BGA glider data sheet - SF 26A

Data source: Flight Manual

Date of issue: 1963

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

UK Agent:

Web site:

Phone:

Fax:

Link to mandatory mods:

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

Kg Pounds 310 684 319 704

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)
Forward C of G limit (aft of datum) Aft C of G limit (aft of datum) Pilot position (forward of datum)

110 mm 329 486 404

242 Inches 12.9 19.1 15.9

Control deflections in mm

Up Down Distance - Max

hinge to measuring point

free play

Ailerons 90 43 ±10 ±5
Elevator 140 140 ±10 ±10

240 300

Trim Rudder

12±5 27±5
Left Right 410 410 ±20 ±20

80 655

Longitudinal datum: Wing root LE at rib 1

Horizontal datum: Rear fuselage top 1000:82 tail down

Maximum speeds

Knots Kph

VNE

108 200 Aerotow

Rough air

75 140 Winch / auto tow

Manoeuvre

Airbrakes open

Knots 75 54 108

Kph 140 100 200

Max winch weak link: 650 Kg (Blue) Tyre pressure: 36 psi (2,5 Bar) Non/semi/fully aerobatic, cloud flying permitted.
Notes: -

This sheet compiled by: Tim Macfadyen Date: 23 July 2003 Page 150 of 178