Piper Turbo Saratoga PA-32-301T Pilot's Manual page 110

SECTION 5 PIPER AIRCRAFT CORPORATION
PERFORMANCE
PA-32-301T,
TURBO SARATOGA
(b)
Takeoff and Landing
I
Now that the
aircraft loading has been determined,
all aspects
of the takeoff
and
landing must be considered.
All of the existing conditions at the
departure
and destination
airport
must
be
acquired, evaluated
and maintained
throughout
the flight.
Apply the
departure
airport
conditions
and takeoff weight to
the appropriate Takeoff Performance
and Takeoff
Ground Roll
graph (Figures 5-7, 5-9, 5-11, 5-13, 5-15 and 5-17) to determine the
length of
runway
necessary
for the takeoff and or the barrier
distance.
The landing distance calculations
are performed in the same
manner
using the existing conditions at the destination
airport
and, when
established,
the landing weight.
The conditions
and calculations for the example flight
are
i
listed
below.
The takeoff and landing distances required for the
flight have fallen well below
the available
runway
lengths.
Departure
Destination
Airport Airport
(l)
Pressure
Altitude 1400 ft.
400 ft.
(2)
Temperature
15°C
24°
(3)
Wind Component 10 KTS 0 KTS
Headwind
(4)
Runway
Length Available 4000 ft. 4600 ft.
(5)
Takeoff
and Landing
Distance
Required
(3
Blade Propeller
and Standard Brakes)
1925 ft.* 1650 ft.**
*reference
Figure 5-7
**reference
Figure 5-41
REPORT:
VB-1070
ISSUED: JANUARY 10, 1980
5-4
REVISED: AUGUST 6, 1982