448
14 CFR Ch. I (1–1–19 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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