# Embraer Temporary Revision 19.1: No revision named - Rights: © Embraer S.A. Filed by the FAA in regulations.gov docket FAA-2016-9049; AD 2017-04-12 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. - Document: [Embraer Temporary Revision 19.1](https://openairdocs.org/service-documents/embraer/tr-19-1.md) - Title as filed: AOM-135-1542-01 - Pages: 92 - PDF: https://openairdocs.org/files/sha256/b7/fb/b7fbd104f3bc1d62c33d34f7174023f175af2065e40f2a5c37d1034feda56190 - Page: https://openairdocs.org/service-documents/embraer/tr-19-1/file/b7fbd104f3bc ## Text Each page's text from the PDF; open the PDF at a page with #page=N. ### Page 1 TEMPORARY REVISION 19.1 Publication: AOM–135/1542-01 - Airplane Operations Manual. Dear Madam or Sir, You are receiving the Temporar y Revision 19.1 of the Airplane Operations Manual which includes the blocks 1-05-10 code 06; 1-05-15 code 06; 1-05-20 code 06 and 1-05-25 code 06. Temporary Revisions pages are printed in yellow paper. Please include new blocks and/or new pages into your manual as a normal revision. Revised pages should be included in your manual facing the current pages. They will be incorporated in the next AOM scheduled revision. The temporary revision will not be in cluded in the List of Effective Pages. In case of question, please contact: Embraer Executive Flight Operations Support E-mail: contact.center@embraer.com THIS PAGE IS NOT PART OF THE MANUAL AND MUST NOT BE INCORPORATED IN YOUR AOM. PLEASE DISCARD IT AFTER READING. ### Page 2 (No text on this page.) ### Page 3 In connection with the use of this document, Embraer does not provide any express or implied warranties and expressly disclaims any warranty of merchantability or fitness for a particular purpose. Copyright © 2001 by Embraer S.A.. All rights reserved. AIRPLANE OPERATIONS MANUAL VOLUME 1 EMBRAER S.A. This manual is applicable to the EMB-135BJ airplanes all models equipped with AE3007A1P, AE3007A1E and AE3007A2 engines and operating under ANAC, FAA and EASA certifications. NOTE: THE EMB-135BJ MODEL HAS THE COMMERCIAL DESIGNATION OF LEGACY 600 OR LEGACY 650. THIS PUBLICATION IS INCOMPLETE WITHOUT AIRPLANE OPERATIONS MANUAL AOM–135/1542 VOLUME 2 AOM–135/1542-01 NOVEMBER 30, 2001 TEMPORARY REVISION 19.1 – APRIL 22, 2014 ### Page 4 (No text on this page.) ### Page 5 AIRPLANE OPERATIONS MANUAL RECORD OF TEMPORARY REVISIONS TEMPORARY REVISION 19.1 RTR-1 AOM-135/1542 RECORD OF TEMPORARY REVISIONS AOM–135/1542-01 TR 19.1 .........................................................................APR 22, 2014 ### Page 6 RECORD OF TEMPORARY REVISIONS AIRPLANE OPERATIONS MANUAL RTR-2 TEMPORARY REVISION 19.1 AOM-135/1542 INTENTIONALLY BLANK ### Page 7 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-10 Page 1 Code 06 AOM-135/1542 CLIMB The climb planning tables show fuel consumption, distance, and time elapsed from the Sea Level to the top of climb. Data are shown for various weights, ISA deviations and cruise altitudes. Two climb schedules are presented: First set of tables presents the sc hedule climb speed according to the autopilot climb mode, i.e.: − 240 KIAS for altitudes up to 10 000 ft, increasing linearly to 290 KIAS at 12000 ft, maintaining 290 KIAS up to 21600 ft and 0.65 Mach above 21600 ft. Second set of tables presents the following climb speed schedule: − 240 KIAS for altitudes up to 10 000 ft, increasing linearly to 260 KIAS at 12000 ft, maintaining 260 KIAS up to 22800 ft and 0.60 Mach above 22800 ft. The associated conditions are: − Thrust Mode .........................CLB − Flaps.....................................UP − Gear .....................................UP − Bleeds ..................................OPEN − Anti-Ice .................................OFF ### Page 8 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-10 Page 2 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 5000 AND 6000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 290 KIAS AT 12000 FT, MAINTAINING 290 KIAS UP TO 21600 FT AND M = 0.65 ABOVE 21600 FT. AUTOPILOT CLIMB SCHEDULE BLEED: OPEN 5000 ft 6000 ft ISA + °C ISA + °C WEIGHT (lb) -20 -10 0 10 20 -20 -10 0 10 20 Fuel LB 161 168 175 184 211 194 202 211 222 254 50000 Distance NM 8 8 9 9 12 10 10 10 11 14 Time MIN 2 2 2 2 3 2 2 3 3 3 Fuel LB 153 159 166 174 199 184 191 200 210 240 48000 Distance NM 7 8 8 9 11 9 9 10 11 13 Time MIN 2 2 2 2 3 2 2 2 2 3 Fuel LB 144 150 157 165 187 173 181 189 198 226 46000 Distance NM 7 7 8 8 10 9 9 9 10 13 Time MIN 2 2 2 2 2 2 2 2 2 3 Fuel LB 136 142 148 156 176 164 171 178 187 212 44000 Distance NM 7 7 7 8 10 8 8 9 9 12 Time MIN 2 2 2 2 2 2 2 2 2 3 Fuel LB 128 134 140 147 165 154 161 168 176 199 42000 Distance NM 6 6 7 7 9 8 8 8 9 11 Time MIN 2 2 2 2 2 2 2 2 2 3 Fuel LB 121 126 131 138 155 145 151 158 166 187 40000 Distance NM 6 6 6 7 8 7 7 8 8 10 Time MIN 1 2 2 2 2 2 2 2 2 2 Fuel LB 114 118 123 130 146 137 142 148 156 175 38000 Distance NM 5 6 6 6 8 7 7 7 8 10 Time MIN 1 1 1 2 2 2 2 2 2 2 Fuel LB 107 111 116 121 136 128 133 139 146 164 36000 Distance NM 5 5 6 6 7 6 7 7 7 9 Time MIN 1 1 1 1 2 2 2 2 2 2 Fuel LB 100 104 108 114 127 120 125 130 136 153 34000 Distance NM 5 5 5 6 7 6 6 6 7 8 Time MIN 1 1 1 1 2 1 2 2 2 2 Fuel LB 93 97 101 106 118 112 116 121 127 142 32000 Distance NM 4 5 5 5 6 5 6 6 6 8 Time MIN 1 1 1 1 2 1 1 1 2 2 Fuel LB 86 90 94 98 110 104 108 113 118 132 30000 Distance NM 4 4 4 5 6 5 5 6 6 7 Time MIN 1 1 1 1 1 1 1 1 1 2 ### Page 9 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-10 Page 3 Code 06 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 7000 AND 8000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 290 KIAS AT 12000 FT, MAINTAINING 290 KIAS UP TO 21600 FT AND M = 0.65 ABOVE 21600 FT. AUTOPILOT CLIMB SCHEDULE BLEED: OPEN 7000 ft 8000 ft ISA + °C ISA + °C WEIGHT (lb) -20 -10 0 10 20 -20 -10 0 10 20 Fuel LB 227 237 247 260 298 260 271 283 298 343 50000 Distance NM 11 12 12 13 17 13 14 14 16 20 Time MIN 3 3 3 3 4 3 3 3 4 5 Fuel LB 215 224 233 246 281 246 256 267 282 323 48000 Distance NM 11 11 12 13 16 13 13 14 15 19 Time MIN 3 3 3 3 4 3 3 3 3 4 Fuel LB 203 211 220 232 264 232 242 253 266 304 46000 Distance NM 10 11 11 12 15 12 12 13 14 18 Time MIN 3 3 3 3 3 3 3 3 3 4 Fuel LB 191 200 208 219 249 219 228 238 251 285 44000 Distance NM 10 10 10 11 14 11 12 12 13 17 Time MIN 2 2 2 3 3 3 3 3 3 4 Fuel LB 180 188 196 206 233 206 215 224 236 268 42000 Distance NM 9 9 10 10 13 11 11 11 12 16 Time MIN 2 2 2 2 3 3 3 3 3 4 Fuel LB 170 177 184 194 219 194 203 211 222 251 40000 Distance NM 8 9 9 10 12 10 10 11 12 15 Time MIN 2 2 2 2 3 2 2 3 3 3 Fuel LB 159 166 173 182 205 182 190 198 208 235 38000 Distance NM 8 8 9 9 12 9 10 10 11 14 Time MIN 2 2 2 2 3 2 2 2 3 3 Fuel LB 149 156 162 170 192 171 178 186 195 220 36000 Distance NM 7 8 8 9 11 9 9 9 10 13 Time MIN 2 2 2 2 3 2 2 2 2 3 Fuel LB 140 146 152 159 179 160 167 174 182 205 34000 Distance NM 7 7 8 8 10 8 8 9 9 12 Time MIN 2 2 2 2 2 2 2 2 2 3 Fuel LB 130 136 142 149 166 149 155 162 170 191 32000 Distance NM 6 7 7 8 9 8 8 8 9 11 Time MIN 2 2 2 2 2 2 2 2 2 3 Fuel LB 121 126 132 138 154 139 144 151 158 177 30000 Distance NM 6 6 7 7 9 7 7 8 8 10 Time MIN 2 2 2 2 2 2 2 2 2 2 ### Page 10 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-10 Page 4 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 9000 AND 10000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 290 KIAS AT 12000 FT, MAINTAINING 290 KIAS UP TO 21600 FT AND M = 0.65 ABOVE 21600 FT. AUTOPILOT CLIMB SCHEDULE BLEED: OPEN 9000 ft 10000 ft ISA + °C ISA + °C WEIGHT (lb) -20 -10 0 10 20 -20 -10 0 10 20 Fuel LB 293 306 319 336 389 327 341 356 375 435 50000 Distance NM 15 16 17 18 23 17 18 19 20 26 Time MIN 4 4 4 4 5 4 4 4 5 6 Fuel LB 277 289 302 318 365 309 322 336 354 409 48000 Distance NM 14 15 16 17 22 16 17 18 19 25 Time MIN 4 4 4 4 5 4 4 4 4 6 Fuel LB 262 273 285 300 344 292 304 317 334 384 46000 Distance NM 14 14 15 16 20 15 16 17 18 23 Time MIN 3 3 3 4 5 4 4 4 4 5 Fuel LB 247 258 269 283 323 275 287 299 315 361 44000 Distance NM 13 13 14 15 19 15 15 16 17 22 Time MIN 3 3 3 3 4 4 4 4 4 5 Fuel LB 233 243 253 266 303 259 270 282 296 338 42000 Distance NM 12 13 13 14 18 14 14 15 16 20 Time MIN 3 3 3 3 4 3 3 3 4 5 Fuel LB 219 228 238 250 284 244 254 265 279 317 40000 Distance NM 11 12 12 13 17 13 13 14 15 19 Time MIN 3 3 3 3 4 3 3 3 3 4 Fuel LB 205 214 223 235 266 229 238 249 261 297 38000 Distance NM 11 11 12 12 16 12 13 13 14 18 Time MIN 3 3 3 3 4 3 3 3 3 4 Fuel LB 193 201 209 220 248 214 223 233 245 277 36000 Distance NM 10 10 11 12 15 11 12 12 13 17 Time MIN 2 2 3 3 3 3 3 3 3 4 Fuel LB 180 188 196 206 232 200 209 218 229 258 34000 Distance NM 9 10 10 11 14 11 11 11 12 15 Time MIN 2 2 2 3 3 3 3 3 3 3 Fuel LB 168 175 182 192 215 187 195 203 213 240 32000 Distance NM 9 9 9 10 13 10 10 11 11 14 Time MIN 2 2 2 2 3 2 2 3 3 3 Fuel LB 156 163 169 178 200 173 181 189 198 223 30000 Distance NM 8 8 9 9 12 9 9 10 11 13 Time MIN 2 2 2 2 3 2 2 2 2 3 ### Page 11 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-10 Page 5 Code 06 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 11000 AND 12000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 290 KIAS AT 12000 FT, MAINTAINING 290 KIAS UP TO 21600 FT AND M = 0.65 ABOVE 21600 FT. AUTOPILOT CLIMB SCHEDULE BLEED: OPEN 11000 ft 12000 ft ISA + °C ISA + °C WEIGHT (lb) -20 -10 0 10 20 -20 -10 0 10 20 Fuel LB 362 378 395 417 486 403 421 440 465 551 50000 Distance NM 20 21 22 23 30 23 24 25 27 36 Time MIN 5 5 5 5 7 5 5 6 6 8 Fuel LB 342 357 373 393 456 381 398 415 439 517 48000 Distance NM 19 19 20 22 28 21 22 23 25 33 Time MIN 4 5 5 5 6 5 5 5 6 7 Fuel LB 323 337 352 371 429 359 375 392 414 485 46000 Distance NM 18 18 19 21 27 20 21 22 24 31 Time MIN 4 4 4 5 6 5 5 5 5 7 Fuel LB 305 318 332 349 402 338 353 369 390 455 44000 Distance NM 16 17 18 19 25 19 20 21 22 29 Time MIN 4 4 4 4 5 4 5 5 5 6 Fuel LB 287 299 312 329 377 319 333 347 366 426 42000 Distance NM 16 16 17 18 23 18 19 20 21 28 Time MIN 4 4 4 4 5 4 4 4 5 6 Fuel LB 270 281 293 309 353 299 313 326 344 399 40000 Distance NM 15 15 16 17 22 17 18 18 20 26 Time MIN 3 4 4 4 5 4 4 4 4 6 Fuel LB 253 264 275 290 330 281 293 306 323 373 38000 Distance NM 14 14 15 16 20 16 16 17 18 24 Time MIN 3 3 3 4 5 4 4 4 4 5 Fuel LB 237 247 258 271 309 263 275 287 302 348 36000 Distance NM 13 13 14 15 19 15 15 16 17 22 Time MIN 3 3 3 3 4 3 4 4 4 5 Fuel LB 221 231 241 253 287 246 257 268 282 324 34000 Distance NM 12 12 13 14 18 14 14 15 16 21 Time MIN 3 3 3 3 4 3 3 3 4 4 Fuel LB 206 215 225 236 267 229 239 249 263 301 32000 Distance NM 11 12 12 13 16 13 13 14 15 19 Time MIN 3 3 3 3 4 3 3 3 3 4 Fuel LB 192 200 209 219 248 213 222 232 244 278 30000 Distance NM 10 11 11 12 15 12 12 13 14 18 Time MIN 2 3 3 3 3 3 3 3 3 4 ### Page 12 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-10 Page 6 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 13000 AND 14000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 290 KIAS AT 12000 FT, MAINTAINING 290 KIAS UP TO 21600 FT AND M = 0.65 ABOVE 21600 FT. AUTOPILOT CLIMB SCHEDULE BLEED: OPEN 13000 ft 14000 ft ISA + °C ISA + °C WEIGHT (lb) -20 -10 0 10 20 -20 -10 0 10 20 Fuel LB 449 469 491 521 632 496 519 544 579 719 50000 Distance NM 26 28 29 31 43 30 32 33 36 52 Time MIN 6 6 6 7 9 7 7 7 7 10 Fuel LB 424 443 463 491 592 468 490 512 545 672 48000 Distance NM 25 26 27 30 40 29 30 31 34 48 Time MIN 6 6 6 6 8 6 6 7 7 10 Fuel LB 399 417 436 462 554 441 461 483 513 628 46000 Distance NM 23 25 26 28 38 27 28 30 32 45 Time MIN 5 5 6 6 8 6 6 6 7 9 Fuel LB 376 393 411 435 519 415 434 454 482 587 44000 Distance NM 22 23 24 26 35 25 27 28 30 42 Time MIN 5 5 5 6 7 6 6 6 6 8 Fuel LB 354 370 387 409 485 391 408 427 453 549 42000 Distance NM 21 22 23 25 33 24 25 26 28 39 Time MIN 5 5 5 5 7 5 5 6 6 8 Fuel LB 333 347 363 384 454 367 383 401 425 512 40000 Distance NM 19 20 21 23 31 22 23 25 27 36 Time MIN 4 5 5 5 6 5 5 5 5 7 Fuel LB 312 326 341 360 424 344 359 376 399 478 38000 Distance NM 18 19 20 22 29 21 22 23 25 34 Time MIN 4 4 4 5 6 5 5 5 5 7 Fuel LB 292 305 319 337 395 322 336 352 373 445 36000 Distance NM 17 18 19 20 27 20 20 21 23 32 Time MIN 4 4 4 4 6 4 4 5 5 6 Fuel LB 273 285 298 314 367 300 314 328 348 413 34000 Distance NM 16 17 17 19 25 18 19 20 22 29 Time MIN 4 4 4 4 5 4 4 4 4 6 Fuel LB 254 265 277 293 341 280 292 306 324 383 32000 Distance NM 15 15 16 17 23 17 18 19 20 27 Time MIN 3 3 4 4 5 4 4 4 4 5 Fuel LB 236 246 257 272 315 260 271 284 300 354 30000 Distance NM 14 14 15 16 21 16 16 17 19 25 Time MIN 3 3 3 3 4 3 4 4 4 5 ### Page 13 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-10 Page 7 Code 06 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 15000 AND 16000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 290 KIAS AT 12000 FT, MAINTAINING 290 KIAS UP TO 21600 FT AND M = 0.65 ABOVE 21600 FT. AUTOPILOT CLIMB SCHEDULE BLEED: OPEN 15000 ft 16000 ft ISA + °C ISA + °C WEIGHT (lb) -20 -10 0 10 20 -20 -10 0 10 20 Fuel LB 546 571 598 639 814 596 625 655 702 918 50000 Distance NM 35 36 38 42 61 39 41 43 47 72 Time MIN 7 8 8 8 12 8 8 9 9 14 Fuel LB 514 538 564 601 759 562 588 617 660 854 48000 Distance NM 33 34 36 39 57 37 39 41 44 67 Time MIN 7 7 7 8 11 8 8 8 9 13 Fuel LB 484 507 531 566 708 528 553 580 620 795 46000 Distance NM 31 32 34 37 53 35 36 38 42 62 Time MIN 7 7 7 7 10 7 7 8 8 12 Fuel LB 455 477 499 532 661 497 520 545 582 740 44000 Distance NM 29 30 32 35 49 33 34 36 39 57 Time MIN 6 6 7 7 10 7 7 7 8 11 Fuel LB 428 448 469 499 616 467 489 512 547 689 42000 Distance NM 27 28 30 32 46 31 32 34 37 53 Time MIN 6 6 6 7 9 6 7 7 7 10 Fuel LB 402 420 440 468 574 438 459 480 512 641 40000 Distance NM 25 27 28 30 43 29 30 32 34 49 Time MIN 5 6 6 6 8 6 6 6 7 9 Fuel LB 377 394 412 438 535 410 430 450 479 596 38000 Distance NM 24 25 26 28 40 27 28 29 32 46 Time MIN 5 5 5 6 8 6 6 6 6 9 Fuel LB 352 369 386 410 497 384 402 421 448 554 36000 Distance NM 22 23 24 26 37 25 26 28 30 43 Time MIN 5 5 5 5 7 5 5 6 6 8 Fuel LB 329 344 360 382 462 358 375 392 417 513 34000 Distance NM 21 22 23 25 34 23 24 26 28 39 Time MIN 4 5 5 5 7 5 5 5 6 8 Fuel LB 306 320 335 355 428 333 349 365 388 475 32000 Distance NM 19 20 21 23 32 22 23 24 26 36 Time MIN 4 4 4 5 6 5 5 5 5 7 Fuel LB 284 297 311 330 395 309 323 338 360 438 30000 Distance NM 18 19 20 21 29 20 21 22 24 34 Time MIN 4 4 4 4 6 4 4 4 5 6 ### Page 14 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-10 Page 8 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 17000 AND 18000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 290 KIAS AT 12000 FT, MAINTAINING 290 KIAS UP TO 21600 FT AND M = 0.65 ABOVE 21600 FT. AUTOPILOT CLIMB SCHEDULE BLEED: OPEN 17000 ft 18000 ft ISA + °C ISA + °C WEIGHT (lb) -20 -10 0 10 20 -20 -10 0 10 20 Fuel LB 649 680 714 767 1032 702 737 774 835 1155 50000 Distance NM 44 46 49 54 84 49 52 54 60 97 Time MIN 9 9 10 10 15 10 10 10 11 18 Fuel LB 610 640 671 721 957 660 693 728 784 1068 48000 Distance NM 41 43 46 50 78 46 48 51 56 90 Time MIN 8 9 9 10 14 9 10 10 11 16 Fuel LB 574 602 631 677 888 621 651 683 736 988 46000 Distance NM 39 41 43 47 72 43 45 48 53 83 Time MIN 8 8 8 9 13 9 9 9 10 15 Fuel LB 540 565 593 635 825 583 611 642 690 916 44000 Distance NM 36 38 40 44 66 41 43 45 49 76 Time MIN 7 8 8 8 12 8 8 9 9 14 Fuel LB 507 531 557 596 766 547 574 602 646 849 42000 Distance NM 34 36 38 41 62 38 40 42 46 71 Time MIN 7 7 7 8 11 8 8 8 9 13 Fuel LB 475 498 522 558 712 513 538 564 605 787 40000 Distance NM 32 34 35 39 57 36 37 39 43 65 Time MIN 7 7 7 7 11 7 7 8 8 12 Fuel LB 445 466 488 522 661 480 503 528 565 730 38000 Distance NM 30 31 33 36 53 33 35 37 40 60 Time MIN 6 6 7 7 10 7 7 7 8 11 Fuel LB 416 435 456 487 613 448 470 493 528 676 36000 Distance NM 28 29 31 34 49 31 33 34 38 56 Time MIN 6 6 6 7 9 6 6 7 7 10 Fuel LB 388 406 425 454 568 418 438 459 491 625 34000 Distance NM 26 27 29 31 45 29 30 32 35 51 Time MIN 5 6 6 6 8 6 6 6 7 9 Fuel LB 361 378 396 422 525 389 407 427 456 577 32000 Distance NM 24 25 27 29 42 27 28 30 32 47 Time MIN 5 5 5 6 8 5 6 6 6 9 Fuel LB 334 350 367 391 484 360 377 396 423 531 30000 Distance NM 22 23 25 27 38 25 26 27 30 44 Time MIN 5 5 5 5 7 5 5 5 6 8 ### Page 15 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-10 Page 9 Code 06 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 19000 AND 20000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 290 KIAS AT 12000 FT, MAINTAINING 290 KIAS UP TO 21600 FT AND M = 0.65 ABOVE 21600 FT. AUTOPILOT CLIMB SCHEDULE BLEED: OPEN 19000 ft 20000 ft ISA + °C ISA + °C WEIGHT (lb) -20 -10 0 10 20 -20 -10 0 10 20 Fuel LB 757 794 835 905 1282 811 852 896 974 1406 50000 Distance NM 54 57 60 67 112 60 63 66 74 126 Time MIN 11 11 11 12 20 12 12 12 13 22 Fuel LB 711 746 784 848 1182 761 800 841 913 1293 48000 Distance NM 51 54 56 63 102 56 59 62 69 115 Time MIN 10 10 11 12 18 11 11 12 13 20 Fuel LB 668 701 736 795 1091 715 750 789 855 1192 46000 Distance NM 48 50 53 59 94 52 55 58 65 106 Time MIN 9 10 10 11 17 10 10 11 12 18 Fuel LB 627 658 691 745 1009 671 704 740 800 1100 44000 Distance NM 45 47 50 55 87 49 52 54 60 97 Time MIN 9 9 9 10 15 10 10 10 11 17 Fuel LB 588 617 648 698 933 629 660 693 749 1016 42000 Distance NM 42 44 46 51 80 46 48 51 56 89 Time MIN 8 9 9 10 14 9 9 10 10 16 Fuel LB 551 578 606 652 864 589 618 649 700 939 40000 Distance NM 39 41 43 48 74 43 45 48 53 82 Time MIN 8 8 8 9 13 8 9 9 10 14 Fuel LB 515 540 567 610 800 550 578 606 654 868 38000 Distance NM 37 38 41 45 68 40 42 44 49 76 Time MIN 7 7 8 8 12 8 8 8 9 13 Fuel LB 481 504 529 568 739 514 539 566 609 802 36000 Distance NM 34 36 38 42 63 37 39 41 46 70 Time MIN 7 7 7 8 11 7 8 8 8 12 Fuel LB 448 470 493 529 683 479 502 527 567 740 34000 Distance NM 32 33 35 39 58 35 37 38 42 64 Time MIN 6 6 7 7 10 7 7 7 8 11 Fuel LB 417 437 458 491 630 445 466 490 526 682 32000 Distance NM 30 31 33 36 53 32 34 36 39 59 Time MIN 6 6 6 7 10 6 6 7 7 10 Fuel LB 386 405 425 455 580 412 432 453 487 627 30000 Distance NM 27 29 30 33 49 30 31 33 36 54 Time MIN 5 6 6 6 9 6 6 6 7 10 ### Page 16 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-10 Page 10 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 21000 AND 22000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 290 KIAS AT 12000 FT, MAINTAINING 290 KIAS UP TO 21600 FT AND M = 0.65 ABOVE 21600 FT. AUTOPILOT CLIMB SCHEDULE BLEED: OPEN 21000 ft 22000 ft ISA + °C ISA + °C WEIGHT (lb) -20 -10 0 10 20 -20 -10 0 10 20 Fuel LB 866 911 958 1046 1539 917 964 1016 1113 1674 50000 Distance NM 65 69 72 81 141 70 74 78 88 157 Time MIN 12 13 13 15 24 13 14 14 16 26 Fuel LB 813 854 899 979 1412 860 904 952 1041 1531 48000 Distance NM 61 64 68 76 129 66 69 73 83 143 Time MIN 12 12 12 14 22 12 13 13 15 24 Fuel LB 763 801 843 916 1298 806 848 892 973 1404 46000 Distance NM 57 60 63 71 118 62 65 69 77 131 Time MIN 11 11 12 13 20 12 12 12 14 22 Fuel LB 715 751 790 857 1196 756 794 835 910 1291 44000 Distance NM 54 56 59 66 108 58 61 64 72 120 Time MIN 10 11 11 12 19 11 11 12 13 20 Fuel LB 670 704 740 802 1103 708 743 782 850 1188 42000 Distance NM 50 53 56 62 100 54 57 60 67 110 Time MIN 10 10 10 11 17 10 11 11 12 19 Fuel LB 627 659 692 749 1018 662 695 731 794 1095 40000 Distance NM 47 49 52 58 92 50 53 56 62 101 Time MIN 9 9 10 10 16 10 10 10 11 17 Fuel LB 586 615 647 699 940 619 650 683 740 1009 38000 Distance NM 44 46 48 54 84 47 49 52 58 93 Time MIN 8 9 9 10 15 9 9 10 10 16 Fuel LB 547 574 603 651 868 577 606 637 689 930 36000 Distance NM 41 43 45 50 78 44 46 49 54 85 Time MIN 8 8 8 9 13 8 9 9 10 15 Fuel LB 509 535 562 606 800 537 564 593 641 856 34000 Distance NM 38 40 42 46 71 41 43 45 50 78 Time MIN 7 8 8 8 12 8 8 8 9 13 Fuel LB 473 497 521 562 736 499 524 550 594 788 32000 Distance NM 35 37 39 43 66 38 40 42 46 72 Time MIN 7 7 7 8 11 7 7 8 8 12 Fuel LB 438 460 483 520 677 462 485 509 550 723 30000 Distance NM 32 34 36 40 60 35 37 39 43 66 Time MIN 6 6 7 7 10 7 7 7 8 11 ### Page 17 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-10 Page 11 Code 06 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 23000 AND 24000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 290 KIAS AT 12000 FT, MAINTAINING 290 KIAS UP TO 21600 FT AND M = 0.65 ABOVE 21600 FT. AUTOPILOT CLIMB SCHEDULE BLEED: OPEN 23000 ft 24000 ft ISA + °C ISA + °C WEIGHT (lb) -20 -10 0 10 20 -20 -10 0 10 20 Fuel LB 962 1012 1066 1173 1798 1006 1059 1116 1232 1921 50000 Distance NM 75 79 84 95 173 80 84 89 102 188 Time MIN 14 14 15 17 29 15 15 16 18 31 Fuel LB 902 948 999 1096 1639 943 992 1045 1150 1746 48000 Distance NM 70 74 78 89 157 75 79 83 95 170 Time MIN 13 14 14 15 26 14 14 15 16 28 Fuel LB 845 888 935 1024 1500 883 929 978 1074 1594 46000 Distance NM 66 69 73 83 143 70 74 78 88 155 Time MIN 12 13 13 14 24 13 13 14 15 26 Fuel LB 791 832 876 956 1376 826 869 915 1002 1459 44000 Distance NM 61 65 68 77 130 65 69 73 82 141 Time MIN 12 12 12 13 22 12 12 13 14 23 Fuel LB 741 779 819 893 1264 773 813 856 936 1339 42000 Distance NM 57 60 64 72 119 61 64 68 76 129 Time MIN 11 11 11 13 20 11 12 12 13 21 Fuel LB 693 728 766 833 1163 723 760 799 872 1230 40000 Distance NM 54 56 60 67 109 57 60 63 71 118 Time MIN 10 10 11 12 18 11 11 11 12 20 Fuel LB 647 680 715 777 1071 675 709 746 813 1131 38000 Distance NM 50 53 56 62 100 53 56 59 66 108 Time MIN 9 10 10 11 17 10 10 11 12 18 Fuel LB 603 634 666 723 986 629 661 695 756 1040 36000 Distance NM 47 49 52 58 92 49 52 55 61 99 Time MIN 9 9 9 10 16 9 9 10 11 17 Fuel LB 561 590 620 672 907 585 615 647 702 955 34000 Distance NM 43 45 48 54 84 46 48 51 57 91 Time MIN 8 8 9 9 14 9 9 9 10 15 Fuel LB 521 547 575 623 833 543 571 600 651 877 32000 Distance NM 40 42 44 50 77 42 45 47 53 83 Time MIN 8 8 8 9 13 8 8 8 9 14 Fuel LB 482 507 532 576 764 503 528 555 602 804 30000 Distance NM 37 39 41 46 71 39 41 44 49 76 Time MIN 7 7 7 8 12 7 8 8 9 13 ### Page 18 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-10 Page 12 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 25000 AND 26000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 290 KIAS AT 12000 FT, MAINTAINING 290 KIAS UP TO 21600 FT AND M = 0.65 ABOVE 21600 FT. AUTOPILOT CLIMB SCHEDULE BLEED: OPEN 25000 ft 26000 ft ISA + °C ISA + °C WEIGHT (lb) -19 -10 0 10 20 -18 -10 0 10 20 Fuel LB 1056 1106 1166 1290 2039 1107 1153 1216 1346 2150 50000 Distance NM 85 89 95 108 204 91 95 100 115 218 Time MIN 16 16 17 19 33 16 17 18 20 35 Fuel LB 988 1035 1091 1203 1849 1035 1078 1137 1255 1946 48000 Distance NM 80 83 88 101 184 85 88 93 107 196 Time MIN 15 15 16 17 30 15 16 16 18 32 Fuel LB 925 968 1020 1122 1684 968 1008 1063 1170 1769 46000 Distance NM 74 78 82 94 166 79 82 87 99 178 Time MIN 14 14 15 16 27 14 15 15 17 29 Fuel LB 865 906 954 1047 1539 905 943 993 1091 1615 44000 Distance NM 69 73 77 87 151 74 77 81 92 161 Time MIN 13 13 14 15 25 13 14 14 16 26 Fuel LB 809 847 892 977 1410 846 881 928 1017 1477 42000 Distance NM 65 68 72 81 138 69 72 76 86 147 Time MIN 12 12 13 14 23 13 13 13 15 24 Fuel LB 756 791 833 910 1294 790 823 866 947 1354 40000 Distance NM 60 63 67 75 126 64 67 71 80 134 Time MIN 11 11 12 13 21 12 12 12 14 22 Fuel LB 706 738 777 848 1188 737 767 807 881 1242 38000 Distance NM 56 59 62 70 115 60 62 66 74 123 Time MIN 10 11 11 12 19 11 11 12 13 20 Fuel LB 658 688 724 788 1091 686 714 752 819 1140 36000 Distance NM 52 55 58 65 106 56 58 61 69 112 Time MIN 10 10 10 11 18 10 10 11 12 18 Fuel LB 611 640 673 732 1002 638 664 699 760 1046 34000 Distance NM 49 51 54 60 97 52 54 57 64 103 Time MIN 9 9 10 10 16 9 10 10 11 17 Fuel LB 567 593 624 678 919 592 616 648 704 959 32000 Distance NM 45 47 50 56 88 48 50 52 59 94 Time MIN 8 9 9 10 15 9 9 9 10 16 Fuel LB 525 549 577 626 842 547 570 599 650 878 30000 Distance NM 42 44 46 51 81 44 46 48 54 86 Time MIN 8 8 8 9 13 8 8 9 9 14 ### Page 19 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-10 Page 13 Code 06 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 27000 AND 28000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 290 KIAS AT 12000 FT, MAINTAINING 290 KIAS UP TO 21600 FT AND M = 0.65 ABOVE 21600 FT. AUTOPILOT CLIMB SCHEDULE BLEED: OPEN 27000 ft 28000 ft ISA + °C ISA + °C WEIGHT (lb) -17 -10 0 10 20 -16 -10 0 10 20 Fuel LB 1159 1202 1267 1403 2254 1213 1251 1320 1460 2354 50000 Distance NM 97 100 106 121 233 103 106 113 128 246 Time MIN 17 18 18 21 37 18 19 19 22 40 Fuel LB 1083 1123 1184 1306 2037 1132 1168 1232 1358 2124 48000 Distance NM 90 94 99 113 209 96 99 105 119 221 Time MIN 16 17 17 19 34 17 17 18 20 36 Fuel LB 1012 1049 1105 1217 1850 1057 1090 1149 1264 1926 46000 Distance NM 84 87 92 105 188 89 92 97 110 199 Time MIN 15 16 16 18 31 16 16 17 19 32 Fuel LB 945 980 1032 1134 1686 987 1018 1072 1177 1753 44000 Distance NM 78 81 86 97 171 83 86 91 102 180 Time MIN 14 14 15 17 28 15 15 16 17 29 Fuel LB 883 915 964 1056 1540 921 950 1000 1095 1601 42000 Distance NM 73 76 80 90 155 77 80 84 95 164 Time MIN 13 14 14 15 25 14 14 15 16 27 Fuel LB 824 854 899 983 1410 859 886 933 1019 1464 40000 Distance NM 68 71 74 84 142 72 74 79 88 149 Time MIN 12 13 13 14 23 13 13 14 15 24 Fuel LB 768 796 838 915 1293 800 825 869 948 1341 38000 Distance NM 63 66 69 78 129 67 69 73 82 136 Time MIN 11 12 12 13 21 12 12 13 14 22 Fuel LB 715 741 780 850 1186 745 768 808 880 1229 36000 Distance NM 59 61 64 72 118 62 64 68 76 124 Time MIN 11 11 11 12 19 11 11 12 13 20 Fuel LB 665 689 724 788 1087 692 713 750 816 1127 34000 Distance NM 55 57 60 67 108 58 59 63 70 113 Time MIN 10 10 10 11 18 10 11 11 12 19 Fuel LB 616 638 671 730 996 641 661 695 755 1032 32000 Distance NM 50 52 55 62 99 53 55 58 65 104 Time MIN 9 9 10 11 16 10 10 10 11 17 Fuel LB 570 590 621 674 911 592 611 642 697 944 30000 Distance NM 47 48 51 57 90 49 51 54 60 94 Time MIN 8 9 9 10 15 9 9 9 10 16 ### Page 20 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-10 Page 14 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 29000 AND 30000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 290 KIAS AT 12000 FT, MAINTAINING 290 KIAS UP TO 21600 FT AND M = 0.65 ABOVE 21600 FT. AUTOPILOT CLIMB SCHEDULE BLEED: OPEN 29000 ft 30000 ft ISA + °C ISA + °C WEIGHT (lb) -15 -10 0 10 20 -14 -10 0 10 20 Fuel LB 1267 1301 1373 1518 2451 1322 1350 1425 1576 2546 50000 Distance NM 109 113 119 136 260 116 119 125 143 273 Time MIN 19 20 20 23 42 20 21 21 24 44 Fuel LB 1182 1213 1279 1410 2208 1231 1257 1326 1462 2291 48000 Distance NM 102 105 111 125 232 108 110 116 132 244 Time MIN 18 18 19 21 37 19 19 20 22 39 Fuel LB 1102 1131 1193 1311 2000 1147 1171 1235 1358 2072 46000 Distance NM 95 97 103 116 209 100 102 108 122 219 Time MIN 17 17 18 20 34 18 18 19 20 35 Fuel LB 1028 1055 1112 1220 1819 1069 1092 1151 1262 1883 44000 Distance NM 88 90 96 108 189 93 95 100 113 198 Time MIN 16 16 16 18 31 16 17 17 19 32 Fuel LB 959 984 1037 1135 1659 996 1017 1072 1174 1716 42000 Distance NM 82 84 89 100 172 86 88 93 105 180 Time MIN 15 15 15 17 28 15 15 16 18 29 Fuel LB 894 917 966 1055 1517 928 948 998 1091 1567 40000 Distance NM 76 78 83 93 156 80 82 87 97 163 Time MIN 14 14 14 16 25 14 14 15 16 26 Fuel LB 832 854 899 981 1388 864 882 929 1013 1433 38000 Distance NM 71 73 77 86 143 74 76 80 90 149 Time MIN 13 13 13 15 23 13 13 14 15 24 Fuel LB 774 794 836 910 1271 803 820 863 940 1312 36000 Distance NM 66 67 71 80 130 69 71 75 83 136 Time MIN 12 12 12 13 21 12 12 13 14 22 Fuel LB 719 737 776 844 1165 745 760 800 871 1201 34000 Distance NM 61 62 66 74 119 64 65 69 77 124 Time MIN 11 11 11 12 19 11 12 12 13 20 Fuel LB 666 683 719 780 1066 690 704 741 805 1099 32000 Distance NM 56 58 61 68 108 59 60 64 71 113 Time MIN 10 10 11 12 18 11 11 11 12 18 Fuel LB 615 631 664 720 974 637 650 684 742 1004 30000 Distance NM 52 53 56 63 99 54 56 59 65 103 Time MIN 9 9 10 11 16 10 10 10 11 17 ### Page 21 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-10 Page 15 Code 06 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 31000 AND 32000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 290 KIAS AT 12000 FT, MAINTAINING 290 KIAS UP TO 21600 FT AND M = 0.65 ABOVE 21600 FT. AUTOPILOT CLIMB SCHEDULE BLEED: OPEN 31000 ft 32000 ft ISA + °C ISA + °C WEIGHT (lb) -13 -5 0 10 20 -12 -5 0 10 20 Fuel LB 1375 1435 1475 1634 2642 1428 1482 1524 1693 2742 50000 Distance NM 122 128 132 150 287 129 134 138 158 302 Time MIN 21 22 22 25 46 22 23 23 26 48 Fuel LB 1280 1335 1372 1514 2373 1328 1377 1416 1567 2458 48000 Distance NM 113 119 122 139 256 119 124 128 146 269 Time MIN 20 20 21 23 41 21 21 22 24 43 Fuel LB 1191 1242 1276 1405 2144 1235 1281 1316 1453 2218 46000 Distance NM 105 110 113 128 230 111 115 118 135 241 Time MIN 18 19 19 21 37 19 20 20 22 38 Fuel LB 1110 1157 1188 1305 1946 1149 1192 1224 1348 2010 44000 Distance NM 98 102 105 119 207 103 107 110 124 217 Time MIN 17 18 18 20 33 18 18 19 21 35 Fuel LB 1033 1077 1106 1212 1772 1070 1109 1139 1251 1828 42000 Distance NM 91 95 98 110 188 95 99 102 115 196 Time MIN 16 16 17 18 30 17 17 17 19 31 Fuel LB 962 1002 1029 1126 1617 995 1032 1059 1161 1666 40000 Distance NM 84 88 90 102 171 88 92 94 106 178 Time MIN 15 15 16 17 28 15 16 16 18 29 Fuel LB 895 932 957 1045 1478 925 959 985 1077 1522 38000 Distance NM 78 82 84 94 155 82 85 87 98 162 Time MIN 14 14 14 16 25 14 15 15 16 26 Fuel LB 831 866 889 969 1352 859 890 914 998 1391 36000 Distance NM 72 76 78 87 142 76 79 81 91 147 Time MIN 13 13 13 15 23 13 14 14 15 24 Fuel LB 771 803 824 897 1237 797 825 847 923 1272 34000 Distance NM 67 70 72 81 129 70 73 75 84 134 Time MIN 12 12 12 14 21 12 13 13 14 22 Fuel LB 714 743 763 829 1131 737 764 784 853 1163 32000 Distance NM 62 65 66 74 118 65 67 69 77 122 Time MIN 11 11 11 13 19 11 12 12 13 20 Fuel LB 659 686 704 764 1033 680 705 723 786 1062 30000 Distance NM 57 60 61 68 107 60 62 64 71 111 Time MIN 10 10 11 12 17 11 11 11 12 18 ### Page 22 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-10 Page 16 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 33000 AND 34000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 290 KIAS AT 12000 FT, MAINTAINING 290 KIAS UP TO 21600 FT AND M = 0.65 ABOVE 21600 FT. AUTOPILOT CLIMB SCHEDULE BLEED: OPEN 33000 ft 34000 ft ISA + °C ISA + °C WEIGHT (lb) -10 -5 0 10 20 -9 -5 0 10 20 Fuel LB 1490 1530 1573 1754 2843 1549 1582 1626 1818 2946 50000 Distance NM 136 140 144 166 317 144 147 151 175 333 Time MIN 24 24 24 27 50 25 25 26 29 53 Fuel LB 1384 1421 1460 1622 2544 1436 1466 1507 1677 2630 48000 Distance NM 126 129 133 153 282 133 136 139 161 295 Time MIN 22 22 23 25 45 23 23 24 27 47 Fuel LB 1286 1320 1356 1501 2291 1333 1361 1398 1550 2364 46000 Distance NM 117 120 123 141 252 123 125 129 148 263 Time MIN 20 21 21 23 40 21 21 22 24 42 Fuel LB 1196 1227 1261 1391 2073 1238 1264 1298 1435 2137 44000 Distance NM 108 111 114 130 227 113 116 119 136 236 Time MIN 19 19 19 22 36 20 20 20 23 38 Fuel LB 1112 1141 1172 1290 1883 1150 1174 1206 1329 1939 42000 Distance NM 100 103 106 120 205 105 107 110 126 213 Time MIN 17 18 18 20 33 18 18 19 21 34 Fuel LB 1034 1061 1089 1196 1715 1069 1091 1120 1231 1764 40000 Distance NM 93 95 98 111 186 97 99 102 116 193 Time MIN 16 16 17 19 30 17 17 17 19 31 Fuel LB 961 986 1012 1108 1566 992 1013 1040 1140 1608 38000 Distance NM 86 88 91 103 169 90 92 95 107 175 Time MIN 15 15 16 17 27 16 16 16 18 28 Fuel LB 892 915 939 1027 1430 920 940 964 1055 1468 36000 Distance NM 80 82 84 95 153 83 85 87 99 159 Time MIN 14 14 14 16 25 14 15 15 16 26 Fuel LB 826 848 870 950 1307 853 870 893 976 1341 34000 Distance NM 74 76 78 88 140 77 79 81 91 145 Time MIN 13 13 13 15 23 13 14 14 15 23 Fuel LB 764 784 805 877 1194 788 804 826 900 1224 32000 Distance NM 68 70 72 81 127 71 72 74 84 132 Time MIN 12 12 12 13 21 12 13 13 14 21 Fuel LB 705 723 742 808 1089 727 742 761 829 1116 30000 Distance NM 63 64 66 74 116 65 67 69 77 120 Time MIN 11 11 11 12 19 11 12 12 13 19 ### Page 23 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-10 Page 17 Code 06 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 35000 AND 36000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 290 KIAS AT 12000 FT, MAINTAINING 290 KIAS UP TO 21600 FT AND M = 0.65 ABOVE 21600 FT. AUTOPILOT CLIMB SCHEDULE BLEED: OPEN 35000 ft 36000 ft ISA + °C ISA + °C WEIGHT (lb) -8 -5 0 10 20 -7 -5 0 10 20 Fuel LB 1612 1638 1683 1884 3057 1681 1699 1746 1953 3176 50000 Distance NM 152 155 159 185 351 162 163 168 195 370 Time MIN 26 26 27 30 55 28 28 28 32 58 Fuel LB 1492 1515 1557 1735 2721 1552 1568 1611 1794 2817 48000 Distance NM 140 142 146 169 309 148 150 154 177 325 Time MIN 24 24 25 28 49 25 25 26 29 51 Fuel LB 1382 1404 1443 1601 2441 1435 1451 1490 1653 2520 46000 Distance NM 129 131 135 155 275 136 138 142 162 288 Time MIN 22 22 23 26 44 23 23 24 27 46 Fuel LB 1283 1303 1338 1480 2202 1330 1343 1380 1525 2269 44000 Distance NM 119 121 125 143 247 126 127 131 149 257 Time MIN 21 21 21 24 39 22 22 22 25 41 Fuel LB 1190 1209 1242 1369 1995 1232 1245 1279 1409 2052 42000 Distance NM 110 112 115 131 222 116 117 120 137 231 Time MIN 19 19 20 22 35 20 20 20 23 37 Fuel LB 1105 1122 1152 1267 1813 1143 1154 1185 1303 1863 40000 Distance NM 102 104 107 121 201 107 108 111 126 209 Time MIN 18 18 18 20 32 18 19 19 21 33 Fuel LB 1025 1041 1069 1172 1651 1059 1070 1098 1204 1695 38000 Distance NM 94 96 99 112 182 99 100 103 116 189 Time MIN 16 16 17 19 29 17 17 17 19 30 Fuel LB 950 965 990 1084 1506 981 991 1017 1113 1544 36000 Distance NM 87 89 91 103 165 91 92 95 107 171 Time MIN 15 15 15 17 26 16 16 16 18 27 Fuel LB 880 893 917 1002 1375 907 917 941 1028 1408 34000 Distance NM 80 82 84 95 150 84 85 87 99 156 Time MIN 14 14 14 16 24 15 15 15 16 25 Fuel LB 813 825 847 924 1254 838 846 869 947 1284 32000 Distance NM 74 75 77 87 137 78 78 81 91 141 Time MIN 13 13 13 15 22 13 13 14 15 23 Fuel LB 749 761 781 850 1143 772 780 800 871 1170 30000 Distance NM 68 69 71 80 124 71 72 74 83 128 Time MIN 12 12 12 13 20 12 12 13 14 21 ### Page 24 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-10 Page 18 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 37000 AND 38000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 290 KIAS AT 12000 FT, MAINTAINING 290 KIAS UP TO 21600 FT AND M = 0.65 ABOVE 21600 FT. AUTOPILOT CLIMB SCHEDULE BLEED: OPEN 37000 ft 38000 ft ISA + °C ISA + °C WEIGHT (lb) -8 -5 0 10 20 -8 -5 0 10 20 Fuel LB 1744 1772 1820 2033 - 1839 1867 1917 2142 - 50000 Distance NM 171 174 179 206 - 186 189 194 224 - Time MIN 29 29 30 34 - 32 32 32 36 - Fuel LB 1604 1629 1674 1861 - 1680 1706 1752 1948 - 48000 Distance NM 156 159 163 187 - 168 171 176 201 - Time MIN 27 27 27 31 - 29 29 29 33 - Fuel LB 1480 1503 1544 1710 2614 1542 1566 1608 1781 - 46000 Distance NM 143 146 150 171 304 153 156 160 182 - Time MIN 25 25 25 28 48 26 26 27 30 - Fuel LB 1368 1389 1426 1575 2346 1420 1443 1481 1634 2451 44000 Distance NM 132 134 137 157 270 140 142 146 166 289 Time MIN 23 23 23 26 43 24 24 25 27 46 Fuel LB 1265 1285 1320 1453 2117 1311 1331 1367 1504 2200 42000 Distance NM 121 123 127 144 242 128 130 134 152 257 Time MIN 21 21 21 24 38 22 22 23 25 41 Fuel LB 1171 1190 1221 1341 1917 1211 1230 1262 1385 1985 40000 Distance NM 112 113 117 132 218 118 120 123 139 230 Time MIN 19 19 20 22 35 20 20 21 23 37 Fuel LB 1084 1101 1130 1239 1742 1119 1136 1166 1277 1799 38000 Distance NM 103 105 107 121 197 108 110 113 127 207 Time MIN 18 18 18 20 31 19 19 19 21 33 Fuel LB 1003 1019 1046 1143 1586 1034 1050 1077 1177 1634 36000 Distance NM 95 96 99 112 178 100 101 104 117 187 Time MIN 16 17 17 18 29 17 17 18 19 30 Fuel LB 927 942 966 1055 1444 954 969 994 1085 1486 34000 Distance NM 87 89 91 103 162 92 93 96 107 169 Time MIN 15 15 15 17 26 16 16 16 18 27 Fuel LB 856 869 892 972 1316 880 893 917 998 1352 32000 Distance NM 80 82 84 94 147 84 85 88 98 153 Time MIN 14 14 14 16 24 15 15 15 16 25 Fuel LB 788 800 821 893 1198 809 822 843 917 1229 30000 Distance NM 74 75 77 86 133 77 78 80 90 139 Time MIN 13 13 13 14 21 13 13 14 15 22 ### Page 25 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-10 Page 19 Code 06 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 39000 SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 290 KIAS AT 12000 FT, MAINTAINING 290 KIAS UP TO 21600 FT AND M = 0.65 ABOVE 21600 FT. AUTOPILOT CLIMB SCHEDULE BLEED: OPEN 39000 ft ISA + °C WEIGHT(lb) -8 -5 0 10 20 Fuel LB - - - - - 50000 Distance NM - - - - - Time MIN - - - - - Fuel LB - - 1853 - - 48000 Distance NM - - 192 - - Time MIN - - 32 - - Fuel LB 1619 1644 1688 1872 - 46000 Distance NM 166 168 173 197 - Time MIN 28 28 29 32 - Fuel LB 1483 1506 1546 1707 - 44000 Distance NM 150 153 157 178 - Time MIN 26 26 26 29 - Fuel LB 1363 1384 1420 1564 - 42000 Distance NM 137 139 143 162 - Time MIN 23 24 24 26 - Fuel LB 1255 1274 1308 1436 2072 40000 Distance NM 125 127 131 147 246 Time MIN 21 22 22 24 39 Fuel LB 1157 1175 1206 1320 1868 38000 Distance NM 115 116 120 135 220 Time MIN 20 20 20 22 35 Fuel LB 1067 1083 1112 1215 1690 36000 Distance NM 105 107 110 123 197 Time MIN 18 18 18 20 31 Fuel LB 983 998 1024 1118 1533 34000 Distance NM 96 98 101 113 178 Time MIN 17 17 17 19 28 Fuel LB 905 919 943 1027 1392 32000 Distance NM 88 90 92 103 161 Time MIN 15 15 16 17 26 Fuel LB 832 844 866 942 1264 30000 Distance NM 81 82 84 94 145 Time MIN 14 14 14 16 23 ### Page 26 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-10 Page 20 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 5000 AND 6000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 260 KIAS AT 12000 FT, MAINTAINING 260 KIAS UP TO 22800 FT AND M = 0.60 ABOVE 22800 FT. ALTERNATIVE CLIMB SCHEDULE BLEED: OPEN 5000 ft 6000 ft ISA + °C ISA + °C WEIGHT (lb) -20 -10 0 10 20 -20 -10 0 10 20 Fuel LB 161 168 175 184 211 194 202 211 222 254 50000 Distance NM 8 8 9 9 12 10 10 10 11 14 Time MIN 2 2 2 2 3 2 2 3 3 3 Fuel LB 153 159 166 174 199 184 191 200 210 240 48000 Distance NM 7 8 8 9 11 9 9 10 11 13 Time MIN 2 2 2 2 3 2 2 2 2 3 Fuel LB 144 150 157 165 187 173 181 189 198 226 46000 Distance NM 7 7 8 8 10 9 9 9 10 13 Time MIN 2 2 2 2 2 2 2 2 2 3 Fuel LB 136 142 148 156 176 164 171 178 187 212 44000 Distance NM 7 7 7 8 10 8 8 9 9 12 Time MIN 2 2 2 2 2 2 2 2 2 3 Fuel LB 128 134 140 147 165 154 161 168 176 199 42000 Distance NM 6 6 7 7 9 8 8 8 9 11 Time MIN 2 2 2 2 2 2 2 2 2 3 Fuel LB 121 126 131 138 155 145 151 158 166 187 40000 Distance NM 6 6 6 7 8 7 7 8 8 10 Time MIN 1 2 2 2 2 2 2 2 2 2 Fuel LB 114 118 123 130 146 137 142 148 156 175 38000 Distance NM 5 6 6 6 8 7 7 7 8 10 Time MIN 1 1 1 2 2 2 2 2 2 2 Fuel LB 107 111 116 121 136 128 133 139 146 164 36000 Distance NM 5 5 6 6 7 6 7 7 7 9 Time MIN 1 1 1 1 2 2 2 2 2 2 Fuel LB 100 104 108 114 127 120 125 130 136 153 34000 Distance NM 5 5 5 6 7 6 6 6 7 8 Time MIN 1 1 1 1 2 1 2 2 2 2 Fuel LB 93 97 101 106 118 112 116 121 127 142 32000 Distance NM 4 5 5 5 6 5 6 6 6 8 Time MIN 1 1 1 1 2 1 1 1 2 2 Fuel LB 86 90 94 98 110 104 108 113 118 132 30000 Distance NM 4 4 4 5 6 5 5 6 6 7 Time MIN 1 1 1 1 1 1 1 1 1 2 ### Page 27 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-10 Page 21 Code 06 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 7000 AND 8000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 260 KIAS AT 12000 FT, MAINTAINING 260 KIAS UP TO 22800 FT AND M = 0.60 ABOVE 22800 FT. ALTERNATIVE CLIMB SCHEDULE BLEED: OPEN 7000 ft 8000 ft ISA + °C ISA + °C WEIGHT (lb) -20 -10 0 10 20 -20 -10 0 10 20 Fuel LB 227 237 247 260 298 260 271 283 298 343 50000 Distance NM 11 12 12 13 17 13 14 14 16 20 Time MIN 3 3 3 3 4 3 3 3 4 5 Fuel LB 215 224 233 246 281 246 256 267 282 323 48000 Distance NM 11 11 12 13 16 13 13 14 15 19 Time MIN 3 3 3 3 4 3 3 3 3 4 Fuel LB 203 211 220 232 264 232 242 253 266 304 46000 Distance NM 10 11 11 12 15 12 12 13 14 18 Time MIN 3 3 3 3 3 3 3 3 3 4 Fuel LB 191 200 208 219 249 219 228 238 251 285 44000 Distance NM 10 10 10 11 14 11 12 12 13 17 Time MIN 2 2 2 3 3 3 3 3 3 4 Fuel LB 180 188 196 206 233 206 215 224 236 268 42000 Distance NM 9 9 10 10 13 11 11 11 12 16 Time MIN 2 2 2 2 3 3 3 3 3 4 Fuel LB 170 177 184 194 219 194 203 211 222 251 40000 Distance NM 8 9 9 10 12 10 10 11 12 15 Time MIN 2 2 2 2 3 2 2 3 3 3 Fuel LB 159 166 173 182 205 182 190 198 208 235 38000 Distance NM 8 8 9 9 12 9 10 10 11 14 Time MIN 2 2 2 2 3 2 2 2 3 3 Fuel LB 149 156 162 170 192 171 178 186 195 220 36000 Distance NM 7 8 8 9 11 9 9 9 10 13 Time MIN 2 2 2 2 3 2 2 2 2 3 Fuel LB 140 146 152 159 179 160 167 174 182 205 34000 Distance NM 7 7 8 8 10 8 8 9 9 12 Time MIN 2 2 2 2 2 2 2 2 2 3 Fuel LB 130 136 142 149 166 149 155 162 170 191 32000 Distance NM 6 7 7 8 9 8 8 8 9 11 Time MIN 2 2 2 2 2 2 2 2 2 3 Fuel LB 121 126 132 138 154 139 144 151 158 177 30000 Distance NM 6 6 7 7 9 7 7 8 8 10 Time MIN 2 2 2 2 2 2 2 2 2 2 ### Page 28 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-10 Page 22 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 9000 AND 10000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 260 KIAS AT 12000 FT, MAINTAINING 260 KIAS UP TO 22800 FT AND M = 0.60 ABOVE 22800 FT. ALTERNATIVE CLIMB SCHEDULE BLEED: OPEN 9000 ft 10000 ft ISA + °C ISA + °C WEIGHT (lb) -20 -10 0 10 20 -20 -10 0 10 20 Fuel LB 293 306 319 336 389 327 341 356 375 435 50000 Distance NM 15 16 17 18 23 17 18 19 20 26 Time MIN 4 4 4 4 5 4 4 4 5 6 Fuel LB 277 289 302 318 365 309 322 336 354 409 48000 Distance NM 14 15 16 17 22 16 17 18 19 25 Time MIN 4 4 4 4 5 4 4 4 4 6 Fuel LB 262 273 285 300 344 292 304 317 334 384 46000 Distance NM 14 14 15 16 20 15 16 17 18 23 Time MIN 3 3 3 4 5 4 4 4 4 5 Fuel LB 247 258 269 283 323 275 287 299 315 361 44000 Distance NM 13 13 14 15 19 15 15 16 17 22 Time MIN 3 3 3 3 4 4 4 4 4 5 Fuel LB 233 243 253 266 303 259 270 282 296 338 42000 Distance NM 12 13 13 14 18 14 14 15 16 20 Time MIN 3 3 3 3 4 3 3 3 4 5 Fuel LB 219 228 238 250 284 244 254 265 279 317 40000 Distance NM 11 12 12 13 17 13 13 14 15 19 Time MIN 3 3 3 3 4 3 3 3 3 4 Fuel LB 205 214 223 235 266 229 238 249 261 297 38000 Distance NM 11 11 12 12 16 12 13 13 14 18 Time MIN 3 3 3 3 4 3 3 3 3 4 Fuel LB 193 201 209 220 248 214 223 233 245 277 36000 Distance NM 10 10 11 12 15 11 12 12 13 17 Time MIN 2 2 3 3 3 3 3 3 3 4 Fuel LB 180 188 196 206 232 200 209 218 229 258 34000 Distance NM 9 10 10 11 14 11 11 11 12 15 Time MIN 2 2 2 3 3 3 3 3 3 3 Fuel LB 168 175 182 192 215 187 195 203 213 240 32000 Distance NM 9 9 9 10 13 10 10 11 11 14 Time MIN 2 2 2 2 3 2 2 3 3 3 Fuel LB 156 163 169 178 200 173 181 189 198 223 30000 Distance NM 8 8 9 9 12 9 9 10 11 13 Time MIN 2 2 2 2 3 2 2 2 2 3 ### Page 29 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-10 Page 23 Code 06 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 11000 AND 12000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 260 KIAS AT 12000 FT, MAINTAINING 260 KIAS UP TO 22800 FT AND M = 0.60 ABOVE 22800 FT. ALTERNATIVE CLIMB SCHEDULE BLEED: OPEN 11000 ft 12000 ft ISA + °C ISA + °C WEIGHT (lb) -20 -10 0 10 20 -20 -10 0 10 20 Fuel LB 361 377 394 415 483 398 415 433 458 536 50000 Distance NM 20 20 21 23 30 22 23 24 26 34 Time MIN 5 5 5 5 7 5 5 5 6 7 Fuel LB 341 356 372 392 454 375 392 409 432 503 48000 Distance NM 18 19 20 22 28 21 22 23 24 32 Time MIN 4 5 5 5 6 5 5 5 5 7 Fuel LB 322 336 351 370 426 354 370 386 407 472 46000 Distance NM 17 18 19 20 26 20 21 21 23 30 Time MIN 4 4 4 5 6 5 5 5 5 7 Fuel LB 304 317 331 348 400 334 348 364 383 443 44000 Distance NM 16 17 18 19 25 18 19 20 22 28 Time MIN 4 4 4 4 5 4 4 5 5 6 Fuel LB 286 298 311 328 375 314 328 342 361 415 42000 Distance NM 15 16 17 18 23 17 18 19 20 26 Time MIN 4 4 4 4 5 4 4 4 5 6 Fuel LB 269 280 293 308 352 295 308 322 339 389 40000 Distance NM 14 15 16 17 22 16 17 18 19 25 Time MIN 3 4 4 4 5 4 4 4 4 5 Fuel LB 252 263 275 289 329 277 289 302 318 364 38000 Distance NM 14 14 15 16 20 15 16 17 18 23 Time MIN 3 3 3 4 4 4 4 4 4 5 Fuel LB 236 247 257 270 307 259 271 283 297 339 36000 Distance NM 13 13 14 15 19 14 15 16 17 21 Time MIN 3 3 3 3 4 3 3 4 4 5 Fuel LB 221 230 240 253 286 242 253 264 278 316 34000 Distance NM 12 12 13 14 18 13 14 15 16 20 Time MIN 3 3 3 3 4 3 3 3 3 4 Fuel LB 206 215 224 235 266 226 236 246 259 294 32000 Distance NM 11 12 12 13 16 12 13 14 15 18 Time MIN 3 3 3 3 4 3 3 3 3 4 Fuel LB 191 199 208 218 246 210 219 228 240 272 30000 Distance NM 10 11 11 12 15 12 12 13 13 17 Time MIN 2 3 3 3 3 3 3 3 3 4 ### Page 30 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-10 Page 24 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 13000 AND 14000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 260 KIAS AT 12000 FT, MAINTAINING 260 KIAS UP TO 22800 FT AND M = 0.60 ABOVE 22800 FT. ALTERNATIVE CLIMB SCHEDULE BLEED: OPEN 13000 ft 14000 ft ISA + °C ISA + °C WEIGHT (lb) -20 -10 0 10 20 -20 -10 0 10 20 Fuel LB 435 454 475 502 592 473 495 517 547 651 50000 Distance NM 25 26 27 29 39 28 29 30 33 44 Time MIN 6 6 6 6 8 6 6 7 7 9 Fuel LB 411 429 448 473 556 447 467 488 516 610 48000 Distance NM 23 24 26 28 36 26 27 29 31 41 Time MIN 5 6 6 6 8 6 6 6 7 9 Fuel LB 387 404 422 446 521 421 440 459 486 572 46000 Distance NM 22 23 24 26 34 25 26 27 29 38 Time MIN 5 5 5 6 7 6 6 6 6 8 Fuel LB 365 381 398 420 489 396 414 433 457 536 44000 Distance NM 21 22 23 24 32 23 24 25 27 36 Time MIN 5 5 5 5 7 5 5 6 6 8 Fuel LB 343 358 374 395 458 373 390 407 430 501 42000 Distance NM 20 20 21 23 30 22 23 24 26 34 Time MIN 5 5 5 5 6 5 5 5 6 7 Fuel LB 323 337 352 371 428 350 366 382 403 469 40000 Distance NM 18 19 20 22 28 20 21 22 24 31 Time MIN 4 4 4 5 6 5 5 5 5 7 Fuel LB 303 316 330 348 400 329 343 358 378 438 38000 Distance NM 17 18 19 20 26 19 20 21 23 29 Time MIN 4 4 4 4 6 4 4 5 5 6 Fuel LB 283 296 309 325 373 308 321 335 354 408 36000 Distance NM 16 17 18 19 24 18 19 20 21 27 Time MIN 4 4 4 4 5 4 4 4 5 6 Fuel LB 265 276 288 304 348 287 300 313 330 380 34000 Distance NM 15 16 16 18 23 17 17 18 20 25 Time MIN 3 4 4 4 5 4 4 4 4 5 Fuel LB 247 257 269 283 323 268 279 292 307 353 32000 Distance NM 14 15 15 16 21 16 16 17 18 24 Time MIN 3 3 3 4 5 4 4 4 4 5 Fuel LB 229 239 249 262 299 248 259 271 285 327 30000 Distance NM 13 13 14 15 19 14 15 16 17 22 Time MIN 3 3 3 3 4 3 3 3 4 5 ### Page 31 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-10 Page 25 Code 06 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 15000 AND 16000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 260 KIAS AT 12000 FT, MAINTAINING 260 KIAS UP TO 22800 FT AND M = 0.60 ABOVE 22800 FT. ALTERNATIVE CLIMB SCHEDULE BLEED: OPEN 15000 ft 16000 ft ISA + °C ISA + °C WEIGHT (lb) -20 -10 0 10 20 -20 -10 0 10 20 Fuel LB 513 536 560 594 712 552 578 604 641 776 50000 Distance NM 31 32 34 37 49 34 36 37 40 55 Time MIN 7 7 7 8 10 8 8 8 8 11 Fuel LB 483 505 528 559 667 521 544 569 604 726 48000 Distance NM 29 30 32 34 46 32 34 35 38 52 Time MIN 7 7 7 7 10 7 7 8 8 11 Fuel LB 455 476 497 527 624 490 513 536 568 679 46000 Distance NM 27 29 30 32 43 30 32 33 36 48 Time MIN 6 6 6 7 9 7 7 7 7 10 Fuel LB 429 448 468 495 584 462 483 504 534 635 44000 Distance NM 26 27 28 30 40 28 30 31 34 45 Time MIN 6 6 6 6 8 6 6 7 7 9 Fuel LB 403 421 440 465 547 434 454 474 502 593 42000 Distance NM 24 25 26 29 38 27 28 29 32 42 Time MIN 5 6 6 6 8 6 6 6 7 9 Fuel LB 379 396 413 437 511 407 426 445 471 554 40000 Distance NM 23 24 25 27 35 25 26 27 30 39 Time MIN 5 5 5 6 7 6 6 6 6 8 Fuel LB 355 371 387 409 477 382 399 417 441 517 38000 Distance NM 21 22 23 25 33 23 24 26 28 37 Time MIN 5 5 5 5 7 5 5 5 6 8 Fuel LB 332 347 363 383 444 357 373 390 412 481 36000 Distance NM 20 21 22 23 31 22 23 24 26 34 Time MIN 4 5 5 5 6 5 5 5 5 7 Fuel LB 310 324 338 357 413 333 348 364 384 448 34000 Distance NM 19 19 20 22 28 20 21 22 24 32 Time MIN 4 4 4 5 6 5 5 5 5 6 Fuel LB 289 302 315 332 384 310 324 339 358 415 32000 Distance NM 17 18 19 20 26 19 20 21 22 29 Time MIN 4 4 4 4 5 4 4 4 5 6 Fuel LB 268 280 292 308 355 288 301 314 332 384 30000 Distance NM 16 17 17 19 24 18 18 19 21 27 Time MIN 4 4 4 4 5 4 4 4 4 6 ### Page 32 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-10 Page 26 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 17000 AND 18000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 260 KIAS AT 12000 FT, MAINTAINING 260 KIAS UP TO 22800 FT AND M = 0.60 ABOVE 22800 FT. ALTERNATIVE CLIMB SCHEDULE BLEED: OPEN 17000 ft 18000 ft ISA + °C ISA + °C WEIGHT (lb) -20 -10 0 10 20 -20 -10 0 10 20 Fuel LB 593 620 649 690 842 634 664 695 740 910 50000 Distance NM 38 39 41 45 62 41 43 45 49 69 Time MIN 8 8 9 9 12 9 9 9 10 14 Fuel LB 559 584 611 649 787 597 625 654 696 849 48000 Distance NM 35 37 39 42 58 39 40 42 46 64 Time MIN 8 8 8 9 12 8 9 9 9 13 Fuel LB 526 550 575 611 735 562 588 615 654 793 46000 Distance NM 33 35 36 39 54 36 38 40 43 60 Time MIN 7 7 8 8 11 8 8 8 9 12 Fuel LB 495 517 541 574 687 529 553 578 614 740 44000 Distance NM 31 33 34 37 50 34 36 37 41 56 Time MIN 7 7 7 8 10 7 8 8 8 11 Fuel LB 465 486 508 539 641 496 519 543 577 691 42000 Distance NM 29 31 32 35 47 32 34 35 38 52 Time MIN 6 7 7 7 9 7 7 7 8 10 Fuel LB 436 456 477 505 599 466 487 509 540 644 40000 Distance NM 27 29 30 33 44 30 31 33 36 48 Time MIN 6 6 6 7 9 6 7 7 7 10 Fuel LB 409 427 447 473 558 436 456 477 506 600 38000 Distance NM 26 27 28 30 41 28 29 31 33 45 Time MIN 6 6 6 6 8 6 6 6 7 9 Fuel LB 382 400 418 442 519 408 427 446 473 558 36000 Distance NM 24 25 26 28 38 26 27 29 31 42 Time MIN 5 5 6 6 8 6 6 6 6 8 Fuel LB 357 373 390 412 483 380 398 416 441 518 34000 Distance NM 22 23 25 26 35 24 26 27 29 39 Time MIN 5 5 5 5 7 5 5 6 6 8 Fuel LB 332 347 363 383 447 354 370 387 410 480 32000 Distance NM 21 22 23 25 32 23 24 25 27 36 Time MIN 5 5 5 5 7 5 5 5 6 7 Fuel LB 308 322 337 356 414 328 343 359 380 444 30000 Distance NM 19 20 21 23 30 21 22 23 25 33 Time MIN 4 4 4 5 6 5 5 5 5 7 ### Page 33 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-10 Page 27 Code 06 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 19000 AND 20000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 260 KIAS AT 12000 FT, MAINTAINING 260 KIAS UP TO 22800 FT AND M = 0.60 ABOVE 22800 FT. ALTERNATIVE CLIMB SCHEDULE BLEED: OPEN 19000 ft 20000 ft ISA + °C ISA + °C WEIGHT (lb) -20 -10 0 10 20 -20 -10 0 10 20 Fuel LB 676 708 741 791 980 717 751 787 841 1049 50000 Distance NM 45 47 49 54 76 48 51 53 58 83 Time MIN 10 10 10 11 15 10 10 11 12 16 Fuel LB 636 666 697 743 913 675 707 740 790 977 48000 Distance NM 42 44 46 50 71 46 48 50 55 77 Time MIN 9 9 9 10 14 10 10 10 11 15 Fuel LB 598 626 655 698 852 634 664 695 742 911 46000 Distance NM 40 41 43 47 66 43 45 47 51 72 Time MIN 8 9 9 10 13 9 9 10 10 14 Fuel LB 562 589 616 655 795 596 624 653 696 849 44000 Distance NM 37 39 41 44 61 40 42 44 48 67 Time MIN 8 8 8 9 12 8 9 9 10 13 Fuel LB 528 553 578 615 741 559 586 613 653 791 42000 Distance NM 35 36 38 42 57 38 39 41 45 62 Time MIN 7 8 8 8 11 8 8 8 9 12 Fuel LB 495 518 542 576 690 525 549 575 611 736 40000 Distance NM 33 34 36 39 53 35 37 39 42 58 Time MIN 7 7 7 8 10 7 8 8 8 11 Fuel LB 464 485 507 539 643 491 514 538 572 685 38000 Distance NM 30 32 33 36 49 33 34 36 39 54 Time MIN 7 7 7 7 10 7 7 7 8 10 Fuel LB 433 453 474 503 597 459 480 502 534 637 36000 Distance NM 28 30 31 34 46 31 32 34 37 50 Time MIN 6 6 6 7 9 7 7 7 7 10 Fuel LB 404 423 442 469 555 428 448 468 497 591 34000 Distance NM 26 28 29 32 42 29 30 31 34 46 Time MIN 6 6 6 6 8 6 6 6 7 9 Fuel LB 376 393 411 436 514 398 416 435 462 547 32000 Distance NM 25 26 27 29 39 27 28 29 32 43 Time MIN 5 5 6 6 8 6 6 6 6 8 Fuel LB 349 365 381 404 474 369 386 404 428 505 30000 Distance NM 23 24 25 27 36 25 26 27 29 39 Time MIN 5 5 5 5 7 5 5 6 6 8 ### Page 34 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-10 Page 28 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 21000 AND 22000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 260 KIAS AT 12000 FT, MAINTAINING 260 KIAS UP TO 22800 FT AND M = 0.60 ABOVE 22800 FT. ALTERNATIVE CLIMB SCHEDULE BLEED: OPEN 21000 ft 22000 ft ISA + °C ISA + °C WEIGHT (lb) -20 -10 0 10 20 -20 -10 0 10 20 Fuel LB 759 795 833 892 1121 802 841 881 945 1199 50000 Distance NM 52 55 58 63 91 56 59 62 68 99 Time MIN 11 11 12 12 17 12 12 12 13 19 Fuel LB 714 748 783 837 1043 754 790 828 887 1114 48000 Distance NM 49 51 54 59 84 53 55 58 64 92 Time MIN 10 11 11 12 16 11 11 12 12 17 Fuel LB 671 703 736 786 971 708 742 777 832 1036 46000 Distance NM 46 48 51 55 78 50 52 55 60 85 Time MIN 10 10 10 11 15 10 11 11 12 16 Fuel LB 630 660 691 737 904 665 697 730 780 964 44000 Distance NM 43 45 48 52 73 47 49 51 56 79 Time MIN 9 9 10 10 14 10 10 10 11 15 Fuel LB 591 619 648 691 842 624 653 684 731 896 42000 Distance NM 40 42 45 49 68 44 46 48 52 74 Time MIN 8 9 9 10 13 9 9 10 10 14 Fuel LB 554 580 607 647 783 584 612 641 684 833 40000 Distance NM 38 40 42 45 63 41 43 45 49 68 Time MIN 8 8 8 9 12 8 9 9 10 13 Fuel LB 519 543 568 605 728 547 572 599 639 774 38000 Distance NM 35 37 39 42 58 38 40 42 46 63 Time MIN 7 8 8 8 11 8 8 8 9 12 Fuel LB 484 507 531 564 677 510 535 560 596 719 36000 Distance NM 33 35 36 40 54 36 37 39 43 59 Time MIN 7 7 7 8 10 7 8 8 8 11 Fuel LB 452 473 495 526 627 476 498 521 555 666 34000 Distance NM 31 32 34 37 50 33 35 36 40 54 Time MIN 6 7 7 7 10 7 7 7 8 10 Fuel LB 420 439 460 488 580 442 463 485 516 616 32000 Distance NM 29 30 31 34 46 31 32 34 37 50 Time MIN 6 6 6 7 9 6 7 7 7 10 Fuel LB 389 407 426 452 536 410 429 449 477 568 30000 Distance NM 26 28 29 32 43 28 30 31 34 46 Time MIN 6 6 6 6 8 6 6 6 7 9 ### Page 35 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-10 Page 29 Code 06 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 23000 AND 24000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 260 KIAS AT 12000 FT, MAINTAINING 260 KIAS UP TO 22800 FT AND M = 0.60 ABOVE 22800 FT. ALTERNATIVE CLIMB SCHEDULE BLEED: OPEN 23000 ft 24000 ft ISA + °C ISA + °C WEIGHT (lb) -20 -10 0 10 20 -20 -10 0 10 20 Fuel LB 842 883 925 995 1275 878 921 965 1041 1347 50000 Distance NM 60 63 66 73 108 64 67 70 78 117 Time MIN 12 13 13 14 20 13 13 14 15 21 Fuel LB 791 829 869 933 1183 824 864 906 975 1247 48000 Distance NM 56 59 62 69 100 60 63 66 73 108 Time MIN 12 12 12 13 19 12 12 13 14 20 Fuel LB 743 778 815 874 1098 774 811 850 914 1156 46000 Distance NM 53 56 58 64 93 56 59 62 68 100 Time MIN 11 11 11 12 17 11 12 12 13 18 Fuel LB 697 730 765 819 1020 726 761 797 856 1073 44000 Distance NM 50 52 55 60 86 53 55 58 64 92 Time MIN 10 10 11 12 16 11 11 11 12 17 Fuel LB 653 685 717 767 948 680 713 747 801 996 42000 Distance NM 46 49 51 56 80 49 52 54 60 85 Time MIN 10 10 10 11 15 10 10 11 11 16 Fuel LB 612 641 671 718 881 637 667 699 749 924 40000 Distance NM 43 46 48 52 74 46 48 51 56 79 Time MIN 9 9 9 10 14 9 10 10 11 15 Fuel LB 572 599 628 670 818 595 624 653 699 857 38000 Distance NM 41 43 45 49 68 43 45 47 52 73 Time MIN 8 9 9 9 13 9 9 9 10 14 Fuel LB 534 560 586 625 758 556 582 610 652 795 36000 Distance NM 38 40 42 46 63 40 42 44 48 68 Time MIN 8 8 8 9 12 8 8 9 9 13 Fuel LB 498 521 546 582 702 518 542 568 606 735 34000 Distance NM 35 37 39 42 58 37 39 41 45 62 Time MIN 7 7 8 8 11 8 8 8 9 12 Fuel LB 463 484 507 540 649 481 504 528 563 679 32000 Distance NM 33 34 36 39 54 34 36 38 42 58 Time MIN 7 7 7 8 10 7 7 7 8 11 Fuel LB 429 449 470 500 598 445 467 489 521 626 30000 Distance NM 30 32 33 36 50 32 33 35 38 53 Time MIN 6 6 7 7 9 7 7 7 7 10 ### Page 36 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-10 Page 30 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 25000 AND 26000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 260 KIAS AT 12000 FT, MAINTAINING 260 KIAS UP TO 22800 FT AND M = 0.60 ABOVE 22800 FT. ALTERNATIVE CLIMB SCHEDULE BLEED: OPEN 25000 ft 26000 ft ISA + °C ISA + °C WEIGHT (lb) -19 -10 0 10 20 -18 -10 0 10 20 Fuel LB 919 959 1006 1086 1418 961 999 1048 1132 1488 50000 Distance NM 68 71 75 83 125 72 75 79 88 134 Time MIN 14 14 14 16 23 14 15 15 16 24 Fuel LB 862 900 944 1017 1311 901 936 982 1059 1374 48000 Distance NM 64 67 70 78 116 68 70 74 82 123 Time MIN 13 13 13 15 21 13 14 14 15 22 Fuel LB 809 844 885 952 1214 845 878 920 991 1271 46000 Distance NM 60 62 65 72 107 63 66 69 77 114 Time MIN 12 12 13 14 19 13 13 13 14 21 Fuel LB 758 791 829 891 1125 792 822 862 927 1176 44000 Distance NM 56 58 61 68 99 59 62 65 72 105 Time MIN 11 11 12 13 18 12 12 12 13 19 Fuel LB 710 741 777 834 1044 741 770 807 867 1090 42000 Distance NM 52 55 57 63 91 55 58 60 67 97 Time MIN 10 11 11 12 17 11 11 12 13 18 Fuel LB 665 694 727 779 968 693 720 755 810 1009 40000 Distance NM 49 51 53 59 84 52 54 56 62 89 Time MIN 10 10 10 11 15 10 11 11 12 16 Fuel LB 621 648 679 727 897 648 673 705 755 935 38000 Distance NM 45 48 50 55 78 48 50 53 58 83 Time MIN 9 9 10 10 14 10 10 10 11 15 Fuel LB 580 605 634 678 830 604 627 657 704 865 36000 Distance NM 42 44 46 51 72 45 47 49 54 76 Time MIN 9 9 9 10 13 9 9 9 10 14 Fuel LB 540 563 590 631 768 562 584 612 654 800 34000 Distance NM 39 41 43 47 66 42 43 46 50 70 Time MIN 8 8 8 9 12 8 9 9 9 13 Fuel LB 501 523 548 585 709 522 542 568 607 738 32000 Distance NM 37 38 40 44 61 39 40 42 46 65 Time MIN 7 8 8 8 11 8 8 8 9 12 Fuel LB 464 484 507 541 653 483 502 526 561 679 30000 Distance NM 34 35 37 41 56 36 37 39 43 59 Time MIN 7 7 7 8 10 7 7 8 8 11 ### Page 37 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-10 Page 31 Code 06 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 27000 AND 28000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 260 KIAS AT 12000 FT, MAINTAINING 260 KIAS UP TO 22800 FT AND M = 0.60 ABOVE 22800 FT. ALTERNATIVE CLIMB SCHEDULE BLEED: OPEN 27000 ft 28000 ft ISA + °C ISA + °C WEIGHT (lb) -17 -10 0 10 20 -16 -10 0 10 20 Fuel LB 1005 1039 1090 1178 1556 1050 1081 1134 1225 1624 50000 Distance NM 77 80 84 93 143 82 84 89 98 151 Time MIN 15 15 16 17 26 16 16 17 18 27 Fuel LB 941 973 1021 1101 1435 983 1012 1061 1144 1495 48000 Distance NM 72 74 78 87 131 76 79 83 92 139 Time MIN 14 14 15 16 24 15 15 16 17 25 Fuel LB 882 912 956 1030 1325 920 947 993 1069 1379 46000 Distance NM 67 70 73 81 120 71 73 77 85 127 Time MIN 13 13 14 15 22 14 14 15 16 23 Fuel LB 826 854 895 963 1226 861 886 929 999 1274 44000 Distance NM 63 65 68 75 111 67 69 72 80 117 Time MIN 12 13 13 14 20 13 13 14 15 21 Fuel LB 773 799 837 899 1134 805 828 869 933 1178 42000 Distance NM 59 61 64 70 102 62 64 67 74 108 Time MIN 12 12 12 13 18 12 12 13 14 19 Fuel LB 722 747 783 840 1050 752 774 811 870 1089 40000 Distance NM 55 57 59 66 94 58 60 63 69 99 Time MIN 11 11 11 12 17 11 12 12 13 18 Fuel LB 674 697 731 783 971 702 722 757 811 1007 38000 Distance NM 51 53 55 61 87 54 56 58 64 92 Time MIN 10 10 11 11 16 11 11 11 12 17 Fuel LB 629 650 681 729 898 654 673 705 755 931 36000 Distance NM 47 49 52 57 80 50 52 54 60 85 Time MIN 9 10 10 11 15 10 10 10 11 15 Fuel LB 585 605 634 678 830 608 626 656 701 860 34000 Distance NM 44 46 48 53 74 47 48 50 55 78 Time MIN 9 9 9 10 13 9 9 10 10 14 Fuel LB 543 561 588 629 765 564 581 609 650 792 32000 Distance NM 41 42 44 49 68 43 44 47 51 72 Time MIN 8 8 9 9 12 8 9 9 10 13 Fuel LB 503 520 544 581 704 522 537 563 601 729 30000 Distance NM 38 39 41 45 63 40 41 43 47 66 Time MIN 8 8 8 8 11 8 8 8 9 12 ### Page 38 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-10 Page 32 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 29000 AND 30000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 260 KIAS AT 12000 FT, MAINTAINING 260 KIAS UP TO 22800 FT AND M = 0.60 ABOVE 22800 FT. ALTERNATIVE CLIMB SCHEDULE BLEED: OPEN 29000 ft 30000 ft ISA + °C ISA + °C WEIGHT (lb) -15 -10 0 10 20 -14 -10 0 10 20 Fuel LB 1097 1124 1180 1274 1692 1144 1167 1225 1324 1762 50000 Distance NM 87 89 94 104 160 92 94 99 110 169 Time MIN 17 17 18 19 28 18 18 18 20 30 Fuel LB 1025 1051 1103 1189 1555 1068 1090 1144 1234 1617 48000 Distance NM 81 83 87 97 146 86 88 92 102 155 Time MIN 16 16 16 18 26 17 17 17 19 27 Fuel LB 959 982 1031 1109 1433 998 1018 1068 1150 1488 46000 Distance NM 76 78 82 90 134 80 82 86 95 142 Time MIN 15 15 15 17 24 15 16 16 17 25 Fuel LB 896 918 963 1035 1322 932 951 997 1073 1371 44000 Distance NM 71 72 76 84 123 75 76 80 88 130 Time MIN 14 14 14 15 22 14 15 15 16 23 Fuel LB 838 858 900 966 1221 871 888 931 1000 1265 42000 Distance NM 66 67 71 78 114 69 71 75 82 119 Time MIN 13 13 13 14 20 13 14 14 15 21 Fuel LB 782 801 840 901 1128 812 828 869 932 1168 40000 Distance NM 61 63 66 73 105 65 66 69 76 110 Time MIN 12 12 12 13 19 12 13 13 14 20 Fuel LB 730 747 783 839 1043 757 772 810 867 1078 38000 Distance NM 57 58 61 67 96 60 61 64 71 101 Time MIN 11 11 12 12 17 12 12 12 13 18 Fuel LB 679 696 730 781 963 705 719 753 806 995 36000 Distance NM 53 54 57 63 89 56 57 60 66 93 Time MIN 10 10 11 12 16 11 11 11 12 17 Fuel LB 632 647 678 725 889 655 668 700 749 918 34000 Distance NM 49 50 53 58 82 52 53 56 61 86 Time MIN 10 10 10 11 15 10 10 10 11 15 Fuel LB 586 600 629 672 819 607 619 649 693 845 32000 Distance NM 46 47 49 54 75 48 49 51 56 79 Time MIN 9 9 9 10 14 9 9 10 10 14 Fuel LB 542 555 582 621 753 561 572 600 640 777 30000 Distance NM 42 43 45 50 69 44 45 47 52 72 Time MIN 8 8 9 9 12 9 9 9 10 13 ### Page 39 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-10 Page 33 Code 06 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 31000 AND 32000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 260 KIAS AT 12000 FT, MAINTAINING 260 KIAS UP TO 22800 FT AND M = 0.60 ABOVE 22800 FT. ALTERNATIVE CLIMB SCHEDULE BLEED: OPEN 31000 ft 32000 ft ISA + °C ISA + °C WEIGHT (lb) -13 -5 0 10 20 -12 -5 0 10 20 Fuel LB 1192 1239 1270 1375 1837 1240 1283 1315 1428 1916 50000 Distance NM 98 102 105 116 179 103 107 110 123 191 Time MIN 19 19 19 21 32 20 20 20 22 33 Fuel LB 1112 1156 1184 1279 1682 1155 1195 1225 1326 1750 48000 Distance NM 91 95 97 108 163 96 99 102 114 173 Time MIN 17 18 18 20 29 18 19 19 21 30 Fuel LB 1038 1079 1105 1191 1544 1077 1114 1142 1234 1603 46000 Distance NM 85 88 90 100 149 89 92 95 105 158 Time MIN 16 17 17 18 26 17 17 18 19 28 Fuel LB 968 1006 1031 1110 1421 1004 1039 1064 1148 1473 44000 Distance NM 79 82 84 93 137 83 86 88 98 144 Time MIN 15 15 16 17 24 16 16 16 18 25 Fuel LB 904 939 962 1034 1310 936 968 992 1068 1355 42000 Distance NM 73 76 78 86 125 77 80 82 90 132 Time MIN 14 14 15 16 22 15 15 15 16 23 Fuel LB 843 875 897 963 1208 873 902 924 994 1249 40000 Distance NM 68 71 73 80 115 72 74 76 84 121 Time MIN 13 13 14 15 20 14 14 14 15 21 Fuel LB 785 815 835 896 1114 812 840 860 924 1151 38000 Distance NM 63 66 68 74 106 66 69 70 78 111 Time MIN 12 12 13 14 19 13 13 13 14 20 Fuel LB 730 759 777 832 1028 755 781 800 858 1060 36000 Distance NM 59 61 63 69 97 62 64 65 72 102 Time MIN 11 12 12 13 17 12 12 12 13 18 Fuel LB 678 704 721 772 947 701 725 742 795 976 34000 Distance NM 54 57 58 64 89 57 59 61 67 94 Time MIN 10 11 11 12 16 11 11 11 12 17 Fuel LB 628 653 668 715 871 650 671 688 736 898 32000 Distance NM 50 52 54 59 82 53 55 56 61 86 Time MIN 10 10 10 11 15 10 10 10 11 15 Fuel LB 581 603 618 660 800 600 620 635 679 824 30000 Distance NM 46 48 49 54 75 49 50 52 57 79 Time MIN 9 9 9 10 13 9 10 10 10 14 ### Page 40 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-10 Page 34 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 33000 AND 34000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 260 KIAS AT 12000 FT, MAINTAINING 260 KIAS UP TO 22800 FT AND M = 0.60 ABOVE 22800 FT. ALTERNATIVE CLIMB SCHEDULE BLEED: OPEN 33000 ft 34000 ft ISA + °C ISA + °C WEIGHT (lb) -10 -5 0 10 20 -9 -5 0 10 20 Fuel LB 1296 1328 1361 1482 2001 1351 1377 1411 1541 2090 50000 Distance NM 110 112 115 130 203 116 119 122 137 216 Time MIN 21 21 21 23 35 22 22 22 25 38 Fuel LB 1206 1236 1266 1375 1821 1254 1279 1311 1426 1896 48000 Distance NM 102 104 107 120 183 107 110 112 126 194 Time MIN 19 19 20 22 32 20 20 21 23 34 Fuel LB 1123 1151 1179 1277 1665 1166 1189 1218 1322 1728 46000 Distance NM 94 97 99 111 166 100 101 104 117 175 Time MIN 18 18 18 20 29 19 19 19 21 31 Fuel LB 1046 1072 1098 1187 1526 1085 1106 1133 1227 1581 44000 Distance NM 88 90 92 102 152 92 94 96 108 159 Time MIN 17 17 17 19 27 17 18 18 19 28 Fuel LB 975 998 1023 1103 1402 1010 1029 1055 1139 1450 42000 Distance NM 81 83 85 95 139 85 87 89 100 145 Time MIN 15 16 16 17 24 16 16 17 18 26 Fuel LB 907 929 952 1025 1290 939 958 981 1057 1332 40000 Distance NM 75 77 79 88 127 79 81 83 92 133 Time MIN 14 14 15 16 22 15 15 15 17 23 Fuel LB 844 865 886 952 1188 873 890 912 981 1224 38000 Distance NM 70 72 74 81 116 73 75 77 85 122 Time MIN 13 13 14 15 21 14 14 14 15 21 Fuel LB 785 804 823 884 1093 811 827 847 910 1126 36000 Distance NM 65 66 68 75 107 68 69 71 79 111 Time MIN 12 12 13 14 19 13 13 13 14 20 Fuel LB 728 745 763 819 1006 752 766 785 843 1035 34000 Distance NM 60 62 63 70 98 63 64 66 73 102 Time MIN 11 12 12 13 17 12 12 12 13 18 Fuel LB 674 690 707 757 924 696 709 726 779 951 32000 Distance NM 55 57 58 64 90 58 59 61 67 93 Time MIN 11 11 11 12 16 11 11 11 12 17 Fuel LB 622 637 653 699 848 642 655 670 718 871 30000 Distance NM 51 52 54 59 82 53 54 56 62 85 Time MIN 10 10 10 11 15 10 10 10 11 15 ### Page 41 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-10 Page 35 Code 06 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 35000 AND 36000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 260 KIAS AT 12000 FT, MAINTAINING 260 KIAS UP TO 22800 FT AND M = 0.60 ABOVE 22800 FT. ALTERNATIVE CLIMB SCHEDULE BLEED: OPEN 35000 ft 36000 ft ISA + °C ISA + °C WEIGHT (lb) -8 -5 0 10 20 -7 -5 0 10 20 Fuel LB 1410 1431 1466 1603 2187 1477 1491 1528 1669 2292 50000 Distance NM 124 126 129 146 230 133 134 137 155 246 Time MIN 23 23 24 26 40 25 25 25 28 43 Fuel LB 1307 1326 1359 1480 1975 1364 1377 1411 1537 2059 48000 Distance NM 114 116 119 133 206 122 123 126 141 219 Time MIN 21 21 22 24 36 23 23 23 25 38 Fuel LB 1213 1230 1261 1369 1794 1263 1275 1306 1418 1864 46000 Distance NM 105 107 110 123 185 112 113 116 130 196 Time MIN 20 20 20 22 32 21 21 21 23 34 Fuel LB 1127 1143 1171 1268 1637 1171 1182 1211 1311 1696 44000 Distance NM 97 99 101 113 168 103 104 107 119 177 Time MIN 18 18 19 20 29 19 19 20 21 31 Fuel LB 1047 1062 1088 1176 1499 1086 1097 1123 1214 1549 42000 Distance NM 90 91 94 104 153 95 96 99 110 160 Time MIN 17 17 17 19 27 18 18 18 20 28 Fuel LB 973 987 1011 1090 1374 1008 1018 1042 1124 1418 40000 Distance NM 83 85 87 96 139 88 89 91 101 146 Time MIN 16 16 16 17 24 16 17 17 18 26 Fuel LB 904 917 939 1011 1262 935 944 967 1041 1300 38000 Distance NM 77 78 80 89 127 81 82 84 93 133 Time MIN 15 15 15 16 22 15 15 15 17 23 Fuel LB 838 850 871 937 1159 867 875 896 963 1193 36000 Distance NM 71 72 74 82 116 75 76 78 86 121 Time MIN 13 14 14 15 20 14 14 14 15 21 Fuel LB 777 788 807 867 1065 802 810 830 891 1094 34000 Distance NM 66 67 69 76 106 69 70 72 79 111 Time MIN 12 13 13 14 19 13 13 13 14 19 Fuel LB 718 729 746 800 977 742 749 767 822 1003 32000 Distance NM 61 62 63 70 97 64 64 66 73 101 Time MIN 11 12 12 13 17 12 12 12 13 18 Fuel LB 663 672 688 738 895 684 690 707 757 918 30000 Distance NM 56 57 58 64 89 59 59 61 67 92 Time MIN 11 11 11 12 16 11 11 11 12 16 ### Page 42 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-10 Page 36 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 37000 AND 38000 FT SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 260 KIAS AT 12000 FT, MAINTAINING 260 KIAS UP TO 22800 FT AND M = 0.60 ABOVE 22800 FT. ALTERNATIVE CLIMB SCHEDULE BLEED: OPEN 37000 ft 38000 ft ISA + °C ISA + °C WEIGHT (lb) -8 -5 0 10 20 -8 -5 0 10 20 Fuel LB 1542 1564 1602 1749 - 1638 1661 1701 - - 50000 Distance NM 142 144 148 166 - 156 159 162 - - Time MIN 26 26 27 29 - 29 29 29 - - Fuel LB 1417 1438 1473 1602 2163 1492 1514 1550 1687 - 48000 Distance NM 129 131 134 151 235 141 143 146 163 - Time MIN 24 24 25 27 41 26 26 27 29 - Fuel LB 1307 1326 1359 1474 1946 1368 1388 1422 1542 - 46000 Distance NM 118 120 123 137 209 128 129 132 148 - Time MIN 22 22 22 25 36 24 24 24 26 - Fuel LB 1208 1226 1256 1359 1763 1259 1278 1309 1416 1852 44000 Distance NM 109 110 113 126 187 116 118 121 134 202 Time MIN 20 20 21 22 33 22 22 22 24 35 Fuel LB 1119 1135 1163 1255 1605 1162 1179 1207 1304 1676 42000 Distance NM 100 102 104 116 169 107 108 111 123 181 Time MIN 19 19 19 21 29 20 20 20 22 31 Fuel LB 1036 1051 1077 1161 1465 1074 1089 1116 1202 1524 40000 Distance NM 92 94 96 106 153 98 99 102 112 163 Time MIN 17 17 18 19 27 18 18 19 20 28 Fuel LB 960 974 997 1073 1341 992 1007 1031 1109 1390 38000 Distance NM 85 86 88 98 139 90 91 93 103 148 Time MIN 16 16 16 18 24 17 17 17 18 26 Fuel LB 889 902 923 992 1228 917 931 953 1024 1270 36000 Distance NM 78 80 82 90 127 83 84 86 95 134 Time MIN 15 15 15 16 22 15 16 16 17 23 Fuel LB 822 834 854 916 1126 847 859 880 944 1161 34000 Distance NM 72 73 75 83 116 76 77 79 87 122 Time MIN 14 14 14 15 20 14 14 15 16 21 Fuel LB 759 770 788 845 1031 781 792 812 870 1062 32000 Distance NM 66 67 69 76 106 70 71 73 80 111 Time MIN 12 13 13 14 19 13 13 13 14 19 Fuel LB 699 709 726 778 943 719 729 747 800 970 30000 Distance NM 61 62 63 70 96 64 65 66 73 101 Time MIN 11 12 12 13 17 12 12 12 13 18 ### Page 43 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-10 Page 37 Code 06 AOM-135/1542 CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: SEA LEVEL TO 39000 SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 260 KIAS AT 12000 FT, MAINTAINING 260 KIAS UP TO 22800 FT AND M = 0.60 ABOVE 22800 FT. ALTERNATIVE CLIMB SCHEDULE BLEED: OPEN 39000 ft ISA + °C WEIGHT(lb) -8 -5 0 10 20 Fuel LB - - - - - 50000 Distance NM - - - - - Time MIN - - - - - Fuel LB - - - - - 48000 Distance NM - - - - - Time MIN - - - - - Fuel LB 1444 1465 1500 1630 - 46000 Distance NM 139 141 145 162 - Time MIN 26 26 26 29 - Fuel LB 1320 1339 1371 1485 - 44000 Distance NM 126 128 131 145 - Time MIN 23 23 24 26 - Fuel LB 1212 1229 1259 1360 1771 42000 Distance NM 114 116 119 132 198 Time MIN 21 21 22 23 34 Fuel LB 1116 1132 1159 1250 1596 40000 Distance NM 104 106 108 120 176 Time MIN 19 20 20 21 31 Fuel LB 1028 1043 1068 1150 1448 38000 Distance NM 96 97 99 110 158 Time MIN 18 18 18 20 27 Fuel LB 948 962 985 1059 1318 36000 Distance NM 88 89 91 100 143 Time MIN 16 16 17 18 25 Fuel LB 874 887 908 975 1201 34000 Distance NM 80 81 83 92 129 Time MIN 15 15 15 16 23 Fuel LB 805 817 836 896 1096 32000 Distance NM 73 75 76 84 117 Time MIN 14 14 14 15 20 Fuel LB 740 751 769 823 999 30000 Distance NM 67 68 70 77 106 Time MIN 13 13 13 14 19 ### Page 44 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-10 Page 38 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 INTENTIONALLY BLANK ### Page 45 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-15 Page 1 Code 06 AOM-135/1542 CRUISE MANEUVER CAPABILITY NOTE: The recommended cruise altit ude must ensure a maneuver load factor of 1.3 g before buffet onset. ### Page 46 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-15 Page 2 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 1.1 1.2 20000 ft 25000 30000 ft 35000 ft 39000 41000 30900 lb 35300 lb 39700 lb 44100 lb 1.0 3.02.0 4.0 MACH LOAD FACTOR 135BJFAA004 - 08MAY2010 26500 lb 53600 lb 48500 lb ### Page 47 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-15 Page 3 Code 06 AOM-135/1542 CRUISE TABLES The long range cruise and maximum speed cruise tables show N1, fuel flow, indicated airspeed, true airspeed, indicated Mach number, buffet margin and specific range. Data are presented for various weights and pressure altitudes. In the long range cruise schedule, all engines operating or one engine inoperative, the airplane is flown at a speed corresponding to a specific range equal to 99% of ma ximum specific range. It is used when range is the principal factor. In the maximum speed schedule, the airplane is flown in a speed resulting from maximum cruise power setting. It is used when minimum flight time is desired. Thrust selection in cruise condition is adjusted to CRZ mode. The climb to cruise transition should be made as follows: − After reaching the cruise level, allow the airplane to accelerate past 0.60M, before selecting cruise mode. − When in cruise mode, adjust thrust to keep N1 or cruise speed constant (whichever occurs first). The associated conditions are: − Flaps.....................................UP − Gear .....................................UP − Bleeds ..................................OPEN − Anti-Ice .................................OFF ### Page 48 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-15 Page 4 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: 5000 FT TO 17000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITIONS ALTITUDE WEIGHT (lb) 5000 10000 11000 12000 13000 14000 15000 16000 17000 N1 % 65.8 70.4 71.0 71.5 72.1 72.7 73.3 73.9 74.5 FF lb/H/ENG 1272 1281 1268 1257 1247 1237 1228 1220 1212 IAS KT 251 259 258 257 256 255 254 253 252 TAS KT 269 299 302 305 309 312 316 320 324 Mach 0.414 0.468 0.475 0. 482 0.489 0.496 0.504 0.512 0.521 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.54 50000 SR NM/lb 0.106 0.117 0.119 0. 121 0.124 0.126 0.129 0.131 0.133 N1 % 65.4 69.7 70.2 70.7 71.3 71.8 72.4 73.0 73.6 FF lb/H/ENG 1255 1241 1229 1215 1204 1194 1184 1175 1167 IAS KT 251 255 254 253 251 250 250 249 248 TAS KT 269 294 298 300 304 307 311 314 318 Mach 0.414 0.461 0.468 0. 474 0.481 0.488 0.496 0.503 0.511 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 48000 SR NM/lb 0.107 0.119 0.121 0. 124 0.126 0.129 0.131 0.134 0.136 N1 % 65.0 68.9 69.4 69.9 70.4 71.0 71.6 72.1 72.7 FF lb/H/ENG 1239 1197 1185 1174 1163 1153 1144 1132 1123 IAS KT 251 250 249 248 248 247 246 244 243 TAS KT 269 289 292 296 299 302 306 309 312 Mach 0.414 0.453 0.459 0. 466 0.474 0.481 0.488 0.495 0.503 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 46000 SR NM/lb 0.109 0.121 0.123 0. 126 0.128 0.131 0.134 0.136 0.139 N1 % 64.7 68.0 68.5 69.0 69.5 70.1 70.7 71.2 71.8 FF lb/H/ENG 1223 1155 1143 1131 1120 1109 1100 1090 1082 IAS KT 251 246 245 244 243 242 241 240 239 TAS KT 269 284 287 290 293 297 300 304 307 Mach 0.414 0.445 0.451 0. 458 0.465 0.472 0.479 0.487 0.494 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 44000 SR NM/lb 0.110 0.123 0.126 0. 128 0.131 0.134 0.136 0.139 0.142 N1 % 64.3 67.1 67.6 68.1 68.6 69.2 69.7 70.3 70.9 FF lb/H/ENG 1189 1118 1102 1089 1078 1067 1056 1047 1038 IAS KT 248 242 240 239 238 237 236 235 234 TAS KT 266 280 282 285 288 291 294 298 301 Mach 0.409 0.438 0.443 0. 450 0.456 0.463 0.470 0.477 0.485 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 42000 SR NM/lb 0.112 0.125 0.128 0. 131 0.134 0.136 0.139 0.142 0.145 ### Page 49 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-15 Page 5 Code 06 AOM-135/1542 LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: 5000 FT TO 17000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITIONS ALTITUDE WEIGHT (lb) 5000 10000 11000 12000 13000 14000 15000 16000 17000 N1 % 63.2 66.1 66.7 67.2 67.8 68.3 68.8 69.3 69.9 FF lb/H/ENG 1149 1075 1063 1051 1039 1026 1015 1005 995 IAS KT 243 237 236 235 234 233 232 231 230 TAS KT 261 274 277 280 283 286 289 292 295 Mach 0.401 0.429 0.436 0. 442 0.448 0.454 0.461 0.468 0.475 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 40000 SR NM/lb 0.114 0.127 0.130 0. 133 0.136 0.139 0.142 0.145 0.148 N1 % 62.1 65.0 65.6 66.2 66.8 67.3 67.9 68.4 68.9 FF lb/H/ENG 1110 1034 1021 1009 997 986 975 965 954 IAS KT 239 232 231 230 229 228 227 226 225 TAS KT 256 269 271 274 277 280 283 287 289 Mach 0.394 0.421 0.427 0. 433 0.439 0.446 0.452 0.459 0.466 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 38000 SR NM/lb 0.115 0.130 0.133 0. 136 0.139 0.142 0.145 0.148 0.152 N1 % 61.1 63.9 64.5 65.1 65.7 66.2 66.8 67.4 67.9 FF lb/H/ENG 1072 994 980 968 956 944 934 923 913 IAS KT 234 228 226 225 224 223 222 221 220 TAS KT 252 263 266 268 271 274 277 280 283 Mach 0.387 0.412 0.418 0. 424 0.430 0.436 0.443 0.449 0.456 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 36000 SR NM/lb 0.117 0.132 0.136 0. 139 0.142 0.145 0.149 0.152 0.155 N1 % 59.9 62.8 63.4 63.9 64.5 65.1 65.7 66.3 66.8 FF lb/H/ENG 1032 955 941 928 915 903 892 882 872 IAS KT 229 223 222 220 219 218 217 216 215 TAS KT 246 258 260 263 265 268 271 274 277 Mach 0.379 0.404 0.409 0. 415 0.421 0.427 0.433 0.439 0.446 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 34000 SR NM/lb 0.119 0.135 0.138 0. 142 0.145 0.148 0.152 0.155 0.159 N1 % 58.8 61.6 62.2 62.7 63.3 63.9 64.5 65.0 65.6 FF lb/H/ENG 993 917 903 888 876 864 852 841 831 IAS KT 224 218 217 216 214 213 212 211 210 TAS KT 241 252 255 257 259 262 265 268 271 Mach 0.371 0.396 0.401 0. 406 0.411 0.417 0.423 0.429 0.436 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 32000 SR NM/lb 0.121 0.138 0.141 0. 145 0.148 0.152 0.155 0.159 0.163 ### Page 50 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-15 Page 6 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: 18000 FT TO 26000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITIONS ALTITUDE WEIGHT (lb) 18000 19000 20000 21000 22000 23000 24000 25000 26000 N1 % 75.2 75.9 76.6 77.4 78.1 78.9 79.7 80.4 81.0 FF lb/H/ENG 1205 1199 1193 1187 1183 1179 1175 1173 1171 IAS KT 251 251 250 249 248 248 247 246 245 TAS KT 328 332 336 340 344 349 353 358 363 Mach 0.529 0.538 0.547 0. 556 0.565 0.575 0.584 0.595 0.605 BM G 2.50 2.46 2.41 2.37 2.32 2.27 2.22 2.17 2.12 50000 SR NM/lb 0.136 0.138 0.141 0. 143 0.146 0.148 0.150 0.153 0.155 N1 % 74.3 74.9 75.6 76.4 77.1 77.9 78.6 79.5 80.2 FF lb/H/ENG 1159 1153 1147 1141 1136 1132 1128 1125 1123 IAS KT 247 246 245 245 244 243 242 242 241 TAS KT 322 326 330 334 338 343 347 352 357 Mach 0.520 0.528 0.537 0. 546 0.555 0.565 0.574 0.584 0.595 BM G 2.53 2.49 2.45 2.41 2.36 2.31 2.26 2.22 2.16 48000 SR NM/lb 0.139 0.141 0.144 0. 146 0.149 0.151 0.154 0.156 0.159 N1 % 73.3 74.0 74.6 75.4 76.1 76.9 77.6 78.4 79.2 FF lb/H/ENG 1115 1108 1101 1095 1090 1085 1081 1078 1077 IAS KT 242 242 241 240 239 238 238 237 237 TAS KT 316 320 324 328 332 337 341 345 351 Mach 0.511 0.519 0.527 0. 536 0.545 0.555 0.564 0.574 0.585 BM G 2.56 2.53 2.49 2.44 2.40 2.36 2.31 2.26 2.21 46000 SR NM/lb 0.142 0.144 0.147 0. 150 0.152 0.155 0.158 0.160 0.163 N1 % 72.4 73.0 73.7 74.4 75.1 75.8 76.6 77.3 78.1 FF lb/H/ENG 1073 1066 1059 1053 1047 1040 1036 1031 1029 IAS KT 238 237 237 236 235 234 233 232 232 TAS KT 311 315 319 323 327 330 335 339 344 Mach 0.502 0.510 0.518 0. 527 0.536 0.544 0.554 0.563 0.574 BM G 2.56 2.56 2.53 2.49 2.45 2.40 2.35 2.31 2.26 44000 SR NM/lb 0.145 0.148 0.150 0. 153 0.156 0.159 0.162 0.164 0.167 N1 % 71.4 72.1 72.7 73.3 74.0 74.7 75.5 76.2 77.0 FF lb/H/ENG 1030 1022 1014 1007 1001 995 990 986 982 IAS KT 234 233 232 231 230 229 229 228 227 TAS KT 305 309 312 316 320 324 328 333 337 Mach 0.492 0.500 0.508 0. 517 0.525 0.534 0.543 0.553 0.562 BM G 2.56 2.56 2.56 2.53 2.49 2.44 2.40 2.35 2.31 42000 SR NM/lb 0.148 0.151 0.154 0. 157 0.160 0.163 0.166 0.169 0.172 ### Page 51 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-15 Page 7 Code 06 AOM-135/1542 LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: 18000 FT TO 26000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITIONS ALTITUDE WEIGHT (lb) 18000 19000 20000 21000 22000 23000 24000 25000 26000 N1 % 70.5 71.0 71.6 72.3 72.9 73.6 74.3 75.1 75.8 FF lb/H/ENG 986 978 971 964 957 951 945 941 936 IAS KT 229 228 227 226 225 225 224 223 222 TAS KT 299 302 306 310 314 318 322 326 330 Mach 0.483 0.490 0.498 0. 507 0.515 0.523 0.532 0.542 0.551 BM G 2.56 2.56 2.56 2.56 2.53 2.49 2.45 2.40 2.35 40000 SR NM/lb 0.151 0.155 0.158 0. 161 0.164 0.167 0.170 0.173 0.176 N1 % 69.4 70.0 70.6 71.2 71.8 72.5 73.2 73.9 74.6 FF lb/H/ENG 945 936 928 920 913 907 901 896 891 IAS KT 224 223 222 221 221 220 219 218 217 TAS KT 293 296 300 303 307 311 315 319 323 Mach 0.473 0.480 0.488 0. 496 0.504 0.513 0.521 0.530 0.539 BM G 2.56 2.56 2.56 2.56 2.56 2.54 2.49 2.45 2.40 38000 SR NM/lb 0.155 0.158 0.162 0. 165 0.168 0.171 0.175 0.178 0.181 N1 % 68.4 69.0 69.6 70.1 70.7 71.3 72.0 72.7 73.4 FF lb/H/ENG 904 895 887 879 872 864 858 853 846 IAS KT 219 218 218 217 216 215 214 213 212 TAS KT 287 290 294 297 301 304 308 312 316 Mach 0.463 0.471 0.478 0. 486 0.494 0.501 0.510 0.519 0.527 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.54 2.50 2.45 36000 SR NM/lb 0.159 0.162 0.166 0. 169 0.172 0.176 0.180 0.183 0.187 N1 % 67.3 67.9 68.4 69.0 69.6 70.2 70.8 71.5 72.1 FF lb/H/ENG 862 853 844 836 829 822 815 809 803 IAS KT 214 213 212 211 211 210 209 208 207 TAS KT 280 283 287 290 294 297 301 305 308 Mach 0.453 0.460 0.467 0. 474 0.482 0.490 0.498 0.507 0.515 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.55 2.50 34000 SR NM/lb 0.163 0.166 0.170 0. 173 0.177 0.181 0.185 0.188 0.192 N1 % 66.2 66.7 67.3 67.8 68.4 69.0 69.5 70.2 70.8 FF lb/H/ENG 821 812 803 794 786 779 772 766 760 IAS KT 209 208 207 206 205 204 204 203 202 TAS KT 274 277 280 283 286 290 293 297 301 Mach 0.442 0.449 0.456 0. 463 0.470 0.478 0.486 0.494 0.503 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 32000 SR NM/lb 0.167 0.170 0.174 0. 178 0.182 0.186 0.190 0.194 0.198 ### Page 52 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-15 Page 8 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: 27000 FT TO 35000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITIONS ALTITUDE WEIGHT (lb) 27000 28000 29000 30000 31000 32000 33000 34000 35000 N1 % 81.7 82.4 83.0 83.7 84.4 85.1 85.9 86.7 87.9 FF lb/H/ENG 1170 1170 1170 1172 1173 1176 1182 1185 1183 IAS KT 245 244 244 243 242 242 242 241 239 TAS KT 368 373 378 384 389 395 401 407 411 Mach 0.616 0.627 0.639 0. 651 0.663 0.676 0.690 0.703 0.712 BM G 2.06 2.01 1.95 1.89 1.82 1.76 1.69 1.62 1.54 50000 SR NM/lb 0.157 0.159 0.162 0. 164 0.166 0.168 0.170 0.172 0.174 N1 % 80.8 81.5 82.1 82.8 83.5 84.2 85.0 85.7 86.6 FF lb/H/ENG 1121 1120 1120 1121 1122 1124 1129 1131 1133 IAS KT 240 240 239 239 238 238 237 237 236 TAS KT 361 366 372 377 382 388 394 400 405 Mach 0.605 0.617 0.628 0. 640 0.651 0.664 0.678 0.690 0.702 BM G 2.11 2.06 2.00 1.94 1.88 1.82 1.75 1.68 1.61 48000 SR NM/lb 0.161 0.164 0.166 0. 168 0.170 0.173 0.175 0.177 0.179 N1 % 79.9 80.6 81.2 81.9 82.6 83.3 84.0 84.7 85.5 FF lb/H/ENG 1073 1072 1071 1071 1071 1073 1077 1078 1081 IAS KT 236 235 235 234 233 233 233 232 231 TAS KT 355 360 365 370 375 381 387 392 398 Mach 0.595 0.606 0.617 0. 628 0.639 0.652 0.665 0.678 0.691 BM G 2.16 2.11 2.05 2.00 1.94 1.87 1.81 1.74 1.67 46000 SR NM/lb 0.165 0.168 0.170 0. 173 0.175 0.178 0.180 0.182 0.184 N1 % 78.9 79.6 80.3 80.9 81.6 82.3 83.0 83.7 84.4 FF lb/H/ENG 1027 1025 1023 1022 1021 1022 1025 1026 1028 IAS KT 231 231 230 229 229 228 228 227 227 TAS KT 349 354 358 363 368 374 380 385 390 Mach 0.584 0.595 0.605 0. 616 0.627 0.639 0.653 0.665 0.677 BM G 2.21 2.16 2.11 2.05 1.99 1.93 1.87 1.81 1.74 44000 SR NM/lb 0.170 0.172 0.175 0. 178 0.180 0.183 0.185 0.188 0.190 N1 % 77.8 78.6 79.3 79.9 80.6 81.3 82.0 82.7 83.4 FF lb/H/ENG 979 977 976 974 972 972 974 975 976 IAS KT 227 226 226 225 224 223 223 223 222 TAS KT 342 346 352 356 361 366 372 377 383 Mach 0.572 0.583 0.594 0. 605 0.615 0.627 0.640 0.652 0.664 BM G 2.26 2.21 2.16 2.11 2.05 1.99 1.93 1.87 1.80 42000 SR NM/lb 0.174 0.177 0.180 0. 183 0.186 0.188 0.191 0.194 0.196 ### Page 53 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-15 Page 9 Code 06 AOM-135/1542 LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: 27000 FT TO 35000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITIONS ALTITUDE WEIGHT (lb) 27000 28000 29000 30000 31000 32000 33000 34000 35000 N1 % 76.6 77.4 78.2 78.9 79.5 80.2 80.9 81.6 82.3 FF lb/H/ENG 933 930 928 927 924 923 924 925 925 IAS KT 222 221 221 220 219 218 218 218 217 TAS KT 335 339 344 349 354 358 364 370 375 Mach 0.561 0.571 0.582 0. 593 0.603 0.614 0.626 0.639 0.650 BM G 2.31 2.26 2.21 2.16 2.10 2.05 1.99 1.93 1.87 40000 SR NM/lb 0.179 0.182 0.185 0. 188 0.191 0.194 0.197 0.200 0.203 N1 % 75.4 76.1 76.9 77.8 78.5 79.1 79.8 80.5 81.2 FF lb/H/ENG 887 883 881 879 876 874 875 876 874 IAS KT 217 216 216 215 214 213 213 213 212 TAS KT 327 332 337 341 346 351 356 362 366 Mach 0.549 0.558 0.569 0. 580 0.590 0.600 0.613 0.625 0.636 BM G 2.36 2.31 2.27 2.22 2.16 2.11 2.05 2.00 1.93 38000 SR NM/lb 0.185 0.188 0.191 0. 194 0.197 0.201 0.204 0.207 0.210 N1 % 74.1 74.9 75.6 76.4 77.3 78.0 78.7 79.4 80.0 FF lb/H/ENG 842 838 835 832 830 827 827 827 825 IAS KT 212 211 210 210 209 208 208 208 207 TAS KT 320 324 329 334 338 343 348 354 358 Mach 0.536 0.546 0.556 0. 566 0.577 0.587 0.599 0.611 0.622 BM G 2.41 2.36 2.32 2.27 2.22 2.17 2.12 2.06 2.00 36000 SR NM/lb 0.190 0.194 0.197 0. 200 0.204 0.207 0.210 0.214 0.217 N1 % 72.8 73.5 74.3 75.1 75.9 76.7 77.5 78.2 78.8 FF lb/H/ENG 798 793 790 786 784 781 779 780 777 IAS KT 206 206 205 205 204 203 203 203 201 TAS KT 312 317 321 325 330 334 340 345 349 Mach 0.524 0.533 0.543 0. 553 0.564 0.573 0.584 0.597 0.607 BM G 2.46 2.42 2.37 2.33 2.28 2.23 2.18 2.13 2.07 34000 SR NM/lb 0.196 0.200 0.203 0. 207 0.211 0.214 0.218 0.221 0.225 N1 % 71.5 72.2 72.9 73.7 74.5 75.2 76.0 76.9 77.5 FF lb/H/ENG 754 749 745 742 740 735 733 733 729 IAS KT 201 200 200 199 199 198 197 197 196 TAS KT 305 309 313 317 322 326 331 336 340 Mach 0.511 0.520 0.529 0. 539 0.550 0.559 0.570 0.582 0.592 BM G 2.51 2.47 2.43 2.38 2.34 2.29 2.24 2.19 2.13 32000 SR NM/lb 0.202 0.206 0.210 0. 214 0.218 0.222 0.226 0.229 0.233 ### Page 54 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-15 Page 10 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: 36000 FT TO 39000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITIONS ALTITUDE WEIGHT (lb) 36000 37000 38000 39000 N1 % 88.9 90.6 91.4 - FF lb/H/ENG 1182 1182 1160 - IAS KT 238 234 228 - TAS KT 415 418 416 - Mach 0.722 0.729 0.725 - BM G 1.47 1.40 1.33 - 50000 SR NM/lb 0.175 0.177 0.179 - N1 % 87.8 89.5 91.3 91.5 FF lb/H/ENG 1135 1136 1138 1089 IAS KT 235 232 229 217 TAS KT 410 414 419 407 Mach 0.715 0.722 0.730 0.710 BM G 1.53 1.46 1.39 1.33 48000 SR NM/lb 0.181 0.182 0.184 0.187 N1 % 86.5 88.3 90.2 91.4 FF lb/H/ENG 1085 1089 1093 1098 IAS KT 231 229 227 224 TAS KT 404 410 415 419 Mach 0.704 0.714 0.723 0.730 BM G 1.60 1.52 1.45 1.38 46000 SR NM/lb 0.186 0.188 0.190 0.191 N1 % 85.2 87.0 88.8 90.8 FF lb/H/ENG 1032 1039 1047 1049 IAS KT 226 225 224 222 TAS KT 397 403 411 415 Mach 0.691 0.704 0.716 0.723 BM G 1.67 1.59 1.52 1.44 44000 SR NM/lb 0.192 0.194 0.196 0.198 N1 % 84.1 85.7 87.5 89.4 FF lb/H/ENG 980 987 998 1001 IAS KT 222 221 221 219 TAS KT 389 396 405 410 Mach 0.678 0.691 0.706 0.715 BM G 1.74 1.66 1.59 1.52 42000 SR NM/lb 0.198 0.201 0.203 0.205 ### Page 55 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-15 Page 11 Code 06 AOM-135/1542 LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: 36000 FT TO 39000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITIONS ALTITUDE WEIGHT (lb) 36000 37000 38000 39000 N1 % 83.1 84.5 86.1 87.9 FF lb/H/ENG 928 934 945 951 IAS KT 217 216 216 215 TAS KT 381 388 397 403 Mach 0.664 0.676 0.692 0.703 BM G 1.80 1.74 1.67 1.59 40000 SR NM/lb 0.205 0.208 0.210 0.212 N1 % 81.9 83.3 84.8 86.5 FF lb/H/ENG 876 882 891 898 IAS KT 211 211 211 210 TAS KT 372 379 387 395 Mach 0.649 0.661 0.675 0.689 BM G 1.87 1.81 1.74 1.67 38000 SR NM/lb 0.212 0.215 0.217 0.220 N1 % 80.8 82.2 83.6 85.2 FF lb/H/ENG 827 831 838 846 IAS KT 206 206 205 205 TAS KT 364 370 378 386 Mach 0.634 0.646 0.660 0.674 BM G 1.94 1.88 1.81 1.75 36000 SR NM/lb 0.220 0.223 0.226 0.228 N1 % 79.5 80.9 82.4 83.9 FF lb/H/ENG 777 781 787 794 IAS KT 201 200 200 200 TAS KT 355 361 369 377 Mach 0.619 0.631 0.644 0.657 BM G 2.01 1.95 1.89 1.83 34000 SR NM/lb 0.228 0.231 0.234 0.237 N1 % 78.2 79.7 81.2 82.7 FF lb/H/ENG 728 732 737 743 IAS KT 196 195 195 194 TAS KT 345 352 359 367 Mach 0.603 0.615 0.628 0.641 BM G 2.08 2.02 1.96 1.90 32000 SR NM/lb 0.237 0.241 0.244 0.247 ### Page 56 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-15 Page 12 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: 5000 FT TO 17000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITIONS ALTITUDE WEIGHT (lb) 5000 10000 11000 12000 13000 14000 15000 16000 17000 N1 % 65.8 76.9 77.7 78.4 79.2 79.9 80.7 81.5 82.3 FF lb/H/ENG 1272 1738 1735 1732 1730 1728 1727 1727 1728 IAS KT 251 320 320 320 320 320 320 320 320 TAS KT 269 368 373 379 384 390 395 401 407 Mach 0.414 0.576 0.587 0. 597 0.608 0.620 0.631 0.643 0.655 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 50000 SR NM/lb 0.106 0.106 0.108 0. 109 0.111 0.113 0.114 0.116 0.118 N1 % 65.4 76.7 77.4 78.2 79.0 79.7 80.4 81.2 82.1 FF lb/H/ENG 1255 1726 1722 1719 1717 1715 1714 1713 1714 IAS KT 251 320 320 320 320 320 320 320 320 TAS KT 269 368 373 379 384 390 395 401 407 Mach 0.414 0.576 0.587 0. 597 0.608 0.620 0.631 0.643 0.655 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 48000 SR NM/lb 0.107 0.107 0.108 0. 110 0.112 0.114 0.115 0.117 0.119 N1 % 65.0 76.5 77.2 78.0 78.7 79.5 80.2 81.0 81.9 FF lb/H/ENG 1239 1714 1710 1707 1704 1702 1701 1700 1700 IAS KT 251 320 320 320 320 320 320 320 320 TAS KT 269 368 373 379 384 390 395 401 407 Mach 0.414 0.576 0.587 0. 597 0.608 0.620 0.631 0.643 0.655 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 46000 SR NM/lb 0.109 0.107 0.109 0. 111 0.113 0.114 0.116 0.118 0.120 N1 % 64.7 76.3 77.1 77.8 78.5 79.3 80.0 80.8 81.6 FF lb/H/ENG 1223 1702 1698 1695 1692 1690 1688 1688 1688 IAS KT 251 320 320 320 320 320 320 320 320 TAS KT 269 368 373 379 384 390 395 401 407 Mach 0.414 0.576 0.587 0. 597 0.608 0.620 0.631 0.643 0.655 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 44000 SR NM/lb 0.110 0.108 0.110 0. 112 0.113 0.115 0.117 0.119 0.121 N1 % 64.3 76.2 76.9 77.6 78.3 79.1 79.8 80.6 81.4 FF lb/H/ENG 1209 1691 1687 1683 1681 1678 1677 1676 1676 IAS KT 251 320 320 320 320 320 320 320 320 TAS KT 269 368 373 379 384 390 395 401 407 Mach 0.414 0.576 0.587 0. 597 0.608 0.620 0.631 0.643 0.655 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 42000 SR NM/lb 0.111 0.109 0.111 0. 112 0.114 0.116 0.118 0.120 0.121 ### Page 57 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-15 Page 13 Code 06 AOM-135/1542 MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: 5000 FT TO 17000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITIONS ALTITUDE WEIGHT (lb) 5000 10000 11000 12000 13000 14000 15000 16000 17000 N1 % 64.0 76.0 76.7 77.4 78.2 78.9 79.6 80.4 81.2 FF lb/H/ENG 1195 1681 1676 1673 1670 1667 1665 1664 1664 IAS KT 251 320 320 320 320 320 320 320 320 TAS KT 269 368 373 379 384 390 395 401 407 Mach 0.414 0.576 0.587 0. 597 0.608 0.620 0.631 0.643 0.655 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 40000 SR NM/lb 0.113 0.109 0.111 0. 113 0.115 0.117 0.119 0.120 0.122 N1 % 63.6 75.8 76.5 77.3 78.0 78.7 79.4 80.2 81.0 FF lb/H/ENG 1181 1671 1666 1663 1659 1657 1655 1654 1653 IAS KT 251 320 320 320 320 320 320 320 320 TAS KT 269 368 373 379 384 390 395 401 407 Mach 0.414 0.576 0.587 0. 597 0.608 0.620 0.631 0.643 0.655 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 38000 SR NM/lb 0.114 0.110 0.112 0. 114 0.116 0.118 0.119 0.121 0.123 N1 % 63.2 75.7 76.4 77.1 77.8 78.5 79.3 80.0 80.8 FF lb/H/ENG 1169 1661 1657 1653 1649 1647 1645 1643 1643 IAS KT 251 320 320 320 320 320 320 320 320 TAS KT 269 368 373 379 384 390 395 401 407 Mach 0.414 0.576 0.587 0. 597 0.608 0.620 0.631 0.643 0.655 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 36000 SR NM/lb 0.115 0.111 0.113 0. 115 0.116 0.118 0.120 0.122 0.124 N1 % 62.9 75.5 76.2 76.9 77.6 78.4 79.1 79.8 80.6 FF lb/H/ENG 1157 1653 1648 1644 1640 1637 1635 1634 1633 IAS KT 251 320 320 320 320 320 320 320 320 TAS KT 269 368 373 379 384 390 395 401 407 Mach 0.414 0.576 0.587 0. 597 0.608 0.620 0.631 0.643 0.655 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 34000 SR NM/lb 0.116 0.111 0.113 0. 115 0.117 0.119 0.121 0.123 0.125 N1 % 62.6 75.4 76.1 76.8 77.5 78.2 78.9 79.7 80.5 FF lb/H/ENG 1146 1644 1639 1635 1632 1629 1626 1625 1624 IAS KT 251 320 320 320 320 320 320 320 320 TAS KT 269 368 373 379 384 390 395 401 407 Mach 0.414 0.576 0.587 0. 597 0.608 0.620 0.631 0.643 0.655 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 32000 SR NM/lb 0.118 0.112 0.114 0. 116 0.118 0.120 0.122 0.123 0.125 ### Page 58 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-15 Page 14 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: 18000 FT TO 26000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITIONS ALTITUDE WEIGHT (lb) 18000 19000 20000 21000 22000 23000 24000 25000 26000 N1 % 83.0 83.7 84.4 85.1 85.7 86.4 87.2 87.5 87.9 FF lb/H/ENG 1729 1731 1734 1738 1746 1759 1776 1752 1726 IAS KT 320 320 320 320 320 320 319 316 311 TAS KT 413 419 425 432 438 445 450 452 453 Mach 0.667 0.680 0.692 0. 706 0.719 0.733 0.744 0.752 0.756 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.51 2.38 2.27 50000 SR NM/lb 0.119 0.121 0.123 0. 124 0.125 0.126 0.127 0.129 0.131 N1 % 82.8 83.5 84.2 84.9 85.5 86.2 87.0 87.5 87.9 FF lb/H/ENG 1715 1717 1720 1723 1731 1743 1763 1753 1727 IAS KT 320 320 320 320 320 320 320 317 312 TAS KT 413 419 425 432 438 445 451 454 455 Mach 0.667 0.680 0.692 0. 706 0.719 0.733 0.747 0.754 0.759 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.48 2.36 48000 SR NM/lb 0.120 0.122 0.124 0. 125 0.127 0.128 0.128 0.129 0.132 N1 % 82.6 83.3 84.0 84.7 85.3 86.0 86.8 87.5 87.8 FF lb/H/ENG 1701 1703 1706 1709 1716 1728 1748 1754 1729 IAS KT 320 320 320 320 320 320 320 318 313 TAS KT 413 419 425 432 438 445 451 455 456 Mach 0.667 0.680 0.692 0. 706 0.719 0.733 0.747 0.756 0.761 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.45 46000 SR NM/lb 0.121 0.123 0.125 0. 126 0.128 0.129 0.129 0.130 0.132 N1 % 82.4 83.1 83.8 84.5 85.1 85.8 86.6 87.5 87.8 FF lb/H/ENG 1688 1690 1692 1696 1702 1714 1733 1755 1730 IAS KT 320 320 320 320 320 320 320 319 314 TAS KT 413 419 425 432 438 445 451 457 458 Mach 0.667 0.680 0.692 0. 706 0.719 0.733 0.747 0.759 0.764 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 44000 SR NM/lb 0.122 0.124 0.126 0. 127 0.129 0.130 0.130 0.130 0.132 N1 % 82.2 82.9 83.6 84.3 85.0 85.6 86.4 87.3 87.8 FF lb/H/ENG 1676 1677 1679 1683 1689 1701 1719 1748 1731 IAS KT 320 320 320 320 320 320 320 320 316 TAS KT 413 419 425 432 438 445 451 458 459 Mach 0.667 0.680 0.692 0. 706 0.719 0.733 0.747 0.761 0.766 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 42000 SR NM/lb 0.123 0.125 0.127 0. 128 0.130 0.131 0.131 0.131 0.133 ### Page 59 AIRPLANE OPERATIONS MANUAL FLIGHT PLANNING LEGACY 600 CONFIG C (lb) TEMPORARY REVISION 19.1 1-05-15 Page 15 Code 06 AOM-135/1542 MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: 18000 FT TO 26000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITIONS ALTITUDE WEIGHT (lb) 18000 19000 20000 21000 22000 23000 24000 25000 26000 N1 % 82.0 82.7 83.4 84.1 84.8 85.5 86.3 87.2 87.8 FF lb/H/ENG 1664 1666 1667 1670 1677 1688 1706 1734 1732 IAS KT 320 320 320 320 320 320 320 320 317 TAS KT 413 419 425 432 438 445 451 458 461 Mach 0.667 0.680 0.692 0. 706 0.719 0.733 0.747 0.761 0.769 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 40000 SR NM/lb 0.124 0.126 0.128 0. 129 0.131 0.132 0.132 0.132 0.133 N1 % 81.9 82.5 83.2 83.9 84.6 85.3 86.1 87.0 87.8 FF lb/H/ENG 1653 1654 1656 1659 1665 1676 1694 1721 1733 IAS KT 320 320 320 320 320 320 320 320 318 TAS KT 413 419 425 432 438 445 451 458 462 Mach 0.667 0.680 0.692 0. 706 0.719 0.733 0.747 0.761 0.771 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 38000 SR NM/lb 0.125 0.127 0.128 0. 130 0.132 0.133 0.133 0.133 0.133 N1 % 81.7 82.4 83.1 83.8 84.5 85.2 85.9 86.8 87.8 FF lb/H/ENG 1643 1643 1645 1648 1653 1664 1682 1709 1734 IAS KT 320 320 320 320 320 320 320 320 319 TAS KT 413 419 425 432 438 445 451 458 464 Mach 0.667 0.680 0.692 0. 706 0.719 0.733 0.747 0.761 0.773 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 36000 SR NM/lb 0.126 0.128 0.129 0. 131 0.133 0.134 0.134 0.134 0.134 N1 % 81.5 82.2 82.9 83.6 84.4 85.0 85.8 86.7 87.8 FF lb/H/ENG 1633 1633 1635 1637 1643 1653 1671 1697 1734 IAS KT 320 320 320 320 320 320 320 320 319 TAS KT 413 419 425 432 438 445 451 458 464 Mach 0.667 0.680 0.692 0. 706 0.719 0.733 0.747 0.761 0.773 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 34000 SR NM/lb 0.126 0.128 0.130 0. 132 0.133 0.134 0.135 0.135 0.134 N1 % 81.3 82.1 82.8 83.5 84.2 84.9 85.6 86.5 87.6 FF lb/H/ENG 1623 1624 1625 1627 1633 1643 1660 1687 1725 IAS KT 320 320 320 320 320 320 320 320 320 TAS KT 413 419 425 432 438 445 451 458 465 Mach 0.667 0.680 0.692 0. 706 0.719 0.733 0.747 0.761 0.776 BM G 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 2.56 32000 SR NM/lb 0.127 0.129 0.131 0. 133 0.134 0.135 0.136 0.136 0.135 ### Page 60 FLIGHT PLANNING LEGACY 600 CONFIG C (lb) AIRPLANE OPERATIONS MANUAL 1-05-15 Page 16 Code 06 TEMPORARY REVISION 19.1 AOM-135/1542 MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING AE3007A1E ENGINES ALTITUDE: 27000 FT TO 35000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITIONS ALTITUDE WEIGHT (lb) 27000 28000 29000 30000 31000 32000 33000 34000 35000 N1 % 87.8 87.8 87.8 87.9 88.2 88.7 89.2 89.7 90.3 FF lb/H/ENG 1672 1616 1561 1507 1470 1436 1407 1379 1358 IAS KT 305 298 292 285 279 274 269 263 259 TAS KT 452 450 447 444 444 443 442 441 442 Mach 0.757 0.756 0.755 0. 754 0.756 0.758 0.760 0.762 0.767 BM G 2.17 2.08 1.99 1.90 1.81 1.73 1.65 1.57 1.48 50000 SR NM/lb 0.135 0.139 0.143 0. 148 0.151 0.154 0.157 0.160 0.163 N1 % 87.8 87.8 87.8 87.8 88.2 88.6 89.2 89.7 90.3 FF lb/H/ENG 1673 1619 1564 1509 1473 1439 1411 1387 1363 IAS KT 306 301 294 287 282 276 271 267 262 TAS KT 453 453 450 448 447 446 445 446 445 Mach 0.760 0.761 0.760 0. 760 0.761 0.763 0.765 0.770 0.773 BM G 2.25 2.15 2.06 1.97 1.88 1.79 1.70 1.61 1.53 48000 SR NM/lb 0.136 0.140 0.144 0. 148 0.152 0.155 0.158 0.161 0.163 N1 % 87.8 87.8 87.8 87.8 88.2 88.6 89.1 89.6 90.3 FF lb/H/ENG 1674 1620 1565 1510 1475 1443 1416 1389 1368 IAS KT 307 302 295 288 283 279 273 268 264 TAS KT 455 454 452 449 448 449 449 448 449 Mach 0.762 0.764 0.763 0. 762 0.764 0.769 0.771 0.773 0.779 BM G 2.34 2.24 2.14 2.05 1.95 1.85 1.76 1.67 1.58 46000 SR NM/lb 0.136 0.140 0.144 0. 149 0.152 0.156 0.158 0.161 0.164 N1 % 87.8 87.8 87.8 87.7 88.1 88.6 89.1 89.6 90.2 FF lb/H/ENG 1675 1621 1566 1513 1478 1445 1420 1394 1371 IAS KT 308 303 296 290 285 280 275 270 265 TAS KT 457 456 453 452 452 451 452 451 451 Mach 0.765 0.767 0.766 0. 768 0.770 0.772 0.777 0.779 0.782 BM G 2.44 2.33 2.23 2.13 2.02 1.93 1.82 1.73 1.64 44000 SR NM/lb 0.136 0.141 0.145 0. 150 0.153 0.156 0.159 0.162 0.164 N1 % 87.8 87.8 87.7 87.7 88.1 88.5 89.1 89.6 90.2 FF lb/H/ENG 1677 1622 1567 1514 1480 1447 1422 1397 1376 IAS KT 310 304 297 292 286 281 277 271 267 TAS KT 458 457 455 454 453 453 454 453 454 Mach 0.767 0.769 0.768 0. 770 0.772 0.775 0.780 0.782 0.788 BM G 2.55 2.43 2.33 2.22 2.11 2.01 1.90 1.81 1.70 42000 SR NM/lb 0.137 0.141 0.145 0. 150 0.153 0.156 0.159 0.162 0.165 The text continues at https://openairdocs.org/service-documents/embraer/tr-19-1/file/b7fbd104f3bc.md?from=61 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). 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