Piper Cherokee Archer II Pilot Operating Handbook page 17

PIPER AIRCRAFT CORPORATION
PA-28-181, CHEROKEE ARCHER II
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(c)
Power Tenninology
Takeoff Power
Maximum Continuous
Power
Maximum Climb Power
Maximum Cruise Power
(d) Engine Instruments
EGTGauge
SECfION 1
GENERAL
Maximum power pennissible for takeoff.
Maximum power permissible continuously during flight.
Maximum power permissible during climb.
Maximum power pennissible during cruise.
Exhaust Gas Temperature Gauge
(e) Airplane Perfonnance and Flight Planning Tenninology
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Climb Gradient
Demonstrated Crosswind
Velocity
Accelera te-Stop Distance
Route Segment
ISSUED: JUNE 18, 1976
REVISED: MARCH30. 1984
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: (I) a
geographical location; or (2) a point at which a defmite radio fix
can be established.
,
REPORT: VB-790
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