BGA glider data sheet - Blanik (Super) L-23

Data source: BGA data sheet

Date of issue:

Manufacturer: Letecke Zavody, 68604 Kunovice, Czech Republic (Previously OLET. The Czech Republic)

UK Agent:

Web site:

Phone:

Fax:

Link to mandatory mods:

Weighing Data:

Kg Pounds

Max weight (Serial Nos to 29003) 510 1124

BGA concession non-aerobatic max weight (dry) [+3%]

525 1158

Max weight (Serial Nos 29004 on) 530 1168

BGA concession non-aerobatic max weight (dry) [+3%]

545 1203

Maximum baggage

10 22

Max pilot weight (seat load)
Forward C of G limit (aft of datum) Aft C of G limit (aft of datum) Front pilot position (aft of datum) Rear pilot position (aft of datum)

mm 112 325 1234 170

Inches 4.4 12.8 48.6 6.7

Control deflections in degrees

Up Down Distance - Max

hinge to measuring point

free play

Ailerons 34±2 13±2

Elevator 32±2 25±1 Trim

Rudder 30±1 Left & right

Longitudinal datum: Wing LE at root

Horizontal datum: Rear fuselage top 1000:51 rear down (points marked on fuselage side).

Maximum speeds

VNE at altitude (feet)

Serial Nos up to Serial Nos from

938100

938101 onwards

Knots

Kph

Height feet

Knots Kph Knots Kph

Rough air 81

150 0 - 13 780

135 250 124 230

Manoeuvre 81

150

13 780 - 20 000

124

230 114 211

Aerotow 81

150

20 000 - 25 000

116

215 105 195

Winch / auto tow

65

120

25 000 - 30 000

108

200 97

180

30 000 - 35 000

100

185 89

165

Max winch weak link: 662 kg (Blue) Tyre pressure:Main psi (Bar) Semi aerobatic @ 510 Kg AUW. Fully aerobatic @ 420 Kg AUW. Cloud flying permitted. Span 16.2 meters? Wing extensions are an optional modification from Serial No 938101 onwards.

This sheet compiled by: Tim Macfadyen Date: 3 July 2003

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