Piper ARCHER III - Page 24

SECTION 1
GENERAL PA-28-181, ARCHER III
SECTION 1
GENERAL PA-28-181, ARCHER III
REPORT: VB-1611 ISSUED: JULY 12, 1995
1-8
REPORT: VB-1611 ISSUED: JULY 12, 1995
1-8
Indicated Th e n um ber actually read from an
Pressure Altitude altimeter when the barometric subscale has
been set to 29.92 inches of mercury (1013.2
millibars).
Pressure Altitude 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.
Station Pressure Actual atmospheric pressure at field
elevation.
Wind 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.
(c) Power Terminology
Takeoff Power Maximum power permissible for takeoff.
Maximum Maximum power permissible continuously
Continuous during flight.
Power
(d) Engine Instruments
EGT Gauge Exhaust Gas Temperature Gauge
Indicated Th e n um ber actually read from an
Pressure Altitude altimeter when the barometric subscale has
been set to 29.92 inches of mercury (1013.2
millibars).
Pressure Altitude 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.
Station Pressure Actual atmospheric pressure at field
elevation.
Wind 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.
(c) Power Terminology
Takeoff Power Maximum power permissible for takeoff.
Maximum Maximum power permissible continuously
Continuous during flight.
Power
(d) Engine Instruments
EGT Gauge Exhaust Gas Temperature Gauge