PERFORMANCE TABLESPHENOM 100

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DEMONSTRATED CROSSWIND

WIND AND ALTITUDE CONVERSION

PERFORMANCE TABLES

The maximum demonstrated crosswind component for operating is 17 kt. This maximum demonstrated value is not considered to be limiting.

2

0

10

20

30

40

50

60

70

80

−10

−20

−30

−40

−50

−60

−70

−80

0 10 20 30 40 50

0° 10° 20°30°

40°50°

60°

70°

80°

90°

100°

110°

120°

130°140°

150°160°

170°180°

WIND COMPONENT

REPORTED WINDSPEED

(CURVED LINES)

EFFE

CTI

VE H

EAD

WIN

DC

OM

PON

ENT

− kt

EFFE

CTI

VE T

AIL

WIN

DC

OM

PON

ENT

− kt

CROSSWINDCOMPONENT − kt

WIND DIRECTION RELATIVETO RUNWAY

(STRAIGHT LINES)

0

10

20

30

40

50

60

70

80

−10

−20

−30

−40

−50

−60

−70

−80

0 10 20 30 40 50

0° 10° 20°30°

4040°5050°

6060°

7070°

80°

90°

100100°

110110°

120120°

130°140140°

150150°160°

170°180°

WIND COMPONENT

REPORTED WINDSPEED

(CURVED LINES)

EFFE

CTI

VE H

EAD

WIN

DC

OM

PON

ENT

− kt

EFFE

CTI

VE T

AIL

WIN

DC

OM

PON

ENT

− kt

CROSSWINDCOMPONENT − kt

WIND DIRECTION RELATIVETO RUNWAY

(STRAIGHT LINES)

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PHENOM 100

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3

REJECTED TAKEOFF (RTO)

This table presents the stall speed values according to the airplanebank angle for the MTOW (10472 lb) with landing gear and flap up.

This table presents the stall speed values according to the airplanebank angle for the MLW (9766 lb) with landing gear down and landingflap 3 or FULL.

NOTE: For airplanes Pre-Mod. SB 500-27-0003 consider landingflap 2 instead of flap 3.

0° 15° 30° 45° 60°

100° 102° 108° 119° 141°

BANKANGLE

STALLSPEED(KIAS)

STALL SPEEDS (KIAS)

0° 15° 30° 45° 60°

81 82 87 96 115

77 79 83 92 109

BANKANGLE

FLAP 3

FLAPFULL

STALL SPEEDS (KIAS)

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PHENOM 100

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N1 FOR T/O MODEICE PROTECTION OFFAIRSPEED: 0 KIAS

Static Air Temperature (°C) PressureAltitude

(ft) -40 -35 -30 -25 -20 -15 -10 -5 0 -1000 78.3 79.1 80.0 80.8 81.6 82.4 83.2 84.0 84.8

0 79.5 80.3 81.2 82.0 82.9 83.7 84.5 85.4 86.2 1000 79.6 80.5 81.3 82.2 83.0 83.8 84.7 85.5 86.3 2000 79.7 80.6 81.4 82.3 83.1 84.0 84.8 85.6 86.4 3000 79.7 80.6 81.4 82.2 83.1 83.9 84.8 85.6 86.4 4000 79.9 80.7 81.6 82.4 83.3 84.1 85.0 85.8 86.6 5000 79.9 80.7 81.6 82.4 83.3 84.1 85.0 85.8 86.7 6000 80.0 80.8 81.7 82.5 83.4 84.2 85.1 85.9 86.8 7000 80.1 81.0 81.8 82.7 83.5 84.4 85.2 86.1 86.9 8000 80.3 81.2 82.0 82.9 83.7 84.6 85.4 86.3 87.1 9000 80.4 81.3 82.1 83.0 83.8 84.7 85.5 86.4 87.2

10000 80.6 81.5 82.3 83.2 84.0 84.9 85.7 86.6 87.4

Static Air Temperature (°C) PressureAltitude

(ft) 5 10 15 20 25 30 35 40 45 -1000 85.6 86.3 87.1 87.8 88.6 88.7 87.9 87.0 86.0

0 86.9 87.7 88.5 89.2 89.8 89.0 88.0 87.0 86.0 1000 87.1 87.8 88.6 89.4 89.8 88.8 87.8 86.8 85.8 2000 87.2 88.0 88.8 89.5 89.6 88.7 87.7 86.6 85.6 3000 87.3 88.0 88.8 89.6 89.4 88.4 87.3 86.3 - 4000 87.4 88.2 89.0 89.6 89.2 88.2 87.1 86.2 - 5000 87.5 88.3 89.1 89.7 88.9 87.9 86.8 85.8 - 6000 87.6 88.4 89.2 89.6 88.7 87.6 86.6 - - 7000 87.8 88.5 89.3 89.4 88.5 87.4 86.4 - - 8000 87.9 88.7 89.5 89.4 88.3 87.2 - - - 9000 88.1 88.9 89.7 89.2 88.1 86.9 - - -

10000 88.3 89.1 89.8 89.0 87.8 86.6 - - -

Static Air Tr Tr emperature (°C)PressureAltitude

(ft) -40 -35 -30 -25 -20 -15 -10 -5 0 -1000 78.3 79.1 80.0 80.8 81.6 82.4 83.2 84.0 84.8

0 79.5 80.3 81.2 82.0 82.9 83.7 84.5 85.4 86.2 1000 79.6 80.5 81.3 82.2 83.0 83.8 84.7 85.5 86.3 2000 79.7 80.6 81.4 82.3 83.1 84.0 84.8 85.6 86.4 3000 79.7 80.6 81.4 82.2 83.1 83.9 84.8 85.6 86.4 4000 79.9 80.7 81.6 82.4 83.3 84.1 85.0 85.8 86.6 5000 79.9 80.7 81.6 82.4 83.3 84.1 85.0 85.8 86.7 6000 80.0 80.8 81.7 82.5 83.4 84.2 85.1 85.9 86.8 7000 80.1 81.0 81.8 82.7 83.5 84.4 85.2 86.1 86.9 8000 80.3 81.2 82.0 82.9 83.7 84.6 85.4 86.3 87.1 9000 80.4 81.3 82.1 83.0 83.8 84.7 85.5 86.4 87.2

10000 80.6 81.5 82.3 83.2 84.0 84.9 85.7 86.6 87.4

Static Air Tr Tr emperature (°C)PressureAltitude

(ft) 5 10 15 20 25 30 35 40 45 -1000 85.6 86.3 87.1 87.8 88.6 88.7 87.9 87.0 86.0

0 86.9 87.7 88.5 89.2 89.8 89.0 88.0 87.0 86.0 1000 87.1 87.8 88.6 89.4 89.8 88.8 87.8 86.8 85.8 2000 87.2 88.0 88.8 89.5 89.6 88.7 87.7 86.6 85.6 3000 87.3 88.0 88.8 89.6 89.4 88.4 87.3 86.3 - 4000 87.4 88.2 89.0 89.6 89.2 88.2 87.1 86.2 - 5000 87.5 88.3 89.1 89.7 88.9 87.9 86.8 85.8 - 6000 87.6 88.4 89.2 89.6 88.7 87.6 86.6 - - 7000 87.8 88.5 89.3 89.4 88.5 87.4 86.4 - - 8000 87.9 88.7 89.5 89.4 88.3 87.2 - - - 9000 88.1 88.9 89.7 89.2 88.1 86.9 - - -

10000 88.3 89.1 89.8 89.0 87.8 86.6 - - -

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PHENOM 100

Altitude (ft) Weight(lb) 5000 10000 15000 20000 22000 24000 26000 28000

N1 % 71.5 73.8 76.3 78.2 79.4 81.1 82.6 83.9 FF LB/H/ENG 445 409 374 340 332 330 324 317 IAS KT 226 218 209 198 196 196 195 192

10400 TAS KT 243 252 262 268 274 283 290 297 Mach 0.373 0.395 0.418 0.437 0.449 0.468 0.484 0.500 BM G 3.27 3.27 3.27 2.88 2.78 2.74 2.67 2.58 SR NM/LB 0.273 0.308 0.350 0.395 0.412 0.429 0.448 0.468 N1 % 70.7 72.7 75.7 77.7 78.7 79.9 81.8 83.1 FF LB/H/ENG 435 397 367 334 324 316 315 308 IAS KT 222 214 208 197 194 191 192 189

10000 TAS KT 239 247 259 266 271 275 286 293 Mach 0.368 0.387 0.414 0.433 0.444 0.456 0.478 0.492 BM G 3.27 3.27 3.27 2.96 2.84 2.72 2.71 2.62 SR NM/LB 0.275 0.311 0.354 0.399 0.417 0.436 0.454 0.475 N1 % 69.8 72.0 75.1 77.1 78.1 79.3 80.6 82.1 FF LB/H/ENG 425 389 360 327 317 310 302 297 IAS KT 219 211 206 195 192 189 187 185

9600 TAS KT 236 244 257 264 268 273 279 287 Mach 0.362 0.382 0.410 0.430 0.440 0.452 0.466 0.482 BM G 3.27 3.27 3.27 3.04 2.91 2.80 2.70 2.63 SR NM/LB 0.277 0.314 0.357 0.404 0.423 0.441 0.461 0.482 N1 % 69.0 71.2 74.2 76.6 77.5 78.4 79.6 81.2 FF LB/H/ENG 416 380 351 321 310 301 292 288 IAS KT 216 208 203 194 190 186 183 182

9200 TAS KT 232 241 253 262 266 269 274 282 Mach 0.357 0.377 0.404 0.427 0.436 0.446 0.457 0.474 BM G 3.27 3.27 3.27 3.13 2.98 2.85 2.73 2.66 SR NM/LB 0.279 0.316 0.361 0.408 0.428 0.448 0.469 0.490

For ICE PROTECTION (WINGSTAB+ENG) ON Increase (%):

5.0 1N 5.4 FF 6.0 SAI 8.0 SAT 5.2 hcaM

Decrease (%): 7.3 RS

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Altitude (ftitude (ftitude (f ) Weight(lb) 5000 10000 15000 20000 22000 24000 26000 28000

N1 % 71.5 73.8 76.3 78.2 79.4 81.1 82.6 83.9 FF LB/H/ENG 445 409 374 340 332 330 324 317 IAS KT 226 218 209 198 196 196 195 192

10400 TAS KT 243 252 262 268 274 283 290 297 Mach 0.373 0.395 0.418 0.437 0.449 0.468 0.484 0.500 BM G 3.27 3.27 3.27 2.88 2.78 2.74 2.67 2.58 SR NM/LB 0.273 0.308 0.350 0.395 0.412 0.429 0.448 0.468

N1 % 70.7 72.7 75.7 77.7 78.7 79.9 81.8 83.1 FF LB/H/ENG 435 397 367 334 324 316 315 308 IAS KT 222 214 208 197 194 191 192 189

10000 TAS KT 239 247 259 266 271 275 286 293 Mach 0.368 0.387 0.414 0.433 0.444 0.456 0.478 0.492 BM G 3.27 3.27 3.27 2.96 2.84 2.72 2.71 2.62 SR NM/LB 0.275 0.311 0.354 0.399 0.417 0.436 0.454 0.475

N1 % 69.8 72.0 75.1 77.1 78.1 79.3 80.6 82.1 FF LB/H/ENG 425 389 360 327 317 310 302 297 IAS KT 219 211 206 195 192 189 187 185

9600 TAS KT 236 244 257 264 268 273 279 287 Mach 0.362 0.382 0.410 0.430 0.440 0.452 0.466 0.482 BM G 3.27 3.27 3.27 3.04 2.91 2.80 2.70 2.63 SR NM/LB 0.277 0.314 0.357 0.404 0.423 0.441 0.461 0.482

N1 % 69.0 71.2 74.2 76.6 77.5 78.4 79.6 81.2 FF LB/H/ENG 416 380 351 321 310 301 292 288 IAS KT 216 208 203 194 190 186 183 182

9200 TAS KT 232 241 253 262 266 269 274 282 Mach 0.357 0.377 0.404 0.427 0.436 0.446 0.457 0.474 BM G 3.27 3.27 3.27 3.13 2.98 2.85 2.73 2.66 SR NM/LB 0.279 0.316 0.361 0.408 0.428 0.448 0.469 0.490

For ICE PROTECTION (WINGSTAB+ENG) ONIncrease (%):

5.01N5.4FF6.0SAI8.0SAT5.2hcaM

Decrease (%):7.3RS

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PHENOM 100

ALTITUDE: 5000 TO 28000 FT CRUISE CONFIGURATION BLEED: OPEN/ISA CONDITION ICE PROTECTION (WINGSTAB+ENG) OFF

LONG RANGE CRUISE – ALL ENGINES OPERATING PHENOM 100 PW617F-E ENGINES

Altitude (ft) Weight(lb) 5000 10000 15000 20000 22000 24000 26000 28000

N1 % 68.2 70.4 73.5 76.2 76.9 77.8 78.8 80.1 FF LB/H/ENG 406 372 343 317 304 294 284 277 IAS KT 213 205 200 193 188 185 181 178

8800 TAS KT 229 238 250 262 264 267 270 276 Mach 0.352 0.372 0.399 0.426 0.433 0.442 0.451 0.464 BM G 3.27 3.27 3.27 3.25 3.08 2.93 2.78 2.68 SR NM/LB 0.281 0.319 0.364 0.413 0.433 0.454 0.475 0.498 N1 % 67.4 69.6 72.7 75.4 76.3 77.2 78.0 79.2 FF LB/H/ENG 398 364 335 309 298 288 277 269 IAS KT 210 202 197 191 187 183 179 175

8400 TAS KT 225 234 247 258 261 265 267 272 Mach 0.347 0.367 0.394 0.420 0.429 0.438 0.446 0.457 BM G 3.27 3.27 3.27 3.27 3.18 3.03 2.86 2.73 SR NM/LB 0.283 0.322 0.368 0.417 0.438 0.459 0.482 0.506 N1 % 66.6 68.5 71.8 74.6 75.6 76.6 77.5 78.5 FF LB/H/ENG 389 354 327 302 292 283 272 262 IAS KT 207 198 194 188 185 182 178 174

8000 TAS KT 222 230 243 255 259 263 266 269 Mach 0.342 0.360 0.388 0.415 0.425 0.435 0.443 0.453 BM G 3.27 3.27 3.27 3.27 3.27 3.14 2.97 2.83 SR NM/LB 0.286 0.325 0.371 0.422 0.443 0.465 0.489 0.513 N1 % 65.8 67.5 71.0 73.8 75.0 76.0 76.8 77.8 FF LB/H/ENG 380 344 319 295 286 277 266 256 IAS KT 204 195 192 186 183 180 176 172

7600 TAS KT 219 225 240 252 257 261 264 266 Mach 0.337 0.353 0.383 0.410 0.421 0.432 0.440 0.448 BM G 3.27 3.27 3.27 3.27 3.27 3.26 3.08 2.92 SR NM/LB 0.288 0.328 0.375 0.427 0.448 0.471 0.495 0.521

For ICE PROTECTION (WINGSTAB+ENG) ON Increase (%):

6.0 1N 6.4 FF 6.0 SAI 8.0 SAT 4.2 hcaM

Decrease (%): 7.3 RS

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Altitude (ftitude (ftitude (f ) Weight(lb) 5000 10000 15000 20000 22000 24000 26000 28000

N1 % 68.2 70.4 73.5 76.2 76.9 77.8 78.8 80.1 FF LB/H/ENG 406 372 343 317 304 294 284 277 IAS KT 213 205 200 193 188 185 181 178

8800 TAS KT 229 238 250 262 264 267 270 276 Mach 0.352 0.372 0.399 0.426 0.433 0.442 0.451 0.464 BM G 3.27 3.27 3.27 3.25 3.08 2.93 2.78 2.68 SR NM/LB 0.281 0.319 0.364 0.413 0.433 0.454 0.475 0.498

N1 % 67.4 69.6 72.7 75.4 76.3 77.2 78.0 79.2 FF LB/H/ENG 398 364 335 309 298 288 277 269 IAS KT 210 202 197 191 187 183 179 175

8400 TAS KT 225 234 247 258 261 265 267 272 Mach 0.347 0.367 0.394 0.420 0.429 0.438 0.446 0.457 BM G 3.27 3.27 3.27 3.27 3.18 3.03 2.86 2.73 SR NM/LB 0.283 0.322 0.368 0.417 0.438 0.459 0.482 0.506

N1 % 66.6 68.5 71.8 74.6 75.6 76.6 77.5 78.5 FF LB/H/ENG 389 354 327 302 292 283 272 262 IAS KT 207 198 194 188 185 182 178 174

8000 TAS KT 222 230 243 255 259 263 266 269 Mach 0.342 0.360 0.388 0.415 0.425 0.435 0.443 0.453 BM G 3.27 3.27 3.27 3.27 3.27 3.14 2.97 2.83 SR NM/LB 0.286 0.325 0.371 0.422 0.443 0.465 0.489 0.513

N1 % 65.8 67.5 71.0 73.8 75.0 76.0 76.8 77.8 FF LB/H/ENG 380 344 319 295 286 277 266 256 IAS KT 204 195 192 186 183 180 176 172

7600 TAS KT 219 225 240 252 257 261 264 266 Mach 0.337 0.353 0.383 0.410 0.421 0.432 0.440 0.448 BM G 3.27 3.27 3.27 3.27 3.27 3.26 3.08 2.92 SR NM/LB 0.288 0.328 0.375 0.427 0.448 0.471 0.495 0.521

For ICE PROTECTION (WINGSTAB+ENG) ONIncrease (%):

6.01N6.4FF6.0SAI8.0SAT4.2hcaM

Decrease (%):7.3RS

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PHENOM 100

ALTITUDE: 5000 TO 28000 FT CRUISE CONFIGURATION BLEED: OPEN/ISA CONDITION ICE PROTECTION (W INGSTAB+ENG) OFF

LONG RANGE CRUISE – ALL ENGINES OPERATING PHENOM 100 PW617F-E ENGINES

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PHENOM 100

ALTITUDE: 30000 TO 41000 FT CRUISE CONFIGURATION BLEED: OPEN/ISA CONDITION ICE PROTECTION (W INGSTAB+ENG) OFF

LONG RANGE CRUISE – ALL ENGINES OPERATING PHENOM 100 PW617F-E ENGINES

Altitude (ft) Weight(lb) 30000 32000 34000 36000 38000 40000 41000

N1 % 85.2 86.6 88.0 89.0 91.1 92.0 - FF LB/H/ENG 310 307 302 296 297 279 - IAS KT 190 189 187 184 182 170 -

10400 TAS KT 303 312 320 326 338 332 - Mach 0.515 0.534 0.553 0.568 0.590 0.578 - BM G 2.46 2.35 2.24 2.10 2.00 1.77 - SR NM/LB 0.489 0.509 0.529 0.551 0.570 0.594 - N1 % 84.6 85.9 87.3 88.4 90.3 92.0 91.6 FF LB/H/ENG 303 298 294 288 286 280 260 IAS KT 188 186 185 182 179 174 160

10000 TAS KT 301 308 316 323 333 338 321 Mach 0.510 0.527 0.546 0.563 0.580 0.589 0.559 BM G 2.52 2.40 2.29 2.16 2.04 1.89 1.69 SR NM/LB 0.496 0.517 0.539 0.561 0.582 0.603 0.616 N1 % 83.8 85.1 86.4 87.8 89.7 91.6 91.6 FF LB/H/ENG 294 288 284 281 279 276 262 IAS KT 185 183 182 180 177 174 165

9600 TAS KT 297 303 312 320 330 338 329 Mach 0.503 0.519 0.538 0.558 0.576 0.590 0.574 BM G 2.58 2.45 2.34 2.23 2.10 1.97 1.81 SR NM/LB 0.504 0.526 0.548 0.571 0.592 0.613 0.628 N1 % 82.9 84.2 85.5 87.0 88.8 90.8 91.6 FF LB/H/ENG 285 279 274 271 269 267 263 IAS KT 182 180 178 177 174 171 168

9200 TAS KT 291 298 306 316 324 334 336 Mach 0.494 0.510 0.528 0.550 0.566 0.582 0.585 BM G 2.62 2.50 2.39 2.28 2.15 2.02 1.94 SR NM/LB 0.512 0.535 0.558 0.581 0.604 0.626 0.638

For ICE PROTECTION (WINGSTAB+ENG) ON Increase (%):

3.0 1N 9.3 FF

0 SAI 4.0 SAT 0.2 hcaM

Decrease (%): 6.3 RS

ICE PROTECTION (W INGSTAB+ENG) OFF

Altitude (ftitude (ftitude (f ) Weight(lb) 30000 32000 34000 36000 38000 40000 41000

N1 % 85.2 86.6 88.0 89.0 91.1 92.0 - FF LB/H/ENG 310 307 302 296 297 279 - IAS KT 190 189 187 184 182 170 -

10400 TAS KT 303 312 320 326 338 332 - Mach 0.515 0.534 0.553 0.568 0.590 0.578 - BM G 2.46 2.35 2.24 2.10 2.00 1.77 - SR NM/LB 0.489 0.509 0.529 0.551 0.570 0.594 -

N1 % 84.6 85.9 87.3 88.4 90.3 92.0 91.6 FF LB/H/ENG 303 298 294 288 286 280 260 IAS KT 188 186 185 182 179 174 160

10000 TAS KT 301 308 316 323 333 338 321 Mach 0.510 0.527 0.546 0.563 0.580 0.589 0.559 BM G 2.52 2.40 2.29 2.16 2.04 1.89 1.69 SR NM/LB 0.496 0.517 0.539 0.561 0.582 0.603 0.616

N1 % 83.8 85.1 86.4 87.8 89.7 91.6 91.6 FF LB/H/ENG 294 288 284 281 279 276 262 IAS KT 185 183 182 180 177 174 165

9600 TAS KT 297 303 312 320 330 338 329 Mach 0.503 0.519 0.538 0.558 0.576 0.590 0.574 BM G 2.58 2.45 2.34 2.23 2.10 1.97 1.81 SR NM/LB 0.504 0.526 0.548 0.571 0.592 0.613 0.628

N1 % 82.9 84.2 85.5 87.0 88.8 90.8 91.6 FF LB/H/ENG 285 279 274 271 269 267 263 IAS KT 182 180 178 177 174 171 168

9200 TAS KT 291 298 306 316 324 334 336 Mach 0.494 0.510 0.528 0.550 0.566 0.582 0.585 BM G 2.62 2.50 2.39 2.28 2.15 2.02 1.94 SR NM/LB 0.512 0.535 0.558 0.581 0.604 0.626 0.638

For ICE PROTECTION (WINGSTAB+ENG) ONIncrease (%):

3.01N9.3FF

0SAI4.0SAT0.2hcaM

Decrease (%):6.3RS

Altitude (ft) Weight(lb) 30000 32000 34000 36000 38000 40000 41000

N1 % 81.7 83.2 84.7 86.1 88.1 90.0 91.0 FF LB/H/ENG 273 269 266 262 260 257 256 IAS KT 177 176 175 174 172 169 167

8800 TAS KT 284 292 302 311 320 329 333 Mach 0.483 0.501 0.521 0.541 0.558 0.573 0.581 BM G 2.62 2.55 2.45 2.34 2.21 2.07 2.01 SR NM/LB 0.520 0.544 0.567 0.592 0.615 0.639 0.651 N1 % 80.7 82.2 83.8 85.2 87.4 89.1 90.2 FF LB/H/ENG 264 259 257 254 253 248 248 IAS KT 174 173 172 172 170 166 165

8400 TAS KT 279 287 297 306 317 324 329 Mach 0.473 0.491 0.512 0.533 0.553 0.564 0.574 BM G 2.65 2.59 2.51 2.40 2.29 2.13 2.07 SR NM/LB 0.529 0.554 0.577 0.603 0.627 0.653 0.664 N1 % 79.6 81.2 82.6 84.3 86.5 88.4 89.3 FF LB/H/ENG 254 250 246 245 245 241 239 IAS KT 170 169 168 168 168 164 162

8000 TAS KT 273 281 289 301 313 321 324 Mach 0.464 0.482 0.500 0.524 0.546 0.559 0.565 BM G 2.69 2.62 2.55 2.47 2.36 2.21 2.13 SR NM/LB 0.538 0.564 0.589 0.614 0.639 0.666 0.679 N1 % 78.5 80.0 81.2 83.1 85.6 87.6 88.5 FF LB/H/ENG 244 239 233 234 236 233 231 IAS KT 166 165 162 164 165 162 160

7600 TAS KT 267 275 280 294 307 317 320 Mach 0.454 0.470 0.484 0.512 0.536 0.552 0.558 BM G 2.73 2.65 2.53 2.52 2.43 2.29 2.22 SR NM/LB 0.548 0.575 0.602 0.626 0.651 0.679 0.693

For ICE PROTECTION (WINGSTAB+ENG) ON Increase (%):

3.0 1N 8.3 FF 7.0 SAI 4.0 SAT

0 hcaMDecrease (%):

5.3 RS

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PHENOM 100

ALTITUDE: 30000 TO 41000 FT CRUISE CONFIGURATION BLEED: OPEN/ISA CONDITION ICE PROTECTION (W INGSTAB+ENG) OFF

LONG RANGE CRUISE – ALL ENGINES OPERATING PHENOM 100 PW617F-E ENGINES

Altitude (ftitude (ftitude (f ) Weight(lb) 30000 32000 34000 36000 38000 40000 41000

N1 % 81.7 83.2 84.7 86.1 88.1 90.0 91.0 FF LB/H/ENG 273 269 266 262 260 257 256 IAS KT 177 176 175 174 172 169 167

8800 TAS KT 284 292 302 311 320 329 333 Mach 0.483 0.501 0.521 0.541 0.558 0.573 0.581 BM G 2.62 2.55 2.45 2.34 2.21 2.07 2.01 SR NM/LB 0.520 0.544 0.567 0.592 0.615 0.639 0.651

N1 % 80.7 82.2 83.8 85.2 87.4 89.1 90.2 FF LB/H/ENG 264 259 257 254 253 248 248 IAS KT 174 173 172 172 170 166 165

8400 TAS KT 279 287 297 306 317 324 329 Mach 0.473 0.491 0.512 0.533 0.553 0.564 0.574 BM G 2.65 2.59 2.51 2.40 2.29 2.13 2.07 SR NM/LB 0.529 0.554 0.577 0.603 0.627 0.653 0.664

N1 % 79.6 81.2 82.6 84.3 86.5 88.4 89.3 FF LB/H/ENG 254 250 246 245 245 241 239 IAS KT 170 169 168 168 168 164 162

8000 TAS KT 273 281 289 301 313 321 324 Mach 0.464 0.482 0.500 0.524 0.546 0.559 0.565 BM G 2.69 2.62 2.55 2.47 2.36 2.21 2.13 SR NM/LB 0.538 0.564 0.589 0.614 0.639 0.666 0.679

N1 % 78.5 80.0 81.2 83.1 85.6 87.6 88.5 FF LB/H/ENG 244 239 233 234 236 233 231 IAS KT 166 165 162 164 165 162 160

7600 TAS KT 267 275 280 294 307 317 320 Mach 0.454 0.470 0.484 0.512 0.536 0.552 0.558 BM G 2.73 2.65 2.53 2.52 2.43 2.29 2.22 SR NM/LB 0.548 0.575 0.602 0.626 0.651 0.679 0.693

For ICE PROTECTION (WINGSTAB+ENG) ONIncrease (%):

3.01N8.3FF7.0SAI4.0SAT

0hcaMDecrease (%):

5.3RS

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PHENOM 100

ALTITUDE: 5000 TO 28000 FT CRUISE CONFIGURATION BLEED: OPEN/ISA CONDITION

MAXIMUM SPEED CRUISE – ALL ENGINES OPERATING PHENOM 100 PW617F-E ENGINES

Altitude (ft) Weight(lb) 5000 10000 15000 20000 22000 24000 26000 28000

N1 % 80.0 83.4 87.1 91.1 92.4 93.1 93.7 94.2 FF LB/H/ENG 580 565 553 554 553 537 517 496 IAS KT 275 275 275 275 274 269 263 256

10400 TAS KT 295 317 341 368 379 384 387 389 Mach 0.454 0.497 0.545 0.599 0.621 0.635 0.645 0.655 BM G 3.27 3.27 3.27 3.27 3.27 3.27 3.27 3.27 SR NM/LB 0.254 0.281 0.309 0.332 0.342 0.357 0.374 0.393 N1 % 79.8 83.2 87.0 90.9 92.4 93.1 93.7 94.2 FF LB/H/ENG 577 562 550 551 553 538 517 496 IAS KT 275 275 275 275 275 270 263 256

10000 TAS KT 295 317 341 368 379 385 388 391 Mach 0.454 0.497 0.545 0.599 0.622 0.637 0.647 0.657 BM G 3.27 3.27 3.27 3.27 3.27 3.27 3.27 3.27 SR NM/LB 0.255 0.282 0.310 0.334 0.343 0.358 0.375 0.394 N1 % 79.6 83.0 86.8 90.8 92.2 93.1 93.6 94.2 FF LB/H/ENG 574 559 547 548 549 538 517 496 IAS KT 275 275 275 275 275 271 264 257

9600 TAS KT 295 317 341 368 379 386 389 392 Mach 0.454 0.497 0.545 0.599 0.622 0.639 0.649 0.659 BM G 3.27 3.27 3.27 3.27 3.27 3.27 3.27 3.27 SR NM/LB 0.257 0.284 0.312 0.336 0.345 0.359 0.376 0.395 N1 % 79.4 82.9 86.6 90.6 92.1 93.1 93.6 94.2 FF LB/H/ENG 571 556 543 545 545 539 518 496 IAS KT 275 275 275 275 275 272 265 258

9200 TAS KT 295 317 341 368 379 387 390 393 Mach 0.454 0.497 0.545 0.599 0.622 0.641 0.651 0.661 BM G 3.27 3.27 3.27 3.27 3.27 3.27 3.27 3.27 SR NM/LB 0.258 0.285 0.314 0.338 0.348 0.360 0.377 0.396

For ICE PROTECTION (WINGSTAB+ENG) ON Increase (%):

2.0 1N 5.3 FF

Decrease (%): 6.3 RS

Altitude (ftitude (ftitude (f ) Weight(lb) 5000 10000 15000 20000 22000 24000 26000 28000

N1 % 80.0 83.4 87.1 91.1 92.4 93.1 93.7 94.2 FF LB/H/ENG 580 565 553 554 553 537 517 496 IAS KT 275 275 275 275 274 269 263 256

10400 TAS KT 295 317 341 368 379 384 387 389 Mach 0.454 0.497 0.545 0.599 0.621 0.635 0.645 0.655 BM G 3.27 3.27 3.27 3.27 3.27 3.27 3.27 3.27 SR NM/LB 0.254 0.281 0.309 0.332 0.342 0.357 0.374 0.393

N1 % 79.8 83.2 87.0 90.9 92.4 93.1 93.7 94.2 FF LB/H/ENG 577 562 550 551 553 538 517 496 IAS KT 275 275 275 275 275 270 263 256

10000 TAS KT 295 317 341 368 379 385 388 391 Mach 0.454 0.497 0.545 0.599 0.622 0.637 0.647 0.657 BM G 3.27 3.27 3.27 3.27 3.27 3.27 3.27 3.27 SR NM/LB 0.255 0.282 0.310 0.334 0.343 0.358 0.375 0.394

N1 % 79.6 83.0 86.8 90.8 92.2 93.1 93.6 94.2 FF LB/H/ENG 574 559 547 548 549 538 517 496 IAS KT 275 275 275 275 275 271 264 257

9600 TAS KT 295 317 341 368 379 386 389 392 Mach 0.454 0.497 0.545 0.599 0.622 0.639 0.649 0.659 BM G 3.27 3.27 3.27 3.27 3.27 3.27 3.27 3.27 SR NM/LB 0.257 0.284 0.312 0.336 0.345 0.359 0.376 0.395

N1 % 79.4 82.9 86.6 90.6 92.1 93.1 93.6 94.2 FF LB/H/ENG 571 556 543 545 545 539 518 496 IAS KT 275 275 275 275 275 272 265 258

9200 TAS KT 295 317 341 368 379 387 390 393 Mach 0.454 0.497 0.545 0.599 0.622 0.641 0.651 0.661 BM G 3.27 3.27 3.27 3.27 3.27 3.27 3.27 3.27 SR NM/LB 0.258 0.285 0.314 0.338 0.348 0.360 0.377 0.396

For ICE PROTECTION (WINGSTAB+ENG) ONIncrease (%):

2.01N5.3FF

Decrease (%):6.3RS

Altitude (ft) Weight(lb) 5000 10000 15000 20000 22000 24000 26000 28000

N1 % 79.3 82.7 86.4 90.4 91.9 93.1 93.6 94.2 FF LB/H/ENG 568 553 540 541 542 539 518 497 IAS KT 275 275 275 275 275 273 266 259

8800 TAS KT 295 317 341 368 379 389 391 394 Mach 0.454 0.497 0.545 0.599 0.622 0.643 0.653 0.663 BM G 3.27 3.27 3.27 3.27 3.27 3.27 3.27 3.27 SR NM/LB 0.260 0.287 0.316 0.340 0.350 0.361 0.378 0.397 N1 % 79.1 82.5 86.2 90.2 91.7 93.1 93.6 94.2 FF LB/H/ENG 564 549 537 538 538 539 518 497 IAS KT 275 275 275 275 275 274 267 260

8400 TAS KT 295 317 341 368 379 390 393 395 Mach 0.454 0.497 0.545 0.599 0.622 0.646 0.655 0.665 BM G 3.27 3.27 3.27 3.27 3.27 3.27 3.27 3.27 SR NM/LB 0.261 0.288 0.318 0.342 0.352 0.362 0.379 0.398 N1 % 78.9 82.4 86.1 90.0 91.5 93.0 93.6 94.2 FF LB/H/ENG 561 546 533 534 535 538 518 497 IAS KT 275 275 275 275 275 275 268 261

8000 TAS KT 295 317 341 368 379 391 394 397 Mach 0.454 0.497 0.545 0.599 0.622 0.647 0.658 0.668 BM G 3.27 3.27 3.27 3.27 3.27 3.27 3.27 3.27 SR NM/LB 0.263 0.290 0.320 0.344 0.355 0.364 0.380 0.399 N1 % 78.7 82.2 85.9 89.9 91.3 92.8 93.6 94.2 FF LB/H/ENG 558 543 530 531 531 534 519 498 IAS KT 275 275 275 275 275 275 269 262

7600 TAS KT 295 317 341 368 379 391 396 399 Mach 0.454 0.497 0.545 0.599 0.622 0.647 0.660 0.671 BM G 3.27 3.27 3.27 3.27 3.27 3.27 3.27 3.27 SR NM/LB 0.264 0.292 0.322 0.347 0.357 0.366 0.381 0.400

For ICE PROTECTION (WINGSTAB+ENG) ON Increase (%):

2.0 1N 5.3 FF

Decrease (%): 5.3 RS

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PHENOM 100

ALTITUDE: 5000 TO 28000 FT CRUISE CONFIGURATION BLEED: OPEN/ISA CONDITION

MAXIMUM SPEED CRUISE – ALL ENGINES OPERATING PHENOM 100 PW617F-E ENGINES

Altitude (ftitude (ftitude (f ) Weight(lb) 5000 10000 15000 20000 22000 24000 26000 28000

N1 % 79.3 82.7 86.4 90.4 91.9 93.1 93.6 94.2 FF LB/H/ENG 568 553 540 541 542 539 518 497 IAS KT 275 275 275 275 275 273 266 259

8800 TAS KT 295 317 341 368 379 389 391 394 Mach 0.454 0.497 0.545 0.599 0.622 0.643 0.653 0.663 BM G 3.27 3.27 3.27 3.27 3.27 3.27 3.27 3.27 SR NM/LB 0.260 0.287 0.316 0.340 0.350 0.361 0.378 0.397

N1 % 79.1 82.5 86.2 90.2 91.7 93.1 93.6 94.2 FF LB/H/ENG 564 549 537 538 538 539 518 497 IAS KT 275 275 275 275 275 274 267 260

8400 TAS KT 295 317 341 368 379 390 393 395 Mach 0.454 0.497 0.545 0.599 0.622 0.646 0.655 0.665 BM G 3.27 3.27 3.27 3.27 3.27 3.27 3.27 3.27 SR NM/LB 0.261 0.288 0.318 0.342 0.352 0.362 0.379 0.398

N1 % 78.9 82.4 86.1 90.0 91.5 93.0 93.6 94.2 FF LB/H/ENG 561 546 533 534 535 538 518 497 IAS KT 275 275 275 275 275 275 268 261

8000 TAS KT 295 317 341 368 379 391 394 397 Mach 0.454 0.497 0.545 0.599 0.622 0.647 0.658 0.668 BM G 3.27 3.27 3.27 3.27 3.27 3.27 3.27 3.27 SR NM/LB 0.263 0.290 0.320 0.344 0.355 0.364 0.380 0.399

N1 % 78.7 82.2 85.9 89.9 91.3 92.8 93.6 94.2 FF LB/H/ENG 558 543 530 531 531 534 519 498 IAS KT 275 275 275 275 275 275 269 262

7600 TAS KT 295 317 341 368 379 391 396 399 Mach 0.454 0.497 0.545 0.599 0.622 0.647 0.660 0.671 BM G 3.27 3.27 3.27 3.27 3.27 3.27 3.27 3.27 SR NM/LB 0.264 0.292 0.322 0.347 0.357 0.366 0.381 0.400

For ICE PROTECTION (WINGSTAB+ENG) ONIncrease (%):

2.01N5.3FF

Decrease (%):5.3RS

Altitude (ft) Weight(lb) 30000 32000 34000 36000 38000 40000 41000

N1 % 94.6 94.6 94.2 93.2 92.7 92.0 - FF LB/H/ENG 472 442 406 362 320 279 - IAS KT 248 238 226 210 192 170 -

10400 TAS KT 390 388 382 370 356 332 - Mach 0.662 0.664 0.660 0.646 0.620 0.578 - BM G 3.05 2.77 2.54 2.38 2.11 1.77 - SR NM/LB 0.413 0.439 0.470 0.511 0.556 0.594 - N1 % 94.6 94.6 94.2 93.2 92.6 92.0 91.6 FF LB/H/ENG 473 442 407 363 321 280 260 IAS KT 249 238 227 212 194 174 160

10000 TAS KT 392 389 384 373 359 338 321 Mach 0.665 0.666 0.663 0.650 0.625 0.589 0.559 BM G 3.15 2.86 2.62 2.47 2.22 1.89 1.69 SR NM/LB 0.414 0.440 0.472 0.513 0.559 0.603 0.616 N1 % 94.6 94.6 94.2 93.2 92.6 92.0 91.6 FF LB/H/ENG 474 442 407 364 321 281 262 IAS KT 250 239 228 213 196 177 165

9600 TAS KT 393 391 386 375 362 343 329 Mach 0.667 0.669 0.666 0.653 0.630 0.599 0.574 BM G 3.25 2.95 2.71 2.55 2.33 2.00 1.81 SR NM/LB 0.415 0.442 0.473 0.515 0.563 0.610 0.628 N1 % 94.7 94.6 94.2 93.2 92.6 92.0 91.6 FF LB/H/ENG 475 443 408 364 322 282 263 IAS KT 251 240 229 214 197 179 168

9200 TAS KT 395 392 387 377 364 348 336 Mach 0.670 0.672 0.669 0.657 0.635 0.607 0.585 BM G 3.27 3.06 2.81 2.64 2.45 2.12 1.94 SR NM/LB 0.416 0.443 0.475 0.517 0.566 0.616 0.638

For ICE PROTECTION (WINGSTAB+ENG) ON Increase (%):

0 1N 0 FF

Decrease (%): 0 RS

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PHENOM 100

ALTITUDE: 30000 TO 41000 FT CRUISE CONFIGURATION BLEED: OPEN/ISA CONDITION

MAXIMUM SPEED CRUISE – ALL ENGINES OPERATING PHENOM 100 PW617F-E ENGINES

Altitude (ftitude (ftitude (f ) Weight(lb) 30000 32000 34000 36000 38000 40000 41000

N1 % 94.6 94.6 94.2 93.2 92.7 92.0 - FF LB/H/ENG 472 442 406 362 320 279 - IAS KT 248 238 226 210 192 170 -

10400 TAS KT 390 388 382 370 356 332 - Mach 0.662 0.664 0.660 0.646 0.620 0.578 - BM G 3.05 2.77 2.54 2.38 2.11 1.77 - SR NM/LB 0.413 0.439 0.470 0.511 0.556 0.594 -

N1 % 94.6 94.6 94.2 93.2 92.6 92.0 91.6 FF LB/H/ENG 473 442 407 363 321 280 260 IAS KT 249 238 227 212 194 174 160

10000 TAS KT 392 389 384 373 359 338 321 Mach 0.665 0.666 0.663 0.650 0.625 0.589 0.559 BM G 3.15 2.86 2.62 2.47 2.22 1.89 1.69 SR NM/LB 0.414 0.440 0.472 0.513 0.559 0.603 0.616

N1 % 94.6 94.6 94.2 93.2 92.6 92.0 91.6 FF LB/H/ENG 474 442 407 364 321 281 262 IAS KT 250 239 228 213 196 177 165

9600 TAS KT 393 391 386 375 362 343 329 Mach 0.667 0.669 0.666 0.653 0.630 0.599 0.574 BM G 3.25 2.95 2.71 2.55 2.33 2.00 1.81 SR NM/LB 0.415 0.442 0.473 0.515 0.563 0.610 0.628

N1 % 94.7 94.6 94.2 93.2 92.6 92.0 91.6 FF LB/H/ENG 475 443 408 364 322 282 263 IAS KT 251 240 229 214 197 179 168

9200 TAS KT 395 392 387 377 364 348 336 Mach 0.670 0.672 0.669 0.657 0.635 0.607 0.585 BM G 3.27 3.06 2.81 2.64 2.45 2.12 1.94 SR NM/LB 0.416 0.443 0.475 0.517 0.566 0.616 0.638

For ICE PROTECTION (WINGSTAB+ENG) ONIncrease (%):

01N0FF

Decrease (%):0RS

Altitude (ft) Weight(lb) 30000 32000 34000 36000 38000 40000 41000

N1 % 94.7 94.6 94.2 93.2 92.6 92.0 91.6 FF LB/H/ENG 476 443 409 365 323 283 264 IAS KT 252 241 230 215 199 181 171

8800 TAS KT 396 394 389 379 367 351 341 Mach 0.672 0.674 0.672 0.660 0.640 0.613 0.594 BM G 3.27 3.17 2.91 2.73 2.57 2.24 2.06 SR NM/LB 0.416 0.444 0.476 0.519 0.569 0.621 0.645 N1 % 94.7 94.6 94.2 93.2 92.6 92.0 91.6 FF LB/H/ENG 477 444 409 365 323 284 265 IAS KT 253 242 231 217 200 183 173

8400 TAS KT 398 395 391 381 369 355 345 Mach 0.675 0.676 0.675 0.664 0.644 0.619 0.602 BM G 3.27 3.27 3.02 2.84 2.69 2.37 2.19 SR NM/LB 0.417 0.445 0.477 0.521 0.572 0.625 0.652 N1 % 94.7 94.5 94.2 93.2 92.6 92.0 91.5 FF LB/H/ENG 478 444 410 366 323 285 265 IAS KT 254 243 232 218 201 185 175

8000 TAS KT 399 396 392 383 371 358 349 Mach 0.677 0.678 0.677 0.667 0.647 0.624 0.608 BM G 3.27 3.27 3.14 2.95 2.81 2.51 2.33 SR NM/LB 0.418 0.446 0.479 0.523 0.574 0.629 0.657 N1 % 94.7 94.5 94.2 93.2 92.6 92.0 91.5 FF LB/H/ENG 479 445 410 366 324 285 266 IAS KT 255 244 233 219 202 186 177

7600 TAS KT 401 398 394 384 373 361 352 Mach 0.681 0.681 0.680 0.670 0.651 0.629 0.614 BM G 3.27 3.27 3.27 3.08 2.94 2.67 2.48 SR NM/LB 0.419 0.447 0.480 0.525 0.577 0.633 0.662

For ICE PROTECTION (WINGSTAB+ENG) ON Increase (%):

0 1N 0 FF

Decrease (%): 0 RS

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PHENOM 100

ALTITUDE: 30000 TO 41000 FT CRUISE CONFIGURATION BLEED: OPEN/ISA CONDITION

MAXIMUM SPEED CRUISE – ALL ENGINES OPERATING PHENOM 100 PW617F-E ENGINES

Altitude (ftitude (ftitude (f ) Weight(lb) 30000 32000 34000 36000 38000 40000 41000

N1 % 94.7 94.6 94.2 93.2 92.6 92.0 91.6 FF LB/H/ENG 476 443 409 365 323 283 264 IAS KT 252 241 230 215 199 181 171

8800 TAS KT 396 394 389 379 367 351 341 Mach 0.672 0.674 0.672 0.660 0.640 0.613 0.594 BM G 3.27 3.17 2.91 2.73 2.57 2.24 2.06 SR NM/LB 0.416 0.444 0.476 0.519 0.569 0.621 0.645

N1 % 94.7 94.6 94.2 93.2 92.6 92.0 91.6 FF LB/H/ENG 477 444 409 365 323 284 265 IAS KT 253 242 231 217 200 183 173

8400 TAS KT 398 395 391 381 369 355 345 Mach 0.675 0.676 0.675 0.664 0.644 0.619 0.602 BM G 3.27 3.27 3.02 2.84 2.69 2.37 2.19 SR NM/LB 0.417 0.445 0.477 0.521 0.572 0.625 0.652

N1 % 94.7 94.5 94.2 93.2 92.6 92.0 91.5 FF LB/H/ENG 478 444 410 366 323 285 265 IAS KT 254 243 232 218 201 185 175

8000 TAS KT 399 396 392 383 371 358 349 Mach 0.677 0.678 0.677 0.667 0.647 0.624 0.608 BM G 3.27 3.27 3.14 2.95 2.81 2.51 2.33 SR NM/LB 0.418 0.446 0.479 0.523 0.574 0.629 0.657

N1 % 94.7 94.5 94.2 93.2 92.6 92.0 91.5 FF LB/H/ENG 479 445 410 366 324 285 266 IAS KT 255 244 233 219 202 186 177

7600 TAS KT 401 398 394 384 373 361 352 Mach 0.681 0.681 0.680 0.670 0.651 0.629 0.614 BM G 3.27 3.27 3.27 3.08 2.94 2.67 2.48 SR NM/LB 0.419 0.447 0.480 0.525 0.577 0.633 0.662

For ICE PROTECTION (WINGSTAB+ENG) ONIncrease (%):

01N0FF

Decrease (%):0RS