BGA glider data sheet - ASW 28-18 & ASW 28-18E
See separate sheet for ASW28

Data source: EASA data

Date of issue: 6 12 2004

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 15m

525

Max weight with water 18m

575

Max wt aerobatics & cloud 15m 409

Max wt aerobatics & cloud 18m 419

Max weight of non lifting components (everything except wings)

285

BGA concession non-aerobatic
max weight of non lifting components [+5%] Max pilot weight (seat load)

299

Baggage compartment

12

mm

Forward C of G limit (aft of datum) 15m 227

Forward C of G limit (aft of datum) 18m 233

Aft C of G limit (aft of datum)

406

1157 1268 902 923 628
660
26.5 Inches 8.94 9.17 13.58

Control deflections in degrees

Up

Down

Controls mass

& moments

Ailerons Elevator Rudder

20° - 25° 12° - 15° 18° - 22° 18° - 22° 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

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: - 825 daN (red) Tyre pressure:Main psi (bar), rear psi (bar) Semi aerobatic without water. Cloud flying permitted, without water. LBA Type certificate No 423 Span optional 15 or 18 meters A self sustaining engine is an option (“E” version).
This sheet compiled by: Tim Macfadyen Date: 8 Jan 2004

Page 34 of 221