test

fast cruise

240 knots, clean, 80%, 1 deg nose down

normal cruise

200 knots, clean, 54%, 0 deg nose

slow cruise

150 knots, clean, 33%, 3.5 deg nose up

normal climb

180 knots, clean, max pwr, 8 deg nose up

terminal route descent

200 knots, clean, 20%, 5 deg nose down

no flap configuration

120 knots, gear down flaps up, 31%, 4 deg nose up

TO flap configuration

120 knots, gear down flaps TO, 42%, 3 deg nose up

landing flap configuration

120 knots, gear down flaps LDG, 52%, 1 deg nose up

When do you complete ops checks

initial departure climb and every 20 min

max climb

140 knots, clean, max pwr, 15 deg nose up

TO procedure

1. 200 ft prior to hold short call tower.
2. Radio, cleared by tower
3. clear left right and up, then lineup checklist,
4. line up on centerline and hold breaks,
5. 30% power, "instruments checked",
6. release breaks, smoothly PCL to max (2-3 sec),
7. 60

How much do you increase rotate speed in gusty conditions

1/2 gust factor up to 10 knots

off airspeed/on altitude correction in level flight

change power, adjust pitch, trim

off airspeed/off altitude correction in level flight

trade speed for altitude or vise versa

on airspeed/off altitude correction in level flight

reduce or add power, allow altitude to change, then return to original power

cruise to climb transition procedure

1. power to max,
2. attitude 12-15 deg nose high,
3. trim
4. as airspeed decreases to 180, lower nose to capture 8 deg nose high,
5. re trim

climb to cruise transition procedure

1. 200 ft prior to level off attitude, begin lowering nose,
2. trim for acceleration,
3. 5 knots prior to cruise airspeed
a. power 54% for normal cruise, 80% for fast,
b. attitude level
c. trim

during climbs greater than -----ft, ---- should be used to clear traffic

1000, TCAS

During climbs and descents, the -------- --------- becomes the nose attitude crosscheck instrument. When leveling off from a climb or descent, the ----- and ------- become the nose attitude crosscheck instruments.

airspeed indicator, altimeter, VSI

cruise to descent transition procedure

1. power reduce to 20%,
2. attitude 5 deg nose low (en route descent),
3. trim for power reduction
4. retrim

descent to cruise transition procedure

100ft prior to level off altitude, simultaneously:
1. power 54% for normal, 80% for fast cruise,
2. attitude raise nose,
3. trim for power addition,
4. retrim

turn pattern procedure

1. establish straight and level on heading,
2. clear area, turn on 90 deg turn with 30 AOB, clear other direction and flow into opposite 90 deg turn.
3. clear area, then reverse into 180deg turn at 45AOB. Clear and flow into opposite 180,
4. clear then do

level speed change sequence

normal cruise (200), downwind (120), landing flap (110), normal cruise (200)

level speed change procedure

1. cruise configuration at any heading.
2. reduce power to idle, trim for deceleration, when airspeed below 150, drop gear.
3. at 120 power to 31%, maintain 120.
4. stablalize and trim for downwind.
5. lower landing flaps, as airspeed approaches 110, powe

define kinesthesia

sense of change in direction or speed of motion

What happens with respect to feeling as stall approaches

lose control effectiveness

3 Cs before stall maneuvers

configuration, checklist, clear area

recovery from stall maneuvers must be above...

6000ft AGL

What defines energy level

airspeed (kinetic energy) and altitude (potential energy)

What three things manipulate energy level

power, drag, g-loading

With the canopy bow on the horizon and max power, what ratio can be accomplished by exchanging altitude for airspeed?

1000ft for 50 knots

optimum energy level in MOA

180-200 knots midway between altitude limits

3 methods of decreasing energy

low power, speed brake, increased AOA (G-loading)

best method to gain energy

climb 140-160 knots at max power

slow flight (SCATSAFE) procedure

1. configuration: slow below 150, drop gear (above 6000ft agl)
2. before landing and pre stalling checklist
3. clear area.
4. lower landing flaps, reduce airspeed to 80 knots (15 units), 45% torque

rudders for coordination exerciser during slow flight SCATSAFE

4 inches right pedal for righ turn, .5 in right pedal for left turn

AOB for coordination exercise during slow flight

15-20

AOB for adverse yaw exercise in slow flight

20 deg

AOB used for steep turns in slow flight

60 deg

when is a power-on-stall maneuver complete

positive rate of climb

For a power-on-stall, an entry speed of --- knots results in ---- to ---- ft altitude gain

150, 1500, 2000

power-on-stall procedure

1. configuration: clean, above 6000ft agl.
2. prestaling, spinning, aero checklist.
3. clear area.
4. power to 30-60%. nose 15-40 deg nose up.
5. increase stick backpressure until uncommanded nose drop or roll.
6. RELAX stick, MAX power, LEVEL wings, cent

best clean glide

125 knots with 1350-1500fpm sink rate

Power-off stall procedure (ELP)

1. configure slow cruise above 6000ft agl.
2. checklist.
3. clear area.
4. wings level. If at or below 150 reduce power to 4-6% and capture 125. If above 150, zoom glide first.
5. as approaching 125, lower nose to 125 knot glide attitude (horizon bisects

altitude loss in ELP stall

800ft

landing pattern stall procedure

1. configuration downwind.
2. checklist.
3. clear area.
4. transition to 180 and make simulated approach turn
5. raise nose 5-10 deg high, power to idle, AOB 20-45 deg, increase backstick pressure
6. recover at first indication of stall

rate of descent in full slip

2000fpm

how to initiate slip in a turn

lower inboard wing, increase top rudder

max speed where full rudder deflection is allowed in a slip

150knots

2 factors that must be present for a spin

stall and yaw

3 phases of spin

post stall gyrations, incipient spin, steady state spin

how to recover from post-stall gyrations

inadvertent departure from controlled flight procedure

Incipient spin phase lasts - turns. After completing the initial turn, the nose will pitch up to -- deg with pitch attitude becoming --------

2, 60, oscillatory

steady state spin characteristics

2-3 sec per turn, alt loss of 400-500 ft per turn, aoa 18, airspeed 120-135

Spins may be performed over an undercast cloud layer that does not exceed...

4500ft agl

spin entry procedure

1. configuration slow cruise (below 22,000ft recovered above 10000ft, min entry alt 13,500ft)
2. checklist.
3. clear area. clearing turn.
4. roll out of clearing turn. power to idle.
5. raise nose 30 deg above horizon. acknowledge gear warning horn.
6. at

incipient spin recovery

pcl - idle
controls - neutral
altitude - check
recover from unusual attitude
(inadvertent departure from controlled flight)

steady state spin recovery procedure

1. at spin entry, look inside for stalled AOA, 120-135 knots, turn needle pegged.
2. full opposite rudder, smooth forward stick (hold until rotation stops).
3. neutralize controls.
4. wings level.
5. smooth pull out with Gs.
6. after straight and level, c

fast cruise

240 knots, clean, 80%, 1 deg nose down

normal cruise

200 knots, clean, 54%, 0 deg nose

slow cruise

150 knots, clean, 33%, 3.5 deg nose up

normal climb

180 knots, clean, max pwr, 8 deg nose up

terminal route descent

200 knots, clean, 20%, 5 deg nose down

no flap configuration

120 knots, gear down flaps up, 31%, 4 deg nose up

TO flap configuration

120 knots, gear down flaps TO, 42%, 3 deg nose up

landing flap configuration

120 knots, gear down flaps LDG, 52%, 1 deg nose up

When do you complete ops checks

initial departure climb and every 20 min

max climb

140 knots, clean, max pwr, 15 deg nose up

TO procedure

1. 200 ft prior to hold short call tower.
2. Radio, cleared by tower
3. clear left right and up, then lineup checklist,
4. line up on centerline and hold breaks,
5. 30% power, "instruments checked",
6. release breaks, smoothly PCL to max (2-3 sec),
7. 60

How much do you increase rotate speed in gusty conditions

1/2 gust factor up to 10 knots

off airspeed/on altitude correction in level flight

change power, adjust pitch, trim

off airspeed/off altitude correction in level flight

trade speed for altitude or vise versa

on airspeed/off altitude correction in level flight

reduce or add power, allow altitude to change, then return to original power

cruise to climb transition procedure

1. power to max,
2. attitude 12-15 deg nose high,
3. trim
4. as airspeed decreases to 180, lower nose to capture 8 deg nose high,
5. re trim

climb to cruise transition procedure

1. 200 ft prior to level off attitude, begin lowering nose,
2. trim for acceleration,
3. 5 knots prior to cruise airspeed
a. power 54% for normal cruise, 80% for fast,
b. attitude level
c. trim

during climbs greater than -----ft, ---- should be used to clear traffic

1000, TCAS

During climbs and descents, the -------- --------- becomes the nose attitude crosscheck instrument. When leveling off from a climb or descent, the ----- and ------- become the nose attitude crosscheck instruments.

airspeed indicator, altimeter, VSI

cruise to descent transition procedure

1. power reduce to 20%,
2. attitude 5 deg nose low (en route descent),
3. trim for power reduction
4. retrim

descent to cruise transition procedure

100ft prior to level off altitude, simultaneously:
1. power 54% for normal, 80% for fast cruise,
2. attitude raise nose,
3. trim for power addition,
4. retrim

turn pattern procedure

1. establish straight and level on heading,
2. clear area, turn on 90 deg turn with 30 AOB, clear other direction and flow into opposite 90 deg turn.
3. clear area, then reverse into 180deg turn at 45AOB. Clear and flow into opposite 180,
4. clear then do

level speed change sequence

normal cruise (200), downwind (120), landing flap (110), normal cruise (200)

level speed change procedure

1. cruise configuration at any heading.
2. reduce power to idle, trim for deceleration, when airspeed below 150, drop gear.
3. at 120 power to 31%, maintain 120.
4. stablalize and trim for downwind.
5. lower landing flaps, as airspeed approaches 110, powe

define kinesthesia

sense of change in direction or speed of motion

What happens with respect to feeling as stall approaches

lose control effectiveness

3 Cs before stall maneuvers

configuration, checklist, clear area

recovery from stall maneuvers must be above...

6000ft AGL

What defines energy level

airspeed (kinetic energy) and altitude (potential energy)

What three things manipulate energy level

power, drag, g-loading

With the canopy bow on the horizon and max power, what ratio can be accomplished by exchanging altitude for airspeed?

1000ft for 50 knots

optimum energy level in MOA

180-200 knots midway between altitude limits

3 methods of decreasing energy

low power, speed brake, increased AOA (G-loading)

best method to gain energy

climb 140-160 knots at max power

slow flight (SCATSAFE) procedure

1. configuration: slow below 150, drop gear (above 6000ft agl)
2. before landing and pre stalling checklist
3. clear area.
4. lower landing flaps, reduce airspeed to 80 knots (15 units), 45% torque

rudders for coordination exerciser during slow flight SCATSAFE

4 inches right pedal for righ turn, .5 in right pedal for left turn

AOB for coordination exercise during slow flight

15-20

AOB for adverse yaw exercise in slow flight

20 deg

AOB used for steep turns in slow flight

60 deg

when is a power-on-stall maneuver complete

positive rate of climb

For a power-on-stall, an entry speed of --- knots results in ---- to ---- ft altitude gain

150, 1500, 2000

power-on-stall procedure

1. configuration: clean, above 6000ft agl.
2. prestaling, spinning, aero checklist.
3. clear area.
4. power to 30-60%. nose 15-40 deg nose up.
5. increase stick backpressure until uncommanded nose drop or roll.
6. RELAX stick, MAX power, LEVEL wings, cent

best clean glide

125 knots with 1350-1500fpm sink rate

Power-off stall procedure (ELP)

1. configure slow cruise above 6000ft agl.
2. checklist.
3. clear area.
4. wings level. If at or below 150 reduce power to 4-6% and capture 125. If above 150, zoom glide first.
5. as approaching 125, lower nose to 125 knot glide attitude (horizon bisects

altitude loss in ELP stall

800ft

landing pattern stall procedure

1. configuration downwind.
2. checklist.
3. clear area.
4. transition to 180 and make simulated approach turn
5. raise nose 5-10 deg high, power to idle, AOB 20-45 deg, increase backstick pressure
6. recover at first indication of stall

rate of descent in full slip

2000fpm

how to initiate slip in a turn

lower inboard wing, increase top rudder

max speed where full rudder deflection is allowed in a slip

150knots

2 factors that must be present for a spin

stall and yaw

3 phases of spin

post stall gyrations, incipient spin, steady state spin

how to recover from post-stall gyrations

inadvertent departure from controlled flight procedure

Incipient spin phase lasts - turns. After completing the initial turn, the nose will pitch up to -- deg with pitch attitude becoming --------

2, 60, oscillatory

steady state spin characteristics

2-3 sec per turn, alt loss of 400-500 ft per turn, aoa 18, airspeed 120-135

Spins may be performed over an undercast cloud layer that does not exceed...

4500ft agl

spin entry procedure

1. configuration slow cruise (below 22,000ft recovered above 10000ft, min entry alt 13,500ft)
2. checklist.
3. clear area. clearing turn.
4. roll out of clearing turn. power to idle.
5. raise nose 30 deg above horizon. acknowledge gear warning horn.
6. at

incipient spin recovery

pcl - idle
controls - neutral
altitude - check
recover from unusual attitude
(inadvertent departure from controlled flight)

steady state spin recovery procedure

1. at spin entry, look inside for stalled AOA, 120-135 knots, turn needle pegged.
2. full opposite rudder, smooth forward stick (hold until rotation stops).
3. neutralize controls.
4. wings level.
5. smooth pull out with Gs.
6. after straight and level, c