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fuselage drag, 16-5
horizontal stabilizer, 16-5
pitch inertia, 16-5
propeller thrust line, 16-5
rotor force, 16-6
trimmed condition, 16-6
STANDARD ATMOSPHERE 8-1
STANDARD-RATE TURN 12-4
STARTING PROCEDURE 9-2
STATIC STOPS 5-5
STEADY-STATE FLIGHT 2-4
STEEP TURNS 20-8
STRESS MANAGEMENT 14-6
S-TURNS 9-16, 20-10
SWASH PLATE ASSEMBLY 5-5
SYMMETRICAL AIRFOIL 2-1
SYSTEM MALFUNCTIONS 11-11
antitorque, 11-11
governor, 11-14
hydraulic, 11-14
main drive shaft, 11-14
TACHOMETER 5-3, 18-3
TAIL ROTOR 1-2, 5-3
TAIL ROTOR FAILURE 11-11
TAIL SURFACES 15-2
TAKEOFF
confined area, 10-8
crosswind, 9-11, 20-4
from a hover, 9-10
from the surface, 9-11
high altitude, 20-4
jump, 20-5
maximum performance, 10-2
night, 13-4
normal, 20-3
pinnacle, 10-9
running/rolling, 10-2
short-field, 20-4
slope, 10-6
soft-field, 20-5
to a hover, 9-5
TAXIING 9-8, 20-1
air, 9-9
hover, 9-9
night, 13-4
surface, 9-9
TEETER BOLT 18-1
TEETERING HINGE 5-5
THROTTLE 4-1, 17-1
THRUST 2-5, 16-4
TIP JETS 18-3
TIP-PATH PLANE 2-2, 9-5
TIP SPEED 3-7, 16-1
TORQUE 1-1, 3-1
TOTAL DRAG 2-6
TOWER BLOCK 18-1
TOWER PLATE 18-1
TRAFFIC PATTERNS 9-18
TRANSLATING TENDENCY 3-1
TRANSLATIONAL LIFT 3-5
R
S
T
I-6
TRANSMISSION 5-3
TRANSVERSE FLOW EFFECT 3-6
TRUE ALTITUDE 8-1
TURBINE ENGINE 5-1
TURN COORDINATOR 12-4
TURN-AND-SLIP INDICATOR 12-4
TURNS 9-12, 12-15, 20-7
aerodynamics, 3-8
TURNS AROUND A POINT 9-17, 20-11
UNANTICIPATED YAW 11-12
UNDERSLING ROTOR 3-3, 18-1
UNLOADED ROTOR 21-3
UNUSUAL ATTITUDES 12-18
USEFUL LOAD 7-1
VENTURI EFFECT 2-3
VERTICAL SPEED INDICATOR (VSI) 12-2
VIBRATIONS 11-14
low frequency, 11-15
medium and high frequency, 11-15
VISION IN FLIGHT 13-1
night, 13-2
VISUAL ILLUSIONS 13-3
autokinesis, 13-3
false horizon, 13-3
landing, 13-4
night myopia, 13-3
VNE (See never exceed speed)
VORTEX RING STATE 11-5
VSI 12-2
VX 20-3
VY 20-3
WEIGHT 2-4, 7-1
limitations, 7-1
WEIGHT AND BALANCE 7-1, 19-1
definitions, 7-1, 7-3, 7-4
WEIGHT AND BALANCE METHODS 7-4
combination method, 7-6
computational method, 7-4
loading-chart method, 7-5
WINGS 15-3
WORKLOAD MANAGEMENT 14-7
YAW, AIRCRAFT 2-5

　
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