在线看免费❗_青青草网上免费完整版_.手.动.输.入.网.址.联.系.客.服.人.员.lanan_shell
The information provided in this document is to be used during simulated flight only and is not intended to be used in real life. Attention VA's - you may post this file on your site for download. Please do not post this information as a web page on your site. To all others: This information is provided for your personal use only. Distribution of this information in any form is not permitted without my approval. Distribution of this information in any payware product, CD or otherwise is not permitted. Compiled by Matt Zagoren 2 ABBREVIATED CHARTS A320 Flight Planning Chart 3 POWER SETTING CHARTS A320 Takeoff Thrust Setting - EPR EPR settings in shaded area are for FLEX EPR only. TAT Pressure Altitude (Feet) (°F/°C) -1000 SL 1000 2000 3000 4000 5000 6000 7000 8000 8500 158/70 1.295 1.294 - - - - - - - - - 154/68 1.303 1.303 1.301 - - - - - - - - 151/66 1.312 1.311 1.310 1.307 - - - - - - - 147/64 1.320 1.320 1.318 1.316 1.323 - - - - - - 144/62 1.329 1.329 1.327 1.325 1.332 1.339 - - - - - 140/60 1.337 1.337 1.336 1.334 1.341 1.348 1.354 - - - - 136/58 1.346 1.346 1.345 1.343 1.351 1.358 1.364 1.363 - - - 133/56 1.355 1.355 1.354 1.352 1.360 1.367 1.374 1.372 1.371 - - 129/54 1.364 1.364 1.363 1.362 1.369 1.377 1.383 1.382 1.381 1.379 - 126/52 1.374 1.373 1.372 1.371 1.379 1.386 1.393 1.392 1.391 1.389 1.388 122/50 1.378 1.383 1.381 1.380 1.388 1.396 1.403 1.402 1.401 1.399 1.398 118/48 1.390 1.391 1.390 1.398 1.405 1.413 1.412 1.411 1.409 1.408 115/46 1.397 1.400 1.399 1.408 1.415 1.423 1.422 1.421 1.419 1.418 111/44 1.409 1.409 1.418 1.426 1.433 1.432 1.431 1.429 1.428 108/42 1.413 1.419 1.428 1.436 1.444 1.442 1.441 1.440 1.438 104/40 1.429 1.438 1.446 1.454 1.453 1.451 1.450 1.448 100/38 1.430 1.448 1.456 1.464 1.464 1.462 1.460 1.459 97/36 1.455 1.466 1.474 1.474 1.473 1.471 1.469 93/34 1.476 1.485 1.484 1.483 1.482 1.480 90/32 1.479 1.495 1.494 1.493 1.492 1.491 86/30 1.504 1.505 1.504 1.503 1.501 82/28 1.514 1.515 1.513 1.512 79/26 1.524 1.525 1.523 75/24 1.534 1.533 72/22 1.537 68/20 50/10 32/0 -4/-20 -40/-40 -76/-60 1.378 1.397 1.413 1.430 1.455 1.479 1.504 1.514 1.524 1.534 1.573 4 A320 Reduced Takeoff Thrust Reduced EPR is the minimum thrust required under normal conditions and is recommended since it results in reduced engine wear and fuel consumption. Do not use reduced takeoff thrust when: • Braking action is reported less than good • The probability of windshear exists • Takeoff runway is other than dry • Headwind adjustment has been used to increase the allowable takeoff weight • Takeoff is made with a tailwind • EPR indications are inop • A brake is deactivated The FMGS automatically computes reduced takeoff thrust when a FLEX temp higher than ambient temp is entered on the MCDU TAKEOFF page. To determine FLEX (ASMD) temp, see the Takeoff Data provided by dispatch. 5 A320 Maximum Climb Thrust - EPR TAT Pressure Altitude (Feet) (°C) SL 2 5 8 12 17 20 25 31 35 39 58 1.180 - - - - - - - - - - 54 1.192 1.197 - - - - - - - - - 50 1.205 1.210 1.210 - - - - - - - - 46 1.219 1.223 1.224 - - - - - - - - 42 1.234 1.238 1.238 1.234 1.219 - - - - - - 38 1.251 1.255 1.254 1.249 1.235 - - - - - - 34 1.267 1.272 1.271 1.265 1.251 1.243 - - - - - 30 1.269 1.289 1.290 1.283 1.269 1.261 1.258 - - - - 26 1.308 1.303 1.289 1.279 1.278 - - - - 22 1.313 1.323 1.310 1.299 1.297 1.275 - - - 18 1.333 1.331 1.321 1.318 1.295 1.288 - - 14 1.340 1.343 1.341 1.316 1.309 - - 10 1.366 1.364 1.340 1.330 - - 6 1.372 1.387 1.365 1.353 1.349 1.345 2 1.395 1.389 1.379 1.371 1.367 -2 1.414 1.403 1.394 1.390 -6 1.428 1.419 1.414 -10 1.448 1.443 1.438 -14 1.466 1.461 -18 1.488 1.483 -22 1.497 -26 -30 -34 -38 -42 -46 ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ ^ -50 1.269 1.289 1.313 1.333 1.340 1.372 1.395 1.414 1.448 1.488 1.497 A320 EPR Mode Inoperative Takeoff Thrust and Maximum Climb Thrust - N1 If the EPR mode is unavailable, thrust control automatically reverts to the N1 mode (rated or unrated), and the autothrottle is not available. In the rated N1 mode, thrust limits for takeoff, maximum climb, maximum continuous and go-around are calculated by the FADEC. Maximum cruise thrust is the only limit not monitored by the FADEC. If one engine reverts to the unrated mode (N1 value not displayed on ECAM), the N1 of the engine in the unrated mode must be aligned with the N1 of the engine in the rated mode. If both engines are in the unrated mode, use the following thrust setting tables. www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：空客A320性能 Airbus A320 Performance
