BGA glider data sheet - L-Spatz 55

Data source: Manufacturer’s Datasheet Date of issue: Undatted

Manufacturer: Scheibe Flugzeughbau, August-Pfaltz, Str.23, 8060 Dachau bei München

UK Agent:

Web site:

Phone:

Fax:

Link to mandatory mods:

Weighing Data:
Max gross weight BGA concession non-aerobatic max weight (dry) [+3%]

Kg Pounds 265 585 273 602

Max weight of non lifting 170 375 components (everything except wings)

Control deflections in mm

Up Down Distance - Max

hinge to measuring point

free play

Ailerons 108 30 ±5 ±5
Elevator 100 120 ±10 ±10

223 300

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

179
110 mm 190 345 322

394
242 Inches 7.5 13.6 12.7

Rudder

Left Right 655 420 420 ±20 ±20

Longitudinal datum: Wing rib 2 LE

Horizontal datum: Fuselage top longeron at tail platform horizontal

Maximum speeds

Knots Kph

VNE

97 180 Aerotow

Rough air

59 110 Winch / auto tow

Manoeuvre

Knots 59 49

Kph 110 90

Max winch weak link: 500 Kg (White) Tyre pressure: 36 psi (2,5 Bar) Semi aerobatic, cloud flying permitted.
Notes: -

This sheet compiled by: Tim Macfadyen Date: 11 October 2001

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