222
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
1.c.3.
...........
One Engine inoperative, re-
jected take off.
Airspeed—
±
3 kt, Altitude—
±
20 ft (6.1m), Torque—
±
3%, Rotor Speed—
±
1.5%,
Pitch Attitude—
±
1.5
°
, Roll
angle—
±
1.5
°
, Heading—
±
2
°
, Longitudinal Control
Position—
±
10%, Lateral
Control Position—
±
10%,
Directional Control Posi-
tion—
±
10%, Collective
Control Position—
±
10%,
Distance—
±
7.5% or
±
30m
(100ft).
Ground, Takeoff
....................
Time history from the take off
point to touch down. Test
conditions near limiting per-
formance.
X X
1.d.
.............
Hover
Performance
..........................
Torque—
±
3%, Pitch Atti-
tude—
±
1.5
°
, Bank Atti-
tude—
±
1.5
°
, Longitudinal
Control Position—
±
5%,
Lateral Control Position—
±
5%, Directional Control
Position—
±
5%, Collective
Control Position—
±
5%.
In Ground Effect (IGE); and
Out of Ground Effect
(OGE).
Record results for light and
heavy gross weights. May
be a series of snapshot
tests.
X X
1.e.
.............
Vertical Climb
Performance
..........................
Vertical Velocity—
±
100 fpm
(0.50 m/sec) or
±
10%, Di-
rectional Control Position—
±
5%, Collective Control Po-
sition—
±
5%.
From OGE Hover
..................
Record results for light and
heavy gross weights. May
be a series of snapshot
tests.
X X
1.f.
..............
Level Flight
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