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Slow Flight
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Procedure:
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3,000' agl +
-
clearing turns
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retard throttles to
15" MAP
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gear & flaps as specified by
examiner
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power required to maintain 90 knots
(1.2*Vs1), +10/-5
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maintain altitude
& heading +/- 100' +/- 10°
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turns up to 30° may
be required, +/- 10° bank
Recovery:
AimTo determine that the candidate can demonstrate good energy
management skills (power/drag) by maintaining safe flight control in all
configurations while maneuvering at speeds in the final approach speed
range.
Description
At an operationally safe altitude or the
manufacturer’s recommended minimum height, whichever is higher, the
candidate will be asked to stabilize the airplane at
1.3 Vso
KIAS or Vmc+10 knots, whichever is greater.
The examiner will then ask the candidate to extend the gear and full
flap deflection and to maneuver the aircraft while maintaining this
reduced airspeed.
In colder temperatures, good airmanship may dictate the extension of
initial approach flap to a maximum of one-half (½) of full deflection to
reduce adverse effects on the engines while slowing to and stabilizing
at the required speed.
Performance Criteria
Assessment will be based on the candidate’s ability to:
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demonstrate good power management;
-
use sufficient rudder for coordinated flight throughout the
maneuver;
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maintain the selected airspeed (+10/-5 knots);
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use appropriate bank angles while maneuvering;
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maintain specified heading(s) during straight flight
(±10 degrees);
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maintain the specified altitude (±100 feet); and
NOTE: This exercise is to be conducted in level
flight. There is no requirement to climb or descend at the target
airspeed.
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Power Off (Landing Configuration) Stalls
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Procedure:
-
3,000' agl +
-
clearing turns
-
retard throttles
15"
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gear & flaps in
specified configuration
-
slow airplane at approach
- t/o speed
-
establish
landing
attitude
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straight ahead or 20°
bank turns
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power to idle
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pitch attitude that will
induce a stall
-
announce first indication
of stall
Recovery:
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At the first indication of buffet or control loss
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slightly lower nose
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add climb (full) power
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level wings
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retract 3rd notch of flaps
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retract gear
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retract 2nd then 1st notch of flaps
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accelerate to Vy
Aim
To determine that the candidate
can recognize and recover smoothly and correctly from an approach to a stall
in a landing configuration with a minimum loss of altitude.
Description
At an operationally safe altitude that would allow
recovery at or above 2,000 feet AGL or the minimum height recommended by the
manufacturer, whichever is higher, a stall will be approached in the landing
configuration from straight and level flight, with the power set at or near
idle on all engines. The candidate will recognize and recover smoothly and
correctly at the first indication of an imminent stall with
a minimum loss of altitude.
Performance Criteria
Assessment will be based on the candidate’s ability to:
-
complete appropriate safety precautions before approaching the
stall;
-
establish the airplane in a landing configuration with landing gear
extended and full flap deflection;
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transition smoothly to an attitude that will induce a stall;
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recognize and announce the onset of an imminent
stall by identifying the first indication (warning horn or light, buffet
or decaying control effectiveness);
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avoid entering a stall;
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promptly and smoothly recover at the first indication using control
application in the proper sequence and appropriate attitude control;
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maintain directional control;
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retract flaps as recommended;
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retract the landing gear after a positive rate of climb is
established, or as recommended by the manufacturer;
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recover safely with minimum loss of altitude; and
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return to the altitude, heading and airspeed specified by the
examiner.
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Power On (Clean Configuration) Stalls
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Procedure:
-
3,000' agl +
-
clearing turns
-
retard throttles
15"
-
gear & flaps in
specified configuration
-
slow airplane at approach
- t/o speed
-
establish approach/takeoff
attitude
-
straight ahead or 20°
bank turns
-
20" 2400
rpm (55% power min.)
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pitch attitude that will
induce a stall
-
announce first indication
of stall
Recovery:
Aim
To determine that the candidate
can recognize and recover smoothly and correctly from an actual stall in a
clean configuration with a minimum loss of altitude.
Description
At an operationally safe altitude that would allow
recovery at or above 2,000 feet AGL or the minimum height recommended by the
manufacturer, whichever is higher, a stall will be entered in a clean
configuration from straight and level flight, with the power set at or near
idle on all engines. The candidate will recognize, enter and recover
smoothly and correctly from an actual stall, with a minimum loss of
altitude.
Note: In cases where the POH/AFM states that
intentional stalls should be avoided or are prohibited, the candidate will
be expected to recover at the first indication of an imminent stall.
Performance Criteria
Assessment will be based on the candidate’s ability to:
-
complete appropriate safety precautions before approaching the
stall;
-
establish the specified configuration;
-
transition smoothly to an attitude that will induce a stall;
-
recognize the onset of a stall;
-
enter a stall;
-
promptly and smoothly recover using control application in the
proper sequence and appropriate attitude control;
-
maintain directional control and recover safely with a minimum loss
of altitude;
-
avoid entering a secondary stall; and
-
return to the altitude, heading and airspeed specified by the
examiner.
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Return to Top
Steep Turns
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3,000' agl +
-
clearing turns
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20" 2400 rpm
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do not exceed Va
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roll into a coordinated 360°
turn; maintain a 45° bank.
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On rollout, Perform task in the
opposite direction for 360°
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Maintain entry altitude within +/- 100',
rolls out on entry heading within +/- 10°, airspeed within +/- 10 knots,
and bank within +/- 5°.
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Vmc Demonstration
Procedure:
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3,000' agl+
-
clearing turns
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Configuration:
landing gear retracted flaps up trim for takeoff propellers set for high RPM cowl flaps open on one closed on other
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close the throttle to idle on one engine (with cowl flaps closed)
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power on operating engine to takeoff manifold
pressure.
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directional control with rudder and aileron
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slowly reduce airspeed 1 mph/sec. with pitch
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limit rudder and aileron control by 84 knots (Vysse)
Recovery:
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FIRST indication of direction control loss or
stall horn recover by: lowering nose reducing power
on operating engine gain directional control
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regain altitude and control with operating engine
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climb at Vyse
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recover within 20° of entry heading
*Keep ball centered and wings level*
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Airspeed/Drag Demonstration
(This is only required if you are going for your Multi-Engine
Instructor or MEI)
Procedure:
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3,000' agl +
-
clearing turns
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retard throttles to 15"
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configuration: landing gear retracted flaps up propellers set for high RPM cowl flaps open on one, closed on other
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close the throttle to idle on one engine (with cowl flaps closed)
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power on operating engine to 31.5"
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zero side slip
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airspeed changes
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flaps 40° - note rate climb/descent - flaps 0°
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prop windmill - note rate climb/descent - prop feather
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gear down - note rate climb/descent
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flaps 40° - note rate climb/descent
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prop windmill - note rate climb/descent
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attempt single engine go-around with max drag
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Normal & Crosswind Takeoff, Climb &
Landing
Takeoff & Climb:
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Taxi into
position and align the airplane on the centerline.
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Ailerons
into the wind.
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Hold
brakes while advancing throttles smoothly to about
20".
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Double-check instruments that both engines are
running, and slowly release brakes.
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Advance
throttle all the way to take off power.
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If
crosswind conditions exist, slowly release aileron
input until the ailerons are neutral at point of
liftoff.
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Rotate
above Vmc-80 knots for liftoff-and accelerate to Vy.
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After a
positive rate of climb is established, put Gear Up.
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Maintain
power and Vy climb +10/-5 knots to a safe altitude.
Approach &
Landing:
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Consider
wind conditions and maintain a suitable track and
touchdown point.
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Maintain
120 knots on downwind.
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Midfield
downwind, verify below VLO speed, then
put Gear Down.
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Abeam the
touchdown point, First notch of Flaps.
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Power
back to 15" mp and turn to base.
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2nd notch
of flaps, maintain 110 knots.
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Turn to
final, 3rd notch of flaps as needed, and GUMPF
Gas on best tank if appropriate
Undercarriage (3 in the Green)
Mixtures Rich
Props Set
Flaps on as appropriate
Yaw dampener off
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Maintain
a stabilized approach at 100 knots
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Quadruple
check that Gear is Down.
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Touch
down within 400 feet of a specified spot, with no
drift, on the centerline.
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Maintain
any crosswind correction as necessary for landing,
and directional control throughout the approach and
landing.
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Ailerons
into the wind.
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EXIT
RUNWAY then complete appropriate checklist:
Flaps Up
Cowl Flaps Open
Transponder Standby
Mixtures Leaned for Taxi
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Short Field Takeoff, Climb & Landing
Takeoff & Climb:
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Taxi into
position at the very end of the runway, and align
the airplane on the centerline. Set flaps as
required.
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Ailerons
into the wind.
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Hold
brakes firmly while advancing throttles smoothly to
takeoff power.
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Double-check instruments that both engines are
running, and carefully release brakes.
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Maintain
directional control and centerline with minimal
rudder input-no brakes.
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Rotate
above Vmc at recommended short field lift off speed,
and accelerate to Vx.
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After a
positive rate of climb is established, put Gear Up.
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Maintain
power and Vx climb +10/-5 knots until obstacle is
cleared or airplane is 50 feet above the surface.
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After
obstacle is cleared, accelerate to and maintain Vy
for +10/-5 knots to the appropriate altitude.
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If any
flaps were used, retract flaps.
Approach &
Landing:
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Consider
wind conditions and maintain a suitable track around
the pattern, and touchdown point.
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Maintain
120 knots on downwind.
-
Midfield
downwind, verify below VLO speed, then
put Gear Down.
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Abeam the
touchdown point, First notch of Flaps.
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Power
back to 15" mp and turn to base.
-
2nd notch
of flaps, maintain 110 knots.
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Turn to
final, 3rd notch of flaps as needed, and GUMPFY
Gas on best tank if appropriate
Undercarriage (3 in the Green)
Mixtures Rich
Props Set
Flaps on as appropriate
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Maintain
a stabilized approach at 90 knots
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Quadruple
check that Gear is Down.
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Touch
down within 200 feet of a specified spot, with no
drift, minimal float, and on the centerline.
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Maintain
any crosswind correction as necessary for landing,
and directional control throughout the approach and
landing.
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Ailerons
into the wind.
-
Apply
brakes as needed to stop in the shortest distance
consistent with safety.
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EXIT
RUNWAY then complete appropriate checklist:
Flaps Up
Cowl Flaps Open
Transponder Standby
Mixtures Leaned for Taxi
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Go-Around/Rejected Landing
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Make the
decision to abort the approach in a timely manner.
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Apply
take-off power Immediately and transition to climb
pitch attitude for Vy.
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Retract
3rd notch of flaps.
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When you
have positive rate of climb, Retract Landing Gear.
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When
stabilized, retract 2nd, then 1st notch of flaps.
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Maintain
power and climb at Vy within +10/-5 knots to a safe
maneuvering or pattern altitude.
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Emergency Descent
(Chop-Drop-Prop)
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Chop-Power to Idle, bring nose up until airspeed is
within gear-down speed.
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Drop-Gear
Down.
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Prop-Push
Prop Full Forward
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Pitch for
152 knots (Max Gear Extended Speed), bank away from
the burning engine if it is a fire, about 30 degree
bank.
Note: Be able to recognize situations such as
depressurization or cockpit smoke and/or fire that
require an emergency descent. Maintain positive
load factors during the descent, and if you are high
enough and have time, complete the appropriate
checklist. |
Engine Failure
During Take-off Before Vmc (Simulated)
(Chop-Hop-Stop)
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Chop
Power-Close BOTH throttles smoothly and immediately
when simulated engine failure occurs.
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Hop on
the rudders-Maintain directional control on runway
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Stop-Smoothly apply brakes as needed.
Note:
Engine failure on take-off roll will be simulated only,
and is to be accomplished Before reaching 50% of the
calculated Vmc. |
Engine Failure
After Lift-Off (Simulated)
(Must be done at a minimum of 500' AGL)
Engine Failure
At Cruise (Simulated)
Engine Failure
to Full Feather At Cruise (Actual)
(The full feathering of one propeller will be demonstrated in flight
in airplanes that can safely perform that maneuver. It will be
performed high enough and in situations where safe landings can be
assured. If the propeller can not be unfeathered during the
practical exam, it will be treated as an actual emergency.)
Instrument
Approaches
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If you hold an Instrument Rating, for
your instrument privileges to extend to your
Multi-Engine License, in addition to the maneuvers
previously listed, you will also be expected to perform
partial panel and single-engine approaches during your
checkride. |
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