BGA glider data sheet - SF(H) 34 & SNC 34 C

Data source: Flight Manual

Date of issue: 1984

Manufacturer: Scheibe Flugzeughbau, August-Pfaltz, Str.23, 8060 Dachau bei München (SF 34)

And SNC (Society New Centrair) (SNC 34 C)

UK Agent:

Web site:

Phone:

Fax:

Link to mandatory mods:

Weighing Data:

Kg Pounds

Max weight (dry)

540 1190

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

556

Max weight of non lifting 370 components (everything except wings)

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

389 110

1226 816 856 242

Forward C of G limit (aft of datum) Aft C of G limit (aft) SF 34 Aft C of G limit (aft) SNC 34 C
Front pilot position (forward of datum) Rear pilot position (forward of datum)

mm Inches 199 7.8 367* 14.4* 350 13.78 1050 41.0 20 0.8

Control deflections in mm

Up Down Distance -
hinge to
measuring
point

Ailerons Elevator

90 40 ±10 ±5
80 80 ±8 ±8

170 210

Airbrakes 150 40±5 Inboard ends Min

Rudder

Left Right 528 305 305 ±15 ±15

Elevator Rudder Ailerons

Moment limits

Mass limits

5,1/6,72 kgcm

1,15/1,51 Kg

16,72/21,28 kgcm 4,84/6,16 Kg

9,42/11,98 kgcm 1,98/2,52 Kg

*Changed by TN 336-8

Longitudinal datum: Wing root LE

Horizontal datum: Rear fuselage top horizontal

Maximum speeds

Knots Kph

Knots Kph

VNE

135 250

Aerotow

93 172

Rough air 93

172

Winch / auto tow 65

120

Manoeuvre 93

172

Airbrakes open

VNE at altitude

Max winch weak link: 600 (Blue) Tyre pressure: Front 36 psi (2,5 Bar) Main 43 psi (3 Bar) Semi aerobatic, cloud flying permitted.
Notes: -
This sheet compiled by: Tim Macfadyen Date: 14 May 2002

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