Airbus Helicopters Tiger HAD
Overview
The Airbus Helicopters Tiger HAD is a tandem-seat, twin-engine attack helicopter developed for armed reconnaissance, escort, ground-fire support, air-to-air combat and anti-tank missions. Airbus describes the HAD as a combat-proven variant equipped with two enhanced MTR 390 turboshaft engines, modern digital avionics and a roof-mounted sight supporting guided weapons. The helicopter’s narrow airframe, four-blade main rotor and survivability features are optimized for operations in demanding combat environments. The HAD is kept as a distinct Tiger variant because its engines, maximum takeoff weight, weapons integration and mission equipment differ from earlier Tiger configurations. Specifications in this profile should therefore remain HAD-specific rather than being generalized across the entire Tiger family.
Quick Facts
Specifications
| ICAO Type Code | TIGR |
|---|---|
| Military Designation | EC665 |
| First Flight | Apr 27, 1991 |
| Introduction Date | 2003 |
| Crew | 2 |
| Length | 46 ft 11 in |
| Wingspan / Rotor Diameter | 42 ft 8 in rotor diameter |
| Height | 13 ft 1 in |
| Empty Weight | 6724 lb |
| Max Takeoff Weight | 14550 lb |
| Cruise Speed | 140 kt |
| Max Speed | 157 kt |
| Range | 430 nm |
| Service Ceiling | 13000 ft |
| Engine Model | 2 |
| Engine Count | 2 |
Data verification status: Unverified