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| General Data |
| Empty Weight of Standard Aircraft |
3,208 lbs. |
| Maximum Takeoff Weight |
6,415 lbs. |
| Useful Load |
3,208 lbs. |
| Maximum Takeoff Weight . . .with External Load |
6,415 lbs. |
| Usable Fuel Capacity . . . Standard Tank |
1,038.6 lb. |
| Baggage Compartment Volume |
38.8 cu.ft. |
| Power Plant |
2 Pratt & Whitney PW 206B2
or
2 Turbomeca Arrius 2B2 turbine |
| Cabin Volume |
134.2 cu.ft. |
| Standard Seating Capacity |
2 + 6 |
Performance Data |
EC135 P2i |
EC135 T2i |
| Never Exceed Speed |
140 kts. |
140 kts. |
| Fast Cruise Speed |
137 kts. |
137 kts. |
| Maximum Range (with no reserves) |
342 nm. |
334 nm. |
| Maximum Endurance
(with no reserves) |
3.35 hrs. |
3.23 hrs. |
| Hover In Ground Effect Ceiling |
10,000 ft. |
10,000 ft. |
| Hover Out of Ground Effect Ceiling |
6,600 ft. |
6,600 ft. |
| Rate of Climb (all engines operative, MCP) |
1,500 fpm. |
1,500 fpm. |
| Takeoff Power Per Engine |
667 shp. |
634 shp. |
| * Performance data is provided at Sea Level, ISA conditions, maximum gross weight, with standard fuel. It is not intended for flight planning purposes. |
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