232
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
3.b.
.............
Leg Balance
Leg Balance
..........................
Based on Simulator Capa-
bility.
N/A
.........................................
Required as part of the
MQTG. The test must dem-
onstrate motion system leg
balance as specified by the
applicant for flight simulator
qualification.
X X X
3.c.
..............
Turn Around
Turn Around
..........................
Based on Simulator Capa-
bility.
N/A
.........................................
Required as part of the
MQTG. The test must dem-
onstrate a smooth turn-
around (shift to opposite di-
rection of movement) of the
motion system as specified
by the applicant for flight
simulator qualification.
X X X
3.d.
.............
Motion system repeatability
With the same input signal,
the test results must be re-
peatable to within
±
0.05g
actual platform linear accel-
eration in each axis.
Accomplished in both the
‘‘ground’’ mode and in the
‘‘flight’’ mode of the motion
system operation.
Required as part of the
MQTG. The test is accom-
plished by injecting a mo-
tion signal to generate
movement of the platform.
The input must be such
that the rotational accelera-
tions, rotational rates, and
linear accelerations are in-
serted before the transfer
from helicopter center of
gravity to the pilot ref-
erence point with a min-
imum amplitude of 5
°
/sec/
sec, 10
°
/sec and 0.3g, re-
spectively.
X
X
X
See Paragraph 6.c. in this at-
tachment for additional in-
formation. Note: if there is
no difference in the model
for ‘‘ground’’ and ‘‘flight’’
operation of the motion
system, this should be de-
scribed in an SOC and will
not require tests in both
modes.
3.e.
.............
Motion cueing performance signature
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