Pilatus PC-24

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Twin engined light business jet.

Lift type	Fixed wing	Search for other aircraft programs with these properties on the Aircraft Programs directory page.
Construction type	Factory-built
Control type	Piloted
Engine type	Turbofan
Application	Business, Cargo
Final assembly	Stans (Buochs)

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AMETEK PDS (U.S.A.)	www.ametekpds.com
Cascade Engineering (U.K.)	www.cascade-engineering.co.uk

Airframer

Pilatus Aircraft Ltd

News

Other aircraft programs: Pilatus PC-7 MKII, Pilatus PC-9 M, Pilatus PC-12, Pilatus PC-21

Supply chain

(28 links)

Materials	Coatings (1) Composites (1) Metals (1)
Components	Actuation (2) Lighting (1) Mechanical Connectors (1)
Airframe Systems	Airframe Assemblies (2) Environmental Systems (1) Fluid Power (1) Landing Assemblies (2)
Avionics	Avionic Components (1) Communications (Airborne) (1) Indicators and Instruments (2)
Power Systems	Electrical Power Systems (2) Engines (1) Fuel Systems (1)
Production	Computer Integrated Manufacturing (1) Technical Consultants (1)
Testing	Test Services (2)

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Materials / Coatings

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Materials / Composites

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Components / Actuation

AMETEK PDS	Analysis \| News	Electromechanical Actuators: ACL23A-4 Aileron and Rudder Trim System
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Components / Lighting

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Components / Mechanical Connectors

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Airframe Systems / Airframe Assemblies

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Airframe Systems / Environmental Systems

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Airframe Systems / Fluid Power

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Airframe Systems / Landing Assemblies

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Avionics / Avionic Components

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Avionics / Communications (Airborne)

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Avionics / Indicators and Instruments

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Power Systems / Electrical Power Systems

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Power Systems / Fuel Systems

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Production / Computer Integrated Manufacturing

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Production / Technical Consultants

Cascade Engineering

Analysis

Engineering Design Services: Provided sizing, development, optimisation, advice throughout rear fuselage and vertical tail development; Technical/Eng/Scientific Studies: Provided sizing, development, optimisation, advice throughout rear fuselage and vertical tail development

Testing / Test Services

Cascade Engineering	Analysis	Stress Analysis: Conducted design, development & certification static stress analysis for the rear fuselage and vertical tail
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Information on this page is compiled from a variety of published sources, and links do not necessarily imply recommendation or confirmation by the airframe manufacturer.