230
14 CFR Ch. I (1–1–14 Edition)
Pt. 60, App. C
T
ABLE
C2A—F
ULL
F
LIGHT
S
IMULATOR
(FFS) O
BJECTIVE
T
ESTS
—Continued
QPS requirements
Information
Test
Tolerance(s)
Flight condition
Test details
Simulator
level
Notes
Entry No.
Title
B C
D
2.d.1.a
........
Lateral
....................................
Roll Rate—
±
10% or
±
3
°
/sec.,
Roll Attitude Change—
±
10% or
±
3
°
.
Cruise Augmentation On and
Off.
Record results for at least
two airspeeds, including
the speed at or near the
minimum power required
airspeed.
Record results for a step con-
trol input. The Off-axis re-
sponse must show correct
trend for unaugmented
cases.
X X X
2.d.1.b.
.......
Directional
..............................
Yaw Rate—
±
10% or
±
2
°
/sec.,
Yaw Attitude Change—
±
10% or
±
2
°
.
Cruise Augmentation On and
Off.
Record data for at least two
airspeeds, including the
speed at or near the min-
imum power required air-
speed.
Record results for a step con-
trol input. The Off-axis re-
sponse must show correct
trend for unaugmented
cases.
X X X
2.d.2.
..........
Directional Static Stability.
Lateral Control Position—
±
10% of change from trim
or
±
0.25 in. (6.3 mm) or
Lateral Control Force—
±
0.5 lb. (0.223 daN) or
10%, Roll Attitude—
±
1.5,
Directional Control Posi-
tion—
±
10% of change from
trim or
±
0.25 in. (6.3 mm)
or Directional Control
Force—
±
1 lb. (0.448 daN)
or 10%, Longitudinal Con-
trol Position—
±
10% of
change from trim or
±
0.25
in. (6.3 mm), Vertical Ve-
locity—
±
100 fpm (0.50m/
sec) or 10%.
Cruise; or Climb (may use
Descent instead of Climb if
desired), Augmentation On
and Off.
Record results for at least
two sideslip angles on ei-
ther side of the trim point.
The force may be shown
as a cross plot for irrevers-
ible systems. May be a se-
ries of snapshot tests.
X
X
X
This is a steady heading
sideslip test at a fixed col-
lective position.
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