The tables below depict the Beechcraft King Air 350 climb performance. These charts show the time, the amount of fuel consumed,
and the distance flown at various takeoff weights and from sea level to altitudes up to 35,000 feet Climb data assumes ISA conditions
and no wind.
|
CLIMB PERFORMANCE |
| Pressure Altitude (ft) |
Takeoff Weight (lb) |
| 15,000 |
14,000 |
13,000 |
12,000 |
| 20,000 |
Time min |
10 |
9 |
8 |
8 |
| Fuel lb |
168 |
153 |
139 |
127 |
| Dist nm |
32 |
29 |
26 |
24 |
| 24,000 |
Time min |
13 |
12 |
11 |
10 |
| Fuel lb |
207 |
187 |
169 |
153 |
| Dist nm |
42 |
38 |
34 |
31 |
| 26,000 |
Time min |
15 |
14 |
12 |
11 |
| Fuel lb |
229 |
207 |
186 |
167 |
| Dist nm |
49 |
44 |
39 |
35 |
| 29,000 |
Time min |
19 |
17 |
15 |
13 |
| Fuel lb |
266 |
238 |
213 |
190 |
| Dist nm |
61 |
55 |
48 |
43 |
| 31,000 |
Time min |
22 |
20 |
17 |
15 |
| Fuel lb |
296 |
262 |
238 |
207 |
| Dist nm |
73 |
64 |
56 |
49 |
| 33,000 |
Time min |
26 |
23 |
20 |
17 |
| Fuel lb |
330 |
290 |
255 |
226 |
| Dist nm |
86 |
74 |
65 |
57 |
| 35,000 |
Time min |
32 |
27 |
23 |
20 |
| Fuel lb |
378 |
324 |
282 |
247 |
| Dist nm |
107 |
90 |
76 |
66 |
|
| |
TAKEOFF PERFORMANCE
TAKEOFF DISTANCE (FT) FLAPS APPROACH — SEA LEVEL |
| Takeoff Weight (lb) |
Outside Air Temperature 15°C / 59°F |
| 15,000 |
3,300 |
| 14,000 |
2,939 |
| 13,000 |
2,737 |
| 12,000 |
2,540 |
|
| |
CRUISE PERFORMANCE |
| Maximum Cruise Power 1500 RPM |
| Cruise Altitude (ft) |
Aircraft Weight (lb) |
| 14,000 |
13,000 |
12,000 |
11,000 |
|
309 |
311 |
312 |
314 |
|
870 |
872 |
872 |
874 |
|
309 |
311 |
313 |
315 |
|
770 |
772 |
774 |
776 |
|
307 |
310 |
312 |
314 |
|
720 |
722 |
726 |
728 |
|
303 |
306 |
310 |
312 |
|
644 |
648 |
650 |
654 |
|
298 |
302 |
306 |
310 |
|
594 |
598 |
602 |
604 |
|
292 |
297 |
302 |
306 |
|
548 |
550 |
552 |
556 |
|
283 |
290 |
295 |
300 |
|
498 |
502 |
504 |
506 |
|
|
| |
| Maximum Range Power 1500 RPM |
| Cruise Altitude (ft) |
Aircraft Weight (lb) |
| 14,000 |
13,000 |
12,000 |
11,000 |
|
219 |
214 |
209 |
206 |
|
458 |
434 |
412 |
394 |
|
226 |
222 |
217 |
212 |
|
432 |
410 |
386 |
364 |
|
228 |
226 |
221 |
215 |
|
418 |
398 |
376 |
352 |
|
236 |
230 |
228 |
221 |
|
408 |
380 |
362 |
336 |
|
243 |
234 |
230 |
226 |
|
410 |
374 |
350 |
330 |
|
241 |
242 |
232 |
230 |
|
398 |
380 |
344 |
322 |
|
229 |
240 |
241 |
231 |
|
380 |
368 |
348 |
314 |
|
| |
LANDING PERFORMANCE |
| Approach Speeds |
| Weight (lb) |
VREF (KIAS) |
| 15,000 |
109 |
| 14,000 |
105 |
| 13,000 |
102 |
| 12,000 |
100 |
| 11,000 |
100 |
| 10,000 |
100 |
|
|
| Normal Landing Distance — Flaps Down |
Field
Elevation
(ft) |
Landing
Weight
(lb) |
Temperature
15°C / 59°F |
| S.L. |
15,000 |
2,692 |
| |
13,000 |
2,490 |
| |
11,000 |
2,390 |
|
|
