R22 - Structure, transmissions, rotor and equipment, normal and abnormal operation of systems
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Magnetos drop at 75% RPM:
An anti-collision strobe light is installed:
A sliding valve controlled by the pilot (carb heat) allows:
Correct throttle linkage (throttle-collective-butterfly valve) adjustment may be verified during preflight:
Where is the first stainless steel firewall located in relation to the engine compartment?
The main gearbox overtemp light is actuated by a temperature switch located:
Prior to a ground contact (run-on) autorotation landing, a detent spring, located in the vertical throttle push-pull tube:
What is the engine layout?