The cambered side of a blade is called ____.

The flat side of the blade is called ____.

The ____ is that part of the propeller blade farthest from the hub, generally defined as the last 6 inches of the blade.

this has been used since the Wright Flyer's first flight in 1903 and are still popular on many amateur-built aero planes.

its light weight, rigidity, economy of production, simplicity of construction, and ease of replacement, is well suited for such small aircraft.

are forged from high-strength aluminum alloy, and after being ground to their finished dimensions and pitch, are anodized to protect them from corrosion.

these are types of propellers except:

are the most widely used types of propeller in aviation.

these are found primarily on transport aircraft.

what type of propeller are forged and machined to the desired contours and the proper twist is achieved by twisting the blades.

used in propeller manufacturing consist of two constituents: the fibers and the matrix.

The strength and stiffness of the blades are determined by the

has the blade pitch, or blade angle, built into the propeller.

this type of propeller is one piece and is constructed of laminated wood or aluminum alloy.

what kind of propeller is inefficient at take-off and landing speeds.

what operates as a fixed-pitch propeller?

this propeller permits a change of blade pitch or angle, while propeller is rotating.

types of controllable pitch propeller

The first popular controllable-pitch propellers were hydraulically actuated by engine lubricating oil supplied through a hollow crankshaft.

what kind of propeller is a system in which the propeller blade angle is varied by the action of a governor to maintain a constant speed.

The pitch changing devices for constant speed propellers include _____, _____, and devices in which centrifugal forces act on flyweights and combinations of these methods

THE BLADE PITCH OR BLADE ANGLE , BUILT INTO THE PROPELLER

THE PITCH OR BLADE ANGLE CAN BE CHANGED ONLY WHEN THE PROPELLER IS NOT TURNING

PROPELLER PERMITS A CHANGE OF BLADE PITCH , OR ANGLE WHILE THE PROPELLER IS ROTATING

Before installing a propeller, the propeller shaft and threads should not be checked for damage.

Boss and hub flange faces should be checked for cleanliness, to ensure that maximum friction will be obtained.

When assembling the hub to the shaft, it is usually recommended that an anti-seize compound should be applied to the threads, and engine oil to the shaft. Where cones are fitted, these should be clean and dry.

The angular position of the propeller on the hub is not important, unless the engine is likely to be started by hand swinging

The attachment bolts should be tightened evenly, and in any sequence, to the specified torque.

when the propeller is rotated the blades should track within 1/4 inch of each other, but a wider tolerance may be permitted on repaired propellers, provided that no vibration is evident during engine runs.

After engine runs to check the reference RPM, the propeller attachment bolts and the hub retaining nut should be checked for tightness, and re-locked.

It is recommended that the bolts should also be checked after each of the first few flights.

The dowels, spacer and flange should be inspected before assembly to ensure that they are undamaged, and the propeller and spacer should be assembled together before installation on the engine.

The propeller attachment bolts should be checked for tightness after the engine run.

The engine should not be ground run after installing the propeller, to check for vibration and determine the engine speed obtained at full throttle.

If the engine is likely to be hand-swung, the propeller should be fitted to the engine in a convenient position. The attachment bolts should be tightened evenly, and in proper sequence, to the specified torque.