CO104

An OCF condition can be caused by stalling the aircraft ______.

in uncoordinated flight

Which is the first, or initial, stage of out-of-control flight?

Poststall gyrations

During a practice OCF entry, you must set the PCL to IDLE ______.

prior to applying rudder

How do know that neutral controls are becoming effective in eliminating an OCF condition?

Yaw rate decreases and the nose pitches down

What are the two categories of steady-state spins for the T-6A?

Erect spins and inverted spins

Rate-of-turn pointer deflection ____ be used to determine the difference between a spiral and a spin.

can NOT

What is a proper indication of an inverted spin?

AOA indicating zero units

The purpose of the stability demonstration is to _____

show that a spin may not be entered if the aircraft is not allowed to stall.

What will happen if OCF recovery procedures are not performed during the initial two stages of an OCF condition?

The aircraft will eventually transition to a steady-state spin.

What is an indication of an incipient spin?

Rate-of-turn pointer fully deflected in the direction of rotation

What is the approximate practice spin entry airspeed?

80 KIAS

You are performing a practice OCF recovery. When do you begin the recovery?

When directed by the IP

What is the first step of the INADVERTENT DEPARTURE FROM CONTROLLED FLIGHT checklist?

PCL - IDLE

When do you begin the unusual attitude recovery after performing the OCF recovery procedure?

When aircraft gyrations stop and the aircraft is under control

Which of the following is an indication of an erect spin?

Airspeed stabilized at 120 - 135 KIAS

To recover from an inverted spin check the following: gear, flaps and speed brake - Retracted, PCL - IDLE, apply full rudder opposite the rate-of-turn pointer, and ______.

stick aft of neutral (up to full aft stick may be used)

The best control inputs to recover from a spiral are PCL to IDLE and _______.

neutral stick and neutral rudder

Enter a stability demonstration maneuver by accelerating to 160 KIAS, adjusting power to 60% torque, and raising the nose to a ______ pitch attitude.

45�