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VERTICAL VIBRATION—A vibration
in which the movement is up and
down, or vertical, as in an out-of-track
condition.
VORTEX RING STATE—A transient
condition of downward flight
(descending through air after just previously
being accelerated downward
by the rotor) during which an appreciable
portion of the main rotor system
is being forced to operate at
angles of attack above maximum.
Blade stall starts near the hub and progresses
outward as the rate of descent
increases.
WEIGHT—One of the four main
forces acting on a rotorcraft.
Equivalent to the actual weight of the
rotorcraft. It acts downward toward
the center of the earth.
YAW—The movement of a rotorcraft
about its vertical axis.
G-6
I-1
ABORTED TAKEOFF, GYROPLANE 21-1
ACCELERATE/STOP DISTANCE 21-1
AERODYNAMICS 2-1, 3-1, 16-1
autorotation, 3-8
forward flight, 3-5
general, 2-1
gyroplane, 16-1
helicopter, 3-1
hovering flight, 3-1
rearward flight, 3-8
sideward flight, 3-8
turning flight, 3-8
vertical flight, 3-4, 16-1
AERONAUTICAL DECISION MAKING (ADM) 14-1, 22-1
decision-making process, 14-3
definitions, 14-2
error chain, 14-1
factors affecting decision making, 14-5
hazardous attitudes, 14-6, 22-1
operational pitfalls, 14-8
origin, 14-2
pilot error, 14-1
risk management, 14-4
situational awareness, 14-8
stress management, 14-6
use of resources, 14-6
workload management, 14-7
AGONIC LINE 12-5
AIRCRAFT LIGHTING 13-3
AIRFOIL 2-1
angle of attack, 2-2
camber, 2-2
center of pressure, 2-1
chord line, 2-2
leading edge, 2-2
pitch angle, 2-2
relative wind, 2-2
resultant relative wind, 3-6
rotational relative wind, 3-6
span, 2-1
trailing edge, 2-2
twist, 2-1
AIRSPEED INDICATOR 12-1, 18-4
AIR TAXI 9-9
AIRWORTHINESS DIRECTIVE 6-4
ALTIMETER 12-2, 18-4
ANGLE OF ATTACK 2-2
ANTI-ICING SYSTEMS 5-11
ANTITORQUE PEDALS 4-3
ANTITORQUE SYSTEM FAILURE 11-11
ANTITORQUE SYSTEMS 1-2
tail rotor, 1-2
fenestron, 1-2
NOTAR®, 1-2
APPROACHES
confined area, 10-7
crosswind, 9-20
night, 13-5
normal to a hover, 9-19
normal to the surface, 9-20
pinnacle, 10-8
shallow approach, 10-5
steep, 10-4
ARM 7-4
ASYMMETRICAL AIRFOIL 2-1
ATTITUDE INDICATOR 12-3
ATTITUDE INSTRUMENT FLYING 12-1
AUTOKINESIS 13-3
AUTOPILOT 5-10
AUTOROTATION 11-1
aerodynamics, 3-8, 16-1
during instrument flight, 12-19
from a hover, 11-4
power recovery, 11-3
straight-in, 11-2
with turn, 11-3
AXIS OF ROTATION 2-2
BASIC EMPTY WEIGHT 7-1
BERNOULLI’S PRINCIPLE 2-3
BLADE
coning, 3-2
driven region, 3-9, 16-2
driving region, 3-9, 16-2
feather, 1-1
flap, 1-1, 16-6, 20-1
lead/lag, 1-1
reverse flow, 16-3
stall, 11-10
stall region, 3-9, 16-2
BLOWBACK 3-8
BUNTOVER 21-3
CARBURETOR 5-7
heat, 5-8
ice, 5-7
CENTER OF GRAVITY 7-2
aft CG, 7-2
forward CG, 7-2
lateral, 7-3, 7-7
CENTER OF PRESSURE 2-1, 16-5
CENTRIFUGAL FORCE 3-2, 3-8
CENTRIPETAL FORCE 3-8
CLUTCH
belt drive, 5-4
centrifugal, 5-4
freewheeling unit, 5-4
sprag, 5-4
COANDA EFFECT 1-3
COCKPIT MANAGEMENT 20-1
COLLECTIVE CONTROL, GYROPLANE 17-2
COLLECTIVE PITCH CONTROL 4-1
INDEX
A
B
C
I-2
COLLECTIVE PITCH/THROTTLE COORDINATION 4-2
COMPASS CORRECTION CARD 12-5
COMPASS DEVIATION 12-5
COMPASS ERRORS 12-4
COMPASS TURNS 12-17
CONFINED AREA OPERATIONS
approach, 10-7
takeoff, 10-8
CONING 3-2
CONING ANGLE 18-1
CORIOLIS EFFECT 3-2
CORRELATOR/GOVERNOR 4-2
CREW RESOURCE MANAGEMENT 14-2
CYCLIC CONTROL, GYROPLANE 17-1
CYCLIC PITCH CONTROL 4-2
DATUM 7-3
DECISION-MAKING PROCESS 14-3
DENSITY ALTITUDE 8-1, 20-5
DIRECT CONTROL 15-2
DISC LOADING 2-4
DISSYMMETRY OF LIFT 3-6, 16-3, 20-1
DIVERSION 11-15
DRAG 2-5
form, 2-5
induced, 2-5
parasite, 2-6
profile, 2-5
rotor, 16-4
skin friction, 2-5
total, 2-6
DUAL ROTOR SYSTEM 1-1
DYNAMIC ROLLOVER 11-7
EFFECTIVE TRANSLATIONAL LIFT 3-5
ELECTRICAL SYSTEMS 5-8
EMERGENCIES
aborted takeoff, 21-1
approach and landing, 21-3
autorotation, 11-1
buntover, 21-3
dynamic rollover, 11-7
ground resonance, 11-7, 21-3
instrument flight, 12-18
　
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