58
14 CFR Ch. I (1–1–14 Edition)
Pt. 60, App. A
T
ABLE
A2A—F
ULL
F
LIGHT
S
IMULATOR
(FFS) O
BJECTIVE
T
ESTS
—Continued
QPS Requirements
Information
Test
Tolerance
Flight conditions
Test details
Simulator level
Notes
Entry No.
Title
A B
C
D
2.d.4.
.............
Spiral Stability
.................
Correct trend and
±
2
°
or
±
10% bank angle in 20
seconds. Alternate test re-
quires correct trend and
±
2
°
aileron.
Cruise, and Approach
or Landing.
Record results for both directions. Air-
plane data averaged from multiple
tests may be used. As an alternate
test, demonstrate the lateral control re-
quired to maintain a steady turn with a
bank angle of 28
°
to 32
°
.
CCA: Test in Non-normal control state
X X
X X
2.d.5.
.............
Engine Inoperative Trim
±
1
°
rudder angle or
±
1
°
tab
angle or equivalent pedal,
±
2
°
sideslip angle.
Second Segment
Climb, and Approach
or Landing.
May be a series of snapshot tests
..........
X
X
X
X
The test should be
performed in a man-
ner similar to that for
which a pilot is
trained to trim an
engine failure condi-
tion. Second seg-
ment climb test
should be at takeoff
thrust. Approach or
landing test should
be at thrust for level
flight.
2.d.6.
.............
Rudder Response
...........
±
2
°
/sec or
±
10% yaw rate
...
Approach or Landing
...
Record
results
for
stability
augmentation
system ON and OFF. A rudder step
input of 20%–30% rudder pedal throw
is used.
CCA: Test in Normal and Non-normal
control states
X X X X
2.d.7.
.............
Dutch Roll, (Yaw Damper
OFF).
±
0.5 sec or
±
10% of period,
±
10% of time to
1
⁄
2
or
double amplitude or
±
.02
of damping ratio.
±
20% or
±
1 sec of time difference
between peaks of bank
and sideslip.
Cruise, and Approach
or Landing.
Record results for at least 6 complete
cycles with stability augmentation OFF.
CCA: Test in Non-normal control state.
X X X
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