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14 CFR Ch. I (1–1–19 Edition)
§ 36.1
restricted categories, the following
terms have the specified meanings:
(1)
Stage 1 noise level
means a takeoff,
flyover, or approach noise level greater
than the Stage 2 noise limits pre-
scribed in section H36.305 of appendix H
of this part, or a flyover noise level
greater than the Stage 2 noise limits
prescribed in section J36.305 of appen-
dix J of this part.
(2)
Stage 1 helicopter
means a heli-
copter that has not been shown under
this part to comply with the takeoff,
flyover, and approach noise levels re-
quired for Stage 2 helicopters as pre-
scribed in section H36.305 of appendix H
of this part, or a helicopter that has
not been shown under this part to com-
ply with the flyover noise level re-
quired for Stage 2 helicopters as pre-
scribed in section J36.305 of appendix J
of this part.
(3)
Stage 2 noise level
means a takeoff,
flyover, or approach noise level at or
below the Stage 2 noise limits pre-
scribed in section H36.305 of appendix H
of this part, or a flyover noise level at
or below the Stage 2 limit prescribed in
section J36.305 of appendix J of this
part.
(4)
Stage 2 helicopter
means a heli-
copter that has been shown under this
part to comply with Stage 2 noise lim-
its (including applicable tradeoffs) pre-
scribed in section H36.305 of appendix H
of this part, or a helicopter that has
been shown under this part to comply
with the Stage 2 noise limit prescribed
in section J36.305 of appendix J of this
part.
(5) A ‘‘Stage 3 noise level’’ means a
takeoff, flyover, or approach noise
level at or below the Stage 3 noise lim-
its prescribed in section H36.305 of ap-
pendix H of this part, or a flyover noise
level at or below the Stage 3 noise
limit prescribed in section J36.305 of
appendix J of this part.
(6) A ‘‘Stage 3 helicopter’’ means a
helicopter that has been shown under
this part to comply with the Stage 3
noise limits (including applicable
tradeoffs) prescribed in section H36.305
of appendix H of this part, or a heli-
copter that has been shown under this
part to comply with the Stage 3 noise
limit prescribed in section J36.305 of
appendix J of this part.
(7)
Maximum normal operating RPM
means the highest rotor speed cor-
responding to the airworthiness limit
imposed by the manufacturer and ap-
proved by the FAA. Where a tolerance
on the highest rotor speed is specified,
the maximum normal operating rotor
speed is the highest rotor speed for
which that tolerance is given. If the
rotor speed is automatically linked
with flight condition, the maximum
normal operating rotor speed cor-
responding with the reference flight
condition must be used during the
noise certification procedure. If rotor
speed can be changed by pilot action,
the highest normal operating rotor
speed specified in the flight manual
limitation section for reference condi-
tions must be used during the noise
certification procedure.
(i) For the purpose of showing com-
pliance with this part for tiltrotors,
the following terms have the specified
meanings:
Airplane mode
means a configuration
with nacelles on the down stops (axis
aligned horizontally) and rotor speed
set to cruise revolutions per minute
(RPM).
Airplane mode RPM
means the lower
range of rotor rotational speed in RPM
defined for the airplane mode cruise
flight condition.
Fixed operation points
mean des-
ignated nacelle angle positions selected
for airworthiness reference. These are
default positions used to refer to nor-
mal nacelle positioning operation of
the aircraft. The nacelle angle is con-
trolled by a self-centering switch.
When the nacelle angle is 0 degrees
(airplane mode) and the pilot moves
the nacelle switch upwards, the na-
celles are programmed to automati-
cally turn to the first default position
(for example, 60 degrees) where they
will stop. A second upward move of the
switch will tilt the nacelle to the sec-
ond default position (for example, 75
degrees). Above the last default posi-
tion, the nacelle angle can be set to
any angle up to approximately 95 de-
grees by moving the switch in the up or
down direction. The number and posi-
tion of the fixed operation points may
vary on different tiltrotor configura-
tions.
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