AN 01-25CN-2	PARAGRAPH 1
	SECTION IV
	MAJOR COMPONENT PARTS AND INSTALLATION

3. Insert the jack point studs in the panel and jack the front and rear of the airplane until the landing gear wheels are off the ground.    4. Remove the bleeder screw at the brake Cylinder on the inner wheel fairing and drain the brake system. Disconnect the hydraulic brake hose at the fitting below the bleeder screw on the torque plate. Remove the two hose clamp fittings from their supports, one at the lower end of the oleo cylinder and the other at the lower trunnion.    5. Unbutton the four Dzus fasteners on the wheel's outer fairing and remove the fairing.    6. Remove the axle cap and the cotter pin and turn the large nut off the axle, freeing the wheels. Pull the wheel and wheel bearings from the axle.		7. Free the upper forward circumference of the canvas in the wheel pocket and turn the canvas out, ex0osing the structural detail in the wheel pocket.    8. Partially retract the landing gear so that the upper retracting links and retracting strut piston end through bolt are accessible through the wheel pocket. (See Fig. 48.)    9. Disconnect the landing gear position indicator linkage at the lower end.    10. Remove the cotter pin, nut, and through bolt connecting the retracting strut piston end to the tipper landing gear retracting links. (See Figs. 49 and 50.)    11. Return the piston completely into the retracting strut by placing the landing gear handle on the control valve in the "DOWN" position and actuating the electric hydraulic pump switch on the control, stick.

---