JETRANGER III / MODEL 206 B
SPECIFICATIONS SUMMARY
WEIGHTS: |
LBS. |
|---|---|
|
*Standard Configuration Weight |
1,625 |
|
Normal Gross Weight |
3,200 |
|
External Load Gross Weight |
3,350 |
|
Standard Conf. Useful Load (Gross Wt. - Std. Conf Wt.) |
1.575 |
|
Max. External Load |
1,500 |
* The Standard Configuration Weight includes the 5-place upholstered interior with individual seat belts, carpeting and soundproofing. Ballast is not included since it is a function of installed optional equipment. Oil 11 lbs. also omitted.
PERFORMANCE SUMMARY: (International Standard Day)
TAKE-OFF, GROSS WEIGHT |
LBS. |
2,600 |
3,000 |
3,200 |
|---|---|---|---|---|
|
I.G.E. Hovering Ceiling (2 ft. skid ht.) |
ft. |
20,000+ |
14,800 |
12,800 |
|
**I.G.E. Hovering Ceiling (2 ft. skid ht.) |
ft. |
16,400+ |
12,200 |
10,200 |
|
O.E.G. Hovering Ceiling |
ft |
19,100 |
10,600 |
8,800 |
|
**O.E.G. Hovering Ceiling |
ft |
12,200 |
7,600 |
3,800 |
|
Certificated Altitude |
ft |
20,000 |
20,000 |
13,500 |
|
ServiceCeiling(MCP) |
ft |
20,000+ |
20,000+ |
13,500 |
|
Sea Level Max. Rate of Climb (TOP) |
ft//min |
2,080 |
1,540 |
1,280 |
|
Max. Allowable TAS (sea level) |
MPH |
150 |
150 |
140 |
|
Max'Allowable TAS (5,000 ft.) |
MPH |
153 |
153 |
133 |
|
Max. Cont. Cruise TAS (sea level) |
MPH |
134 |
131 |
128 |
|
Max. Cont. Cruise TAS (5,000 ft.) |
MPH |
142 |
136 |
132 |
|
***Range (Sea Level) |
st. miles |
437 |
425 |
419 |
|
***Range (5,000 ft.) |
st. miles |
496 |
476 |
465 |
NOTE: **HOT DAY - International Standard Day + 20C. ***Cruise at Long Range Cruise Speed, 6.8 Ib./gal. fuel. No reserve.
|
POWER RATINGS: |
|
|---|---|
|
Engine (Allison 250-C2OJ) |
|
|
Take-off Horsepower, SHP |
420 |
|
Max. Continuous, SHP |
370 |
|
Airframe Ratings |
|
|
Take-off Horsepower, SHP |
317 |
|
Max. Continuous, SHP |
270 |
|
|
|
|
Fuel Type/ Capacity |
Aviation Turbine/91 Gallons |
THE DATA SET FORTH ON THIS DOCUMENT ARE GENERAL IN NATURE AND MAY VARY WITH CONDITIONS. FOR PERFORMANCE DATA AND OPERATING LIMITATIONS FOR ANY SPECIFIC FLIGHT MISSION. REFERENCE MUST BE MADE TO THE APPROVED FLIGHT MANUAL.
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