DOCUMENT NUMBER:
L500-912.820 ISSUE JUL 20, 2016
AMENDMENT: 00
DATE: --
CHAPTER-
PAGE 2-3
MAINTENANCE MANUAL STEMME S12
VERTICAL TAIL
Design
Web GFRP, skin CFRP, rudder GFRP-sandwich.
Span
1.60 m
5.25 ft
Area
1.78 m²
19.16 sqft
Airfoil
FX71-L150/30 x*1.3
WEIGHTS
Max. T/O-weight
900 kg
1984 lb
Empty weight
690 kg
(approx., min. equipment.)
1556 lb
Maximum weight of
non-lifting parts
610 kg
1345 lb
Total useful load
(Occupants, fuel, baggage)
210 kg
463 lb
WING FLAPS (CENTER WING)
Span
4.39 m
14.40 ft
Area
0.75 m²
8.07 sqft
Flap positions:
-10°, -5°, 0°, +5°, +10°, L (+16°)
AILERONS (OUTER WINGS AND EXTENSIONS)
Span
5.70 m + 1.50 m
18.70 ft + 4.92 ft
Area
0.78 m² + 0.13 m
2
8.40 sqft. + 1.40 sqft
LANDING GEAR
2 main wheels with brake discs, rim of wheel
127x127-30
Tire size
6.00-5
Wheel track
1.36 m
4.46 ft
Tail wheel (steerable), tire size
210 x 65
Wheel base
5.46 m
17.91 ft
Summary of Contents for S12
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Page 255: ...A FLIGHT CONTROLS PITCH CONTROL AND TRIM ...
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