finished
Quiz yourself by thinking what should be in
each of the black spaces below before clicking
on it to display the answer.
Help!
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| show | True
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| As airspeed increases, trim appears to become ___________________.(-1 pg 6-2) | show 🗑
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| Pulsing the trim control is ___________ to avoid over-trimming at higher airspeeds. (-1 pg 6-2) | show 🗑
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| During rapid acceleration from low to high speed, the pilot_______need to initially trim nose down a rapid build up in forces | show 🗑
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| show | False (adequate)
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| show | 100
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| The directional trim is commanded by the trim aid computer as a function of? (-1 pg 6-2) | show 🗑
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| (T/F) The trim aid computer will completely trim the aircraft directionally? (-1 pg 6-2) | show 🗑
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| show | Very little
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| show | True
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| show | False (Buffeting intensifies)
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| show | False – The speed brake-elevator interconnect reduces the pitch tendency.
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| (T/F) The flap/speed brake interconnect prevents the use of the speed brake with the flaps extended. (-1 pg 6-3) | show 🗑
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| (T/F) If the flaps are extended, the speed brake will not retract if extended. (-1 pg 6-3) | show 🗑
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| If the speed brake has been extended, it will automatically retract if the flaps are set to any position other than ________.(-1 pg 6-3) | show 🗑
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| The reversible flight control system becomes more sensitive as airspeed _______.(-1 pg 6-3) | show 🗑
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| show | Can
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| Frequent cross-checks of airspeed are ____________ during climb out to prevent deviations from the climb airspeed schedule. (-1 pg 6-3) | show 🗑
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| (T/F) The aircraft will decelerate rapidly with power in a dive. (-1 pg 6-3) | show 🗑
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| If uncoordinated rolling maneuvers are initiated at –1 G, the maximum bank angle change is ________ degrees. (-1 pg 6-3) | show 🗑
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| Recommended entry speed for a lazy eight is___KIAS(-1 pg 6-3) | show 🗑
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| show | 230-250
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| show | 120-140
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| show | 230-250
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| show | 200-220
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| Recommended entry speed for a Barrel Roll is ________ KIAS. (-1 pg 6-3) | show 🗑
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| Recommended entry speed for a Cuban Eight is ________ KIAS. (-1 pg 6-3) | show 🗑
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| Recommended entry speed for an Aileron Roll is ________ KIAS. (-1 pg 6-3) | show 🗑
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| Recommended entry speed for a Chandelle is ________ KIAS. (-1 pg 6-3) | show 🗑
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| Factor(s) which effect glide performance are________. (-1 pg 6-4) | show 🗑
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| show | False – Clean = 125, Gear = 105, Gear/Flaps = 95
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| Best glide speed in clean configuration is approximately _____ KIAS with a sink rate of __________ fpm. (-1 pg 6-4) | show 🗑
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| show | 105, 1500
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| show | Cannot
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| show | True
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| The stick shaker provides artificial stall warning in each cockpit a minimum of _____ knots before the stall is reached. (-1 pg 6-4) | show 🗑
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| show | 3
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| show | True
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| show | True
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| show | Increased buffet Roll off Wing-drop Roll-off and wing-drop
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| During a wings level power-on stall, _________ rolling tendency is induced at stall by engine torque before reaching full aft stick. (-1 pg 6-4) | show 🗑
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| show | 60
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| show | Pronounced
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| Altitude lost during recovery from a wings level stall is usually less than ______ feet, assuming a prompt application of recovery power. (-1 pg 6-7) | show 🗑
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| In general, OCF can be divided into which following categories: (-1 pg 6-7) | show 🗑
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| show | Stall and prior to the incipient spin
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| (T/F) A poststall gyration can occur at high airspeed but not at low airspeed. (-1 pg 6-7) | show 🗑
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| show | True
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| show | Incipient spin
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| An incipient spin is characterized by oscillations in ________. (-1 pg 6-8) | show 🗑
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| An incipient spin can be identified by an oscillatory spin like motion, ________________ , ______________, and airspeed that is accelerating or decelerating toward the steady-state value. (-1 pg 6-8) | show 🗑
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| show | 4500
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| (T/F) The aircraft has shown an overall capitulation to un-intentional spins. (-1 pg 6-8) | show 🗑
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| (T/F) Recovery from inadvertent loss of aircraft control, including poststall gyrations and incipient spins, can be accomplished by promptly advancing power to MAX, and positively neutralizing flight controls in all axes. (-1 pg 6-8) | show 🗑
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| show | 160
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| A spiral can result from misapplication of ________________. (-1 pg 6-8) | show 🗑
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| (T/F) Anti-spin controls may not be effective in arresting the spiral and may actually aggravate the situation. (-1 pg 6-8) | show 🗑
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| The best response to a spiral is to neutralize the ___________ and reduce ____________ until motion stops. (-1 pg 6-8) | show 🗑
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| show | Stalled angle-of-attack, sustained yaw rate
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| show | False
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| show | 15-20
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| Spins below 10,000 feet MSL are prohibited due to ______________________ which occur during the spin maneuver with the propeller RPM below 80%.(-1 pg 6-9) | show 🗑
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| show | 80
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| Entry into idle power, erect spins are characterized by roll and yaw in the ___________________ is applied. (-1 pg 6-9) | show 🗑
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| (T/F) After completing the initial turn, of an erect spin, the nose will pitch to approximately 60 below the horizon. (-1 pg 6-9) | show 🗑
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| show | 3
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| Spin rotation rates will stabilize to approximately ____________ seconds per turn with altitude loss of ____________ feet per turn. (-1 pg 6-9) | show 🗑
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| show | False – turn needle will show the direction of the spin.
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| show | True
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| show | True
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| show | Oscillatory
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| show | True
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| T or F A progressive spin is a result of misapplication of recovery controls. (-1 pg 6-9) | show 🗑
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| What is the best means of recovery if a progressive spin is inadvertently encountered? (-1 pg 6-9) | show 🗑
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| An aggravated spin is caused by ____________. (-1 pg 6-9) | show 🗑
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| What is the best means of recovery if an aggravated spin is inadvertently encountered? (-1 pg 6-9) | show 🗑
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| show | Prohibited
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| Intentional spins in other than cruise configuration at idle power are ____________.(-1 pg 6-10) | show 🗑
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| Erect spin recovery is ___________ after recovery controls are applied. (-1 pg 6-10) | show 🗑
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| When spin recovery controls are applied the pitch attitude will ___________ and spin rate will initially ____________.(-1 pg 6-10) | show 🗑
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| show | 1 ½
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| show | 500, 1500-2000
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| show | True
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| Altitude loss during dive recovery is determined by the following independent factors. (-1 pg 6-11) | show 🗑
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| show | True
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