BGA glider data sheet - Glasflügel 304 B

Data source: BGA data

Designer: Glasflügel

Manufacturer: Jastreb in Yugoslavia

Agent: H G Streifeneder, Glasfaser-Flügzeug-Service, Brühlstrasse 12, 7318-Lenningen 2, Germany

Weighing Data:

Control deflections in mm

Max weight with water

Kg Pounds 450 992

Up

Down

Distance -

hinge to

measuring

point

Max weight of non-lifting components (everything except wings)

Ailerons

BGA concession non-aerobatic
max weight of non-lifting components [+5%] Max in baggage compartment

Elevator Flaps °

Max water

Rudder

Controls max free play (controls central)

Max pilot weight (seat load)

110 242

mm Inches

Forward C of G limit (aft of datum) 200 7.87

Aft C of G limit (aft of datum)

325 12.79

Pilot position (fwd)

Longitudinal datum: Wing root LE.

Horizontal datum: Top of rear fuselage 1000:52 rear down

Knots Kph

Maximum speeds
Knots Kph

VNE at altitude Knots Kph

VNE

135 250

Winch / auto tow 81

150

0-6600 feet

Rough air 108

200

Flaps

108 200

6600–10 000

Manoeuvre

Landing flap

10 000–13 000

Aerotow

U/C raising or lowering

13 000–16 000 16 000-20 000

Notes: -

Max winch weak link: 600 Kg (Blue)

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

Semi aerobatic without water. Cloud flying permitted.

Span 15 meters

LBA Type certificate number 335/88

The Glasflügel 304 was manufactured by Glasflügel (they made 65 from 1980 to 1982).

The Glasflügel 304B was manufactured later by Jastreb in what was then Yugoslavia (they made one small batch only).
This sheet compiled by: Tim Macfadyen Date: 28 November 2002
Updated 15 Dec 2011 – Manufacturer corrected

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