spaschal on DSK3GDR082PROD with CFR

Section 1.1

14 CFR Ch. I (1-1-19 Edition)

the engine operating limitations established under part 33, and limited in use
to periods of not over 5 minutes for
takeoff operation.
Rated takeoff thrust, with respect to
turbojet engine type certification,
means the approved jet thrust that is
developed statically under standard sea
level conditions, without fluid injection and without the burning of fuel in
a separate combustion chamber, within
the engine operating limitations established under part 33 of this chapter,
and limited in use to periods of not
over 5 minutes for takeoff operation.
Rated 30-minute OEI power, with respect to rotorcraft turbine engines,
means the approved brake horsepower
developed under static conditions at
specified altitudes and temperatures
within the operating limitations established for the engine under part 33 of
this chapter, and limited in use to one
period of use no longer than 30 minutes
after the failure or shutdown of one engine of a multiengine rotorcraft.
Rated 21-2-minute OEI power, with respect to rotorcraft turbine engines,
means the approved brake horsepower
developed under static conditions at
specified altitudes and temperatures
within the operating limitations established for the engine under part 33 of
this chapter for periods of use no
longer than 21-2 minutes each after the
failure or shutdown of one engine of a
multiengine rotorcraft.
Rating means a statement that, as a
part of a certificate, sets forth special
conditions, privileges, or limitations.
Reference landing speed means the
speed of the airplane, in a specified
landing configuration, at the point
where it descends through the 50 foot
height in the determination of the
landing distance.
Reporting point means a geographical
location in relation to which the position of an aircraft is reported.
Restricted area. A restricted area is
airspace designated under Part 73 within which the flight of aircraft, while
not wholly prohibited, is subject to restriction.
Rocket means an aircraft propelled by
ejected expanding gases generated in
the engine from self-contained propellants and not dependent on the intake
of outside substances. It includes any

part which becomes separated during
the operation.
Rotorcraft means a heavier-than-air
aircraft that depends principally for its
support in flight on the lift generated
by one or more rotors.
Rotorcraft-load combination means the
combination of a rotorcraft and an external-load, including the external-load
attaching means. Rotorcraft-load combinations are designated as Class A,
Class B, Class C, and Class D, as follows:
(1) Class A rotorcraft-load combination
means one in which the external load
cannot move freely, cannot be jettisoned, and does not extend below the
landing gear.
(2) Class B rotorcraft-load combination
means one in which the external load is
jettisonable and is lifted free of land or
water during the rotorcraft operation.
(3) Class C rotorcraft-load combination
means one in which the external load is
jettisonable and remains in contact
with land or water during the rotorcraft operation.
(4) Class D rotorcraft-load combination
means one in which the external-load
is other than a Class A, B, or C and has
been specifically approved by the Administrator for that operation.
Route segment is a portion of a route
bounded on each end by a fix or navigation aid (NAVAID).
Sea level engine means a reciprocating
aircraft engine having a rated takeoff
power that is producible only at sea
level.
Second in command means a pilot who
is designated to be second in command
of an aircraft during flight time.
Show, unless the context otherwise
requires, means to show to the satisfaction of the Administrator.
Small aircraft means aircraft of 12,500
pounds or less, maximum certificated
takeoff weight.
Small unmanned aircraft means an unmanned aircraft weighing less than 55
pounds on takeoff, including everything that is on board or otherwise attached to the aircraft.
Small unmanned aircraft system (small
UAS) means a small unmanned aircraft
and its associated elements (including
communication links and the components that control the small unmanned
aircraft) that are required for the safe

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