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Rotorcraft Flying Handbook, FAA-H-8083-21

Rotorcraft Flying Handbook, FAA-H-8083-21

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These charts, graphs, and tables vary in style but all<br />

contain the same basic information. Some examples<br />

of the performance information that can be found in<br />

most flight manuals include a calibrated versus indicated<br />

airspeed conversion graph, hovering ceiling<br />

versus gross weight charts, and a height-velocity diagram.<br />

[Figure 6-7] For information on how to use the<br />

charts, graphs, and tables, refer to Chapter 8—<br />

Performance.<br />

12,000<br />

10,000<br />

8,000 FT.<br />

DENSITY ALTITUDE<br />

MIXTURE<br />

FULL RICH<br />

ers should describe the systems in a manner that is<br />

understandable to most pilots. For larger, more complex<br />

rotorcraft, the manufacturer may assume a higher<br />

degree of knowledge. (For more information on rotorcraft<br />

systems, refer to Chapter 5—Helicopter Systems<br />

and Chapter 18—Gyroplane Systems.)<br />

HANDLING, SERVICING, AND<br />

MAINTENANCE<br />

The Handling, Servicing, and Maintenance section<br />

describes the maintenance and inspections recommended<br />

by the manufacturer, as well as those required<br />

by the regulations, and Airworthiness Directive (AD)<br />

compliance procedures. There are also suggestions on<br />

how the pilot/operator can ensure that the work is done<br />

properly.<br />

PRESSURE ALTITUDE ~ FEET<br />

8,000<br />

6,000<br />

4,000<br />

2,000<br />

OAT 0°F<br />

OAT 20°F<br />

OAT 40°F<br />

OAT 60°F<br />

OAT 80°F<br />

OAT 100°F<br />

OAT 120°F<br />

This section also describes preventative maintenance<br />

that may be accomplished by certificated pilots, as<br />

well as the manufacturer’s recommended ground handling<br />

procedures, including considerations for<br />

hangaring, tie down, and general storage procedures<br />

for the rotorcraft.<br />

SUPPLEMENTS<br />

The Supplements Section describes pertinent information<br />

necessary to operate optional equipment installed on<br />

the rotorcraft that would not be installed on a standard<br />

aircraft. Some of this information may be supplied by the<br />

aircraft manufacturer, or by the maker of the optional<br />

equipment. The information is then inserted into the<br />

flight manual at the time the equipment is installed.<br />

0<br />

1,400<br />

1,500<br />

1,600 1,700 1,800<br />

GROSS WEIGHT ~ LBS<br />

Figure 6-7. One of the performance charts in the Performance<br />

Section is the “In Ground Effect Hover Ceiling versus Gross<br />

Weight” chart. This chart allows you to determine how much<br />

weight you can carry and still operate at a specific pressure<br />

altitude, or if you are carrying a specific weight, what is your<br />

altitude limitation.<br />

SAFETY AND OPERATIONAL TIPS<br />

The Safety and Operational Tips is an optional section<br />

that contains a review of information that could<br />

enhance the safety of the operation. Some examples of<br />

the information that might be covered include: physiological<br />

factors, general weather information, fuel conservation<br />

procedures, external load warnings, low rotor<br />

r.p.m. considerations, and recommendations that if not<br />

adhered to could lead to an emergency.<br />

WEIGHT AND BALANCE<br />

The Weight and Balance section should contain all the<br />

information required by the <strong>FAA</strong> that is necessary to<br />

calculate weight and balance. To help you correctly<br />

compute the proper data, most manufacturers include<br />

sample problems. (Weight and balance is further discussed<br />

in Chapter 7—Weight and Balance.)<br />

AIRCRAFT AND SYSTEMS<br />

DESCRIPTION<br />

The Aircraft and Systems Description section is an<br />

excellent place to study and familiarize yourself with<br />

all the systems found on your aircraft. The manufactur-<br />

Airworthiness Directive (AD)—A<br />

regulatory notice that is sent out<br />

by the <strong>FAA</strong> to the registered owners<br />

of aircraft informing them of<br />

the discovery of a condition that<br />

keeps their aircraft from continuing<br />

to meet its conditions for airworthiness.<br />

Airworthiness<br />

Directives must be complied with<br />

within the required time limit, and<br />

the fact of compliance, the date of<br />

compliance, and the method of<br />

compliance must be recorded in<br />

the aircraft maintenance records.<br />

6-4

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