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5

2. Put the stopper (P/N.2670-96220) into a sparkplug hole (Fig.1) of the cylinder(

) which

is located closer to the rotor than other cylinder when viewed from intake manifold side
(Fig.2).

3. Turn the rotor counterclockwise until piston touches the stopper.
4. Unscrew the rotor nut.
5. Remove the rotor by using the puller (P/N. 1490-96101).

Do not hit the crankshaft end by metal hammer, that may cause the crankshaft to be
bent out of alignment.

c. Assembling crankcase 

1. Apply grease on the oil seal lips and oil on the bearing. 
2. Assemble the crankshaft with a new gasket. 
3. When both front and rear crankcases are tightened, the portion of gasket protruding on

the cylinder mount surface should be cut off with a knife until the gasket becomes flush
with the cylinder mounted surface. 

d. Assembling piston 

Before assembling the piston, apply the oil on the small end bearing and piston, and set
the piston ensuring that the arrow mark on the top of piston is directed toward the
direction of exhaust port. 

e. Re-assembling cylinder and intake manifold

1. Coat the oil on the inner surface of cylinder. 
2. The piston is provided with a knock pin which stops the piston ring from turning. Set the

split section of piston ring at the knock pin and assemble the cylinder ensuring not to
break the piston ring. 

3. Keep cylinder bolts unfastened before installing the intake manifold to the cylinder.
4. Fixing the intake manifold to the intake port of each cylinder.
5. Then, tighten cylinder bolts.

f. Assembling rotor

Make sure to put lock tight (Medium strength type: TreeBond 1322N, LOCTITE 242,243,
PACER ZAP Z-42) on the rotor fixing nut (P/N:1100-43231).

g. Recommended tightening torque for bolts/nuts

Be sure to follow the recommended tightening torque for bolts/nuts in assembling at each
part.
1. Rotor nut (M10)

: 250 ~ 300 kg-cm

2. Crankcase bolt (M5)

:

50 ~   90 kg-cm

3. Cylinder bolt (M5)

:

50 ~   90 kg-cm

4. Engine mount bolt (M6)

:

80 ~ 120 kg-cm

5. Propeller hub bolt (M6)

:

80 ~ 120 kg-cm

6. Source coil bolt (M4)

:

15 ~   20 kg-cm

h. Adjusting air gap of coil. 

The air gap of coil should be adjusted to 0.3 mm (0.01"). 

i. Adjusting ignition time. 

This engine with the point-less C.D.I. type requires no adjustments of ignition time.

Fig. 1

Fig. 2

(

)

Stopper

Summary of Contents for G800BPU

Page 1: ...of the engine This engine is designed to be used to Radio controlled products In case any modification by customer ZENOAH shall not bear any responsibility from the damage caused by such modification...

Page 2: ...the reverse side of the mount to prevent bolts from sinking into the mount Before flying the aircraft be sure to check for loose bolts 2 Since this engine is equipped with a float less carburetor wit...

Page 3: ...3 and the engine will start NOTE Be sure to keep holding propeller firmly by other hand while winding up the spring for starter Be sure to open the choke when the engine first fires When the choke is...

Page 4: ...gradually This engine is used for power source for radio controlled airplane so you are strictly requested to check engine and relative parts of airplane 1 Daily check before starting Leakage damage c...

Page 5: ...e Re assembling cylinder and intake manifold 1 Coat the oil on the inner surface of cylinder 2 The piston is provided with a knock pin which stops the piston ring from turning Set the split section o...

Page 6: ...0 in x 1 22 in x 2 Compression ratio 8 1 1 Maximum output 5 52kW 10000rpm 4 41kW 10000rpm with Muffler Operating engine speed 1800 10000rpm Weight 3 5kg 7 9Ibs with mufflers spring starter Ignition sy...

Page 7: ...202 Bearing 1 49 1400 21220 Oil seal 1 Q ty unit Description Parts No Index No 50 2670 21250 Elbow 1 51 1065 81100 Pipe 1 52 2898 21310 Gasket crankcase 1 53 01252 30520 Bolt 4 54 T2002 41110 Piston 2...

Page 8: ...hall not compensate any other accompanied or benefit losses caused to user and distributor manufacture by such faults and through repairing or replacing 4 Term of Warranty Three 3 months after purchas...

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