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33 

Federal Aviation Administration, DOT 

Pt. 60, App. A 

T

ABLE

A1A—M

INIMUM

S

IMULATOR

R

EQUIREMENTS

—Continued 

QPS requirements 

Simulator levels 

Information 

Entry No. 

General simulator requirements 

Notes 

6.a. ...........

The simulator must have a visual sys-

tem providing an out-of-the-flight 
deck view.

X X X X 

6.b. ...........

The simulator must provide a contin-

uous collimated field-of-view of at 
least 45

° 

horizontally and 30

° 

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 si-
multaneously. The minimum hori-
zontal field-of-view coverage must be 
plus and minus one-half (

1

2

) of the 

minimum continuous field-of-view re-
quirement, centered on the zero de-
gree azimuth line relative to the air-
craft fuselage.

An SOC is required and must explain 

the system geometry measurements 
including system linearity and field- 
of-view. 

Additional field-of-view capability may be added at 

the sponsor’s discretion provided the minimum 
fields of view are retained. 

6.c. ............

(Reserved).

6.d. ...........

The simulator must provide a contin-

uous collimated visual field-of-view of 
at least 176

° 

horizontally and 36

° 

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 min-

imum continuous field-of-view re-
quirement, centered on the zero de-
gree azimuth line relative to the air-
craft fuselage.

An SOC is required and must explain 

the system geometry measurements 
including system linearity and field- 
of-view. 

X  The horizontal field-of-view is traditionally described 

as a 180

° 

field-of-view. However, the field-of-view 

is technically no less than 176

°

. Additional field-of- 

view capability may be added at the sponsor’s dis-
cretion provided the minimum fields-of-view are 
retained. 

6.e. ...........

The visual system must be free from 

optical discontinuities and artifacts 
that create non-realistic cues.

X  Non-realistic cues might include image ‘‘swimming’’ 

and image ‘‘roll-off,’’ that may lead a pilot to make 
incorrect assessments of speed, acceleration, or 
situational awareness. 

6.f. ............

The simulator must have operational 

landing lights for night scenes. 
Where used, dusk (or twilight) 
scenes require operational landing 
lights.

X X X X 

6.g. ...........

The simulator must have instructor con-

trols for the following: 

(1) Visibility in statute miles (km) and 

runway visual range (RVR) in ft. (m). 

(2) Airport selection. 
(3) Airport lighting. 

X X X X 

6.h. ...........

The simulator must provide visual sys-

tem compatibility with dynamic re-
sponse programming.

X X X X 

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