Piper Aircraft Corporation Cherokee Arrow II, Руководство по эксплуатации

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SECTION II
PR(,)CEDURES
ARROW
A. SYSTEM OPERA TIO NS
I ·.
• •
·;
'.
I.
-: The: stall-warning system is inoperative with the master
·
swhch off.
2.
The electric fuel pump must be on ,for both landing and takeoff.
3.
Some aircraft are equipped with an airspeed - power sensing system (back-up gear
extender) which extends the landing gear under low airspeed - power conditions•
even though the pilot . may not have selected gear down. �is system will also prevent .
retraction of thcf mnding gear by normai m , eans when the airspeed - power values are
below a predetermined minimum. (See Item
5,
Procedures Section.) To override this
system or t(?
.•
hC?.ld the emergency
1
,ge� _ r , l�v,er in the
I
overnde n J. • P, - Pdsition without
main taini ng _ rrtaiu�al . pressure on th e1 �m . �!8e
.
n c y gea,r leve r , · pJJU-
.
t . be il
e'v cm Jull up and
push the latch ' p i n in. To release the override, pull lever up to disengage latch pin,
then release lever. For normal operation, the pilo� should extem.ir..ami r.e.tractrthe goar
with the gear selector swit ch
.
located on the instrument panel, just as he would
if
the
back-up , gear extender system .�er;e not ii:i.stalled. ., · • • ..
- :n·- ::.,·;-• Y:
. :-:·
:,1
. �
ri . . . .
\ _. ( .. J • ., ... - . . :- •
•Approximatel:)!
l , OS
.mph IAS
- at any ' al tt tude ; power ' off .' ' ··
J. ·
4. • l.4n4in$ g��
.
r p 9si t i on . i n
.
Q�cati o n a n d , w aming lights:
,:
1•,;; __ _.; '- • •
1
(a} . !be
.
.red .
·_
gear w�r: i:iiQ. g . Hgbt o n :
.
th e.
r
,i n stru m en t pane J
!
a-rt d ' : the - : hom operate
,' .
�im u ltan:�o�sJy w�cn:-
.:
•�-· :
!
. .- ..
, ,:. : .
. ·_
-.r.
,· .. :- =-�- .
··
(1)
In flight, when the throttle . is
·
1
r.ed uc. ed · to w h er:c .- the manifold pressure is
approximately 14 inches of mercury or below, �nd the gear select9r switch
is not in the down position.
1
\
(2) On aircraft equipped with the backup gear extender, when.&he system has
lowered the landing gear a . nd the , gear selector
.
s w i t ch is not • in the down
· .. ; ,< . . · .. ,
1
position and the
·
throttle is not full open. ., :,
. (3) �
On the gr9und, when the
.
master switch is on and. t h e-gea r:s ete , c : tc>:r � switch is
in _ the up
·
po�ition .
· ·,
1:�:::•)L .. ,.1,.
'' NOTE ,
··r
· ·,·
.
..
.
'• �
... q�� ,
��,ri -
.
�tiicb
:
a��11ot
_ ���p�d
.
�t� t� �
c�u� • g�ar
'. '
r
, ·:{i-'i
-�
'j:
· r _
�xteQdijr
1
a� : a diji t1 \'i na 1 wtti�fa s
taUed
· : wh1 &i« cu v � \ es ,
.
1 \'
. '
. : r
J J tll$mritirig
; :b'om �
.
- i M 3' 1Ig \
fr , �•. iH entver-
·
�
1
fla
l'
s 'l ife •✓ �
·
•,
· extended .- bey.ond the approach position ( I 00) and : ttie
·;
1
·
·-''.:
Iar:iding gear are not down and locked.
(b) · The three green
·
lights on the in-strurnent p�nel ope��e i il'}divi_dually
..
�
,
c-:ach
I
·
assooia teq ,gear
, .i's . - locked Ji,n lth�itxt�dea'
;,�moo.
I� .. :1-"'G
·�!
;-J :'m;
. "�
� . r -.
,.
-�. ·
�. l" -�- fw,· "',
1
(c) The yellow "In • Transit' � . light on tbe i�strume,it panel operates whenever ariy of
tbe thfiCe
·
geai:s J
·
s :
�t
J!!(;.;i�-the� �lly;i(�t�;cied .pc;>iiti:on� o,r il:!:e fully e?{tended
·.
and l�
_
ket�i;ti
, o,n.
N? · :-1
.
, 0 _ 1c,
·
:-'"i"��-Jl
.··
..
··: ;-·
..
':··. �-.
( d)
.
On aircraft eqhi�ed-wfttt � M ' titck'of � �t' · b � te n <i�(tlld )� ll�\ � / .. Auto Ext. Off"
light immediately below
.
the , gear selector switch flashes whertever the _ emergency
gear lever is in the full µp position.
F �A ·
APPROVED October 14, 1981
· -��l�ED:-·J�-.,. 31, 1917
N16422 POH