Commercial Flight Manuevers Flashcards

1
Q

What is a steep turn?

A
  • Steep turns are those resulting from a degree of bank (more than approximately 45 degrees)
  • Overbanking tendency of an airplane overcomes stability, and the bank tends to increase unless pressure is applied to the aileron controls to prevent it.
  • Maximum turning performance is attained and relatively high load factors are imposed.
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2
Q

What is the desired bank angle in a steep turn?

A

A bank angle of at least 50° (±5°) is desired.

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3
Q

What is the recommended entry speed for a steep turn?

A

Establish the manufacturer’s recommended airspeed or if one is not stated, a safe airspeed not to exceed VA.

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4
Q

How do you maintain altitude in a steep turn?

A
  • If the altitude begins to increase or decrease, changing elevator back pressure can be used to alter the altitude;
  • however, a more effective method is a slight increase or decrease in bank angle to control small altitude deviations.
  • If the altitude is decreasing, reducing the bank angle a few degrees helps recover or stop the altitude loss trend
  • if the altitude is increasing, increasing the bank angle a few degrees will help recover or stop the altitude increase trend.
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5
Q

What are the altitude, airspeed, bank, and heading tolerances for a steep turn?

A

Maintain the entry altitude, ±100 feet, airspeed, ±10 knots, bank, ±5°; and roll out on the entry heading, ±10°.

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6
Q

What is a chandelle?

A
  • A “chandelle” is a maximum performance climbing turn beginning from approximately straight and level flight
  • ending at the completion of 180° of turn in a wings-level, nose-high attitude at the minimum controllable airspeed.
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7
Q

In a chandelle, constant bank and changing pitch occur in what part of the maneuver?

A

The first 90° of turn require a constant 30° of bank and a gradual and constant change in pitch attitude.

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8
Q

In a chandelle, constant pitch and changing bank occur in what part of the maneuver?

A

The last 90° of turn requires a very gradual change in bank from 30° to 0° and a constant pitch attitude so as to arrive at minimum airspeed as the airplane is rolled out to a wings-level attitude.

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9
Q

What is the maximum amount of bank in the chandelle?

A

30° of bank.

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10
Q

What should your speed be upon completion of the chandelle?

A

You should begin a coordinated constant-rate rollout from the 90° point to the 180° point, ±10° just above a stall airspeed, and maintaining that airspeed momentarily avoiding a stall.

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11
Q

At what two points will your wings be level in a chandelle?

A

Immediately before entering the chandelle and upon rollout at the 180° point.

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12
Q

What is a lazy eight?

A

A lazy eight consists of two 180° turns, in opposite directions, while making u climb and a descent in a symmetrical paltern during check of the turns.

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13
Q

What procedures are recommended prior to beginning a lazy-eight maneuver?

A
  • Prior to performing a lazy eight, the airspace behind and above should be clear of other air traffic.
  • The maneuver should be enlered from straight-and-level flight at normal cruise power and at the airspeed recommended by the manufacturer or at the airplane’s design maneuYering speed.????
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14
Q

Where should the highest pitch attitude occur in a lazy eight?

A
  • At the 45° point the pitch attitude should be at a maximum and the angle of bank conti nuing to increase.
  • Also, at the 45° point, the pitch attitude should start to decrease slowly toward the horizon at the 90° reference point.
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15
Q

Where should the lowest nose-down attitude occur in a lazy eight?

A

When the airplane has turned 135°, the nose should be at its lowest pitch attitude.

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16
Q

What are the altitude, airspeed and heading tolerances allowed when performing a lazy eight?

A

You should achieve the following throughout the maneuver:

a. Approximately 30° bank at the steepest point.
b. Constant change of pitch , roll rate, and airspeed.
c. Altitude tolerance at 180° points, ±100 feet (30 meters) from entry altitude.
d. Airspeed tolerance at the 180° point, ±10° knots from entry airspeed.
e. Heading tolerance at the 180° point, ±10°.

17
Q

To summarize, describe the appropriate values to be obtained in a lazy eight at the entry, 45-, 90-, 135- and -180-degree points.

A

Entry

  • Level flight
  • Maneuvering or cruise speed (whichever is less) or manufacturer’s recommended speed

45° point

  • Maximum pitch-up attitude
  • Bank angle at 15°

90° point

  • Bank angle approximately 30°
  • Minimum airspeed
  • Maximum altitude
  • Level pitch attitude

135° point

  • Maximum pitch-down attitude
  • Bank approximately 15°

180° point

  • Level flight
  • Original heading (±10°)
  • Entry airspeed (±10 knots)
  • Entry altitude (±100 feet)
18
Q

What are eights-on-pylons?

A
  • Eights-on-pylons is a training maneuver that involves flying the airplane in circular paths, alternately left and right, in the form of a figure-8 around two selected points or pylons on the ground.
  • No attempt is made to maintain a uniform distance from the pylon.
  • Instead, the airplane is flown at such an altitude and airspeed that a line parallel to the airplane’s lateral axis, and extending from the pilot’s eye appears to pivot on each of the pylons.
19
Q

How do you determine pivotal altitude for eights-onpylons?

A
  • A rule of thumb for estimating pivotal altitude using true airspeed in no-wind conditions, or ground speed when the wind is blowing, is to square the speed and divide by 15 for miles per hour or 11.3 for knots.
20
Q

Does the pivotal altitude change in eights-on-pylons?

A
  • Yes, the pivotal altitude is critical and will change with variations in ground speed. Remember …

Ground speed goes UP, Pivotal Altitude goes UP.

Ground speed goes DOWN, Pivotal Altitude goes DOWN.

21
Q

How far should one pylon be from the other pylon in eights-on-pylons?

A

They should be of sufficient distance apart to permit straight and level flight between pylons.

22
Q

At the steepest point, the bank angle in an eights-onpylon maneuver should be what value?

A

Establish the correct bank angle for the conditions, not to exceed 40°.

23
Q

Where is the highest pivotal altitude likely to occur in eights-on-pylons?

A

As the airplane turns downwind the ground speed increases; consequently the pivotal altitude is higher and the airplane must climb to hold the reference line on the pylon.

24
Q

Where is the lowest pivotal altitude likely to occur in eights-on-pylons?

A

As the airplane heads into the wind, the ground speed decreases; consequently the pivotal altitude is lower and the airplane must descend to hold the reference line on the pylon.

25
Q

What action should you take if your wing reference point appears to move ahead of the pylon? Move behind the pylon?

A
  • If the reference line appears to move ahead of the pylon, the pilot should increase altitude.
  • If the reference line appears to move behind the pylon, the pilot should decrease altitude.
  • Varying rudder pressure to yaw the airplane and force the wing and reference line forward or backward to the pylon is a dangerous technique and must not be attempted.
26
Q

What is a power-off 180° accuracy approach and landing?

A

Power-off accuracy approaches and landings are made by gliding, with the engine idling, from a specific point on downwind to touchdown, in a normal landing attitude at or within 200 feet beyond the specified touchdown point.

27
Q

State the objective of learning a power-off 180° accuracy approach and landing.

A
  • The objective is to instill the judgment and procedures necessary for accurately flying the airplane, without power, to a safe landing.
  • The ability to estimate the distance an airplane will glide and maintain the proper glide path while maneuvering the airplane is the real basis of all power-off accuracy approaches and landings.
28
Q

What are the standards expected of a student when executing this type of approach and landing?

A

a. Complete the appropriate checklist.
b. Make radio calls as appropriate.
c. Plan and follow a flightpath to the selected landing area taking

into consideration altitude, wind, terrain, and obstructions.

d. Position airplane on downwind leg, parallel to landing runway.
e. Correctly configure the airplane.
f. As necessary, correlate crosswind with direction of forward slip

and transition to side slip for landing.

g. Touch down within -0/+200 feet from the specified touchdown point with no side drift, minimum float, and with the airplane’s longitudinal axis aligned with and over the runway centerline.

29
Q

What is a steep spiral?

A

A steep spiral is nothing more than a constant gliding turn, during which a constant radius around a point on the ground is maintained similar to the maneuver “turns around a point.” The radius should be such that the steepest bank will not exceed 60°.

30
Q

What is the objective of a steep spiral? (

A
  • The objective of this maneuver is to improve pilot techniques for airspeed control, wind drift control, planning, orientation, and division of attention.
  • The steep spiral is not only a valuable flight training maneuver, but has practical application by providing a procedure for dissipating altitude while remaining over a selected spot in preparation for landing, especially for emergency forced landings.
31
Q

During the steep spiral, how will you maintain a turn of constant radius around the selected spot on the ground?

A

Maintaining a constant radius during the maneuver will require correction for wind drift by steepening the bank on downwind headings and shallowing the bank on upwind headings. During the descending spiral, the pilot must judge the direction and speed of the wind at different altitudes and make appropriate changes in the angle of bank to maintain a uniform radius.

32
Q

What standards must you maintain when executing a steep spiral?

A

Start at an altitude that will allow a series of three 360°-turns. Maintain the specified airspeed ±10 knots, roll out toward object or specified heading ±10°, and do not exceed 60° of bank while applying wind drift correction to track a constant radius circle around a defined reference point.

33
Q

What is an accelerated stall?

A

Accelerated stalls are stalls that occur at higher indicated airspeeds and/or lower than anticipated pitch attitudes as a result of excessive loads being suddenly imposed on an aircraft during improperly executed steep turns, stall and spin recoveries, and pull-ups from steep dives.

34
Q

What is the objective of performing an accelerated stall?

A

The objective of demonstrating accelerated stalls is not to develop competency in setting up the stall, but rather to learn how they may occur and to develop the ability to recognize such stalls immediately, and to take prompt, effective recovery action.

35
Q

If an airplane is skidding-towards the outside of a steep turn, which wing will stall first?

A

It will have a tendency to roll to the inside of the turn because the inside wing stalls first.

36
Q

What standards must you maintain when executing an accelerated stall?

A

a. Clear the area.
b. Select an entry altitude that will allow the task to be completed

no lower than 3,000 feet AGL.

c. Establish the configuration as specified by the evaluator.
d. Set power appropriate for the configuration, such that the

airspeed does not exceed the maneuvering speed (V .J, flap

extension speed (VFE,), landing gear extended speed (VLE,), and

any other POH/AFM limitation.

e. Establish and maintain a coordinated turn in a 45° bank,

increasing elevator back pressure smoothly and firmly until an

impending stall is reached.

f. Acknowledge the cues and recover promptly at the first indication

of an impending stall (e.g., aircraft buffet, stall horn, etc.).

g. Execute a stall recovery in accordance with procedures set

forth in the POH/AFM.

h. Retract the flaps to the recommended setting, if applicable;

retract the landing gear, if retractable, after a positive rate of

climb is established.

  1. Accelerate to Yx or Vy speed before the final flap retraction;

return to the altitude, heading, and airspeed specified by the

evaluator.

37
Q

Additional Study Questions

  1. Why does the airplane have a tendency to overbank in a

steep turn? (FAA-H-8083-3)

  1. What effect will a steep turn have on an airplane’s stall

speed and load factor? Why? (FAA-H-8083-3)

  1. Discuss the potential outcome of the chandelle

maneuver if you use too much pitch initially; not enough

pitch initially. (FAA-H-8083-3)

  1. What altitude and airspeed will you use when entering a

chandelle? (FAA-H-8083-3)

  1. When entering a lazy eight, will you establish the bank

first, pitch first, or both at the same time? (FAA-H-8083-3)

  1. Discuss reference point selection for the lazy eight
    maneuver. (FAA-H-8083-3)
  2. When performing a lazy eight, why is more right rudder

required in the right turn than in the left turn?

(FAA-H-8083-3)

  1. When performing an eights-on-pylon maneuver, where

will the steepest angle of bank occur? (FAA-H-8083-3)

  1. Will the pivotal altitude change when changing the

angle-of-bank in an eights-on-pylon maneuver?

(FAA-H-8083-3)

1 o. What initial altitude and airspeed will you use when

entering an eights-on-pylon maneuver? (FAA-H-8083-3)

A

x