"OUR HELICOPTER"

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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