Futaba T18MZWC-24G Radio Control User Manual 2

Download:
Mirror Download [FCC.gov]
Document ID	2898094
Application ID	o+AllvWQ9xbRi5ftAwbBCg==
Document Description	User Manual 2
Short Term Confidential	No
Permanent Confidential	No
Supercede	No
Document Type	User Manual
Display Format	Adobe Acrobat PDF - pdf
Filesize	322.53kB (4031606 bits)
Date Submitted	2016-02-05 00:00:00
Date Available	2016-02-05 00:00:00
Creation Date	2016-01-27 16:12:32
Producing Software	Acrobat Distiller 7.0.5 (Windows)
Document Lastmod	2016-01-27 16:12:37
Document Title	User Manual 2
Document Author:	Konno

'LDO0RQLWRU
'LVSOD\VWKHSRVLWLRQRIWKHGLDOVVOLGHUOHYHUVDQGGLJLWDOWULP
Digital trim position display (T1-T6, CD)
Digital trim step amount (T1-T6, CD)
The Dial Monitor displays the current position and
step amount of each digital trim. The trim step can
be set directly on the dial monitor.
The trim step of the T1-T6 and CD can be set
directly on the dial monitor menu.
VR and slide lever position display (LST, LS, LD,
RD, RS, RST)
$,53/$1(
Displays the current position (black ) and last
operating position (green ) of the VRs and slider
levers.
ŏ 7RXFK WKH >'LDO 0RQLWRU@ EXWWRQ LQ WKH /LQNDJH
0HQXWRFDOOWKHVHWXSVFUHHQVKRZQEHORZ
ŏ5HWXUQWR/LQNDJH0HQX
*/,'(5
ŏ7ULPFKDQJHVIURPWKHVWHSWRGLVSOD\
ŏ'LJLWDOWULPVWHSDPRXQW
+(/,&237(5
Knob and Lever Position display
(LD, RD, LS, LST, RS, RST)
Recalling Dial Position
(LST, LS, LD, RD, RS, RST)
The Dial Monitor displays the current position
and last operating position of each knob and lever.
Although neither knob nor lever can hold the last
operation position as they are “analog” type, the
SRVLWLRQGDWDGXULQJWKHODVWRSHUDWLRQLVPHPRUL]HG
in the model memory. By moving the knob and lever
to the position displayed on the monitor, the last
operation position is recalled.
The dial position data at the last operation is
displayed for each knob and lever in this monitor.
*UHHQDUURZ
94 ＜ Linkage Menu ＞
0RYHWKHEODFNDUURZ FXUUHQWSRVLWLRQ WRWKH
JUHHQDUURZSRVLWLRQE\RSHUDWLQJWKHGHVLUHG
NQRE RU OHYHU WR UHFDOO WKH ODVW RSHUDWLQJ
SRVLWLRQ
)XQFWLRQ1DPH
)XQFWLRQ1DPHVFDQEHFKDQJHGLQWKLVPHQX
$,53/$1(
The setup screen will display function names in both
DQGFKDUDFWHUV
ŏ 7RXFK WKH >)XQFWLRQ 1DPH@ EXWWRQ LQ WKH /LQNDJH
0HQXWRFDOOWKHVHWXSVFUHHQVKRZQEHORZ
+(/,&237(5
*/,'(5
ŏ5HWXUQWR/LQNDJH0HQX
＜ Linkage Menu ＞ 95
'LVSOD\LQJGDWDIURPWKHUHFHLYHU
7HOHPHWU\
$,53/$1(
WARNING
This screen displays your choice of data from the
receiver.
'RQRWZDWFKWKHWUDQVPLWWHUVFUHHQGXULQJÀLJKW
Also warnings can be activated regarding the data.
7HOHPHWU\@EXWWRQRIWKH/LQNDJH0HQX
ŏ5HWXUQWR/LQNDJH0HQX
*/,'(5
ŏ ,W FDQ DOVR FDOO E\ WKLV PHWKRG +RPH VFUHHQ
>+RPH@ →$UELWUDU\VHQVRUV →+RPH>6HOHFW@
ŏ7KHVORWQXPEHURIWKHVHQVRUGLVSOD\HGRQ
DVFUHHQLVFKRVHQ
ŏ,WFKRRVHV
ZKHWKHU
WRPDNHLW
GLVSOD\
+(/,&237(5
212))
ŏ7KHLQWHUYDOZKLFKJLYHVD
VSHHFKGDWD VHF
ŏ:KHQJLYLQJDVSHHFK
LWFKRRVHV2))
ŏ+RPHGLVSOD\
,QWKHFDVHRIDKHOLFRSWHUWKH
SRVLWLRQRI3,7DQG7+5LVGLVSOD\HG
$WLPHUGLVSOD\LVRQH
96 ＜ Linkage Menu ＞
ŏ+RPHGLVSOD\
ŏ7KLVGLVSOD\LVWKH
PD[LPXPPLQLPXPDIWHU
VWDUWLQJUHFHSWLRQXQWLOLW
WXUQVRIIDWUDQVPLWWHU
Audible telemetry information
*/,'(5
ŤƏƗƌƗƘƇƈŃŖœƐŏ
ʄ7KHYRLFHLVLQHQJOLVK
ʄ7KHDXGLEOHLQGLFDWRULVFDSDEOHRIQRWLQJWKHGDWDIURPDQ\
ŖŔŏŃŖŕŏŃŖŖŏŃŖŗ
RUDOO RIWKHWKUHHVHQVRUVVHOHFWHG
ʄ :KHQ XVLQJ WKH YRLFH UHDG IXQFWLRQ VHW WKH >7LPHU DQG 3,7
DQG7+5@VHWWLQJRIWKHKRPHVFUHHQWRWKH>2))@PRGH
ʄ,WLVSRVVLEOHWRDGMXVWKRZRIWHQWKHGDWDLVFRQYH\HGWRWKH
PRGHOHU7KHIUHTXHQF\UDQJHVIURPVHFRQGV,IVHWDW
XSGDWHVZLOORFFXUFRQWLQXRXVO\,IVHWWRXSGDWHVZLOO
RFFXUHYHU\VHFRQGV
ʄ 7KH 70=:& RIIHUV WKH DELOLW\ WR DGMXVW WKH YROXPH RI WKH
DXGLEOHWHOHPHWU\GDWD7KHYROXPHIRUWKHWHOHPHWU\GDWD
LV FRPELQHG ZLWK WKH (UURU:DUQLQJ YROXPH  7R DFFHVV
WKLVDGMXVWPHQW>6\VWHP0HQX@ → >6RXQG9ROXPH@ → (UURU
:DUQLQJ
ʄ:KHQRQO\RQHNLQGRIGDWDLVVHWWRUHDG21WKHGDWDLVUHSHDWHGO\UHDGLQWKHIROORZLQJRUGHU
>6HQVRU7\SH'DWD8QLWV@>'DWD@>'DWD@>'DWD@>'DWD@
([DPSOH 5HDGLQJRIUHFHLYHUYROWDJH
%DWWHU\ HLJKW SRLQW RQH YROW HLJKW SRLQW RQH HLJKW SRLQW RQH HLJKW SRLQW RQH HLJKW SRLQW RQH
EDWWHU\LVUHSHDWHG,I\RXKDYHDFWLYDWHGWKHDXGLEOHLQGLFDWRUVIRUPXOWLSOHVHQVRUVWKH70=
:&ZLOOF\FOHWKURXJKWKHLQGLFDWRUVDWWKHVHOHFWHGWLPLQJLQWHUYDOVDFFRUGLQJO\
ʄ :KHQ WKH YRLFH UHDG IXQFWLRQ LV WXUQHG RQ IRU WHOHPHWU\ GDWD ZLWK DODUP VHW ZKHQ DQ DODUP LV
DFWLYDWHGDYRLFHDODUPLVJLYHQLQDGGLWLRQWRWKHDODUPVRXQGZKHQWKHDODUPZDVDFWLYDWHG
>:DUQLQJ@>6HQVRU7\SH'DWD8QLWV@
$,53/$1(
In addition to the on-screen telemetry data
information, the T18MZ-WC now has the ability to
audibly indicate the aircraft status.
ŏ,WZLOOJLYHDVSHHFKLIWXUQHGRQ
+(/,&237(5
ŏ+RPHVFUHHQ → +RPHVFUHHQ
ŏ ,W LV DOVR SRVVLEOH WR WXUQ WKH DXGLEOH
LQIRUPDWLRQ RQRII E\ WKH XVH RI DQ
DUELWUDU\VZLWFKDQGRUVZLWFKSRVLWLRQ
＜ Linkage Menu ＞ 97
A setup of each sensor display
ŏ&DOOWKHIROORZLQJVHWWLQJVFUHHQE\SUHVVLQJWKH
>7HOHPHWU\@EXWWRQRIWKH/LQNDJH0HQX
$,53/$1(
ŏ:KDWLVUHJLVWHUHGE\WKH6HQVRURIWKHIROORZLQJ
FODXVHLVGLVSOD\HG
ŏ$ERXWWKHSUHVHWYDOXHRI7KUHVKROG
7KH SUHVHW YDOXH RI Ń PD[LPXP LV QRW PDGH
EHORZWKHSUHVHWYDOXHRIŅPLQLPXP
*/,'(5
7KH SUHVHW YDOXH RI Ņ PLQLPXP LV QRW PDGH
DERYH WKH SUHVHW YDOXH RI Ń PD[LPXP
Receiver Battery Display
ŏ$ GRZQZDUG DUURZ VKRZV WKDW WKH
DODUP RSHUDWHV ZKHQ OHVV WKDQ WKH
VHWXSQXPHULFDOYDOXH
ŏ5HFHLYHUEDWWHU\YROWDJH
ŏ([WHUQDO,QSXWYROWDJH
(([WUD9ROWDJHFRQQHFWRU 
ŏ,IYROWDJHIDOOVIXUWKHUWKDQWKHYROWDJH
VHWXSKHUHWKHDODUPZLOORSHUDWH
ŏ5HWXUQWR7HOHPHWU\
9
99
+(/,&237(5
ŏ&KDQJHRI
DQXPHULFDO
YDOXH
99
ŏ3UHVVWRVHWXSDQDOHUW
ŏ,WLVVHOHFWLRQRIWKH
VHQVRUGLVSOD\HGRQ
KRPHVFUHHQ
ŏ 3UHVVWRVHWXSYLEUDWLRQDOHUWV
W\SHVRIYLEUDWLRQVHOHFWLRQVDUHSRVVLEOH
ŏ7KLVGLVSOD\LVWKHPD[LPXPDQG
PLQLPXPDIWHUVWDUWLQJUHFHSWLRQXQWLO
LWWXUQVRIIDWUDQVPLWWHU
,QRUGHUWRPHDVXUH([W%DWWHU\YROWDJHCA-RVIN-700
(;7(51$/92/7$*(,1387&$%/( RIDQRSWLRQLVUHTXLUHG
98 ＜ Linkage Menu ＞
ŏ,1+ → $&7DYRLFH
DODUPLVJLYHQLQ
DGGLWLRQWRWKH
DODUPVRXQGZKHQ
WKHDODUPZDV
DFWLYDWHG
ŏ'LVSOD\RIWKHPD[LPXP
DQGPLQLPXPUDQJHV
IRUYROWDJH>&OHDU@WR
UHVHW
Temperature Display
7HPSHUDWXUHVHQVRUSBS-01T/TELVUHTXLUHG
ŏ , I  W H P S H U D W X U H  U H D F K H V  K L J K H U  W K D Q  W K H
WHPSHUDWXUHVHWXSKHUHWKHDODUPZLOORSHUDWH
ŏ7HPSHUDWXUH'LVSOD\
PLQPD[
ŏ&KDQJHRI
DQXPHULFDO
YDOXH
ŏ3UHVVWRVHWXSDQDOHUW
ŏ,WLVVHOHFWLRQRIWKH
VHQVRUGLVSOD\HGRQ
KRPHVFUHHQ
ŏ3UHVVWRVHWXSYLEUDWLRQDOHUWV
W\SHVRIYLEUDWLRQVHOHFWLRQVDUHSRVVLEOH
ŏ'LVSOD\RIWKHPD[LPXP
DQGPLQLPXPUDQJHVIRU
WHPSHUDWXUH>&OHDU@WRUHVHW
530VHQVRUSBS-01RM/RO/RBLVUHTXLUHG
ŏ,1+ → $&7DYRLFH
DODUPLVJLYHQLQ
DGGLWLRQWRWKHDODUP
ŏ,I530JRHVORZHUWKDQWKH530 VRXQGZKHQWKHDODUP
VHWKHUHWKHDODUPZLOORSHUDWH ZDVDFWLYDWHG
ŏ,I530JRHVKLJKHUWKDQWKH530
VHWKHUHWKHDODUPZLOORSHUDWH
ŏ530'LVSOD\
ŏ5HWXUQWR7HOHPHWU\
PD[
ŏ3UHVVWRVHWXSDQDOHUW
ŏ&KDQJHRI
DQXPHULFDO
YDOXH
0DJQHW
6%650ń *HDUUDWLR a
2SWLFV
6%652ń )LQ
a
%UXVKOHVVPRWRU 6%65%ń 3ROH
a
ŏ,W LV VHOHFWLRQ RI WKH
VHQVRU GLVSOD\HG RQ
KRPHVFUHHQ
ŏ3UHVVWRVHWXSYLEUDWLRQDOHUWV
W\SHVRIYLEUDWLRQVHOHFWLRQVDUHSRVVLEOH
ŏ7RXFK WKH >&RQGLWLRQ@ EXWWRQ 7KH
VFUHHQWKDWDSSHDUVQH[WGHQRWHV
W K H  P D [ L P X P  5 3 0  D F K L H Y H G
IRU HDFK RI WKH IOLJKW FRQGLWLRQV
SURJUDPPHGLQWRWKHWUDQVPLWWHU
ŏ7KH GLVSOD\ RI WKH PD[LPXP DIWHU
FDUU\LQJRXWSRZHU21
ŏ'LVSOD\RIWKHPD[LPXP
UDQJHVIRU530>&OHDU@
WRUHVHW
＜ Linkage Menu ＞ 99
*/,'(5
RPM Display
ŏ,1+ → $&7DYRLFH
DODUPLVJLYHQLQ
DGGLWLRQWRWKHDODUP
VRXQGZKHQWKHDODUP
ZDVDFWLYDWHG
+(/,&237(5
ŏ7KLVGLVSOD\LVWKHPD[LPXPDQGPLQLPXP
DIWHUVWDUWLQJUHFHSWLRQXQWLOLWWXUQVRIID
WUDQVPLWWHU
$,53/$1(
ŏ,I WHPSHUDWXUH EHFRPHV ORZHU WKDQ WKH
WHPSHUDWXUH VHW XS KHUH WKH DODUP ZLOO
RSHUDWH
ŏ5HWXUQWR7HOHPHWU\
$OWLWXGHVHQVRUSBS-01/02ALVUHTXLUHG
Altitude Display
Atmospheric pressure is measured by a sensor. The
actual altitude is measured in regards to the difference
between the ground and atmospheric pressure.
Atmospheric pressure when the power supply of the
altitude sensor is set to ON is displayed as a standard
P 
[Reset] Push the button to re-set to a standard
altitude.
What altitude is it?
$,53/$1(
ŏ3UHVVWRVHWXSDQDODUPW\SHDOHUW
ŏ9DULRPHWHU'LVSOD\：+RZPDQ\
PHWHUULVH GHVFHQW LQVHFRQG
ŏ5HWXUQWR7HOHPHWU\
ŏ,I$OWLWXGHEHFRPHVKLJKHUWKDQWKH
$OWLWXGHVHWKHUHWKHDODUPZLOORSHUDWH
ŏ$OWLWXGH'LVSOD\
ŏ,I$OWLWXGHEHFRPHVORZHUWKDQWKH
$OWLWXGHVHWKHUHWKHDODUPZLOORSHUDWH
PLQPD[
ŏ&KDQJHRI
DQXPHULFDO
YDOXH
PLQPD[
*/,'(5
ŏ$WPRVSKHULFSUHVVXUH'LVSOD\
ŏ7KLV GLVSOD\ LV WKH PD[LPXP
DQG PLQLPXP DIWHU VWDUWLQJ
UHFHSWLRQ XQWLO LW WXUQV RII D
WUDQVPLWWHU
Variometer melody function
+(/,&237(5
When using a variometer, the T18MZ-WC
offers the option of incorporating a tonal
indication of the aircraft's rate of ascent or
descent.
ʄ 7R HQVXUH WKDW WKH SLORW LV DZDUH DV
WR WKH PRGHO V VWDWXV WKH 70=:&
LQFRUSRUDWHV D GLIIHUHQW PHORG\ IRU
DVFHQW DQG GHVFHQW  $GGLWLRQDOO\
GHSHQGLQJ XSRQ WKH UDWH RI FOLPE RU
GHVFHQW WKH WRQHV YDU\ WR LQGLFDWH
ZKHWKHURUQRWWKHDLUSODQHLVFOLPELQJRU
GHVFHQGLQJDWDUDSLGUDWH
ʄ7KHPHORG\IXQFWLRQDQGWKHYRLFHUHDG
IXQFWLRQ FDQ EH XVHG VLPXOWDQHRXVO\
:KHQ WKH YRLFH UHDG IXQFWLRQ ZDV
WXUQHGRQGDWDLVUHDGDVIROORZV
&OLPELQJ[“Climb” climb speed “m/s”]
6LQNLQJ[“Sink” sink speed “m/s”]
100 ＜ Linkage Menu ＞
ŏ3UHVVWRVHWXS
YLEUDWLRQDOHUWV
W\SHVRIYLEUDWLRQ
VHOHFWLRQVDUH
SRVVLEOH
ŏ,I3UHVHWLVSXVKHG
WKHSUHVHQW
DWPRVSKHULFSUHVVXUH
DOWLWXGHRIP
ŏ,1+ → $&7DYRLFH
DODUPLVJLYHQLQ
DGGLWLRQWRWKHDODUP
VRXQGZKHQWKH
DODUPZDVDFWLYDWHG
ŏ'LVSOD\RIWKHPD[LPXP
DQGPLQLPXPUDQJHV
IRU530>&OHDU@WR
UHVHW
ŏ,WLVVHOHFWLRQRIWKH
VHQVRUGLVSOD\HGRQ
KRPHVFUHHQ
*36VHQVRUSBS-01GLVUHTXLUHG
ŶƓƈƈƇ
*Positioning time of GPS
:KHQ SRZHUHG XS WKH 6%6* EHJLQV WR
DFTXLUH *36 VDWHOOLWH GDWD 7KLV SURFHVV FDQ
take several minutes. Please do not move the
model during this process. During acquisition,
WKH /(' RQ WKH 6%6* ZLOO EOLQN JUHHQ
after the satellites signals have been acquired,
WKH/('ZLOOEHFRPHVROLGJUHHQDQGWKH*36
signal strength display on the transmitter will
show three bars.
Moving the model before the satellites are fully
acquired will cause a delay in acquiring the
satellite signal.
ƓƒƖƌƗƌƒƑ
ŧƌƖƗƄƑƆƈ
ŏ,IWKLVYDOXHLVH[FHHGHG
WKHDODUPZLOORSHUDWH
ŏ*36SRVLWLRQLQJGLVSOD\
7KUHHEDUVLQGLFDWHVDFTXLVLWLRQRIWKH
*36VDWHOOLWHGDWD>3UHVHW@PD\EH
SXVKHGWRORFNLQWKHPRGHOVFXUUHQW
SRVLWLRQDVWKHVWDUWLQJSRVLWLRQ
ŏ,I LW EHFRPHV ORZHU WKDQ WKLV
YDOXHWKHDODUPZLOORSHUDWH
ŏ7KLVGLVSOD\LVWKHGLVWDQFHWRD ŏ3UHVVWRVHWXSDQ
PRGHO ↔SUHVHWSRVLWLRQ 
DODUPW\SHDOHUW
ŏ5HFHLYHU → WUDQVPLWWHU
VLJQDOVWUHQJWK
ŏ$/7GLVSOD\VGDWD
IURPWKHDWPRVSKHULF
SUHVVXUHVHQVRU*36
GLVSOD\VGDWDIURPWKH
*363UHVVWRFKDQJH
ŏ5HWXUQWR
7HOHPHWU\
ŏ,1+ → $&7:KHQ
DFWLYDWHGDYRLFH
DOHUWZLOODOVR
VRXQGLQDGGLWLRQ
WRWKHDODUP
ŏ6SHHG
'LVSOD\
$,53/$1(
)XWDED V*36VHQVRU 6%6* REWDLQVSRVLWLRQ
GDWDIURP*36DQGGLVSOD\VWKHVSHHGFDOFXODWHG
from the distance, and distance from a preset
position.
Additionally the sensor includes an accurate
atmospheric pressure sensor that provides altitude
and variometer (vertical speed) data.
*/,'(5
GPS Display
ŏ&KDQJHRI
DQXPHULFDO
YDOXH
ŏ7KH GLVSOD\ RI WKH PD[LPXP DIWHU
FDUU\LQJRXWSRZHU21
ŏ&KRRVHEHWZHHQ>6ODQW@WKH
GLVWDQFHWRDPRGHOWDNLQJDOWLWXGH
LQWRFRQVLGHUDWLRQRU>6XUIDFH@WKH
GLVWDQFHWRWKHPRGHORQDWZR
GLPHQVLRQDOPDSGLVUHJDUGLQJ
DOWLWXGH
nt
Sla
ŏ,ISUHVHWLVSXVKHG
GLVWDQFHRIP
ŏ'LVSOD\RIWKHPD[LPXP
UDQJHV>&OHDU@WRUHVHW
ŏ7KLVVHOHFWVRIWKH
VHQVRUVGLVSOD\HGRQ
KRPHVFUHHQ
ŏ3UHVVWRVHWXSYLEUDWLRQDOHUWV
W\SHVRIYLEUDWLRQVHOHFWLRQVDUH
SRVVLEOH
Altitude
Surface
＜ Linkage Menu ＞ 101
+(/,&237(5
ŏ&XUUHQWPRGHOSRVLWLRQ
Voltage Display
9ROWDJHVHQVRUSBS-01VLVUHTXLUHG
7KH 6%69 KDV WKH FDSDELOLW\ RI PHDVXULQJ
voltage from two different batteries at the same
time. It will measure the voltage that its normal
3-pin connector is plugged into, such as a receiver ŏ$GRZQZDUGDUURZVKRZVWKDWWKHDODUPRSHUDWHV
RU VHUYR EDWWHU\ SDFN  DGGLWLRQDOO\ LW KDV DQ ZKHQOHVVWKDQWKHVHWXSQXPHULFDOYDOXH
H[WHUQDO OHDG WKDW FDQ EH XVHG WR PHDVXUH KLJK
ŏ,IYROWDJHIDOOVIXUWKHUWKDQWKHYROWDJH
voltages like drive batteries.
VHWXSKHUHWKHDODUPZLOORSHUDWH
$,53/$1(
ŏ5HWXUQWR
7HOHPHWU\
ŏ1RUPDOOLQH
EDWWHU\
YROWDJH
ŏ([WOLQH,QSXW
YROWDJH
9ROWDJH
9

99
ŏ&KDQJHRI
DQXPHULFDO
YDOXH

99
ŏ3UHVVWRVHWXSDQDOHUW
ŏ3UHVVWRVHWXSYLEUDWLRQDOHUWV
ŏ6HOHFWVWKHVHQVRU
ŏ,1+ń$&76RXQGVD
W\SHVRIYLEUDWLRQVHOHFWLRQVDUHSRVVLEOH GLVSOD\HGRQKRPH
YRLFHDOHUWLQDGGLWLRQ
VFUHHQ
WRWKHDODUPVRXQG
ŏ7KLV GLVSOD\ LV WKH PD[LPXP DQG
ZKHQWKHDODUPLV
ŏ'LVSOD\VWKHPD[LPXP DFWLYDWHG
PLQLPXPDIWHUVWDUWLQJUHFHSWLRQXQWLO
DQGPLQLPXPYROWDJH
WKHWUDQVPLWWHULVWXUQHGRII
UDQJHV>&OHDU@WRUHVHW
*/,'(5
＜ Two examples of wiring are shown ＞
Two drive batteries are measured (SBS-01V use)
Drive battery 1
EXT Battery)
Drive battery 2
EXT Battery)
EXT Line
Normal Line
WR6%86
SRUW
56%
Receiver battery
*The same
receiver battery
+(/,&237(5
●Battery voltage measurement for receivers [R7008SB use]
●Battery voltage measurement for receivers [SBS-01V use]
●The drive battery 1 is measured in an EXT port [R7008SB use]
●The drive battery 2 is measured in an EXT line [SBS-01V use]
Two drive batteries and power supplies for servos are measured (SBS-01V use)
Drive battery 1
EXT Battery)
Drive battery 2
EXT Battery)
Power supplies
for servos
*SBS-01V measures two voltage. One corresponds to high voltages, such as a drive battery,
with an EXT line. Another is a normal line and is measurement of the battery for receivers of a
line connected to 3P connector, or the battery for servos.
EXT Line
6ZLWFK
Normal Line
WR6%86
SRUW
$QRWKHUSRZHU
VXSSO\+XE
56%
Receiver battery
S.BUS2
servos
●Battery voltage measurement for receivers [R7008SB use]
●The drive battery 1 is measured in an EXT port [R7008SB use]
●The drive battery 2 is measured in an EXT line [SBS-01V use]
●The voltage for servos is measured in a power supply line [SBS-01V use]
5HIHUWRWKHPDQXDORI6%69IRUWKHGHWDLOVRIZLULQJ
102 ＜ Linkage Menu ＞
Current / Voltage / Capacity Display
&XUUHQWVHQVRUSBS-01CLVUHTXLUHG
7KH 6%6& KDV WKH FDSDELOLW\ RI PHDVXULQJ
current, voltage and capacity from drive battery at
the same time.
ŏ,IWKLVYDOXHLVH[FHHGHG
WKHDODUPZLOORSHUDWH
ŏ5HWXUQWR
7HOHPHWU\
ŏ'ULYH
EDWWHU\
FXUUHQW
PLQPD[
ŏ'ULYH
EDWWHU\
YROWDJH
PLQPD[
ŏ&KDQJHRI
DQXPHULFDO
YDOXH
$,53/$1(
ŏ,ILWEHFRPHVORZHUWKDQWKLV
YDOXHWKHDODUPZLOORSHUDWH
ŏ3UHVVWRVHWXSDQDOHUW
*/,'(5
ŏ3UHVVWRVHWXSYLEUDWLRQDOHUWV
ŏ6HOHFWVWKHVHQVRU
ŏ,1+ń$&76RXQGVD
W\SHVRIYLEUDWLRQVHOHFWLRQVDUHSRVVLEOH GLVSOD\HGRQKRPH
YRLFHDOHUWLQDGGLWLRQ
VFUHHQ
WRWKHDODUPVRXQG
ŏ7KLV GLVSOD\ LV WKH PD[LPXP DQG
ZKHQWKHDODUPLV
ŏ'LVSOD\VWKHPD[LPXP DFWLYDWHG
PLQLPXPDIWHUVWDUWLQJUHFHSWLRQXQWLO
DQGPLQLPXPYDOXH
WKHWUDQVPLWWHULVWXUQHGRII
UDQJHV>&OHDU@WRUHVHW
+(/,&237(5
ŏ'ULYH
EDWWHU\
FDSDFLW\
5HIHUWRWKHPDQXDORI6%6&IRUWKHGHWDLOVRIZLULQJ
＜ Linkage Menu ＞ 103
6HUYRVHQVRUSBS-01SLVUHTXLUHG
Servo sensor Display
S.BUS2 servo only
◆ Current
◆ Operation
◆ Temperature
ŏ,IWKLVYDOXHLVH[FHHGHG
WKHDODUPZLOORSHUDWH
ŏ6HUYR&XUUHQW'LVSOD\
ŏ6HUYR7HPSHUDWXUH'LVSOD\
ŏ,ILWEHFRPHVORZHUWKDQWKLV
YDOXHWKHDODUPZLOORSHUDWH
ŏ5HWXUQWR7HOHPHWU\
$,53/$1(
PLQPD[
ŏ&KDQJHRI
DQXPHULFDO
YDOXH
ŏ3UHVVWRVHWXSDQDOHUW
ŏ,WLVVHOHFWLRQRIWKH
VHQVRUGLVSOD\HGRQ
KRPHVFUHHQ
ŏ3UHVVWRVHWXSYLEUDWLRQDOHUWV
W\SHVRIYLEUDWLRQVHOHFWLRQVDUHSRVVLEOH
*/,'(5
ŏ7KLVGLVSOD\LVWKHPD[LPXPDQGPLQLPXP
DIWHUVWDUWLQJUHFHSWLRQXQWLOLWWXUQVRIID
WUDQVPLWWHU
ŏ6HUYR$QJOH'LVSOD\
ŏ,1+ → $&7DYRLFH
DODUPLVJLYHQLQ
DGGLWLRQWRWKHDODUP
VRXQGZKHQWKHDODUP
ZDVDFWLYDWHG
ŏ'LVSOD\RIWKHPD[LPXP
DQGPLQLPXPUDQJHVIRU
WHPSHUDWXUH>&OHDU@WRUHVHW
ŏ6HUYR>&XUUHQW@>7HPS@
ŏ6HUYR>$QJOH@>&RQQHFWLRQ@
ŏ6HUYR>&XUUHQW@>7HPS@
ŏ6HUYR>$QJOH@>&RQQHFWLRQ@
PLQPD[
+(/,&237(5
ŏ6HUYRFRQQHFWLRQDODUP：
,I\RXIRUJHWWRFRQQHFWWKHVHUYRZLULQJ
GXULQJIXVHODJHDVVHPEO\RUWKHVHUYR
ZDV GLVFRQQHFWHG DQ DODUP FDQ EH
DFWLYDWHGDWWKHWUDQVPLWWHU
ŏ&RQQHFWLRQHUURUGLVSOD\
Forgotten wiring
alarm.
104 ＜ Linkage Menu ＞
9DULRXVWHOHPHWU\VHQVRUVVHWWLQJ
The telemetry sensor slot number and which sensor
is used in each slot can be changed in this screen.
Since the sensor in each slot is determined at
LQLWLDOL]DWLRQDQGWKHVDPHVORWQXPEHULVPHPRUL]HG
even for sensors sold separately, sensors can be
used by simply connecting them to S.BUS2. When
FXVWRPL]LQJ WKH VHQVRUV \RXUVHOI SHUIRUP WKH
settings in this screen.
*Three slots of altitude sensor are used.
(LJKWVORWVRI*36VHQVRUDUHXVHG
[What is a slot?]
Servos are classified by CH, but sensors are
classified in units called “slot”. There are slots
from #1 to #31.
Altitude sensors, GPS sensors and other data
sensor units may use multiple slots.
By the sensor which uses two or more slots,
the required number of slots is automatically
assigned by setting up a start slot.
When 2 or more of the same kind of sensor
are used, the sensors themselves must allocate
XQXVHGVORWVDQGPHPRUL]HWKDWVORW
ŏ7RXFKWKH>6HQVRU@EXWWRQLQWKH/LQNDJH0HQXWR
FDOOWKHVHWXSVFUHHQVKRZQEHORZ
ŏ6HQVRU,' ,WLVXQQHFHVVDU\ZKHQXVLQJHYHU\RQH
ŏ5HWXUQWR/LQNDJH0HQX
VHQVRURIVHYHUDONLQGVPD\VWLOOEHVXIÀFLHQW
$,53/$1(
6HQVRU
＜ Assignable slot ＞
$OWLWXGHVHQVRUV*36VHQVRUVDQGRWKHUGDWDVHQVRUXQLWVPD\XVHPXOWLSOHVORWV
*The sensor which uses two or more slots has restriction in a start slot.
Sensor
The required
number of slots
The number which can be used as a start slot
TEMP (SBS-01T,
SBS-01TE)
RPM (SBS-01RM,
SBS-01RO, SBS01RB)
1slot
1 ∟ 31
1slot
1 ∟ 31
Voltage (SBS-01V)
2slot
Altitude (SBS-01/02A)
3slot
Current (SBS-01C)
3slot
S.BUS2 Servo sensor
(SBS-01S)
GPS(SBS-01G)
TEMP125-F1713
8slot
1slot
VARIO-F1712
2slot
VARIO-F1672
2slot
6slot
CURR-F1678
3slot
GPS-F1675
Kontronik ESC
ROXXY
8slot
8slot
5slot
JetCat V10
14slot
PowerBox
16slot
1,2,3,4,5,6,8,9,10,11,12,13,14,16,17,18,19,
20,21,22,24,25,26,27,28,29,30
1,2,3,4,5,8,9,10,11,12,13,16,17,18,19,20,21,
24,25,26,27,28,29
1,2,3,4,5,8,9,10,11,12,13,16,17,18,19,20,21,
24,25,26,27,28,29
1,2,8,9,10,16,17,18,
24,25,26
8,16,24
1 ∟ 31
1,2,3,4,5,6,8,9,10,11,12,13,14,16,17,18,19,
20,21,22,24,25,26,27,28,29,30
1,2,3,4,5,6,8,9,10,11,12,13,14,16,17,18,19,
20,21,22,24,25,26,27,28,29,30
1,2,3,4,5,8,9,10,11,12,13,16,17,18,19,20,21,
24,25,26,27,28,29
8,16,24
8,16,24
1,2,8,9,10,16,17,18,24,25,26
1,2,3,4,5,6,7,8,9,10,11,12,13,14,15,16,17,
18
8,16
Selling area
Global
+(/,&237(5
9ROWDJH
*/,'(5
9ROWDJH
Europe
＜ Linkage Menu ＞ 105
Next explanation is required when using two or more the same kind of sensors.
【Example 1
Altitude sensor × 1, Temperature sensor × 1】
A setup is unnecessary. Two sensors are packed by HUB and it connects with S.BUS2 of a receiver.
【Example 2
Altitude sensor × 1, Temperature sensor × 2】
It is unnecessary to set up one altitude sensor and one temperature sensor. Sensor registration is required for
two temperature sensors.
Sensor unit registration
The sensor unit of each transmitter slot is registered and the slot
number of each sensor unit is changed automatically.
T18MZ
Hub
or Y-adapter
Sensor
$,53/$1(
*/,'(5
 ,QVHUW D WZRZD\ FRUG VXFK DV D GXDO VHUYR H[WHQVLRQ
)870 LQWRWKH6%86VHWWLQJFRQQHFWLRQLQWKHUHDURI
WKH70=:&&RQQHFWDEDWWHU\WRRQHSRUWRIWKHWZR
ZD\FRUGDQGWKHQLQVHUWWKHVHQVRUWREHUHJLVWHUHGLQWRWKH
RWKHU
2SHQWKHVHQVRUXQLWVHWWLQJVFUHHQE\WRXFKLQJWKH>6HQVRU@
EXWWRQLQWKH/LQNDJH0HQX
  7RXFK WKH  WR HQWHU WKH VHFRQG SDJH RI WKH 6HQVRU
VFUHHQ7KHQWRXFKWKH>5HJLVWHU@EXWWRQ
,IUHJLVWUDWLRQLVVXFFHVVIXOWKHIROORZLQJVFUHHQZLOODSSHDU
"The registering succeeded."&ORVHWKHPHVVDJHE\WRXFKLQJ
WKH>&ORVH@EXWWRQ
,IUHJLVWUDWLRQIDLOHGDVFUHHQOLNHWKHIROORZLQJZLOODSSHDU
"There are not enough available slots"
6RPH VHQVRUV UHTXLUH PXOWLSOH FRQWLQXRXV VORWV IRU WKHLU
RSHUDWLRQ)RUH[DPSOHVORWV,IFRQWLQXRXVVORWVDUHQRW
DYDLODEOH WKHVH VHQVRUV ZLOO QRW EH UHJLVWHUHG DFFRUGLQJO\
,IWKHUHDUHXQXVHGVORWVEXWWKH\DUHQRWFRQWLQRXVSOHDVH
XVH WKH 6HQVRU 8QLW 5HDOORFDWLRQ IHDWXUH ZKLFK IROORZV WR
FKDQJHWKHVORWVRIWKHH[LVWLQJVHQVRUVWRDFFRPPRGDWHWKH
VHQVRUVZKLFKUHTXLUHFRQWLQXRXVVORWV
$OWLPHWHUVORWVUHTXLUHG
*36VORWVUHTXLUHG
"The connected sensor is not ready"
1RUHVSRQVHIURPVHQVRUXQLW&KHFNWKHFRQQHFWLRQV
Receiver battery
Sensor unit reallocation
106 ＜ Linkage Menu ＞
Hub
Sensor
Sensor
Hub
Sensor
Sensor
Hub
Sensor
 7R SURSHUO\ UHDOORFDWH WKH VORWV LW LV QHFHVVDU\ WR FRQQHFW
DOOUHJLVWHUHGXQLWVWRWKH6%86FRQQHFWLRQLQWKHUHDURIWKH
WUDQVPLWWHU$GGLWLRQDOO\LWLVQHFHVVDU\WRFRQQHFWDEDWWHU\
WRWKHVHVHQVRUXQLWVYLDDZD\KXERUWZRZD\FRUG
2SHQWKHVHQVRUXQLWVHWWLQJVFUHHQE\WRXFKLQJWKH>6HQVRU@
EXWWRQLQWKH/LQNDJH0HQX
 7RXFK WKH  WR HQWHU WKH VHFRQG SDJH RI WKH VHWWLQJ
VFUHHQ7KHQWRXFKWKH>5HORFDWH@EXWWRQ
,WZLOOWDNHWLPHLIPDQ\VHQVRUVDUHFRQQHFWHG:DLWWKHQ
,IUHDOORFDWLRQZDVVXFFHVVIXODVFUHHQOLNHWKHIROORZLQJZLOO
DSSHDU
"All sensors are relocated successfully"
,IDOOWKHUHJLVWHUHGVHQVRUVDUHQRWFRQQHFWHGWKHIROORZLQJ
PHVVDJHLVGLVSOD\HGDQGUHDOORFDWLRQLVQRWSHUIRUPHG6HW
VORWVDOORFDWHGWRXQXVHGVHQVRUVWR>,QKLELW@RQWKHVHQVRUXQLW
VHWWLQJVFUHHQ
"Some sensors of the registered sensors cannot be found."
T18MZ
Sensor
+(/,&237(5
This function is used to reallocate slots to ensure that all sensors are
registered and operate as desired. As noted above, some sensors
require adjoining, or continuous, slots in order to register properly.
([DPSOHVRIVXFKVHQVRUVLQFOXGHEXWDUHQRWOLPLWHGWRDOWLPHWHUV
DQG*36XQLWV
Receiver battery
(3.7-7.4V)
Next explanation is required when using two or more the same kind of sensors.
Sensor unit setting reread
This function rereads the slot number setting of the
connected sensor units. This is a convenient way to allow
another T18MZ-WC user to pilot your aircraft.
&RQQHFWDOOUHJLVWHUHGXQLWVWRWKH6%86FRQQHFWLRQ
LQ WKH UHDU RI WKH WUDQVPLWWHU $GGLWLRQDOO\ LW LV
QHFHVVDU\WRFRQQHFWDEDWWHU\WRWKHVHVHQVRUXQLWV
YLDDZD\KXERUWZRZD\FRUG
2SHQWKHVHQVRUXQLWVHWWLQJVFUHHQE\WRXFKLQJWKH
>6HQVRU@EXWWRQLQWKH/LQNDJH0HQX
 7RXFK WKH  WR HQWHU WKH VHFRQG SDJH RI WKH
VHWWLQJVFUHHQ7KHQWRXFKWKH>5HUHDG@EXWWRQ
,IUHUHDGZDVVXFFHVVIXODVFUHHQOLNHWKHIROORZLQJLV
GLVSOD\HG
7KHUHORDGLQJWKHFRQÀJXUDWLRQRIVHQVRUVVXFFHHGHG
$,53/$1(
T18MZ
Hub
Receiver battery
(3.7-7.4V)
*/,'(5
Sensor
Sensor
Sensor
Hub
Sensor
Sensor
Sensor
Hub
■ The procedure described below is in 2/2 of the sensor screens.
ŏ &DOO WKH IROORZLQJ VHWWLQJ VFUHHQ E\ SUHVVLQJ WKH
>@EXWWRQRIWKHVHQVRUGLVSOD\
ŏ6HQVRUXQLWVHWWLQJUHUHDG
ŏ6HQVRUXQLWUHDOORFDWLRQ
ŏ6HQVRUXQLWUHJLVWUDWLRQ
ŏ&KDQJLQJWKHVORWQXPEHU
＜ Linkage Menu ＞ 107
+(/,&237(5
ŏ5HWXUQWR/LQNDJH0HQX
Next explanation is required when using two or more the same kind of sensors.
It is necessary where a sensor is registered manually here.
This item is unnecessary if "Sensor unit registration" is performed.
Procedure for changing the slot number of each sensor
unit
T18MZ
Hub
or Y-adapter
Sensor
$,53/$1(
6HOHFW>6HQVRU@RQSDJHRIWKH/LQNDJH0HQX
 &DOO SDJH  E\ SUHVVLQJ >@ DQG SUHVV >&KDQJH
6ORW@
 &RQQHFW WKH UHFHLYHU EDWWHU\ DQG WKH VHQVRU XQLW
WR WKH 6,) FRQQHFWRU EHKLQG WKH UHDU FRYHU RI WKH
WUDQVPLWWHUXVLQJDZD\KXERUZD\FRUG
 3UHVV WKH >5HDG@ NH\ 7KH FXUUHQW VORW QXPEHU LV
GLVSOD\HG
:KHQDQXPEHULVSUHVVHGWKH> △ @> ▽ @> △ △ @
DQG> ▽ ▽ @NH\VDSSHDU1RZFKDQJHWKHGHVLUHG
QXPEHU
:KHQWKH>:ULWH@NH\LVSUHVVHGWKHGHVLUHGQXPEHU
LVZULWWHQWRWKHVHQVRU
*/,'(5
ŏ&DOO WKLV VFUHHQ E\ VZLWFKLQJ WR SDJH  E\
SUHVVLQJ WKH >@ EXWWRQ RQ WKH 6HQVRU
VFUHHQDQGWKHQSUHVVLQJ>&KDQJH6ORW@
Receiver battery
ŏ7KHVORWQXPEHULVZULWWHQWRWKHVHQVRU
+(/,&237(5
ŏ:KHQSUHVVHGWKHFXUUHQWVORW
QXPEHULVGLVSOD\HG
Procedure for changing the sensor of each slot number
6HOHFW>6HQVRU@IURPWKH/LQNDJH0HQX
6HOHFWWKHVHQVRURIWKHVORWQXPEHUWREHFKDQJHG
6HOHFWWKHW\SHRIGLVSOD\HGVHQVRU
:KHQWKH>6HQVRU1DPH@EXWWRQRIWKH/LQNDJH0HQX
ŏ5HWXUQWR/LQNDJH0HQX
*/,'(5
ŏ$UHJLVWHUHGVHQVRUXQLWLVGLVSOD\HG
Sensor name function
+(/,&237(5
 7RXFK WKH >6HQVRU 1DPH@ EXWWRQ LQ WKH /LQNDJH 0HQX WR RSHQ WKH
VHWWLQJVFUHHQ$OLVWRIVHQVRUXQLWVLVGLVSOD\HG
6HOHFWWKHW\SHRIVHQVRUXQLWIRUZKLFKWKHQDPHLVWREHFKDQJHG$
QDPHFKDQJHVFUHHQDSSHDUV:KHQPXOWLSOHVHQVRUXQLWVRIWKHVDPH
W\SH DUH UHJLVWHUHG WKH >6ORW@ EXWWRQ LV GLVSOD\HG 6HOHFW WKH VORW WR
ZKLFKWKHVHQVRUXQLWZKRVHQDPHLVWREHFKDQJHG
7RXFKWKH>5HQDPH@EXWWRQ$FKDUDFWHULQSXWVFUHHQDSSHDUV,QSXW
WKHQHZQDPH 8SWRFKDUDFWHUV
,IVRGHVLUHGWKHVHQVRUQDPHFDQEHUHWXUQHGWRWKHGHIDXOWE\
SUHVVLQJWKH>5HVHW@EXWWRQ
110 ＜ Linkage Menu ＞
7HOHPHWU\6HWWLQJ
'DWDORJJLQJRIWHOHPHWU\7XUQV212))WKHWHOHPHWU\DODUP
Telemetry data has been adapted to the log function
which is recorded at the SD card.
ŏ7RVZLWFKVHOHFWVFUHHQ
7XUQV212))WKHWHOHPHWU\DODUP
$OOWHOHPHWU\DODUPVVWRS
Setting method
2SHQWKHOLQNDJHPHQX7HOHPHWU\/RJVFUHHQ
/RJUHFRUGLQJFDQEHVWDUWHGDQGVWRSSHGE\
RSHUDWLQJDVZLWFK7KH/RJ6WDUW6WRSVZLWFKLV
VHOHFWHG
7KHORJRXWSXWLQWHUYDOFDQEHVHW
 7KH GDWD WR EH UHFRUGHG LV XSGDWHG DW WKH
WLPH VHW E\ /LQNDJH 0HQXń6\VWHP 7\SH
VFUHHQ'/,QWHUYDO)RUH[DPSOHZKHQWKHORJ
RXWSXWLQWHUYDOLVVHFRQGDQGWKH'/LQWHUYDO
LVVHFRQGVWKHVDPHGDWDLVRYHUODSSHGDQG
UHFRUGHGWZLFH
Operation method
,QVHUWWKH6'FDUGLQWRWKHFDUGVORW
6HWWKHVZLWFKVHWE\/RJ6WDUW6WRS6ZLWFKWR
21 $ EHHS VRXQGV DQG D ORJ ILOH LV FUHDWHG
DQGUHFRUGLQJRIWKHWHOHPHWU\GDWDEHJLQV
Absolutely never remove the SD card while
log data is being recorded.
 6HW WKH VZLWFK VHW E\ /RJ 6WDUW6WRS 6ZLWFK
WR 2)) $ EHHSLQJ VRXQG LV JHQHUDWHG DQG
UHFRUGLQJRIWKHWHOHPHWU\GDWDVWRSV
7XUQRIIWKHWUDQVPLWWHUSRZHUDQGUHPRYHWKH
6'FDUG
ʄ /RJÀOH
$ ORJ ILOH LV FUHDWHG LQ WKH 6' FDUG /2*
IROGHU 7ZR ILOHV ZLWK WKH VDPH ILOHQDPH EXW
D GLIIHUHQW H[WHQVLRQ DUH FUHDWHG ([DPSOH
)/,)/'
ʄ([WHQVLRQ)/,6ORWDOORFDWLRQLQIRUPDWLRQÀOH
ʄ([WHQVLRQ)/'/RJGDWDÀOH
:KHQ FRS\LQJ RU PRYLQJ D ORJ ILOH DOZD\V
VHOHFWERWKWKH)/,ÀOHDQG)/'ÀOH
/RJ ÀOHV FDQ EH FRQYHUWHG WR &69 IRUPDW E\
using the telemetry log converter available at
the Futaba website.
ʄNotes
◇ $OWLPHWHU DOWLWXGH GDWD DQG *36 GLVWDQFH
DQG DOWLWXGH GDWD RXWSXW ZLWK WKH SRLQW WKDW
WLPH ORJJLQJ VWDUWHG DV WKH UHIHUHQFH P 
:KHQWKHWUDQVPLWWHUSUHVHWSRVLWLRQDQGWKH
ORJVWDUWSRVLWLRQDUHGLIIHUHQWWKHWUDQVPLWWHU
GLVSOD\ DQG WKH ORJ GDWD GLVSOD\ ZLOO DOVR EH
GLIIHUHQW 7KH DOWLWXGH DQG GLVWDQFH IURP WKH
WDNHRIISRVLWLRQFDQEHUHFRUGHGE\VWDUWLQJ
ORJJLQJLPPHGLDWHO\DIWHUWDNHRII
◇ 7KH WUDQVPLWWHU JHDU UDWLRQXPEHU RI ILQV
QXPEHU RI SROHV VHWWLQJ LV QRW UHIOHFWHG LQ
WKH VSHHGRPHWHU ORJ GDWD VSHHG  0XOWLSO\
WKHJHDUUDWLRRUQXPEHURIÀQVE\WKHVSHHG
GDWD
◇ :KHQ WKH 6' FDUG EHFRPHV IXOO UHFRUGLQJ
VWRSVDQGGRHVQRWUHVXPHHYHQLIORJJLQJLV
UHVWDUWHG
＜ Linkage Menu ＞ 111
+(/,&237(5
ŏ5HWXUQWR/LQNDJH0HQX
*/,'(5
$,53/$1(
ŏ7RXFKWKH>7HOHPHWU\6HWWLQJ@EXWWRQLQWKH/LQNDJH
0HQX  WRFDOOWKHVHWXSVFUHHQVKRZQEHORZ
6HWWLQJRIZDUQLQJVRXQGDQGYLEUDWLRQ
:DUQLQJ
A warning upon powering up your transmitter can be
set up for the following functions.
Default setting is ON. Leave ON any function that
you feel is dangerous upon power up. that you feel is
dangerous upon power up.
The alarm is stopped at power up if the function is
changed to OFF.
* If a throttle stick turns on a power supply at full
throttle as in the case of the electric craft, it may
begin to turn the prop at high rotation suddenly,
and this is very dangerous. We recommend you set
the throttle position warning to ON.
$,53/$1(
ŏ7RXFKWKH>:DUQLQJ@EXWWRQLQWKH/LQNDJH0HQX 
WRFDOOWKHVHWXSVFUHHQVKRZQEHORZ
ŏ5HWXUQWR/LQNDJH0HQX
*/,'(5
ŏ,IWKLVLVWXUQHGRQWKHDODUPZLOOEHDYLEUDWLRQLQWKH
WUDQVPLWWHUZKHQ\RXSRZHURQWKHUDGLR
ŏ,I WKLV LV FKDQJHG WR RII DODUP ZLOO QRW VRXQG
GXULQJSRZHULQJXSRI\RXUWUDQVPLWWHU
ŏ,I D WKURWWOH VWLFN LV DERYH ORZ WKURWWOH ZKHQ \RX SRZHU RQ \RXU
WUDQVPLWWHUWKHQH[WVFUHHQZLOODSSHDUDQGDQDODUPZLOOVRXQG
'DWD5HVHW@EXWWRQLQWKH/LQNDJH0HQX
WRFDOOWKHVHWXSVFUHHQVKRZQEHORZ
Data Resetting
7RXFKWKHGHVLUHGEXWWRQWRUHVHWWKHGDWD
 3HUIRUP WKH GDWD UHVHW DFFRUGLQJ WR WKH
LQVWUXFWLRQV GLVSOD\HG RQ WKH VFUHHQ  :KHQ
FRPSOHWH WRXFK WKH GDWD UHVHW EXWWRQ WR
H[LW
WARNING
Default setting of the motor channel will be
reversed once a reset is complete.
＜ Linkage Menu ＞ 113
+(/,&237(5
*/,'(5
ŏ5HWXUQWR/LQNDJH0HQX
&RQGLWLRQ+ROG
&RQGLWLRQKROGIXQFWLRQ +HOLFRSWHURQO\
$,53/$1(
7KLV IXQFWLRQ PD\ EH XVHG WR OLPLW WKH PD[LPXP
speed of the engine so that you may adjust flight
conditions when the engine is running. An alarm
indicates that the function is operating. It will
prevent the engine from racing dangerously when
adjusting the Idle-Up settings.
While this function is active, the throttle servo
SRVLWLRQLVÂż[HGDWWKHSRLQWWKDW\RXKDYHLQGLFDWHG
when the function is activated. You must deactivate
this function when you are through making
adjustments.
The system will not allow you to activate/deactivate
this function in either of the following states:
‡ :KHQ DQ\ RI WKH IOLJKW FRQGLWLRQ VZLWFKHV
DUHRQ
‡ :KHQ WKH WKURWWOH VWLFN LV KLJKHU WKDQ WKH
SRLQW
*/,'(5
+(/,&237(5
114 ＜ Linkage Menu ＞
To activate/deactivate Condition hold:
(Home screen)
6HWWKHWKURWWOHVWLFNORZHUWKDQWKHSRLQW
3XVKWKHGLUHFWNH\6 &RQG+ROG WRDFWLYDWH
WKHFRQGLWLRQKROGIXQFWLRQ
:KHQ WKLV IXQFWLRQ LV DFWLYH &RQGLWLRQ +ROG LV
DFWLYHDSSHDUVRQWKHVFUHHQ
(LINKAGE menu/MODEL menu)
6HWWKHWKURWWOHVWLFNORZHUWKDQWKHSRLQW
 3XVK WKH ,1+ RU WKH GLUHFW NH\ 6  EXWWRQ WR
DFWLYDWHWKHFRQGLWLRQKROGIXQFWLRQ
2SHUDWLRQLVGLVSOD\HGDWWKHERWWRPRIWKHPHQX
)XQFWLRQ2121LVGLVSOD\HG
)XQFWLRQ2)),1+LVGLVSOD\HG
02'(/0(18 &20021)81&7,216
Note: The T18MZ-WC is designed so that the airplane
and glider (including EP glider) model types are
compatible with fuselages of similar type wings.
This section outlines the relationship between the
functions common to airplanes and gliders, except
some dedicated functions, and model type.
The setting items depend on the number of servos
and other differences according to the wing type
used, but reread them. The setup screens in the
instruction manual are typical examples.
$,53/$1(
This section describes the AFR, program mixing,
and other functions common to all model types.
Before setting the model data, use the Model Type
function of the Linkage Menu to select the model
type matched to the fuselage. When another model
type is selected thereafter, the AFR, program mixing,
and other setting data are reset.
The functions in the Model Menu can be set for each
ÀLJKWFRQGLWLRQ:KHQ\RXZDQWWRXVHWKHV\VWHPE\
VZLWFKLQJWKHVHWWLQJVIRUHDFKFRQGLWLRQE\VZLWFK
stick position, etc., use the Condition Select function
WRDGGÀLJKWFRQGLWLRQV 8SWRFRQGLWLRQVFDQEH
used)
ŏ7RXFKWKH0RGHO0HQXEXWWRQRIWKH+RPHVFUHHQWRFDOOWKH
Model Menu.
ŏ:KHQWKHEXWWRQRIWKHIXQFWLRQ\RXZDQWWRVHWLVWRXFKHGD
setup screen appears.
ŏ5HWXUQWR+RPHVFUHHQ
*/,'(5
ŏ7RQH[W
page
(Model Menu screen example)
*The Model Menu screen depends on the model type. This screen is for model type Airplane Wing Type 4AIL+4FLP.
Ɣ6HUYR0RQLWRU
Ɣ3URJ0L[HV
6HUYR WHVW DQG VHUYR SRVLWLRQ GLVSOD\ )RU D
description of its functions, see the Linkage Menu
section.)
3URJUDPPL[LQJZKLFKFDQEHIUHHO\FXVWRPL]HG8S
to 10 mixes can be used for each condition.
Ɣ&RQGLWLRQ6HOHFW
0L[LQJXVHGLQQHHGOHDGMXVWPHQWRIHQJLQHVZKLFK
use a fuel mixture control carburetor. [Airplane,
helicopter]
Flight conditions addition, deletion, copy, condition
renaming, and condition delay can be set.
Ɣ)XHO0L[WXUH
Ɣ$)5 '5
Sets the rudder angle and curve of all the operation
IXQFWLRQV$'5FXUYHZKLFKFDQEHVZLWFKHGZLWKD
VZLWFKHWFFDQDOVREHDGGHG
＜ Model Menu (Common Functions) ＞ 115
+(/,&237(5
0RGHO0HQXIXQFWLRQV &RPPRQ WDEOH
&RQGLWLRQ6HOHFW
Flight conditions addition, deletion, copy, condition renaming, and
FRQGLWLRQGHOD\FDQEHVHW>$OOPRGHOW\SHV@
The functions in the Model Menu can be used by
VZLWFKLQJ WKH VHWWLQJV RI XS WR  IOLJKW FRQGLWLRQV
E\XVLQJWKH&RQGLWLRQ6HOHFWIXQFWLRQWRDGGÀLJKW
conditions. Add conditions, as required.
:KHQ\RXGRQRWZDQWWRXVHWKH&RQGLWLRQ6HOHFW
function, this setting is unnecessary. In this case, use
WKHÀLJKWFRQGLWLRQV &RQGLWLRQ DVVLJQHGDWLQLWLDO
setting.
$,53/$1(
ŏ 6LQFH VZLWFKLQJ E\ VWLFN DQG OHYHU SRVLWLRQ LQ
addition to ordinary toggle switch, is possible
as the flight condition selector switch, this
IXQFWLRQFDQEHOLQNHGZLWKRWKHURSHUDWLRQV
ŏ $ &RQGLWLRQ 'HOD\ IXQFWLRQ FDQ EH VHW
Unnecessary fuselage motion generated
when there are sudden changes in the servo
positions and when there are variations in
the operating time between channels during
condition switching can be suppressed. The
delay can be set for each channel.
When setting the delay function at the
switching destination condition, the related
function changes after a delay corresponding
to the set amount.
ŏ :KHQ PXOWLSOH FRQGLWLRQV DUH VHW WKHLU
operation priority can be freely changed.
ŏ 7KH FRQGLWLRQ QDPH FDQ EH FKDQJHG 7KH
selected condition name is displayed on the
screen. When a condition has been added,
JLYHLWDQDPHZKLFKFDQEHHDVLO\FRQÀUPHG
ŏ 7RXFK WKH >&RQGLWLRQ 6HOHFW@ EXWWRQ LQ WKH 0RGHO
Menu to call the setup screen shown below.
ŏ5HWXUQWR0RGHO0HQX
(Currently selected condition name)
(Conditions List)
*/,'(5
3ULRULW\FKDQJH
1. Touch the condition whose priority
you want to change in Conditions
List.
2. Change the priority with the
SULRULW\> @RU> @EXWWRQ 7KHODVW
condition has the highest priority.)
*The initial setting condition cannot
be moved. It has the lowest
priority.
+(/,&237(5
&RQGLWLRQ$GGLWLRQ
:KHQWKH>$GG@EXWWRQLVWRXFKHGWKH
&RQGLWLRQ6HOHFWVFUHHQDSSHDUV
*Only the number of buttons
corresponding to the conditions which
can be added are displayed.
6HOHFWWKHGHVLUHGFRQGLWLRQVE\
touching the buttons.
*The selected conditions are added to
Conditions List.
7RXFKWKH>18//@EXWWRQWRFDOOWKH
6ZLWFK!VFUHHQ
6HOHFWWKHVZLWFKWREHXVHGLQFRQGLWLRQ
switching.
(For a description of the switch selection
method, see next page.)
5. The "Condition 1" data for the added
conditions is copied.
116 ＜ Model Menu (Common Functions) ＞
ŏ&RQGLWLRQGHOD\
setting
(For a description of
the setting method,
see the next page.)
&RQGLWLRQ5HVHW
6HOHFWWKHFRQGLWLRQ
by touching the
condition you want
to reset in Conditions
List.
7RXFKWKH>5HVHW@
button.
:KHQWKH>1R@
button.)
&RQGLWLRQ5HQDPLQJ
6HOHFWWKHFRQGLWLRQE\
touching the condition
you want to rename in
Conditions List.
7RXFKWKH>5HQDPH@
button.
3. Enter the new name from
WKHNH\ERDUGZKLFK
appears on the screen.
:KHQWKHNH\ERDUG
>5HWXUQ@NH\LVWRXFKHG
the new name is
registered. (To abort
registration, touch the
>(6&@NH\
&RQGLWLRQ&RS\
7RXFKWKH>&RS\@EXWWRQ7KH&RS\VFUHHQDSSHDUV
6HOHFWWKHFRQGLWLRQE\WRXFKLQJWKHEXWWRQRIWKHFRS\
source conditions.
1H[WVHOHFWWKHFRQGLWLRQE\WRXFKLQJWKHFRS\
destination condition.
7RXFKWKH>&23<@EXWWRQ
:KHQWKH>1R@EXWWRQ
&RQGLWLRQVZLWFKVHWWLQJDQG212))GLUHFWLRQVZLWFKLQJ
(Currently selected condition name)
*/,'(5
ŏ 7RXFK WKH >'HOD\@ EXWWRQ RQ WKH &RQGLWLRQ
6HOHFW VFUHHQ WR FDOO WKH &RQGLWLRQ 'HOD\
screen shown below.
ŏ5HWXUQWR&RQGLWLRQ
6HOHFWVFUHHQ
$,53/$1(
)RUDGHVFULSWLRQRIWKHVHOHFWLRQPHWKRGVHH>6ZLWFK6HWWLQJ0HWKRG@DW
the back of this manual.
&RQGLWLRQGHOD\VHWWLQJ
ŏ*URXSVLQJOHPRGHVZLWFKLQJ *U6QJO
(For a description of the operation method,
VHHWKHGHVFULSWLRQDWWKHEDFNRIWKLVPDQXDO
+(/,&237(5
6ZLWFKWRWKHFRQGLWLRQ\RXZDQWWRVHW
7RXFKWKH'HOD\EXWWRQRIWKHFKDQQHO\RXZDQWWRVHW
3. Use the adjustment buttons to set the delay.
ŏ,QLWLDOYDOXH
ŏ$GMXVWPHQWUDQJHa PD[LPXPGHOD\
＜ Model Menu (Common Functions) ＞ 117
$)5 '5 
7KHUXGGHUDQJOHDQGFXUYHRIHDFKRSHUDWLRQIXQFWLRQFDQEHVHW$'5FXUYH
ZKLFKFDQEHVZLWFKHGE\VZLWFKHWFFDQDOVREHDGGHG>$OOPRGHOW\SHV@
$,53/$1(
$)5 IXQFWLRQ LV XVHG WR DGMXVW WKH WKURZ DQG
RSHUDWLRQ FXUYH RI WKH VWLFN OHYHU DQG VZLWFK
IXQFWLRQV &+WR&+ IRUHDFKÀLJKWFRQGLWLRQ
7KLV LV QRUPDOO\ XVHG DIWHU (QG 3RLQW $79  KDV
GHILQHGWKHPD[LPXPWKURZGLUHFWLRQV (QG3RLQW
DFWVRQ$//ÀLJKWFRQGLWLRQVHWWLQJV :KHQPL[LQJ
is applied from one channel to another channel,
both channels can be adjusted at the same time
by adjusting the operation rate through the AFR
function.
6HWWLQJPHWKRG
ŏ 2SHUDWLRQ FXUYH DGMXVWPHQW 6L[ W\SHV RI
FXUYHV OLQHDU(;3(;3975OLQHDQGVSOLQH 
FDQEHVHOHFWHG$PD[LPXPSRLQWVFXUYH
can be used for the line and spline curve
W\SHV ,QLWLDO VHWWLQJ  SRLQWV  7KH QXPEHU RI
points can also be increased and decreased
and curves from complex curves to simple
curves can be used.
ŏ 2SHUDWLRQ VSHHG DGMXVWPHQW 7KH RSHUDWLRQ
speed of each function when the function
is operated (including at flight condition
switching) can be adjusted. The function
operates smoothly at a constant speed
corresponding to the set speed.
ŏ7RXFKWKH>$)5 '5 @EXWWRQLQWKH0RGHO0HQXWRFDOO
the setup screen shown below.
&XUUHQWO\VHOHFWHGUDWHQDPH$)5'5a
)XQFWLRQVHOHFWLRQ
1. When the function select button is touched, a selection screen appears.
6HOHFWWKHIXQFWLRQ\RXZDQWWRVHWDWWKHVHOHFWLRQVFUHHQ
ŏ*URXSVLQJOHPRGHVZLWFK *U6QJO
*/,'(5
)RUPRUHLQIRUPDWLRQVHHWKHGHVFULSWLRQDWWKHEDFNRIWKLVPDQXDO
ŏ5HWXUQWR0RGHO0HQX
+(/,&237(5
7RWDOQXPEHURI$)5
DQG'5FXUYHV
set in the currently
selected condition)
(Currently selected condition name)
ŏ2SHUDWLRQFXUYHVHWWLQJ
(For a description of the setting method, see the
GHVFULSWLRQDWWKHEDFNRIWKLVPDQXDO
6FUHHQPRGHVZLWFKLQJ
ŏ6HUYRVSHHGVHWWLQJ
(For a description of the setting
method, see the description at
WKHEDFNRIWKLVPDQXDO
When setting the D/R function, the screen display mode
can be changed. Each time the button is touched, the mode
LVVZLWFKHG
ŏ'5IXQFWLRQVHWWLQJ
118 ＜ Model Menu (Common Functions) ＞
>6QJO@ LQLWLDO VHWWLQJ  2QO\ WKH FXUUHQWO\ RSHUDWLQJ
curve is displayed.
7KH$)5DQG'5FXUYHVVHWDWWKHFXUUHQWO\RSHUDWLQJ
condition are displayed.
>$OO &RQG@ 7KH $)5 FXUYH VHW DW DOO FRQGLWLRQV LV
displayed.
>6HOHFWHG$)5@7KHVHOHFWHGIXQFWLRQLVGLVSOD\HG
6HWWLQJPHWKRG
8SWRGXDOUDWHVFDQEHVHWIRUHDFKFRQGLWLRQ
ŏ 7RXFK WKH >'5@ EXWWRQ IURP WKH $)5 '5 
screen of the function (ailerons, elevators,
etc.) whose dual rate you want to set. The
'5OLVWVFUHHQVKRZQEHORZLVGLVSOD\HG7RXFK
the (function) button of the dual rate number
to be assigned. That rate is automatically
assigned to that function.
ŏ 1H[W VHOHFW WKH VZLWFK DQG LWV 212))
directions.
'5 'XDO5DWH LVVHWIRUHDFKFRQGLWLRQDQGLVQRWUHÀHFWHG
at other conditions.
'5 'XDO5DWH DWWKHWRSRIWKH'5OLVWKDVSULRULW\
&ORVH
6WDUW'5
ŏ7RVWDUW'5
WRXFKWKH>,1+@
button.
ŏ:KHQWKHDLOHURQEXWWRQLVWRXFKHGWKHV\VWHP
DVNVIRUD>1R@7RFKDQJHWKHIXQFWLRQ
VZLWFK WR WKH IXQFWLRQ VHOHFWHG DW WKH $)5
VFUHHQE\DQVZHULQJ>&ORVH@EXWWRQ
)XQFWLRQFKDQJH
$,53/$1(
'XDO5DWHVHWWLQJ
1DPLQJ'5
6ZLWFKVHWWLQJ
7RXFKWKH>18//@EXWWRQ7KH
6ZLWFK!VFUHHQDSSHDUV
6HOHFW FRQÀUP WKHVZLWFKDQG
LWV21GLUHFWLRQ
6HWWLQJH[DPSOH
6LQFHWKHIXQFWLRQVVKRZQEHORZDUHXVHGLQVSHFLDO
W\SHVRIVHWXSV$)5 '5 FDQQRWEHFKRVHQ
*Aileron2, Aileron3, Aileron4
*Flap2, Flap4
5XGGHU
Throttle(Only helicopter)
Pitch
Camber
*\UR 58' *\UR $,/ *\UR (/(
*RYHUQRU
Mixture
*Elevator2
$)5 '5 FDQEHVHWXS
according to a wing type.
%XWWHUÁ\
ŏ5XGGHU212))E\VZLWFK
:KHQ'5LVXVHGE\XVLQJWKH
condition with the same switch,
another rudder angle can
be set.
＜ Model Menu (Common Functions) ＞ 119
+(/,&237(5
 7R QDPH '5 WRXFK WKH >'5@
EXWWRQ $ NH\ERDUG DSSHDUV RQ WKH
screen.
2. Enter the desired name from this
NH\ERDUGDQGUHJLVWHULWE\WRXFKLQJ
WKHNH\ERDUG>5HWXUQ@NH\7RFDQFHO
input and close the screen, touch the
>(6&@NH\
3URJ0L[HV
3URJUDPPL[LQJZKLFKFDQEHIUHHO\FXVWRPL]HG8SWRPL[LQJVFDQ
EHXVHGIRUHDFKFRQGLWLRQ>$OOPRGHOW\SHV@
$,53/$1(
Programmable mixing may be used to correct
undesired tendencies of the aircraft, and it may also
be used for unusual control configurations. Mixing
means that the motion of a command channel, called
the "master," is added to the motion of the mixed
channel, called "slave."
You may choose to have the Masters trim added to
WKH 6ODYH FKDQQHO UHVSRQVH LI \RX GHVLUH 7ULP
setting). The mixing curve can be changed so that
the undesired tendencies can be corrected effectively
by setting the LINEAR1/LINEAR2/EXP1/EXP2/
975/,1(63/,1(PRGHV7KH'HOD\IXQFWLRQFDQ
be programmed for each rate. The Delay is used to
FKDQJHWKHUDWHVPRRWKO\ZKHQVZLWFKLQJ3URJ0L[HV@EXWWRQLQWKH0RGHO0HQXWR
call the setup screen shown below.
ŏ5HWXUQWR0RGHO0HQX
*/,'(5
ŏ*URXSVLQJOHPRGHVZLWFKLQJ *U6QJO
0L[LQJEXWWRQV
After this function is activated, the
PDVWHUDQGVODYHIXQFWLRQQDPHV RU
offset mixing) are displayed.
ŏ6ZLWFKVHOHFWLRQ
)RUPRUHLQIRUPDWLRQVHHWKHGHVFULSWLRQDWWKHEDFNRI
this manual.)
ŏ0L[LQJPRGHFKDQJHEXWWRQ
(Curve-type
mixing)
+(/,&237(5
ŏ6HUYRVSHHGVHWWLQJ
ŏ2SHUDWLRQFXUYHVHWWLQJ
ŏ)LQHWXQLQJWULPVHWWLQJ
(Offset-type mixing)
(Timer mode)
1RUPDOPRGH
7LPHUPRGH
7KHRQWLPH VWDUWVWRSWLPH FDQEHVHWXSWR
seconds. It is useful for landing gear control of
the jet or scale plane, etc.
120 ＜ Model Menu (Common Functions) ＞
6HWWLQJPHWKRGV&XUYHPL[LQJ
*Each time this button is touched, it toggles between
>,1+@DQG>212))@
ŏ0L[LQJ 212)) VZLWFK VHWWLQJ DQG 212))
direction switching
$Q212))VZLWFKLVQRWVHWHYHQZKHQWKHIXQFWLRQ
is activated.
 :KHQ \RX ZDQW WR WXUQ PL[LQJ 212)) E\
VZLWFK WRXFK WKH >18//@ EXWWRQ WR FDOO WKH
6ZLWFK! VFUHHQ DQG WKHQ VHOHFW WKH VZLWFK
DQGLWV21GLUHFWLRQ
*For a description of the selection method, see
>6ZLWFK6HWWLQJ0HWKRG@DWWKHEDFNRIWKLVPDQXDO
ŏ0DVWHUFKDQQHOVHWWLQJ
1. Touch the Master button to call the Function
menu and select the master channel.
7ROLQNWKLVPL[LQJZLWKRWKHUPL[LQJWRXFKWKH
button at the left of the master channel and
VHOHFWOLQN
*Each time the button is touched, it toggles between
PL[LQJGLUHFWLRQDQGDQG1RGLVSOD\ QROLQN 
0DVWHUFKDQQHOFRQWUROFDQEHVHWWRVWLFN95DQG
RWKHUVLPSOHWUDYHOVZKLFKGRQRWLQFOXGH$79$)5
'5 PL[LQJ VHWWLQJ HWF ,Q WKLV FDVH GLVSOD\ WKH
6ZLWFK!VFUHHQE\WRXFKLQJWKH>+:@EXWWRQDQG
then select master channel side control.
ŏ6ODYHFKDQQHOVHWWLQJ
 7RXFK WKH 6ODYH EXWWRQ WR FDOO WKH )XQFWLRQ
menu and select the slave channel.
 7R OLQN WKLV PL[LQJ ZLWK RWKHU PL[LQJ WRXFK
the button at the right-hand side of the slave
FKDQQHODQGVHOHFWOLQN
*Each time this button is pressed, it toggles between
>21@DQG>2))@
7KLVLVHIIHFWLYHZKHQPDNLQJFRUUHFWLRQVZKHQWKH
fuselage is the same but the rudder angles are
substantially different.
ŏ0L[LQJFXUYHW\SHVHOHFWLRQ
1. Touch the curve type selection button of the
curve type you want to use to display the
selection screen and then select the curve
you want to use.
$,53/$1(
ŏ0L[LQJVHWXSVFUHHQVHOHFWLRQ
1. Touch the button of the mixing you want
to set. The mixing setup screen is displayed.
Activate the function.
 $FWLYDWH WKH IXQFWLRQ E\ WRXFKLQJ WKH >,1+@
button.
ŏ6ODYHFKDQQHO$)5PRGH 67.ń67.
 :KHQ /LQN LV VHW DW WKH VODYH VLGH DQG \RX
ZDQW WR DGG $)5 '5  WR WKH PL[LQJ UDWH
VHOHFW >21@ :KHQ \RX GR QRW ZDQW WR DGG
$)5 '5 WRWKHPL[LQJUDWHVHOHFW>2))@
*For a description of the curve setting method, see
WKHGHVFULSWLRQDWWKHEDFNRIWKLVPDQXDO
ŏ)LQHWXQLQJWULPVHWWLQJ
1. When using the curve fine tuning function,
WRXFK WKH >18//@ EXWWRQ RI WKH )LQH 7XQLQJ
LWHP WR FDOO WKH 6ZLWFK! VFUHHQ DQG WKHQ
VHOHFWWKHOHYHU95HWF\RXZDQWWRXVH
*For a description of the fine tuning trim setting
PHWKRG VHH WKH GHVFULSWLRQ DW WKH EDFN RI WKLV
manual.
ŏ6HUYRVSHHGVHWWLQJ
1. When setting the servo speed, touch the
6SHHGEXWWRQ7KH6HUYR6SHHGVHWXSVFUHHQ
is displayed.
*/,'(5
*Each time the button is touched, it toggles between
WKH*UDQG6QJOPRGHV
>21@DQG>2))@
*This is effective when the master channel is set by
Function.
*For a description of the servo speed setting method,
VHHWKHGHVFULSWLRQDWWKHEDFNRIWKLVPDQXDO
2IIVHWPL[LQJFKDQJHVWKHVSHHG8VHWKH6SHHG,Q
DQG6SHHG2XWEXWWRQVWRUHDGMXVWWKHVSHHG
The mixing switch can set a delay with a different
rate at starting and stopping.
*This function is inactive when a mixing switch is not
set.
ŏ7KHSURJUDPPDEOHPL[LQJ LQPL[LQJPRGH 67.
WR67.PL[LQJIXQFWLRQFDQEHXVHGHYHQZKHQ
WKH 0DVWHU IXQFWLRQ LV FRQWUROOHG E\ D VWLFN RU
other hardware.
*Each time the button is pressed, it toggles between
PL[LQJGLUHFWLRQDQGDQG1RGLVSOD\ QROLQN 
ŏ7ULPPRGH212))VHWWLQJ
7RWXUQWKHWULPPRGH212))WRXFKWKH7ULP
button on the screen.
*When mixing includes master side trim, set the Trim
EXWWRQ WR >21@ :KHQ PL[LQJ GRHV QRW LQFOXGH
PDVWHUVLGHWULPVHWWKH7ULPEXWWRQWR>2))@
*Each time this button is pressed, it toggles between
＜ Model Menu (Common Functions) ＞ 121
+(/,&237(5
ŏ*URXSVLQJOHPRGHVHOHFWLRQ
Activating functions for only the selected
FRQGLWLRQV
 7RXFK WKH *URXS EXWWRQ DQG VZLWFK WR WKH
6QJOPRGH
6HWWLQJPHWKRGV2IIVHWPL[LQJ
ŏ*URXSVLQJOHPRGHVHOHFWLRQ
Activating functions for only the selected
FRQGLWLRQV
 7RXFK WKH *URXS EXWWRQ DQG VZLWFK WR WKH
6QJOPRGH
*Each time the button is touched, it toggles between
WKH*UDQG6QJOPRGHV
$,53/$1(
ŏ0L[LQJPRGHVHOHFWLRQ
8VLQJWKHRIIVHWPRGH
1. Touch the Mode button and switch to the
Offset mode.
*For a description of the servo speed setting method,
VHHWKHGHVFULSWLRQDWWKHEDFNRIWKLVPDQXDO
2IIVHWPL[LQJFKDQJHVWKHVSHHG8VHWKH6SHHG,Q
DQG6SHHG2XWEXWWRQVWRUHDGMXVWWKHVSHHG
The mixing switch can set a delay with a different
rate at starting and stopping.
*This function is inactive when a mixing switch is not
set.
ŏ'HOD\VHOHFWLRQ
8VLQJWKHQRUPDOPRGH
*Each time the button is touched, it toggles between
the Mix and Offset modes.
*/,'(5
ŏ0L[LQJVHWXSVFUHHQVHOHFWLRQ
1. Touch the button of the mixing you want
to set. The mixing setup screen is displayed.
Activate the function.
 $FWLYDWH WKH IXQFWLRQ E\ WRXFKLQJ WKH >,1+@
button.
6:21 0,;6WDUW
6 ‫ڀ‬
*Each time this button is touched, it toggles between
>,1+@DQG>212))@
ŏ0L[LQJ 212)) VZLWFK VHWWLQJ DQG 212))
direction switching
$Q212))VZLWFKLVQRWVHWHYHQZKHQWKHIXQFWLRQ
is activated.
 :KHQ \RX ZDQW WR WXUQ PL[LQJ 212)) E\
VZLWFK WRXFK WKH >18//@ EXWWRQ WR FDOO WKH
6ZLWFK! VFUHHQ DQG WKHQ VHOHFW WKH VZLWFK
DQGLWV21GLUHFWLRQ
6:2)) 0,;6WRS
6 ‫ڀ‬
ŏ'HOD\VHOHFWLRQ
8VLQJWKHWLPHUPRGH
+(/,&237(5
*For a description of the selection method, see
>6ZLWFK6HWWLQJ0HWKRG@DWWKHEDFNRIWKLVPDQXDO
ŏ6ODYHFKDQQHOVHWWLQJ
 7RXFK WKH 6ODYH EXWWRQ WR FDOO WKH )XQFWLRQ
menu and select the slave channel.
ŏ)LQHWXQLQJWULPVHWWLQJ
:KHQXVLQJWKHÀQHWXQLQJIXQFWLRQWRXFKWKH
>+:18//@ EXWWRQ RI WKH )LQH 7XQLQJ LWHP WR
FDOOWKH6ZLWFK!VFUHHQDQGWKHQVHOHFWWKH
OHYHU95HWF\RXZDQWWRXVH
*For a description of the fine tuning trim setting
PHWKRG VHH WKH GHVFULSWLRQ DW WKH EDFN RI WKLV
manual.
ŏ6HUYRVSHHGVHWWLQJ
1. When setting the servo speed, touch the
6SHHGEXWWRQ7KH6HUYR6SHHGVHWXSVFUHHQ
is displayed.
122 ＜ Model Menu (Common Functions) ＞
6:21 0,;6WDUW
6 ‫ڀ‬
0,;6WRS
)XHO0L[WXUH
'HGLFDWHGPL[LQJXVHGLQQHHGOHDGMXVWPHQWRIHQJLQHVZKLFKXVHDIXHO
PL[WXUHFRQWUROFDUEXUHWRU>$LUSODQHKHOLFRSWHU@
This function is dedicated mixing used in needle
adjustment of an engine that uses a fuel mixture
control carburetor.
7KHQHHGOHFKDQQHOLVDVVLJQHGWR&+DVDGHIDXOW
ŏ7RXFKWKH>)XHO0L[WXUH@EXWWRQLQWKH0RGHO0HQXWR
call the setup screen shown below.
$,53/$1(
ŏ5HWXUQWR0RGHO0HQX
ŏ2SHUDWLRQFXUYHVHWWLQJ
*/,'(5
(For a description of the setting method, see the
GHVFULSWLRQDWWKHEDFNRIWKLVPDQXDO
&750 PRGH Maximum change near center by
FHQWHUWULPRSHUDWLRQ 'RHVQRWFKDQJHDWHQGRIWKH
VWLFNPRYHPHQW :KHQWKHDGMXVWPHQWUDQJH 5DQJH 
value is made small, trim is active only near the
center.
1250 PRGH 1RUPDO WULP OLQHDU  RSHUDWLRQ
When the adjustment range value is decreased, trim
LVDFWLYHRQO\QHDUWKHFHQWHU1HHGOHKLJKWULPZRUNV
as high trim based on the center. This operation is
similar to reverse ATL trim.
3. A needle throttle cut function can be set.
7KLVRSHUDWLRQFDQEHOLQNHGZLWKWKHWKURWWOH
hold functions (Cut and Idle), Throttle Cut
IXQFWLRQDQG,GOH'RZQ
7KHQHHGOHVLGHFXWSRVLWLRQFDQEHVHW6HWLW
to the fuel side full open position.
When MIX mode is selected, the throttle
curve setting becomes the master.
In the UNMIXPRGHWKHWKURWWOHVWLFNSRVLWLRQ
becomes the master.
1. An acceleration function can be set. This is
used when the mixture is either too rich or
too lean, which can be caused by sudden
RSHUDWLRQRIWKHWKURWWOHVWLFN
 7KH UHWXUQ WLPH DIWHU RSHUDWLRQ 'XPS  FDQ
EHVHWIRUERWKVHWWLQJV $FFHOHUDWLRQ+LJK 
＜ Model Menu (Common Functions) ＞ 123
+(/,&237(5
6HWWLQJPHWKRG
02'(/0(18 $,53/$1(*/,'(5)81&7,216
Select function to add flight conditions. (Up to 8
conditions can be used)
$,53/$1(
These are the menus usable when either airplane,
glider, or EP glider model type have been selected,
and displayed in the Model Menu screen. First use
the Model Type function of the Linkage Menu to
select your model type, wing type, and tail type.
Changing these later will reset any data set in this
menu.
7KHVHGHGLFDWHGPL[LQJVFDQEHVHWIRUHDFKÀLJKW
condition, as required. When you want to use the
system by switching the settings for each condition
by switch or stick position, use the Condition
Note: The T18MZ-WC is designed so that the airplane
and glider (including EP glider) model types can
handle fuselages of the same wing type. The
functions common to airplanes and gliders, except
IRUDIHZVSHFLÀFIXQFWLRQVDUHVKRZQEHORZ
,WHPVPD\EHGLIIHUHQWGHSHQGLQJRQWKHQXPEHU
of servos, etc. and according to the wing type used.
However, reread them. The setup screens in the
instruction manual are typical examples.
ŏ7RXFKWKH0RGHO0HQXEXWWRQRIWKH+RPHVFUHHQWR
call this Model Menu.
ŏ:KHQWKHEXWWRQRIWKHIXQFWLRQ\RXZDQWWRVHWLV
touched, a setup screen appears.
ŏ5HWXUQWR+RPHVFUHHQ
ŏ7RQH[W
page
*/,'(5
(Model Menu screen example)
*The Model Menu screen depends on the model type. This screen is for model type Airplane Wing Type 4AIL+4FLP.
0RGHO0HQXIXQFWLRQVWDEOH
Ɣ$,/'LIIHUHQWLDO
This function adjusts the left and right ailerons.
5ROOD[LVFRUUHFWLRQDQGÂżQHWXQLQJZLWKD95DUH
also possible. This is convenient when making
VHWWLQJVGXULQJÀLJKW
[Airplane/glider, 2 ailerons or more]
Ɣ)ODS6HWWLQJ
The flaps can be adjusted independently. For a 4
flaps model, the camber flaps can be mixed with
WKHEUDNHÀDSV
>$LUSODQHJOLGHUÀDSVRUPRUH@
Ɣ$,/WR&DPEHU)/3
7KLVPL[LQJRSHUDWHVWKHFDPEHUÀDSVLQWKHDLOHURQ
mode. It improves the operation characteristic of
the roll axis.
>$LUSODQHJOLGHUDLOHURQVÀDSVRUPRUH@
Ɣ$,/WR%UDNH)/3
7KLVPL[LQJRSHUDWHVWKHEUDNHÀDSVLQWKHDLOHURQ
mode. It improves the operation characteristic of
the roll axis.
>$LUSODQHJOLGHUÀDSVRUPRUH@
Ɣ$,/WR58'
This mixing is used when you want to operate the
rudder with aileron operation. Banking at a shallow
bank angle is possible.
>$LUSODQHJOLGHUDLOHURQVÀDSVRUPRUH@
Ɣ$LUEUDNHWR(/(
This mixing is used to correct operation of the
airbrakes (spoilers) when landing.
[Airplane/glider, general]
Ɣ58'WR$,/
This mixing is used to correct roll maneuvers, knife
edge, etc. of stunt planes.
[Airplane/glider, general]
Ɣ&DPEHU0L[
124 ＜ Model Menu (Airplane/Glider Functions) ＞
This mixing adjusts the camber and corrects the
elevators.
[Airplane/glider, 2 ailerons or more]
AIR BRAKE
FLP 3
(Brake Flap)
FLP 4
(Brake Flap)
FLP 2
(Camber Flap)
AIL 2
(Main Aileron) AIL 4
(Chip Aileron)
FLP 1
(Camber Flap)
AIL1
(Main Aileron) RUDDER
AIL 3
(Chip Aileron)
ELEVATOR 2
ELEVATOR
(AILERON 6)
(AILERON 5)
at AILEVATOR
at Flying wing
V-TAIL
RUDDER 2
ELEVATOR
(RUDDER 2)
RUDDER
(ELEVATOR 2)
RUDDER 1
Winglet
Winglet
( at Flying
wing )
( at Flying wing )
＜ Model Menu (Airplane/Glider Functions) ＞ 125
$,53/$1(
Ɣ$LOHYDWRU
This function adjusts the elevators and ailerons of
PRGHOVZLWKHOHYDWRUVSHFLÂżFDWLRQV
>$LUSODQHJOLGHUHOHYDWRUVSHFLÂżFDWLRQV@
Ɣ:LQJOHW
This function adjusts the left and right rudders of
winglet models.
>$LUSODQHJOLGHUZLQJOHWVSHFLÂżFDWLRQV@
Ɣ0RWRU
The operation speed when the motor of F5B and
other EP gliders is started by switch can be set.
[EP glider, general]
Ɣ58'WR(/(
This function is used to correct roll maneuvers,
knife edge, etc. of stunt planes.
[Airplane, general]
Ɣ6QDSUROO
This function selects the snap roll switch and
adjusts the steering angle of each rudder. Servo
speed can also be adjusted.
[Airplane general]
Ɣ0XOWL(QJLQH
This function adjusts the throttles independently
when using a multi engine model. (Maximum 4
engines)
[Airplane, general]
Ɣ$FFHOHUDWLRQ
Acceleration setting can be performed at elevator,
ELE to Camber and AIL to RUD.
[Glider/EP glider]
*/,'(5
Ɣ(/(WR&DPEHU
This mixing is used when you want to the mix
camber flaps with elevator operation. Lift can be
increased with raised elevators.
[Airplane/glider, 2 ailerons or more]
Ɣ&DPEHU)/3WR(/(
This mixing is used to correct for attitude changes
ZKHQWKHFDPEHUÀDSVDUHEHLQJXVHG
>$LUSODQHJOLGHUDLOHURQVÀDSRUPRUH@
Ɣ%XWWHUÀ\ &URZ
This function is used when powerful brake
operation is necessary.
[Glider, 2 ailerons or more]
Ɣ7ULP0L[
The ailerons, elevators, and flaps trim offset rate
can be utilized by a switch or condition selection.
[Glider, 2 ailerons or more]
Ɣ$LUEUDNH
This function is used when airbrakes are necessary
ZKHQODQGLQJRUZKHQGLYLQJGXULQJÀLJKW
[Airplane, general]
Ɣ*\UR
This is dedicated mixing when a gyro is used.
[Airplane/glider, general]
Ɣ9WDLO
This function adjusts the elevators and rudder of
9WDLOPRGHOV
>$LUSODQHJOLGHU9WDLOVSHFLÂżFDWLRQV@
>$LUSODQHJOLGHUDLOHURQVRUPRUH
$,/'LĂ­HUHQWLDO
The left and right ailerons differential can be
adjusted independently. The differential rate can also
EHDGMXVWHGDFFRUGLQJWRWKHÀ\LQJVWDWHE\VHWWLQJD
ÂżQHWXQLQJ95
ŏ$ÀQHWXQLQJFXUYHFDQEHVHW
$,53/$1(
Note: $LOHURQXSGRZQVHWWLQJ  UHVHWLV
ZKHQUHVHWZKHQVHWWLQJLVDQGZKHQUHVHW
when setting is -. Left and right mixing causes + and
WRFKDQJH%HIRUHÁ\LQJFRQÀUPWKHGLUHFWLRQRI
operation.
AIL1
(Main Aileron)
AIL 3
(Chip Aileron)
AIL 2
(Main Aileron)
AIL 4
(Chip Aileron)
ŏ7RXFKWKH>$,/'LIIHUHQWLDO@EXWWRQLQWKH0RGHO0HQXWR
FDOOWKHVHWXSVFUHHQVKRZQEHORZ
:LQJW\SHDLOHURQVVFUHHQ!
*The display screen is an example. The actual screen
depends on the Model Type.
ŏ5HWXUQWR0RGHO0HQX
ŏ&DOOVWKH$)5VFUHHQGLUHFWO\
when adjusting aileron
RSHUDWLRQ$)5
*/,'(5
ŏ2YHUDOO
adjustment
E\5DWH$
DQG5DWH%
ŏ)LQHWXQLQJFXUYHVHWWLQJ
ŏ $LOHURQ OHIWULJKW
adjustment
*The display is reversed
E\ PL[LQJ ZLWK DLOHURQ
operation
(For a description of the setting
method, see the description at
the end the manual.)
ŏ)LQHWXQLQJ95VHWWLQJ
7KHJUDSKLVRSHUDWHGE\VHWWLQJD95HWF
ŏ*URXSVLQJOHPRGHVZLWFKLQJ *U6QJO
(For more information, refer to the
GHVFULSWLRQDWWKHEDFNRIWKLVPDQXDO
6HWWLQJPHWKRG
ŏ7RXFKWKHDLOHURQ $,/ aOHIW RUULJKW EXWWRQDQG
DGMXVWWKHDLOHURQDQJOHVZKHQWKHVWLFNLVPRYHGWR
the left (or right) end.
7KHDLOHURQ$)5VFUHHQFDQEHGLUHFWO\FDOOHGIURP
WKH$,/'LIIHUHQWLDOVHWXSVFUHHQ >0DVWHU@EXWWRQ
ŏ:KHQVHWWLQJWKHÀQHWXQLQJ95WRXFKWKH18//
EXWWRQWRFDOOWKH6ZLWFK!VFUHHQDQGWKHQVHOHFW
WKHÀQHWXQLQJ95
ŏ7KHÀQHWXQLQJUDWHFDQEHVHWE\FXUYH
126 ＜ Model Menu (Airplane/Glider Functions) ＞
>&RUUHVSRQGLQJPRGHOW\SH@$LUSODQHJOLGHUÁDSVRUPRUH
)ODS6HWWLQJ
The up/down travel of each flap (camber flaps:
FLP1/2, brake flaps: FLP3/4) can be adjusted
independently at each servo according to the wing
type.
ŏ7KHRSHUDWLRQUHIHUHQFHSRLQWRIHDFKÁDSFDQEH
offset
FLP 3
FLP 1
(Brake Flap)
(Camber Flap)
FLP 4
(Brake Flap)
FLP 2
(Camber Flap)
ŏ$Q212))VZLWFKFDQEHVHW
ŏ 7RXFK WKH >)ODS 6HWWLQJ@ EXWWRQ LQ WKH 0RGHO 0HQX WR
FDOOWKHVHWXSVFUHHQVKRZQEHORZ
:LQJW\SHÀDSVVFUHHQ!
*The display screen is an example. The actual screen
depends on the model type.
ŏ*URXSVLQJOHPRGHVZLWFKLQJ
*U6QJO
$,53/$1(
7KHFDPEHUIODSVRIDIODSPRGHOFDQEHPL[HG
ZLWKWKHEUDNHÀDSV %UDNH)/3WRFDPEHU)/3
(For more information, see the
GHVFULSWLRQDWWKHEDFNRIWKLV
manual.)
*/,'(5
ŏ5HWXUQWR0RGHO0HQX
ŏ2SHUDWLRQUHIHUHQFHSRLQWRIIVHW
ŏ8SVLGH'RZQVLGHDGMXVWPHQW
6HWWLQJPHWKRG
ŏ7RXFKWKHÁDS )/3 a8SRU'RZQEXWWRQ
according to the wing type and adjust the travel
independently.
ŏ7RRIIVHWWKHRSHUDWLRQUHIHUHQFHSRLQWRIHDFK
ÁDSWRXFKWKHFRUUHVSRQGLQJ2IIVHWEXWWRQ8VH
WKHDGMXVWPHQWEXWWRQVGLVSOD\HGRQWKHVFUHHQWR
offset the reference point.
ŏ:KHQXVLQJ%UDNH)/3WR&DPEHU)/3PL[LQJWRXFK
WKH$&7EXWWRQDQGVHWWKHIXQFWLRQWR$&7 21 
 :KHQVHWWLQJDVZLWFKWRXFKWKH>21@EXWWRQRIWKH
VZLWFKWRFDOOWKH6ZLWFK!VFUHHQDQGWKHQVHOHFW
WKHVZLWFKDQGVHWLWV21GLUHFWLRQ $OZD\V21DW
21VHWWLQJ
(For a description of the switch selection method,
VHHWKHGHVFULSWLRQDWWKHEDFNRIWKLVPDQXDO
＜ Model Menu (Airplane/Glider Functions) ＞ 127
$,/WR&DPEHU)/3
>&RUUHVSRQGLQJPRGHOW\SH@$LUSODQHJOLGHUDLOHURQVÁDSV
or more
This mixing operates the camber flaps (FLP1/2)
in the aileron mode. When the aileron stick is
manipulated, the ailerons and camber flaps move
simultaneously and the roll axis is improved.
ŏ7KHDLOHURQOHIWULJKWPL[LQJUDWHRIHDFKÁDSVHUYR
FDQEHÀQHWXQHG
ŏ$PL[LQJFXUYHFDQEHVHW
ŏ$Q212))VZLWFKFDQEHVHW
ŏ/LQNLQJWRRWKHUPL[HVLVSRVVLEOH
FLP 1
(Camber Flap)
AIL1
(Main Aileron)
$,53/$1(
AIL 3
(Chip Aileron)
FLP 2
(Camber Flap)
AIL 2
(Main Aileron)
AIL 4
(Chip Aileron)
ŏ7RXFKWKH>$,/WR&DPEHU)/3@EXWWRQLQWKH0RGH
0HQXWRFDOOWKHVHWXSVFUHHQVKRZQEHORZ
*The display screen is an example. The actual screen
depends on the model type.
ŏ/HIWULJKWRYHUDOO
adjustment at
5DWH$DQG5DWH%
ŏ5HWXUQWR0RGHO0HQX
*/,'(5
ŏ$GMXVWPHQWRIHDFKÁDS
servo
ŏ*URXSVLQJOHPRGHVHWWLQJ *U6QJO
ŏ0L[LQJFXUYHVHWWLQJ
(For a description of the curve setting
PHWKRGVHHWKHGHVFULSWLRQDWWKHEDFN
of this manual.)
(For more information, see the description at
WKHEDFNRIWKLVPDQXDO
6HWWLQJPHWKRG
ŏ7RXFKWKH$&7EXWWRQDQGVHWWKHIXQFWLRQWR$&7
21 
ŏ:KHQVHWWLQJDVZLWFKWRXFKWKH>21@EXWWRQRIWKH
VZLWFKWRFDOOWKH6ZLWFK!VFUHHQDQGWKHQVHOHFW
WKHVZLWFKDQGVHWLWV21GLUHFWLRQ $OZD\V21DW
21VHWWLQJ
(For a description of the switch selection method,
VHHWKHGHVFULSWLRQDWWKHEDFNRIWKLVPDQXDO
ŏ7RXFKWKHOHIWRUULJKWEXWWRQRIHDFKÁDSVHUYRDQG
DGMXVWWKHPL[LQJUDWHZLWKWKHDGMXVWPHQWEXWWRQV
:KHQWKHPL[LQJGLUHFWLRQLVUHYHUVHGGXHWROLQNDJH
VHWXSDGMXVWPHQWVFDQEHPDGHE\FKDQJLQJWKH
rate value from + to - (positive to negative).
128 ＜ Model Menu (Airplane/Glider Functions) ＞
ŏ$PL[LQJFXUYHFDQEHVHW
(For a description of the mixing curve setting
PHWKRGVHHWKHGHVFULSWLRQDWWKHEDFNRIWKLV
manual.)
ŏ7RVHWOLQNLQJWRXFKWKH/LQNEXWWRQDQGVHWLWWR21
$,/WR%UDNH)/3
>&RUUHVSRQGLQJPRGHOW\SH@$LUSODQHJOLGHUÁDSVRUPRUH
This mixing operates the brake flaps (FLP3/4)
in the aileron mode. When the aileron stick is
manipulated, the aileron and brake flaps perform
the aileron operation simultaneously and the
performance of the roll axis is improved.
FLP 3
(Brake Flap)
AIL1
(Main Aileron)
ŏ$PL[LQJFXUYHFDQEHVHW
ŏ0L[LQJGXULQJÁLJKWFDQEHWXUQHG212))E\VHWWLQJ
DVWLFN $OZD\V21DW21VHWWLQJ
FLP 4
(Brake Flap)
AIL 2
(Main Aileron)
AIL 4
(Chip Aileron)
AIL 3
(Chip Aileron)
ŏ/LQNLQJFDQEHVHW/LQNVWKLVPL[LQJWRRWKHUPL[LQJV
ŏ 7RXFK WKH >$,/ WR %UDNH )/3@ EXWWRQ LQ WKH 0RGHO
0HQXWRFDOOWKHVHWXSVFUHHQVKRZQEHORZ
*The display screen is an example. The actual screen
depends on the model type.
$,53/$1(
ŏ7KHDLOHURQOHIWDQGULJKWPL[LQJUDWHVFDQEH
DGMXVWHGIRUHDFKÁDSVHUYR
ŏ/HIWULJKWRYHUDOO
DGMXVWPHQWE\
5DWH$DQG5DWH%
*/,'(5
ŏ5HWXUQWR0RGHO0HQX
ŏ$GMXVWPHQWRIHDFKÁDS
servo
ŏ0L[LQJFXUYHVHWWLQJ
ŏ*URXSVLQJOHPRGHVHWWLQJ *U6QJO
Ɣ6HWWLQJPHWKRG
ŏ7RXFKWKH$&7EXWWRQDQGVHWWKHIXQFWLRQWR$&7
21 
ŏ:KHQVHWWLQJDVZLWFKWRXFKWKH>21@EXWWRQRIWKH
VZLWFKWRFDOOWKH6ZLWFK!VFUHHQDQGWKHQVHOHFW
WKHVZLWFKDQGVHWLWV21GLUHFWLRQ $OZD\V21DW
21VHWWLQJ
ŏ7RXFKWKHOHIWRUULJKWEXWWRQRIHDFKÁDSVHUYRDQG
DGMXVWWKHPL[LQJUDWHZLWKWKHDGMXVWPHQWEXWWRQV
:KHQWKHPL[LQJGLUHFWLRQLVUHYHUVHGGXHWROLQNDJH
VHWXSDGMXVWPHQWVFDQEHPDGHE\FKDQJLQJWKH
rate value from + to - (positive to negative).
ŏ$PL[LQJFXUYHFDQEHVHW
ŏ7RVHWOLQNLQJWRXFKWKH/LQNEXWWRQDQGVHWLWWR21
＜ Model Menu (Airplane/Glider Functions) ＞ 129
$,/WR58'
>&RUUHVSRQGLQJPRGHOW\SH@$LUSODQHJOLGHUJHQHUDO
Use this mixing when you want to mix the
rudders with aileron operation.
AIL1
(Main Aileron)
ŏ$PL[LQJFXUYHFDQEHVHW
ŏ0L[LQJGXULQJÁLJKWFDQEHWXUQHG212))E\
VHWWLQJDVZLWFK $OZD\V21DW21VHWWLQJ
ŏ7KHPL[LQJUDWHFDQEHÀQHWXQHGE\VHWWLQJD95
AIL 2
(Main Aileron)
AIL 4
(Chip Aileron)
AIL 3
(Chip Aileron)
RUDDER
at Flying wing
$,53/$1(
RUDDER 2
ŏ 7RXFK WKH >$,/ WR 58'@ EXWWRQ LQ WKH 0RGHO
0HQXWRFDOOWKHVHWXSVFUHHQVKRZQEHORZ
RUDDER 1
RUDDER
AIL1
at V-TAIL
AIL2
RUDDER 2
*The display screen is an example. The actual
screen depends on the model.
ŏ/HIWULJKWRYHUDOO
DGMXVWPHQWE\
5DWH$DQG5DWH%
ŏ5HWXUQWR0RGHO0HQX
*/,'(5
ŏ)LQHWXQLQJ95VHWWLQJ
ŏ0L[LQJFXUYHVHWWLQJ
ŏ*URXSVLQJOHPRGHVHWWLQJ *U6QJO
ŏ&XUYHGLVSOD\PRGHVHOHFWLRQ 6LQJOH)LQHWXQLQJ$OO&RQG
6HWWLQJPHWKRG
ŏ7RXFKWKH$&7EXWWRQDQGVHWWKHIXQFWLRQWR$&7
21 
ŏ:KHQVHWWLQJDVZLWFKWRXFKWKH>21@EXWWRQRIWKH
VZLWFKWRFDOOWKH6ZLWFK!VFUHHQDQGWKHQVHOHFW
WKHVZLWFKDQGVHWLWV21GLUHFWLRQ $OZD\V21DW
21VHWWLQJ
ŏ:KHQVHWWLQJD95WRXFKWKH)LQH7XQLQJ18//
EXWWRQWRFDOOWKH6ZLWFK!VFUHHQDQGWKHQVHOHFW
WKH957KHDGMXVWPHQWUDWHDQGGLUHFWLRQFDQEH
VHW7KH95RSHUDWLRQPRGHFDQDOVREHVHOHFWHG
ŏ$PL[LQJFXUYHFDQEHVHW
ŏ7KHFXUYHGLVSOD\PRGHFDQEHFKDQJHG
 6LQJOH'LVSOD\VWKHPL[LQJFXUYHRQO\
 )LQHWXQLQJ'LVSOD\VWKHPL[LQJUDWHRIWKHÀQH
WXQLQJ95
 $OO&RQG'LVSOD\VWKHPL[LQJFXUYHRIDOOWKH
conditions. (When conditions are set)
)LQHWXQLQJ95VHWWLQJ
ŏ95VHOHFWLRQ
ŏ5DWHDGMXVWPHQW
)LQH7XQLQJ
/'


ŏ2SHUDWLRQPRGH
selection
'LVSOD\HGDW95VHWWLQJ
ŏ$GMXVWPHQW
direction setting
>2SHUDWLRQPRGHV@
0L[LQJUDWHDWFHQWHURI95
:KHQWKH95LVWXUQHG
FRXQWHUFORFNZLVHDQGFORFNZLVHWKH
mixing rate increases and decreases,
respectively.
0L[LQJUDWHDWOHIWHQGRI95
:KHQWKH95LVWXUQHGWKHPL[LQJUDWH
increases.
0L[LQJUDWHDWULJKWHQGRI95
:KHQWKH95LVWXUQHGWKHPL[LQJUDWH
increases.
:KHQWKH95LVWXUQHGWRWKHOHIWRU
right of the neutral position, the mixing
rate increases.
130 ＜ Model Menu (Airplane/Glider Functions) ＞
>&RUUHVSRQGLQJPRGHOW\SH@$LUSODQHJOLGHUJHQHUDO
$LUEUDNHWR(/(
AIRBRAKE
This mixing is used when you want to mix the
elevators with airbrake (spoiler) operation. It raises
the elevators to correct for drooping of the nose
during airbrake operation.
*This function does not operate when airbrake is not assigned.
ELEVATOR ELEVATOR 2
ŏ5DWHVLGH5DWHVLGHPL[LQJUDWHRIWKH
HOHYDWRUVHUYRVFDQEHDGMXVWHG
ŏ$PL[LQJFXUYHFDQEHVHW
ŏ0L[LQJGXULQJÁLJKWFDQEHWXUQHG212))E\
VHWWLQJDVZLWFK $OZD\V21DW21VHWWLQJ
ŏ7KHPL[LQJUDWHFDQEHÀQHWXQHGE\VHWWLQJD95
ELEVATOR
ŏ7RXFKWKH>$LUEUDNHWR(/(@EXWWRQLQWKH0RGHO0HQX
WRFDOOWKHVHWXSVFUHHQVKRZQEHORZ
ŏ/HIWULJKWRYHUDOO
DGMXVWPHQWE\
5DWH$DQG5DWH%
*/,'(5
ŏ5HWXUQWR0RGHO0HQX
ELEVATOR 2
$,53/$1(
V-TAIL
ŏ)LQHWXQLQJ95VHWWLQJ
ŏ0L[LQJFXUYHVHWWLQJ
ŏ&XUYHGLVSOD\PRGHVZLWFKLQJ
6LQJOH)LQHWXQLQJ$OO&RQG
ŏ*URXSVLQJOHPRGHVZLWFK *U6QJO
6HWWLQJPHWKRG
ŏ7RXFKWKH,1+EXWWRQDQGVHWWKHIXQFWLRQWR$&7
21 
ŏ:KHQVHWWLQJDVZLWFKWRXFKWKH>21@EXWWRQWRFDOO
WKH6ZLWFK!VFUHHQDQGWKHQVHOHFWWKHVZLWFK
DQGVHWLWV21GLUHFWLRQ $OZD\V21DW21VHWWLQJ
ŏ:KHQVHWWLQJD95WRXFKWKH)LQHWXQLQJ18//
EXWWRQWRFDOOWKH6ZLWFK!VFUHHQDQGWKHQVHOHFW
WKH957KHDGMXVWPHQWUDWHDQGGLUHFWLRQFDQEH
VHW7KH95RSHUDWLRQPRGHFDQDOVREHVHW
ŏ$PL[LQJFXUYHFDQEHVHW
ŏ7KHFXUYHGLVSOD\PRGHFDQEHVHW
 6LQJOH'LVSOD\VWKHPL[LQJFXUYHRQO\
 )LQHWXQLQJ'LVSOD\VWKHDGMXVWPHQWUDWHRIWKHÀQH
WXQLQJ95
 $OO&RQG'LVSOD\VWKHPL[LQJFXUYHRIDOOWKH
conditions. (When conditions are set)
＜ Model Menu (Airplane/Glider Functions) ＞ 131
58'WR$,/
>&RUUHVSRQGLQJPRGHOW\SH@$LUSODQHJOLGHUJHQHUDO
This function is used when you want to mix
the ailerons with rudder operation. It is used
when rudder is applied during roll maneuvers,
knife edge, etc. of stunt planes. It can be used to
bank scale models, large models, etc. like a full
size plane.
position at that time is displayed on the mixing
curve. When the memory mode is exited, the
PHPRUL]HGSRLQWVDUHDXWRPDWLFDOO\UHÁHFWHGRQ
the curve. (When the memory function is used,
/LQHW\SHFXUYHLVDXWRPDWLFDOO\VHOHFWHG
ŏ/LQNLQJFDQEHVHW/LQNVWKLVPL[LQJWRRWKHUPL[LQJV
ŏ7KHPL[LQJUDWHFDQEHÀQHWXQHE\VHWWLQJD95
$,53/$1(
ŏ$PL[LQJFXUYHFDQEHVHW
ŏ0L[LQJGXULQJÁLJKWFDQEHWXUQHG212))E\VHWWLQJ
DVZLWFK $OZD\V21DW21VHWWLQJ
ŏ7KHUDWHRIUXGGHUFRUUHFWLRQFDQEHPHPRUL]HGE\
using the memory function. This is convenient when
setting a mixing curve. When memory operation
(switch operation) is performed in memory mode
with the rudder correction, the switch operation
AIL1
RUDDER
AIL 2
ŏ7RXFKWKH>58'WR$,/@EXWWRQLQWKH0RGHO0HQXWR
FDOOWKHVHWXSVFUHHQVKRZQEHORZ
ŏ5HWXUQWR0RGHO0HQX
*/,'(5
ŏ2YHUDOO
adjustment
E\5DWH$
DQG5DWH%
ŏ)LQHWXQLQJ95VHWWLQJ
ŏ:KHQVHWWR21E\WRXFKLQJ>,1+@WKH
memory items are displayed.
6HWWLQJPHWKRG
ŏ7RXFKWKH,1+EXWWRQDQGVHWWKHIXQFWLRQWR$&7
21 
ŏ:KHQVHWWLQJDVZLWFKWRXFKWKH>21@EXWWRQWRFDOO
WKH6ZLWFK!VFUHHQDQGWKHQVHOHFWWKHVZLWFK
DQGVHWLWV21GLUHFWLRQ $OZD\V21DW21VHWWLQJ
ŏ:KHQVHWWLQJD95WRXFKWKH)LQHWXQLQJ18//
EXWWRQWRFDOOWKH6ZLWFK!VFUHHQDQGWKHQVHOHFW
WKH957KHDGMXVWPHQWUDWHDQGDGMXVWPHQW
GLUHFWLRQFDQEHVHW
7KH95RSHUDWLRQPRGHFDQDOVREHVHW
ŏ$PL[LQJFXUYHFDQEHVHW
ŏ7KHFXUYHGLVSOD\PRGHFDQEHFKDQJHG
6LQJOH'LVSOD\VWKHPL[LQJFXUYHRQO\
)LQHWXQLQJ'LVSOD\VWKHDGMXVWPHQWUDWHRIWKHÀQH
WXQLQJ95
$OO&RQG'LVSOD\VWKHPL[LQJFXUYHRIDOOWKH
conditions. (When conditions are set)
ŏ:KHQOLQNLQJ7RXFKWKH/LQNEXWWRQDQGVHWLWWR21
132 ＜ Model Menu (Airplane/Glider Functions) ＞
ŏ0L[LQJFXUYHVHWWLQJ
>&RUUHVSRQGLQJPRGHOW\SH@$LUSODQHJOLGHUDLOHURQVRUPRUH
This function adjusts the AFR (D/R) rate of camber
operation which operates the wing camber (ailerons,
camber flaps, brake flaps) in the negative and
SRVLWLYHGLUHFWLRQV7KHDLOHURQÀDSDQGHOHYDWRU
rates can also be adjusted independently by curve,
and attitude changes caused by camber operation
can be corrected.
,QLWLDOVHWWLQJDVVLJQVFDPEHURSHUDWLRQWRVLGHOHYHU
567 6WLFN0RGH /67 6WLFNMode 1).
ŏ7KHGLUHFWLRQRIWKHDLOHURQÁDSDQGHOHYDWRU
VHUYRVFDQEHDGMXVWHGE\DFXUYH:KHQGLUHFWLRQ
LVUHYHUVHGDWWKHOLQNDJHE\WKLVPL[\RXFDQ
UHYHUVHLWE\FKDQJLQJWKHUDWHVWRHLWKHURU
(positive or negative).
ŏ0L[LQJGXULQJÁLJKWFDQEHWXUQHG212))E\VHWWLQJ
DVZLWFK $OZD\V21DW21VHWWLQJ
ŏ$GHOD\FDQEHVHWIRUHDFKFRQGLWLRQ$FXWVZLWFK
ZKLFKFDQWXUQ2))WKHGHOD\IXQFWLRQFDQEHVHW
ŏ7KHVSHHGRIWKHDLOHURQÁDSDQGHOHYDWRUVHUYRV
FDQEHVHW ,1VLGH287VLGH
ŏ7RXFKWKH>&DPEHU0L[@EXWWRQLQWKH0RGHO0HQXWRFDOOWKHVHWXS
VFUHHQVKRZQEHORZ
$,53/$1(
&DPEHU0L[
*The display screen is an example. The actual screen depends on the model type.)
*/,'(5
ŏ5HWXUQWR0RGHO0HQX
ŏ&RQGLWLRQGHOD\FXWVZLWFK
ŏ&DPEHU$)5 '5 VHWXSVFUHHQFDOO
ŏ&RQGLWLRQGHOD\VHWWLQJ
ŏ*URXSVLQJOHPRGHVZLWFK *U6QJO
ŏ$LOHURQUDWHDGMXVWPHQW
&XUYHUDWHVHWXSVFUHHQ
ŏ2YHUDOO
adjustment
E\5DWH$
DQG5DWH%
ŏ6HUYRVSHHGVHWWLQJ
ŏ0L[LQJFXUYHVHWWLQJ
＜ Model Menu (Airplane/Glider Functions) ＞ 133
6HWWLQJPHWKRG
&XUYHUDWHVHWXSVFUHHQ
$,53/$1(
ŏ7RXFKWKH,1+EXWWRQDQGVHWWKHIXQFWLRQWR$&7
21 
ŏ:KHQVHWWLQJDVZLWFKWRXFKWKH>21@EXWWRQWRFDOO
WKH6ZLWFK!VFUHHQDQGWKHQVHOHFWWKHVZLWFK
DQGVHWLWV21GLUHFWLRQ $OZD\V21DW21VHWWLQJ
ŏ:KHQVHWWLQJDFRQGLWLRQGHOD\WRXFKWKH&RQGLWLRQ
'HOD\EXWWRQDQGVHWWKHGHOD\ZLWKWKHDGMXVWPHQW
EXWWRQVZKLFKDSSHDURQWKHVFUHHQ
 7KH95RSHUDWLRQPRGHFDQDOVREHVHW
ŏ&DPEHU$)5 '5 VFUHHQFDOO
 7RXFKWKH&DPEHU$)5EXWWRQWRFDOOWKHVHWXS
screen.
ŏ7KHFXUYHDQGUDWHDUHDGMXVWHGE\FDOOLQJWKH
DLOHURQÁDSDQGHOHYDWRUFXUYHUDWHVFUHHQV
 7KHUDWHDQGFXUYHRIHDFKVHUYRFDQEHVHWE\
FDOOLQJHDFKVFUHHQ7KHVHUYRVSHHGFDQDOVREH
adjusted.
*/,'(5
FLP 3
(Brake Flap)
FLP 1
(Camber Flap)
AIL1
(Main Aileron)
AIL 3
(Chip Aileron)
ELEVATOR
ELEVATOR 2
(at AILEVATOR)
at V-TAIL
ELEVATOR
FLP 4
(Brake Flap) FLP 2
(Camber Flap)
AIL 2
(Main Aileron)
AIL 4
(Chip Aileron)
ELEVATOR 2
134 ＜ Model Menu (Airplane/Glider Functions) ＞
>&RUUHVSRQGLQJPRGHOW\SH@$LUSODQHJOLGHUDLOHURQVRUPRUH
ŏ$PL[LQJFXUYHFDQEHVHW
ŏ0L[LQJGXULQJÁLJKWFDQEHWXUQHG212))E\VHWWLQJ
DVZLWFK $OZD\V21DW21VHWWLQJ
ŏ7KHPL[LQJUDWHFDQEHÀQHWXQHGE\VHWWLQJD95
ŏ7RXFKWKH>(/(WR&DPEHU@EXWWRQLQWKH0RGHO
0HQXWRFDOOWKHVHWXSVFUHHQVKRZQEHORZ
ŏ&XUYHGLVSOD\PRGHVZLWFKLQJ
ŏ *URXSVLQJOH PRGH VZLWFKLQJ
*U6QJO
6LQJOH)LQHWXQLQJ$OO&RQG
ŏ5HWXUQWR0RGHO0HQX
ŏ)LQHWXQLQJ95VHWWLQJ
ŏ2YHUDOO
DGMXVWPHQWE\
5DWH$DQG
5DWH%
ŏ0L[LQJFXUYHVHWWLQJ
$LOHURQVDQGÁDSVUDWHDGMXVWPHQWVFUHHQ
6HWWLQJPHWKRG
ŏ7RXFKWKH$&7EXWWRQDQGVHWWKHIXQFWLRQWR
$&7 21 
ŏ:KHQVHWWLQJDVZLWFKWRXFKWKH>21@EXWWRQRIWKH
VZLWFKWRFDOOWKH6ZLWFK!VFUHHQDQGWKHQVHOHFW
WKHVZLWFKDQGVHWLWV21GLUHFWLRQ $OZD\V21DW
21VHWWLQJ
ŏ:KHQVHWWLQJD95WRXFKWKH)LQHWXQLQJ18//
EXWWRQWRFDOOWKH6ZLWFK!VFUHHQDQGWKHQ
VHOHFWWKH957KHDGMXVWPHQWUDWHDQGDGMXVWPHQW
GLUHFWLRQFDQEHVHW
 7KH95RSHUDWLRQPRGHFDQDOVREHVHOHFWHG
ŏ$PL[LQJFXUYHFDQDOVREHVHW
ŏ7KHFXUYHGLVSOD\PRGHFDQEHFKDQJHG
 6LQJOH'LVSOD\VWKHPL[LQJFXUYHRQO\
 )LQHWXQLQJ'LVSOD\VWKHÀQHWXQLQJ95DGMXVWPHQW
rate.
 $OO&RQG'LVSOD\VWKHPL[LQJFXUYHRIDOOWKH
conditions (When conditions are set).
＜ Model Menu (Airplane/Glider Functions) ＞ 135
$,53/$1(
This function is used when you want to mix the
FDPEHUÀDSVZLWKHOHYDWRURSHUDWLRQ:KHQPL[LQJ
LVXVHGVRWKDWWKHÀDSVDUHORZHUHGE\XSHOHYDWRU
lift can be increased.
*/,'(5
(/(WR&DPEHU
>&RUUHVSRQGLQJPRGHOW\SH@$LUSODQHJOLGHUDLOHURQV
ÁDSRUPRUH
&DPEHU)/3WR(/(
This mixing is used to correct changes (elevator
GLUHFWLRQ JHQHUDWHGZKHQWKHFDPEHUÀDSV VSHHG
ÀDSV DUHXVHG
$,53/$1(
ŏ7KHHOHYDWRUVHUYRUDWHVFDQEHDGMXVWHG:KHQ
WKHPL[FDXVHWKHVHUYRGLUHFWLRQWREHUHYHUVHG
DGMXVWPHQWVFDQEHPDGHE\FKDQJLQJWKHPL[LQJ
rates at - to + (negative to positive).
ŏ$PL[LQJFXUYHFDQEHVHW
ŏ0L[LQJGXULQJÁLJKWFDQEHWXUQHG212))E\VHWWLQJ
DVZLWFK $OZD\V21DW21VHWWLQJ
ŏ7KHPL[LQJUDWHFDQEHÀQHWXQHGE\VHWWLQJD95
FLP 1
(Camber Flap)
FLP 2
(Camber Flap)
ELEVATOR
ELEVATOR 2
ŏ *URXSVLQJOH PRGH VZLWFKLQJ
*U6QJO
ŏ 7RXFK WKH >&DPEHU )/3 WR (/(@ EXWWRQ LQ
the Model Menu to call the setup screen
VKRZQEHORZ
*The display screen is an example. The actual
screen depends on the model type.
ŏ2YHUDOO
adjustment
E\5DWH$
DQG5DWH%
ŏ5HWXUQWR0RGHO0HQX
*/,'(5
ŏ)LQHWXQLQJ95VHWWLQJ
ŏ0L[LQJFXUYHVHWWLQJ
ŏ&XUYHGLVSOD\PRGHVZLWFKLQJ
6LQJOH)LQHWXQLQJ$OO&RQG
ŏ(OHYDWRUUDWHDGMXVWPHQW
6HWWLQJPHWKRG
ŏ7RXFKWKH$&7EXWWRQDQGVHWWKHIXQFWLRQWR
$&7 21 
ŏ:KHQVHWWLQJDVZLWFKWRXFKWKHVZLWFKEXWWRQ
WRFDOOWKH6ZLWFK!VFUHHQDQGWKHQVHOHFWWKH
VZLWFKDQGVHWLWV21GLUHFWLRQ $OZD\V21DW
21VHWWLQJ
ŏ7RXFKWKHHOHYDWRUVHUYRVOHIWDQGULJKWEXWWRQV
and adjust the mixing rate with the adjustment
EXWWRQVGLVSOD\HGRQWKHVFUHHQ
*When the mixing direction is reversed due to
OLQNDJH VHWXS DGMXVWPHQWV FDQ EH PDGH E\
changing the rate value from + to - (positive to
negative).
136 ＜ Model Menu (Airplane/Glider Functions) ＞
ŏ:KHQVHWWLQJD95WRXFKWKH)LQHWXQLQJ18//
EXWWRQWRFDOOWKH6ZLWFK!VFUHHQDQGWKHQ
VHOHFWWKH95
 7KH95RSHUDWLRQPRGHFDQEHVHOHFWHG
ŏ$PL[LQJFXUYHFDQEHVHW
ŏ7KHFXUYHRSHUDWLRQPRGHFDQEHFKDQJHG
 6LQJOH'LVSOD\VRQO\WKHPL[LQJFXUYH
 )LQH7XQLQJ'LVSOD\VWKHDGMXVWPHQWUDWHRIWKH
ÀQHWXQLQJ95
 $OO&RQG'LVSOD\VWKHPL[LQJFXUYHRIDOOWKH
conditions (when conditions are set).
%XWWHUs\
>&RUUHVSRQGLQJPRGHOW\SH@*OLGHUDLOHURQVRUPRUH
ŏ0L[LQJGXULQJÁLJKWFDQEHWXUQHG212))E\VHWWLQJ
DVZLWFK $OZD\V21DW21VHWWLQJ
This function allows powerful brake operation by
simultaneously raising the left and right ailerons
DQGORZHULQJWKHÀDSV FDPEHUÀDSEUDNHÀDS 
Butterfly (Crow) produces an extremely efficient
landing configuration by accomplishing the
following:
6ORZLQJWKHDLUFUDIW¡VYHORFLW\
3URYLGLQJZDVKRXWDWWKHZLQJWLSVWRUHGXFH
the tendency to tip stall.
3. Creating more lift toward the center of the
ZLQJDOORZLQJLWWRÁ\DWDVORZHUVSHHG
ŏ7KHDLOHURQVÁDSVDQGHOHYDWRUVRSHUDWLRQVSHHG
FDQEHDGMXVWHG ,1VLGH287VLGH
ŏ$GHOD\FDQEHVHWIRUHDFKFRQGLWLRQ$FXWVZLWFK
ZKLFKFDQWXUQ2))WKHGHOD\IXQFWLRQFDQDOVREH
set.
ŏ7KHGLIIHUHQWLDOUDWHFDQEHDGMXVWHG
:KHQVHUYRELQGLQJRFFXUVZKHQVHWWLQJWKH
DLOHURQVDQGÁDSVLQEXWWHUÁ\PL[LQJXVHWKH$)5
function to adjust the rudder angle.
ŏ7RXFKWKH>%XWWHUÁ\@EXWWRQLQWKH0RGHO0HQX
WRFDOOWKHVHWXSVFUHHQVKRZQEHORZ
(The display screen is an example. The actual
screen depends on the model type. The screen
VKRZQEHORZLVIRUDLOHURQVDQGÁDSV
ŏ7RVHWWKHRIIVHWSRLQWIRUEXWWHUÁ\PRYHWKH
ÁDSVWLFNWRWKHSRVLWLRQZKHUH\RXZDQW\RXU
EXWWHUÁ\VHWWLQJVWREHFRPHDFWLYH3XVKWKH
>2IIVHW@EXWWRQWRVHWWKDWSRLQW7KHUHIHUHQFH
SRLQWGLVSOD\V:KHQ>21@
EXWWRQWRFDOOWKH6ZLWFK!VFUHHQDQGWKHQ
VHOHFWWKHVZLWFKDQGVHWLWV21GLUHFWLRQ
ŏ7RXFKWKH0L[LQJ5DWH$,/DQG
)/3 EXWWRQV DQG DGMXVW WKH
mixing rates.
ŏ5HWXUQWR0RGHO0HQX
ŏ$LOHURQDQGÁDSVHUYRVVSHHG
setting
ŏ'LIIHUHQWLDOUDWH
adjustment
ŏ &RQGLWLRQ GHOD\ VHWWLQJ DQG FXW
switch setting
ŏ7RHOHYDWRUFRUUHFWLRQ
setup screen
It is not displayed in a
Á\LQJZLQJ
ŏ&DOOVWKH%XWWHUÁ\$)5 '5 VHWXSVFUHHQ
＜ Model Menu (Airplane/Glider Functions) ＞ 137
ŏ 7RXFK WKH (/( FRUUHFWLRQ UDWH EXWWRQV DQG
DGMXVWWKHUDWHVZLWKWKHDGMXVWPHQWEXWWRQV
displayed on the screen.
>(/(6HWXS@VFUHHQ
ŏ6HUYRVSHHGVHWWLQJ
ŏ0L[LQJFXUYHVHWWLQJ
*/,'(5
AIL 3
(Chip Aileron)
AIL1
(Main Aileron)
FLP 1
(Camber Flap)
FLP 3
(Brake Flap)
ELEVATOR
ELEVATOR 2
(at AILEVATOR)
ELEVATOR
FLP 4
(Brake Flap)
FLP 2
(Camber Flap)
AIL 2
(Main Aileron)
AIL 4
(Chip Aileron)
at V-TAIL
ELEVATOR 2
138 ＜ Model Menu (Airplane/Glider Functions) ＞
7ULP0L[
>&RUUHVSRQGLQJPRGHOW\SH@*OLGHUDLOHURQVRUPRUH
7KHDPRXQWRIDLOHURQVHOHYDWRUDQGÀDSV FDPEHU
ÀDSEUDNHÀDS WULPRIIVHWFDQEHVHWWRDVZLWFK
As an example 7ULP 0L[  can be set up for
launching, with speed flaps and ailerons dropped,
and a slight amount of up elevator. 7ULPPL[ can
be used for high speed flying, with both ailerons
DQGVSHHGÀDSVUHÀH[HGVOLJKWO\DQGDELWRIGRZQ
elevator.
7KHWULPIXQFWLRQVFDQEHDFWLYDWHGGXULQJÀLJKWE\
setting a switch. To prevent sudden trim changes
ZKHQVZLWFKLQJÀLJKWFRQGLWLRQVDGHOD\FDQEHVHW
to provide a smooth transition between the two.
([DPSOH
7RXFKWKH$&7EXWWRQDQGVHWWKHWULPPL[IXQFWLRQ
WR>21@
*When separating the settings for each condition,
WRXFKWKHJURXSPRGHEXWWRQDQGVHWLWWR>6QJO@
6HOHFWWKH212))VZLWFK
6HOHFWWKH>0DQXDO@RU>$XWR@PRGH
 ,QWKH>$XWR@PRGHDOVRVHOHFWDQDXWR6:7KLV
VZLWFKFDQEHOLQNHGWRDVWLFNHWF
6SHHG!
 ,Q7KHRSHUDWLRQVSHHGDWVZLWFK21FDQEHVHW
 2XW7KHUHWXUQVSHHGDWVZLWFK2))FDQEHVHW
)LQH7XQLQJ!
 7KHRIIVHWUDWHFDQEHYDULHGLQWKH)LQH7XQLQJ
QXPHULFUDQJHVHWDWVFUHHQ>@E\95HWF
selection.
&RQGLWLRQ'HOD\!
 :KHQÁLJKWFRQGLWLRQVDUHVHWWKHRSHUDWLRQVSHHG
FDQEHVHWIRUHDFKFRQGLWLRQ&RQGLWLRQGHOD\
RSHUDWLRQFDQEHLQWHUUXSWHGDQGHDFKUXGGHU
TXLFNO\UHWXUQHGWRLWVRULJLQDOSRVLWLRQE\VHOHFWLQJD
cut switch.
ŏ 7RXFK WKH >7ULP 0L[ @ EXWWRQ LQ WKH 0RGHO 0HQX WR FDOO WKH VHWXS VFUHHQ VKRZQ
EHORZ
7RXFKWKH>@EXWWRQWRVZLWFKWRSDJH
ŏ7RXFKWKH$&7EXWWRQDQGVHWWKHIXQFWLRQWR$&7 21 
ŏ:KHQVHWWLQJDVZLWFKWRXFKWKH6ZLWFKEXWWRQWRFDOOWKH6ZLWFK!VFUHHQDQGWKHQ
VHOHFWWKHVZLWFKDQGVHWLWV21GLUHFWLRQ $OZD\V21DW21VHWWLQJ
ŏ*URXSVLQJOHPRGHVZLWFKLQJ
*U6QJO
ŏ :KHQ XVLQJ D ILQH WXQLQJ 95 WRXFK WKLV
EXWWRQWRFDOOWKH6ZLWFK!VFUHHQ
ŏ5HWXUQWR0RGHO0HQX
ŏ$LOHURQVÁDSVDQ
elevators servo speed
setting
7ULPPL[VHWXSSDJH
ŏ&RQGLWLRQGHOD\VHWWLQJDQG
cut switch setting
ŏ0DQXDO$XWRPRGHVHOHFWLRQ
0DQXDO6ZLWFKHVWKHIXQFWLRQ212))E\VZLWFK
$XWR7ULPPL[IXQFWLRQFDOOFDQEHOLQNHGWRDVWLFN
HWF$VWLFNVZLWFKHWFVHSDUDWHIURPWKHIXQFWLRQ
212))VZLWFKLVVHW
＜ Model Menu (Airplane/Glider Functions) ＞ 139
*/,'(5
(The display screen is an example. The actual screen depends on the model type. The screen
VKRZQEHORZLVIRUDLOHURQVDQGÁDSV
ŏ7KHDLOHURQVÁDSVDQGHOHYDWRUV
RIIVHWUDWHFDQEHDGMXVWHG
 7RXFKWKHFRUUHVSRQGLQJEXWWRQ
and adjust the rate with the
DGMXVWPHQWEXWWRQVGLVSOD\HGRQ
the screen.
ŏ5HWXUQWR0RGHO0HQX
ŏ:KHQDÀQHWXQLQJ95LVVHWRQWKHQH[WSDJH  WKHDLOHURQV
DQGÁDSVWULPUDWHVFDQEHDGMXVWHG
 7RXFKWKHFRUUHVSRQGLQJEXWWRQDQGDGMXVWWKHUDWHZLWKWKH
DGMXVWPHQWEXWWRQVGLVSOD\HGRQWKHVFUHHQ
*/,'(5
FLP 3
(Brake Flap)
FLP 1
(Camber Flap)
FLP 4
(Brake Flap) FLP 2
(Camber Flap)
AIL1
(Main Aileron)
AIL 4
(Chip Aileron)
AIL 3
(Chip Aileron)
ELEVATOR
ELEVATOR 2
(at AILEVATOR)
at V-TAIL
ELEVATOR
AIL 2
(Main Aileron)
ELEVATOR 2
140 ＜ Model Menu (Airplane/Glider Functions) ＞
>&RUUHVSRQGLQJPRGHOW\SH@$LUSODQHJHQHUDO
This function is used when an air brake is
necessary when landing or diving, etc.
7KHSUHVHWHOHYDWRUVDQGÀDSV FDPEHUÀDSEUDNH
ÀDS RIIVHWDPRXQWFDQEHDFWLYDWHGE\DVZLWFK
The offset amount of the aileron, elevator, and
flap servos can be adjusted as needed. Also the
VSHHGRIWKHDLOHURQHOHYDWRUDQGÀDSVHUYRVFDQ
be adjusted. (IN side/OUT side) A delay can be set
for each condition, and a Cut switch which will
turn OFF the delay can be chosen. Trim amounts
FDQEHILQHWXQHGE\VHWWLQJD95a@$,/>a@(/(>a@
Note: The input numerics are examples. Adjust the
travel to match the fuselage.
3DJH
$&7>21@
*URXS>6QJO@
6ZLWFK>6&&@
0RGH>0DQXDO@
ELEVATOR 2
(at AILEVATOR)
ELEVATOR
FLP 2
AIL1
ŏ7RXFKWKH>$LUEUDNH@EXWWRQLQWKH0RGHO0HQXWRFDOOWKHVHWXSVFUHHQVKRZQ
EHORZ 7KH GLVSOD\ VFUHHQ LV DQ H[DPSOH 7KH DFWXDO VFUHHQ GHSHQGV RQ WKH
PRGHOW\SH7KHVFUHHQVKRZQEHORZLVIRUDLOHURQVDQGÁDSV
ŏ7RXFKWKH$&7EXWWRQDQGVHWWKHIXQFWLRQWR$&7 21 
ŏ:KHQVHWWLQJDVZLWFKWRXFKWKH6ZLWFKEXWWRQWRFDOOWKH6ZLWFK!VFUHHQDQG
WKHQVHOHFWWKHVZLWFKDQGVHWLWV21GLUHFWLRQ $OZD\V21DW21VHWWLQJ
ŏ*URXSVLQJOHPRGHVZLWFKLQJ
*U6QJO
ŏ :KHQ XVLQJ D ILQH WXQLQJ 95 WRXFK WKLV
EXWWRQWRFDOOWKH6ZLWFK!VFUHHQ
ŏ5HWXUQWR0RGHO0HQX
ŏ$LOHURQVÁDSVDQHOHYDWRUVVHUYRVSHHG
setting
(For a description of the setting method, see
WKHGHVFULSWLRQDWWKHEDFNRIWKLVPDQXDO
$LUEUDNHVHWXSVFUHHQ
ŏ&RQGLWLRQGHOD\VHWWLQJ IRU
a description of the setting
method, see the description
DWWKHEDFNRIWKLVPDQXDO 
and cut switch setting.
ŏ0DQXDO$XWRPRGHVHOHFWLRQ
0DQXDO6ZLWFKHVWKHIXQFWLRQ212))E\VZLWFK
$XWR7ULPPL[IXQFWLRQFDOOFDQEHOLQNHGWRDVWLFN
HWF$VWLFNVZLWFKHWFVHSDUDWHIURPWKHIXQFWLRQ
212))VZLWFKLVVHW
＜ Model Menu (Airplane/Glider Functions) ＞ 141
$,53/$1(
$LUEUDNH
ŏ7KHDLOHURQÁDSDQGHOHYDWRURIIVHW
UDWHVFDQEHDGMXVWHG
 7RXFKWKHFRUUHVSRQGLQJEXWWRQ
and adjust the rate with the
DGMXVWPHQWEXWWRQVGLVSOD\HGRQ
the screen.
ŏ5HWXUQWR0RGHO0HQX
$,53/$1(
ŏ:KHQDÀQHWXQLQJ95LVVHWRQWKHQH[WVFUHHQ  WKHDLOHURQ
DQGÁDSWULPUDWHVFDQEHDGMXVWHG7RXFKWKHFRUUHVSRQGLQJ
EXWWRQDQGDGMXVWWKHUDWHVZLWKWKHDGMXVWPHQWEXWWRQV
displayed on the screen.
FLP 3
(Brake Flap)
FLP 1
(Camber Flap)
AIL1
(Main Aileron)
AIL 3
(Chip Aileron)
FLP 4
(Brake Flap)
FLP 2
(Camber Flap)
AIL 2
(Main Aileron)
AIL 4
(Chip Aileron)
ELEVATOR
ELEVATOR 2
(at AILEVATOR)
142 ＜ Model Menu (Airplane/Glider Functions) ＞
>&RUUHVSRQGLQJPRGHOW\SH@$LUSODQHJOLGHUJHQHUDO
*Initial setting does not assign a sensitivity channel. Use the
Function menu of the Linkage Menu to assign the sensitivity
channel (Gyro/Gyro2/Gyro3) used to a vacant channel
beforehand.
This function is used when a gyro is used to
stabilize the fuselage attitude. The sensitivity and
RSHUDWLRQ PRGH 1RUPDO PRGH**\UR@EXWWRQLQWKH0RGHO0HQX
WRFDOOWKHVHWXSVFUHHQVKRZQEHORZ
ŏ5HWXUQWR0RGHO0HQX
(For more information, see the description
DWWKHEDFNRIWKLVPDQXDO
$,53/$1(
*\UR
ŏ7KUHHUDWHV 5DWH5DWH5DWH FDQEHXVHG
ŏ7RXFKWKH$&7EXWWRQRIWKHUDWHWREHXVHGDQGVHWWKHIXQFWLRQWR$&7 >21@RU>2))@ 
ŏ :KHQ D )XWDED J\UR LV XVHG ZKHQ >*<@ W\SH LV VHOHFWHG WKH VHQVLWLYLW\ VHW YDOXH LV
GLUHFWO\UHDGLQERWKWKH$9&6DQG125PRGHV
ŏ:KHQVHWWLQJDVZLWFKWRXFKWKHVZLWFKEXWWRQWRFDOOWKH6ZLWFK!VFUHHQDQGWKHQ
VHOHFWWKHVZLWFKDQGVHWLWV21GLUHFWLRQ
([DPSOH 6HWWLQJWKUHHD[LVXVLQJD*<$DQG*<$ 
ŏ:LQJW\SH$LOHURQVHUYRVPRXQWHGIXVHODJHVHOHFWHG
ŏ6HW 5CH → GYRO *<$$,/  7CH → GYRO2 *<$(/(  8CH → GYRO3 *<$58'  Control and Trim → NULL 
DWWKH)XQFWLRQPHQXRIWKH/LQNDJHPHQX
ŏ*<52VHWWLQJRIWKH0RGHOPHQX
Rate
ACT
OFF/ON
INH
ON/OFF
Type
GY
Switch
SE
GYRO
GYRO ２
GYRO ３
AVCS : 60% AVCS : 60% AVCS : 60%
GY
SE
NORM : 60% NORM : 60% NORM : 60%
*Set so that Rate 1 is turned on at the back position of switch
E and Rate 3 is turned ON at the front position. Since switch
E is turned OFF at the center, Rate 2 remains [INH].
R7008SB
AVCS
GAIN 0％
GYA431
Aileron servo
NORMAL
When AVCS is used we
recommend that the
sensitivity CH be set to
the 3-position.
S.BUS2 port
GYA431
Elevator servo
GYA430
Rudder servo
＜ Model Menu (Airplane/Glider Functions) ＞ 143
*/,'(5
ŏ7KHRSHUDWLRQPRGH $9&6125 DQGVHQVLWLYLW\RI
WKHD[HV*\UR*\UR*\URFDQEHVHW
9WDLO
>&RUUHVSRQGLQJPRGHOW\SH@$LUSODQHJOLGHU9WDLO
$,53/$1(
This function let’s you adjust for left and right rudder
angle changes at elevator and rudder operation of a
9WDLODLUSODQH
9WDLOLVZKHQVHUYRVDUHXVHGWRJHWKHUWRFRQWURO
rudder movement as Elevators. In addition to each
rudder side moving up and down together, each
side moves in opposite directions when moving
DV (OHYDWRUV 2Q D9WDLO WKLV LV DOVR NQRZQ DV D
Ruddervator, as they can serve the same purpose.
ŏ7RXFKWKH>9WDLO@EXWWRQLQWKH0RGHO0HQX
WRFDOOWKHVHWXSVFUHHQVKRZQEHORZ
ŏ5HWXUQWR0RGHO0HQX
ŏ *URXSVLQJOH PRGH VZLWFKLQJ
*U6QJO
*/,'(5
5XGGHUIXQFWLRQ
Left and right travel adjustment at rudder operation
(Elevator function)
 8SDQGGRZQWUDYHODGMXVWPHQWDWHOHYDWRU
operation
ELEVATOR
(RUDDER 2)
RUDDER
(ELEVATOR 2)
V-TAIL
144 ＜ Model Menu (Airplane/Glider Functions) ＞
$LOHYDWRU
>&RUUHVSRQGLQJPRGHOW\SH@$LUSODQHJOLGHU97DLO
(Effective only when 2 servos used at the elevators)
$,53/$1(
This function improves the operating performance of
the roll axis by operating the elevators as ailerons.
Ailevator is where each elevator in a standard
FRQYHQWLRQDO  RU YWDLO PRYHV LQGHSHQGHQWO\ OLNH
ailerons on a wing. In addition to each elevator side
moving up and down together, each side moves in
opposite directions when moving as an Ailevator. On
D9WDLOWKLVLVDOVRNQRZQDVD5XGGHUYDWRUDVWKH\
can serve the same purpose. Typically, both Ailevator
and ailerons are coupled together to maximize roll
performance, especially on larger wingspan planes.
Note: Select Ailevator as the Model Type at the Model
Type screen. This changes the output channel.
Check the Function menu.
ŏ7RXFKWKH>$,/@EXWWRQLQWKH0RGHO0HQXWR
FDOOWKHVHWXSVFUHHQVKRZQEHORZ
ŏ *URXSVLQJOH PRGH VZLWFKLQJ
*U6QJO
*/,'(5
ŏ5HWXUQWR0RGHO0HQX
(Aileron function)
ŏ:KHQWKHHOHYDWRUVDUHXVHGDVDLOHURQVDLOHURQ
WUDYHORIWKHOHIWDQGULJKWHOHYDWRUVFDQEH
adjusted.
(Elevator function)
ŏ7KHXSDQGGRZQUDWHRIWKHOHIWDQGULJKW
HOHYDWRUVZKHQWKHHOHYDWRUVWLFNLVPDQLSXODWHG
FDQEHLQGLYLGXDOO\DGMXVWHG
AILERON 1
ELEVATOR
AILERON 2
ELEVATOR 2
(AILERON 6)
＜ Model Menu (Airplane/Glider Functions) ＞ 145
:LQJOHW
>&RUUHVSRQGLQJPRGHOW\SH@$LUSODQHJOLGHUZLQJOHW
$,53/$1(
This function adjusts the rudder left and right rudder
DQJOHRIZLQJOHWVSHFLÂżFDWLRQVIXVHODJHV
Winglets are used to improve the efficiency of
DLUFUDIW ORZHULQJ WKH OLIWLQGXFHG GUDJ FDXVHG E\
wingtip vortices. The winglet is a vertical or angled
extension at the tips of each wing.
Winglets work by increasing the effective aspect
ratio wing without adding greatly to the structural
VWUHVVDQGKHQFHQHFHVVDU\ZHLJKWRILWVVWUXFWXUHDQ
extension of wing span would also permit lowering
of induced drag, though it would cause parasitic drag
and would require boosting the strength of the wing
DQGKHQFHLWVZHLJKWWKHUHZRXOGFRPHDSRLQWDW
which no overall useful saving would be made. A
winglet helps to solve this by effectively increasing
the aspect ratio without adding to the span of the
wing.
RUDDER 2
Winglet
( at Flying wing )
RUDDER 1
Winglet
( at Flying wing )
*/,'(5
ŏ 7RXFK WKH >:LQJOHW@ EXWWRQ LQ WKH 0RGHO
0HQXWRFDOOWKHVHWXSVFUHHQVKRZQEHORZ
ŏ5HWXUQWR0RGHO0HQX
ŏ *URXSVLQJOH PRGH VZLWFKLQJ
*U6QJO
5XGGHU
ŏ7KHWUDYHODWUXGGHUVWLFNOHIWDQGULJKWRSHUDWLRQ
FDQEHLQGLYLGXDOO\VHW
146 ＜ Model Menu (Airplane/Glider Functions) ＞
>&RUUHVSRQGLQJPRGHOW\SH@(3JOLGHU$LUSODQHJHQHUDO
This function lets you set the operation speed when
the motor of a F5B or other EP glider is started by
switch. The operation speed can be set in 2 ranges
RIVORZVSHHGÀLJKWDQGKLJKVSHHGÀLJKW 6SHHG
Speed 2). This function can also be operated as a
safety function by setting 2 switches.
ŏ7KH,QVLGHDQG2XWVLGHRSHUDWLQJVSHHGVFDQ
EHDGMXVWHGLQGHSHQGHQWO\LQUDQJHV 6SHHG
6SHHG 
ŏ7KHERXQGDU\EHWZHHQWKHUDQJHVFDQEHVHW
)URP6SHHGWR6SHHG
ŏ7KHVHWRSHUDWLRQVSHHGRSHUDWLRQFDQEHDFWLYDWHG
at initial operation only. (1 time operation) However,
RSHUDWLRQFDQEHUHSHDWHGE\VHWWLQJWKHVZLWFKWR
2))EHIRUHRSHUDWLRQLVÀQLVKHG:KHQ\RXZDQWWR
UHVHWWLPHRSHUDWLRQVHWWKH$&7EXWWRQWR>,1+@
DQGWKHQUHVHWLWWR>21@
ŏ7KHPRWRULVFRQWUROOHGE\6:*>0RGH@6:
(>0RGH@ ,QLWLDOVHWWLQJ :KHQFKDQJLQJWKH
VZLWFKRUVWLFNZKLFKFRQWUROVWKHPRWRUÀUVWFKDQJH
)XQFWLRQRIWKH/LQNDJH0HQX
Note: When using this function, always check initial
operation with the propeller removed.
Note: A warning message appears when this mix is
on at the time of power up.
ŏ0RYHWKHFXUVRUE\VHW
VZLWFKRU95
ŏ7RXFKWKH>0RWRU@EXWWRQLQWKH0RGHO0HQX
WRFDOOWKHVHWXSVFUHHQVKRZQEHORZ
$,53/$1(
0RWRU
,Q
ŏ2SHUDWLRQ
 7RXFK WKH EXWWRQ DQG VHW WKH IXQFWLRQ WR
21
ŏ*URXSVLQJOHPRGHVZLWFKLQJ *U6QJO
ŏ6ZLWFK
A switch that turns the function itself
212))FDQEHVHOHFWHG
ŏ0RWRURII
 >1R@ DUH GLVSOD\HG E\ WRXFKLQJ
WKH0RWRU2IIEXWWRQZKHQ>6:* 0RGH @
>6:( 0RGH @(Initial setting)is in the motor
2)) SRVLWLRQ :KHQ >21@
ŏ6SHHGWR
 7KH6SHHGDQG6SHHGUHJLRQERXQGDU\
FDQEHFKDQJHG
ŏ2SHUDWLRQVSHHGDGMXVWPHQW
 7KH VSHHG ZKHQ 6SHHG  DQG 6SHHG  DUH
21 ,Q DQG2)) 2XW FDQEHDGMXVWHG
1RWHV
ŏ)LUVWGHFLGHWKHPRWRU2))SRLQWDQGWKHQVHWWKHVSHHG:KHQ\RXZDQWWR
UHVHWWKHPRWRU2))SRLQWDOVRUHVHWWKHVSHHG
ŏ:HUHFRPPHQGWKDW0RWRU2))EHVHWLQFRPELQDWLRQZLWK)6
ŏ6HWWKHEDVLFRSHUDWLRQGLUHFWLRQZLWKWKH5HYHUVHIXQFWLRQWRPDWFKWKH
amp used.
ŏ$OZD\VVHWWKH0RWRU2))SRVLWLRQ
＜ Model Menu (Airplane/Glider Functions) ＞ 147
*/,'(5
ŏ5HWXUQWR0RGHO0HQX
58'WR(/(
>&RUUHVSRQGLQJPRGHOW\SH@$LUSODQHJHQHUDO
This function is used when you want to mix elevator
operation with rudder operation. It is used to correct
undesirable tendencies when rudder is applied in roll
maneuvers, knife edge, etc. of acrobatic planes.
$,53/$1(
ŏ$PL[LQJFXUYHFDQEHVHW
ŏ0L[LQJGXULQJÁLJKWFDQEHWXUQHG212))E\VHWWLQJ
DVZLWFK $OZD\V21DW21VHWWLQJ
ŏ7KHDPRXQWRIFRUUHFWLRQUXGGHUFDQEHPHPRUL]HG
E\XVLQJWKH0HPRU\IXQFWLRQ7KLVLVFRQYHQLHQW
at mixing curve setting. When memory operation
(switch operation) is performed with correction
UXGGHUDSSOLHGLQWKH0HPRU\0RGHWKHVWLFN
position at that time is displayed on the mixing
FXUYH7KHSRLQWLVDXWRPDWLFDOO\UHÁHFWHGLQWKH
FXUYH :KHQWKH0HPRU\IXQFWLRQLVXVHG/LQHLV
automatically selected as the curve type.)
ŏ/LQNFDQEHVHW/LQNVWKLVPL[LQJWRRWKHUPL[LQJV
ŏ7KHPL[LQJUDWHFDQEHÀQHWXQHGE\VHWWLQJD95
(Fine tuning)
ŏ7RXFKWKH>58'WR(/(@EXWWRQLQWKH0RGHO0HQXWR
FDOOWKHVHWXSVFUHHQVKRZQEHORZ
ŏ*URXSVLQJOHPRGHVZLWFKLQJ *U6QJO
ŏ2YHUDOO
adjustment
E\5DWH$
DQG5DWH%
ŏ5HWXUQWR0RGHO0HQX
ŏ)LQHWXQLQJ95VHWWLQJ
ŏ0L[LQJFXUYHVHWWLQJ
ŏ:KHQ>,1+@LVWRXFKHGWKHPHPRU\
items are displayed.
6HWWLQJPHWKRG
ŏ7RXFKWKH,1+EXWWRQDQGVHWWKHIXQFWLRQWR
$&7 21 
ŏ:KHQVHWWLQJDVZLWFKWRXFKWKH21EXWWRQWRFDOO
WKH6ZLWFK!VFUHHQDQGWKHQVHOHFWWKHVZLWFK
DQGVHWLWV21GLUHFWLRQ $OZD\V21DW21VHWWLQJ
(For a description of the switch setting method, see
WKHGHVFULSWLRQDWWKHEDFNRIWKLVPDQXDO
ŏ:KHQVHWWLQJD95WRXFKWKH)LQH7XQLQJ18//
EXWWRQWRFDOOWKH6ZLWFK!VFUHHQDQGWKHQ
VHOHFWWKH957KHÀQHWXQLQJUDWHDQGDGMXVWPHQW
GLUHFWLRQFDQEHVHW
 7KH95RSHUDWLRQPRGHFDQDOVREHVHW
ŏ7KHFXUYHGLVSOD\PRGHFDQEHFKDQJHG
 6LQJOH'LVSOD\VWKHPL[LQJFXUYHRQO\
 )LQH7XQLQJ'LVSOD\VWKHÀQHWXQLQJUDWHRIWKHÀQH
WXQLQJ95
 $OO&RQG'LVSOD\VWKHPL[LQJFXUYHRIDOOWKH
conditions (When conditions are set)
ŏ:KHQVHWWLQJ/LQNWRXFKWKH/LQNEXWWRQDQGVHWLWWR
21
148 ＜ Model Menu (Airplane/Glider Functions) ＞
0HPRU\IXQFWLRQXVDJHPHWKRG
([DPSOH 8VLQJWKHPHPRU\IXQFWLRQZLWKDQ)$
DLUSODQH NQLIHHGJHFRUUHFWLRQ
*When call switch
>6:+@ZHUHVHW
>6:$@DQGPHPRU\VZLWFK
>0HPRU\IXQFWLRQRSHUDWLRQ@
0HPRU\IXQFWLRQPRGH>0DQXDO@ >0HPRU\@
:KHQWKHPHPRU\VZLWFK 6:+ LVVHWWR21ZKLOH
performing elevator correction when rudder was
DSSOLHGDWNQLIHHGJHWKHSRLQWSRVLWLRQDWWKDW
WLPHLVPHPRUL]HG0HPRUL]DWLRQLVSHUIRUPHG
ZKLOHFKDQJLQJWKHOHIWDQGULJKWVWLFNSRVLWLRQV
7RUHFDOOWKHPHPRUL]HGSRVLWLRQVVHW>6:$@WR21
 7KHPHPRUL]HGFRUUHFWLRQUDWHLVUHÁHFWHGRQWKH
curve, and operation is simultaneously set.
1RWH:KHQPHPRUL]HGIURPPDQXDOEHIRUHÁLJKW
be sure that the memory SW is not accidentally
set to ON and incorrect mixing setting is not
applied when taxiing, starting the engine, etc.
>&RUUHVSRQGLQJPRGHOW\SH@$LUSODQHJHQHUDO
6QDS5ROO
([DPSOH 6HWWLQJH[DPSOHIRU)$
ŏ)RXUVQDSUROOGLUHFWLRQVFDQEHVHW 5LJKW
XSULJKWGRZQOHIWXSOHIWGRZQ
ŏ2SHUDWLRQPRGH:KHQ>0DVWHU@PRGH
LVVHOHFWHGWKH6QDS5ROOIXQFWLRQLV
WXUQHG212))E\PDVWHUVZLWFKLQWKH
state in which the direction switch was
switched to the direction in which you
ZDQWWRVQDSUROO:KHQ>6LQJOH@PRGHLV
selected, snap roll in each direction can
EHH[HFXWHGE\PHDQVRILQGHSHQGHQW
switches.
ŏ$VDIHW\VZLWFKFDQEHVHW$VD
VDIHW\PHDVXUHWKHVZLWFKFDQEH
set so that snap roll is not executed
when, for instance, the landing gear
is lowered, even if the switch is turned
on accidentally. The snap roll switch is
activated only when the safety switch is
21
ŏ7KHRSHUDWLRQVSHHGRIWKHDLOHURQ
HOHYDWRUDQGÁDSVHUYRVFDQEHDGMXVWHG
IRUHDFKVQDSUROOGLUHFWLRQ ,QVLGH2XW
VLGH  3DJH
ŏ0RGH>0DVWHU@
ŏ6DIHW\6:>6:*@ 6DIHW\PHDVXUH
ŏ0DVWHU6:>6:+@ 0DLQVZLWFKIRUH[HFXWLQJVQDSUROO
ŏ'LUHFWLRQVZLWFKHV
*The snap roll up side left and right and down side left and right
direction switches are selected here.
5LJKW8S2))>6:'@5LJKW'RZQ2))>6:'@/HIW8S2))>6:$@
/HIW'RZQ2))>6:$@
ŏ6SHHGDGMXVWPHQW 6FUHHQ
The operation speed of each control surface when
WKH VQDS VZLWFK LV 21 FDQ EH FKDQJHG DQG VQDS UROO
H[HFXWHGE\VWLFNZKLOHWKHUHLVVZLWFKRSHUDWLRQFDQEH
performed.
AIL1
RUDDER
ELEVATOR
AIL2
ELEVATOR 2
(at AILEVATOR)
ŏ&XUYHGLVSOD\PRGHVZLWFKLQJ
ŏ*URXSVLQJOHPRGHVZLWFKLQJ *U6QJO
6LQJOH)LQHWXQLQJ$OO&RQG
ŏ5HWXUQWR0RGHO0HQX
ŏ'LUHFWLRQVZLWFKHV
(For more information, see the description at
WKHEDFNRIWKLVPDQXDO
ŏ5DWHDGMXVWPHQWRIHDFKUXGGHU
ŏ$GMXVWPHQWRIWKHVHUYRVSHHGRIHDFKUXGGHU
＜ Model Menu (Airplane/Glider Functions) ＞ 149
$,53/$1(
This function selects the switch and rate
adjustment of each rudder, (ailerons,
elevators, or flaps) when a snap roll is
performed.
0XOWL(QJLQH
>&RUUHVSRQGLQJPRGHOW\SH@$LUSODQHJHQHUDO
This function lets you adjust the throttle when using
a multi engine airplane with up to 4 engines. The
Throttle Cut function, Idle Down function, Throttle
Hold function, High Trim, and Idle Trim can be
adjusted by throttle channel (THR, THR2, THR3,
THR4).
$,53/$1(
,QLWLDOVHWWLQJDVVLJQVRQO\RQHWKURWWOHFKDQQHO 7+5 
:KHQ XVLQJ WKLV IXQFWLRQ WKH QXPEHU RI WKURWWOH
FKDQQHOV PXVW EH DVVLJQHG EHIRUHKDQG DW WKH
)XQFWLRQPHQXRIWKH/LQNDJH0HQX
ŏ7KHWKURWWOHFXWSRVLWLRQFDQEHVHWIRUHDFKWKURWWOH
FKDQQHO7KURWWOHFXWRSHUDWLRQLVOLQNHGWRWKH
switch set with the Throttle Cut function of the
/LQNDJH0HQX
*The idle down offset rate set at this screen is
effective.
ŏ2SHUDWLRQFDQEHÀ[HGDWWKHHQJLQHVSHHG
FDUEXUHWRURSHQLQJDQJOH IRUHDFKWKURWWOH
channel with the Hold Position function. The hold
SRVLWLRQFDQEHFKDQJHG
ŏ+LJKVLGHWULPDQGLGOHWULPFDQEHVHWIRUHDFK
FKDQQHO2SHUDWLRQDFWVDVKLJKWULPRULGOHWULP
EDVHGRQWKHFHQWHU
*The throttle cut position set at this screen is effective.
ŏ7KHWKURWWOHGRZQRIIVHWUDWHFDQEHVHWIRUHDFK
WKURWWOHFKDQQHO,GOHGRZQRSHUDWLRQLVOLQNHGWR
WKHVZLWFKVHWZLWKWKH,GOH'RZQIXQFWLRQRIWKH
/LQNDJH0HQX
ŏ7RXFKWKH>0XOWL(QJLQH@EXWWRQLQWKH0RGHO
0HQXWRFDOOWKHVHWXSVFUHHQVKRZQEHORZ
ŏ5HWXUQWR0RGHO0HQX
THR1
THR2
THR3
THR4
7KHQXPEHURIHQJLQHV a DVVLJQHGE\
)XQFWLRQPHQXLQWKH/LQNDJH0HQXVHWXS
screen is displayed.
ŏ7KURWWOHFXWSRVLWLRQVHWWLQJ IRUHDFK
engine)
ŏ,GOHGRZQRIIVHWUDWHVHWWLQJ IRUHDFK
engine)
ŏ7KURWWOHKROGSRVLWLRQVHWWLQJ
ŏ+LJK7ULPVHWWLQJ IRUHDFKHQJLQH
ŏ,GOH7ULPVHWWLQJ IRUHDFKHQJLQH
150 ＜ Model Menu (Airplane/Glider Functions) ＞
$FFHOHUDWLRQ
>&RUUHVSRQGLQJPRGHOW\SH@(3JOLGHUJOLGHU
Acceleration setting can be performed at elevator,
ELE to Camber and AIL to RUD. (Glider and EP
glider only)
ŏ)XQFWLRQ212))VZLWFKVHWWLQJLVSHUIRUPHGIRU$,/
WR58'VHWWLQJRQO\
ŏ$,/WR58'VHWWLQJLVDFFHOHUDWLRQ
IXQFWLRQVHWWLQJIRU$,/WR58'PL[LQJ,WLVQRW
SHUIRUPHGZKHQ$,/WR58'PL[LQJLV,1+
ŏ7KLVVHWWLQJLVGLYLGHGLQWRHOHYDWRUVHWWLQJDQG
FDPEHUVHWWLQJ7KHVHWWLQJPHWKRGLVWKHVDPH
ŏ&DPEHUVHWWLQJVHWVWKHDFFHOHUDWLRQIXQFWLRQIRU
(/(WR&DPEHUPL[LQJ6HWWLQJLVQRWSHUIRUPHG
ZKHQ(/(WR&DPEHUPL[LQJLV,1+
ŏ7KHDFFHOHUDWLRQIXQFWLRQFDQEHVHWIRUERWKWKH
8SVLGHDQG'RZQVLGH
*/,'(5
ŏ5HWXUQWR0RGHO0HQX
ŏ(OHYDWRU$FFHOHUDWLRQ
ŏ(/(WR&DPEHU$FFHOHUDWLRQ
ŏ5HWXUQWR0RGHO0HQX
ŏ$,/WR58'$FFHOHUDWLRQ
＜ Model Menu (Airplane/Glider Functions) ＞ 151
02'(/0(18 +(/,&237(5
7KLVVHFWLRQFRQWDLQVLQIRUPDWLRQRQWKHFRPPDQGV
WKDW DSSO\ WR KHOLFRSWHUV RQO\ )RU LQVWUXFWLRQV RQ
$LUSODQHVDQG*OLGHUVUHIHUWRWKHVHFWLRQVSHUWDLQLQJ
WRWKRVHDLUFUDIW(DFKRIWKHVHIXQFWLRQVFDQEHVHW
LQGHSHQGHQWO\IRUGLIIHUHQWÀLJKWFRQGLWLRQV7RJHW
WRWKHVHVHWWLQJVWRXFKWKHGHVLUHGIXQFWLRQEXWWRQWR
EHDFFHVVHG
8VHWKH0RGHO7\SHIXQFWLRQLQWKH/LQNDJH0HQX
WR VHOHFW WKH VZDVK W\SH PDWFKHG WR WKH IXVHODJH
EHIRUHKDQG ,I \RX ODWHU FKDQJH PRGHO W\SHV DOO
VHWWLQJVZLOOEHORVW
$OVRDGGIOLJKWFRQGLWLRQVDWWKH&RQGLWLRQ6HOHFW
VFUHHQEHIRUHVHWWLQJWKHPRGHOGDWDDWHDFKIXQFWLRQ
8SWRFRQGLWLRQVFDQEHXVHG
7KH$)5IXQFWLRQIXHOPL[WXUHDQGRWKHUIXQFWLRQV
FRPPRQ WR DOO PRGHO W\SHV DUH GHVFULEHG LQ D
VHSDUDWHVHFWLRQ
ŏ7RXFKWKH0RGHO0HQXEXWWRQRIWKH+RPHVFUHHQWR
FDOOWKHPHQXVKRZQEHORZ7RXFKWKHEXWWRQRIWKH
IXQFWLRQ\RXZDQWWRVHWWRFDOOWKHVHWXSVFUHHQ
ŏ5HWXUQWR+RPHVFUHHQ
Condition Hold function ON/OFF button
)RUDGHWDLOHGGHVFULSWLRQVHH3 &RQGLWLRQ+ROGIXQFWLRQ 
0RGHO0HQXIXQFWLRQV KHOLFRSWHU WDEOH
+(/,&237(5
PIT Curve:$GMXVWVUHVSRQVHLQGLIIHUHQWÀLJKWFRQGLWLRQV
THR Curve:7KURWWOHFXUYHDQGKRYHULQJWULPDGMXVWPHQW
Acceleration:&RXQWHUDFWVWRUTXHGXHWRVXGGHQWKURWWOHDQGSLWFKFRPPDQGV
Throttle Hold:0RYHVWKHWKURWWOHWRLGOHGXULQJDXWRURWDWLRQ
Swash Mix:&RPSHQVDWHVIRUHDFKFRQWUROUHVSRQVH
Throttle Mix:&RPSHQVDWHVIRUSRZHUORVVZKHQF\FOLFDSSOLHG
Pit to Needle:$GMXVWVUHVSRQVHFXUYHLQGLIIHUHQWÀLJKWFRQGLWLRQV
Pit to RUD:+DQGOHVWRUTXHFKDQJHVIURPSLWFKDQJOHLQSXWV
Fuel Mixture:&RPPDQGVDVHFRQGVHUYRWRDGMXVWWKHIXHOPL[WXUHDWWKHFDUEXUHWRU
Gyro:8VHGWRVZLWFK)XWDED*<VHULHVJ\URVHQVLWLYLW\
Governor:8VHGWRVZLWFK530RIWKHKHOLFRSWHUÂśVKHDG
Throttle Limiter:/LPLWVWKHKLJKUDQJHRIWKHWKURWWOHPRYHPHQWE\DQ\VOLGHURUWULPPHU
152 ＜ Model Menu (Helicopter Functions) ＞
3,7&XUYH3LWFK7ULP
3,7&XUYH
7KLVIXQFWLRQDGMXVWVWKHSLWFKRSHUDWLRQFXUYHIRU
HDFKÀLJKWFRQGLWLRQIRUWKHRSWLPDOÀLJKWUHVSRQVH
UHODWLYHWRPRYHPHQWRIWKHWKURWWOHVWLFN
7KHSLWFKFXUYHFDQEHIUHHO\VHOHFWHGIURPOLQHDURSHUDWLRQ
FXUYHWRVPRRWKFXUYHDQGDGMXVWHGWRPDWFKWKHFXUYH\RX
ZDQW E\ PHDQV RI WKH70=:&ÂśV SRZHUIXO &XUYH (GLW
)XQFWLRQ W\SHVRIFXUYHVFDQEHVHOHFWHG 8SWRSRLQWV
FDQ EH VHW IRU OLQHDU RU FXUYH W\SHV +RZHYHU ZKHQ XVLQJ
WKHSRLQWVRUSRLQWVVSHFLÂżHGWRFUHDWHDFXUYHDVLPSOH
DQGVPRRWKFXUYHFDQEHFUHDWHGE\VHOHFWLQJWKHFXUYHW\SH
DQGUHGXFLQJWKHQXPEHURILQSXWSRLQWVWRRUDQGWKHQ
HQWHULQJWKHVSHFLÂżHGYDOXHDWWKHFRUUHVSRQGLQJSRLQWVWKDW
\RX FUHDWHG$ FXUYH D VLPSOH DQG VPRRWK FXUYH FDQ EH
FUHDWHGE\VHOHFWLQJWKHFXUYHW\SHDQGUHGXFLQJWKHQXPEHU
RILQSXWSRLQWVWRRUDQGWKHQHQWHULQJWKHVSHFLÂżHGYDOXH
DWWKHFRUUHVSRQGLQJSRLQWVWKDW\RXFUHDWHG
ŏ 7RXFK WKH >3,7 &XUYH@ EXWWRQ LQ WKH 0RGHO 0HQX WR
FDOOWKHVHWXSVFUHHQVKRZQEHORZ
ŏ 7KHUH DUH  W\SHV RI GLVSOD\ 7KH FXUYH RI DOO WKH
FRQGLWLRQV RU WKH SLWFK DQG WKURWWOH FXUYHV FDQ EH
GLVSOD\HGRQRQHVFUHHQ
ŏ5HWXUQWR0RGHO0HQX
ŏ7ULPFDQEHXVHG
DVKRYHULQJSLWFK
DQGSLWFKWULP
7KHKLJKDQGORZ
VLGHSLWFKFDQ
EHÀQHWXQHG
ŏ/LQHDUW\SHLVSRLQWVEXWIRU
VLPSOH XVH a SRLQWV DUH
VXIÀFLHQW
ŏ1RUPDOO\XVH6HSDUDWH
ŏ 8QLWV FDQ EH VHOHFWHG IURP >@ DQG >'HJ@ :KHQ >'HJ@ LV
VHOHFWHGWKHURWRUSLWFKDQJOHLVGLVSOD\HGDQGEHFRPHVWKH
VHWWLQJVWDQGDUG:KHQ>'HJ@ZDVVHOHFWHGWKHKLJKFHQWHU
DQGORZSLWFKDQJOHVDUHHQWHUG
ŏ&DQEHFRSLHGWRWKHSLWFKWULPDGMXVWPHQWSRVLWLRQ
ŏ :KHQ WKH >$QJOH@ EXWWRQ LV WRXFKHG WKH SLWFK DQJOH LQSXW
VFUHHQLVGLVSOD\HG,QSXWWKHPD[LPXPSLWFKFHQWHUDQGORZ
SLWFK
Normal curve adjustment
+(/,&237(5
ŏ)RUQRUPDOFXUYHXVXDOO\XVH>/LQH@W\SHDQG
FUHDWHDEDVLFSLWFKFXUYHFHQWHUHGDERXW
KRYHULQJ8VHWKLVIXQFWLRQWRJHWKHUZLWKWKH
7+5&XUYH 1RUPDO IXQFWLRQDQGDGMXVWWKH
FXUYHVRWKDWXSGRZQFRQWUROLVEHVWDWD
FRQVWDQWHQJLQHVSHHG
Idle up curve adjustment
ŏ )RU WKH KLJK VLGH SLWFK FXUYH VHW WKH
PD[LPXP SLWFK ZKLFK GRHV QRW DSSO\ D
ORDG WR WKH HQJLQH )RU WKH ORZ VLGH SLWFK
FXUYHFUHDWHFXUYHVPDWFKHGWRORRSUROO
'DQGRWKHUSXUSRVHVDQGXVHWKHLGOHXS
FXUYHVDFFRUGLQJWRWKHSHUIRUPDQFH
Note:,I\RXFKDQJHWKHFXUYHW\SHDOOGDWDZLOOEH
UHVHW.
Throttle hold curve adjustment
Operation precautions
WARNING
:KHQDFWXDOO\VWDUWLQJWKHHQJLQHDQGIO\LQJ
DOZD\VVHWWKHLGOHXSFRQGLWLRQVZLWFKWR>2))@
DQGVWDUWWKHHQJLQHLQWKHLGOLQJVWDWH
ŏ7KHWKURWWOHKROGFXUYHLVXVHGZKHQ
H[HFXWLQJDXWRURWDWLRQGLYHV
＜ Model Menu (Helicopter Functions) ＞ 153
Setting method
ŏ*URXSEXWWRQ:KHQ\RXDOVRZDQWWRHQWHUWKH
GDWDWRDOORWKHUFRQGLWLRQVHQWHUWKHGDWDLQWKH
JURXSPRGH *53 :KHQGRLQJVRWKHVDPH
VHWWLQJVDUHLQSXWWRDOOWKHRWKHUFRQGLWLRQV
:KHQ\RXZDQWWRVHWGDWHLQWRHDFKFRQGLWLRQ
LQGHSHQGHQWO\VHOHFWWKHVLQJOH 61*/ PRGH
ŏ1RUPDOLQSXWRUDQJOHLQSXWFDQEHVHOHFWHGDW
UDWHDGMXVWPHQWDWFXUYHVHWWLQJ)RUDQJOHLQSXWLI
WKHKLJKVLGHORZVLGHDQGFHQWHUDQJOHVDUHLQSXW
EHIRUHKDQGWKHUDWHFDQEHVHWE\UHDGLQJWKH
DQJOHGLUHFWO\ VWDQGDUG 
ŏ7KHFXUYHJUDSKGLVSOD\PRGHFDQEHVHOHFWHG7KLV
LVFRQYHQLHQWZKHQFKHFNLQJFXUYHVRWKHUWKDQWKH
FXUYHFXUUHQWO\EHLQJVHW
 >6QJO@'LVSOD\VRQO\WKHFXUYHFXUUHQWO\EHLQJVHW
 >)LQH7XQLQJ@:KHQSLWFKWULPLVXVHGDFXUYHZLWK
SLWFKWULPDGMXVWPHQWDGGHGLVDOVRGLVSOD\HG
Curve setting examples
7KH VFUHHQV VKRZQ EHORZ DUH FXUYHV FUHDWHG E\
HQWHULQJWKHSLWFKDQJOHDWORZFHQWHUDQGKLJKVLGH
 SRLQWV RU  SRLQWV DW HDFK FRQGLWLRQ7KH\ ZHUH
FUHDWHG E\ UHGXFLQJ WKH QXPEHU RI SRLQWV WR WKH
 SRLQWV RI ORZ VLGH FHQWHU DQG KLJK VLGH:KHQ
DFWXDOO\FUHDWLQJDFXUYHLQSXWWKHDQJOHVSHFLÂżHGDW
 >$OO&RQG@'LVSOD\VWKHSLWFKFXUYHRIDOOWKH
FRQGLWLRQV7KHFXUYHRIWKHFRQGLWLRQFXUUHQWO\LQ
XVHLVLQGLFDWHGE\DEROGOLQH
 >3,7 7+5@7KHWKURWWOHKROGFXUYHRIWKHFRQGLWLRQ
FXUUHQWO\LQXVHLVDOVRGLVSOD\HG
ŏ7KH7KURWWOH&XUYHVHWXSVFUHHQFDQEHFDOOHG
ZLWKRQHWRXFKZKLFKLVFRQYHQLHQWZKHQPDNLQJ
DGMXVWPHQWVDOWHUQDWHO\ZLWKWKHWKURWWOHFXUYH
ŏ7KHVHUYRRSHUDWLRQVSHHGFDQEHVHW:KHQ
DGMXVWHGZKHQWKHSLWFKLVWRRVHQVLWLYHWKHSLWFK
RSHUDWLRQIHHOLQJFDQEHFKDQJHG
ŏ:KHQLQFUHDVLQJWKHQXPEHURISRLQWVRQ\RXU
FXUYHXVHWKHFXUVRUNH\V>@>!@DQGPRYHWKH
FXUVRUWRWKHVSRWZKHUH\RXZDQWWRHQWHUDQHZ
FXUYHSRLQW  WKHQWRXFKWKH5DWHEXWWRQ$QHZ
SRLQWLVFUHDWHG
WKHIXVHODJH RUWKHUHIHUHQFHYDOXH 
)RUDGHVFULSWLRQRIWKHFXUYHVHWWLQJPHWKRGVHHWKH
GHVFULSWLRQDWWKHEDFNRIWKLVPDQXDO
Ɣ3LWFK&XUYH ([DPSOH
Normal Curve
Idle-up 1 Curve
Idle-up 2 Curve
Hold Curve
3LWFK7ULP +RYHULQJSLWFKKLJKSLWFKORZSLWFK
+(/,&237(5
7KHKRYHULQJSLWFKORZSLWFKDQGKLJKSLWFKWULPVHWXSVFUHHQFDQEHFDOOHGIURPWKH3,7&XUYHVHWXSVFUHHQ
ŏ5HWXUQWR0RGHO0HQX
ŏ$GMXVWVWKHDGMXVWLQJGLDO
ŏ+RYHULQJSLWFK
WULPVHWWLQJ
154 ＜ Model Menu (Helicopter Functions) ＞
ŏ/RZ+LJKSLWFKWULP
Hovering pitch trim
High Pitch/Low Pitch Trim
7KH +RYHULQJ 3LWFK IXQFWLRQ WULPV WKH SLWFK QHDU
WKH KRYHULQJ SRLQW 1RUPDOO\ LW LV XVHG ZLWK WKH
KRYHULQJFRQGLWLRQ7KHKRYHULQJSLWFKFDQEHILQH
WXQHG IRU FKDQJHV LQ URWRU VSHHG DFFRPSDQ\LQJ
FKDQJHVLQWHPSHUDWXUHKXPLGLW\DQGRWKHUIOLJKW
FRQGLWLRQV$GMXVWWKHKRYHULQJSLWFKVRWKDWURWRU
VSHHGLVFRQVWDQW7KLVIXQFWLRQFDQEHXVHGWRJHWKHU
ZLWKWKH+RYHULQJ7KURWWOH7ULPIXQFWLRQIRUPRUH
GHOLFDWHRSHUDWLRQ
+LJK3LWFK/RZ3LWFK7ULPLVWKHSLWFKVHUYRKLJK
VLGHDQGORZVLGHWULPIXQFWLRQ
ŏ :KHQ XVLQJ RQO\ WKH KRYHULQJ QRUPDO 
FRQGLWLRQ VZLWFK WKH JURXS EXWWRQ WR WKH
VLQJOHPRGHEHIRUHVHWWLQJ
ŏ6HWWKHIXQFWLRQWR$&7>21@
ŏ  6 H O H F W  W K H  D G M X V W P H Q W  N Q R E   6 H O H F W L R Q
H[DPSOH/'RU7
ŏ7KHWULPRSHUDWLRQPRGH 0RGH&7501250 
FDQEHVHOHFWHG
 CTRM mode: 0D[LPXP FKDQJH QHDU FHQWHU
E\FHQWHUWULPRSHUDWLRQ 'RHVQRWFKDQJHDW
HQGRIWKHVWLFNPRYHPHQW
 NORM mode: 1RUPDO WULP OLQHDU  RSHUDWLRQ
7KH DGYDQWDJH RI XVLQJ WKLV PRGH LV WKDW
WKH KRYHULQJ SLWFK FDQ EH DGMXVWHG ZLWKRXW
FKDQJLQJWKHFXUYH
ŏ7ULPDGMXVWPHQWUDQJH 5DQJH VHWWLQJ
:KHQ WKLV YDOXH LV PDGH VPDOO WULP FDQ RQO\
EHXVHGQHDUWKHFHQWHU
ŏ 7KH WULP UDWH FDQ EH DGMXVWHG DQG WKH
RSHUDWLRQGLUHFWLRQFDQEHFKDQJHG
ŏ :KHQ VHWWLQJ WKH DGMXVWPHQW NQREV FRPPRQ
WR DOO WKH FRQGLWLRQV VHW WKHP LQ WKH JURXS
PRGH
ŏ6HWWKHIXQFWLRQWR$&7 21 
ŏ 6HOHFW WKH DGMXVWPHQW NQREV 6HOHFWLRQ
H[DPSOH/67 KLJKVLGH 567 ORZVLGH
ŏ 7KH WULP UDWH FDQ EH DGMXVWHG DQG WKH
RSHUDWLRQGLUHFWLRQFDQEHFKDQJHG
ŏ7ULPDFWVDVKLJKVLGHRUORZVLGHWULPZLWKWKH
FHQWHUDVWKHVWDQGDUG
+(/,&237(5
Setting method
Setting method
＜ Model Menu (Helicopter Functions) ＞ 155
7+5&XUYH7KURWWOH+RYHUWULP
7+5&XUYH
7KLVIXQFWLRQDGMXVWVWKHWKURWWOHRSHUDWLRQFXUYHIRU
HDFK FRQGLWLRQ IRU RSWLPL]LQJ WKH HQJLQH VSHHG WR
WKURWWOHVWLFNPRYHPHQW
$ WKURWWOH FXUYH IURP OLQHDU RSHUDWLRQ WR VPRRWK
FXUYHFDQEHVHW$GMXVWPHQWWRWKHFXUYH\RXZDQW
WRXVHLVSRVVLEOHE\XVLQJWKH0=:& VSRZHUIXO
&XUYH(GLW)XQFWLRQ8SWRFXUYHSRLQWVFDQEH
VHWKRZHYHUZKHQWKHSRLQWVDQGRWKHUSRLQWGDWD
LV XVHG D VPRRWK FXUYH FDQ EH HDVLO\ FUHDWHG E\
UHGXFLQJWKHQXPEHURISRLQWVRIWRDQGHQWHULQJ
WKHVSHFLÂżHGYDOXHDWWKHFRUUHVSRQGLQJSRLQWV
ŏ 7RXFK WKH >7+5 &XUYH@ EXWWRQ LQ WKH 0RGHO
0HQXWRFDOOWKHVHWXSVFUHHQVKRZQEHORZ
ŏ5HWXUQWR0RGHO0HQX
Normal curve adjustment
ŏ1RUPDOFXUYHFUHDWHVDEDVLFFXUYHFHQWHUHG
DURXQGKRYHULQJ8VHLWDORQJZLWKWKHQRUPDOSLWFK
FXUYHDQGDGMXVWVRWKDWXSGRZQFRQWURODWD
FRQVWDQWHQJLQHVSHHGLVHDVLHVW
Idle up curve adjustment
+(/,&237(5
ŏ6HWDQRUPDOXSFXUYHWKDWPDLQWDLQVDFRQVWDQW
VSHHGDWDOOWLPHVHYHQZKHQRSHUDWLRQZKLFK
UHGXFHVWKHSLWFKZDVSHUIRUPHGLQÁLJKW&UHDWH
DFXUYHPDWFKHGWRORRSUROO'RURWKHU
SXUSRVHVDQGWKHLGOHXSFXUYHDFFRUGLQJWRWKH
SHUIRUPDQFH
Operation precautions
WARNING
:KHQ DFWXDOO\ VWDUWLQJ WKH HQJLQH DQG IO\LQJ
DOZD\VVHWWKHLGOHXSFRQGLWLRQVZLWFKWR>2))@
DQGVWDUWWKHHQJLQHLQWKHLGOLQJPRGH
Setting method
ŏ*URXSEXWWRQ:KHQ\RXDOVRZDQWWRHQWHUWKH
GDWDWRDOORWKHUFRQGLWLRQVHQWHUWKHGDWDLQWKH
JURXSPRGH *53 :KHQGRLQJVRWKHVDPH
VHWWLQJVDUHLQSXWWRDOOWKHRWKHUFRQGLWLRQV
:KHQ\RXZDQWWRVHWGDWHLQWRHDFKFRQGLWLRQ
LQGHSHQGHQWO\VHOHFWWKHVLQJOH 61*/ PRGH
ŏ7KHFXUYHJUDSKGLVSOD\PRGHFDQEHVHOHFWHG7KLV
LVFRQYHQLHQWZKHQFKHFNLQJFXUYHVRWKHUWKDQWKH
RQHEHLQJVHW
 >6QJO@'LVSOD\VRQO\WKHFXUYHEHLQJVHW
 >)LQH7XQLQJ@:KHQ7KURWWOH+RYHUWULPLVXVHGD
FXUYHZLWKWULPDGMXVWPHQWDGGHGLVDOVRGLVSOD\HG
 >$OO&RQG@'LVSOD\VWKHWKURWWOHFXUYHRIDOOWKH
156 ＜ Model Menu (Helicopter Functions) ＞
FRQGLWLRQV7KHFXUYHRIWKHFRQGLWLRQFXUUHQWO\LQ
XVHLVLQGLFDWHGE\DEROGOLQH
 >3,7 7+5@7KHSLWFKFXUYHRIWKHFRQGLWLRQFXUUHQWO\
LQXVHLVDOVRGLVSOD\HG
ŏ7KHSLWFKFXUYHVHWXSVFUHHQFDQEHFDOOHGZLWK
RQHWRXFK7KLVLVFRQYHQLHQWZKHQDOWHUQDWHO\
DGMXVWLQJWKHVHFXUYHVZLWKWKHSLWFKFXUYH
ŏ7KHVHUYRVSHHGFDQEHVHW$GMXVWWKHWKURWWOH
VSHHGZKHQWKHWKURWWOHLVWRRVHQVLWLYH
Curve setting examples
7KHFXUYHVVKRZQEHORZZHUHFUHDWHGE\XVLQJWKH
/LQH PRGH DQG LQSXWWLQJ WKH GDWD RI WKH  SRLQWV
 ORZ VLGH    FHQWHU   
KLJK VLGHDWHDFKFRQGLWLRQ7KH\ZHUHFUHDWHGE\
UHGXFLQJWKHQXPEHUSRLQWVRIWKHOLQHWR:KHQ
DFWXDOO\FUHDWLQJDFXUYHHQWHUWKHGDWDVSHFLÂżHGSHU
WKHIXVHODJH RUWKHUHIHUHQFHYDOXH 
Ɣ7KURWWOH&XUYH ([DPSOH
Normal Curve
Idle-up 1 Curve
Idle-up 2 Curve
7KURWWOH+RYHUWULP
7KH7KURWWOH+RYHUWULPVHWXSVFUHHQFDQEHFDOOHGIURPWKH7+5&XUYHVHWXSVFUHHQ
ŏ5HWXUQWR0RGHO0HQX
ŏ6HWVWKHGLDOXVHG
7KH7KURWWOH+RYHUIXQFWLRQWULPVWKHWKURWWOHQHDU
WKHKRYHULQJSRLQW1RUPDOO\XVHLWZLWKKRYHULQJ
FRQGLWLRQV &KDQJHV LQ URWRU VSHHG DFFRPSDQ\LQJ
FKDQJHVLQWKHWHPSHUDWXUHKXPLGLW\DQGRWKHUÀLJKW
FRQGLWLRQVFDQEHWULPPHG$GMXVWWKHWKURWWOHVRWKDW
URWRUURWDWLRQLVPRVWVWDEOH0RUHGHOLFDWHWULPPLQJ
LVDOVRSRVVLEOHE\XVLQJWKLVIXQFWLRQDORQJZLWKWKH
+RYHU3LWFKIXQFWLRQ
Setting method
ŏ:KHQXVLQJWKHKRYHULQJ QRUPDO FRQGLWLRQRQO\
VZLWFKWKH>*U@ JURXSEXWWRQ PRGHWRWKH>6QJO@
VLQJOH PRGHDQGPDNHWKHVHWWLQJV
ŏ6HWWKHIXQFWLRQWR$&7 >21@ 
ŏ6HOHFWWKHDGMXVWPHQWNQRE6HOHFWLRQH[DPSOH5'
ŏ7KHWULPRSHUDWLRQPRGH 0RGH&7501250 FDQ
EHVHOHFWHG
 CTRM mode:0D[LPXPFKDQJHQHDUFHQWHUE\
FHQWHUWULPRSHUDWLRQ 'RHVQRWFKDQJHDWHQGRI
WKHVWLFNPRYHPHQW
 NORM mode: 1RUPDOWULP OLQHDU RSHUDWLRQ7KH
DGYDQWDJHRIXVLQJWKLVPRGHLVWKDWKRYHULQJ
WKURWWOHFDQEHDGMXVWHGZLWKRXWFKDQJLQJWKH
FXUYH
ŏ7ULPDGMXVWPHQWUDQJH 5DQJH VHWWLQJ
 :KHQWKHYDOXHLVPDGHVPDOOWULPDFWVRQO\QHDU
WKHFHQWHU
ŏ7KHWULPUDWHFDQEHDGMXVWHGDQGWKHRSHUDWLRQ
GLUHFWLRQFDQEHVHW
＜ Model Menu (Helicopter Functions) ＞ 157
+(/,&237(5
ŏ6HWV7KURWWOH+RYHUWULP
$FFHOHUDWLRQ0L[LQJ
$Q DFFHOHUDWLRQ IXQFWLRQ FDQ EH VHW7KLV LV XVHG
WR DGMXVW WKH SLWFK DQG WKURWWOH VHWWLQJV ZKHQ WKH
PL[WXUHLVHLWKHUWRRULFKRUWRROHDQZKLFKFDQEH
FDXVHGE\VXGGHQRSHUDWLRQRIWKHWKURWWOHVWLFN
ŏ7RXFKWKH>$FFHOHUDWLRQ@EXWWRQLQWKH0RGHO
0HQXWRFDOOWKHVHWXSVFUHHQVKRZQEHORZ
ŏ5HWXUQWR0RGHO0HQX
ŏ3LWFKVHWWLQJ
ŏ7KURWWOHVHWWLQJ
ŏ2SHUDWLRQSRLQWVHWWLQJ
+(/,&237(5
Setting method
ŏ$FFHOHUDWLRQFDQEHVHWDWERWKVHWWLQJDW
DFFHOHUDWLRQ KLJK DQGVHWWLQJDWGHFHOHUDWLRQ
ORZ 
 7KHRSHUDWLRQSRLQWLVGLVSOD\HGRQDJUDSK
ŏ$FFHOHUDWLRQUDWHVHWWLQJ 5DWH
ŏ7KHUHWXUQWLPHDIWHURSHUDWLRQ 'XPSLQJ FDQEH
VHW
ŏ7KHRSHUDWLRQSRLQWDWDFFHOHUDWLRQDQG
GHFHOHUDWLRQFDQEHVHW:KHQDQRSHUDWLRQSRLQWLV
H[FHHGHGDFFHOHUDWLRQLVSHUIRUPHG
Note: When using the Acceleration function, since
the pitch stroke is large, make your settings so there
is no binding of your linkage.
158 ＜ Model Menu (Helicopter Functions) ＞
7KURWWOH+ROG
7KLVIXQFWLRQVHWVWKHWKURWWOHFXWSRVLWLRQGXULQJDQ
DXWRURWDWLRQGLYH7KHWKURWWOHSRVLWLRQFDQDOVREH
VHWWRDQLGOLQJSRVLWLRQVHSDUDWHIURPWKHWKURWWOHFXW
SRVLWLRQ6HWWLQJRIWKHVHSRVLWLRQVFDQEHVHOHFWHG
E\ VZLWFK 7KLV DOORZV XVH IRU VZLWFKLQJ GXULQJ
WUDLQLQJ
ŏ7RXFKWKH>7KURWWOH+ROG@EXWWRQLQWKH0RGHO
0HQXWRFDOOWKHVHWXSVFUHHQVKRZQEHORZ
ŏ5HWXUQWR0RGHO0HQX
ŏ6HOHFWWKH6:WREHXVHG
ŏ6HWWRWKHHQJLQHVWRSSRVLWLRQ
Note: When throttle hold is set to ON in the normal
condition, throttle hold acts and the throttle servo
is deactivated. Always set throttle hold to ON in
the hold condition.
Operation precautions
WARNING
:KHQVWDUWLQJWKHHQJLQHFRQÂżUPWKDWWKHLGOHXS
FRQGLWLRQDQGWKURWWOHKROGFRQGLWLRQDUH>2))@
Setting method
ŏ2SHUDWLRQPRGHVHOHFWLRQ
 Manual mode:7KHWKURWWOHKROGIXQFWLRQLVRSHUDWHG
E\VZLWFKRSHUDWLRQRQO\
 Auto mode:7KHWKURWWOHKROGIXQFWLRQRSHUDWLRQLV
OLQNHGWRWKHWKURWWOHVWLFNSRVLWLRQ
 Auto position setting::KHQWKH$XWRPRGHZDV
VHOHFWHGWKHWKURWWOHSRVLWLRQ DXWRSRVLWLRQ FDQEH
VHOHFWHG0RYHWKHWKURWWOHVWLFNWRWKHSRVLWLRQ\RX
ZDQWWRVHWDQGWRXFKWKH DXWRSRVLWLRQ EXWWRQ
ŏ+ROGSRVLWLRQDGMXVWPHQW
 Throttle Hold (Cut)VHWVWKHWKURWWOHFXWSRVLWLRQ
$GMXVWLWVRWKDWWKHFDUEXUHWRULVIXOORSHQ
 Throttle Hold (Idle):0DNHWKLVDGMXVWPHQWWR
PDLQWDLQLGOLQJIRUWUDLQLQJ$GMXVWPHQWVFDQEH
PDGHEDVHGRQWKHWKURWWOHFXUYHLGOHSRVLWLRQ
ŏ7KHWKURWWOHVHUYRRSHUDWLQJVSHHGFDQEHDGMXVWHG
6SHHG
ŏ7KH+ROGVZLWFKFDQEHXVHGWRFKDQJHEHWZHHQ
WKH7KURWWOHFXWRU7UDLQLQJIXQFWLRQ
＜ Model Menu (Helicopter Functions) ＞ 159
+(/,&237(5
Example of use
ŏ 6LQFH 7KURWWOH +ROG KDV  PRGHV &XW  DQG
,GOH  LW LV FRQYHQLHQW WR XVH LW LQ WKH ,GOH
PRGH GXULQJ WUDLQLQJ DQG LQ WKH &XW PRGH
ZKHQVWRSSLQJWKHHQJLQH
ŏ6HWWRWKHLGOLQJSRVLWLRQ
6ZDVK0L[LQJ
7KHVZDVKPL[IXQFWLRQLVXVHGWRFRUUHFWWKHVZDVK
SODWHLQWKHDLOHURQ UROO GLUHFWLRQDQGHOHYDWRU F\FOLF
SLWFK  FRUUHVSRQGLQJ WR HDFK RSHUDWLRQ RI HDFK
FRQGLWLRQ
$GMXVWPHQW E\ LQGHSHQGHQW FXUYH IRU DLOHURQ
HOHYDWRU DQG SLWFK RSHUDWLRQV LV SRVVLEOH 7KH
RSHUDWLRQ FDQ EH VPRRWKO\ DGMXVWHG E\ FDOOLQJ XS
WKH³&XUYHVHWXS´VFUHHQE\WRXFKLQJWKHEXWWRQWKDW
FRUUHVSRQGVWRWKHPL[LQJDQGGLUHFWLRQZKLFKQHHGV
FRUUHFWLRQ
Example of use
ŏ$VDQH[DPSOHXVHVZDVKPL[LQJWRFRUUHFW
XQGHVLUDEOHWHQGHQFLHVLQWKHUROOGLUHFWLRQ
ŏ)RUDFRQGLWLRQZKLFKXVHV$,/WR(/(VHWWKLV
IXQFWLRQ WR 21 :KHQ UDLVLQJ WKH QRVH DW D
ULJKW UROO ZKHQ WKH 5DWH % VLGH LV LQSXW DQG
WKH ULJKW DLOHURQ LV RSHUDWHG WKH HOHYDWRU
PRYHV WR WKH GRZQ VLGH 7XQH E\ DGMXVWLQJ
WKH 5DWH )RU ULJKW UROO DGMXVW WR WKH 5DWH $
VLGH
ŏ 7RXFK WKH >6ZDVK 0L[@ EXWWRQ LQ WKH 0RGHO
0HQXWRFDOOWKHVHWXSVFUHHQVKRZQEHORZ
ŏ5HWXUQWR0RGHO0HQX
+(/,&237(5
Setting method
ŏ:KHQXVLQJWKLVIXQFWLRQWRXFKWKH>,1+@EXWWRQDQG
GLVSOD\>21@RU>2))@
ŏ:KHQ\RXZDQWWRVHWWKHVDPHVHWWLQJVWRRWKHU
FRQGLWLRQVVHOHFWWKHJURXSPRGH *U :KHQ\RX
ZDQWWRDGGVHWWLQJVWRWKHVHOHFWHGFRQGLWLRQRQO\
VHOHFWWKHVLQJOHPRGH 6QJO 
ŏ7KHFRUUHFWLRQUDWHFDQEHVHWE\FXUYH
ŏ$VZLWFKFDQEHVHW
 :KHQ>21@LVVHWWKHVZDVKPL[LQJIXQFWLRQLV
RSHUDWHGE\PHUHO\VHOHFWLQJWKHFRQGLWLRQ
 :KHQVHWWLQJDQ>21@>2))@VZLWFKWRXFKWKH>21@
EXWWRQDQGVHWWKHVZLWFKDQGLWV21SRVLWLRQDWWKH
6ZLWFK!VFUHHQ
160 ＜ Model Menu (Helicopter Functions) ＞
ŏ 7ULPRQRIIVHWWLQJ
 7KURWWOH0L[@EXWWRQLQWKH0RGHO
0HQXWRFDOOWKHVHWXSVFUHHQVKRZQEHORZ
ŏ5HWXUQWR0RGHO0HQX
Setting method
ŏ:KHQXVLQJWKLVIXQFWLRQWRXFKWKH>,1+@EXWWRQDQG
GLVSOD\>21@RU>2))@
ŏ:KHQ\RXZDQWWRVHWWKHVDPHVHWWLQJVWRRWKHU
FRQGLWLRQVVHOHFWWKHJURXSPRGH *U :KHQ\RX
ZDQWWRDGGVHWWLQJVWRWKHVHOHFWHGFRQGLWLRQRQO\
VHOHFWWKHVLQJOHPRGH 6QJO 
ŏ7KHFRUUHFWLRQUDWHFDQEHVHWE\FXUYH
ŏ$VZLWFKFDQEHVHW
 :KHQ>21@LVVHWWKHIXQFWLRQLVRSHUDWHGE\PHUHO\
VHOHFWLQJWKHFRQGLWLRQ
 :KHQVHWWLQJDQ>21@>2))@VZLWFKWRXFKWKH>21@
EXWWRQDQGWKHQVHWWKHVZLWFKDQGLWV21GLUHFWLRQ
DWWKH6ZLWFK!VFUHHQ

ŏ $FFHOHUDWLRQ FDQ EH VHW IRU ERWK VHWWLQJV
+LJK  DQG /RZ  DW PD[LPXP FRUUHFWLRQ
UDWH
ŏ$FFHOHUDWLRQUDWHVHWWLQJ 5DWH
ŏ7KHUHWXUQWLPH 'XPS DIWHURSHUDWLRQFDQ
EHVHW
ŏ 7KH RSHUDWLRQ SRLQW ZKHQ WKH FRUUHFWLRQ
UDWHLVLQFUHDVHGDQGGHFUHDVHGFDQEHVHW
LQGHSHQGHQWO\ :KHQ DQ RSHUDWLRQ SRLQW
LV H[FHHGHG DFFHOHUDWLRQ RSHUDWLRQ LV
SHUIRUPHG
＜ Model Menu (Helicopter Functions) ＞ 161
+(/,&237(5
ŏ0RGHVHOHFWLRQ
3,7WR1HHGOH0L[LQJ
7KLV PL[LQJ LV XVHG ZKHQ WKH HQJLQH LV HTXLSSHG
ZLWK QHHGOH FRQWURO RU RWKHU IXHODLU PL[WXUH
DGMXVWPHQW$QHHGOHFXUYHFDQEHVHW
7KH$FFHOHUDWLRQ IXQFWLRQ ZKLFK FDQ WHPSRUDULO\
LQFUHDVHQHHGOHRSHUDWLRQGXULQJWKURWWOHDFFHOHUDWLRQ
GHFHOHUDWLRQ RSHUDWLRQ FDQ EH VHW 7KH ULVH
FKDUDFWHULVWLFRIWKHQHHGOHVHUYRGXULQJDFFHOHUDWLRQ
DQGGHFHOHUDWLRQRSHUDWLRQFDQEHDGMXVWHG
ŏ7RXFKWKH>3,7WR1HHGOH@EXWWRQLQWKH0RGHO
0HQXWRFDOOWKHVHWXSVFUHHQVKRZQEHORZ
ŏ1RUPDOO\XVH>/LQHDU@W\SH
ŏ5HWXUQWR0RGHO0HQX
+(/,&237(5
Setting method
ŏ:KHQXVLQJWKLVIXQFWLRQWRXFKWKH>,1+@EXWWRQDQG
GLVSOD\>21@RU>2))@
ŏ:KHQ\RXZDQWWRVHWWKHVDPHVHWWLQJVWRRWKHU
FRQGLWLRQVVHOHFWWKHJURXSPRGH *U :KHQ\RX
ZDQWWRDGGVHWWLQJVWRWKHVHOHFWHGFRQGLWLRQRQO\
VHOHFWWKHVLQJOHPRGH 6QJO 
ŏ$QHHGOHFXUYHFDQEHVHW
ŏ$VZLWFKFDQEHVHW
 :KHQ>21@LVVHWWKHIXQFWLRQLVRSHUDWHGE\PHUHO\
VHOHFWLQJWKHFRQGLWLRQ
 :KHQVHWWLQJDQG>21@>2))@VZLWFKWRXFKWKH>21@
EXWWRQDQGVHWWKHVZLWFKDQGLWV21GLUHFWLRQDWWKH
6ZLWFK!VFUHHQ
162 ＜ Model Menu (Helicopter Functions) ＞
< Acceleration function setting>
ŏ$FFHOHUDWLRQ FDQ EH VHW DW ERWK VHWWLQJ
DW DFFHOHUDWLRQ +LJK  DQG VHWWLQJ DW
GHFHOHUDWLRQ /RZ 
ŏ7KHDFFHOHUDWLRQUDWH 5DWH DQGWKHUHWXUQ
WLPHDIWHURSHUDWLRQ 'XPS FDQEHVHW
ŏ$Q RSHUDWLRQ SRLQW 2SHUDWLRQ 3RLQW  DW
DFFHOHUDWLRQ DQG GHFHOHUDWLRQ FDQ EH
VHW :KHQ DQ RSHUDWLRQ SRLQW LV H[FHHGHG
DFFHOHUDWLRQRSHUDWLRQLVSHUIRUPHG
3,7WR58'0L[LQJ 5HYROXWLRQ0L[LQJ
8VH WKLV PL[LQJ ZKHQ \RX ZDQW WR VXSSUHVV WKH
UHDFWLRQ WRUTXH JHQHUDWHG E\ PDLQ URWRU SLWFK DQG
VSHHGFKDQJHVDWSLWFKRSHUDWLRQ$GMXVWVRWKDWWKH
QRVHGRHVQRWPRYHLQWKHUXGGHUGLUHFWLRQ
$QDFFHOHUDWLRQIXQFWLRQZKLFKWHPSRUDULO\LQFUHDVHV
WKH FRUUHFWLRQ UDWH DW WKURWWOH VWLFN DFFHOHUDWLRQ
GHFHOHUDWLRQRSHUDWLRQFDQEHVHW7KHPL[LQJUDWHDW
DFFHOHUDWLRQGHFHOHUDWLRQFDQEHVHW
+RZHYHUZKHQD*<6HULHVRURWKHUKHDGLQJKROG
J\URLVXVHGVLQFHFRUUHFWLRQLVSHUIRUPHGE\WKH
J\URWKLVPL[LQJLVQRWXVHGIf this function is used
when the gyro operation mode is the AVCS mode,
the neutral position will change.
ŏ7RXFKWKH>3,7WR58'@EXWWRQLQWKH0RGHO
0HQXWRFDOOWKHVHWXSVFUHHQVKRZQEHORZ
ŏ5HWXUQWR0RGHO0HQX
ŏ1RUPDOO\XVH>/LQH@W\SH
Setting method
ŏ:KHQXVLQJWKLVIXQFWLRQWRXFKWKH>,1+@EXWWRQDQG
GLVSOD\>21@RU>2))@
ŏ:KHQ\RXZDQWWRVHWWKHVDPHVHWWLQJVWRRWKHU
FRQGLWLRQVVHOHFWWKHJURXSPRGH *U :KHQ\RX
ZDQWWRDGGVHWWLQJVWRWKHVHOHFWHGFRQGLWLRQRQO\
VHOHFWWKHVLQJOHPRGH 6QJO
ŏ$PL[LQJFXUYHLVVHW
 7KH PL[LQJ FXUYH UDWH VWDUWV IURP D VPDOO
YDOXH
 )RU D URWRU ZLWK D FORFNZLVH RSHUDWLRQ
GLUHFWLRQ SRODULW\ ZKHQSLWFKZDVRSHUDWHG
DW WKH SOXV VLGH VHW VR WKDW PL[LQJ LV LQ WKH
FORFNZLVH GLUHFWLRQ )LUVW WULP DW KRYHULQJ
DQGWKHQDGMXVWWKHQHXWUDOSRVLWLRQ
$GMXVWPHQWEHWZHHQVORZDQGKRYHULQJ
 5HSHDWHGO\ KRYHU IURP WDNH RII DQG ODQG
IURP KRYHULQJ DW D FRQVWDQW UDWH PDWFKHG
WR\RXURZQUK\WKPDQGDGMXVWWKHSLWFKVR
WKHQRVHGRHVQRWGHÁHFWZKHQWKHWKURWWOH
LVUDLVHGDQGORZHUHG
 7KURWWOH KLJK VLGH XS WR FOLPELQJ IURP
KRYHULQJDQGGLYLQJKRYHULQJ
5HSHDW FOLPELQJ DQG GLYLQJ IURP KRYHULQJ DW D
FRQVWDQW UDWH PDWFKHG WR \RXU RZQ UK\WKP DQG
DGMXVWWKHSLWFKVRWKDWWKHQRVHGRHVQRWGHÁHFW
ZKHQWKHWKURWWOHLVUDLVHGDQGORZHUHG

 6HWWKHPL[LQJUDWHVRWKDWWKHUXGGHU
GLUHFWLRQDWKLJKVSHHGÁLJKWLVVWUDLJKW
DKHDG$GMXVWIRUHDFKFRQGLWLRQXVHG

ŏ $Q DFFHOHUDWLRQ IXQFWLRQ FDQ EH VHW 7KLV LV
XVHG ZKHQ WKH PL[WXUH LV HLWKHU WRR ULFK RU
WRR OHDQ ZKLFK FDQ EH FDXVHG E\ VXGGHQ
RSHUDWLRQRIWKHWKURWWOHVWLFN
ŏ$FFHOHUDWLRQUDWHVHWWLQJ 5DWH
ŏ7KHUHWXUQWLPHDIWHURSHUDWLRQ 'XPS FDQ
EHVHWIRUERWKVHWWLQJV $FFHOHUDWLRQ +LJK 
DQG 'HFHOHUDWLRQ /RZ 
ŏ$Q2SHUDWLRQ3RLQWGXULQJDFFHOHUDWLRQDQG
GHFHOHUDWLRQ FDQ EH VHW LQGHSHQGHQWO\
:KHQ WKLV SRLQW LV H[FHHGHG DFFHOHUDWLRQ
RSHUDWLRQLVSHUIRUPHG
＜ Model Menu (Helicopter Functions) ＞ 163
+(/,&237(5

*\UR0L[LQJ
7KLVIXQFWLRQLVXVHGZKHQDJ\URLVXVHGWRVWDELOL]H
WKHIXVHODJHDWWLWXGH7KHVHQVLWLYLW\DQGRSHUDWLRQ
PRGH 1RUPDOPRGH*<PRGH FDQEHVHWXSZLWK
WKUHHJ\URVIRUHDFKFRQGLWLRQUHVSHFWLYHO\
6HQVLWLYLW\ DQG RSHUDWLRQDO PRGH 1RUPDO PRGH
*< PRGH  FDQ EH VHW XS IRU WKUHH *\URV IRU HDFK
FRQGLWLRQUHVSHFWLYHO\
Note:$OZD\VVHWERWK $&7 DQG 7ULP IRUWKH>*\UR@
IXQFWLRQ
Setting example
ŏ 1RUPDOO\ LW LV FRQYHQLHQW WR SUHVHW KLJK
VHQVLWLYLW\ 5DWH   DQG ORZ VHQVLWLYLW\ 5DWH
  ZKHQ HLWKHU WKH $9&6 PRGH RU 1RUPDO
PRGHLVXVHG
ŏ $ VHWXS RI WKH PRGH RI  *\URV DQG 5HWH
ŏ7RXFKWKH>*\UR@EXWWRQLQWKH0RGHO0HQX
FDQEHSHUIRUPHGRQWKLVVFUHHQ
WRFDOOWKHVHWXSVFUHHQVKRZQEHORZ
ŏ5HWXUQWR0RGHO0HQX
ŏ$GHWDLOHGVHWXSRIHDFK*\URFDQEH
SHUIRUPHGRQWKLVVFUHHQ
ŏ5HWXUQWR*\UR0HQX
+(/,&237(5
ŏ6HOHFWVWKHVHOHFWRUVZLWFK
ŏ$GMXVWVWKHJ\URVHQVLWLYLW\E\UDWH
ŏ6HOHFWV>$9&6@RU>125@ QRUPDO 
ŏ6HOHFWWKHW\SHRIJ\URXVHG
Setting method
ŏ7RXFKWKH>,1+@EXWWRQRIWKHUDWHWREHXVHGDQG
GLVSOD\>21@
ŏ:KHQ\RXZDQWWRVHWWKHVDPHVHWWLQJVWRRWKHU
FRQGLWLRQVVHOHFWWKHJURXSPRGH *U :KHQ\RX
ZDQWWRDGGVHWWLQJVWRWKHVHOHFWHGFRQGLWLRQRQO\
VHOHFWWKHVLQJOHPRGH 6QJO 
ŏ7KUHHUDWHVFDQEHVZLWFKHGIRUHDFKFRQGLWLRQ
5DWH5DWH5DWH
ŏ$ÀQHWXQLQJ95FDQEHVHW
164 ＜ Model Menu (Helicopter Functions) ＞
*RYHUQRU0L[LQJ
7KLVLVXVHGWRVZLWFKWKH530RIWKHKHOLFRSWHUV
KHDG8SWRUDWHVFDQEHVHWIRUHDFKFRQGLWLRQ
7KHJRYHUQRULVXVHGE\FRQQHFWLQJWKHJRYHUQRUVSHHGVHWWLQJ
FKDQQHOWRJRYHUQRUIXQFWLRQ
:KHQ XVLQJ DQ LQGHSHQGHQW JRYHUQRU >21@>2))@ VZLWFK
FRQQHFWWKH$8; >21@>2))@ FRQQHFWRURIWKHJRYHUQRUWR
*RYHUQRUDQGVHWWKHVZLWFKWR*RYHUQRUDWWKH)XQFWLRQ
PHQXRIWKH/LQNDJH0HQX
:KHQXVLQJWKH)XHO0L[WXUHIXQFWLRQWKHPL[WXUHVHUYRLV
FRQWUROOHGIURPWKHJRYHUQRU:KHQWUDQVPLWWLQJWKHPL[WXUH
FXUYHGDWDIURPWKHWUDQVPLWWHUWRWKHJRYHUQRUWKHJRYHUQRU
$8; PWUP  FRQQHFWRU PXVW EH FRQQHFWHG WR *RYHUQRU
IXQFWLRQ DQG JRYHUQRU VLGH VHWWLQJ SHUIRUPHG 6HH WKH
JRYHUQRULQVWUXFWLRQPDQXDO
Note: Always set (Act) and (Trim) to [NULL] for
[Governor] and [Governor 2] of the Function
menu.
The subtrim of [Governor] is made 0%.
Make the reverse direction normal.
ŏ 7RXFK WKH >*RYHUQRU@ EXWWRQ RI WKH 0RGHO
0HQXWRFDOOWKHVHWXSVFUHHQVKRZQEHORZ
ŏ5HWXUQWR0RGHO0HQX
ŏ:KHQWKH´0RGHµEXWWRQRQ
WKH*RYHUQRUVFUHHQLV
SUHVVHGWKHGLVSOD\PRGHLV
VZLWFKHG
USPPRGH
USPPRGH
ŏ7KHUSPPRGHDQGUSPPRGHDUHGLIIHUHQWZKHQWKH
UDWH LV  USP  RU JUHDWHU $W UDWHV EHORZ  WKH
USPGLVSOD\LVWKHVDPHIRUERWKPRGHV
ŏ:KHQWKHUSPPRGHLVVHW USP
7KHPD[LPXPYDOXHLV USP
ŏ:KHQWKHUSPPRGHLVVHW USP
7KHPD[LPXPYDOXHLV USP &RQYHQWLRQDO
VSHFLÀFDWLRQV 
ŏ 7KHUH LV QR FKDQJH LQ WKH WUDQVPLWWHU RXWSXW HYHQ ZKHQ WKH
USP PRGH DQG USP PRGH DUH VZLWFKHG &DOLEUDWLRQ
PXVWEHSHUIRUPHGDWWKHJRYHUQRUVLGH
 $OVRWKLVPL[LQJDQGWKHJRYHUQRUVLGHVSHHGVHWWLQJ
PXVWEHPDWFKHGEHIRUHKDQGE\WKHIROORZLQJ
PHWKRG
ŏ6HWVRWKDWZKHQWKHJRYHUQRUVLGHLVSODFHGLQ
WKHVSHHGVHWWLQJLWHPVWDWHDQG>USP@RI6HW
*29RIWKHVFUHHQDERYHLVWRXFKHGWKHJRYHUQRU
VSHHGLVVHWWRZKHQWKH>USP@EXWWRQ
LVWRXFKHGWKHJRYHUQRUVSHHGLVVHWWR
DQGZKHQWKH>USP@EXWWRQLVWRXFKHGWKH
JRYHUQRUVSHHGLVVHWWR
ŏ:KHQ\RXZDQWWRUHDGWKHVSHHGGLUHFWO\SUHVVWKH
>@EXWWRQDQGGLVSOD\>USP@
ŏ7KHVSHHGFDQEHZLWFKHGE\VHWWLQJDVZLWFK
$OVRZKHQ>2))@LVVHWLQVWHDGRIVSHHGVHWWLQJWKH
JRYHUQRUFDQEHWXUQHG>21@>2))@ZLWKRXWVHWWLQJ
DVHSDUDWH>21@>2))@VZLWFK
ŏ$VSHHGÀQHWXQLQJ95FDQEHVHW
95 VHOHFWLRQ DGMXVWPHQW ZLGWK DQG DGMXVWPHQW
GLUHFWLRQFDQEHVHW
＜ Model Menu (Helicopter Functions) ＞ 165
+(/,&237(5
Setting method
ŏ7RXFKWKH>,1+@EXWWRQRIWKHUDWHWREHXVHGDQG
GLVSOD\>21@
ŏ:KHQ\RXZDQWWRVHWWKHVDPHVHWWLQJVWRRWKHU
FRQGLWLRQVVHOHFWWKHJURXSPRGH *U :KHQ\RX
ZDQWWRDGGVHWWLQJVWRWKHVHOHFWHGFRQGLWLRQRQO\
VHOHFWWKHVLQJOHPRGH 6QJO 
ŏ7KUHHVSHHGV UDWHV FDQEHVHWIRUHDFKFRQGLWLRQ
5DWH5DWH5DWH
ŏ(QGSRLQWLQLWLDOL]DWLRQ
7KHJRYHUQRURXWSXWFKDQQHOHQGSRLQW $79 
´WUDYHO¾DQG´OLPLW¾DUHQRZLQLWLDOL]HGZKHQWKH
JRYHUQRUVHWWLQJ´2SHUDWH¾EXWWRQZDVSUHVVHG
ŏ:KHQVZLWFKHGIURP,1+WR21RU2))´WUDYHOµLV
LQLWLDOL]HGWRDQG´OLPLW¾LVLQLWLDOL]HGWR
ŏ:KHQ´2SHUDWHµRIUDWHVDQGLVVZLWFKHG
WR,1+XQGHUDOOFRQGLWLRQV´WUDYHO¾LVLQLWLDOL]HGWR
DQG´OLPLW¾LVLQLWLDOL]HGWR
7KURWWOH/LPLWHU
7KLVIXQFWLRQOLPLWVWKHKLJKUDQJHRIWKHWKURWWOH
PRYHPHQWE\DQ\VOLGHURUWULPPHU7KHDGMXVWPHQW
UDQJHRIWKHKLJKDQGORZHQGFDQEHVHW
ŏ 7RXFK WKH >7KURWWOH /LPLWHU@ EXWWRQ RI WKH
0RGHO0HQXWRFDOOWKHVHWXSVFUHHQVKRZQ
EHORZ
ŏ5HWXUQWR0RGHO0HQX
&RQWUROVHOHFWLRQ
EXWWRQ
5DQJHJDXJH
5DWHDGMXVWEXWWRQ
Setting method
ŏ$FWLYDWHWKHPL[LQJDQGVHOHFWWKHRQRIIVZLWFK
ŏ6HOHFWWKHFRQWUROIRUDGMXVWPHQWRIWKHKLJKOLPLW
ŏ6HWWKHKLJKUDQJH7KHUDQJHJDXJHVKRZVWKH
VHWWLQJSRVLWLRQ
ŏ6HWWKHORZUDQJHVDPHDVKLJKUDQJHVHWWLQJ
+(/,&237(5
The limit value at the operation hardware neutral position can now be adjusted using the throttle limiter.
6HW´&HQWHUSRVLWLRQ¾RQWKHWKURWWOHOLPLWHU VFUHHQWR2SHUDWH
:KHQWKH´&HQWHUSRVLWLRQ¾UDWHLVFKDQJHGWKHOLPLWYDOXHDWWKHRSHUDWLRQKDUGZDUHQHXWUDOSRVLWLRQFDQEH
DGMXVWHG
ŏ7KHOLPLWYDOXHDWWKHRSHUDWLRQKDUGZDUHQHXWUDOSRVLWLRQZKHQ´&HQWHUSRVLWLRQµZDVFKDQJHGWR,1+ DW
FRQYHQWLRQDORSHUDWLRQ LVWKHFHQWHUYDOXHEHWZHHQ´+LJKVLGHUDQJH¾DQG´/RZVLGHUDQJH¾
ŏ:KHQ´&HQWHUSRVLWLRQµZDVVZLWFKHGIURP,1+WR2SHUDWHWKH´&HQWHUSRVLWLRQµUDWHLVUHVHWWRWKHFHQWHUYDOXH
EHWZHHQ´+LJKVLGHUDQJH¾DQG´/RZVLGHUDQJH¾
ŏ7KH´&HQWHUSRVLWLRQµUDWHFDQEHVHWEHWZHHQ´+LJKVLGHUDQJHµDQG´/RZVLGHUDQJHµ
166 ＜ Model Menu (Helicopter Functions) ＞
&2002123(5$7,21686(',1)81&7,216(783
6&5((1
This section describes the functions often used at the function setup screen. Refer to it when setting each
function.
2SHUDWLRQVUHODWHGWRÀLJKWFRQGLWLRQV
Group/single mode switching (Gr./Sngl)
*U
:KHQVHWWLQJPXOWLSOHÀLJKW
conditions, linking the setting contents
with other conditions (Gr.) or setting
independently (Sngl) can be selected.
When the button is touched, it toggles
between Gr. and Sngl.
*Group mode (Gr.) (initial setting): The same
setting contents are set to all the flight
conditions in the group mode.
*Single mode (Sngl): Select this mode when
the setting contents are not linked with
other conditions.
*Selecting the single (Sngl) mode at each
condition after presetting in the group
mode (Gr.) is convenient.
Condition delay setting
Unnecessary fuselage motion generated when
there are sudden changes in the servo position and
variations in the operating time between channels
at condition switching can be suppressed.
When the delay function is set at the switching
destination condition, a delay corresponding to
that amount is applied and the related functions
change smoothly.
Operations related to VR tuning
Fine tuning VR setting
ŏ95VHOHFWLRQ
ŏ5DWHDGMXVWPHQW
)LQH7XQLQJ
/'


ŏ2SHUDWLRQPRGHVHOHFWLRQ
*Displayed at VR setting.
ŏ$GMXVWPHQWGLUHFWLRQ
setting
>2SHUDWLRQPRGHV@
Mixing rate 0% at center of VR
When the VR is turned counterclockwise
and clockwise, the mixing rate increases
and decreases, respectively.
Mixing rate 0% at left end of VR
When the VR is turned, the mixing rate
increases.
Mixing rate 0% at right end of VR.
When the VR is turned, the mixing rate
increases.
When the VR is turned to the left or right
of the neutral position, the mixing rate
increases.
>6HWWLQJPHWKRG@
1. Switch to the condition you want to set.
2. Touch the Delay button.
8VHWKHDGMXVWPHQWEXWWRQVWRVHWWKHGHOD\
*Initial value: 0
 $GMXVWPHQWUDQJHa PD[LPXPGHOD\
＜ Data ＞ 167
Operations related to servo speed
speed corresponding to the set speed.
Master mode: The servo movement is
traced by the setting curve. The trace
VSHHGLVDGMXVWHGE\LQDQGRXWVSHHG
Servo speed setting (1)
6SHHG
,1
287
The speed during operation (including flight
condition switching) can be adjusted. The
servos operate smoothly at a constant speed
corresponding to the speed set for them. The
operation speed (In Speed) and the return speed
(Out Speed) can be set individually.
Switch the operation mode according to the set
function. When the button is touched, it toggles
between [LIN] and [SYM].
"SYM" mode: Mode used with ailerons and
other self-neutral functions
"LIN" mode: Mode used with functions which
hold the operation position of the throttle
and switch channel, etc.
>6HWWLQJPHWKRG@
 6HOHFW WKH IXQFWLRQ >/,1@ RU
>6<0@ PDWFKHGWRWKHPDVWHU
channel. Each time the
button is touched, it toggles
5HVHW
EHWZHHQ>/,1@DQG>6<0@
 7RXFK WKH ,Q RU 2XW 6SHHG
button and set the servo
speed.
Initial value: 0
6HWWLQJUDQJHa
Servo speed setting (2) (Prog. Mix only)
6HUYR6SHHG
,Q6SHHG
2XW6SHHG
6WDUW'HOD\
ۢ
6WRS'HOD\
ۢ
&ORVH
6ODYH
Speed mode: Slave/Master
The speed mode can be selected.
Slave mode: The speed at programmable
PL[LQJ VZLWFKLQJ FDQ EH DGMXVWHG 7KH
servos operate smoothly at a constant
168 ＜ Data ＞
>6HWWLQJPHWKRG@
1. When setting the servo speed, touch the
Speed button. The Servo Speed setup
screen shown above is displayed.
6HOHFWWKHIXQFWLRQ >/,1@RU>6<0@ PDWFKHG
to the master channel. Each time the
EXWWRQLVWRXFKHGLWWRJJOHVEHWZHHQ>/,1@
DQG>6<0@
"SYM" mode: Mode used with ailerons and
other self-neutral functions.
"LIN" mode: Mode used with functions
which hold the operating position of the
throttle and switch channel, etc.
3. Touch the In Speed button and set the
servo speed.
Initial value: 0
 6HWWLQJUDQJHa
 7RXFK WKH 2XW 6SHHG EXWWRQ DQG VHW WKH
servo speed.
Initial setting: 0
 6HWWLQJUDQJHa
5. Touch the Start Delay button and set the
GHOD\ WLPH IURP VZLWFK 21 WR WKH VWDUW RI
function operation.
Initial setting: 0.0 sec
 6HWWLQJUDQJHaVHFV
6. Touch the Stop Delay button and set the
GHOD\ WLPH IURP VZLWFK 2)) WR WKH VWDUW RI
function operation.
Initial setting: 0
 6HWWLQJUDQJHaVHFV
$WPDVWHUPRGH
1. Set desired in and out speed.
2. Select the master channel to any toggle
switch.
3. The slave channel's servo traces the setting
curve as the master toggle switch is moved.
%HORZWKHFDVH$8;VHUYRWUDFHVDQ(;3
FXUYHDVWKH6:)LVRSHUDWHG
&XUYHVHWWLQJRSHUDWLRQ
This section describes the setting procedure of curves which are used with the AFR function and each mixing
function.
Curve type selection
When the curve type select button on the mixing function screen or other screen is touched, the setup screen
shown below is called.
ŏ5HWXUQWRRULJLQDOVHWXS
screen of original function
Curve type selection
1. Touch the button of the curve type you want to use.
*The curve type changes and the display returns to the original screen.
When curve type is changed:
The curve shape is inherited when the curve type
is changed.
([DPSOH&KDQJHVIURP(;3WR/LQHFXUYHW\SH
retrieved from the previous setting data when
changing the curve type.
At the curve type changes, the dialogue box asks
whether the current curve is reset or inherited. The
default curve is used when selecting the Yes button
RQWKHFRQÂżUPDWLRQGLDORJXH
Changed to line or spline mode, the curve is
retrieved as 17 points curve.
The Rate A and Rate B are inherited on the
linear, EXP1, EXP2 and VTR.
Other data except Rate A and Rate B are
＜ Data ＞ 169
Setting by curve type
When the curve type is selected as described above, adjustment buttons corresponding to the curve type appear
on the original screen. Adjust each curve as described below.
Linear curve adjustment
(Linear curve)
Rate A and Rate B can be adjusted separately or
simultaneously.
>6HWWLQJPRGHV@
*[Separate] mode:5DWHVDUHDGMXVWHG
separately.
*[Combined] mode:5DWHVDUHDGMXVWHG
simultaneously.
>6HWWLQJPHWKRG@
1. Select the setting mode.
7RXFKWKH5DWH$RU5DWH%EXWWRQ
8VHWKHDGMXVWPHQWEXWWRQVWRVHWWKHUDWH
*Initial value: +100.0%
 $GMXVWPHQWUDQJHa
The curve can also be offset horizontally in the
vertical direction and the rate reference point can be
offset to the left or right.
>2IIVHWWLQJ WKH FXUYH KRUL]RQWDOO\ LQ WKH YHUWLFDO
GLUHFWLRQ@
7RXFKWKH2IIVHWEXWWRQ
8VHWKHDGMXVWPHQWEXWWRQVWRPRYHWKHFXUYH
KRUL]RQWDOO\XSDQGGRZQ
*Initial value: +0.0%
>2IIVHWWLQJWKHUDWHUHIHUHQFHSRLQW
WRWKHOHIWRUULJKW@
7RXFKWKH;2IIVHWEXWWRQ
 8VH WKH DGMXVWPHQW EXWWRQV WR
move the reference point to the
left or right.
*Initial value: +0.0%
170 ＜ Data ＞
5DWHDGMXVWPHQWEXWWRQV
5HVHW
ŏ5HWXUQWRLQLWLDOYDOXH
EXP1 curve adjustment
(;3FXUYH
Rate A and Rate B can be adjusted separately or
simultaneously. The EXP curves rate (EXP A, EXP B)
can also be adjusted separately or simultaneously.
>6HWWLQJPRGHV@
*[Separate] mode:5DWHVDUHDGMXVWHG
separately.
*[Combined] mode:5DWHVDUHDGMXVWHG
simultaneously.
>6HWWLQJPHWKRG@
1. Select the setting mode.
7RXFKWKHEXWWRQRIWKHUDWHRU(;3FXUYHUDWH
your want to set.
8VHWKHDGMXVWPHQWEXWWRQVWRVHWWKHUDWH
 ,QLWLDOYDOXH UDWH  (;3UDWH
ŏ8VLQJWKH(;3FXUYHLVKHOSIXOLQ
smoothening starting of the ailerons,
elevators, rudder, etc.
(;3FXUYH
The curve can also be horizontally offset in the
vertical direction.
>2IIVHWWLQJ WKH FXUYH KRUL]RQWDOO\ LQ WKH YHUWLFDO
GLUHFWLRQ@
7RXFKWKH2IIVHWEXWWRQ
8VHWKHDGMXVWPHQWEXWWRQVWRPRYHWKHFXUYH
KRUL]RQWDOO\XSRUGRZQ
*Initial value: +0.0
VTR curve adjustment
Rate A and Rate B can be adjusted separately or
simultaneously. The VTR curve point positions (P.
Pos. A, P. Pos. B) and rates (P. Rate A, P. Rate B) can
also be adjusted separately or simultaneously.
>6HWWLQJPRGHV@
*[Separate] mode:3RVLWLRQVDQGUDWHVDUH
DGMXVWHGVHSDUDWHO\
*[Combined] mode:3RVLWLRQVDQGUDWHVDUH
DGMXVWHGVLPXOWDQHRXVO\
>6HWWLQJPHWKRG@
1. Select the setting mode.
2. Touch the button of the rate or VTR curve
point position (or rate) you want to set.
 8VH WKH DGMXVWPHQW EXWWRQV WR VHW WKH 975
curve point position (or rate).
 ,QLWLDOYDOXHV 5DWH  33RV$ 
 33RV%  35DWH
The curve can also be offset horizontally in the
vertical direction.
>2IIVHWWLQJ WKH FXUYH KRUL]RQWDOO\ LQ WKH YHUWLFDO
GLUHFWLRQ@
7RXFKWKH2IIVHWEXWWRQ
8VHWKHDGMXVWPHQWEXWWRQVWRPRYHWKHFXUYH
KRUL]RQWDOO\XSDQGGRZQZLWKWKHDGMXVWPHQW
buttons.
*Initial value: +0.0%
ŏ8VLQJWKH(;3FXUYHLVKHOSIXOLQHQJLQH
rise and other engine control.
(VTR curve)
ŏ6HWWLQJLVIDVWLIOHIWULJKWXSDQGGRZQ
DUHÀUVWGHFLGHGLQWKH&RPELQHGPRGH
and the mode is then switched to the
Separate mode.
When this curve is used when the
operating rudder angle is large such as
with acrobatic models, switching from
QRUPDOÁLJKWWRDFUREDWLFUXGGHUDQJOHLV
performed without switch operation.
＜ Data ＞ 171
Line and spline curve adjustment
(Line curve)
Line curves or spline curves of up to 17 points can
be used. (Initial value: 7/9 points) The set points can
be freely increased, decreased, and offset. Curves
which are symmetrical to the left and right of center
can also be set.
>6HWWLQJPRGHV@
*[Separate] mode: Normal setting
*[Combined] mode: Creates a left and right
symmetrical curve.
>$GMXVWLQJWKHUDWHRIHDFKSRLQW@
8VHWKHPRYHEHWZHHQSRLQWVEXWWRQV>@
RU>!!@WRVHOHFWWKHSRLQW 7KHSLQNSRLQWLV
the selected point.)
2. Touch the Rate button.
8VHWKHDGMXVWPHQWEXWWRQVWRDGMXVWWKHUDWH
[Point addition method]
 $IWHU WRXFKLQJ WKH SRLQW EXWWRQ PRYH WKH
stick, etc. to the point you want to add and
SUHVV WKH >0RYH@ EXWWRQ $Q RXWOLQHG SRLQW
appears on the graph.)
2UPRYHWKHVWLFNHWFWRWKHSRVLWLRQ\RXZDQW
WR DGG DQG SUHVV WKH >0RYH@ EXWWRQ $Q
outlined point appears on the graph.)
 8VH WKH PRYH EXWWRQV >   @ RU > ! @ WR ILQH
DGMXVWWKHSRVLWLRQ
3. Touch the Insert button.
 $QHZSRLQWLVFUHDWHG
[Point deletion]
8VHWKHPRYHEHWZHHQSRLQWVEXWWRQ>@RU>
!!@DQGVHOHFWWKHSRLQW 7KHSLQNSRLQWLVWKH
selected point.)
 %HFDXVH >5DWH@ LV SXVKHG DQG >'HOHWH@ LV
GLVSOD\HG WRXFK WKH >'HOHWH@ EXWWRQ 7KH
selected point becomes an outlined point.)
7RXFKWKHPRYHEHWZHHQSRLQWEXWWRQ>@
RU>!!@
*The point is deleted.
The curve can also be offset horizontally in the
vertical direction.
>2IIVHWWLQJ WKH FXUYH KRUL]RQWDOO\ LQ WKH YHUWLFDO
GLUHFWLRQ@
7RXFKWKH2IIVHWEXWWRQ
8VHWKHDGMXVWPHQWEXWWRQVWRPRYHWKHFXUYH
KRUL]RQWDOO\XSDQGGRZQ
*Initial value: +0.0%
172 ＜ Data ＞
(Spline curve)
5DWHDGMXVWPHQWEXWWRQV
0RYH
'HOHWH
6ZLWFKVHOHFWLRQPHWKRG
The various functions used in the T18MZ-WC can be selected by switch. The switch (including when stick, trim
lever, or VR are used as a switch) setting method is common to all functions.
Switch mode selection (Single switch/Logic switch)
When the switch select button in a mixing function screen or other screen is touched, the switch mode selection
screen shown below is called. Single mode or logic mode can be selected.
Logic switch
The Logic switch can activate functions by the use of other switch
combinations. Up to 4 switch combinations can be set. The Logic switch can
EHDVVLJQHGWRWKHPL[LQJIXQFWLRQDVZHOODVWKHÀLJKWFRQGLWLRQVHOHFW H[FHSW
for Snap roll function on airplane mode).
(Switch mode selection screen example)
,QFDVHRIWKHÁLJKWFRQGLWLRQVHOHFWWKH
top of the switch on/off status display is
not shown.
ŏ6ZLWFKVHOHFWLRQEXWWRQ
ŏ0RGHVHOHFWLRQEXWWRQ
If using the single switch:
If using the logic switch:
3XVKWKHVZLWFKVHOHFWLRQEXWWRQ
1.The switch mode display is changed by
pushing the mode selection button. Then
SXVKWKH>&ORVH@
ŏMode: Lin/Sym
ŏType: Hysteresis (Hys.)/box (Box)
:KHQWKH21SRVLWLRQEXWWRQLVWRXFKHGDIWHU
stick, etc. was selected, the screen shown
below appears.
2. Select the mode you want to use, and set it
as described below.
&ORVHWKHVFUHHQE\WRXFKLQJ>&ORVH@
＜ Data ＞ 175
Operation modes
The operation modes when stick, trim lever or VR are selected are described below. Change the operation mode
by touching the Mode and Type buttons.
Linear hysteresis mode
This setting method selects function ON/OFF based
on the set point. Hysteresis (dead band) can be set
between ON and OFF. The ON and OFF positions
can be reversed with the Reverse button.
When shifting the ON/OFF point
The ON/OFF and hysteresis (dead band)
boundary point (there are 2 points: top and
bottom) position can be shifted. ON/OFF is
possible at a free position.
Top point
Bottom point
Symmetrical hysteresis mode
Operation is the same as the linear hysteresis
mode, but left and right (up and down) operations
are symmetrical about the neutral position. For
example, when you want to switch DR1 with the
aileron stick, when the stick is moved to the left or
right, DR1 can be turned ON at the same left and
right position.
Linear box mode
This mode turns on the switch within a range of
2 points. Each point can be set. The ON and OFF
positions can be reversed with the Reverse switch.
Symmetrical box mode
Operation is the same as the linear box mode,
but left and right (up and down) operation is
symmetrical about the neutral position.
176 ＜ Data ＞
>6HWWLQJPHWKRG@
1. Select the top and bottom boundary points
ZLWKWKH>3RLQW@EXWWRQ
2. Move the stick, etc. to the point you want
WR VKLIW DQG WRXFK WKH >(QWHU@ EXWWRQ 7KH
boundary points change.
 $OVRVKLIWRWKHUSRLQWVDVUHTXLUHG
83'$7,1*
Your Futaba T18MZ-WC transmitter programming can be updated easily and at no cost online. When functions
DUHDGGHGRULPSURYHGWKHXSGDWHÂżOHFDQEHGRZQORDGHGIURPRXUZHEVLWH&RS\WKHXSGDWHÂżOHVWRWKH6'FDUG
and then use the following procedure to update the program.
Check our web site for the FAQ regarding updating for more information.
Updating procedure
Note: If the battery fully discharges during
program updating, updating will fail. When
the remaining battery capacity is 50% or
less, always recharge the battery before
updating.
Note: The model data in the transmitter can
be used unchanged after updating, but to
be safe, back up the model data before
updating.
,QVHUWWKH6'FDUGFRQWDLQLQJWKHXSGDWHÀOH
into the card slot.
 8VH WZHH]HUV WR VZLWFK WKH VOLGH VZLWFK
(update switch) at the side of the card slot in
the up direction.
 7XUQ RQ WKH WUDQVPLWWHU SRZHU $Q XSGDWH
screen is displayed. Rotary key or the
arbitrary direct keys are pressed.
4. When updating is complete, the screen
shown below appears.
7XUQRIIWKHSRZHUVZLWFK$IWHUWKHPRQLWRU
LED goes off, switch the update switch in the
down direction.
If a problem occurs,an error message
will appear and the update will not be
complete.
 $ I W H U  W K H  X S G D W L Q J  D E R Y H  K D V  E H H Q
completed, turn on the power and then
check the system program version at the
system menu information screen.
＜ Data ＞ 177
70=‫ ڀ‬70=:&02'(/'$7$&219(56,21
The model data (only latest version) of T14MZ can be copied to T18MZ-WC.
* The card reader of a personal computer, SD card, and CF card is required.
* The model data of T18MZ-WC cannot be copied to T14MZ.
&)FDUGLVFRQQHFWHGWRD
personal computer with a card
reader.
0RGHOGDWDLVFRSLHGWR&)FDUG
CFDP32M
Card Reader
Data-Pack
T14MZ
䣏䣑䣆䣇䣎
SD
card
T18MZ
The model data of SD card is used
E\70=:&
>0RGHOGDWDFRQYHUVLRQPHWKRG@
7KHGDWDZKLFK70=ZDQWVWRFRS\LVSXW
LQWR&)FDUG
2. The card reader of option marketing is
connected to the personal computer of
DVWRFNDQG&)FDUGLVLQVHUWHGLQDFDUG
reader.
3. SD card is connected to the personal
computer.
4. With the personal computer, the model data
RI&)FDUGLVFRSLHGWR6'FDUG
7KH6'FDUGLVLQVHUWHGLQ70=:&DQGLW
FRSLHVWR70=:&IURP6'FDUGE\WKH
>/LQNDJHPHQX@DQG>0RGHOVHOHFW@
Model data is copied to SD card
as it is with a personal computer.
:KHQ6'FDUGFDQQRWEHUHFRJQL]HGLWPD\EHDEOH
to be used if it reformats by SD formatter offered from
6'$VVRFLDWLRQ
6'IRUPDWWHULVGRZQORDGDEOHIURP6'$VVRFLDWLRQ
(https://www.sdcard.org/).
$VRI'HFHPEHU
CAUTION
After the completion of a data copy should fully
perform a check of operation on the model to be
used.
Check well all the directions of operation and all
the operation switches.
FUTABA CORPORATION
1080 Yabutsuka, Chosei-mura, Chosei-gun, Chiba-ken, 299-4395, Japan
Phone: +81 475 32 6982, Facsimile: +81 475 32 6983
2015, 12 (1)
178 ＜ Data ＞

---

Source Exif Data:

File Type                       : PDF
File Type Extension             : pdf
MIME Type                       : application/pdf
PDF Version                     : 1.6
Linearized                      : Yes
XMP Toolkit                     : 3.1-702
Modify Date                     : 2016:01:27 16:12:37+08:00
Create Date                     : 2016:01:27 16:12:32+08:00
Metadata Date                   : 2016:01:27 16:12:37+08:00
Format                          : application/pdf
Title                           : ????1.pdf
Creator                         : Konno
Document ID                     : uuid:f9408c26-27cd-4811-8d9f-ba1cd0b899e5
Instance ID                     : uuid:8f434a2c-f071-44be-8f6a-cdd394abe63f
Producer                        : Acrobat Distiller 7.0.5 (Windows)
Page Count                      : 85
Author                          : Konno

EXIF Metadata provided by EXIF.tools