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