PZL Swidnik SW-4 - program supplier guide | Airframer

PZL Swidnik SW-4

In production

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Overview Supply chain (2) Downloads

Single turboshaft light utility helicopter.

Lift type

Rotary wing

Assembly

Factory-built

Control

Piloted, Remotely piloted

Engine type

Turboshaft

Application

Agricultural, Business, Cargo, Military transport, Search & rescue, Surveillance, Utility

Design & construction

The aircraft as engineered: what it is built from, the systems it flies with, and its configuration — each box a theme.

Airframe & structure

Primary structure

Mixed

Landing gear

Skids

Ice protection

None

Pressurisation

Unpressurised

Systems & avionics

Autopilot

3-axis

Avionics architecture

Integrated glass suite

Configuration & certification

Rotor configuration

Single main + tail

Certification

Part 27

Minimum crew

Notable technologies — each tag names a technology on our research record for this aircraft, with its fitting status: Primary, Standard, Option or Planned.

Composite fuselage (primary structure) Standard

Technical reference compiled with AI research; a value appears only where two independent research passes and a web fact-check agree. Gaps are deliberate.

A deeper insight into the PZL Swidnik SW-4

Supplier geography and market analysis for this program — with an Analytics subscription.

The industry ledger — an Analytics feature — holds every dated event on this program: contracts, certifications, first flights and appointments, each linked to its source. See a worked example →

Type variants

Variant	Launch / first flight	Notes
PZL Swidnik SW-4	1994 / 1996	Production: 3 (2016) GAMA: Leonardo SW4. Light utility helicopter, as of 2016 civil varaint designated AW009 and military variant retained SW-4 name.
PZL Swidnik SW-4 Solo	2012 / 2016	RUAS/OPH variant.
PZL Swidnik AW009	2016 / 2016	Civil variant.

Airframer

PZL Swidnik S.A.

News

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The program’s dated history — milestones, contracts, supplier selections and facilities, each linked to its source. Log in to view.

Information on this page is compiled from a variety of published sources; links do not necessarily imply recommendation or confirmation by the airframe manufacturer.