Index
L
- Landing stuck left pedal — 11-17
- stuck neutral or right pedal — 11-17
- Leading edge — 2-8
- Lift — 2-3
- Loading Chart Method — 6-4
- Low-G Conditions and Mast Bumping — 11-14
- Low Reconnaissance — 10-2
- Low Rotor RPM and Rotor Stall — 11-15
- LTE at Altitude — 11-21
M
- Main Rotor disk interference (285–315°) — 11-20
- system — 4-2
- transmission — 4-11
- Maximum Performance Takeoff — 10-2
- Medium and High Frequency Vibrations — 11-23
- Minimum Equipment Lists (MELs) and Operations with Inoperative Equipment — 8-2
- Moisture — 7-2
- Multi-Engine Emergency Operations — 11-23
- Myopia — 12-2
N
- Newton’s Third Law of Motion — 2-5
- Night Flight — 12-7
- Night Myopia — 12-2
- Night Traffic Patterns — 12-8
- Night Vision — 12-4
- Normal Approach to a Hover — 9-19
- Normal Approach to the Surface — 9-20
- Normal Descent — 9-5
- Normal Takeoff From a Hover — 9-12
- Normal Takeoff From the Surface — 9-12
- Normal Takeoffs and Landings — 11-13
- NOTAR® — 1-3
O
- Obstruction Detection — 12-5
- Oculogravic illusion — 13-13
- Out of Ground Effect — 2-12
P
- Passengers — 8-4
- PAVE Checklist — 13-6
- Pendular Action — 2-15
- Performance Charts — 7-2
- climb performance — 7-6
- Pilot at the Flight Controls — 8-6
- Pinnacle and Ridgeline Operations — 10-11
- Pitch Control — 2-17
- Powered Flight — 2-14
- Power Failure in a Hover — 11-8
- Practice Autorotation With A Power Recovery — 11-7
- Preflight — 8-2,12-7
- Presbyopia — 12-2
R
- Ramp Attendants and Aircraft Servicing Personnel — 8-4
- Rapid Deceleration or Quick Stop — 10-4
- Rearward Flight — 2-24
- Reciprocating Engines — 4-14
- Reconnaissance Procedures — 10-2
- Recovery From Low Rotor RPM — 11-16
- Recovery Technique — 11-21
- Relative-Motion Illusion — 12-6
- Relative wind — 2-8,2-9
- Resultant relative wind — 2-8,2-9
- Retreating Blade — 2-20
- Retreating Blade Stall — 11-10
- Reversible Perspective Illusion — 12-6
- Rigid Rotor System — 4-3
- Rods — 12-4
- Root — 2-9
- Rotational Relative Wind (Tip Path Plane) — 2-9
- Rotorcraft — 1-1
- Rotorcraft Flight Manual (RFM) — 5-1
- aircraft and systems description — 5-5
- emergency procedures — 5-4
- general information — 5-2
- handling, servicing, and maintenance — 5-5
- normal procedures — 5-5
- operating limitations — 5-2
- airspeed — 5-2
- altitude — 5-3
- flight — 5-4
- placards — 5-4
- powerplant — 5-3
- rotor — 5-3
- weight and loading distribution — 5-4
- performance — 5-5
- preliminary pages — 5-2
- safety and operational tips — 5-6
- supplements — 5-6
- weight and balance — 5-5
- Rotor Safety Considerations — 8-3
- Rotor System — 1-3
- Running/Rolling Takeoff — 10-3
S
- Shallow Approach and Running/Roll-On Landing — 10-6
- Sideward Flight — 2-23
- Sikorsky, Igor — 1-2
- Single-Engine Failure — 11-23
- Slips — 9-4
- Slope Takeoff — 10-8
- Slope Takeoffs and Landings — 11-13
- Stability Augmentations Systems — 4-17
- Structural Design — 4-12
- Swash Plate Assembly — 4-6
- synchropter — 1-4
- System Malfunctions — 11-16
T
- Takeoff — 10-10
- Tandem rotor — 1-3,4-6
- Taxiing — 9-10
- Taxi Technique — 12-8
- The Effect of Weight Versus Density Altitude — 7-3
- The Four Fundamentals — 9-2
- Throttle — 1-6
- Throttle Control — 3-2
- Thrust — 2-3,2-6
- Tip — 2-9
- Traffic Patterns — 9-17
- Trailing edge — 2-8
- Translating Tendency or Drift — 2-15
- Translational Lift — 2-21
- Transmission System — 4-10
- Transverse Flow Effect — 2-23
- Turbine — 4-10
- Turbine Age — 1-2
- Turbine Engines — 4-16
- Turning Flight — 2-24
- Turns — 9-3
- Twist — 2-9
U
- Unanticipated Yaw/Loss of Tail Rotor Effectiveness (LTE) — 11-18
- Use of Collective — 11-13
V
- Venturi effect — 2-4
- Vertical Flight — 2-17
- Vertical Takeoff to a Hover — 9-6
- VFR Flight into IMC — 11-24
- Vision in Flight — 12-2
- Visual Acuity — 12-3
- Visual Deficiencies — 12-2
- Vortex Ring State — 11-9
- Vuichard Recovery — 11-10