ID: 3658
Customer: Oleg Ostapenko E-mail: ostapenko2002@yahoo.com
Customer: Oleg Ostapenko E-mail: ostapenko2002@yahoo.com
PRINCIPLES OF FLIGHT INDEX
Flutter |
274, 323 |
Flying Control Surfaces |
255, 267 |
Force |
8 |
Form Drag |
94 |
Fowler Flap |
206 |
Free-stream Airfow |
70 |
Friction |
9 |
Frise Ailerons |
266 |
G
General Limitations |
321 |
Geometric Pitch |
148 |
Glide Performance |
124 |
Gravitational Acceleration |
130 |
Gravitational Field |
129 |
Gravity |
33 |
Ground Effect |
109, 111 |
Ground Loads |
342 |
Gust Envelope |
339 |
Gyroscopic Effect |
166 |
H
Helix Angle |
150 |
High-lift Devices |
202, 212 |
Humidity |
20 |
I
ICAO Standard Atmosphere (ISA) |
25, 81 |
Indicated Airspeed |
80, 81 |
Induced Drag |
91,98 |
|
103 |
Inertia |
14 |
Inertial Loads |
331 |
Inset Hinge |
270 |
Instrument Error in the ASI |
84 |
Interference Drag |
97 |
Internal Balance |
271 |
L
Laminar Flow Aerofoil |
77 |
Landing Flap |
211 |
Landing Gear Limiting Speeds |
341 |
Landing with Crosswind |
344 |
Lateral Axis |
225 |
Lateral Control |
255, 259 |
Lateral Stability |
233 |
Leading - Edge Slat |
216 |
Order: 6026
Customer: Oleg Ostapenko E-mail: ostapenko2002@yahoo.com
Customer: Oleg Ostapenko E-mail: ostapenko2002@yahoo.com
PRINCIPLES OF FLIGHT INDEX
Leading Edge |
74 |
Leading Edge High-lift Devices |
212 |
Leading Edge Slot |
214,301 |
Lift |
34,177 |
Lift - Dependent Drag |
91, 98 |
Lift - Drag Ratio |
119, 122 |
Lift Augmentation |
201 |
Lift Equation |
57 |
Limiting Speeds and Loads |
338 |
Limiting Speeds on the Airspeed Indicator |
342 |
Load Factor |
189, 325 |
Load Factor Limits |
329 |
Longitudinal Axis |
225 |
Longitudinal Control About The Lateral Axis (Pitch) |
258 |
Longitudinal Stability |
226 |
M
Manoeuvre Envelope |
338 |
Mass |
8,33 |
Mass Balancing |
274 |
Maximum Camber |
71, 74 |
Maximum Gross Weight |
137 |
Maximum Lift-drag Ratio |
123, 210 |
Maximum Thickness |
75 |
Mean Camber Line |
74 |
Mesosphere |
24 |
Minimum Drag Speed |
107 |
Moments |
9 |
Momentum |
8 |
N
Navigation Computer |
82 |
Negative Load Factors |
331 |
Newton’s 1st Law of Motion |
14 |
Newton’s 2nd Law of Motion |
14,145 |
Newton’s 3rd Law of Motion |
14 |
Newtonian Explanation of Lift |
39 |
Normal Axis |
225 |
P
Parasite Drag |
91, 92 |
Performance Criteria |
123 |
Pitot Tube |
80 |
Plain Flap |
205 |
Plane of Rotation |
147 |
Pressure Error |
84 |
Power |
13 |
Powered Flap System |
204 |
ID: 3658
Customer: Oleg Ostapenko E-mail: ostapenko2002@yahoo.com
Customer: Oleg Ostapenko E-mail: ostapenko2002@yahoo.com
PRINCIPLES OF FLIGHT INDEX
Pressure |
11 |
Pressure Gradient |
71 |
Principal Flight Forces |
177 |
Propellers |
146 |
Propeller Diameter |
156 |
Propeller Effciency |
155 |
Propeller Power |
154 |
Propeller Slip |
149 |
Propeller Slipstream |
193 |
Propeller Theory |
150 |
Propeller Torque Effect |
166 |
R
Rate of Change of Momentum |
145 |
Rectifed Airspeed |
82 |
Rectangular Wings |
304 |
Roll |
244 |
Rudder |
255 |
S
Scalar Quantities |
15 |
Secondary Effect of Aileron |
261 |
Secondary Effect of Rudder |
260 |
Separation Point |
71 |
Servo Tab |
274 |
Side Loads on the Undercarriage |
343 |
Signs of the Approaching Stall |
306 |
- Airframe Buffeting |
306 |
- Stall Warning |
310 |
Skid |
191 |
Skidding Turns |
190 |
Skin-Friction Drag |
70,92 |
Slip |
191 |
Slipping Turns |
190 |
Slipstream Effect |
165 |
Slotted Flap |
206 |
Speed Never To Exceed |
185 |
Spin, The |
310 |
- Spin Avoidance |
313 |
- Spin Recovery |
312 |
Spinner |
147 |
Split Flap |
205 |
Spring Bias Trimming System |
279 |
Stability |
223 |
- Dynamic Stability |
224 |
- Static Stability |
223 |
Stalling |
289 |
- Effect of Altitude on Stall Speed |
296 |
- Effect of Flaps on the Stall |
302 |
- Effect of Power, on the Stall |
303 |
Order: 6026
Customer: Oleg Ostapenko E-mail: ostapenko2002@yahoo.com
Customer: Oleg Ostapenko E-mail: ostapenko2002@yahoo.com
PRINCIPLES OF FLIGHT INDEX
- Effect of the Position of Centre of Gravity of the Stall |
301 |
- Effect of Weight on the Stall |
292 |
- Effect of Wing Plan Form on the Stall |
304 |
Stalling Angle of Attack |
289 |
Stall Strips |
300 |
Static Pressure |
12,22 |
Straight Flight Stalling Speed |
291 |
Streamlines |
45,95 |
Structural Integrity |
136, 321 |
Swept Back Wings |
238 |
Symmetrical Aerofoils |
75 |
T
Take-Off Flap |
210 |
Tail Fin |
241 |
Tapered Wings |
304 |
Temperature |
24 |
- Measurement of Temperature |
26 |
Thickness |
75,76 |
Thickness/chord Ratio |
75 |
Three Dimensional Airfow |
99 |
Thrust |
33, 143, |
|
177 |
Torque |
10,153 |
Total Drag |
106 |
Total Pressure |
50, 79 |
Total Reaction |
38 |
Trailing Edge Flaps |
203 |
Trailing Edge Vortices |
100 |
Trailing Edge Tabs |
272 |
Transition Point |
71 |
Trimming |
276 |
Troposphere |
24 |
True Airspeed |
78, 84 |
Turning Flight |
187 |
U |
|
Upwash |
37,52,99 |
Useful Load |
137 |
V |
|
Variable-Pitch Constant-Speed Propellers |
164 |
Variable Incidence Tailplane |
279 |
Vector Quantities |
15 |
Venturi Tube |
77 |
Vertical Stabiliser |
241 |
Viscosity |
9,69 |
VNE |
185 |
ID: 3658
Customer: Oleg Ostapenko E-mail: ostapenko2002@yahoo.com
Customer: Oleg Ostapenko E-mail: ostapenko2002@yahoo.com
PRINCIPLES OF FLIGHT INDEX
W
Washout |
105, 305 |
Water Vapour |
20 |
Weathercocking |
241 |
Weight |
8, 33, |
|
129, 177 |
Weight and Mass |
129 |
Winglets |
106 |
Wingtip Vortices |
100 |
Wing Contamination |
303 |
Wing Dihedral |
234 |
Wing Drop at the Stall |
309 |
Wing Position |
236 |
Y |
|
Yaw |
244 |
Order: 6026
Customer: Oleg Ostapenko E-mail: ostapenko2002@yahoo.com
Customer: Oleg Ostapenko E-mail: ostapenko2002@yahoo.com
PRINCIPLES OF FLIGHT INDEX
ID: 3658
Customer: Oleg Ostapenko E-mail: ostapenko2002@yahoo.com
Customer: Oleg Ostapenko E-mail: ostapenko2002@yahoo.com
AEROPLANE PERFORMANCE INDEX
INDEX
A
Absolute Ceiling |
403 |
Accelerate Stop Distance Available or ASDA |
361 |
Aircraft Configuration |
402 |
Aircraft Mass/Weight. |
364 |
Aircraft Weight |
400 |
Air Density |
365 |
-Airfeld Elevation |
365 |
-Air Pressure |
365 |
-Air Temperature |
365 |
-Humidity of the Air |
365 |
Altitude |
365, 402 |
Atmospheric Density |
402 |
C
Calculating Runway Slope |
372 |
-Runway Surface |
372 |
Clearway |
361 |
Climb |
389 |
- Aerodynamic Drag |
390 |
-Aircraft Confguration |
394 |
-Angle of Climb |
389 |
-Best Rate of Climb |
397 |
-Climb Performance |
404 |
-Density |
396 |
-Drag |
390 |
-Equilibrium |
389 |
-Flaps |
394 |
-Forces in the Climb |
392 |
-Gradient of Climb |
398 |
-Obstacle Clearance Performance |
389 |
-Parasite Drag |
395 |
-Performance Tables |
404 |
-Power Available |
399 |
-Power Required |
399 |
-Thrust |
389 |
-Total Drag Curve |
399 |
-Undercarriage |
394 |
-Weight Apparent Drag |
390 |
Cruise |
419 |
D
Descent |
431 |
-Angle Of Descent |
431 |
-Best Glide Performance |
433 |
-Flaps |
433 |
-Glide Angle |
432 |
-Rate Of Descent (Descent Endurance) |
435 |
-Speed |
433 |
-VMD |
433 |
Order: 6026
Customer: Oleg Ostapenko E-mail: ostapenko2002@yahoo.com
Customer: Oleg Ostapenko E-mail: ostapenko2002@yahoo.com
AEROPLANE PERFORMANCE INDEX
E
Emergency Distance Available (EMDA or EDA) |
361 |
Engine Failure After Take-Off |
375 |
En-Route |
419 |
-Aircraft Confguration |
424 |
-Cruise |
419 |
-Cruise Performance Graphs |
428 |
-Cruising Altitude |
419 |
-Density Altitude |
405 |
-Effects of Wind on Range |
427 |
-Endurance |
423 |
-Initial Descent |
419 |
-Lift-Weight Force Couple |
419 |
-Maximum Range |
424 |
-Minimum Drag |
424 |
-Power Available |
421 |
-Range |
423 |
-Speed for Maximum Range |
424 |
-Stabilator |
419 |
-Tailplane |
419 |
-Thrust-Drag Force Couple |
419 |
-Wind Speed And Direction |
424 |
G
Gross Performance Figures |
356 |
I
ICAO Standard Atmosphere (ISA) |
405 |
L
Landing |
443 |
-Air Density |
445 |
-Asphalt Surface |
449 |
-Down-Hill Slope |
448 |
-Grass Runways |
449 |
-Headwinds |
446 |
-Landing Distance |
443 |
-Landing Performance Data |
451 |
-Landing Screen Height |
443 |
-Maximum Braking |
453 |
-Obstacle Clearance Performance |
446 |
-Runway Slope |
448 |
-Runway Surface |
449 |
-Surface Snow or Slush |
449 |
-Tailwind Component |
446 |
-Undershoot |
447 |
-Uphill Slope |
448 |
-Vertical Descent Speed |
447 |
ID: 3658
Customer: Oleg Ostapenko E-mail: ostapenko2002@yahoo.com
Customer: Oleg Ostapenko E-mail: ostapenko2002@yahoo.com
AEROPLANE PERFORMANCE INDEX
-Vref |
443 |
-Vso |
443 |
-Wind Gradient |
447 |
-Wind, Speed And Direction |
446 |
Lift Force |
365 |
N
Net Performance Figures |
356 |
Net Thrust |
363 |
R
Runway Slope |
|
-Calculating Runway Slope |
372 |
S
Screen Height |
359 |
Service Ceiling |
403 |
Stopway |
360 |
Straight And Level |
420 |
T
Take-Off |
359 |
-Declared Distances |
361 |
-Initial Climb |
359 |
-Lift-Off |
359 |
-Take-Off Decision Point |
375 |
-Take-Off Distance |
359 |
-Take-Off Distance Available |
361 |
-Take-Off Distance Graphs And Tables |
375 |
-Take-Off Distance Required |
359, 367 |
-Take-Off Performance |
362 |
-Take-Off Roll |
359 |
-Take-Off Run Available (TORA) |
360 |
-Take-Off Run Required (TORR) |
359 |
-Take-Off Safety Speed |
359 |
Take-Off Performance |
|
-Accounting for Air Density Performance Calculations |
366 |
-Coeffcient of Lift |
363 |
-Engine Performance |
365 |
-Flap Setting |
373 |
-Indicated Take-Off Speed |
366 |
-Initial Climb Performance |
366 |
-Lift-Off |
363 |
-Propeller Thrust |
365 |
-Runway Slope |
371 |
-Tailwinds |
368 |
-Take-Off Performance Graphs |
373 |
-Take-Off Speed |
363 |
Threshold |
360 |
Thrust |
363, 419 |
Tyre Pressure |
375 |
Order: 6026
Customer: Oleg Ostapenko E-mail: ostapenko2002@yahoo.com
Customer: Oleg Ostapenko E-mail: ostapenko2002@yahoo.com
AEROPLANE PERFORMANCE INDEX
U
UK CAA Safety Sense Leaflet No 7 |
355 |
W
Weight |
419 |
Wind Speed and Direction |
396 |
Wind Strength and Direction |
367 |
-Calculating Crosswind Component |
370 |
-Calculating Headwind Component |
369 |
-Crosswinds |
369 |
-Headwinds |
367 |
-Tailwinds |
368 |
-Turbulence and Windshear |
370 |
Wing Contamination |
374 |