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Solo AC-6

SOLO AC-6.

 

Solo of 15 meters class is intended for training and competitions.

High-fineness tapered wing has laminated profile FX60-157 with high value of accessional force. The outer wing is connected with one butt joint in the middle that has an eccentric at the end for gathering during assembling.

 

 

Aircraft performance AC-6

Wing area

9.5 sc.m.

102.2 sc.f

Wing aspect ratio

23,6

Tare weight

180 kg

397 lbs

Maximum flight weight 

300 kg

661 lbs

Maximum disposable load

120 kg

25 lbs

Range operating overload

+5.3/-2.65

Wing loading with flight weight 210 кг 

31.5 kg/sc.m.

6.45 lbs/sc.f.

Breaking tension on a tow

500 кг.

1120 lbs

 

Main dimensions

Wingspread

15 m

49.2 f

Length of a plane

6.75 m

22.1 f

Height of a plane

1.3 m

4.31 f

 

Speed measures in a gliding flight


Flight weight

300 kg

 

 

Stall speed

- [km/h]

- [miles/h]

- [knots]

72

45

39

 

 

Minimum descent altitude

- [m/sec]

- [f/min]

at a speed of

- [km/h]

- [miles/h]

- [knots]

0,7

138

 

88

54

47

 

 

Maximum speed of aerodynamic quality

- [km/h]

- [miles/h]

- [knots]

Sink rate

- [m/sec]

- [f/min]

90

55

48

 

0.75

150

 

 


 

Restrictions and the basic modes of flight

The maximum aerodynamic quality Кmax (relative range of planning L/H) and value of speeds of the basic modes of flight:

Кmax

42:1

Max. additional speed (Vne)

Max. add. maneuver speed (Va)

200 km/hour (124 miles/hours, 108 knots)

159 km/hour (99 miles/hours, 86 knots)

Corkscrew and figures of difficult pilotage

Deliberate performance of a corkscrew, flights on performance of figures of difficult pilotage are forbidden until the special permission of the Manufacturer

Speed of prelanding planning under normal weather conditions, not less   

100 km/hour (60 miles/hours, 55 knots)


WING

The trapezoid wing of the big lengthening (23,6) has laminar profile FX60-157 with high value of the maximum carrying power.
Specific loading on a wing of 27,5 kg / sq. m at weight of 255 kg. The glider possesses highly maneuvor properties: time
of a rerun for spirals–45 degrees in 45 degrees makes of a list no more than 3,5 seconds.
The sinuosity of a surface of a wing along a profile makes 0,1 mm (under the American standard) that corresponds to the
higher range of quality of a surface under the American standard.
Wing consoles incorporate in the center one adjusting finger having on the end the eccentric for tightening of consoles at
joining. Automatic connection of control systems by elerons and air brakes is realized thanks to system of cross-section
drafts with funneled edge-lines, incorporating to spherical tips of onboard swings.

THE CHASSIS

Glider AC-6 is equipped by a cleaned basic wheel of chamber type with the pneumo-hydraulic shock-absorber. The cylinder of
a wheel in diameter 360х160 mm reliably works on absorption of shock loadings; the tail wheel in diameter of 220 mm stabilizes
s rectilinear movement on run. In a design of the basic wheel ball bearings, and as the brake of "drum" type put in
action with the help of rope cable conducting of type "Bouden" are built in. The brake copes the lever of bicycle type
established on the handle of management.

CABIN

The spacious cabin of a glider allows to take place conveniently in it even to broad-shouldered pilots growth 180 - 190 sm,
thus remain enough empty seat in the field of a head and high knees of legs; the pilot cabin is equipped by pedals of
a wheel of a direction regulated on length and a back of sitting moved largely.
The lantern of a cabin consisting of 2 parts, gives to the pilot the full review outside spaces within corners not
less than 300 degrees: "at the left-upwards-to the right". The lantern Windshield is fixed, and its central part can open
and lean back to the right thanking to a ball-type suspension bracket. Emergency dump of a lantern can be executed by moving
of two red handles conveniently located on both boards of the bottom contours of a lantern.
The compact control panel has enough free space for placing of the standard complete set of pilot-navigating devices, plus
possibility of a custom-made configuration, including an additional variometer or other devices.
The standard 4 dot fastened system is applied. VHF aerial is placed in keel.