Piper PA-46-350P Malibu Mirage Pilot's Manual And Operation Manual page 24

SECTION 1
GENERAL
1.21 SYMBOLS, ABBREVIATIONS AND TERMINOLOGY (Continued)
(c) Power Terminology
Takeoff Power
Maximum Con-
tinuous Power
Maximum Climb
Power
Maximum Cruise
Power
(d) Engine Instruments
T.I.T. Gauge
(e) Airplane Performance and Flight Planning Terminology
Climb Gradient
Demonstrated
Crosswind
Velocity
Accelerate-Stop
Distance
Route Segment
REPORT: VB-1710
1-10
Maximum power permissible for takeoff.
Maximum power permissible contin-
uously during flight.
Maximum power permissible during
climb.
Maximum power permissible during
cruise.
Turbine Inlet Temperature
The demonstrated ratio of the change in
height during a portion of a climb, to the
horizontal distance traversed in the same
time interval.
The demonstrated crosswind velocity is the
velocity of the crosswind component for
which adequate control of the airplane
during takeoff and landing was actually
demonstrated during certification tests.
The distance required to accelerate an air-
plane to a specified speed and, assuming
failure of an engine at the instant that speed
is attained, to bring the airplane to a stop.
A part of a route. Each end of that part is
identified by (1) a geographical location
or (2) a point at which a definite radio fix
can be established.
ISSUED: FEBRUARY 23, 1999
PA-46-350P, MALIBU