首頁 > Y12E
            Y12E Aircraft Technical Data

            Overview

            Y12E airplane is of a multi-purpose aircraft developed by AVIC HAIG. The aircraft features twin engine, high monoplane, shear wing-tip, single vertical tail, low horizontal tail and fixed tricycle landing gears.


            Y12 E aircraft has been type-certified by CAAC in Dec. 2001, type-certified by FAA in Aug. 2006. In Aug. 2015, Y12E obtained Russia IAC AR VTC.


            Easy to operate and high maneuverability, Y12E is able to take off and land on high and hot airfield as well as unpaved strip. It can be operated during day or night in VFR and IFR. The deicing unit equipped on the empennage enables the aircraft to be operated in icing conditions. It is applicable to passenger/cargo transportation, aerial photography, flight training, air drop and parachuting, EMS, maritime surveillance, agriculture and forestry, artificial precipitation, geological surveys, SAR, etc.

            Dimensions

            Overall Data

            Overall Data
            Wing span 19.2 m
            Airframe height 5.675 m
            Airframe length 14.86 m
            Wheel track 3.61 m
            Wheel base 4.702 m

            Cabin data

            Cabin data
            Passenger cabin length 4.82 m
            Passenger cabin width 1.6 m
            Cabin length 1.70 m
            Effective capacity 12.00 m3

            Luggage compartment

            Luggage compartment
            FWD luggage compartment length 0.96 m
            FWD luggage compartment capacity 0.77 m3
            AFT luggage compartment length 1.00 m
            AFT luggage compartment capacity 1.89 m3

            Cabin door data

            Cabin door data
            Cockpit door (width × height) 0.65 m×1.12 m
            Passenger cabin door (width × height) 0.65 m×1.38 m
            Passenger /cargo door (width × height) 1.45 m×1.38 m
            FWD luggage compartment door (width × height) 0.75 m×0.60 m
            AFT luggage compartment door (width × height) 0.65 m×0.91 m

            Performance data

            Capacity

            Capacity
            Passenger transport 2 pilots + 18 passengers

            Weight data

            Weight data
            Max. ramp weight 5700 kg
            Max. take-off weight 5670 kg
            Max. landing weight 5400 kg
            Max. payload 1984 kg
            Max. Zero fuel weight 5188 kg
            Max. useable fuel 1230 kg

            Flight performance

            Flight performance
            Max. level flight speed 344 km/h
            Economic cruising speed 270 km/h
            Rate of climb, AEO 7.8 m/s
            Rate of climb, OEI 1.5 m/s
            Service ceiling, AEO 7000 m
            Service ceiling, OEI 4200 m
            Take-off running distance 465 m
            Landing distance 590 m
            Maximum range (45min fuel reserve) 1340 km
            Maximum range with full load (45min fuel reserve) 382 km

            Powerplant data

            Powerplant data
            Engine type 2 PT6A-135A turboprop engines, Pratt&Whitney, Canada
            Power, single engine 750 shp
            Operating limitation power 620shp
            Blade quantity 4

            Operating limitation

            Operating limitation
            Maximum operating height 7000 m
            Operating Temperature -50 ℃~+50 ℃

            Reliability

            Reliability
            TTFO, aircraft 4000FH/6000C
            Service life of aircraft 36000FH/54000C
            Note:The data above are used for presentation only; they may vary with different conditions.

            AVIC HAIG Aircraft Sales Department

            Telephone:86-0451-86582224
            Fax:86-0451-86582881
            E-mail:feijixiaoshou@avic.com

            Tel: 86-0451-86583902 Fax: 86-0451-86582881 Mail: feijixiaoshou@avic.com ICP record number: 黑ICP備20001170號-1
            影音先锋最av资源