Piper WARRIOR III PA-28-161 Pilot Operating Handbook page 17

PIPER AIRCRAFT CORPORATION
PA-28-161, WARRIOR III
Indicated Pressure
Altitude
Pressure Altitude
Station Pressure
Wind
(c) Power Terminology
Takeoff Power
Maximum Con-
tinuous Power
Maximum Climb
Power
Maximum Cruise
Power
(d) Engine Instruments
EGT Gauge
ISSUED: JULY 1, 1994
T h e n u m b e r a c t u a l l y r e a d f r o m a n
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
instr u m e n t e r r o r. I n t h i s h a n d b o o k ,
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.
Maximum power permissible during
climb.
Maximum power permissible during
cruise.
Exhaust Gas Temperature Gauge
SECTION 1
GENERAL
REPORT: VB-1565
1-7