Pilatus PC-6 포터 - 사진 및 비디오

Pilatus PC-6 Porter
국가	스위스
역할	STOL 여객기 및 다용도 항공기
첫 비행	1959년 5월 4일
내장	600

필라투스 PC-6 포터는 스위스의 필라투스 에어크래프트가 설계한 단일 엔진 STOL 유틸리티 항공기입니다. 1959년에 처음 비행한 PC-6는 스위스 슈탄스의 Pilatus Flugzeugwerke에서 계속 생산되고 있습니다. 피스톤 엔진과 터보프롭 동력 버전으로 제작되었으며 미국의 페어차일드 힐러(Fairchild Hiller)가 한동안 라이선스 하에 생산했습니다. 60년 동안 약 600건의 배송을 마친 필라투스는 2019년 초에 마지막 배송을 할 예정이다.

소스: Pilatus PC-6 Porter의 Wikipedia 님

필라투스 PC-6 포터 산책
사진 작가	블라디미르 야쿠보프
로컬라이제이션	리노 에어 레이스
사진	107

대기,검색 필라투스 PC-6 포터 당신을 위해...

참고 항목:

The Legendary Swiss STOL Bush Transport

Tthe 필라투스 PC-6 포터 (and its turbine-powered counterpart, the PC-6/B Turbo-Porter) is a world-renowned single-engine Short Takeoff and Landing (STOL) utility aircraft designed and built by the Swiss manufacturer Pilatus Aircraft. First flown in 1959 with a piston engine and later upgraded to turboprop power, the PC-6 was engineered to operate out of the world’s most extreme environments—from high-altitude Alpine glaciers to short, unpaved jungle airstrips. Featuring a high-wing configuration, long high-lift wings, a boxy cabin with large double doors, and a rugged taildragger landing gear system, the Porter earned an unmatched reputation as the ultimate bush plane. Over six decades of production, it served military forces, humanitarian agencies, skydiving centers, and covert intelligence operators around the globe.

Attribute	Technical Specification (Pilatus PC-6/B2-H4 Turbo-Porter Standard)
역할	Single-Engine Utility STOL Transport / Skydiving & Bush Aircraft
Crew / Capacity	1 Pilot + up to 10 Passengers (or 1,200 kg / 2,646 lbs cargo load)
동력 장치	1 × Pratt & Whitney Canada PT6A-27 turboprop engine (680 shp, flat-rated to 550 shp)
최대 속도	232 km/h (144 mph / 125 knots) max cruise \| ~96 km/h (60 mph / 52 knots) stall speed
Gross / Takeoff Weight	2,800 kg (6,173 lbs) maximum gross weight \| ~1,270 kg (2,800 lbs) empty weight
Service Ceiling / Operational Range	8,150 m (26,740 ft) ceiling \| ~1,612 km (1,002 miles) max range with external tanks
Takeoff / Landing Distance	Takeoff ground roll: ~197 m (646 ft) \| Landing ground roll: ~130 m (427 ft)
Wing Structure & Dimensions	Wingspan: 15.87 m (52 ft 1 in) \| High constant-chord wing with full-span trailing-edge flaps
Landing Gear & Tail Structure	Fixed heavy-duty taildragger gear with long-stroke oil/pneumatic shock absorbers; wheel, ski, or float options
Production Total	604 units produced in Switzerland by Pilatus (1959–2022) plus 92 licensed Fairchild Hiller units in the US

Design Engineering: Turboprop Integration, Beta Propeller Braking, and High-Lift Wings

High-Lift Unswept Constant-Chord Wing: The PC-6 incorporates a large, rectangular high-mounted wing utilizing a modified NACA 64-series airfoil. Combined with large electrically operated trailing-edge slotted flaps, the wing generates massive lift at low airspeeds, allowing the aircraft to maintain control at speeds down to 50 knots.
PT6A Turboprop Engine & Reversible Beta Pitch: Transitioning from early Lycoming piston engines to the Pratt & Whitney Canada PT6A turboprop transformed the airframe. The engine’s reversible-pitch propeller allows pilots to enter “Beta mode” immediately upon touchdown, providing reverse thrust that halts the aircraft on impossibly short landing strips or permits steep combat dive descents without exceeding speed limits.
High Ground Clearance Taildragger Gear: Built specifically for unprepared turf, mud, or snow, the long-legged main landing gear uses wide-track oleo-pneumatic shock absorbers. The gear layout raises the nose high off the ground, shielding the large propeller blades from debris damage during rough landings.
Modular Box Cabin & Sliding Cargo Doors: The rectangular, slab-sided fuselage maximizes interior volume. Featuring large sliding side doors and removable passenger seating, the cabin can be reconfigured in minutes from passenger transport to freight hauling, air ambulance evacuation, or skydiving jump runs.