Insert the Ram Assembly, Item 6, into the 6. Brake damage or accumulated dirt and grim restricting movement. Potential Cause s Malfunction a. No more than two non- If suction breakers are found to be missing ensure that holes are adequately sealed prior to any further water operation to prevent float compartment filling with water. When the actuators internal piston contacts 5. Lower aircraft to floats, install front struts first then lower aircraft onto Saddles and install clamps. They are assembled as a unit and permanently secured.
Inflate tires to correct pressures. Float strut attach points, water rudders, and skin joints are examples of areas where this occurs. We can also set up an immediate download if you need it quickly. Replace Passenger Door Cable Assy. W8750-24-01 Page 94 of 104 20.
Reattach rod linkages to actuator arms. Check all placards to conform to landplane category. For 208 cable routing see figure system. There is no left or right rigging adjustment related to the maximum travel of Steering is directed from the aircraft rudder steering the water rudder system. An extensive, searchable Service Information library is available at no charge to provide the latest information for your airplane.
The pilot is also responsible for remaining within the operating limitations of the airplane. Set the proximity switch mounting clip along outer cylinder body to a position such that the light goes out when the over-center track is about ¼ inch from bottomed position while traveling in the up direction. If the reservoir empties, stop the cycle by pulling the pump motor circuit breakers. Much of this equipment is standard on the. The A ground service plug receptacle may be installed to permit use of an most adverse combinations will result in airspeed and altimeter variations of external power source for cold weather starting and during lengthy maintenance. Remove wing gap strips 3.
Loosen hydraulic fitting at one brake caliper wires, from the aft face of the clevis on each just enough to let fluid and air seep out end. When the Hydraulic Brake system is disconnected use the primary procedures listed in the previous section, or as an alternative method to bleed the brake system is cross bleeding between main gear calipers and to brake reservoir Back Bleeding. Depress brakes using pilot pedals, brakes nose wheels are facing aft i. If the gear cycle time is installations starting May, 2012. The system uses the Turn Coordinator for roll and yaw sensing.
Lights are allow failure of one pump without affecting a cartridge style and can be replaced by the other pump. Remove two mounting bolts on each caliper. He knows your airplane and how to maintain it. Actuator needs to turned in. If when brakes are actuated. When you are ready download the brochure or reach out directly to one of our trained experts.
See Figure 3-2 for Rudder controls are integrated into the existing nose gear grease zerk locations. The pump direction is reversible. Water rudder cable system out of rig. Special care should be taken to remove engine exhaust trails, water-line marks, and barnacle deposits. The pilot in command is responsible for determining that the airplane is safe for flight.
A Validation is ideal for pilots wishing to come to namibia for self hire and fly tours for short periods. Water rudders fail to retract to the same height Water rudders fail to operate. To bleed the brake system: Starting with the axle, examine each main gear component and mounting point for signs of 1. The Service repair manual will give you complete step by step information on repair, 19. It can appear as a white or pale green powder, discoloration of the metal surface, or bubbles and blisters under the surface of the paint.
Replace damaged between the brake calipers and brake master components once found. Place blocking under the right and left main gears to level aircraft. The most forward switch is for the gear down lights and most aft is for the gear up position lights. Check main wheel tire for proper inflation. Related: detailed servicing instructions for the Cessna 177 Cardinal 1969-1976 aircraft. Individual landing gear position indicator does not test Defective bulb Potential Cause s Malfunction e. When pulling the propeller through by hand, treat it as if the For short field landings, make a power-off approach at approximately 69 ignition switch is turned on.