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beardpapa
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The aircraft incorporates a _______ flight control system.
Reversible
- aerodynamic forces are fed back to the pilot from each conrol surface througha system of push rods, cables and pulleys.
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As airspeed increases, trim appears to become (less/more) effective, more noticeable in the ____ and _____ axes.
more, roll and yaw
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NOTE:
During acceleration from low to high speed, the pilot will need to initially trim ________ to avoid a rapid buildup in forces.
nose-down
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At approach speeds or below with flaps in LDG position, full _______ trim is required at 100% torque.
nose-right
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The four inputs to the TAD are:
engine torque, indicated airspeed, pressure altitude, and pitch rate.
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Extension of the speed brake causes a slight _______ tendency.
nose-up
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Recommended Entry Speed:
Aileron Roll
Chandelle
Inverted Flight
Barrel Roll*
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Recommended Entry Speed:
Wingover/Lazy Eight
Clover Leaf
Loop
Cuban Eight
- 160-250
- 210-250
- 200-250
- 210-250
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Recommended Entry Speed:
Immelmann
Slit S
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Asymmetric Manuevers
As much as possible, maintain _________ roll and yaw control inputs during asymmetric manuevers.
coordinated
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Asymmetric Manuevers
If rolling pullouts at greater than ____ G are uncooridinated, limit roll input to _______ stick.
+2 G, one-half lateral
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Asymmetric Manuevers
If uncoordinated rolling maneuvers are initiated at -1 G, the max bank angle change is _____ degrees.
180
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(four) Factors that affect glide performance:
airspeed, configuration (gear and flaps), angle of bank, coordinated/uncoordinated flight.
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Best Glide Speed is approximately ______ KIAS with a sink rate of _______ feet per minute and a glide ratio of _______ feet.
125 KIAS, 1350 feet per minute, 2.0NM/1000ft
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With the landing gear down and flaps and speed brake retracted, best glide speed is approximately ______ KIAS with a sink rate of approx _____ feet per minute and a glide ratio of ________.
105 KIAS, 1500 feet per min, 1.6NM/1000ft
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A stick shaker, activated by the ________ system, provides artificial stall warning in each cockpit a minimum of ___ knots before the stall is reached.
- angle of attack system
- 5 kts (5-10kts depending on manuever)
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Natural stall warning (aerodynamic buffet) occurs approx __ kts before the stall.
3 kts
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A ______ or _____ together with increased ______ is the defining charactersitic of an upright, wings-level stall.
roll-off, wing-drop, buffet
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With power off, lateral roll-off during a wings-level stall is typically to the ______ and occurs near ______ stick.
right, full aft stick
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Above _____ torque, full right rudder and full right aileron may not prevent a _____ roll-off at stall.
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Three categories of OCF
- poststall gyrations
- incipient spins
- steady-state spins
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Poststall Gyration symptoms
- uncommonded aircraft motions
- a feeling that the cotrols are no longer effective
- stalled or near stalled AOA
- transient or erratic airspeed indications
- random turn needle deflections
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Incipient Spin Syptoms
- oscillations in pitch, roll and yaw attitudes and rates
- fully deflected turn needle
- stalled AOA
- airspeed that is accelerating or decelerating toward the steady-state spin value
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NOTE: During a spin, oil pressure may decrease below ____ psi with idle power. This acceptable provided no operating limits are exceeded and normal indications return after recovery.
40 psi
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Erect Steady State Spin
- nose 60° below horizon
- 400-500 ft per 2-3 seconds
- AOA: 18+
- Airspeed 120-135 KIAS
- Turn Needle: Fully Deflected
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A _______ spin is a result of misapplication of recovery controls where opposite rudder is applied while mainting full back stick.
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Entry into an __________ spins is caused by maintaining pro-spin rudder while moving the stick forward.
aggrevated spins
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Aggrevated spins greater than four turns may cause _______.
Oil starvation problems.
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