236 

14 CFR Ch. I (1–1–14 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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