(�I' I•·--'
#
,
_
.
�
·
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.
J•
.
111:,r,
-
-
...
r.'
r.
,41
1
".i'/
'
.. �
STALLS
1 '
CRUISING
• _
L.
�:
! 1 � -- ; , , : ur �v.
t
,
•-
1
!
•. ,
·
..
.,...
"! n . , . \ ...
....
,.
. ...
;.,...,
·-�-
f,
lf:,. .• ·!
r;.
!...;..;: \C;--1;:t'.
,
h
;• •:
"-�--�-
I
--·�:..1.�·., .... ,
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
··,
,
;
,
;;.,
,.
•\
1
••
-.
,
1
1
·
,•r
r
"'
r
•
;
•
/
manua
.
.
.
,l,Jl.)�·�•;1q
s
mb:;,r
,'?I
_l.!'U:i
k
�-
':�f.l r;_. -�
!2
·"'--- ·•
r·
'
'•,
;;
•
;
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
Содержание Cherokee Arrow II
Страница 34: ...ARROW II OVERRIDE LATCH 2 4 Throttle Quadrant Console AIRPLANE AND SYSTEMS REVISED August 30 1973 N16422 POH...
Страница 37: ...AIRPLANE AND SYSTEMS ISSUED Novemoer 15 1971 Main Wheel Assembly ARROWil BRAKE HOUSING 2 7 N16422 POH...
Страница 47: ...AIRPLANE AND SYSTEMS ISSUED November 1s 1971 Static System ARROW IT 2 17 _ I N16422 POH...
Страница 52: ...ARROW II 2 22 THIS PAGE INTENTIONALLY LEFT BLANK AIRPLANE AND SYSTEMS ISSUED November 15 1971 N16422 POH...
Страница 100: ...ARROW TIDS PAGE INTENTIONALLY LEFT BLANK REPORT VB 334 PAGE S 30 MODEL PA 28R 200 l UED October 14 1971 N16422 POH...
Страница 112: ...ARROW II 6 8 THIS PAGE INTENTIONALLY LEFT BLANK OPERATING INSTRUCTIONS ISSUED November 15 1971 N16422 POH...
Страница 113: ...THJS PAGE INTENTIONALLY LEFT BLANK OPERATING INSTRUCTIONS ISSUED February 4 1972 ARROW 11 6 9 N16422 POH...
Страница 114: ...ARROWD 6 10 Tms PAGE INTENTIONALLY LEFT BLANK OPERATING INSTRUCTIONS ISSUED February 4 1972 N16422 POH...
Страница 138: ...ARROW II 9 10 THIS PAGE INTENTIONALLY LEFT BLANK a I l j I HANDLING AND SERVICING ISSUED November 15 1971 u J N16422 POH...