Contact FTI Chapter 5 Flight Procedures Flashcards by What_If All

Fast Cruise

240 KIAS
~80% Torque
1 degree nose down

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Normal Cruise

200 KIAS
~54% Torque
0 degrees nose up

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Slow Cruise

150 KIAS
~33% Torque
3.5 degrees nose up

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Normal Climb

180 KIAS
100% Torque
8 degrees nose up

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Terminal Route Descent

200 KIAS
20% Torque
5 degrees nose down

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Fast Cruise Descent

240 KIAS
~40% Torque
5 degrees nose down

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No-Flap (NF) Configuration

120 KIAS / Gear Down, Flaps Up
~31% Torque
4 degrees nose up

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Takeoff Flap (TF) Configuration

120 KIAS / Gear Down, Flaps TO
~42% Torque
3 degrees nose up

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Landing Flap (LF) Configuration

120 KIAS / Gear Down, Flaps LDG
~52% Torque
1 degree nose up

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NOTE: Power settings are approximate and will vary with aircraft weight, altitude, etc. Make corrections as needed. Throughout this manual, when mandated by procedure to establish a specific power setting, a power setting within +- ___ % is acceptable. The only exception is for procedures that mandate a ____ % power setting to simulate the feathered condition or if maintaining a desired airspeed (the power setting is just an approximate starting point)

+-3%

4-6%

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For safety considerations, complete an operations check at least once every ___ minutes in flight, with the first check being accomplished during the ____.

20 minutes
initial departure climb

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The takeoff and climb process is one continuous maneuver divided into three separate steps:

1)
2)
3)

1) Takeoff Roll
2) Rotation
3) Initial Climb

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To rotate, apply backstick pressure at ___ KIAS

90 KIAS

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Takeoff attitude is ___ degrees nose high, spinner on or slightly below the ____

7-10 degrees nose high

Spinner on or slightly below the horizon

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Once two positive rate of climb (as noted on ___ and ___) are verified and a ___ cannot be made on the remaining runway in front of you, raise the gear and flaps. Accelerate to ___-___ KIAS (IAW local SOP or Course Rules)

Altimeter and VSI

safe landing

140-180 KIAS

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T-6B best rate of climb speed is ___ KIAS and ___ nose high

140 KIAS
15 degrees nose high

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[TAKEOFF 505.3.a]

Approaching hold short line (approximately ___ feet prior) switch to Tower frequency

200 feet

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[TAKEOFF 505.3.c]

After acknowledging tower’s “Cleared for takeoff” or “Lineup and wait” call, ___ clear final, then begin taxi to the takeoff position and initiate the ___ checklist. Verbally note ___ as called out by tower. Verify with ___, if available.

visually clear final

initiate Lineup Checklist

verbally note left or right crosswind

verify with windsock

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[TAKEOFF 505.3.d]

With the nosewheel centered, disengage NWS and complete ___ Checklist. Once cleared for takeoff, increase torque to ~___% and check engine instruments. Report over ICS, “Instruments checked.”

Lineup Checklist

~30% torque

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[TAKEOFF 505.3.e]

Select a reference point. Position the elevator ___ of neutral… To compensate for torque effect when left crosswind is below approximately ___ knots, add ___ aileron at MAX power. Release brakes, dropping your heels to the deck (toes off the brakes).

aft of neutral

10 knots

right aileron

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[TAKEOFF 505.3.f]

Release the brakes and allow the plane to roll forward momentarily to ensure the ___. Smoothly advance the PCL to MAX in ___ seconds. Anticipate the need for ___ rudder as the engine spools up. Maintain directional control.

nose wheel is centered

2-3 seconds

right rudder

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[TAKEOFF 505.3.g]

At ___ KIAS, check torque is at or above minimum power calculated on the Before Takeoff Checklist and fuel flow is less than ___ lbs. If not, abort the takeoff.

60 KIAS

800 lbs (per hour)

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[TAKEOFF 505.3.h]

At ___ KIAS, smoothly apply back-stick pressure and position the nose to takeoff attitude (___ degrees nose high, spinner on or slightly below the horizon). Allow the aircraft to fly itself off the deck.

90 KIAS

7-10 degrees

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[TAKEOFF 505.3.h]

NOTE: If gusty winds are present, increase rotation speed by ___ the gust factor (up to ___ KIAS)

1/2 the gust factor (up to 10 KIAS)

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[TAKEOFF 505.3.i] When a safe landing ___, check for two positive rate of climb (___ and ___) and airspeed below ___ KIAS. Report over ICS, "Two positive rate, Gear," then raise the gear. When airspeed is above ___ KIAS, Report over ICS, "Airspeed above ___ KIAS, Flaps." then raise the flaps. Report over the ICS, "Gear up, flaps up at XXX KIAS."

when a safe landing can no longer be made ALT and VSI 150 KIAS 110 KIAS, 110 KIAS

[TAKEOFF 505.3.i] NOTE: Retraction of flaps from the TO to UP position is not recommended below ___ KIAS to preclude the aircraft from settling back to the runway. However, there is no minimum to raise the flaps from the ___ to ___ position once safely airborne.

110 KIAS LDG to TO position

[TAKEOFF 505.3.j] Check nose attitude at ___ degrees nose high and continue acceleration, trimming as necessary. Approaching ___ KIAS, set the ___ knots climbing attitude and climb out in accordance with local SOP or Course Rules or departure procedures.

7-10 degrees nose high 180 KIAS, 180 knot climbing attitude

[CROSSWIND TAKEOFF 506.2] Use up to ___ aileron deflection into the wind at the ___ of the takeoff roll, and relax aileron input as speed ___ to the amount required to keep the wings level at liftoff.

up to full aileron deflection into the wind relax aileron input as speed increases

[CROSSWIND TAKEOFF 506.2] ___ rotate the aircraft off the runway when flying speed is reached to avoid side-slipping and damage to the tires. Once the aircraft has safely left the runway in controlled flight, ___ the wings, allow the aircraft to crab into the wind, and check ___ centered.

Firmly rotate level the wings balance ball centered

[Cruise to Climb 510.1] -Smoothly advance PCL to ___ -Raise the nose to ___ degrees nose high -Trim as required -As airspeed decreases to ___ KIAS, lower nose slightly to the normal climbing attitude, ~___ degrees nose high -Re-trim as necessary

-Max -12-15 degrees nose high -180 KIAS -~8 degrees nose high

[Climb to Cruise 510.2] -___ feet prior to level-off altitude, begin lowering nose toward the level flight attitude -Trim for acceleration -___ knots prior to desired cruise airspeed (P.A.T)

-200 feet prior to level-off -5 knots prior

[Cruise to Descent 510.3] -Smoothly reduce to ___% -Lower nose to the en route descent nose attitude (~___ degrees nose low) -Trim for power reduction and commence ___ turns as appropriate -Re-trim as necessary

- 20% torque - ~5 degrees nose low - clearing turns

[Descent to Cruise 510.4] -___ feet prior to level-off altitude, simultaneously (P.A.T.) -Re-trim as necessary

- 100 feet prior

The Turn Pattern (TP) is started in ___ or ___ cruise on any numbered heading.

Normal or Slow Cruise

The TP consists of 1) two ___ AOB turns in opposite directions for ___ degrees of heading change 2) two ___ AOB turns in opposite directions for ___ degrees of heading change 3) two ___ AOB turns in opposite directions for ___ degrees of heading change

1) 2x30 AOB for 90 degrees 2) 2x45 AOB for 180 degrees 3) 2x60 AOB for 360 degrees

[LEVEL SPEED CHANGE 513] The LSC maneuver will be commenced on any numbered heading. The sequence is flown from ___ cruise to the ___ configuration, to the ___ configuration, and then to ___ cruise.

Normal cruise No Flap Configuration Landing Flap Configuration Normal cruise

[LEVEL SPEED CHANGE 513.3] 1) ___ cruise on any numbered heading 2) PCL ___, below ___ KIAS gear 3) Stabilize at ___ configuration 4) Flaps ___ and stabilize at ___ configuration 5) ___ checklist 6) PCL ___, airspeed below ___ KIAS, raise gear and flaps. "Gear up, flaps up at XXX KIAS" 7) Accelerate to ___ cruise 8) Re-trim as necessary

1) Normal cruise 2) PCL idle, below 150 KIAS gear 3) Stabilize at NF configuration 4) Flaps LDG and stabilize at LDG Flap configuration 5) Before Landing Checklist 6) PCL MAX, airspeed below 150 KIAS, raise gear and flaps 7) Accelerate to normal cruise 8) Re-trim as necessary

[SLOW FLIGHT 514.3] 1) Complete maneuver above ___ feet AGL 2) Slow aircraft below ___ KIAS and configure with the landing gear down 3) ___ and ___ checklist 4) ___ area 5) Flaps ___, slow to approximately ___ KIAS while setting approximately ___ torque 6) Level, coordinated ___ AOB turn for ___ degrees of heading change (followed by same in opposite direction) 7) PCL ___, airspeed below ___ KIAS, raise gear and move flaps from LDG to TO. Once airspeed is above ___ KIAS, retract the flaps. "Gear up, flaps up at XXX KIAS" 8) Accelerate to ___ cruise 9) Re-trim as necessary

1) Complete maneuver above 6000 feet AGL 2) Slow aircraft below 150 KIAS and configure with the landing gear down 3) Before Landing and Pre-Stalling, Spinning, and Aerobatic Checklist 4) Clear area 5) Flaps LDG, slow to approximately 85 KIAS while setting approximately 45% torque 6) Level, coordinated 30 AOB turn for 180 degrees of heading change (followed by same in opposite direction) 7) PCL MAX, airspeed below 150 KIAS, raise gear and move flaps from LDG to TO. Once airspeed is above 110 KIAS, retract the flaps. "Gear up, flaps up at XXX KIAS" 8) Accelerate to normal cruise 9) Re-trim as necessary

[SCATSAFE 515] Complete maneuver above ___ feet AGL, slow the aircraft below ___ KIAS and configure with the landing gear down

6000 feet AGL Below 150 KIAS

[SCATSAFE 515] ___ and ___ checklist over ICS

Before Landing and Pre-Stalling, Spinning, and Aerobatic Checklist

[SCATSAFE 515] Clear working area, lower flaps to ___. Continue reducing airspeed to approximately ___ KIAS (___ units AOA), while setting approximately ___% torque NOTE: The ___ may be on throughout the maneuver

LDG 80 KIAS 15 units AOA 45% torque stick shaker

[SCATSAFE 515] S C A T S A F E

S - Straight and Level C- Coordination Exercise A- Adverse Yaw T- Torque and Turns S- Steep Turns A- Abrupt Control Movement F- Flap Retraction E- Effectiveness of Controls

[SCATSAFE 515.3] Straight and Level Back side of power curve. This is the sight picture a pilot should see at ___ during takeoff or just prior to ___ during landing.

rotation touchdown

[SCATSAFE 515.3] Coordination Exercise Conduct a series of left and right turns, using ___ angle of bank. Approximately ___ inches of right rudder is required to maintain straight and level, coordinated flight. Right turns require approximately ___ the rudder deflection to maintain coordination. Left turns require approximately ___ inch of right rudder to maintain coordination.

15-20 degrees angle of bank 2 inches of right rudder Twice the rudder deflection 1/2 inch of right rudder

[SCATSAFE 515.3] Adverse Yaw Without applying rudder, initiate a rapid right turn with ___ degrees bank. Note the initial tendency to yaw ___. After approximately ___ degrees of turn, roll out rapidly without using rudder. The nose continues past the selected point then comes back. (Repeat with coordinated rudder)

20 degrees bank yaw left 20 degrees of turn

[SCATSAFE 515.3] Torque and Turns The T-6B initially tends to pitch ___, yaw, and roll ___ if positive control is not maintained during full power takeoffs and landings. Quickly increase power to MAX and release the controls. Recover from buffet prior to stall. (Repeat with proper takeoff pitch and coordinated rudder)

pitch up, yaw and roll left

[SCATSAFE 515.3] Steep Turns Slowly increase bank towards ___ degrees AOB while adding power and back pressure to maintain level flight. Watch the wingtip appear to pivot around the selected point. Roll out of the bank to recover from the impending ___

60 degrees AOB impending stall

[SCATSAFE 515.3] Abrupt Control Movement Abruptly apply back-stick pressure to ___ degrees nose high to simulate snatching the control stick in the flare. The AOA rapidly increases and the aircraft progresses towards a full stall. Release backpressure to recover.

20 degrees nose high

[SCATSAFE 515.3] Flap Retraction From straight and level coordinated slow flight, raise the flaps from ___ to ___ without pausing at the ___ position. ... Recover from the stall by selecting ___ flaps

LDG to UP TO position

[SCATSAFE 515.3] Effectiveness of Controls Rapid control inputs, especially in the flare, often do not give the aircraft sufficient time to respond. Move the ailerons with small, ___ movements. Notice that even with aileron movement, there is ___ effect on heading or bank during slow flight. In slow flight, ___, ___ inputs are required to effectively control the aircraft as there is less airflow over the control surfaces at slow airspeeds

rapid movements little smooth, positive inputs

[ENERGY MANAGEMENT 516] Energy level is defined by ___ (kinetic energy) and ___ (potential energy) and is manipulated with ___, ___, and ___. Plan maneuvers in an order that minimize the requirement for deliberate energy changes, and make use of inherent energy gaining or losing properties of individual maneuvers

airspeed, altitude power, drag, G-loading

[ENERGY MANAGEMENT 516] ___ feet of altitude equals approximately ___ knots of airspeed with the canopy bow on the horizon and maximum power

1000 feet 50 knots

[ENERGY MANAGEMENT 516] In a typical MOA, optimum energy level for aerobatic maneuvering is ___ KIAS at an altitude midway between the top and bottom area limits

180-200 KIAS

[STALLS 517] A full or complete stall is caused by exceeding the wing's critical angle of attack (___ units) ... the ___ flow over the wing's top section is detached causing a drastic reduction in lift

18.0 units laminar flow

[STALLS 517] NOTE: When the aircraft stalls with torque above ___%, full right rudder and full right aileron will not prevent a left torque roll

60%

[STALLS 517] NOTE: When the aircraft stalls with power off at idle, the aircraft may pitch up to approximately ___ and roll off to the ___.

10 degrees right

[STALLS 517] Ways we detect a stall without instruments 1) 2) 3) 4)

1) Vision (aircraft attitude in relation to horizon, not including aerobatics) 2) Hearing (noise decreases as airspeed decreases, until airframe buffet) 3) Kinesthesia (seat of the pants ... plane settling) 4) Feel of control pressures (mushy controls)

[STALLS 517] The stick shaker will normally activate ___ knots prior to the stall based on aircraft weight, but is always activated at ___ units AOA.

5-10 knots prior 15.5 units AOA

[STALLS 517] WARNING: Stall recovery procedures have ___ effect on aircraft control if the aircraft has departed from controlled flight ... If aircraft condition (stalled or OCF) is in doubt, immediately execute ___.

no effect NATOPS Inadvertent Departure from Controlled Flight procedures

[STALLS 517] WARNING: If OCF in an unrecoverable rapid descent, EJECT if below ___ feet AGL.

6,000 feet AGL

[STALLS 517] WARNING: The AOA system may ___ the wing's actual AOA during rapid G onset (accelerated stall)

lag

[STALLS 517] WARNING: The surest stall indications regardless of AOA are: 1) 2) 3) 4)

1) un-commanded pitch up 2) nose drop 3) wing roll off 4) up and down pitch oscillations with successively increasing airspeed and G's known as pitch "bucking"

[STALLS 517] NOTE: The NATOPS stated stick shaker activation ___ knots prior to stall may only be valid during un-accelerated ___G flight.

5-10 knots prior 1G flight

[STALLS 517] Accomplish the THREE C's before performing stall maneuvers. The THREE C's may be accomplished in any order and are not required between individual maneuvers if flown in a series 1) 2) 3)

1) Configuration 2) Checklist - Pre-Stalling, Spinning, and Aerobatic Checklist 3) Clear Area

[STALLS 517] Recovery from all stall maneuvers must be accomplished above ___ feet AGL

6,000 feet AGL

[POWER-ON STALL 518] Aircraft pitch and bank angle will be held constant until un-commanded nose drop and/or unplanned rolling motion. An entry speed of ___ KIAS results in about ___ feet altitude gain.

150 KIAS 1500-2000 feet altitude gain

[POWER-ON STALL 518.d] Straight-Ahead Stall Adjust PCL to ___ torque. Raise the nose to a ___ degree nose high attitude

30-60% torque 15-40 degrees nose high attitude

[POWER-ON STALL 518.e] Recovery 1) 2) 3) 4) NOTE: Use maximum AOA to minimize altitude loss (___ units AOA) to attain best angle of climb Vx

1) RELAX 2) MAX *Simultaneously *3) LEVEL *4) BALL 14-17.9 units AOA

[POWER-ON STALL 518.f] Maneuver is complete when the aircraft is wings level with two positive rates of climb (as indicated on the ___ and ___)

altimeter and VSI

[POWER-ON STALL 518.g] Turning Stall Setup is the same as the straight-ahead stall, except ___ degrees angle of bank in either direction is added Recovery is the ___ as for the straight-ahead stall

20-30 degrees angle of bank same

[POWER-OFF STALL (ELP STALL) 519] Before starting this maneuver, ensure you have plenty of airspace below you, as you will lose at least ___ feet during the recovery, and will probably lose another ___ feet while setting up your dead engine glide.

800 feet 1000-2000 feet

[POWER-OFF STALL (ELP STALL) 519] Best glide speed in the clean configuration is approximately ___ KIAS with a sink rate of ___ feet per minute

125 KIAS 1350-1500 feet per minute

[POWER-OFF STALL (ELP STALL) 519] Begin the maneuver at slow cruise (___ KIAS) ... complete the maneuver above ___ feet AGL Perform the ___ checklist Clear the working area

150 KIAS Pre-Stalling, Spinning, and Aerobatic Checks

[POWER-OFF STALL (ELP STALL) 519.d] Roll wings level. If at or below 150 KIAS, retard PCL to ___% torque and begin decelerating towards best glide speed, ___ KIAS. If above 150 KIAS, retard PCL to ___% torque and zoom glide to capture best glide speed, ___ KIAS

4-6% torque 125 KIAS 4-6% torque 125 KIAS

[POWER-OFF STALL (ELP STALL) 519.e] As airspeed approaches ___ KIAS, lower nose to the ___ KIAS glide attitude (horizon bisecting windscreen). Crosscheck and Verbalize VSI for ___ feet per minute sink rate. Re-trim and stabilize

125 KIAS 125 KIAS 1350-1500 fpm

[POWER-OFF STALL (ELP STALL) 519.f] Simulate ___ and lower the landing gear; re-trim for ___ KIAS glide speed and commence a ___ degree AOB turn to ___. Complete the ___ checklist.

high key 120 KIAS 15-20 degree AOB low key Before Landing Checklist

[POWER-OFF STALL (ELP STALL) 519.g] Raise the nose to ___ degrees nose high attitude and allow airspeed to decay until the first indication of stall (airframe buffet or ___)

5-10 degrees nose high stick shaker

[POWER-OFF STALL (ELP STALL) 519.h] Maintain the turn or profile on ground track and recover by lowering the pitch attitude to put the prop arc on the horizon (~___ degrees nose low) until ___ KIAS is regained

~8 degrees nose low 120 KIAS

[LANDING PATTERN STALLS 520] If a stall indication occurs in the landing pattern, ___ ground track, and recover as described in the FTI. If in the landing pattern, do not hesitate to ___ if recovery appears unlikely. Approach Turn Stalls (ATS) may be practiced in either direction and in any ___ configuration

disregard ground track eject flap configuration

[LANDING PATTERN STALLS 520] Approach Turn Stall Establish the aircraft in the appropriate Downwind configuration (___ KIAS gear down, flaps as required) Perform the ___ checklist Clear Area

120 KIAS Pre-Stalling, Spinning, and Aerobatic Checklist, and the Before Landing Checklist

[LANDING PATTERN STALLS 520.d] Approach Turn Stall Simulate the transition near the Abeam position IAW Contact FTI landing pattern procedures. Power should be approximately ___% torque, airspeed ___/___/___ KIAS based on flap setting, trimmed in a descending ___ degree AOB turn to simulate the approach turn to final

20% torque 120/115/110 KIAS 30 degree AOB

[LANDING PATTERN STALLS 520.e] Approach Turn Stall Once stabilized on airspeed ___/___/___ KIAS in the simulated approach turn, raise the nose to ___ degrees nose high attitude, and retard PCL to idle. Adjust ailerons to maintain AOB between ___ degrees, and increase back stick pressure to hold the pitch attitude

120/115/110 KIAS 5-10 degrees nose high 20-45 degrees

[LANDING PATTERN STALLS 520.f] Approach Turn Stall At ___ indication of stall (___ or stick shaker) recover with ___ altitude loss

first indication airframe buffet minimal altitude loss

[LANDING PATTERN STALLS 520] Landing Attitude Stall Establish a simulated final approach at ___ knots above final approach airspeed commensurate with flap setting Perform the ___ checklist Clear Area

5-10 knots Pre-Stalling, Spinning, and Aerobatic Checklist and the Before Landing Checklist

[LANDING PATTERN STALLS 520] Landing Attitude Stall Retard the PCL to idle and execute a simulated ___. Hold the landing attitude constant until an approach-to-stall indication occurs. At first indication of stall (airframe buffet or ___) recover with minimal altitude loss

simulated landing transition stick shaker

[LANDING PATTERN STALLS 520] Landing Pattern Stall Recovery For Landing Pattern stalls, recover at ___ indication of stall (airframe buffet or stick shaker), whichever occurs ___. Do not enter a ___!

first indication first full stall

[LANDING PATTERN STALLS 520] Landing Pattern Stall Recovery NOTE: If at first indication of stall, the nose attitude is within ___ degrees nose high attitude, ___ the attitude to preserve altitude. If the nose is above this range, the attitude should be lowered (i.e. RELAX) to prevent a full stall from developing ... If the nose is lowered below ___ degrees nose high attitude during the impending stall, a prop strike or porpoise is likely

5-10 degrees nose high maintain 5-10 degrees nose high

[SLIP 521] A slip is an out-of-balance flight condition used to ___ sink rate and lose ___ altitude while maintaining a constant ___ and specific track over the ground. In a full slip, the rate of descent may be in excess of ___ feet per minute.

increase sink rate lose excess altitude constant airspeed 2,000 fpm

[SLIP 521] It will normally be demonstrated and introduced at altitude simulating the Slip to ___ at ___ KIAS, clean configuration. Slips may be demonstrated at ___ KIAS with gear down/flaps as required. Always announce the slip, "left/right wing down, left/right top rudder" NOTE: Caution must be exercised, since stall speed is ___ in this out-of-balance flight condition

high key 125 KIAS 120 KIAS increased

[SLIP 521] Take out the slip inputs smoothly/carefully with enough altitude remaining (___ feet) to slow the rate of descent and ensure positive control of the aircraft during the final moments of the maneuver to decrease the possibility of a ___ landing

200-300 feet hard landing

[SLIP 521] NOTE: The ___ warning light for the low-wing tank may illuminate regardless of fuel state

low-fuel

[SPIN 522] Two primary factors must be present for an aircraft to spin; ___ and ___

Stalled AOA Yaw (rotation about the vertical axis)

[SPIN 522] Practice spins to the left and right ... the spin entry is not a ___ maneuver. It requires ___ back stick (ailerons neutral), ___ deflected rudder, and PCL to idle.

finesse full back stick fully deflected rudder

[SPIN 522] If the aircraft will not recover, the pilot needs to recognize it in ample time to ___ safely. A spin progresses through three phases: 1) 2) 3)

eject 1) Post-stall gyrations 2) Incipient spin 3) Steady state spin

[SPIN 522] NOTE: Spins shall be practiced in the ___ configuration. In the event of an unintentional spin with gear and/or flaps down, they shall be retracted ___ to prevent possible damage by exceeding their ___ limitations

clean immediately airspeed

[SPIN 522] Post-stall gyrations A post-stall gyration can usually be identified by ___ (and often rapid) aircraft motions about any axis, a feeling that the controls are no longer ___ nor acting in the normal sense, stalled or near stalled angle of attack, transient or ___ airspeed indications, and ___ turn needle deflection. Recover with the ___ procedure

un-commanded effective erratic random Inadvertent Departure from Controlled Flight procedure

[SPIN 522] Incipient Spin An incipient spin can be identified by an ___ spin-like motion, a ___ turn needle, a stalled angle of attack, and airspeed that is accelerating or decelerating toward the ___. The incipient spin phase lasts approximately ___ turns. After completing the initial turn, the nose will pitch to approximately ___ degrees below the horizon, with pitch attitude becoming ___ Recover with the ___ procedure

oscillatory fully deflected steady state value two turns 60 degrees oscillatory Inadvertent Departure from Controlled Flight procedure

[SPIN 522] Steady State Spin After completing approximately ___ turns, the spin will have entered a near steady-state condition. Spin rotation will stabilize to approximately ___ seconds per turn, with altitude loss of ___ feet per turn. The angle of attack will be ___ units and airspeed will stabilize at ___ KIAS. The turn needle will be ___ deflected in the direction of the spin. Recover using the ___ procedure

three turns 2-3 seconds per turn 400-500 feet per turn 18+ units 120-135 KIAS fully deflected NATOPS erect spin recovery procedure

[SPIN 522] All spin maneuvers shall be done with a ___. Spin maneuvers may be performed over an undercast cloud layer that does not exceed ___ feet AGL

clearly defined horizon 4,500 feet AGL

[SPIN 522.3] Establish the aircraft in slow cruise (___ KIAS). Trim will remain ___ throughout the maneuver. Start the maneuver at an altitude so that the spin itself is entered below ___ feet pressure altitude, and recovered before ___ feet pressure altitude. Minimum entry altitude is ___ feet AGL Perform the ___ checklist Clear Area

150 KIAS constant 22,000 feet 10,000 feet 13,500 feet Pre-Stalling, Spinning, and Aerobatic Checklist

[SPIN 522] Trim the aircraft for ___ KIAS in straight and level flight Check wings level, retard the PCL to idle, and smoothly raise the nose to ___ above the horizon. When the gear warning horn activates, SNA shall ___ the warning horn, however, the ___ shall silence the horn prior to spin entry At the ___, lead the stall with a slight amount of ___ in the desired direction of spin When the aircraft stalls (recognized by the nose ___), smoothly apply full rudder in the direction of spin and full back-stick. Do not use ___ in the entry or during the spin Call out ___, ___, ___, ___/___

150 KIAS 30 degrees acknowledge IP Stick shaker rudder pitching down aileron altitude, AOA, airspeed, turn needle deflection/direction

[SPIN 522] Incipient Spin Recovery Initiate the ___ procedure in accordance with the NATOPS NOTE: When positioning the controls to neutral, it is not uncommon to mistakenly position the elevator slightly ___ of neutral. If the aircraft is not recovering as expected, slowly feed in ___ stick until the neutral elevator position is reached and the aircraft recovers

Inadvertent Departure from Controlled Flight procedure aft forward stick

[SPIN 522] Steady-State Spin Recovery Apply ___ rudder opposite to the direction of turn needle. Follow immediately with smooth, positive ___ stick to a position ___ of neutral. Do not use ___ Hold the controls in position until the rotation stops, and then recover from the unusual attitude with a minimum loss of altitude a) b) c) Continue the pullout until the nose is positioned to the level flight attitude. Emphasis is on smooth control inputs Check and report oil pressure (minimum of ___ psi) Add power as required

full rudder forward forward ailerons a) Neutralize the controls b) Level the wings by referencing the horizon c) Commence a smooth pullout 90 psi

Contact FTI Chapter 5 Flight Procedures Flashcards

(103 cards)