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BY ORDER OF THE SECRETARY OF THE AIR FORCE AIR FORCE ...

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32<br />

AFMAN 11-217V1 3 JANUARY 2005<br />

heading or while turning. (For a constant heading, pitch and bank control techniques<br />

are the same as discussed under straight and level flight.) During a turn, the change in<br />

lift vector affects pitch control. For example, when entering a turn after a constant<br />

airspeed climb or descent has been established, the pitch attitude will have to be<br />

decreased slightly to maintain the airspeed. When entering a turn while performing a<br />

rate climb or descent, be prepared to increase the pitch attitude slightly to maintain<br />

the vertical velocity and add power to maintain the airspeed.<br />

2.4.6. Level off. Level offs are required during all phases of instrument flight. The high<br />

rates of climbs or descents possible in some aircraft can cause an overshoot of the desired<br />

altitude. The following techniques are designed to allow for a precise, easily controlled<br />

level-off maneuver.<br />

2.4.6.1. Desired airspeed. At least 1,000 feet below or above the desired altitude,<br />

reduce the pitch attitude to obtain a maximum of 1,000 to 2,000 fpm rate of climb or<br />

descent. Adjust the power to maintain the desired airspeed. Knowledge of<br />

approximate or known values of power and pitch simplifies aircraft control during<br />

this phase of flight. When the lead point for level off is reached, perform a normal<br />

level off.<br />

2.4.6.1.1. NOTE: At 1,000 feet below or above the desired altitude, a pitch<br />

change of one-half the previous pitch angle will normally provide a more<br />

controllable vertical velocity at the lead point for level off.<br />

2.4.6.2. Pitch change for level off. The total pitch change required for level off can<br />

be estimated by dividing the vertical velocity by the mach number times 1,000 (or<br />

miles per minute times 100). For example, an aircraft climbing or descending at .6<br />

mach with a vertical velocity of 3,600 fpm would require approximately 6° of pitch<br />

change to obtain a level flight attitude.<br />

3,600 fpm = 6° or 3,600 fpm = 6°<br />

0.6 mach x 1,000 6 mpm x 100<br />

2.4.6.3. Selecting level-off point. Upon approaching the desired altitude, select a<br />

predetermined level off lead point. As a guide, use 10 percent of the vertical velocity.<br />

Smoothly adjust the power to an approximate setting required for level flight, and<br />

simultaneously change the pitch attitude to maintain the desired altitude.<br />

2.5. Basic Aircraft Control Maneuvers.<br />

2.5.1. Vertical "S" Series. The vertical "S" maneuvers are proficiency maneuvers<br />

designed to improved a pilot's crosscheck and aircraft control. There are four types: the<br />

A, B, C, and D.<br />

2.5.1.1. Vertical "S"- A. (Figure 2.5) The vertical "S"-A maneuver is a continuous<br />

series of rate climbs and descents flown on a constant heading. The altitude flown<br />

between changes of vertical direction and the rate of vertical velocity used must be<br />

compatible with aircraft performance. The vertical "S"- A if flown at final approach<br />

airspeed and configuration is excellent for practicing entry to and control of precision<br />

glide paths. The transition from descent to climb can be used to simulate the missed<br />

approach. However, allow sufficient altitude for "cleaning up" the aircraft and<br />

establishing the climb portion of the maneuver. Level off, reestablish configuration

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