5-10 PERFORMANCE / NORMAL RUNWAY LANDING PERFORMANCE
ICON A5-B / PILOT’S OPERATING HANDBOOK CHANGE A1
CHAPTER 5
Includes 0.2 gal for engine start, taxi, and takeoff.
Includes fuel and distance to climb to the given altitude.
Includes 45 minutes fuel reserve at 4500 RPM at the given alti-
tude.
5.13 NORMAL RUNWAY LANDING PERFORMANCE
Conditions
1510 lb
f
Flaps—0°
Level and dry asphalt runway
Reasonable braking
Zero wind
STD Temp - 20°F STD Temp STD Temp + 20°F
Press
Alt
(ft)
RPM KTAS
Endur
ance
(hrs)
Range
(nm)
KTAS
Endur
ance
(hrs)
Range
(nm)
KTAS
Endur
ance
(hrs)
Range
(nm)
Sea
Level
4500 76 4.8 369 75 5.1 381 75 5.3 394
5000 86 3.7 317 86 3.9 332 86 4.1 348
5500 95 2.1 202 95 2.5 237 95 3.0 284
2000
4500 75 5.1 384 75 5.3 398 74 5.6 417
5000 86 3.9 337 86 4.1 354 85 4.3 372
5500 95 2.7 257 95 3.3 316 95 3.5 334
4000
4500 74 5.3 403 73 5.7 424 73 6.0 444
5000 85 4.1 360 85 4.4 379 85 4.6 400
5500 95 3.3 322 94 3.6 343 94 3.8 364
6000
4500 73 5.7 429 72 6.1 453 71 6.4 466
5000 85 4.4 386 84 4.7 408 84 4.9 427
5500 94 3.6 350 94 3.8 374 94 4.1 395
8000
4500 72 6.1 454 70 6.4 470 69 6.6 471
5000 84 4.7 414 84 5.0 435 83 5.2 451
5500 94 3.9 381 94 4.1 404 93 4.3 422
10000
4500 70 6.4 465 68 6.5 466 66 6.7 467
5000 83 5.0 438 83 5.2 456 82 5.4 473
5500 94 4.1 409 93 4.3 429 93 4.5 449
12000
4500 67 6.4 462 65 6.6 463 63 6.8 463
5000 83 5.2 460 82 5.4 478 81 5.7 498
5500 93 4.3 435 93 4.6 457 93 4.8 480