Overview: The Pilatus Porter PC-6, known as "The Porter," is renowned for its exceptional short take-off and landing (STOL) capabilities, reliability, and versatility in various weather and terrain conditions. It is designed to operate from unprepared, rough, and short airstrips, making it suitable for remote areas and high altitudes.

Specifications: The aircraft is powered by a 550 shp Pratt & Whitney Canada PT6A-27 Turboprop Engine with a thermodynamic rating of 680 shp. It features a glass cockpit designed for single-pilot operation, with optional co-pilot controls. The Porter can be customized with individual exterior paint schemes and is easily convertible for missions such as transport, para-dropping, aerial photography, surveillance, and search and rescue.

Features: The PC-6 includes a Hartzell three-blade aluminum propeller, with a four-blade option available. It has landing gear suitable for various unprepared airstrips, with optional floats and skis. The aircraft has large sliding doors on both sides, a spacious cabin accommodating up to 10 passengers or over 2,200 lb (1,000 kg) payload, and passenger seat stowage in the rear fuselage. An optional trap door for in-flight operations is also available.

Performance: Under international standard atmospheric conditions, the PC-6/B2-H4 has a take-off distance over a 50 ft obstacle of 1,444 ft (440 m) and a landing distance of 1,033 ft (315 m). It has a maximum rate of climb of 1,010 ft/min (5.13 m/sec), a maximum cruise speed of 125 KTAS (232 km/h), and a maximum range of 500 nm (926 km) at 10,000 ft, extendable to 870 nm (1,611 km) with underwing tanks. The maximum certified altitude is 25,000 ft (7,620 m), with stall speeds of 58 KEAS (107 km/h) with flaps up and 52 KEAS (96 km/h) with full flaps.

Weights and Dimensions: The basic operating weight is 2,756 lb (1,250 kg), with a maximum take-off weight of 6,173 lb (2,800 kg) and a maximum landing weight of 5,863 lb (2,660 kg). The maximum payload is approximately 2,646 lb (1,200 kg), or 2,381 lb (1,080 kg) with full fuel. The aircraft's dimensions include a wing span of 52 ft 1 in (15.87 m), a length of 35 ft 9 in (10.9 m), and a height of 10 ft 6 in (3.20 m).