Supplement POH
Cessna 172 R&S
(FAA-Version)
Page 5a-10
Issue 3
Revision -, June 2016
MAXIMUM RATE-OF-CLIMB at 1111 kg (2450 lbs)
Conditions:
Take-off weight 1111 kg (2450 lbs)
Climb speed v
y
= 70 KIAS
Flaps Up
Full Power
Notes:
1. For operation in air colder than this table provides, use cold-
est data shown.
2. For operation in air warmer than this table provides, use
extreme caution.
Figure 5-3a Maximum Rate of Climb at take-off weight
1111 kg (2450 lbs)
PRESS Climb Rate of Climb [ft/min]
ALT speed Outside Air Temperature [°C]
[FT] [KIAS] -20°C 0°C +20°C +40°C +50°C
070
596 576 558 458 354
1000 70
587 567 548 447 343
2000 70
577 557 538 437 333
3000 70
567 547 527 426 321
4000 70
557 536 516 414 310
5000 70
547 525 505 403 298
6000 70
536 514 494 391 286
7000 70
503 481 460 358 255
8000 70
470 447 426 326 224
9000 70
436 413 391 292 193
10000 70
403 379 356 259 161
11000 70
368 344 321 225 128
12000 70
334 309 286 190 96
13000 70
299 273 250 156 63
14000 70
263 238 213 120 29
15000 70
228 201 177 85 -5
16000 70
192 165 140 49 -39
17000 70
155 128 102 12 -74
18000 70
118 90 64 -24 -109
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