66 

14 CFR Ch. I (1–1–14 Edition) 

Pt. 60, App. A 

T

ABLE

A2A—F

ULL

F

LIGHT

S

IMULATOR

(FFS) O

BJECTIVE

T

ESTS

—Continued 

QPS Requirements 

Information 

Test 

Tolerance 

Flight conditions 

Test details 

Simulator level 

Notes 

Entry No. 

Title 

A B 

C 

D 

..................

300 ms (or less) after air-

plane response.

Take-off, cruise, and 

approach or landing.

One test is required in each axis (pitch, 

roll and yaw) for each of the three 

conditions (take-off, cruise, and ap-

proach or landing).

X 

X 

The visual scene or 

test pattern used 

during the response 

testing should be 

representative of the 

system capacities 

required to meet the 

daylight, twilight 

(dusk/dawn) and/or 

night visual capa-

bility as appropriate. 

..................

150 ms (or less) after air-

plane response.

Take-off, cruise, and 

approach or landing.

One test is required in each axis (pitch, 

roll and yaw) for each of the three 

conditions (take-off, cruise, and ap-

proach or landing)..

X X 

4.a.2.

.............

Transport Delay.

..................

300 ms (or less) after con-

troller movement.

N/A

...............................

A separate test is required in each axis 

(pitch, roll, and yaw).

X 

X 

If Transport Delay is 

the chosen method 

to demonstrate rel-

ative responses, the 

sponsor and the 

NSPM will use the 

latency values to en-

sure proper simu-

lator response when 

reviewing those ex-

isting tests where la-

tency can be identi-

fied (e.g., short pe-

riod, roll response, 

rudder response) 

..................

150 ms (or less) after con-

troller movement.

N/A

...............................

A separate test is required in each axis 

(pitch, roll, and yaw).

X X 

4.b.

................

Field-of-view. 

VerDate Mar<15>2010 

20:48 Jan 30, 2014

Jkt 232047

PO 00000

Frm 00076

Fmt 8010

Sfmt 8002

Q:\14\14V2.TXT

ofr150

PsN: PC150