228
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.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 con-
trol input. The Off-axis re-
sponse must show correct
trend for unaugmented
cases.
X
X
This is a ‘‘short time’’ test
conducted in a hover, in
ground effect, without en-
tering translational flight, to
provide better visual ref-
erence.
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 con-
trol input. The Off-axis re-
sponse must show correct
trend for unaugmented
cases.
X
X
This is a ‘‘short time’’ test
conducted in a hover, in
ground effect, without en-
tering translational flight, to
provide better visual ref-
erence.
2.b.3.d.
.......
Vertical
...................................
Normal Acceleration—
±
0.1 g.
Hover Augmentation On and
Off.
Record results for a step con-
trol input. The Off-axis re-
sponse must show correct
trend for unaugmented
cases.
X 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 in-
clude minimum power re-
quired speed. Record data
for a step control input.
The Off-axis response
must show correct trend for
unaugmented cases.
X X X
2.c.2.
...........
Static Stability
........................
Longitudinal Control Position:
±
10% of change from trim
or
±
0.25 in. (6.3 mm) or
Longitudinal Control Force
:
±
0.5 lb. (0.223 daN) or
±
10%.
Cruise or Climb. Autorotation.
Augmentation On and Off.
Record results for a minimum
of two speeds on each side
of the trim speed. May be
a series of snapshot tests.
X X X
2.c.3.
...........
Dynamic Stability
VerDate Mar<15>2010
20:48 Jan 30, 2014
Jkt 232047
PO 00000
Frm 00238
Fmt 8010
Sfmt 8002
Q:\14\14V2.TXT
ofr150
PsN: PC150