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ARROW II
Soft Field, No Obstacle:
Proc
e
ed as abov
e
aft
e
r gear r
e
traction, continue climb at b
e
st rat
e
of climb spe
e
d. 100 MPH.
and slowly r
e
tract th
e
flaps.
•If d
e
sired on th
e
aircraft equipped with th
e
backup g
e
ar extend
e
r, th
e
ov
e
rride up posh�on
can b
e
selected and latched before take-off. and the gear will then retract as soon as the gear
selector switch is pla�edjn the up position. ln this cas
e
care should b
e
taken not to retract th
e
gear
pr
e
maturely, or the afrcr
'
aft
'
could settl
e
back onto the runway. If the override lock is used for take
off, it should b
e
disengaged as soon as suffici
e
nt t
e
rrain clearance is obtained, to return th
e
g
e
ar
syst
e
m to normal operation,
CLIMB
Th
e
best rate o(climb at gross w
e
ight will b
e
obtained at
9S
MPH with g
e
ar down and 100
MPH with g
e
ar up. The b
e
st angl
e
of climb may b
e
obtained at 8S MPH with g
e
ar down and 96
MPH with
gear
up. For climbing
e
n route cf.'Spee.d of I
to
MPH is r
e
com�end
e
d. This will produce
bett
e
r forward spe
e
d and increase visibility over th
e
nose during the climb, with little sacrifice in
rate of climb.
?
Air
,
f?rt1>
.
tif>
:
Pfif J.9
.
,Y
:.
!'e- t��
�
JllQJ\
;
-f-t�r: .all pbstacics
·
.
ha
Y
e
.
bee
:n cleared.
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-
...
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r.
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STALLS
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CRUISING
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h
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Angle of Bank
,,
0
1('.,
.
11".:
•
.
' ill:,
I
I
'1,.
,.
I
•
..
;,
Of
The cruising sp
ee
d of the Ch
e
rok
e
e Arrow lI is
,
d
e
t
e
rm\Il
e
J'b!(Jna'nY fa-�oi- ,
t
nc-luding
'
pow
e
r
setting, altitude, temJ>.en�� l<?adi.ng, �9�
.:.
;Wr»�Qt
,
ri
nsitallech.p.n
t
ttJ�
:
Yai�ne'
.
Th
e
normal
ciuisi�g l'OW�r
-
�s
1S%
bhli
e
'raied
�OfSCiJ�'IY
,
e
�
gf \he��gi1'1;;,,]01e:a�
,,
�11,�
�fbe
obtaine�
at vanous altitudes
·
and
,
powcr settings
can be
.
dct,c.m\11�cd ( ram th
e
.
c�rt� ,iq s"-ec�100 XI
,
lI of this
l
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r
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manua
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When selecting
RPJ.{ below
·
2400, Jimiting f!Ul.nifpJd.prcss1,ire. fQr contin�o1:15 operation, as
specified by the
.
Lycortling pperator's Manual, should b
e
obscrv
e
a.
·
To INCREASE power, first increas
e
RPM (pr-0peller
.
controi); then increase manifold
pressure (throttl
e
control).
_
To DECREASE power, first decreas
e
manifold pr
e
ssure (throttle): th
e
n decrease RPM
(propell
e
r cQntrol).
N16422 POH
