Nose Gear Push-Pull Control Rod Removal; Main Landing Gear Push-Pull Control Cables Removal - Piper PA-24 Comanche Service Manual

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PIPER COMANCHE SERVICE MANUAL
c.
Actach the rmse:tioD
SPrinl
(22 or 23)
to
the craalllLilliClD IIld adiu. the coaer pin
bftWCICD
the
sprinl aDd
floorboard co
maiIltaiD
coup tcnsioa on the
sprm,
to
bold the 1hnsmj.IioQ away from the
mncrion torque tubc durinl cJIIG'I'l'Dcy
par
ateasioa.
d. Lllbricare me torque
anD
mroupa bolt (13) aDd book the tn"""issjoD tv.be
(19)
0ftT
me bah.
e. Place the
ancqascy
rdeuc baDdle (18) in the dowa
aad
locked poIitioQ.lock.iaI the tnD. .jaiOD
Nbc uound the throup bolt.
f.
CODDee:t the decaica1 leads
aDd tUde
the prouccite
c:owriaI
O¥a'
the termiDalI aDd
tic at both
ends.
I.
Check
for properopention uad adjust. (Refer
to
panpoapb
~'4.)
6-46. Ranoval
Of
No. Ge.r
P1IIb~
CoD1I'01 Rod. (Refer
to
Fipre 6-14.)
a. Place the airplane aDjada. (Refer
to
JackiDI.
Secr:ion 11.)
b. Remove carpet
aftI.ChiDI screws
aDd
roU
it buk off
the
frODt CCIlter
accaI
panel.
c. Remove
froDt CCDtG' acCCII panel
by
removiDl
aaachinI
SCftWS.
On
airplanes with Serial
Nos.
24-4783. 140-4804 and
up.
remove the rcmction mD-.oD
ac~
door
locued
benn:cD the cwo front
scatS.
d.
DiscoDDCCt
the crusmission by
pu1liq up aD the rei_
leva'.
e. Rem.ct the
landinc
aar
IlDtil it banp
in the
Dean
poIition. by .... the ClDCfPDCY au_on
lever.
f. Disconnect
the
push-pull
rod
(11) from the UDdenide of the left IOrque arm
(9)
by
ranoviaa
the
cotter
pin. wuber
and
pin.
,.
Disconnect the forward CDd of the rod
at
the left
dni
Uak
located in the
DOIC
~
wbeel
weI1
by
removing nuc. washer aDd bolt. Rctn.ct
the
FU moucb
to
allow
removal of
the
arw:binl
bolt
throup
provided hole ill the
Dose
section
dwlncl.
h.
Remove the rod by rcmoviDJ CIId
bariDt
aDd
pulliDl
it
tbtoap ...
aDd
DOle
~
wbeel well.
6.... 7. Removal Of
MaiD
Landi'nI
Gar PuIM'uI CoBuol CIbJa. (Rda'to Fipft 6-14.)
a, Place the airplane on
jacks.
(Refer to
JackiDI.
Section II.)
b. Remove
carpet
aaachq
screws
and roU c:.upct back off the front cauer access panel.
c.
On airplanes with Serial Nos. 24-4783. 1.....04 &adup.
tanCWC
the
recractiOft
mnsmission acccsa
door located between the two front
scats.
d. Remove
the
rear scacs and
carpet
attaehiDIscrews.
e. Roll the
cu:pet
back aDd remove floor
panel jut 1ft of
the mraction tnmIIlisllon.
f. Disconnect thc mnani_ion by pulJiq up on the re1cue Incr.
I· Retract the landin,
,eat
until it banp in cbc Della potiIion. by
usiDI
the emeqcncy extension
lever.
h.
Disconnect the mraction cables (7 aDd 8) from the torque arms (9 aDd 10) by removinc attac:hiDc
cotter pins. wuhen aDd pins.
i.
Remove castle
ftUts
(3
&ad 4) from cables
It
the bulkhad aft of the
m:ractiOft
tra.nIIIlisIion.
J.
Remove damps scc:uriq cables
to
bottom of the
fuIclate.
k.
Enter throUJh the wbed well and disconnect cable ends from upper maiD gear drag
links by
removing attaching nut. _uhen aDd bola.
LANDING GEAR AND BRAKE SYSTEM
REVISED:
6/25na
IJ13