48
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
1.e.3.
.............
Stopping distance, using
wheel brakes and no
reverse thrust on a wet
runway.
±
10% of distance or
±
200 ft
(61 m).
Landing
........................
Either flight test data or manufacturer’s
performance manual data must be
used where available. Engineering
data based on dry runway flight test
stopping distance modified by the ef-
fects of contaminated runway braking
coefficients are an acceptable alter-
native.
X X
1.e.4.
.............
Stopping distance, using
wheel brakes and no
reverse thrust on an
icy runway.
±
10% of distance or
±
200 ft
(61 m).
Landing
........................
Either flight test or manufacturer’s per-
formance manual data must be used,
where available. Engineering data
based on dry runway flight test stop-
ping distance modified by the effects
of contaminated runway braking coeffi-
cients are an acceptable alternative.
X X
1.f.
.................
Engines.
1.f.1.
..............
Acceleration
....................
(
±
10% T
t
) and (
±
10% T
i
, or
±
0.25 sec.).
Approach
or
landing
....
Record engine power (N
1
, N
2
, EPR,
Torque) from flight idle to go-around
power for a rapid (slam) throttle move-
ment.
X
X
X
X
See Appendix F of this
part for definitions of
T
i
and T
t
.
1.f.2.
..............
Deceleration
....................
(
±
10% T
t
) and (
±
10% T
i
, or
±
0.25 sec.).
Ground
.........................
Record engine power (N
1
, N
2
, EPR,
Torque) from Max T/O power to 90%
decay of Max T/O power for a rapid
(slam) throttle movement.
X
X
X
X
See Appendix F of this
part for definitions of
T
i
and T
t
.
2. Handling Qualities.
..................
For simulators requiring Static or Dynamic tests at the controls (i.e., column, wheel, rudder pedal), special
test fixtures will not
be required during initial or upgrade evaluations if the sponsor’s QTG/MQTG shows both test fixture results
and
the results of
an alternative approach, such as computer plots produced concurrently, that provide satisfactory agreement. Repeat of the al-
ternative method during the initial or upgrade evaluation satisfies this test requirement. For initial and upgrade evaluations,
the
control dynamic characteristics must be measured at and recorded directly from the flight deck controls, and must be accom-
plished in takeoff, cruise, and landing flight conditions and configurations. Testing of position versus force is not applicabl
e if
forces are generated solely by use of airplane hardware in the FFS.
Contact the NSPM for
clarification of any
issue regarding air-
planes with revers-
ible controls.
2.a.
................
Static Control Tests.
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