Harbin Y-11

Airplanes

Length

12.02 m

Flat Wing Span

17 m

Height

4.64 m

Flat Wing Area

34 m²

Flat Wing Aspect Ratio

8.5

Max Seating

Cruise Speed

175 km/h

Max Speed

220 km/h

Max Ceiling

4000 m

Number of Engines

Aircraft Engine

First Flight

1975-12-30

Number Built

Maximum Take-Off Weight

3.25 t (paragliders: kg)

Total Fuel Capacity

285

Maximum Range

995 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Harbin Y-11	3.25	285	995

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Central Centaur IIA	Beardmore 160 hp	11.8872	19.2024	9	Compare
Fairchild 45-80 Sekani		11.94	17.27	12	Compare
Vulcanair Canguro		12.15	15	9	Compare
Avro Anson		12.8016	17.0688		Compare
Grigorovich MR-5		11.4	15.6		Compare
Caproni Ca.313	Isotta Fraschini Delta	11.8	16.65		Compare

All data (29 fields)

Name: Harbin Y-11
Manufacturer: Harbin Aircraft Manufacturing Corporation
Description: The Harbin Y-11 (NATO reporting name Chan) is a high wing twin-engine piston utility and geological survey aircraft built by Harbin Aircraft Manufacturing Corporation (HAMC).
ICAO Code: Y11
First Flight: 1975-12-30
Designer: Harbin Aircraft Manufacturing Corporation
Type: utility aircraft
Length (m): 12.02
Height (m): 4.64
Cockpit Crew: 2
Max Seating: 8
Max Speed (km/h): 220
Cruise Speed (km/h): 175
Min Speed (km/h): 105
Max Ceiling (m): 4000
Rate of Climb (m/s): 4.0996
Capacity Description: ; 7–8 passengers or; 900 kg chemicals or; 900 L chemicals
Endurance (h): 7
Number Built: 50
Powerplant Description: 2 × Huosai-6A 9-cylinder air-cooled radial engine, 213 kW (285 hp) each
Primary Users: CAAC Airlines
Status: Retired
Wikipedia Article (URL): en.wikipedia.org/wiki/Harbin_Y-11
Flat Wing Span (m): 17
Flat Wing Area (m²): 34
Flat Wing Aspect Ratio: 8.5
Wake Category: L
Aircraft Engine: Ivchenko AI-14
Number of Engines: 2