SC-POH-1-1-17
Revision: -
Date of issue: 2011-09-01
SECTION 1
GENERAL INFORMATION
S
S
p
p
o
o
r
r
t
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C
C
r
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u
u
i
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s
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1-4
Main airplane dimensions:
Wing span ......................................................
28.22 ft
Length............................................................
21.72 ft
Height ............................................................
7.6 ft
Wing area ......................................................
132.3 sq ft
Wing loading ..................................................
10 lb/sq ft
Cockpit width .................................................
46 in
Flight control surfaces travel:
Rudder ...........................................................
30°
±2°
to each side
Elevator .........................................................
+24° / -24° ±2°
Aileron ...........................................................
+15° / -15° ±1°
Flaps ..............................................................
0° to 30°
±1°
Aileron trim ....................................................
+ 20° / -20° ±2°
Elevator trim ..................................................
+ 22° / -28° ±2°
Engine:
Manufacturer .................................................BRP-Powertrain GmbH&Co.KG
Model number ................................................912 ULS
Maximum power rating ..................................
98.6 hp at 5,800 RPM
Cooling ..........................................................liquid and air
Type ...................... 4-stroke, 4 cylinder, horizontally opposed, spark ignition
engine with one central camshaft-push-rod-OHV
Propeller:
Manufacturer .................................................WOODCOMP s.r.o.
Model number ................................................KLASSIC 170/3/R
Number of blades ..........................................
3
Diameter ........................................................
68 in
Pitch setting ...................................................
17.5 ± 0.5°
Type ..............................................................three composite blades,
ground adjustable
2-4
Date of Issue: 12/2007
Revision: 2.0
Airframe
All-metal construction, stressed skin, single curvature metal skins riveted
to stiffeners. Construction is of 6061-T6 aluminum sheet metal riveted to
aluminum angles with Avex rivets. This high strength aluminum alloy
construction provides long life and low maintenance costs thanks to its
durability and corrosion resistance characteristics.
The wing has a high lift airfoil equipped with slotted flaps.
Control system
The plane is equipped with a dual stick control, the adjustable rudder
pedals with pedal hydraulic brakes for easy ground control of the
castering nose wheel.
The elevator and aileron trim are electrically actuated by buttons on the
control stick. Wing flaps are electrically actuated by the rocker switch
located on the middle panel.
Deflections:
Rudder deflections ...............................
30
(
to each side
Elevator deflections ..............................
+ 28
(
- 25
(
Aileron deflections ................................
+ 20
(
- 15
(
Flap deflections ....................................
0
(
to 30
(
Aileron trim deflections .........................
+
(
/-
(
Elevator trim deflections .......................
+ 22
(
- 28
(
Landing gear
Tricycle landing gear with the castering nose wheel. Main landing gear
uses two fiberglass spring elements.
