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Military Helicopters ·PZL-Świdnik

W-3 Sokol

Polish utility helicopter, renowned for search and rescue missions, particularly during UN peacekeeping operations in Bosnia-Herzegovina in the 1990s.

PZL-Świdnik W-3 Sokol military helicopters in flight
Origin country
🇵🇱 Poland
First flight
1979Nov 16
Introduced
1986
Produced
149units
Active worldwide
86
PZL-Świdnik W-3 Sokol military helicopters side profile drawing
Side profile · PZL-Świdnik W-3 Sokol · length 14.2 m
Technical SpecificationsVersion: W-3A
Crew2 members
Length14.2 m (46.6 ft)
Wingspan15.7 m (51.5 ft)
Height5.1 m (16.9 ft)
Empty weight3,850 kg (8,488 lbs)
Max. takeoff weight6,400 kg (14,110 lbs)
Powerplant2 × turboshafts PZL-Rzeszów PZL-10W 662 kW each
PerformanceVersion: W-3A
Maximum speed260 km/h (162 mph)
Operational range745 km (463 mi)
Service ceiling4,910 m (16,109 ft)
Climb rate9.3 m/s (30.5 ft/s)
Operators — 2026
ActiveOn order
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🇨🇿 Czechia· 🇩🇿 Algeria· 🇲🇲 Myanmar· 🇵🇭 Philippines· 🇵🇱 Poland

Description

The PZL W-3 Sokół is a medium-size, twin-engine multipurpose helicopter manufactured by Polish company PZL-Świdnik (now Leonardo). Designed as the first helicopter developed and produced entirely in Poland, the type was built to fulfill military and civil requirements across Poland and the Warsaw Pact. The prototype conducted its maiden flight on 16 November 1979, and serial production began in 1985.

Development

In 1973, design work commenced at PZL Świdnik under an in-house team led by Stanisław Kamiński to address military and civil requirements for Soviet and Warsaw Pact operators. Production began in 1985, and the Soviet Chief Inspectorate of Civil Aviation issued provisional airworthiness certification on 26 September 1988. The W-3A variant achieved US FAA FAR Part 29 certification in May 1993, and the 100th aircraft was completed in June 1996. Development of an attack derivative designated the Huzar was initiated in the 1990s but was cancelled in 1999 due to delays and integration disputes. Later development focused on modernization, leading to the W-3PL Głuszec combat search and rescue variant equipped with FADEC software, upgraded flight controls, and glass cockpit avionics.

Design

The W-3 is powered by two Pratt & Whitney Rzeszów PZL-10B turboshaft engines rated at 671 kW (900 hp) each. Composite materials are incorporated into the four-bladed main rotor and three-bladed tail rotor, which feature electrical ice protection allowing operations between -40 and +43°C. Naval and search-and-rescue configurations carry floats, a transponder, GPS navigation, night-vision equipment, and a Lucas winch. Modernized military variants feature glass cockpits with multi-function displays, HUD, TACAN, INS/GPS navigation, and radar warning receivers.

Armament

The armed W-3W and W-3WA variants feature four weapon pylons and an integrated twin 23 mm GSz-23L cannon. The W-3PSOT and W-3PL Głuszec variants retain weapon pylons but substitute the cannon for a single pilot-controlled 12.7 mm WKM-Bz machine gun with 350 rounds. Prototype configurations were tested with Mars-2, B8-10, and ZR-8 pods, 9M114 missiles, ZT3 Ingwe ATGMs, and HOT-3 missiles.

Operational History

The Polish Armed Forces operate the type across land, air, naval, and government VIP transport roles. In 1996, Poland transferred 11 W-3 helicopters to the Czech Republic in exchange for 10 Mikoyan MiG-29 fighters. Eight Polish W-3WA helicopters deployed to Iraq between 2003 and 2008 for coalition operations, including leaflet distribution; two aircraft were lost in crashes in 2004 and 2006. Export customers include the German Saxony State Police, the Philippine Air Force, the Myanmar Air Force, and South Korean commercial operators Citiair and Helikorea.

Variants

  • W-3A Sokół: Civil and military transport variant certified to US FAA FAR Part 29 standards.
  • W-3W / W-3WA Sokół: Armed military version equipped with a twin 23 mm GSz-23L cannon and four weapon pylons.
  • W-3RM Anakonda: Navalized search and rescue variant equipped with floats and maritime equipment.
  • W-3PL Głuszec: Modernized combat search and rescue upgrade featuring glass cockpit avionics, FADEC engine controls, and a 12.7 mm machine gun.
  • W-3P/S/A VIP Sokół: Dedicated transport configuration operated for government and official airlift duties.

Frequently Asked Questions

What type of aircraft is the W-3 Sokol?
The PZL-Świdnik W-3 Sokol is a military helicopters aircraft developed by PZL-Świdnik and entered service in 1986.
What is the maximum speed of the W-3 Sokol?
The PZL-Świdnik W-3 Sokol has a maximum speed of 260 km/h (161 mph).
What is the range of the W-3 Sokol?
The PZL-Świdnik W-3 Sokol has an operational range of 745 km (462 miles). This range can vary based on payload, altitude, and mission profile.
When did the W-3 Sokol first fly?
The PZL-Świdnik W-3 Sokol made its first flight on November 16, 1979. It entered operational service in 1986.
How many W-3 Sokol have been built?
Approximately 149 units of the PZL-Świdnik W-3 Sokol have been produced since it entered service in 1986.
Which countries operate the W-3 Sokol?
The PZL-Świdnik W-3 Sokol is operated by 5 countries with approximately 86 aircraft in active service. The largest operators include Poland, Myanmar, and Czechia.
What is the service ceiling of the W-3 Sokol?
The PZL-Świdnik W-3 Sokol has a service ceiling of 4,910 meters (16,108 feet). This is the maximum altitude at which the aircraft can maintain controlled flight.
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