ICON A5, Pilot Operating Handbook

Page: 84 / 161

5-11 PERFORMANCE / RANGE AND ENDURANCE
ICON A5 / PILOT’S OPERATING HANDBOOK CHANGE A0
CHA
P
T
E
R 5
5.11 RANGE AND ENDURANCE
Conditions
1510 lb
f
and Forward CG
Flaps—0°
Landing gear—UP
Windows installed
Zero wind
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.
4000 45 7.1 0.6 7.2
5000 41 9.2 0.8 9.4
6000 37 11.5 0.9 11.8
8000 30 16.6 1.3 17.3
10000 23 22.9 1.6 24.3
12000 16 31.1 2.1 33.7
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
Press Alt
(ft)
STD Temp
(°F)
From Sea Level
Time (min)
Fuel Used
(gal)
Distance
(nm)