NOTE:
1.
GROUND ROLL DISTANCE
IS
20% OF TAKE·OFF DISTANCE OVER 50·FT OBSTACLE.
2.
DISTANCES
ASSUME
AN ENGINE FAILURE AT
lIFT·OFF
AND PROPELLER
IMMEDIATELY FEATHERED.
3.
WEIGHTS
IN
SHADED
AREA
MAY
NOT
PROV.IDE
POSITIVE
ONE.ENGINE·INOPERATIVE CLIMB. REFER
TO
TAKE-OFF WEIGHT GRAPH FOR
MAXIMUM WEIGHT AT WHICH THE ACCELERATE·GO PROCEDURE SHOULD
BE
ATIEMPTED.
ASSOCIATED CONDITIONS:
POWER TAKE·OFF POWER
AT
2700
RPM.
SET BEFORE BRAKE RELEASE.
FLAPS up"- --------------- -
--
-
LANDING GEAR RETRACT AFTER lIFT·OFF.
RUNWAy PAVED,
LEVel,
DRY SURFACE.
COWL FLAPS OPEN
MIXTURE FULL RICH (ABOVE 5000
FT,
SET TO
7S:100"F
ON
RICH SIDE
OF
PEAK EGT)
em
c m
om
f£
(IJ 0
~~
:!J
~
6000
1§
tu
.':::t
wi!
~
z
7000 I
:J
w
~
(J
ffi
(J
;:
a:
6000
13
~
~
w
0
a:
'fi;.
~
5000
a:
~
0
w
(J
4000
~
!i1
0
LL
~
:iOOOq
w
~~
~
3 .
2000
I» 0
0
10
20
30
~
~
WIND COMPONENT
- KNOTS
EXAMPLE:
OAT
15"C
PRESSURE ALTITUDE SL
TAKE·OFF WEIGHT 3350
LBS
HEADWIND COMPONENT
10
KTS
TOTAL DISTANCE OVER
50·FTOBSTACLE 4700 FT
GROU~D-ROLL
: _940
FT
36003200 3400 3600
WEIGHT - POUNDS
TAKE·OFF SPEEDS
(ALL WEIGHTS)
lIFT·OFF
71
KNOTS
50
FT
90
KNOTS
W
3000
Wmfj"
~-
W
.~
W
a:
ACCELERATE-GO
DISTANCE
,s"-
;S\,:
11
'/-@
i
-30
-20
-10
0
10
20
30
40
50
60
OUTSIDE AIR TEMPERATURE
-
"c
~
.~~Q~
~
1f1?\
!-\
r..'i>~
i<-~.
,?,?-'<-'"
~'"
~
f
~
~
..Jl>
~
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