TYPE CERTIFICATE № СТ357-Y12
Issued by Aviation Register of the Interstate Aviation Committee.
21 August 2015
PRESENTATION OF THE FIRST CERTIFICATE IN THE HISTORY ON THE CHINESE AIRCRAFT WAS HELD AT THE OFFICIAL EVENT OF MAKS-2015
TYPE CERTIFICATE ISSUED BY CAAC
TYPE CERTIFICATE ISSUED BY FAA
TYPE CERTIFICATE ISSUED BY CAA
|Engine||Manufacturer||Pratt & Whitney Canada|
|Takeoff/Max. continuous power (SHP)||750|
|Operation limit power (SHP)||620|
|Np limit (RPM)||1900|
|Qty. of blade (pc)||4|
Y12 series aircraft are equipped with engine air intake anti-icing system and propeller electric de-icing system.
|Overall length (m)||14.86|
|Overall Height (m)||5.675|
|Wing span (m)||19.2|
|Wheel track (m)||3.61|
|Nose wheel track (m)||4.702|
|Cabin length (m)||4.82|
|Cabin width (m)||1.6|
|Cabin height (m)||1.7|
(height by width) (m)
|1.38 х 1.45|
|Cabin capacity (m3)||12|
compartment capacity (m3)
hold capacity (m3)
|Max. takeoff weight||5670 kg|
|Max. landing weight||5400 kg|
|Max. payload||1984 kg|
|Fuel weight||1230 kg|
|Max. cruising speed||340 kmph|
(carrying 19 passengers)
(with full fuel)
|Operating ceiling||7000 m|
(with one engine inoperative)
|Takeoff distance||450 m|
|Landing distance||590 m|
|Diagrammatic navigation system|
|GPS, VHF Communication and navigation system|
|Single band radio|
|Automatic direction finder|
|Air data computer|
|Cabin voice recorder|
High reliability Common mechanical control system
Rudder control system
Elevator control system
Aileron control system
Fixed tricycle landing gear
a strut type structure of nose landing gear
a rocker arm type structure of main landing gear
Hydraulic power system functions to control main wheel braking, differential braking, and aircraft parking braking.
It consists of hydraulic power supply, indication system and wheel braking system (normal and emergency breaking system separately).
The accumulator is supplied with the hydraulic energy produced by electric pump or hand pump.
The DC power supply system consists of two DC starter generators (28V, 6KW) and a set of nickle-cadmium battery (43amh).
Secondary (AC) power supply system consists of two single-phase static inverters (115V/26V,400Hz, 600VA) which operates together.
The aircraft is equipped with an external 28VDC power supply receptacle.
The power supply system is provided with a protection and monitoring device.
|TIME BEFORE OVERHAUL|
6000h or 9000 cycles
Cargo transportation version：
Main retrofits in parachute version:
Maritime survey version:
Maritime environment survey and law enforcement
Aerial camera etc.
Crew and occupants：
2 pilots + 3 operators
Photography version：Aerial photography
Aerial camera RC30
Full-digital 3D color remote sensing system
RAMSTM “3S” integration system
Crew and occupants：
2 pilots + 1 operator
Rescue version:Mission equipment：
Geological survey version:
Land and resources investigation and survey
Artificial rainfall version:
Artificial rainfall in the droughty or rainless regions
Your request has been accepted.
Information with the application has been sent to you on the mail
In the near future our managers will contact you for details.