Piper CHEROKEE WARRIOR 1976 Pilot Operating Handbook page 15

PIPER AIRCRAFT CORPORATION
PA-28-151, CHEROKEE WARRIOR
SECTION 1
GENERAL
(c) Power Terminology
Takeoff Power
Maximum Continuous
Power
Maximum Climb Power
Maximum Cruise Power
Maximum power permissible for takeoff.
Maximum power permissible continuously during flight.
Maximum power permissible during climb.
Maximum power permissible during cruise.
(d) Engine Instruments
EGT Gauge
Exhaust Gas Temperature Gauge
(e) Airplane Performance and Flight Planning Terminology
#
Climb Gradient
Demonstrated Crosswind
Velocity
Accelerate-Stop Distance
Route Segment
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 airplane 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: JUNE 17, 1976
REVISED: AUGUST 17, 1988
REPORT: VB-780
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