Specification SP-30

Geometrical data

Length, m

6,3

High, m

2,69

Maximum fuselage width, m

1,2

Base chassis, m

1,4

Wheel track, m

1,8

Size of pneumatic tires of the wheels

440х190

Wing:
- wing span, m
- wing area, m2
- area drooping ailerons, m2


9,4
13,4
0,98х2

Empennage:
- vertical empennage area , m 2
- horizontal empennage area, m 2
- elevator area, m 2


0,98
2,3
1,21

Weight and center of gravity data

Weight of the empty aircraft, kg

350

Maximum take-off weight, kg

500

Centre of gravity range:
- very front %
- very rear %


20
35

Engine data

Engine

- model

ROTAX 912 ULS

- type

four-stroke, four-cylinder, opposed

- Power
at takeoff, h.p.
at maximum continuous rating, h.p.
at 75% engine speed, h.p.


100 with n=5800
95 with n=5500
78 with n=4350

- fuel rate (l/h)
hourly takeoff fuel consumption
hourly continuous rating consumption
hourly consumption at 75% engine speed


22,7
21,3
16,2

Service data

Amount of fuel tanked, l

60

Operating oil amount, l

2,5

Coolant amount, l

1,5

Pressure in the pneumatic wheels, kg/sm2

1,6

Flight performance data

Speeds

- maximum horizontal flight speed

140 km/h

- cruise speed

110 km/h

- stall speed

55 km/h

- climb rate

3,0 m/s

Maximum altitude

3000m

Maximum time of flight

3 h + 3h with extra fuel tank

Effective width

20m

Flow rate of the working fluid

3-8 l/hectare.

Average output

100 hectare/h.

Operating limitations

Outside air temperature near earth, о С

+45
-10

Minimal conditions of flight

- time of the day

day

- height of the lowed edge of the clouds, m

150

- horizontal visibility, m

3000

- maximum altitude, m

3000

- maximum wind velocity for takeoff and landing, m/s
- headwind
- lateral wind


12
6

Maximum takeoff weight, kg

520

Maximum takeoff weight of crew, cargo and fuel, kg

215

Maximum allowable flight speed, km/h

- in take off configuration 150

120

- in landing configuration 300

95

Non-exceeding speed (solidity conditions), km/h

180

Maximum operating overload

+4

Minimal operating overload

-2

Maximum angle of bank , degree

60

Limitation of the engine and it's systems (reference)

- duration of negative overload

no more than 5 sec.

- time of incorrect work on low gas (n=1400 rpm)

no more than 5 min

- time of incorrect work on takeoff

no more than 5 min

Maximum valid frequency of rotation of a cranked shaft, rpm

5800

Maximum valid temperature of cylinder heads, 0С

150

Minimal valid temperature of cylinder heads, 0С

50

Maximum valid oil temperature, 0С

140

Minimal oil pressure, kg/sm2

1,5

Maximum oil pressure, kg/sm2

5,0

Maximum short-term oil pressure during cold starts, kg/sm2

7,0

SP-30 in Australia, New Zealand, USA and the world:
Spectr SP-30: English Speaking Representative: Australia, ph.: +61(431) 244-940; www.sp-30.com e-mail in english: smehatylka19@gmail.com
Russian speaking manufacturer, Производитель СП-30 в России: tel. (russian speaking only) +7(928) 175 44 36
e-mail in russian: bonal2@mail.ru

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