30
14 CFR Ch. I (1–1–14 Edition)
Pt. 60, App. A
T
ABLE
A1A—M
INIMUM
S
IMULATOR
R
EQUIREMENTS
—Continued
QPS requirements
Simulator levels
Information
Entry No.
General simulator requirements
A
B
C
D
Notes
2.f. ............
The simulator must provide for manual
and automatic testing of simulator
hardware and software programming
to determine compliance with simu-
lator objective tests as prescribed in
Attachment 2 of this appendix.
An SOC is required.
X
X Automatic ‘‘flagging’’ of out-of-tolerance situations is
encouraged.
2.g. ...........
Relative responses of the motion sys-
tem, visual system, and flight deck
instruments, measured by latency
tests or transport delay tests. Motion
onset should occur before the start of
the visual scene change (the start of
the scan of the first video field con-
taining different information) but must
occur before the end of the scan of
that video field. Instrument response
may not occur prior to motion onset.
Test results must be within the fol-
lowing limits:
The intent is to verify that the simulator provides in-
strument, motion, and visual cues that are, within
the stated time delays, like the airplane re-
sponses. For airplane response, acceleration in
the appropriate, corresponding rotational axis is
preferred.
2.g.1. ........
300 milliseconds of the airplane re-
sponse.
X X
2.g.2. ........
150 milliseconds of the airplane re-
sponse.
X X
2.h. ...........
The simulator must accurately repro-
duce the following runway conditions:
X X
(1) Dry.
(2) Wet.
(3) Icy.
(4) Patchy Wet.
(5) Patchy Icy.
(6) Wet on Rubber Residue in Touch-
down Zone.
An SOC is required.
2.i. .............
The simulator must simulate:
(1) brake and tire failure dynamics, in-
cluding antiskid failure.
(2) decreased brake efficiency due to
high brake temperatures, if applica-
ble.
An SOC is required.
X
X Simulator pitch, side loading, and directional control
characteristics should be representative of the air-
plane.
2.j. .............
The simulator must replicate the effects
of airframe and engine icing.
X X
2.k. ............
The aerodynamic modeling in the simu-
lator must include:
(1) Low-altitude level-flight ground ef-
fect;
(2) Mach effect at high altitude; ............
(3) Normal and reverse dynamic thrust
effect on control surfaces;
X
See Attachment 2 of this appendix, paragraph 5, for
further information on ground effect.
(4) Aeroelastic representations; and
(5) Nonlinearities due to sideslip.
An SOC is required and must include
references to computations of
aeroelastic representations and of
nonlinearities due to sideslip.
2.l. .............
The simulator must have aerodynamic
and ground reaction modeling for the
effects of reverse thrust on direc-
tional control, if applicable.
An SOC is required.
X X X
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