Color code for instrument markings, GREEN:

If a difference is observed between the engine and rotor tachometers during flight:

The tail rotor blades are constructed with:

Power failure general:

The pilot notices during flight that the auxiliary tank is approaching “Empty”, while there is still lots of fuel in the main tank. Given that the pilot remembers from ground school that the two tanks are interconnected, she is very worried.

The low RPM light and horn indicate rotor RPM:

BRAKE light ON in flight:

If power failure occurs at night:

What is the minimum solo pilot weight plus forward baggage weight with all doors installed in a R-22?

The following action should first be taken when an electrical fire in flight occurs:

Each tach, the governor, and the low RPM warning horn are:

The LOW FUEL light comes on when there is approximately:

Hover performance data presented in section 5 of the POH was obtained:

The OIL PRESSURE gage Lower red line corresponds to:

When operating at high density altitudes, governor response rate:

A caution CLUTCH LIGHT on the panel is ON whenever the electric actuator is:

Yellow arc on Manifold Pressure gage:

Satisfactory engine cooling has been demonstrated to an outside temperature of:

The battery voltage is:

The Demonstrated Operating Temperature at an altitude of 4000’ is:

If the master battery and alternator switch are both off:

Upon inadvertently encountering moderate, severe, or extreme turbulence adjust forward speed:

The sensor for the rotor tachometer senses the signal provided:

When the collective control is raised the engine throttle:

A pilot with 150 helicopter hours, 10 000 aeroplane hours and 50 hours on the R-22 wants to fly. The wind is 5 gusting 25 knots. May he fly?

When the fuel gages read E the tanks:

A discharged battery is Airworthy:

The high hover point:

If there is a CHIP warning light, but no abnormal noises:

The blade skins (main rotor) are made of: