A320 Speed Book

Takeoff Speed Tables Instructions1. Use only Optimum V2 takeoff speeds from the specific

airport runway analysis page when utilizing OptimumV2 performance.

2. Use actual takeoff weight rounded DOWN to thenearest 1,000 kg. increment for takeoff speed deter-mination.

3. Make speed adjustments as instructed on the TakeoffSpeed Adjustments page.

Takeoff Speed Adjustments"3 1. Make V1A/R density altitude adjustments from the0 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 (Flexf Thrust).D 2. Add 1 knot to all speeds when operating with Ex--j tended Forward C.G..

3. V1 for takeoff is the lesser of the Speed Book V1 ort the Performance Handbook MAX V1 for the appropri-I ate runway condition and aircraft configuration.

MINIMUM SPEEDSA320-200 V2500-AI

V1VRV2

FLAPS 1114119

FLAPS 2112117

FLAPS 3112117

120

VMCGVMCAVMCA

55

! ' Maneuvering and Landing Speedsf ' 3 1. Use estimated landing weight rounded to the nearestj,! 5 1,000 kg. increment for V|s/Vref determination.

2. Add 2 knots to all speeds for Extended Fwd C.G..(forward of 25% MAC)

3. Minimum maneuvering speeds are based on a bank") angle of 30 plus a 15 overshoot before ccmax at an5 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 feet5 above 10,000. In smooth air at the appropriate5 minimum maneuvering speed, amax will occur atI 1.41 g, which is the loading in a level, 45 bank turn.

Holding SpeedsThe Holding Speeds table provides the green dotspeeds, which are between minimum fuel speed andminimum drag speed. These speeds are protected by atleast a 1.3g buffet margin.

High Altitude Buffet BoundariesThe Buffet Boundaries tables provide the speeds atwhich the aircraft will experience high and low speedbuffet 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 moder-ate turbulence.

HOLDING SPEEDSALL ENGINES OPERATING

A320-200

ALTITUDEFL390FL370FL350FL300FL250FL20015,000 FT10,000 FT5,000 FT1,500 FT

HOLDING SP

Gross Wei501991971951901S180180180180180

EEDS

52203201199194189184184184184184

AREB

54208206204199194189189189189189

ASED

57212210208203198193193193193193

ONTH

59217215213208203198198198198198

EGRE

ght (1,000 kg.)61222220218213208203203203203203

EN DO

63226224222217212207207207207207

TSPE

66

229227222217212212212212212

;D.

68

233231226221216216216216216

/O

238236231226221221221221221

73

240235230225225225225225

HIGH ALTITUDELOW AND HIGH SPEED BUFFET BOUNDARIES1.3 G-LOAD (39 degree BANK ANGLE)

A320-200

DWEIGHTFL390

FL370

FL350

FL330

FL310

52,000.660 - .820201 -255.624 - .820198-267

.589 - .820195 - 280.556 - .820192-292

.524 -.820189-306

54,000.676 - .820206 - 255.640 - .820203 - 267.605 - .820201-280.571 - .820198 - 292

.538 - .820195 - 306

57,000.692 - .820211 -255

.655 - .820209 - 267.620 - .820206 - 280.585 - .820203-292.553 - .820200 - 306

59,000.707 - .820216-255

.670 - .820214 - 267

.634 - .820211 -280.600 - .820209-292

.567 - .820205 - 306

61,000.720 - .818221 -254

.685 - .820219-287.648 -.820216-280.61 3 -.820213-292.580 - .820210-306

MACHKIAS

.

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A320-200

WEIGHTFU390

FL.370

FL350

FL330

FU10

63,000.735 -.811226 - 252.699 - .820224 - 267.662 - .820221 - 280.626 - .820218 - 292.593 - .820215-306

66,000.751 - .803231 - 249.711 -.820228 - 267.675 - .820226-2BO.639 - .820223 - 292.606 - .820220 - 306

68,000.776 - .783240 - 242.724 - .816233-266.688 - .820231 - 280.652 - .820228 - 292.61 8 -.820225-306

70,000

.737 - .810237-263.701 - .820235 - 280.665 - .820233 - 292.630 - .820230 - 306

73,000

.752 - .803243 - 261.712 - .820239 - 280.677 - .820237 - 292.641 - .820234 - 306

MACH IKIAS |

HIGH ALTITUDELOW AND HIGH SPEED BUFFET BOUNDARIES1.3 Q-LOAD (39 degree BANK ANGLE)

A320-200

WEIGHTFL290

FL280

FL270

FL260

FL250

52,000.495 - .820186-319

.481 - .820185-326

.467 - .820183-333

.454 - .820182-340

.441 - .820180-347

54,000.508 - .820191 - 319

.494 - .820190-326

.480 - .820189 - 333

.466 - .820187-340

.453 - .820186-347

57,000.522 - .820197-319

.507 - .820195-326

.493 - .820194 - 333

.479 - .820192-340

.465 - .820191 - 347

59,000.535 - .820202-319

.520 - .820200 - 326

.505 - .820199 - 333

.491 - .820197-340

.478 - .820196-347

61,000.548 - .820207-319

.532 - .820205 - 326.51 7 -.820204 - 333

.503 - .820202 - 340.489 - .820201 - 347

MACHKIAS


A320-200

WEIGHTFL290

FL280

FL270

FU60

FL250~

63.000561 -.820212-319,545 - .820210 - 326529 - .820J09 333.515-.820207 340.501 -.820206-347

,573 - .820217 319.557 - .820215 - 326.541 - .820214 - 333526 - .820212 - 340.512 - .820210-347

68,000SBS - .820222-319,569 - .820J20-326.553 - .820219 - 333,538 - .820217-340.523 - .820215-347

70.000.597 - .820227 - 319.581 - .820225 - 326.565 - .820223 - 333

[.549 - .820222 - 340.534-.820220 - 347

73,OQ9I.609 - .820231-319.592 - .820230 - 326.576 - .820228-333

[.561 - .820226-340

J.54S-.820225 - 347

MACHKIAS

Maneuvering and Landing Speeds - continuedBefore slowing to a maneuvering speed, determine if1.4 g will provide sufficient margin. Moderate turbu-,lence will produce aircraft loading of 1.3 g, therefore,the maneuvering speeds would only be appropriatein turbulent conditions if little or no turning is re-quired. Adding 15 knots to the maneuvering speedswill increase the buffet margin to approximately 1.6 g(52 bank).

4. Maneuvering speeds are equivalent to Vls for eachflap setting. Therefore, maneuvering speeds can beused as V,8 for non-normal landing flap settings inemergency situations.

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A320 Speed Book

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