The Z-9-H410A, a variant of the Harbin Z-9 Haitun, was initially powered by WZ8A engines (the Chinese produced Turboméca Arriel 1C1).  Maximum internal and external payloads are 1,900 kg and 1,600 kg, respectively.  The H410A could be equipped with Turboméca Arriel 2C engines, instead.  The helicopter features three pairs of doors, the rearmost pair being aft-sliding; the aircraft requires a single pilot and can hold a maximum of 13 passengers.  Accessories can include a searchlight, optoelectronic system and emergency flotation gear.

The H410A received domestic type and production certificates in April 2001, followed by its maiden flight in December 2003.  The helicopter was granted CAAC certification in July 2002.

Overview

Data on design, manufacture and status

Parent type: Harbin Z-9

Aircraft status: Status unknown

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift devices: 1 Single main rotor

Dedicated control device: 1 Fenestron/Shrouded tail rotor

Crew required: 1 in Side-by-side arrangement

Landing gear: Wheels (all retractable)

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

Related VFS Resources

Resources related to the H410A , provided by the Vertical Flight Society.
Forum Proceedings
 
Vertiflite articles
Enter a search term in the box above.
Web files from vtol.org
Enter a search term in the box above.
Webpages from vtol.org
Enter a search term in the box above.

Related Public Resources

Resources related to the H410A , provided by public sources across the internet.

Images