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
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ABBREVIATED CHARTS
A320 Flight Planning Chart
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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
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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.
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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.
　
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