328 

14 CFR Ch. I (1–1–14 Edition) 

Pt. 60, App. D 

T

ABLE

D2A—F

LIGHT

T

RAINING

D

EVICE

(FTD) O

BJECTIVE

T

ESTS

—Continued 

QPS requirements 

Information 

Test 

Tolerances 

Flight conditions 

Test details 

FTD level 

Notes 

Entry No. 

Title 

5 6 7 

2.b.3.a.

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

Longitudinal

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

Pitch Rate—

±

10% or 

±

2

°

/sec. 

Pitch Attitude Change—

±

10% 

or 1.5

°

.

Hover. Augmentation 

On and Off.

Record results for a step control 

input. The Off-axis response 

must show correct trend for un-

augmented cases. This test 

must be conducted in a hover, 

in ground effect, without enter-

ing translational flight.

X 

This is a ‘‘short time’’ test. 

2.b.3.b.

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

Lateral

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

Roll Rate—

±

10% or 

±

3

°

/sec. Roll 

Attitude Change—

±

10% or 

±

3

°

.

Hover Augmentation 

On and Off.

Record results for a step control 

input. The Off-axis response 

must show correct trend for un-

augmented cases.

X 

This is a ‘‘short time’’ test 

conducted in a hover, in 

ground effect, without en-

tering translational flight, 

to provide better visual 

reference. 

2.b.3.c.

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

Directional

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

Yaw Rate—

±

10% or 

±

2

°

/sec. 

Heading Change—

±

10% or 

±

2

°

.

Hover Augmentation 

On and Off.

Record results for a step control 

input. The Off-axis response 

must show correct trend for un-

augmented cases. This test 

must be conducted in a hover, 

in ground effect, without enter-

ing translational flight.

X 

This is a ‘‘short time’’ test. 

2.b.3.d.

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

Vertical

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

Normal Acceleration 

±

0.1g

...........

Hover Augmentation 

On and Off.

Record results for a step control 

input. The Off-axis response 

must show correct trend for un-

augmented cases.

X 

2.c.

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

Longitudinal Handling Qualities. 

2.c.1.

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

Control Response

.........

Pitch 

Rate—

±

10% or 

±

2

°

/sec. 

Pitch Attitude Change—

±

10% 

or 

±

1.5

°

.

Cruise Augmentation 

On and Off.

Results must be recorded for two 

cruise airspeeds to include min-

imum power required speed. 

Record data for a step control 

input. The Off-axis response 

must show correct trend for un-

augmented cases.

X X X 

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