Instructions

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Alsoobservethatthehingeformedattherudder(5)mustbettedintoapreparedslotandthattherudderdoesnot
cantbutrunsinparalleltotheruddern.
Alsocheckifinstallationaccordingtogure3ispossiblewithoutproblems.Ideally,thewingshouldbeinstalledforthis
andthetailunitalignedaccordingtotheillustrationingure3.
Ifeverythingisperfect,thetailunitmustbegluedtothefuselagewith5-minuteepoxy-resinglue.
Apply a little glue to the left and right of the fuselage slot. Remove the protective foil from the fuselage and push the
two parts together.
Fastenthetwopartswithadhesivetapeuntilthegluecuressothattheangletothewingiscompliedwith.Adhesive
residue must be removed at once.
b) Mounting the Elevator and Rudder Linkage Rods
Put the rudder horns of the servos at precisely 90° to the
servo casing.
Shorten the rods for elevator and rudder at the dampening
areas by twisting the clevises in or out so that the dampen-
ing surfaces are in neutral position and attach the clevises
to the rudder horns (1 and 2).
Forelevatorsandrudders,theclevisesshouldbeattached
totheouterholeoftherudderhornfortherstights.
Thecorrectfunctionisexplainedinchapter„Checkingthe
ControlFunctions“.
c) Checking the Linkage Rods at the Ailerons
Thelinkagesofthe ailerons are pre-installed exworks.
Check with the remote control activated whether the servo
rudder horn (1) is at a 90° angle to the servo housing. Also
check if the rudder horns of the linkage rods are in the
outer-most position of the rudder horns (2).
In the neutral position of aileron trimming and control le-
ver, the ailerons need to be in the neutral position as well
andendushwiththerearwingedge.Ifthisisnotthe
case,theirlengthmustbeadjustedbytwistingtheclev-
ises in or out.
The connection of the aileron servos is shown in the fol-
lowingchapter„MountingtheWing“.Thecorrectfunction
isexplainedinthechapter„CheckingtheControlFunc-
tions“.
Figure 4
Figure 5