BGA glider data sheet - ASW 28

Data source: BGA & FAA data

Date of issue: 2001

Manufacturer: Fa. A Schleicher GmbH & Co, Segelflugzeugbau, 36161 Poppenhausen, Germany

UK Agent: Peter Wells

E Mail: zuluglasstek@clara.net

Phone: 01844 208 157

Link to mandatory mods:

Fax: 01844 201 028

Weighing Data:

Kg Pounds

Max weight with water

525

Max weight (dry)
BGA concession non-aerobatic max weight (dry) [+3%]
Max weight of non lifting components (everything except wings)
BGA concession non-aerobatic
max weight of non lifting components [+5%] Max pilot weight (seat load) Baggage compartment
Forward C of G limit (aft of datum) Aft C of G limit (aft of datum) Pilot position (forward)

380 391 260
273
12 mm 222 345

1157 838 863
573
602
26.5 Inches 8.74 13.58

Control deflections in degrees

Up

Down

Controls mass

& moments

Ailerons 20° - 25° 12° - 15° Elevator 18° - 22° 18° - 22°
Rudder left and right 29° - 33°

Controls max free play (controls central)

Longitudinal datum: Wing root LE Horizontal datum: Rear fuselage sloping rear down 49: 1000 Put a maximum of 1 Kg of water in the fin tank for every Kg in the wings.

Knots

VNE

146

Rough air 108

Winch / 75 auto tow

Maximum speeds

Kph Knots

270 Manoeuvre

108

200 Wheel operating 108

140 Aerotow

92

Airbrakes open 146

Kph 200 200 170 270

VNE at altitude

Height in feet 20 000 - 26 000 26 000-33 000

Meters 6 - 8 000 8 - 10 000

Knots Kph 127 236 113 209

Max winch weak link: 660 daN (Blue)

Tyre pressure:Main psi (bar), rear psi (bar)

Semi aerobatic without water. Cloud flying permitted, without water.

The Hydraulic brake fluid is Aeroshell Fluid 4 or Esso Univis J-13. Theses fluids are mineral based and are very corrosive.

Span 15 meters.

LBA Type certificate No 423

This sheet compiled by: Tim Macfadyen Date: 8 Jan 2005

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