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:[email protected]

Tel: 86-0451-86583902 Fax: 86-0451-86582881 Mail: [email protected]
体彩七星彩走势图