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Basic Profile

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

First Flight Apr 27, 1991
Crew 2
Range 430 nm
Cruise Speed 140 kt
Max Speed 157 kt

Specifications

ICAO Type CodeTIGR
Military DesignationEC665
First FlightApr 27, 1991
Introduction Date2003
Crew2
Length46 ft 11 in
Wingspan / Rotor Diameter42 ft 8 in rotor diameter
Height13 ft 1 in
Empty Weight6724 lb
Max Takeoff Weight14550 lb
Cruise Speed140 kt
Max Speed157 kt
Range430 nm
Service Ceiling13000 ft
Engine Model2
Engine Count2

Data verification status: Unverified

Source: https://en.wikipedia.org/wiki/Eurocopter_Tiger