A320 Speed Book

Takeoff Speed Tables Instructions 1. Use only Optimum V2 takeoff speeds from the specific airport runway analysis page when utilizing Optimum V2 performance. 2. Use actual takeoff weight rounded DOWN to the nearest 1,000 kg. increment for takeoff speed determination.

Takeoff Speed Adjustments "3 1. Make V1A/R density altitude adjustments from the 0 graph located on each page using the temperature -j at which thrust will be set. Use the assumed tem.-, perature if making a reduced thrust takeoff (Flex f Thrust). D -j

2. Add 1 knot to all speeds when operating with Extended Forward C.G..

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3. V1 for takeoff is the lesser of the Speed Book V1 or the Performance Handbook MAX V1 for the appropriate runway condition and aircraft configuration.

3. Make speed adjustments as instructed on the Takeoff Speed Adjustments page.

A320-200 V2500-AI

MINIMUM SPEEDS

V1 VR V2

FLAPS 1 FLAPS 2 FLAPS 3 114 112 112 117 117 119 120

VMCG VMCA VMCA

! ' Maneuvering and Landing Speeds f ' 3 1. Use estimated landing weight rounded to the nearest j,! 5 1,000 kg. increment for V|s/Vref determination. 2. Add 2 knots to all speeds for Extended Fwd C.G.. 5 (forward of 25% MAC) •5 3. Minimum maneuvering speeds are based on a bank ") angle of 30° plus a 15° overshoot before ccmax at an 5 altitude of 10,000 feet and are equivalent to Vls as ~ displayed on the PFD. They may be applied up to FL200, but must be increased by 1 knot/2,000 feet 5 above 10,000. In smooth air at the appropriate 5 minimum maneuvering speed, amax will occur at I 1.41 g, which is the loading in a level, 45° bank turn.

Holding Speeds The Holding Speeds table provides the green dot speeds, which are between minimum fuel speed and minimum drag speed. These speeds are protected by at least a 1.3g buffet margin. High Altitude Buffet Boundaries The Buffet Boundaries tables provide the speeds at which the aircraft will experience high and low speed buffet at a 1,3 G-load. A 1.3 G-load is equivalent to a 39" bank angle in still air or straight and level flight in moderate turbulence.

A320-200

HOLDING SPEEDS ALL ENGINES OPERATING

ALTITUDE FL390 FL370 FL350 FL300 FL250 FL200 15,000 FT 10,000 FT 5,000 FT 1,500 FT

50 199 197 195 190 1«S 180 180 180 180 180

52 203 201 199 194 189 184 184 184 184 184

Gross Wei ght (1,000 kg.) 57 59 61 63 66 208 212 217 222 226 206 210 215 220 224 229 204 208 213 218 222 227 199 203 208 213 217 222 194 198 203 208 212 217 189 193 198 203 207 212 189 193 198 203 207 212 189 193 198 203 207 212 189 193 198 203 207 212 189 193 198 203 207 212 54

;D. HOLDING SPEEDS AREBASED ONTHEGREEN DOTSPE

68

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73

233 231 226 221 216 216 216 216 216

238 236 231 226 221 221 221 221 221

240 235 230 225 225 225 225 225

HIGH ALTITUDE

A320-200

D

LOW AND HIGH SPEED BUFFET BOUNDARIES 1.3 G-LOAD (39 degree BANK ANGLE) WEIGHT FL390 FL370 FL350 FL330 FL310

52,000 54,000 57,000 59,000 61,000 .660 - .820 .676 - .820 .692 - .820 .707 - .820 .720 - .818 MACH 201 -255 206 - 255 211 -255 216-255 221 -254 KIAS .624 - .820 .640 - .820 .655 - .820 .670 - .820 .685 - .820 198-267 203 - 267 209 - 267 214 - 267 219-287 .589 - .820 .605 - .820 .620 - .820 .634 - .820 .648 -.820 195 - 280 201-280 206 - 280 211 -280 216-280 .556 - .820 .571 - .820 .585 - .820 .600 - .820 .61 3 -.820 192-292 198 - 292 203-292 209-292 213-292 .524 -.820 .538 - .820 .553 - .820 .567 - .820 .580 - .820 189-306 195 - 306 200 - 306 205 - 306 210-306

HIGH ALTITUDE LOW AND HIGH SPEED BUFFET BOUNDARIES 1.3 G-LOAD (39 degree BANK ANGLE) WEIGHT FU390 FL.370

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FL350 FL330

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A320-200

73,000 70,000 68,000 66,000 63,000 MACH .735 -.811 .751 - .803 .776 - .783 KIAS 226 - 252 231 - 249 240 - 242 .699 - .820 .711 -.820 .724 - .816 .737 - .810 .752 - .803 224 - 267 228 - 267 233-266 237-263 243 - 261 .662 - .820 .675 - .820 .688 - .820 .701 - .820 .712 - .820 221 - 280 226-2BO 231 - 280 235 - 280 239 - 280 .626 - .820 .639 - .820 .652 - .820 .665 - .820 .677 - .820 218 - 292 223 - 292 228 - 292 233 - 292 237 - 292 .593 - .820 .606 - .820 .61 8 -.820 .630 - .820 .641 - .820 215-306 220 - 306 225-306 230 - 306 234 - 306

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A320-200 HIGH ALTITUDE LOW AND HIGH SPEED BUFFET BOUNDARIES

A320-200

1.3 G-LOAD (39 degree BANK ANGLE)

1.3 Q-LOAD (39 degree BANK ANGLE) WEIGHT FL290 FL280 FL270 FL260 FL250

52,000

54,000

57,000

59,000

.495 - .820

.508 - .820

.522 - .820

.535 - .820

186-319 .481 - .820 185-326 .467 - .820 183-333 .454 - .820 182-340 .441 - .820 180-347

191 - 319 .494 - .820 190-326 .480 - .820 189 - 333 .466 - .820 187-340 .453 - .820 186-347

197-319 .507 - .820 195-326 .493 - .820 194 - 333 .479 - .820 192-340 .465 - .820 191 - 347

202-319 .520 - .820 200 - 326 .505 - .820 199 - 333 .491 - .820 197-340 .478 - .820 196-347

HIGH ALTITUDE LOW AND HIGH SPEED BUFFET BOUNDARIES

61,000 .548 - .820

MACH 207-319 KIAS .532 - .820 205 - 326 .51 7 -.820 204 - 333 .503 - .820 202 - 340 .489 - .820 201 - 347

WEIGHT FL290 FL280 FL270 FU60 FL250~

73,OQ9I 70.000 68,000 63.000 .609 - .820 MACH .597 .820 SBS .820 561 -.820 ,573 - .820 231-319 KIAS 212-319 217 • 319 222-319 227 - 319 .592 - .820 .581 .820 ,569 .820 .557 .820 ,545 - .820 225 - 326 230 - 326 210 - 326 215 - 326 J20-326 .576 - .820 529 - .820 .541 - .820 .553 - .820 .565 - .820 228-333 223 - 333 219 333 214 333 J09 • 333 [.561 - .820 .515-.820 526 - .820 ,538 - .820 [.549 - .820 226-340 207 • 340 212 - 340 217-340 222 - 340 J.54S-.820 .534-.820 .501 -.820 .512 - .820 .523 - .820 220 - 347 225 - 347 215-347 210-347 206-347

Maneuvering and Landing Speeds - continued Before slowing to a maneuvering speed, determine if 1.4 g will provide sufficient margin. Moderate turbu-, lence will produce aircraft loading of 1.3 g, therefore, the maneuvering speeds would only be appropriate in turbulent conditions if little or no turning is required. Adding 15 knots to the maneuvering speeds will increase the buffet margin to approximately 1.6 g (52° bank). 4. Maneuvering speeds are equivalent to Vls for each flap setting. Therefore, maneuvering speeds can be used as V,8 for non-normal landing flap settings in emergency situations.

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