Light multi-purpose aircraft type Y1 "DELFIN"
Aircraft Yl "Delfin" is designed for as follows:
- primary flight training of pilots;
- carrying out of flights within local airlines;
- carrying out of flights for monitoring of the ground and water surfaces.
Aircraft Yl "Delfin" provides carrying out of the following main tasks as follows:
- in the multi-purpose category:
- training for fundamentals of pilot technique (circuit flights, zone flight for elementary and advanced flying);
- training for spin performance and going out of the spin;
- training for fundamentals of navigation;
- training for instrument flight technique during landing approach with Landing systems usage;
- training for actions in special cases;
- in the normaL category:
- performance of planned-route flights.
Sizes and areas | |
AIRFRAME |
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Length, m | 8,000 |
Height in the parking area,m | 3,005 |
Wing span, m | 9,976 |
LANDING GEAR |
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Parking track, m | 2,864 |
Parking base, m | 1,884 |
WING |
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Area, m2 | 13,3 |
CABIN |
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Length, m | 2,366 |
Width, m | 1,12 |
Height, m | 1,16 |
WEIGHT DATA |
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Maximum takeoff weight, kg | 1400 |
Maximum usable fueL capacity, L | 170 |
Maximum payLoad weight, kg | 440 |
Flight characteristics |
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Maximum allowable speed, km/h | 350 |
Maximum horizontal flight speed, km/h | 310 |
Cruising speed, km/h | 280 |
Maximum flight altitude, m | 3000 |
(according to the cabin un-pressurization conditions |
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and absence of oxygen equipment) |
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Flight range with fuel reserve for 30 minutes of flight |
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with takeoff weight 1300 kg, km | 1650 |
Engine SR-305-230
The aircraft is equipped with a four-cylinder piston engine of diesel cycle with direct fuel injection, this engine is designed and manufactured by the French company SMASAFRAN.
The power plant incorporates three-blade variable-pitch propeller
MTV9-B-S/198-58B produced by MT Propeller, Germany.
With the help of the propeLLer hydraulic governor engine speed is maintained constant (2200 rev/ min) during the entire running time.
Engine type | SR-305-230 |
Fuel: aviation kerosene | Jet-A,Jet-Al,TC-l |
Maximum power | 230 l/s |
Fuel consumption per hour | 33-35 l/h |
Maximum steady speed | 2200 rpm. |
Two variants of aircraft onboard equipment completeness are used.
The first variant - onboard equipment on the base of analog instruments. The second one - onboard equipment according to the type of "glass cabin" on the base of onboard radio electronic complex GARMIN (USA).
The equipment installed on aircraft provides the aircraft operation with one pilot according to the instrument flight ruLes and makes it possible to solve the tasks of short-range navigation, providing the operation with any radio beacons VOR or NDB and satellites GPS NAVSTAR.
Advantages oF the aircraft as compared with analogs
The usage of emergency systems | ||
Aircraft systems | The main system | Emergency system |
Engine control | Electronic | Mechanic |
Landing gear retraction and extension system | Electrical drive | Mechanical drive |
Electric system | Generator Emergency accumulator
| Main accumulator |
The usage of doubling systems | ||
Aircraft systems | Back-up system | |
Fuel consumption measurement | Two independent systems: - fuel measuring system; - fuel consumption measurement. | |
Radio, flight-control and navigation equipment | The doubling of: - Altimeter; - Speed indicator; - Gyrohorizon; - Course system; - Radio set. |