The Partia1 Revision for Addition of FA-200 New vHF COMM/NAV Unit and Magnetos
Since design change for addition of new VCO/NAV InitP/N: KX-155 Honeyie11
and Magneios P/N: 4347 4370 and 4373 Slickhad arovahf JCAB N0.20-14-A3July
172009N0.22-10-A4 0uly 17 2009N0.20-14-A4January 13 20and N0.22-10-A5
January 13 20101FA-200 SeTvice Manual and Parts Catalogue has been lodified Error
correcliols are inchldedjso we wiH ilfaTm you of lhe lodified contents
We attached Servjce Maal anj Parts Catalogue separately.Please replace the
corresponding pages according to the fojHowingJDints.

320-8564TEL028(684)7253FA(028(684)7260
PAGE 21 38
PAGE 39 60
PAGE 61 74
Fig.N0
1-5
sTALLEDtEFr DuRINQ ACROBλΥlc FUGHT.
2DO N07 KsEP INvERTED AΥΥΓnJDEllNvSRTEDn;IG1Tls
PROHIBITED.ACROBATICCATEGORTMAX WEIGHT72 LBS.
MANEUVERSs ENTRY SPEEDI
STALLSXCEPTWHIP STALL SLOW DECELtRAT10N
LOO . 15S MPH 13S XNOTS
CUBAN EIGHT ISS MPH 135 KNO7S
IMMELMANN 7uRN ls5 MPH !a5XNOTs
CLOVER LEAF .’ 15MPH135KNOTS
BARREL ROLL 130 MPH U3KNOTS
SNAP ROLL 100 MPH’87 XNOTS
.wlNG OVgR ‘ 120 MPH 104 KNOTS
BAMMER gEAD sTALL 120 MPH 104 KNOTS
SNNSFLAP UP £NGINEIDLE SLOW DECELERATION
UTIL17Y CATECORY MAX. W£IGH7 2425 LBS.
ACROSATIC MANEUVERS ARE LIMITEDTOTE FOLLOWING.
STALLEXCEPT WHIP STALLSTESPTURli.LAZY EIGHT
CHANDELLE4 SPlNSFLAP UP ENCINE IDL ‘
’
D
FA200460
Decll λIRSPEED INDICATOR MARKING ARE MARXED
FOR NORMAL OR UTXLITy CA?EGORY. FOR ACROBATIC CATEGORY SEE 711E APPROVED
AIRPLAlgE FLIGH MANUAL.
l
TH£DSSIGN MANEUVERING SPE£D ’ NORMAL AND UTIUTy CATEGORY 134 MPH u6KNOT ’.ACROBATIC CATEGORT 148 MPH 129 KNOT THEIMOgSTRATED CROSS WIND 15 KNOTS
FA200-1
Decal THEESIGN MANEUVERING SPEED
NOIMAL AND UTIUTTCATEGORY 143 MPR 124 XNOT ACltOBATIC CATliGORy !54 MPI134KNOT.
THE DEMONSRATED CROSS WD 15 KNOTS
TABLE I-5 PLACARDS ON INSTRUMENT'PANEL AND ADJACENT AREAS{2/4}
ISS11D : IAlali 2a10 148
Letter Slze

ΥΥ

11 Bo



TABLE I-5 PLACARDS ON INSTRUMENT PANEL AND ADJACET ARIEAS(3/4)
114
41 DESCRIPTION
EA-200-160 is powered by anAvco Lycoming model O320-D2A, 160 HP and FA-200-180 is powered by
anAvcoljycoming model IO360BIB180 HP.
Both engines are air cooled,horizontalopposed 4 cyhnder, direct driven, wet sump engines.
TheratedpowerofO-320D2Ais 160 HP/2,700 rpm and that ofIO360-BIB is 180 HP/2,700 rpm.
The cylinders are numbered as f1)nows:R/H fiont cynnder…N0.1L/H£ront cyhnder…N0.2R/H
rearcynnder…N0.3,andLSrear cylinder…N0.4,designated based on the order of connecting rods;
The engine data are shown in para. 4-2.Per11}rm engine checks rerring to Chapter 3, Periodic Check
Table,Major repah and overhaul of enginesshall be carried out hl accordance with Overhaul Manual
(P/N 60294-7)issuedbyAvcoLycoming
43 ENGINli cowLING (SEE FIG.4)
Tne engixle cowlhlg comists of.the upper cowling and lower cowling. The upper cowlins is provjded
with laige access doors on both L/H d R/H sides which can be opened or closed without any
toolsjfacmtathroutine oilservicingand inspeciion of acceories.
-
necowlhlg is removed by loosening the cowling fastenersand removing the nose cap joint
screws and fifewan attachscrews. Before removing the lower cowlingremove 2 hoses.between the
cowling and heat exchanger, fuel pump coolinghose and hose;for the engine cowling airintake.
4-3-2 1NS17XLLAI'|ON OF ENGINECOWLING
I When thg cowling is instanedbe sure to installthe hoses removed. Bend the sealingof the bafnes in
l such a direction(inwds)that airaround the enline cal now correcily.Ilsta!1ationis accomplished
inthe feversed ordef of the removal procedules.. . .
4-33 CLEANING AND INSPECTION OF ENGINE COWLING
Clelan the inside of the cowling with cloth moistesd with cleanser (FedetaI Spedfication P-S-661o
equivalent.lf.the inside is found smeared with onj etc.spray.cleanser on it,leave it a whne as jtiss
wash it with soapy water to remove aU foreign nlattels and wipe off soapy water with dry cloth. As
lfor the pajnted suffllce of the cowljng clean it with.neutral cleansers wash it away wjth a plenty of
watefd wax it aft.irwashing to extend the durabmty of the pajJ11ed surface. After washing check
the cowlifof delts, cracks and looΣivets.
RepaiΣall defbcts discovered so that propagation of such defects to other portions can be prevented.
4-34 REPAIR OF E:NGINE COWLING
ln case.the cowliskin is damaged excessivelysreplace it wililnew one. ln case of small cracks
da gtop hols aldsman dents can be comcted by hammexifrom inside.

4152 HARNESSASSEMBLy
The ignition harness consistsof 4 nexible shielded high tension lead wires. 0ne hamess is connected
to the L/H magneto L/H upper and R/H lower oneswhile the other harness is connected to the R/H
harness,R/H upper and L/H lower spark plugs. Check the harness assembly as 11)11ows:
(1)Checke lead wires lbr nicks, cuts or wear.
(2)Check the spark plug sleeves for scratches and damage. Check the coupling nuts for damaged
thread.Check the compression spring for deteriorated tension and damage. Check the grommets fbr
damage. Check allattach brackets and clamps for security
(3)Checke conductiviof the lead wires.lfany wire is fotmd non-conductivethe wire is cut
somewhere.Replace such a wire.
(4)Thescopeofminorrepairoftheharnessassemblyislimitedtothereplacementofthecontact
springspring retainer assemblz insulating sleeve or a single lead wire. Such replacement can be
accompnshed while itis instaned on the engine.
415,3 MAGNETO
O-320 series enne is equipped wthe magnetos 84LN21(L/H)and S4LN20(R/H)or Slick 4373
(L/H)and Snck 4370 (R/H)and IO-360 series engine is equipped with the magnetos S4LN-200(L/H)
and S4LN204(R/H)or Shck 4347 (L/H)an(I Skk 4370 CR/H)in the aft portion of the accessory
section.Each of these magnetos has a magnet with 2 poles rotating at the engine speed. The magneto
is designed to generate high voltage which enables the spark plugs to emit sparks in the cynnder to
ignite the mixture gas
Per)rm maintenance and inspection refer to L-1363C 4300/6000 Series Magneto
Maintenance and overhaul Manual issued by unison lndustries. BothljH and
R/H Magneto should use the same manufacturer.
4-154 1MEAINTENANCEANDINSPECTIONOFIVAGNETO
(1)At every periodic check, check the contact points of the breaker assembly for excessive wear and
burn.Replace the points with deep cavity or excessive burn. Check if the cam feltis properly
lubricated.ln case point polishing is considered necessary smooth them with hard nishing
sandpaper.Cleantheinsideofthebreakercompartmentwithcleancloth.
(2)ln case the engine has failed due to a cause associated with the ignition system, check the spark
plugs and wiring nrst bef1)rechecking the magnetos. Send the intemany fjled magnetos to the
overhaul shop 11)rrepair and tests.
(3)visuany inspect the system to determine thecauseofthe failure
a.With the hamess outletplate removed om the magneto check the grommet and high
tension section of the distributx)rblock fbr moisture. lf moisture is found presentwipe it of nghtly
with soft,drynnt.
CAUTION
Do not use gasoline or any other solvent to clean the distributor block.
Removalofthe wax coat results in electrical short-circuit.
ISSUED : JANI!ARY 2010
b.WiththebreakercoverremovedcheckifthecamfonoweriSinpositiyacgnt.act with thg spg.
Check.also if the screws have attached the breakef paftsin placositively.Qleck the contact pohlts
for excessiveweaf and bunl,.. .
Discard the points wideep pitsoi excessivebum.
Normal point is
of paint wear
V111 dafied und
- - -
Do lnot poUsh e contact point iuifiicel iiith whetstone.A
pohlt with Ut rougjiiless may be dedai itis. ln ease the
point has excessivi wgai or ixTegular Uilevemlessjorcaie lt
haS been lOOSened rep1Ce the COlmplete brelakeΣ‘.I ‘
,.c. Chgck jf the cam follower feltis !ubiicated properly..HOlde lelt between the .thumbdthe
forefinger. lf oiliness Qan not feltsupply a.fbw dJops of S4E 60 (Scinta1086527)ontoit. lt
takeS approximately 30 min for the felt tO abSOrbltlii on COmplletely.¨Wipe off the exaSiVe OU With
dry cloth. Excessive oilif left unattened may cause malfunctioninof the contact point or liea
bum.
d. Check the capacitor moullt bracket for lcracks and looseness. Check the capacity of the capac-
tof with a tester or equkalent equjpment The capadty shaU be at least.0.30 microfirad.
422
14-2-1
14-2-2
14-2-3
KX-160 0PERAIrING PROCEDURES
14-1
14-2-7 INSTALLATIONANDREMOVALOFMAR-6Y
14,2-14
14,2,15
14-2-16
14-2-17
14-3-1
14-2-9 ARC522A(iJ)(Altc-5a2A(;1))OPERA'rING PROCEDURES 14-9
14-2-10 1NsTALLA'rloNAND REMovAL OFARc-522Ag)CARc-632A)) 1410

COISIPOSITION AND PERFORMANCE OF KX-175 14-12A
1412B
142-19 1NSTALLArIONAND REMOVAL OF KX-155
14-2-20 TROUBLESHOOTINGOFAIRCOMMUNICA'rlONEQUIPMENT 14-13
KX-160 0PERATING PROCEDUI!ES
INS?ALLAIrlON AND REMOiLOFKX-160
1NSIALLA'rlONAND REMOiL OFARC522A(J)(ARC-542A(J))14-20
COIMIPOSITION AND PERFORIMIANCE OF KX-170
SERVICE XEWS 200-020
14-8-10 1NSrlALLAIrlON AND REMOMAL OF KX-170
14-3-11 COMPOSITIONAND PERFORMANCE OF KX175
14812 KX-176 0PERATING PROCEDURES
14-a18 1NSIALLAIrION AND REMOilAL OF KX175
14-314 COM:POSITION AND PERFORMANCE OF KX-155
14315 KX-165 0PERATING PROCEDURES
14-816 1NSIAILArlONANDREMOilALOFKX156
14-4 ADFRA:DIO NjWIGAIrlON EQUIPMENT

INSIALLAIrlONAND REMOVAL OF KR80
COMFOSITIONAND PERFORMANCE OF KR-85
14-4-8 COMPOSITIONANDPERFORISIANCEOFARC-824A
144-10 1NSIALLAIrlONANDREMOVALOFAllC-824A
1480
1NSIALLAIrIONANDREMOVALOFINTERCOMEQUIPMENT 1491
ISSSI:IAA2010

(1)Composition
Ahtenna Microphone
6 dB drop width 8.1KHzorless
60dBop width 20.0KHzorless 100mWat500Ωload
Speaker 4W at 4Ωload
From 5μv to 20,000μv audio output wm not vary more
than3dB.
3

(2)Rotate the controlswitch knob (1)ofthe£rontpanelofthereceiverclockwiseto“ON".
(3)Adjust the knob (2)so that the frequency indication window (3)win show a desired£requency.
Keep the vOL knob (1)at a proper posmon.
(4)Communicate with thecontroltowerand adjust the knob (D to a proper sound level.Forthe
transmission of messages,takethehandmicrophoneoffthequadlantandpressthepushbuttonofthe
)rreception of extremely feeble signal.
(7)Afteruse,turnthepowersupplyoftheradioequipmentbyrotatingthecontrolswitd(1)to
“OFF".
procedules as KX170 are appncable.)
(2)Removal of antenna (CI 121)
a. Disconnectthe coaxial cable terminal at the antenna connection.
b.Loosen the four antenna mounting nuts and puU out the antenna 5om the mounting hole
outside the body For the installation of the transmitter-receiverproper and antenna reverse the
removal procedures.
142-20 TROUBLESHOOTING OFAIR COMMUNICAIION EQUIPMENT
Trouble
(2)BumtfUse.
(2)lnadeguaze.squelch
adiustment
and conect ifnecessazy
colltained in radio equipment)
coiiect
I j- (1)Check and replaca.
(2)Check ald comct.
(3)Chea and repalr
cogect
’?
14-3-I GENERAL
T11e VOR Xlavigation equipment is used to ny e aircraft in a desired direction, measurithe bearing
of the aircraft. The operatjng frequency iange is from 108 MHz to 117.95 MHz. lt indicates the
VOR.bearinlon thle indicator receivka different phase radio wave with.respect to each masnetic
bearing transmitted from a ground station.
The vORequipment proper used in the FA-200 is one with the vHF ajr communication equjpment
proper. The operating frequency sound vohme and other conols andprovided on the front panel
of the equipment proper. The vOR indicator or course indicator in another nanlel is located ol the
.leftlinStmment pane1.
For homins accordhlg to reception from the VOR station, set a desired VOR angle ol the angle settiηg
indow of tlie indieator alld ny the aircraft in such a way that the vertical pointer wm stay the in
center of the indicator.
lf the aircraft deilafes to the right fiom the.couzse the pointer shifts to the left. lfitdiatestthe
‘left fiom the course the poijlter ifts to the rjght. .
Theindicatorhas “TO”,“FROM’l and “OFF” marks. The‘rO”and “FROM”marksindicatewhether
the aircraft isheadiilg to the VOR statiol or parting fiom the sjon.The“OFF”majndiqates
reception.
The VOR indicator has two angles where the vertjcal pointer comes to the center. The difference
between the angles is 180°.
Fig. 14-6 is lm explanatory drawinS
Sll5pose that ihe aircraft is nyingtat the p.ohlt ARg.14-6.The pointer of.the iildicator c6mes to
the center at two angles, 30 “FROM” and 210° “TO”.
At the point A, tllese two indicat19×ls are presented regardless of the dkection of the ajrcraft.
To detemline wheth.er the aircraft is headhlg tooi paffing from the vOR.station,watch the standby
compass and judse from its indicatioxl.lf the standby compass indication js around 30° and the vOR
illdication 30°“FROM” it fo11Qws that the aifcraft js parting from the “VOR” station. lftheVOR
indication is 2 10°“TO”.jt fbUows that the aircraft is he.ading to the VOR station. .
lfthestandbycompassindicationisaiound210°reversejseca.
The use of the vOR navigatjon equipment offels the advstage of mght almost strajght to the VOR
station regardless of the attitude of the aircraft which may challge lndereeffectsofwindalldothers.
The VOR antenna js located at the end of the vertilcal stabmzef.
1414
14-312 KX-175 0PERATING PROCEDURES
(1)Turn on Master Switcb located on the lower pcrtion of tlleinstrument panal.
(2)Place selectnr switcllknob (1)'on tllereceiver lront panel in IDENT or VOICE psltln and set
to ON.
(3)Select tllefrequenay of a desired VOR station in frequency window (3)by turning two eoncentric
lgnobs(2).Turn ljlelarger knob fr MHz slectionand tllesmaller onQ fr KEz salatinH
(4)Adjust VOL Knob (4)to obtain a proper s6und leve1.
(5),Set s‘elac.!x,rswitcllk(1)to IDENT psitinand check fr the dasidvOR tin.After
confirmtionsettllelknob to vOICE position.
(6)Sat t}lelaesired lrection just under tlletop inaicator indax (5)by turnjOBS knol3 (6)
(7)Mainlaining a cnteredaevidn neeale wlll prviae homlng.
(8)Aftrusset thseletf switcb t0FF.posltion.


(1),Refer to para 14-3-10 fbrinstahtion and removal ofvOR receiver proper (KX-175),VOR
indicator CKI-201B)and antenna (OD-2).(The same proced2es as KX170 are appUcable.)
14-314 COMPOSITION AND PERFORMANCE OF KX155
(1)Composition
Antenna
60 dB drop width 31.5 KHzorless
100mWat500Ωload
Fyom 5μv to 20,000μv audio output wnl not vary more
than 3 dB. °
(1)Setthe“MASTER"switchlocatedonthelowerpaneloftheinstrumentpanelto“ON".
(2)Rotate the knob (1)ofthe front panel ofthe receiver clockwise to“ON".
(3)Adjust the knob (2)so that the frequency indication window (3)win show the frequency of a
desired vOR station.
(4)Adjust the vOL knob (4)ta proper sound level.
(5)Pull the knob (4)to“IDEN' and check that the desired vOR station has been selected.After
conrmingit,push the knob (4)to“VOICE".
(6)Select a desired vOR angle on the vOR angle setting window (5)of the indicator by turning the
OBS knob (6).
(7)For homing, ny the aircrtin such a way that the vOR pointer win stay in the center of the
indicator.
1422B




FUJI FA-200 SERVICE MANUAL
(1)Rer to para 14-3-10 fbr instanation and removal of the vOR receiver proper (KX155)the
vOR indicator (KI-208)and the antenna (OD-2).(The same procedures as KX170 are
applicable.)
Ttouble
but‘!OFF!slmkonndic
.equipmentl
j tJ
|
FIIG11!rSOEn∃E!ID.ACBAIIC CASxl011
MAliJVIRS2 ENTRy sPEn)z
cEsDnlJ 135(11? XNos) IAZy ll(IE 135 MS(11?SOIS) S!ZP SIN 135 M(117SOS) .SiAIZ(Clpi WlpAj) SM)Wmx31RAI!I lz10P i55ME(135 SOIS)
gBAN trG!! 155 MFI(135SOs) MKEIASS 155 MS(135OS) cIz)VIR ilAF '155 M(135SOis) AnZRO1 1a11 1 130 Mly!I(113QS)
BAIL 101Z 130‘ M]?II(113OS)‘ .'SApIZ .... 100 MS(8?SOS)
W3G OVlll l 120 M(104SOS) 11AMMIR UAI)SS11 12Cj M(1040!IS) SMNS(nAp lIF. SGIDlj) Si£)WCZIRA!Eroll
1l!yCjO11yX11 2425 1.BS.‘ . ACIOBAI!IC MAISIVIS A11 1JIID¶X31IX3jWI. silA;L(XCXPI WE:rP SA11).SSIP SRN(n7Kt)1ArlGll!(U7Kt) cnlDl(n?Kt)sPnis'(nAP lyPING3mDI,I!).' .‘.
NORXAI CAgSIOli MAX. wlGH!r2510 1Bg. NO ACROBA¶!C‘rVlilS:Clm)llG SPllS AIE AIPplg)VII)... I .
AIRSpEED XNDlcATOR MARXIC IRE MARXED FoaNORMAL aR UuTy cATEGORY.
FCR ICROIA7IC CA?EGOlll SEE THZ APPROVED AIRPLAXE rLIGITIMANUAL

‘

134 MPH 116 KNOT 1dMPH129 KNOT
15 KNO7S

TABLE I5 .PLACARDS ON iNSTRIaMENT PANEL AND ADJACENT AREAS(3/4)
ISSED : JANIAly 1011
SERVICE NEWS 200-020
Plac&rd Descriptin
SE DESIGN MANEUVZRING SPEED NORI A14D LMy CAXIORy 143 MpH124KI!oT
.ACROBAIIC CASRy 154 MS 134 KNO!r llSDSONSIRAllD CIOSS WEND 15 KNOIS.

- -
’






10
11

A11
A11
11
All
DURING FLIGHTAVOID CONTINUOUS
OPERATIN FROM 2216 TO 2550 R.P.M WITH MANIFOLD PRESSURE O TO IS INCHES MERCURY
R.H.TANK
14 All

TABLE I-5 PLACARDS ON INSTRUMENT PANEL AND ADJACENT .AREAS{4/4}
144
4-I DESCRIP″rION
RA200 airplane is equipped withoneof tha three dif111rentmodels of Ayco Lycoming nginessaU of
which ae air cooledhorizontalopposed 4-cylinderdirect dzivenwet sump engines. Engine
applicabmty and relaisd inirmation is prcvided in the lblowlngEngine Data.
The cylindars are numbered as fi11]ow9:R/Hont cylinder…N0.1LZHontcylinder…N0.2R/H
rear cylinder...N0.3sand L/H rear cylinder...N0.4designatedbasedontheorderofeonnectingrods.
Perilrm engina checkl prChapter 8s Periodic Ch8ck ″nlble.Major repairs andoverhaul of enghles
shaUbecaiedouiina(sordance with overhaul Mallual(P/N60294-7)isgued byAyco licoming.
4-2 ENGINE DAIA
)
! upper and lower cowlings both of which are
mad !]

-
? °

’
ul)per and lower cowling attaching fasxiers1oeliand ovtwo bbncling
w1r1lg termixla



(4ea). a1dlasaizlg light
Whentha cowling is installed-be sure to reinstall thabonaing jumpers and
lazldijlg 11t 4rizlg remvea ih the above stepi Bend the sealing .of he baffles
in luch a c11rection (i71wa.rds)that air arouJla t;ezxgine ca71 now correctly.
lnstallation is accosplished in the revers s.
43-3 CL11:ANING AiiD ISlgPECTION OFIENGINE cowLING !
Cfean the insjde of the cowljwjth coth moistesd with cleanser(Federal Specinqation P-S-661o
equivalent.lf the inside is found eared with oiletcjpray cleanser on itjeave it a while as jtis.
wash it with solpy watef to remove all foreign matters s!d wipe off soapy water with dry cloth. As
ror the pajnted surface of the cowlings clean jt with neutfal cleanser,wash it away wjth a plenty of
water and wax it after wshinSto extend the durability of the painted surface. After washing chegk
thecowing for 4ents cracks and loose rivets.
.RepaifaJl defects discolered so thatlpropaSation ouch defects to other poltions canbe pfevenled.


- -
4-2
FUJI Fλ-200 SERVICE MANUAL
1i°'
!lcn system consitsf the spark p111gs harnass
agneto and‾igzlition switch.
415I SPARK PLUG
Eaah cylinder is provided with two 18 mm spark pluSs which are used to isnite ixture gas at the top
of the compression stroke. The life of a spark pluSdQpends upon the.operating conditions..Frequent
cleaniand colrectap adjustment ensure a16erlife.
(1)Every 50 hours remove.clean and check ajl spark plugs and ad3ustthe gap. ln case the lower
spark plugs are instaled in the upper positions of the cylinder or lice versa be sure to rota!e them at
every 50 hour check. Since the lower spark plugs usuaUy deteriorate faster than the upper ones the
spazk plugs arotated to extend the service e.
2Tightenthesparkplugstotilecylinderwithinthespecifiedtoique. 0therwiseljgasleakordamage

FA-200-160180.
)
FUjl FA-200 SERVICE MANUAL ‘
(3)Since dirtyspark plugs or damaged heUcons may cause misrecleanthem with clothmoistened
with methylethyl ketone.
The igllitionhamess consistsof 4 nexible shielded high tensionlead wires. 0ne harness is used to
connect the L/H magneto and the L/H upper and R/H lower spark plugswhile the other harness
provides connection between the R/H magneto and the R/H upper an(1LjH lower spark phlgs. Check
the harness assembly as follows:
(1)Check thelead wireslbr nickscutsor wear
(2)Checke spark plug sleevesforscratchesand damage. Check the couplingnuts fordamaged
thread.Check the compression spring fk)rdeterioratedtensionand damage. Check the grommets jbr
damage. Check an attach bra(lketsand clamps forsecurity
(3)Checktheconductivityoftheleadwires.lfanywireisfoundnon-condu(ve,the wire is cut
springspringretainer assemblyinsulating sleeve or a singlelead wire. Such replacement can be
accomphshed whne itisinstaned on the engine.
4153 1SIAGNETO
O-320 seriesene is equipped with the magnetosS4LN21(L/H)an(I S4LN-20 (R/H)or Snck 4373
(L/H)and Shck 4370 (R/H)andlO-360 seriesengine is equipped with the magnetosS4LN-200(L/H)
and S4LN-204 CR/H)or Slick 4347 (L/H)and SHck 4370 CR/H)in the aftportion of the accessory
section.A dual magneto D4LN-2021 or D4LN-3000 is instane(1on O-360-A5AD series en!e.
Each of these magnetos has a magnet with 2 poles(4 poles lbr D4LN2021 and D4LN3000 )
rotating at the engine speed. The magneto is designed to generate high voltagewhich enables the
spark plugs to emit sparks in the cynn(1ertoignite the mixtule gas.
CAUTION
Para4-15-44-15-6 are conceming Bendix magnetx).Regarding Snck magneto
Perform maintenance and inspection refer to L1363C 4300/6000 Series Magneto
Maintenance and overhaul Manual issued by unison lndustries. Both L/H and
R/H Magneto should use the same manufhcturer.
4-15-4 MAINTENANCEANDINSPECTIONOFMAGNgro
(1)At every periodic check, checkthecontactpointsofthebreakerassemblyfbrexcessivewearand
burn.Replace the points with deep cavity or excessive burn. Check if the cam felt is properly
hlbricated.ln case point polishing is considered necessar34 smooth them with hard nishhlg
sandpaper.CleantheinBideofthebreakerCompartmentwithcleancloth.
(2)ln case the engine has failed due to a cause associated with the ipition system check the spark
plugs and w1ring st bd)re checking the magnetos. Send the intemally f1ed magnetos to the
overhaul shop fbr repair and tests.
(3)visuallyinspectthesystemtodeterminethecauseofthe£ailure.
a. With the harness outlet plate removed from the magneto check the grommet and high
tension section of the distributor block fk)rmoisture. lf moisture is found present wipe it off nghtly
withsoftdryhnt.
CAUTION
Do not use gasoline or any other solvent to clean the distributorbk)ck.
Removalofthewaxcoatresults inelectricalshortcircuit.
SERVICE NEWS 200-020
142 VHFAIRCOMMUNICATIONEQUIPMENT

14-2-I GENERAL
14-2-2 COM:POSITIONANDPERFORMANCEOFXX160
14-2-3 KX-160 0PERArrINGPROCEDURES
14-24
INS?ALLA″rlONANDREMOVA:LOFIMEAR,6y 14-8
1429 ARc-522Ag)CARc-532A(J))OPERAIrING PRocEDUREs
14210 1NS'IALLAI?IONANIREMOVAL OFARC522A(J)CARC-532A6J))
14-2-11
14-2-12
KX-170 0PERArrING PROCEDURES
CO11POSITIONANDPERFOR2MEANCEOFKX-175
1414A
1414A
14a voRRAI)IO NAvlGATION EQUIPMENT 1416
COM:POSITION AND PERFORMANCE OF KX-160
KX-160 0PERjMrINGPROCEDURES.
COMPOSITIONAND PERFORMANCE OFARC522A(J)(ARC-542A(J))
ARC-522A(J)CAIC542A(J))OPERATING PROCEDURES 14-21
COIMIPOSITIONAND PERFORIMIANCE OF KX-170
143-10 1NSrrALLArllIONANDREMOIALOFKX-170
14-343 1NSTALLATIONANDREMOVALOFKX175
14,48

14-8-17 TROUBLE-SHOOTING OF VOR NAVIGAIrlON EQUIPMENT 14-26B
14-27

14-4-2 COMPO8ITION AND PERFORMANCE OF KR80
KR'80 0PERArING PROCEDURES 1428
INS″rALLArrION AND RMOrVALOFKR8014-29
COMPOSITION AND PERFORIMIANCE OF KR-8511aa 14-29
KR-85 0PERATING PROCEDURES
1448 COMPOSITIONANDPERFORIMIANCEOFARC-824A 14-81
1449 ARc324A OPERAnNG PRocEDIJIEs 1432
14-4-10 1NSI!ALLAIrIONANI)REMOVAL OFARC-824A 14-88

1484

14-5-8 INTERCOM EQUIPMENT OPERA11NG PROCEDURES 1435
14-5-4 1NSIALLAIrIONANDREMOVALOFINTERCOMEQUIPMRNT 14-85
ISSUED : IAKIJARY 2010
(1)Composition
6 dB drop width 8.1KHzorless
60dBop width 20.0KHzorless 100mWat500Ωload
Speaker 4W at 4Ωload
Rrom 5μv to 20,000μv audio output wm not valy more
than 3 dB.
3

(2)Rotatethecontrol switch knob (1)ofthe£rontpanelofthe receiver clockwise to“ON".
(3)Adjust the knob (2)so that the hquency indication window (3)will show a desired hquency.
Keep the vOL knob (I)at a proper position.
(4)Communicate with the control tx)werand adjust the knob (1)to a proper sound level.Forthe
transmission of messages, take the hand microphone o£fthequadrant and press the pushbutton ofthe
hand microphone as you speak.
(5)For headset reception,inserttheplugsoftheheadsetintotherespectivejacksonbothsidesof
the lower panel of the instrument panel and you can use the headphones.
(6)The “TEST" position of thecontrolswitch(1)isusedfk)r automatic squelch release test and also
)rreceptionofextremelyeble signal.
142-19 1NSIALLATIONAND REMOVAL OF KX-155
(1)Refer to para. 14-213 for removal of the transmitter-receiver proper (KX-155).(Thesame
procedures as KX170 are appncable.)
(2)Removalofanterma(CI 121)
a. Discom!ectthe coaxial cable terminal at the antenna connection.
b.Loosen the fbur antenna mountinrnuts and puU out the antenna fyom the mounting hole
outside the body. For the installation of the transmitter-receiver proper and antemla reverse the
relnoval procedures.
142-20 7ROUBLESHOOTING OFAIR COMMUNICATION EQUIPMENT
Trouble ProbableCause Remedy
1.Power supply unavailable
3.Transmission satisfactory
but receptionimpossible
(satisfactorywith headphone)
(I)Defective speaker.
correct
(2)Defectiveladio eqliipment
J
143-I GENERAL
The VOR naviSation equipment is used to fly the aircr8ft inla desired djrection measurini the bearing
of the aircraft Theoperatins frequency ranSe is from l08 MHz to H7.95 MHz. Iltindicates the
VOR bearing qn the indicatorl .re‘ceivinSa diffirent phase raditwvelwjth respect to each magnetic
beaing transmitted nom a groulld station.
Tbe VOR eqQipmeηtpper used in the FA-200 is one with the VHFair clommunicationequipment
proper. The opeiatinS frequencys sound volume and other controls andprovided on the ffont pancl
of the equipment proper. TheVOR indicator or course hldicator in another namejs located on the
left instrument panel.
For homing according to rgception from lthe VOR lstationI Set a desiied vOR sngle otheISle setting
wdow of the indicatol and ny the aircrafl in such a way that the vertjcal pointer win stay tha in
center of the indicator.
lf the aireraft deviates to the rigllt from the course the pointir shifts to -the left. lfit deviates to the
.leftfrom the course the pointer shifts to the right.
The indicatoi has “TO’‘FOM” and “OFFI’ mazks. The“TO”and“FROM”marksindicatewhetller
the aircraft is heading to the vOR station or parting from the station. The “OFF” mark indicates no
reception.
The VOR indicator has two angles where thel vertical pointer comes to the center. Thg difference
be.tweentheanlaesis180°.
Fig.14-6 is an explanatory drawing
Suppose that theaircraft’ is .flyhls?t the poillt A ii Fig. 146. The poiiltei ofe indicator eomes to
the center at tWo angles 30.“FROMIl and 210°“TO¨.
At the point A. these two indications are presented regardless of the direction of the aircraft.
To determine whether the aircraft is heading tojr parting from the vOR stationl watch the standby
compass and judge from its indication. lf the siandby compass indication is around 30° and the vOR
indication 30°“FROM¨it follows that the aircraft is plartilfrom the “VOR” station. lfthevOR
indication is 210°“TO’?it foUows that the aircraft is heading to the vOR station.
lfthestandbycompassindicationisaround210°reverse is.the case.
The use oftVOR navigation equipment offeis the advantage of njght almost strajgJlt to the vOR
Statjon regardeSS Of the attitde of the ajrCraft WhiChlmay Change Under the effeCtS Of Wind and OtherS.
The VOR antenna is located ’atthe end of the vertjcal stabUizer.
14-16
14-312 KX-175 0PERATING PROCEDURES
(1)Turnon Master Switc11,1o{3ated on the lower portion of t}le instrument panel.
(2)Place selector switch knob (1)on tlle receiver front panel in IDENT or VOICE positian and sit
to ON
(3)Select t}le frequen‘cy o‘fa dsired vOR statiorl in frequency window (3)by .txlrning two concentric
knobs(2).Turn t}lelarger knob for MHz sslaction and tlle,smlller one for KEz salction H
4Adjust VOL Knob (4)to obtain a proper sound level.
(5)Set salector switeh knob (1)to IDENT positian and check lor tlle desired VOR stion.After
confiim&tionset the knb to vOICE psition.
(6)Set tbe desired djrectjn just under the tp indicatr index 5by turning OBS kn(6)
7Mainlaining a centered deviation needla wiU prde lloming
(8).Aitlr useset tha 1ectar switcll.QFF pQsitian


(1)Refertopara14-3-10fbrinstanationandremovalofvORreceiverproper(KX175),VOR
14,8-14 COMPOSITIONAND PERFORMANCE OF KX-155
(1)Composition
Antenna
200 channels 108.00MHzton7.95MHz 50KHz 2μV
6 dB drop width 16.0KHzorless 60 dB drop width 31.5KHzorless 100mWat500Ωload
Speaker 4XV at 4Ωload
From 5μv to 20,000μv audio output wm not vary more
than3dB.
(1)Setthe“MASTER"switchlocatedonthelowerpaneloftheinstrumentpanelto“ON"
(2)Rotate the knob (1)ofthe£rontpanelofthereceiverclockwise‘ON".
(3)Adjust the knob (2)so that the frequency indication window (3)wm show the frequencyofa
desired vOR station.
(4)Adjust the vOL knob (4)to a proper sound leve1.
(5)Pull the knob (4)to“IDENT" and check that the desired vOR station has been selected.After
conrmingit,push the knob (4)to“VOICE".
(6)Select a desired vOR angle on the vOR angle setting window (5)of the indicator by turning the
OBS knob (6).
(7)For homing, ny the aircraftin such a way that the vOR pointer win stay in the center of the
indicator.
148-16 1NSIALLAIION AND REMOVAL OF KX-155
(1)Refer to pan. 14-3-10 forinstaUation and removal of the vOR receiver proper (KX-155)the
vOR indicator (KI-203)and the antenna (OD-2).(The same procedures as KX-170 al‘e
applicable.)
Ttouble ProbableCause Remedy
equipment)
ofindicatordoesnot
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