if no further aeronautical
study is necessary, the FAA may ter-
minate the study.
§ 77.31
Determinations.
(a) The FAA will issue a determina-
tion stating whether the proposed con-
struction or alteration would be a haz-
ard to air navigation, and will advise
all known interested persons.
(b) The FAA will make determina-
tions based on the aeronautical study
findings and will identify the fol-
lowing:
(1) The effects on VFR/IFR aero-
nautical departure/arrival operations,
air traffic procedures, minimum flight
altitudes, and existing, planned, or pro-
posed airports listed in § 77.15(e) of
which the FAA has received actual no-
tice prior to issuance of a final deter-
mination.
(2) The extent of the physical and/or
electromagnetic effect on the oper-
ation of existing or proposed air navi-
gation facilities, communication aids,
or surveillance systems.
(c) The FAA will issue a Determina-
tion of Hazard to Air Navigation when
the aeronautical study concludes that
the proposed construction or alteration
will exceed an obstruction standard
and would have a substantial aero-
nautical impact.
(d) A Determination of No Hazard to
Air Navigation will be issued when the
aeronautical study concludes that the
proposed construction or alteration
will exceed an obstruction standard but
would not have a substantial aero-
nautical impact to air navigation. A
Determination of No Hazard to Air
Navigation may include the following:
(1) Conditional provisions of a deter-
mination.
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