
3. In order to make sure the en
ine does not speed excessivel
without a positive control installed, throttle return sprin
s
must be left in place.
4.
fter
ou have connected the return sprin
to the throttle
servo
ou ma
unhook it(do not remove it), since it acts as
a spacer for the butterfl
. The butterfl
will work loose b
removin
the return sprin
.
5. The i
nition batter
should be mounted externall
,nea
the
cowl, at least twelve inches from the receiver o
throttle servo
that connects to the receiver.
6. The carburetor needs at least 1 1/2"
38mm
of clearance
between the intake and the bottom of the cowl. If there is less
than 1 1/2", make an openin
in the cowl below the
carbureto
at least as lar
e as the carbureto
intake diameter.
7.
lon
, narrow, screw drive
is recommended to drill small
holes in the cowl fo
ad
ustin
the needle valves, since the
carburetor must often be ad
usted differentl
with the cowl on
as compared to off.
8. The en
ines are equipped with a diaphra
m pump carburetor
makin
tank location not critical relative to the carburetors
fuel entr
position. Place the tank on the aircraft’s center of
ravit
CG
. Then aircraft trim chan
es durin
fli
ht will not
be necessar
fromafulltoanempt
tank
L:
Clean petrol 93# is stron
l
recommend fo
ou
DL
en
ines.
Lubrication Ratio of trial Run is 25:1~30:1, while normal fl
in
is
40:1~50:1, Hi
her-octane fuel will not
enerate more powe
and ma
cause the en
ine to run slowe
and overheat.
Note: Dama
e caused b
fuel additives, such as nitro,
over-lean carbureto
settin
s, over-advanced timin
and
over-heatin
are not covered under warrant
.
n
t
on s
stem
DLA I
nition details:
• The red cable is positive
+
, while the black is ne
ative
-
.
• Workin
volta
e: 6.6V~8.4V
7.4V ,2S Li-Po batter
is
recommended
• Please connect Li-Po batter
to DL
i
nition directl
.
• It is important to achieve the correct coordination of the
sensor
s
to the ma
nets for fittin
anewi
nition.