Airplane Flying Handbook

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Airplane Flying Handbook 2016 U.S. Department of Transportation FEDERAL AVIATION ADMINISTRATION Flight Standards Service
Page 4 and 5: ii
Page 6 and 7: iv
Page 8 and 9: vi
Page 10 and 11: Chapter 4 Maintaining Aircraft Cont
Page 12 and 13: Chapter 11 Transition to Complex Ai
Page 14 and 15: Basic Safety Concepts..............
Page 16 and 17: Pre-Solo Solo Maneuvers Cross-count
Page 18 and 19: eference since the parts are numeri
Page 20 and 21: in the United States and for Americ
Page 22 and 23: Lesson ________________________ Stu
Page 24 and 25: without further testing by the FAA.
Page 26 and 27: psychological and physiological con
Page 28 and 29: Figure 1-15. All student pilots mus
Page 30 and 31: 1-16
Page 32 and 33: Flying an airplane presents many ne
Page 34 and 35: Airplane Documents Original Airwort
Page 36 and 37: hangar rash incidents—dents and d
Page 38 and 39: and engine failure. During the pref
Page 40 and 41: maximize the flight’s successes.
Page 42 and 43: helicopters, and errant animals. Th
Page 44 and 45: • Pilot seat occupant, after maki
Page 46 and 47: esult in tire damage or an uncontro
Page 48 and 49: • Vacuum System—must show an ac
Page 50 and 51: 2-20
Page 52 and 53:
The Four Fundamentals To master any
Page 54 and 55:
Feel of the Airplane The ability to
Page 56 and 57:
30 30 6 6 NAV1 108.00 113.00 NAV2 1
Page 58 and 59:
Left wingtip Right wingtip NAV1 108
Page 60 and 61:
• Habitually flying with one wing
Page 62 and 63:
Level flight Steeply banked turn Ve
Page 64 and 65:
W 30 OBS W 30 24 OBS W NAV 30 S GS
Page 66 and 67:
e smoothly relaxed so that the cont
Page 68 and 69:
W W S S E E TAS 106KT OAT 7°C 2 1
Page 70 and 71:
obstacles during a landing approach
Page 72 and 73:
• The normal stability and inhere
Page 74 and 75:
3-24
Page 76 and 77:
To maintain aircraft control when f
Page 78 and 79:
Performing the Slow Flight Maneuver
Page 80 and 81:
• Vision—since the airplane can
Page 82 and 83:
throttle promptly, but smoothly, as
Page 84 and 85:
Power-On Stall and Recovery Slow to
Page 86 and 87:
to centerline by increasing the ban
Page 88 and 89:
udder use, the pilot may not be awa
Page 90 and 91:
Spin Recovery Template 1. Reduce th
Page 92 and 93:
an unusual attitude, but would not
Page 94 and 95:
for pilots to reduce surprise and i
Page 96 and 97:
Prevention through Proportional Cou
Page 98 and 99:
Spiral Dive Recovery Template 1. Re
Page 100 and 101:
Though it may seem relatively simpl
Page 102 and 103:
the rudder pedals so that the toes
Page 104 and 105:
speed that is higher or lower than
Page 106 and 107:
This “skipping” is usually indi
Page 108 and 109:
can be used to the pilot’s advant
Page 110 and 111:
Takeoff Roll As the airplane is ali
Page 112 and 113:
5-14
Page 114 and 115:
A pilot must develop the proper coo
Page 116 and 117:
Current Current No current, no drif
Page 118 and 119:
headed downwind, the turn bank angl
Page 120 and 121:
to prevent drifting in or out of th
Page 122 and 123:
• Failure to establish a constant
Page 124 and 125:
Steeper bank WIND Level with crab i
Page 126 and 127:
Wind Steeper bank Steepest bank Ste
Page 128 and 129:
airplane flies a prescribed path ov
Page 130 and 131:
Eights-on-pylons are performed at b
Page 132 and 133:
Airport Traffic Patterns and Operat
Page 134 and 135:
Traffic pattern indicators (indicat
Page 136 and 137:
such as doorposts and wings. High-w
Page 138 and 139:
Normal Approach and Landing A norma
Page 140 and 141:
flap setting, and one wind conditio
Page 142 and 143:
When the AOA is increased, the lift
Page 144 and 145:
Near zero rate of descent 15 feet 2
Page 146 and 147:
3° approach angle 400 feet x 100 f
Page 148 and 149:
ate of sideward movement, is determ
Page 150 and 151:
have the landing gear in the down-a
Page 152 and 153:
34 WIND Figure 8-17. Crosswind appr
Page 154 and 155:
Headwind Component 0° 70 60 50 40
Page 156 and 157:
34 Unstabilized Figure 8-23. Unstab
Page 158 and 159:
The use of brakes on a soft field i
Page 160 and 161:
45° Power reduced base leg speed C
Page 162 and 163:
ut full flaps are not used until es
Page 164 and 165:
1. Airspeed—70 KIAS (flaps UP) 65
Page 166 and 167:
Although back-elevator pressure may
Page 168 and 169:
does not bounce like a rubber ball.
Page 170 and 171:
Touchdown in a Drift or Crab At tim
Page 172 and 173:
Viscous Hydroplaning Viscous hydrop
Page 174 and 175:
Performance maneuvers also allow fo
Page 176 and 177:
• Ineffective use of power • In
Page 178 and 179:
complete or exceeds the 180° turn
Page 180 and 181:
its lowest pitch attitude. [Figure
Page 182 and 183:
For 14 CFR part 61 operations, the
Page 184 and 185:
electronic glide slope or visual ap
Page 186 and 187:
use is to always initially key the
Page 188 and 189:
Lighted runways, buildings, or othe
Page 190 and 191:
attempting night operations, pilots
Page 192 and 193:
Straight Elliptical Tapered Delta S
Page 194 and 195:
The time of flap extension and degr
Page 196 and 197:
the torque, or power, delivered to
Page 198 and 199:
pm and horsepower can steadily buil
Page 200 and 201:
When the waste gate is open, the tu
Page 202 and 203:
Landing gear indicator (top) illumi
Page 204 and 205:
Compressed Gas Hand Pump Hand Crank
Page 206 and 207:
This technique greatly reduces the
Page 208 and 209:
11-18
Page 210 and 211:
The modern, well-equipped multiengi
Page 212 and 213:
Change in Equivalent Parasite Drag
Page 214 and 215:
used in training, this saves much e
Page 216 and 217:
Anti-Icing/Deicing Anti-icing/deici
Page 218 and 219:
Takeoff planning factors include we
Page 220 and 221:
The payload is the maximum combinat
Page 222 and 223:
of an engine failure. Additional al
Page 224 and 225:
1 Downwind 1. Flaps-approach positi
Page 226 and 227:
field approach and landing procedur
Page 228 and 229:
Liftoff Engine failure Descend at V
Page 230 and 231:
Securing Failed Engine Mixture.....
Page 232 and 233:
TAS 106KT OAT 7°C 2 1 1 2 There ar
Page 234 and 235:
If a yaw string is attached to the
Page 236 and 237:
Spin Awareness No multiengine airpl
Page 238 and 239:
Figure 13-1. The Piper Super Cub on
Page 240 and 241:
After a brief period of acceleratio
Page 242 and 243:
the tail makes contact first. Provi
Page 244 and 245:
Soft-Field Landing The tailwheel sh
Page 246 and 247:
Gas Turbine Engine Both piston (rec
Page 248 and 249:
Planetary production gears Reverse-
Page 250 and 251:
Exhaust outlet Reduction gearbox Fu
Page 252 and 253:
Pull Up } Reverse Idle Beta Feather
Page 254 and 255:
Primary Inverter Left Main Bus Righ
Page 256 and 257:
Flight training should prepare the
Page 258 and 259:
14-14
Page 260 and 261:
Jet Engine Basics A jet engine is a
Page 262 and 263:
TAT +13c ---- 10 28.8 8 6 4 65 10 0
Page 264 and 265:
Slow Acceleration of the Jet Engine
Page 266 and 267:
POWER NAV1 108.00 117.95 Airspeed I
Page 268 and 269:
The AOA of the wing has the greates
Page 270 and 271:
A Jet Aircraft B Propeller-Driven A
Page 272 and 273:
1 Spanwise flow of boundary layer d
Page 274 and 275:
Target or Clamshell Reverser Cascad
Page 276 and 277:
airplane, power reduction must be m
Page 278 and 279:
In order to use the MEL properly, i
Page 280 and 281:
power, they should not be readjuste
Page 282 and 283:
primary deceleration force during a
Page 284 and 285:
• Approach climb—the speed that
Page 286 and 287:
1,000' window 500' window Threshold
Page 288 and 289:
stop must be made on the runway tha
Page 290 and 291:
15-32
Page 292 and 293:
Light Sport Airplane (LSA) Backgrou
Page 294 and 295:
atings. For example, a commercial p
Page 296 and 297:
finish. Generally, composite constr
Page 298 and 299:
limitations, systems, performance,
Page 300 and 301:
Figure 16-14. Split flap. Figure 16
Page 302 and 303:
flight in turbulence may couple mot
Page 304 and 305:
16-14
Page 306 and 307:
Emergency Landings This section con
Page 308 and 309:
can be accomplished in an effective
Page 310 and 311:
• If heavy tree trunk contact is
Page 312 and 313:
particular airplane. For the purpos
Page 314 and 315:
When experiencing a loss of up-elev
Page 316 and 317:
Electrical Loads for Light Single A
Page 318 and 319:
Malfunction Loss of rpm during crui
Page 320 and 321:
instruments while searching outside
Page 322 and 323:
encountered in individual maneuvers
Page 324 and 325:
Airplane Owner/Information Manual.
Page 326 and 327:
Cambered. The camber of an airfoil
Page 328 and 329:
Delamination. The separation of lay
Page 330 and 331:
Fuel control unit. The fuel-meterin
Page 332 and 333:
Induction manifold. The part of the
Page 334 and 335:
Moment. The product of the weight o
Page 336 and 337:
Reverse thrust. A condition where j
Page 338 and 339:
Standard atmosphere. At sea level,
Page 340 and 341:
Turbofan engine. A turbojet engine
Page 342 and 343:
V YSE . Best rate-of-climb speed wi
Page 344 and 345:
Fixed-pitch propellers.............
Page 346 and 347:
M Mach buffet boundaries...........
Page 348:
Flight school......................
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