G
 

GO-AROUND 9-20, 20-15 GOVERNOR 4-2 failure, 11-14 GROSS WEIGHT 7-1 GROUND EFFECT 3-3 GROUND HANDLING 18-4 GROUND REFERENCE MANEUVERS 9-14, 20-8 rectangular course, 9-14, 20-8 s-turns, 9-16, 20-10 turns around a point, 9-17, 20-11 GROUND RESONANCE 11-7, 21-3 GYROPLANE components, 15-2 instruments, 18-3 stability, 16-5 types, 15-1 GYROSCOPIC INSTRUMENTS 12-3 attitude indicator, 12-3 heading indicator, 12-3 

turn indicators, 12-4 GYROSCOPIC PRECESSION 3-4
H

HANG TEST 19-4 HAZARDOUS ATTITUDES 14-5
anti-authority, 14-6, 22-3
impulsivity, 14-6, 22-1
invulnerability, 14-6, 22-1
macho, 14-6, 22-2
resignation, 14-6, 22-2 HEADING INDICATOR 12-3 HEIGHT/VELOCITY DIAGRAM 11-4, 19-3 HELICOPTER SYSTEMS 5-1
anti-icing, 5-11
autopilot, 5-10
carburetor, 5-7
clutch, 5-4
electrical, 5-8
engine, 5-1
environmental, 5-10
flight control, 4-1
fuel, 5-6
hydraulics, 5-9
main rotor, 5-4
pitot-static, 12-1
stability augmentation system, 5-10
swash plate assembly, 5-5
tail rotor drive, 5-3
transmission, 5-3 HIGH RATE OF DESCENT 20-12 HINGES 5-5 HOVERING
aerodynamics, 3-1
flight, 9-5 HOVERING OPERATIONS
autorotation, 11-4
forward flight, 9-7
rearward flight, 9-8
sideward flight, 9-7
turn, 9-6
vertical takeoff, 9-5 HOVER TAXI 9-9 HUMAN FACTORS 14-1 HYDRAULIC FAILURE 11-14
I
INDUCED DRAG 2-5 INDUCED FLOW 3-6 INSTRUMENT CROSS-CHECK 12-5 INSTRUMENT FLIGHT 12-5
aircraft control, 12-7
bank control, 12-9
emergencies, 12-18
straight-and-level flight, 12-7
straight climbs, 12-11
straight descents, 12-14
takeoff, 12-19
turns, 12-15
unusual attitudes, 12-18 INSTRUMENT INTERPRETATION 12-6 INSTRUMENT TURNS 12-15 30° bank turn, 12-17 climbing and descending turns, 12-17 compass turns, 12-17 timed turns, 12-16 turns to a predetermined heading, 12-16 ISOGONIC LINES 12-5
L

LANDING crosswind, 9-11, 20-14 high-altitude, 20-14 illusions, 13-4 night, 13-5 normal, 20-13 running/roll-on, 10-5 short-field, 20-13 slope, 10-6 soft-field, 20-14 LANDING GEAR 1-2, 15-3, 18-4 LAW OF CONSERVATION OF ANGULAR MOMENTUM 3-2 L/DMAX 2-6 LIFT 2-3, 16-4 Bernoulli’s Principle, 2-3 magnus effect, 2-3 Newton’s Third Law of Motion, 2-4 LIFT-OFF AT LOW AIRSPEED AND HIGH ANGLE OF ATTACK 21-1 LIFT-TO-DRAG RATIO 2-6 LOAD FACTOR 2-4 LOSS OF TAIL ROTOR EFFECTIVENESS 11-12 LOST PROCEDURES 11-16 LOW G CONDITIONS 11-10 LOW ROTOR RPM 11-10 LTE (See loss of tail rotor effectiveness)
M

MAGNETIC COMPASS 12-4 acceleration/deceleration error, 12-5 compass correction card, 12-5 magnetic deviation, 12-5 magnetic dip, 12-5 turning error, 12-5 variation, 12-4 MAGNUS EFFECT 2-3 MAIN ROTOR SYSTEM 1-1, 5-4 combination, 5-5 fully articulated, 1-1, 5-4 rigid, 1-2, 5-5 semirigid, 1-2, 5-5 MANEUVERS 9-1, 10-1, 20-1 after landing and securing, 9-20, 20-15 approaches, 9-19 climb, 9-13, 20-6 confined area operations, 10-7 crosswind landing, 9-20, 20-14