Normal Short Field Ground Roll Distance- No Obstacle - Piper CHEROKEE WARRIOR II Information Manual

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PIPER AIRCRAFT CORPORATION
PA-28-161, CHEROKEE WARRIOR
II
SECTION 5
PERFORMANCE
PA-28-161
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40
80
OF
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-20
0
20
oc
2325
2200
2000
1800
1600
0
5
10
15
WIND-KTS.
WEIGHT-LBS.
OUTSIDE AIR TEMP.
Example:
Departure
airport pressure altitude:
1500
ft.
Departure airport temperature:
80°
F
Weight:
2325
lbs.
Wind: 15 KTS
headwind
Ground roll: 1150 ft.
Lift-off
speed: 50
KIAS
NORMAL SHORT FIELD GROUND ROLL DISTANCE- NO OBSTACLE
Figure 5-5
2400
2 2 00
2000
18 0 0
1600
l--
L.i...
1400
....J
....J
0
12
oo-
c::
Cl
:z:
'1000
=
0
c:::
c.::I
800
L.i...
L.i...
0
600
1..1..J
::>e::
<
l--
400
200
ISSUED: DECEMBER16, 1976
REVISED: JULI 11, 1977
REPORT: VB-880
5-13

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