Arrow PA-28R-201 Pilot's Operating Handbook And Faa Approved Airplane Flight Manual page 92

SECTIONS
PERFORMANCE
PIPER AIRCRAFT CORPORATION
PA·28R·201, ARROW
5.5 FLIGHT PLANNING EXAMPLE (continued)
(b) Takeoff and Landing
Now that the airplane loading has been determined, all
aspects of the takeoff and landing must now 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 5-9, 5-11, 5-13 and 5-15) 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 (
listed below. The takeoff and landing distances required for the
flight have fallen well below the available runway lengths.
Departure
Airport
(1) Pressure Altitude 1900 ft.
(2) Temperature 20
0
e
(3) Wind Component 4KTS
(4) Runway Length Available 3000 ft.
(5) Runway Required 2550 ft.*
NOTE
The remainder of the performance charts used
in this flight planning example assume a no
wind condition. The effect of winds aloft must
be considered by the pilot when computing
climb, cruise and descent performance.
*reference Figure 5-13
**reference Figure 5-39
Destination
Airport
1900 ft.
20°C
2KTS
4600 ft.
1490 ft.**
REPORT: VB·1365
5·4
ISSUED: SEPTEMBER 15, 1988
(