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SECTION
1 !
GENERAL
PIPER
AIRCRAFT
CORPORATION
PA-28-181, ARCHER
II
Indicated
Pressure Altitude
Pressure Altitude
Station Pressure
Wind
(c}
Power Terminology
Takeoff Power
Maximum
Continuous
Power
(d)
Engine Instruments
EGT Gauge
REPORT:
VB-1120
1-8
The
number
actually
read
from
an
altimeter when the barometric subscale has
been set to 29.92 inches of mercury (1013.2
millibars).
Altitude measured from standard sea-level
pressure (29.92 in. Hg) by a pressure or
barometric
altimeter.
It is the indicated
pressure altitude corrected for position and
instrument
error.
In
this
handbook,
altimeter
instrument
errors are assumed
to be zero.
Actual
atmospheric
pressure
at
field
elevation.
The wind velocities recorded as variables
on the charts of this handbook are to be
understood
as the headwind
or tailwind
components of the reported winds.
Maximum
power permissible for takeoff.
Maximum power permissible continuously
during flight.
Exhaust Gas Temperature Gauge
ISSUED: JULY 2, 1979
REVISED: JUNE 29, 1984
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