Fuel, Time And Distance To Descend - Piper Dakota PA-28-236 Pilot Operating Handbook

PA-28-236
FUEL, TIME AND DISTANCE TO DESCEND
137 KIAS, 2400 RPM, THROTTLE
AS REQUIRED FOR 1000 FPM
~OOO RATE OF DESCENT NO WIND
$
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10 000
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" ALl" FT,
800 0 PRESS . .
,
Example:
Cruise pressure altitudE
~
Cruise outside air temp
0
Landing pressure altitu,
6000 .....
Landing outside air tern
~ '
,
,
Descent distance: 20 -~
:0
Descent time; 8 -2 6
Descent fuel: 2 -.5 1.
4000
,
,
t
.,
2000
-
~ , ,
,
'
,
,
-40 -20 0 20 40
OUTSIDE AIR TEMPERATURE - °C
o
10 20 30 40
TIME DISTANCE AND FUEL TO DESCEND
8000 ft.
12°C
e: 1800 ft.
.: 31°C
5
=
15.5 NM
min.
gal.