The repair must be examined at specified intervals and replaced if deterioration or damage is found.

Make sure that there is clearance between the lever and the roller.

If it is possible that the temperature values will be more than the permitted limits, decrease the power.

Procedures shall be provided for all airplanes for all cases of engine failure during takeoff and in flight.

The primary function of the hydraulic pressure system is to supply pressure for the operation of the flight controls.

To bleed the braking system, operate the hand pump handle through its full travel.

Adjust the indicator to zero once there is contact with the elevator tab leading edge.

When you lift or lower the aircraft, always keep it in a level attitude.

Most secondary structures are important to the performance of the airplane.

Remove the protective layer from one side of the new gasket with ANTENNA SIDE markings.

Obey local regulations for the correct procedures to use or discard solvents.