324
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
Performance and
Trimmed Flight Con-
trol Positions.
Vertical Velocity—
±
100 fpm (61
m/sec) or
±
10% Pitch Atti-
tude—
±
1.5
°
Sideslip Angle—
±
2
°
Longitudinal Control Posi-
tion—
±
5% Lateral Control Posi-
tion—
±
5% Directional Control
Position—
±
5% Collective Con-
trol Position—
±
5%.
All engines operating
One engine inoper-
ative.
Augmentation Sys-
tem(s) On and Off.
Record results for two gross
weight and CG combinations.
The data presented must be for
normal climb power conditions.
May be a series of snapshot
tests.
X X
X
1.h.
........................
Descent.
1.h.1.
.....................
Descent Performance
and Trimmed Flight
Control Positions.
Torque—
±
3% Pitch Attitude—
±
1.5
°
Sideslip Angle—
±
2
°
Lon-
gitudinal Control Position—
±
5%
Lateral Control Position—
±
5%
Directional Control Position—
±
5% Collective Control Posi-
tion—
±
5%.
At or near 1,000 fpm
(5 m/sec) rate of
descent (RoD) at
normal approach
speed.
Augmentation Sys-
tem(s) On and Off.
Record results for two gross
weight and CG combinations.
May be a series of snapshot
tests.
X X X
1.h.2.
.....................
Autorotation Perform-
ance and Trimmed
Flight Control Posi-
tions.
Pitch Attitude—
±
1.5
°
Sideslip
Angle—
±
2
°
Longitudinal Con-
trol Position—
±
5% Lateral Con-
trol Position—
±
5% Directional
Control Position—
±
5% Collec-
tive Control Position—
±
5%.
Steady descents.
Augmentation Sys-
tem(s) On and Off.
Record results for two gross
weight conditions. Data must
be recorded for normal oper-
ating RPM. (Rotor speed toler-
ance applies only if collective
control position is full down.)
Data must be recorded for
speeds from 50 kts,
±
5 kts
through at least maximum glide
distance airspeed. May be a
series of snapshot tests.
X X
X
1.i.
..........................
Autorotation.
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