226
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.a.1.
..........
Cyclic
.....................................
Breakout—
±
0.25 lbs. (0.112
daN) or 25%; Force—
±
1.0
lb. (0.224 daN) or 10%.
Ground; Static conditions with
the hydraulic system (if ap-
plicable) pressurized; sup-
plemental hydraulic pres-
surization system may be
used. Trim On and Off.
Friction Off Augmentation
(if applicable) On and Off.
Record results for an uninter-
rupted control sweep to the
stops. (This test does not
apply if aircraft hardware
modular controllers are
used.)
X
X
X
Flight Test Data for this test
does not require the rotor
to be engaged/turning. The
phrase ‘‘if applicable’’ re-
garding stability augmenta-
tion systems means if an
augmentation system is
available and if this system
may be operational on the
ground under static condi-
tions as described here.
2.a.2.
..........
Collective/Pedals
...................
Breakout—
±
0.5 lb. (0.224
daN) or 25%; Force—
±
1.0
lb. (0.224 daN) or 10%.
Ground; Static conditions with
the hydraulic system (if ap-
plicable) pressurized; sup-
plemental hydraulic pres-
surization system may be
used. Trim On and Off.
Friction Off. Augmentation
(if applicable) On and Off.
Record results for an uninter-
rupted control sweep to the
stops.
X
X
X
Flight Test Data for this test
does not require the rotor
to be engaged/turning. The
phrase ‘‘if applicable’’ re-
garding stability augmenta-
tion system means if a sta-
bility augmentation system
is available and if this sys-
tem may be operational on
the ground under static
conditions as described
here.
2.a.3.
..........
Brake Pedal Force vs. Posi-
tion.
±
5 lbs. (2.224 daN) or 10%.
Ground; Static conditions.
X
X
X
2.a.4.
..........
Trim System Rate (all appli-
cable systems).
Rate—
±
10%.
Ground; Static conditions.
Trim On, Friction Off.
The tolerance applies to the
recorded value of the trim
rate.
X X X
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