Piper WARRIOR III PA-28-161, Руководство по эксплуатации для пилотов

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SECTION 1 PIPER AIRCRAFT CORPORATION
GENERAL PA-28-161, WARRIOR III
SECTION 1 PIPER AIRCRAFT CORPORATION
GENERAL PA-28-161, WARRIOR III
REPORT: VB-1565 ISSUED: DECEMBER 08, 1995
1-6
REPORT: VB-1565 ISSUED: DECEMBER 08, 1995
1-6
V
NE
/M
NE
Ne v e r E x c e e d S p e e d o r M a c h
N u m b e r i s t h e s p e e d l i m i t t h a t
should not be exceeded at any time.
V
NO
Maximum Structural Cruising Speed is the
speed that should not be exceeded except
in smooth air and then only with caution.
V
S
Stalling Speed or the minimum steady
flight speed at which the airplane is
controllable.
V
SO
Stalling Speed or the minimum steady
flight speed at which the airplane is
controllable in the landing configuration.
V
X
Best Angle-of-Climb Speed is the airspeed
which delivers the greatest gain of altitude
in the shortest possible horizontal distance.
V
Y
Best Rate-of-Climb Speed is the airspeed
which delivers the greatest gain in altitude
in the shortest possible time.
(b) Meteorological Terminology
ISA International Standard Atmosphere in
which: The air is a dry perfect gas; The
temperature at sea level is 15 Celsius (59
Fahrenheit); The pressure at sea level is
29.92 inches Hg (1013.2 mb); The tempera-
ture gradient from sea level to the altitude
at whic h t h e t e m p e r a t u r e i s - 5 6 . 5 C
( - 6 9 .7F) is -0.00198C (-0.003564F) per
foot and zero above that altitude.
OAT Outside Air Temperature is the free air
static temperature obtained either from
inflight temperature indications or ground
meteorological sources, adjusted for in-
strument error and compressibility effects.
V
NE
/M
NE
Ne v e r E x c e e d S p e e d o r M a c h
N u m b e r i s t h e s p e e d l i m i t t h a t
should not be exceeded at any time.
V
NO
Maximum Structural Cruising Speed is the
speed that should not be exceeded except
in smooth air and then only with caution.
V
S
Stalling Speed or the minimum steady
flight speed at which the airplane is
controllable.
V
SO
Stalling Speed or the minimum steady
flight speed at which the airplane is
controllable in the landing configuration.
V
X
Best Angle-of-Climb Speed is the airspeed
which delivers the greatest gain of altitude
in the shortest possible horizontal distance.
V
Y
Best Rate-of-Climb Speed is the airspeed
which delivers the greatest gain in altitude
in the shortest possible time.
(b) Meteorological Terminology
ISA International Standard Atmosphere in
which: The air is a dry perfect gas; The
temperature at sea level is 15 Celsius (59
Fahrenheit); The pressure at sea level is
29.92 inches Hg (1013.2 mb); The tempera-
ture gradient from sea level to the altitude
at whic h t h e t e m p e r a t u r e i s - 5 6 . 5 C
( - 6 9 .7F) is -0.00198C (-0.003564F) per
foot and zero above that altitude.
OAT Outside Air Temperature is the free air
static temperature obtained either from
inflight temperature indications or ground
meteorological sources, adjusted for in-
strument error and compressibility effects.