Harbin Z-9 - Wikiwand (2025)

The Harbin Z-9 (NATO reporting name "Haitun", Chinese: 海豚; lit. 'Dolphin'[1]) is a Chinese military utility helicopter with armed variants, manufactured by Harbin Aircraft Manufacturing Corporation. It is a license-built variant of the French Eurocopter AS365 Dauphin.

Quick Facts Z-9, General information ...

Z-9

A Chinese naval Z-9 departs HMS Cornwall

General information
TypeMedium multi-purpose utility helicopter
National originChina
ManufacturerHarbin Aircraft Manufacturing Corporation
StatusIn service
Primary usersPeople's Liberation Army Ground Force

Pakistan Naval Air Arm Royal Cambodian Air Force

Number built200+
History
Manufactured1981–present
Introduction date1994
First flight1981
Developed fromEurocopter AS365 Dauphin
VariantsHarbin Z-19

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Design and development

The first Z-9 flew in 1981, and was built in China from components supplied by Aérospatiale as part of a production patent bought on 15 October 1980.[2] On 16 January 1992, the indigenous variant Z-9B, constructed with 70% Chinese-made parts, flew successfully. The flight test was completed in November 1992 and the design was finalized a month later. Z-9B production began in 1993 and entered PLA service in 1994.[3]

The Z-9B features an 11-blade Fenestron faired-in tail rotor with wider-chord, all-composite blades replacing the 13-blade used in the original AS365N. As a light tactical troop transport, the Z-9 has the capacity to transport 10 fully armed soldiers. Generally the Z-9 is identical to the AS365N Dauphin, though later variants of the Z-9 incorporate more composite materials to increase structural strength and lower radar signature.

The helicopter has a four-blade main rotor, with two turboshaft engines mounted side by side on top of the cabin with engine layout identical to the AS365N. The Z-9 teardrop-shaped body features a tapered boom to the tail fin, with rounded nose and stepped-up cockpit, retractable gear, and all flat bottom.

In 2002, Harbin obtained Chinese certification for the new H410A variant of the Z-9, which features more powerful Turbomeca Arriel 2C turboshaft engines; Eurocopter issued official objections to Harbin's decision to continue production in spite of the license-production agreement having expired, leading to a period of highly sensitive international negotiations to resolve the dispute.[4]

Variants

An armed variant has been fielded by the PLA since the early 1990s as the Z-9W, with pylons fitted for anti-tank missiles. These helicopters lack the maneuverability and survivability of a proper attack helicopter, and merely provide a stopgap during the development of the Z-10. The latest armed version, the Z-9W, was introduced in 2005 and has night attack capabilities, with an under-nose low-light TV and infra-red observing and tracking unit.

The naval version introduced in the 1990s is known as the Z-9C. As well as SAR and ASW duties, the Z-9C can be fitted with an X-band KLC-1 surface search radar to detect surface targets beyond the range of shipborne radar systems.[5]

Z-9
License-produced variant of the French AS.365N1.
Z-9A
Kit-built variant of the AS.365N2.
Z-9A-100
Prototypes for domestic market versions with WZ8A engines. First flight 16 January 1992, approved 30 December 1992.
Z-9B
Initial version based on Z-9A-100. Multi-role.
Z-9C
License-produced variant of the Eurocopter AS.565 Panther for the PLA Naval Air Force.
Z-9EC
ASW variant produced for the Pakistan Naval Air Arm. Configured with pulse-compression radar, low frequency dipping sonar, radar warning receiver and doppler navigation system, it is also armed with torpedoes for use aboard Pakistan Navy's Zulfiquar-class frigates.[6]
Z-9EH
Transport, emergency and/or passenger variant.[7]
Z-9W
Armed version with optional pylon-mounted armament, gyro stabilization and roof-mounted optical sight. Export designation Z-9G, roof-mounted sight optional. First flown in 1987, with the first weapons tests in 1989.[8]
Z-9WA
A newer night-capable version has been built with nose-mounted FLIR. July 2011, Xinhua News Agency released a photo of Z-9WA firing AKD10 air-to-ground missile.[9] Incorporates a domestic Chinese helmet mounted sight that is compatible with anti-tank missiles such as HJ-8 /9/ 10, as well as light anti-ship missiles such as C-701/703 and TL-1/ 10 when they are used as air-to-surface missiles, air-to-air missiles such as TY-90 and other MANPAD missiles for self-defense.[10]
H410A
Version with 635kW WZ8C turbo-shaft engines. First flight September 2001, CAAC certification 10 July 2002. One is currently being fitted with a new Mast-Mounted Sighting (MMS) system.
H425
Newest VIP version of the H410A.
H450
Projected development.
Z-19
Attack helicopter development with tandem seats. The Z-19 shares the same powerplant as the Z-9WA.

Operators

Harbin Z-9 - Wikiwand (8)Bangladesh
  • Bangladesh Navy (on order)[11][12][13][14]
Harbin Z-9 - Wikiwand (9)Bolivia
  • Bolivian Army[15]
Harbin Z-9 - Wikiwand (10)Cambodia
  • Cambodian Air Force[15]
  • Cambodian Gendarmerie
Harbin Z-9 - Wikiwand (11)Cameroon
  • Cameroon Air Force[15]
Harbin Z-9 - Wikiwand (12)China
  • People's Liberation Army Air Force[15]
  • People's Liberation Army Ground Air Force
  • People's Liberation Army Naval Air Force[15]
    • Type 052D destroyer
    • Type 053 frigate, Type 053H3 frigate, Type 054 frigate, Type 054A frigate (Z-9C)
    • Type 056 corvette (Z-9C)
Harbin Z-9 - Wikiwand (13)Djibouti
  • Djiboutian Air Force[15]
Harbin Z-9 - Wikiwand (14)Equatorial Guinea
  • Armed Forces of Equatorial Guinea[16]
Harbin Z-9 - Wikiwand (15)Ghana
  • Ghana Air Force[17]
Harbin Z-9 - Wikiwand (16)Kenya
  • Kenya Defence Forces[15]
Harbin Z-9 - Wikiwand (17)Laos
  • Laotian Air Force[15]
Harbin Z-9 - Wikiwand (19)Mali
  • Mali Air Force[18]
Harbin Z-9 - Wikiwand (20)Mauritania
  • Mauritanian Air Force[15]
Harbin Z-9 - Wikiwand (21)Myanmar
  • State Administration Council[19]
Harbin Z-9 - Wikiwand (22)Namibia
  • Namibian Air Force[15]
Harbin Z-9 - Wikiwand (23)Pakistan
  • Pakistan Naval Air Arm[15]
Harbin Z-9 - Wikiwand (24)Zambia
  • Zambian Air Force[15]

Specifications (Z-9B)

Data from [20]

General characteristics

  • Crew: 1 or 2 pilots
  • Capacity: 10 passengers or 1,900kg (4,189lb) payload internal, 1,600kg (3,527lb) payload slung
  • Length: 12.11m (39ft 9in)
  • Height: 4.01m (13ft 2in)
  • Empty weight: 2,050kg (4,519lb)
  • Max takeoff weight: 4,100kg (9,039lb)
  • Powerplant: 2 × Zhuzhou Aeroengine Factory WZ-8A turboshaft, 632kW (848hp) each
  • Main rotor diameter: 11.94m (39ft 2in)
  • Main rotor area: 111.98m2 (1,205.3sqft) swept area

Performance

  • Maximum speed: 305km/h (190mph, 165kn)
  • Cruise speed: 260km/h (160mph, 140kn)
  • Ferry range: 1,000km (620mi, 540nmi) with internal auxiliary tank
  • Endurance: 5 hours
  • Service ceiling: 4,500m (14,800ft)
    Hovering ceiling in ground effect: 2,600m (8,530ft)
    Hovering ceiling out of ground effect: 1,600m (5,249ft)

Armament

  • Guns: two fixed 23 mm Type 23-2 (AM-23) cannon on attack variants.
  • Hardpoints: Pylons for rockets, gun pods, ET52 torpedo, HJ-8 anti-tank missiles, or TY-90 air-to-air missiles.

See also

  • List of utility helicopters

Related development

  • Eurocopter AS365 Dauphin
  • Eurocopter Panther
  • Harbin Z-19

Aircraft of comparable role, configuration, and era

  • Sikorsky SH-60 Seahawk
  • Eurocopter HH-65 Dolphin
  • Agusta A109
  • AgustaWestland AW139
  • Bell Huey family
  • Bell 222/230/430
  • Sikorsky S-76
  • TAI T625
  • HAL Dhruv

References

External links

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