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VerDate Sep<11>2014
QPS requirements

Information

Jkt 247047

Test
Tolerance(s)
Entry No.
4.b.1. ..........

Flight condition

Test details

Title
Continuous field-of-view.

Simulator
level
B

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356

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The simulator must provide a
continuous field-of-view of
at least 75Section horizontally
and 30Section vertically per pilot
seat or the number of degrees necessary to meet
the visual ground segment
requirement, whichever is
greater. Both pilot seat visual systems must be operable simultaneously. Wideangle systems providing
cross-flight deck viewing
(for both pilots simultaneously) must provide a
minimum field-of-view of at
least 146Section horizontally and
36Section vertically. 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.
Additional horizontal field-ofview capability may be
added at the sponsor-s discretion provided the minimum field-of-view is retained.

X

C

Notes

D

Pt. 60, App. C

16:30 Jun 25, 2019

TABLE C2A - FULL FLIGHT SIMULATOR (FFS) OBJECTIVE TESTS - Continued

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.

PC31

14 CFR Ch. I (1-1-19 Edition)

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