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Piper PA-24-250 Comanche User Manual

Piper PA-24-250 Comanche
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Aircran Publications
Piper Comanche
250
(Early Model)
TAKEOFF PERFOkMANCE
PA-24-250
*
2800
LBS GROSS WEIGHT
Takeoff Ground Run and Total Distance Over a
50
fi
Obstacle
(1 8
Degrees of Flap)
Runway conditions: paved, level, dry.
Weight
Ibs
2500
2800
2500
2800
2500
2800
2500
2800
2500
2800
2500
2800
2500
2800
2500
2800
2500
2800
Pressure Temperature Ground Run
Altitude ~eg
FIC
Sea Level
40105
Sea Level
40105
Sea Level
60115
Sea Level
60115
Sea Level
80127
Sea Level
80127
At Wind Velocity
0
mph
10
mph
20
mph
Section
-
5
Performance
Total Distance
At Wind Velocity
0
mph
10
mph
20
mph
1150 900 800
1450 1165 915
1275 1000 825
1575 1265 995
1400 1100 850
1700 1365 1075
Example shown
in
bold
type:
Airplane weight
=
2800
lbs
*
Airport altitude
=
2000
ft
*
Air temperature
=
70
degrees F or
21
degrees
C
*
Headwind component
=
10
mph.
Takeoff ground run distance
=
1020
ft.
Total distance over
50
ft
obstacle
=
1590
ft.
,
,
Also see Takeoff Performance chart. (Figure
5-08)
I\
\_
Figure
5-01
Copyright:
1993
Page
5-5

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Piper PA-24-250 Comanche Specifications

General IconGeneral
BrandPiper
ModelPA-24-250 Comanche
CategoryAircrafts
LanguageEnglish

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