Pilatus PC-6 Porter

Summary

Category	Transport aircraft
Origin country	🇨🇭 Switzerland
First flight	4 May 1959
Year of introduction	1960
Number produced	604 units
Average unit price	$0.1 million

Description

Designed by Pilatus Aircraft of Switzerland, the PC-6 Porter is a single-engine STOL utility aircraft that first flew on 4 May 1959 with a 254 kW (340 shp) piston engine. In May 1961, the first Turbo Porter, equipped with a Turbomeca Astazou II turboprop engine, conducted its maiden flight. The Astazou II variant offered increased gross capacity and top speed, as well as automatic handling functions. Early turbine-powered models initially used the Astazou II powerplant, however, reliability concerns led to the adoption of the Garrett AiResearch TPE 331 as an alternative. By May 1966, the first PC-6 equipped with the Pratt & Whitney Canada PT6A engine performed its initial flight. Production primarily occurred at Pilatus Flugzeugwerke in Stans, Switzerland, but was also undertaken under license by Fairchild Hiller in the United States. To mitigate manufacturing costs, Pilatus distributed production work to other countries, including the Czech Republic and, later, China, with the intention of eventually transferring global production to a facility in Chongqing. After 604 deliveries, Pilatus ended production in 2022.

Most PC-6s are powered by a single Pratt & Whitney Canada PT6A turboprop engine, driving a fully reversible, constant-speed, three-bladed HC-B3TN-3D or a four-bladed HC-D4N-3P Hartzell aluminium propeller. The aircraft’s undercarriage is designed to provide high wing and propeller clearances, reducing its susceptibility to damage on unprepared surfaces; various landing gear types, including floats and skis, can be installed. The airframe is constructed to be rugged and require low maintenance, with high accessibility and interchangeability of parts. The wings, fuselage, and empennage are manufactured using conventional semi-monocoque construction techniques, with the primary structure composed of aluminium, treated for corrosion resistance; the central structure retains critical strength despite the cutout areas for the main cabin’s sliding doors. For role flexibility, individual aircraft can be converted for various mission types, such as transport, paradrop, aerial photography, surveillance, air medical services, and search and rescue.

The PC-6 has seen deployment in various theaters around the world, often operating from challenging environments that would be inaccessible to most fixed-wing aircraft. During the Vietnam War, the CIA-controlled airline Air America operated up to 23 PC-6s for missions including paradropping supplies, transporting passengers, conducting psychological warfare, performing reconnaissance, and other intelligence operations. Since 1976, the Austrian Air Force has utilized a fleet of 12 PC-6 Porters in support roles such as transport, search and rescue, firefighting, observation, target-towing, and paradropping. The AU-23A Peacemaker, a gunship version used by the U.S. Air Force during the Vietnam War, proved troublesome and was quickly withdrawn from service. In 1996, a PC-6 was used in Zaire during the First Congo War, but it was lost due to an accident shortly after arriving. Its operational strengths lie in its STOL capabilities, allowing it to operate from short, unprepared airstrips in remote areas and at high altitudes. A noted weakness, particularly in early models, was the reliability of the Turbomeca Astazou II engine, which led some operators to retrofit their aircraft with the Garrett AiResearch TPE 331. The PC-6 has been used globally by various military, law enforcement, and civil operators, with a significant portion of the European fleet being utilized for skydiving activities.

Main Variants:

PC-6/340 Porter: The initial production version, it was powered by a 254-kW (340-hp) Lycoming GSO-480-B1A6 flat-six piston engine and had a maximum takeoff weight of 1,960 kg (4,320 lb).
PC-6/A Turbo-Porter: This was the initial turboprop-powered version, fitted with a 390 kW (523 shp) Turbomeca Astazou IIE or IIG turboprop engine.
PC-6/B Turbo-Porter: This variant was powered by a 410-kW (550-shp) Pratt & Whitney Canada PT6A-6A turboprop engine.
PC-6/B2-H4 Turbo-Porter: This version featured improved airframe structuring and extended, upturned wingtips.
AU-23A Peacemaker: An armed gunship, counter-insurgency, and utility transport version for the U.S. Air Force, 15 were built under license in the USA by Fairchild Industries and used during the Vietnam War in the early 1970s.

Technical specifications

Version: PC-6/B
Crew	1 pilot
Maximum speed	244 km/h (152 mph)
Wing area	30.2 m² (324.5 sqft)
Wingspan	15.9 m (52.1 ft)
Height	3.2 m (10.5 ft)
Length	10.9 m (35.8 ft)
Service ceiling	10000 m (32808 ft)
Empty weight	1260 kg (2778 lbs)
Max. takeoff weight	2800 kg (6173 lbs)
Climb rate	5.13 m/s (16.8 ft/s)
Takeoff distance	152 m (499 ft)
Powerplant	1 × turboprop Pratt & Whitney Canada PT6A-27 delivering 410 kW