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Official dealer of aircraft Y12

Aircraft Y12 E

Самолет Y12 E

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

Type Y12E
Engine Manufacturer Pratt & Whitney Canada
Type PT6A-135A
Takeoff/Max. continuous power (SHP) 750
Operation limit power (SHP) 620
Qty. (set) 2
Propeller Manufacturer HARTZEL, USA
Type HC-D4N-3N/D9511FK
Qty. (set) 2
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
Cabin door
(height by width) (m)
1.38 х 1.45
Cabin capacity (m3) 12
Front baggage
compartment capacity (m3)
0.77
Rear luggage
hold capacity (m3)
1.89
Max. takeoff weight 5670 kg
Max. landing weight 5400 kg
Max. payload 1984 kg
Fuel weight 1230 kg
Max. passenger 19
Max. cruising speed 340 kmph
Max. range
(carrying 19 passengers)
650 km
Max. range
(with full fuel)
1310 km
Operating ceiling 7000 m
Operating ceiling
(with one engine inoperative)
4149 m
Takeoff distance 450 m
Landing distance 590 m
VFR
Horizon
Heading indicator
Air speed indicator 
Magnetic compass
Altimeter
 
Instrument of Engine
Instrument of Power supply system
Instrument of Fuel system
Instrument of hydraulic system
IFR
DME VOR navigation system
Marker beacon receiver
Gliding receiver
Coding altimeter
Diagrammatic navigation system
GPS, VHF Communication and navigation system
VOR indicator
Single band radio
Audio center
Automatic direction finder
Responder
Radio altimeter
Vertical gyro
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.

Optional systems

The heating system is designed to mix the bleed air from engine with the cold air sucked by means of injector for heating in the cockpit and cabin. The ram and natural air ventilation is designed for ventilation system in the cockpit and cabin.

Aircraft Y12E

SERVICE LIFE
  • Airframe service life
36000h/54000 cycles
TIME BEFORE OVERHAUL
  • Initial TBO
  • Engine PT6A-135A
  • Propeller HC-D4N-3N/D9511FK
6000h or 9000 cycles
3800h
4000h

Main Purposes

Cargo transportation version:

Parachute version:

Main retrofits in parachute version:

Maritime survey version:
Maritime environment survey and law enforcement

Mission equipment:

Search radar
Infrated survey
equipment
Aerial camera etc.

Crew and occupants:

2 pilots + 3 operators

Photography version:Aerial photography

Mission equipment:

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:
Stretcher (3 sets of stretcher for each group,total 6/9 sets of stretcher for 2/3 groups)
First-aid kit
Standard seats
Crew and occupants:
2 pilots + 6 seriously wounded persons + 4 minor wounded persons/medical staff

Geological survey version:
Land and resources investigation and survey

Mission equipment:
VLF probe
Magnetic probe
Control cabinet
Crystal box
Photography window
Crew and occupants:
2 pilots + 1 navigator + 1 operator

Artificial rainfall version:
Artificial rainfall in the droughty or rainless regions

Mission equipment:
Catalyst spreader
Airborne silver iodide spreader
Airborne silver iodide cartridge launching system
Airborne dry ice spreader
Physical detection equipment for cloud and rain
Airborne PMS system “120” ice particle counter
Airborne tester for liquid water content
Console
Tape recorder
CRT droplet spectrum display
CPU
Crew and occupants:
2 pilots + 3 operators

info@flavicaero.com tel: 971-56-714-77-54 ru en

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