356 

14 CFR Ch. I (1–1–19 Edition) 

Pt. 60, App. C 

T

ABLE

C2A—F

ULL

F

LIGHT

S

IMULATOR

(FFS) O

BJECTIVE

T

ESTS

—Continued 

QPS requirements 

Information 

Test 

Tolerance(s) 

Flight condition 

Test details 

Simulator 

level 

Notes 

Entry No. 

Title 

B C D 

4.b.1. ..........

Continuous field-of-view. 

The simulator must provide a 

continuous field-of-view of 
at least 75

° 

horizontally 

and 30

° 

vertically per pilot 

seat or the number of de-
grees necessary to meet 
the visual ground segment 
requirement, whichever is 
greater. Both pilot seat vis-
ual systems must be oper-
able simultaneously. Wide- 
angle systems providing 
cross-flight deck viewing 
(for both pilots simulta-
neously) must provide a 
minimum field-of-view of at 
least 146

° 

horizontally and 

36

° 

vertically. Any geo-

metric error between the 
Image Generator eye point 
and the pilot eye point 
must be 8

° 

or less. 

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

An SOC is required and must 

explain the geometry of the 
installation. 

Additional horizontal field-of- 

view capability may be 
added at the sponsor’s dis-
cretion provided the min-
imum field-of-view is re-
tained. 

X 

Horizontal field-of-view is 

centered on the zero de-
gree 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 5

° 

squares. 

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