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https://en.wikipedia.org/wiki/Harbin_Y-12
The Harbin Y-12 is a high wing twin-engine turboprop utility aircraft built by Harbin Aircraft Industry Group (HAIG). The Y-12 started as a development of the Harbin Y-11 airframe called Y-11T in 1980. The design featured numerous improvements including a redesigned wing with a new low drag section, a larger fuselage and bonded rather than riveted construction. The first prototype, followed by about 30 production Y-12 (I) aircraft before a revised version was produced. This was designated the Y-12 (II), which featured more powerful engines and removal of leading edge slats, first flying on 16 August 1984 and receiving Chinese certification in December of the following year. The power plants are two Pratt & Whitney Canada PT6A-27 turboprops with Hartzell propellers. The Y-12 has a maximum takeoff weight of 5,700 kg (12,600 lb) with seating for 17 passengers and two crew. The aircraft is operated as a light commuter and transport aircraft. The latest development is Y-12F, which is almost a new design with many improvements: new wings, new landing gears, new fuselage, with more powerful engines from Pratt & Whitney Canada and extended payload and range. The Y-12F made its maiden flight on December 29, 2010, received the CAAC type certification on December 10, 2015, and the FAA type certification on February 22, 2016. In 2015 Kenmore Air announced that they would begin development of floats for the Y-12 for FAA certification. The Y-12 completed the FAA evaluation flight tests for its automatic flight control system on June 30, 2018, with its performance meeting the requirements, said AVIC Harbin Aircraft Industry Company Ltd (AVIC HAFEI). Role Twin-engine turboprop utility aircraft National origin China Manufacturer Harbin Aircraft Industry Group First flight 14 July 1982 Status Active, In production Primary user People's Liberation Army Air Force Produced 1985 - present Unit cost US$3 million (1998) Developed from Harbin Y-11 Specifications (Y-12 (II)) General characteristics Crew: 2 Capacity: 17 pax / 1,700 kg (3,748 lb) max payload Length: 14.86 m (48 ft 9 in) Wingspan: 17.235 m (56 ft 7 in) Height: 5.575 m (18 ft 3 in) Wing area: 34.27 m2 (368.9 sq ft) Airfoil: LS(1)-0417 Empty weight: 2,840 kg (6,261 lb) Max takeoff weight: 5,300 kg (11,684 lb) Fuel capacity: 1,616 l (427 US gal; 355 imp gal) / 1,230 kg (2,712 lb) max usable fuel weight Powerplant: 2 × Pratt & Whitney Canada PT6A-27 turboprop engines, 462 kW (620 hp) each Propellers: 3-bladed Hartzell HC-B3TN-3B/T10173B-3, 2.49 m (8 ft 2 in) diameter constant-speed fully-feathering reversible-pitch propellers (4 and 5 bladed propellers used on some models) Performance Maximum speed: 328 km/h (204 mph, 177 kn) VMO (maximum operating speed) at 3,000 m (9,843 ft) Cruise speed: 292 km/h (181 mph, 158 kn) (max) at 3,000 m (9,843 ft) 250 km/h (160 mph; 130 kn) (economical) at 3,000 m (9,843 ft)Range: 1,340 km (830 mi, 720 nmi) at econ cruise, 45 min reserves at 3,000 m (9,843 ft) Endurance: 5 hours 12 minutes at econ cruise Service ceiling: 7,000 m (23,000 ft) 3,000 m (9,843 ft) on one engineRate of climb: 8.1 m/s (1,590 ft/min) 1.4 m/s (4.6 ft/s) on one engineWing loading: 145.9 kg/m2 (29.9 lb/sq ft) Power/mass: 0.106 kW/kg (0.064 hp/lb) Take-off run: 370 m (1,214 ft) Take-off run to 15 m (49 ft): 490 m (1,608 ft) Landing run: 340 m (1,115 ft) Landing run from 15 m (49 ft): 630 m (2,067 ft) * |
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Miloch wrote in
: https://en.wikipedia.org/wiki/Harbin_Y-12 The Harbin Y-12 is a high wing twin-engine turboprop utility aircraft built by Harbin Aircraft Industry Group (HAIG). Harbin is a city in northern China known for it's ice festival. |
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In article , Mitchell Holman
says... Miloch wrote in : https://en.wikipedia.org/wiki/Harbin_Y-12 The Harbin Y-12 is a high wing twin-engine turboprop utility aircraft built by Harbin Aircraft Industry Group (HAIG). Harbin is a city in northern China known for it's ice festival. ....better known now days for its corona virus lockdown! https://www.scmp.com/news/china/soci...wn-bid-contain * |
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