Hartzell HC-E3YR-7 Owner's Manual page 42

Term
Impact Damage . . . . . . Damage that occurs when the
Low Pitch . . . . . . . . . . . The lowest blade angle attainable
Major Propeller Effect . The major propeller effects are
Nick . . . . . . . . . . . . . . . Removal of paint and possibly a
Onspeed . . . . . . . . . . . . Condition in which the RPM
Overhaul . . . . . . . . . . . . The periodic disassembly,
Overspeed . . . . . . . . . . Condition in which the RPM of
Overspeed Damage . . . Damage that occurs when the
Pitch . . . . . . . . . . . . . . . Same as "Blade Angle".
INTRODUCTION
Propeller Owner's Manual
136
propeller blade or hub assembly
strikes, or is struck by, an object
while in flight or on the ground.
by the governor for constant speed
operation.
defined in Title 14 CFR section
35.15(g)(2).
small amount of material.
selected by the pilot through the
propeller control lever and the actual
engine (propeller) RPM are equal.
inspection, repair, refinish, and
reassembly of a propeller assembly
to maintain airworthiness.
the propeller or engine exceeds
predetermined maximum limits;
the condition in which the engine
(propeller) RPM is higher than the
RPM selected by the pilot through
the propeller control lever.
propeller hub assembly rotates at a
speed greater than the maximum
limit for which it is designed.
61-00-36
Definition
Page 1-14
Rev. 2 Feb/17