Piper ARCHER III - Page 100

SECTION 5
PERFORMANCE PA-28-181, ARCHER III
SECTION 5
PERFORMANCE PA-28-181, ARCHER III
REPORT: VB-1611 ISSUED: JULY 12, 1995
5-4 REVISED: APRIL 3, 1997
REPORT: VB-1611 ISSUED: JULY 12, 1995
5-4 REVISED: APRIL 3, 1997
(b) Takeoff and Landing
After determining the aircraft loading, all aspects of takeoff
and landing must be considered.
Conditions of 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 graph (Figure5-7 or 5-9) to
determine the barrier distance or (Figure5-11 or 5-13) to determine
the length of runway necessary for the takeoff.
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 example
flight have fallen well below the available runway lengths.
Departure Destination
Airport Airport
(1) Pressure Altitude 2000 ft. 2500 ft.
(2) Temperature 23°C 21°C
(3) Wind Component (Headwind) 8 Kt. 5 Kt.
(4) Runway Length Available 7000 ft. 4500 ft.
(5) Runway Required 1073 ft.* 820 ft.**
NOTE
The remainder of the performance charts used in
this flight plan 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 5-11 or 5-13
**reference Figure 5-37
(b) Takeoff and Landing
After determining the aircraft loading, all aspects of takeoff
and landing must be considered.
Conditions of 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 graph (Figure5-7 or 5-9) to
determine the barrier distance or (Figure5-11 or 5-13) to determine
the length of runway necessary for the takeoff.
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 example
flight have fallen well below the available runway lengths.
Departure Destination
Airport Airport
(1) Pressure Altitude 2000 ft. 2500 ft.
(2) Temperature 23°C 21°C
(3) Wind Component (Headwind) 8 Kt. 5 Kt.
(4) Runway Length Available 7000 ft. 4500 ft.
(5) Runway Required 1073 ft.* 820 ft.**
NOTE
The remainder of the performance charts used in
this flight plan 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 5-11 or 5-13
**reference Figure 5-37