54 

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 

2.b.5.

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

Small Control Inputs— 

Roll.

±

0.15

°

/sec body roll rate or 

±

20% of peak body roll 

rate applied throughout 

the time history.

Approach 

or 

landing

....

Control inputs must be typical of minor 

corrections made while established on 

an ILS approach course, using from 

0.5

°

/sec to 2

°

/sec roll rate. The test 

may be run in only one direction; how-

ever, for airplanes that exhibit non- 

symmetrical behavior, the test must in-

clude both directions. Time history 

data must be recorded from 5 seconds 

before until at least 5 seconds after 

initiation of control input.

CCA: Test in normal and non-normal 

control states. 

X X 

2.b.6.

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

Small Control Inputs— 

Yaw.

±

0.15

°

/sec body yaw rate or 

±

20% of peak body yaw 

rate applied throughout 

the time history.

Approach 

or 

landing

....

Control inputs must be typical of minor 

corrections made while established on 

an ILS approach course, using from 

0.5

°

/sec to 2

°

/sec yaw rate. The test 

may be run in only one direction; how-

ever, for airplanes that exhibit non- 

symmetrical behavior, the test must in-

clude both directions. Time history 

data must be recorded from 5 seconds 

before until at least 5 seconds after 

initiation of control input.

CCA: Test in normal and non-normal 

control states. 

X X 

2.c.

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

Longitudinal Control Tests. 

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

Power setting is that required for level flight unless otherwise specified. 

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