Piper CHEROKEE ARCHER II Pilot Operating Handbook page 14

PIPER AIRCRAFT CORPORATION
PA-28-18I, CHEROKEE ARCHER
II
(e) Power Terminology (Specific)
Takeoff Power
Maximum Continuous
Power
Maximum Climb Power
Maximum Cruise Power
Flight Idle Power
Ground Idle Power
(d) Engine In strument s
EOT Gauge
Maximum Rated Power (180 HP
@
2700 RPM)
Maximum Rated Power (180 HP@ 2700 RPM)
Maximum Rated Power (180 HP@ 2700 RPM)
Maximum Rated Power (180 HP@ 2700 RPM)
Throttle Closed
Throttle Closed
Exhaust Gas Temperature Gauge
SECTION I
GENERAL
(e) Airplane Performance and Flight Planning Terminology
Climb Gradient
Demonstrated Crosswind
Velocity
Accelera te-Stop Distance
MEA
Route Segment
ISSUED: AUGUST IS, 1975
The demonstrated ratio of the change in height during a portion of
a climb, to the horizontal di stanc e traversed in the same time
interval.
The demonstrated crosswind ve locity is the velocity of the
crosswind component for which adequate control of the airpl ane
during takeoff and landing ,va s actually demon strated during
certification tests.
The distance required to accelerate un airplane to a specified speed
and. assuming failure of an engine at the in stant thai speed is
altained. to bring the airplane (0 a stop.
Minimum en route IFR altitude.
A pan of a route. Each end of that part is identified
by: (1)
a
geographical location; or (2) a point al which a definite radio fix
can be established.
REPORT: VB· 760
1-7