Y12F Aircraft Technical Data
Overview
Y12F is a new-generation multi-purpose turbo-prop transport aircraft designed and manufactured by AVIC HAIG. Based on the advantages of Y12 series aircraft, Y12F has been improved in the flight comfort, platform performance, reliability and maintainability. This model features high safety, high reliability and low cost. Y12F aircraft, a nonpressurized high-wing monoplane, adopts normal arrangement of single vertical tail and low horizontal tail, and retractable tricycle landing gears. This aircraft is designed with glass cockpit and double-pilot system. The maximum passenger capacity is 19; the maximum payload is 3 tons. Cargo bay can load 3 LD3 containers. By corresponding retrofit, Y12F model is capable of conducting a wide range of missions, such as VIP transport, maritime surveillance, and aerial photography operations.
Y12F model has been granted CAAC type certificate in Dec. 2015 and FAA type certificate in Feb. 2016.
Dimensions
Overall Data
Overall Data |
Wing span |
19.888 m |
Airframe height |
6.035 m |
Airframe length |
16.47 m |
Wheel track |
3.20 m |
Wheel base |
5.75m |
Cabin
Cabin |
Passenger cabin length |
7.30 m |
Passenger cabin width |
1.90 m |
Passenger cabin length |
1.85 m |
Passenger cabin capacity |
25 m3 |
Luggage compartment
Luggage compartment |
FWD luggage compartment length |
0.64m |
FWD luggage compartment capacity |
0.44m3 |
AFT luggage compartment length |
0.89m |
AFT luggage compartment capacity |
2.68m3 |
Door
Door |
Cockpit door (width × height) |
0.76 m×1.32 m |
Passenger cabin door (width × height) |
0.90 m×1.74 m |
Passenger /cargo door (width × height) |
2.32 m×1.74 m |
FWD luggage compartment door (width × height) |
0.59 m×0.61 m |
AFT luggage compartment door (width × height) |
0.66 m×0.85 m |
Performance data
Capacity
Capacity |
Passenger transport |
2 pilots + 19 passengers |
Freight transport |
2 pilots + 3 LD3 containers/ pallet / bulk product |
Weight
Weight |
Max. ramp weight |
8450 kg |
Max. take-off weight |
8400 kg |
Max. landing weight |
8000 kg |
Max. payload |
3000 kg |
Max. Zero fuel weight |
7750 kg |
Max. useable fuel |
2454 kg |
Flight performance
Flight performance |
Max. level flight speed |
430 km/h |
Economic cruising speed |
380 km/h |
Rate of climb, AEO |
10.1 m/s |
Rate of climb, OEI |
2.25 m/s |
Service ceiling, AEO |
7000 m |
Service ceiling, OEI |
4600 m |
Take-off running distance |
720 m |
Landing distance |
843 m |
Maximum range (45min fuel reserve) |
2255 km |
Maximum range with full load (45min fuel reserve) |
357 km |
Maximum range with passenger full (45 min fuel reserve + 200 nm fuel reserve) |
994 km |
Powerplant data
Powerplant data |
Engine type |
2 PT6A-65B turboprop engines, Pratt&Whitney, Canada |
Power, single engine |
1100 shp |
Operating limitation power |
1000 shp |
Blade quantity |
5 |
Operating limitation
Operating limitation |
Maximum operating height |
7000 m |
Operating Temperature |
-50 ℃~+54 ℃ |
Reliability
Reliability |
TTFO, aircraft |
12000FH/18000C |
Service life of aircraft |
40000FH/62000C |
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