Manufacturer: PPHU
EKOLOT
Type: KR-030 TOPAZ
Handling, Maintenance and Periodic Inspections
Manual
Issue: 1
Rev. N
o
:
Date: July 2010
Date:
Page
23
4. The lever must be fixed in a position allowing to screw in the locking
bolt (Pic. 9.1.7, page 18 – Bolt M5x10, 8,8 DIN 912). The bolt must be
secured with LOCTITE 262.
5. Tighten the clamp bolt (Pic. 9.1.7, page17)
When installing front undercarriage with a new pole:
1. Match new slide bearing in the guiding bushing to the new pole.
2. Install and adjust the rudder control system (point 9.3.1)
3. Carry out activities no. 1, 2, 3 of the front undercarriage installation (Pic.
9.1.11, page 21).
4. Check if the pole turns without frictional resistance (should be turned
easily with one hand) in the slide bearing within the angle range ±30
º
.
5. Set and lock the rudder in the neutral position.
6. Set the front wheel in parallel to the axis of the airplane.
7. Maintaining this position tighten the clamp bolt on the control lever
J.13.122.00.01 (Pic. 9.1.7, page 17) in order to fix its position in relation
to the pole.
8. Drill a hole
Ø
4 through the hole
Ø
5 in the pole’s wall and cut M5 thread.
9. Screw in the locking bolt (Pic. 9.1.7, page 18 – Bolt M5x10, 8,8 DIN
912). Secure the bolt with LOCTITE 262.
9.1.12 Replacement of tyre
1. Perform the procedure 9.1.8
2. Take the assembly shown in 9.1.5, perform the procedure 9.1.9, but do
not dismantle the assembly shown in the point 9.1.2.
3. Rub the inner surface with talcum or other substance used for
preservation of rubber.
4. Put a new inner tube inside the tyre.
5. Put the tyre with the tube on the rim 42206-0 (Pic. 9.1.4, page 16). Put
the wheel valve into the hole located in the rim.
6. Put the rim and tyre on the hub J.13.130.01.02 in assembly 9.1.2 (see
point 5), and the rim 42206-1 and the clamp ring J.13.130.02.01.
7. Screw the bolts as shown in the point 9.1.4.
8. Pump the wheel to the required pressure.
9. Install the wheel on the front fork (reverse order of procedure described
in point 9.1.8).