kpayne on VMOFRWIN702 with $$_JOB

VerDate Sep<11>2014
N/A .........................................

An SOC is required and must
explain the geometry of the
installation.
Horizontal field-of-view of at
least 146Section (including not
less than 73Section measured either side of the center of
the design eye point). Additional horizontal field-ofview capability may be
added at the sponsor-s discretion provided the minimum field-of-view is retained.
Vertical field-of-view of at
least 36Section measured from
the pilot-s and co-pilot-s
eye point.

4.b.3. ..........

Continuous field-of-view.

Continuous field-of-view of at
least 176Section horizontal and
56Section vertical field-of-view for
each pilot simultaneously.
Any geometric error between the Image Generator
eye point and the pilot eye
point must be 8Section or less.

N/A .........................................

An SOC is required and must
explain the geometry of the
installation.
Horizontal field-of-view is
centered on the zero degree azimuth line relative
to the aircraft fuselage.
Horizontal field-of-view
must be at least 176Section (including not less than 88Section
either side of the center of
the design eye point). Additional horizontal field-ofview capability may be
added at the sponsor-s discretion provided the minimum field-of-view is retained.
Vertical field-of-view must not
be less than a total of 56Section
measured from the pilot-s
and co-pilot-s eye point.

X

PO 00000

Horizontal field-of-view is
centered on the zero degree azimuth line relative
to the aircraft fuselage.
Field-of-view may be
measured using a visual
test pattern filling the entire
visual scene (all channels)
with a matrix of black and
white 5Section squares.

Frm 00367
Sfmt 8002

357

Fmt 8010

X

Q:\14\14V2.TXT

The horizontal field-of-view is
traditionally described as a
180Section field-of-view. However, the field-of-view is
technically no less than
176Section. Field-of-view may be
measured using a visual
test pattern filling the entire
visual scene (all channels)
with a matrix of black and
white 5Section squares.

PC31

Pt. 60, App. C

The simulator must provide a
continuous field-of-view of
at least 146Section horizontally
and 36Section vertically or the
number of degrees necessary to meet the visual
ground segment requirement, whichever is greater.
The minimum horizontal
field-of-view coverage must
be plus and minus one-half
(1-2) of the minimum continuous field-of-view requirement, centered on the zero
degree azimuth line relative
to the aircraft fuselage. Any
geometric error between
the Image Generator eye
point and the pilot eye
point must be 8Section or less.

Jkt 247047

Continuous field-of-view.

Federal Aviation Administration, DOT

16:30 Jun 25, 2019

4.b.2. ..........