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Archive / FAA Weight-Shift Control Aircraft Flying Handbook / FAA Weight-Shift Control Aircraft Flying Handbook: Chapter 10 — Weight and Balance

Chapter 10 — Weight and Balance

Chapter 10 — Weight and Balance — Part 1

FAA-H-8083-5 (2008)

Chapter 10

Airport Traffi c Patterns .....................................10-1

Introduction .................................................................10-1

Airport Operations .......................................................10-2

Standard Airport Traffi c Patterns .................................10-2

Chapter Summary ........................................................10-8

Chapter 11

Approaches and Landings ...............................11-1

Introduction ..................................................................11-1

Normal (Calm Wind) Approaches and Landings ........11-2

Throttle Use ..............................................................11-2

Base Leg ...................................................................11-2

Estimating Height and Movement ............................11-5

Roundout (Flare) ......................................................11-6

Touchdown ...............................................................11-7

After-Landing Roll ...................................................11-7

Effect of Headwinds During Final Approach ..............11-8

Stabilized Approach Concept ....................................11-10

Go-Around (Rejected Landings) ................................11-13

Power ......................................................................11-13

Short and Soft Field Landing Techniques .................11-14

Short-Field Approaches and Landings ...................11-14

Soft and Rough Field Approaches and Landings ...11-15

Power-on Approach and Landing for

Turbulant Air ....................................................11-16

Crosswind Approaches and Landings ........................11-17

Crosswind Pattern Procedures ...............................11-17

Effects and Hazards of High Crosswinds

for Approaches and Landings ................................11-17

Crosswind Landings ...............................................11-19

Maximum Crosswind Velocities ............................11-19

Steep Approaches .......................................................11-20

Steep Angle ............................................................11-21

Alternating Turns ...................................................11-21

Power-Off Accuracy Approaches ..............................11-21

90° Power-Off Approach .......................................11-22

180° Power-Off Approach .....................................11-23

360° Power-Off Approach .....................................11-25

Emergency Approaches and Landings

(Simulated Engine Out) .............................................11-26

Faulty Approaches and Landings ...............................11-27

Low Final Approach ...............................................11-27

High Final Approach ..............................................11-27

Slow Final Approach ..............................................11-27

Use of Power ..........................................................11-28

High Roundout .......................................................11-28

Late or Rapid Roundout .........................................11-28

Floating During Roundout .....................................11-28

Ballooning During Roundout .................................11-29

Bouncing During Touchdown ................................11-29

Porpoising ...............................................................11-29

Wing Rising After Touchdown ..............................11-30

Hard Landing ..........................................................11-30

Chapter Summary ......................................................11-30

Chapter 12

Night Operations ...............................................12-1

Introduction ..................................................................12-1

Pilot Requirements .......................................................12-2

Equipment and Lighting ..............................................12-2

Pilot Equipment ........................................................12-3

Airport and Navigation Lighting Aids .....................12-4

Night Vision .................................................................12-5

Unique WSC Flight Characteristics .............................12-7

Night Illusions ..............................................................12-7

Preparation and Prefl ight ..............................................12-8

Starting, Taxiing, and Runup .......................................12-8

Takeoff and Climb .......................................................12-9

Orientation and Navigation ........................................12-10

Approaches and Landings ..........................................12-11

Night Emergencies .....................................................12-12

Chapter Summary ......................................................12-13

Chapter 13

Abnormal and Emergency Procedures ...........13-1

Introduction ..................................................................13-1

Ballistic Parachute System (BPS) ................................13-2

Procedures for Using a BPS .....................................13-3

Emergency Landings ...................................................13-3

Types of Emergency Landings .................................13-3

Psychological Hazards .............................................13-3

Basic Safety Concepts ..............................................13-4

Attitude and Sink Rate Control ................................13-5

Terrain Selection ......................................................13-6

Approach ..................................................................13-6

Terrain Types ...........................................................13-7

Water Landings (Ditching) .......................................13-8

Emergency Equipment and Survival Gear ...............13-8

Engine Failure After Takeoff ...................................13-9

Emergency Descents ..................................................13-10

Infl ight Fire ................................................................13-10

Engine Fire .............................................................13-10

Electrical Fires ........................................................13-12

System Malfunctions .................................................13-12

Electrical System ....................................................13-12

Pitot-Static System .................................................13-12

Landing Gear Malfunction .....................................13-13

Inadvertant Propeller Strike ...................................13-13

Stuck or Runaway Throttle ....................................13-13

Abnormal Engine Instrument Indications ..............13-13

Weather Related Emergencies ...................................13-15

High Winds and Strong Turbulence .......................13-15

High Winds and Turbulence During

Cruise Flight .......................................................13-15

High Winds and Turbulence During Takeoffs

and Landings .......................................................13-15

High Winds During Taxi ....................................13-15

Inadvertent Flight into Instrument Meteorological

Conditions (IMC) ...................................................13-16

Recognition .........................................................13-17

Maintaining Aircraft Control ..............................13-17

Attitude Control ..................................................13-18

Turns ...................................................................13-18

Chapter Summary ......................................................13-19

Glossary ..............................................................G-1

Index ......................................................................I-1

Introduction

Weight-shift control (WSC) aircraft means a powered aircraft

with a framed pivoting wing and a fuselage controllable only

in pitch and roll by the pilot’s ability to change the aircraft’s

center of gravity (CG) with respect to the wing. Flight control

of the aircraft depends on the wing’s ability to deform fl exibly

rather than on the use of control surfaces.

This chapter provides background on the development of the

WSC aircraft, its unique characteristics, the requirements for

obtaining a WSC license (airman certifi cate), aeronautical

decision-making (ADM), and the unique medical factors

required to operate WSC aircraft safely. Further, it is highly

recommended that all pilots develop a general understanding

of aviation by becoming familiar with the Pilot’s Handbook

of Aeronautical Knowledge and the Aeronautical Information

Manual (AIM). Listings of other available handbooks can be

found on the Federal Aviation Administration (FAA) website

at www.faa.gov.

Introduction To

Weight-Shift Control

Chapter 1

Figure 1-1. Otto Lilienthal, the German “Glider King.”

Figure 1-2. Various models of Otto Lilienthal’s glider, the forerunner of weight-shift control aircraft today.

History

From the beginning of mankind, we have looked to the skies

where legends and myths have entertained and provided us

the dream to fl y. Through the middle ages, the idea of fl ight

evolved across Europe, with Leonardo Da Vinci well known

for designing fl ying machines to carry humans. In 1874, Otto

Lilienthal, a German mechanical engineer, started designing,

building, and flying bird-like wings. [Figure 1-1] He

published his work in 1889, and by 1891 made fl ights of

over 100 feet in distance. Otto was the fi rst successful hang

glider pilot to design, build, and fl y a number of wing designs.

[Figure 1-2]

In 1903, the Wright brothers’ gliders became powered and

the airplane was born as the Wright Flyer. In the early 1900s,

aircraft confi gurations evolved as faster speeds and heavier

loads were placed on aircraft in fl ight. As a result of the new

demands, the simple fl exible wing was no longer suffi cient

and aircraft designers began to incorporate rigid wings with

mechanical aerodynamic controls. These new ideas in wing

design eventually resulted in the familiar aileron and rudder

confi gurations found on the modern airplane.

Commercial applications were driving the need for faster and

heavier aircraft; however, the dream of achieving manned

powered fl ight in its most bird-like form was evolving along

a different path. As rigid wing design enjoyed development

for military and commercial applications, the fl exible wing

concept lay largely dormant for decades. In 1948, a fl exible

wing design was created by Francis Melvin Rogallo as a fl ying

toy kit for which he obtained a patent in 1951. [Figure 1-3]

Rogallo’s design concept evolved down two parallel paths

in the early 1960s, military and sport fl ight. The military

application was the National Aeronautics and Space

Administration (NASA) development of the Rogallo wing

into the Paresev (Paraglider Research Vehicle) later renamed

the Parawing. That aircraft had rigid leading edges shown

in Figure 1-4. NASA had the cart attached to the keel hanging

below the wing and using weight shift to control the wing in

the same fashion as modern WSC aircraft today.

Figure 1-3. Rogallo’s flexible wing for a kite, submitted for patent

in 1948.

Figure 1-5. Barry Palmer flying a foot-launched hang glider in

1961.

Figure 1-4. NASA testing the Rogallo wing, which led to the modern

hang glider and WSC aircraft.

During this same period, other pioneering engineers and

enthusiasts started developing the Rogallo wing for sport. One

was aeronautical engineer, Barry Palmer, who saw pictures of

the NASA wings and, in 1961, constructed and fl ew a number

of hang gliders based on the Rogallo design. [Figure 1-5]

His efforts and others evolved to the WSC aircraft in the late

1960s. Another pioneer was John Dickenson of Australia

who used the NASA Rogallo wing design but incorporated

a triangular control bar that provided structure for the wing

during fl ight with fl ying wires. [Figure 1-6]

Original source PDFPublished from pages 12–17 of the recorded source chapter.
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