MANUFACTURE : MBB IPTN 1983/84
 
POWER PLANT
| Power Plant |
:2 (two) Roll Royce / Allison 250-C 20B (400 HP Each) |
| Take Off Power |
:400 SHP |
| Max. Contingengy Power |
:385 SHP |
SPECIFICATIONS
| Seating Capacity |
:1 Cockpit + 4 Seat |
| Litter Capacity |
:2 Each |
| Avarage Cruise Speed |
:110 Kts |
| Speed with Slung Load |
:40 -80 Kts |
| Max. Speed (VNE) |
:144 Kts |
| Fuel Consumption |
:210 Ltr/hr |
| Fuel Capacity |
:Internal Tank : 570 Ltr |
|
:Ferry Tank (1) : 200 Ltr |
| Max. Range (15'' Reserve) |
:270 Nm / 501 Km |
| Ceiling (T/O & Landing) |
:10000 ft |
| Ceiling (Inflight) |
:17000 ft |
| Max. Rate of Climb |
:1379 ft/min |
DIMENSION
| Rotor Blades |
:4 Semi Rigid Hingeles |
| Fuselage Length |
:8.81 M |
| Overall Length |
:11.86 M |
| Fuselage Width |
:1.58 M |
| Overall Height |
:3.02 M |
| Main Rotor Diameter |
:9.84 M |
| Tail Rotor Clearance |
:1.89 M |
LOADING INFORMATION
| Max. Gross Weight |
:2400 Kg / 5290 Lb |
| Empty Weight - Std |
:1400 Kg / 3086 Lb |
| Usefuel Load - Int |
:1000 Kg / 2204 Lb |
| Usefuel Load - Ext |
:900 Kg / 6539 Lb |
HELIPAD SIZE
| Base |
:10 x 15 Base |
| Remote Area |
:6 x 6 M |
|
