spaschal on DSK3GDR082PROD with CFR

Federal Aviation Administration, DOT

Section 1.1

(i) The aircraft is operated in accordance with title 10 of the United States
Code;
(ii) The aircraft is operated in the
performance of a governmental function under title 14, 31, 32, or 50 of the
United States Code and the aircraft is
not used for commercial purposes; or
(iii) The aircraft is chartered to provide transportation to the armed forces
and the Secretary of Defense (or the
Secretary of the department in which
the Coast Guard is operating) designates the operation of the aircraft as
being required in the national interest.
(3) An aircraft owned or operated by
the National Guard of a State, the District of Columbia, or any territory or
possession of the United States, and
that meets the criteria of paragraph (2)
of this definition, qualifies as a public
aircraft only to the extent that it is
operated under the direct control of
the Department of Defense.
Rated 30-second 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 continuation of one
flight operation after the failure or
shutdown of one engine in multiengine
rotorcraft, for up to three periods of
use no longer than 30 seconds each in
any one flight, and followed by mandatory inspection and prescribed maintenance action.
Rated 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 continuation of one
flight operation after the failure or
shutdown of one engine in multiengine
rotorcraft, for up to three periods of
use no longer than 2 minutes each in
any one flight, and followed by mandatory inspection and prescribed maintenance action.
Rated continuous 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 the
time required to complete the flight
after the failure or shutdown of one engine of a multiengine rotorcraft.
Rated maximum continuous augmented
thrust, with respect to turbojet engine
type certification, means the approved
jet thrust that is developed statically
or in flight, in standard atmosphere at
a specified altitude, with fluid injection or with the burning of fuel in a
separate combustion chamber, within
the engine operating limitations established under Part 33 of this chapter,
and approved for unrestricted periods
of use.
Rated maximum continuous power,
with respect to reciprocating, turbopropeller, and turboshaft engines,
means the approved brake horsepower
that is developed statically or in flight,
in standard atmosphere at a specified
altitude, within the engine operating
limitations established under part 33,
and approved for unrestricted periods
of use.
Rated maximum continuous thrust,
with respect to turbojet engine type
certification, means the approved jet
thrust that is developed statically or in
flight, in standard atmosphere at a
specified altitude, 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 approved for unrestricted periods
of use.
Rated takeoff augmented thrust, with
respect to turbojet engine type certification, means the approved jet thrust
that is developed statically under
standard sea level conditions, with
fluid injection or with 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 takeoff power, with respect to
reciprocating, turbopropeller, and turboshaft engine type certification,
means the approved brake horsepower
that is developed statically under
standard sea level conditions, within

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