STEMME S10 - Page 81

Maintenance Manual STEMME S 10 Date of Issue: Oct. 01, 1990 fig. 6.4.1.a
Amendment No.: 7 Date: Dec. 05, 1994
Fig. 6.4.1.a
Alignment Record (Pattern; the complete form can be obtained from the manufacturer)
A4010021_B19.doc-0/27.01.14 14:18/27.01.14 14:18
Note: In the following tables the rated values with their permissible tolerances are figuring in the left cells.
Please enter the measured value in the respective right cell.
Control Surface Deflections:
All positive values (+) indicate the max. positive control surface deflection (downwards), negative values indi-
cate the max. negative deflection (upwards).
Elevator:
Measuring point: inner end rib of the elevator. Distance to hinge axis: 140 mm
- 48
+2
/
-5
mm
[mm]
+ 48
+5
/
-2
mm
[mm]
Trim:
With the trim lever in neutral position, the elevator deflection (pos. or
neg.) shall not exceed ± 5 mm (same measuring point as above).
[mm]
Rudder:
Measuring point: lower rear corner of the rudder's trailing edge. Distance to hinge axis: 420 mm
left: +220 ± 15 mm [mm]
right: -220 ± 15 mm [mm]
Wing Flaps and Ailerons:
Flap lever
position
Stick
position
Measuring points:
aileron: inner end rib of the control suface. Distance to hinge axis: 163 mm
wing flap: inner end rib of the control suface.Distance to hinge axis: 175 mm
left ail. [mm] left flap [mm] right flap [mm] right ail. [mm]
- 10° neutral
-31 ± 4 -31 ± 4
- 5° neutral
-15 ± 4 -15 ± 4
0
left
neutral
right
-48 ± 4
0 ± 2
+27 ± 3
0 ± 2 0 ± 2
+27 ± 3
0 ± 2
-48 ± 4
+ 5° neutral
+15 ± 4 +15 ± 4
+ 10° neutral
+31 ± 4 +31 ± 4
L (+16°) neutral
+51 ± 4 +51 ± 4
Control system friction:
Static friction is to be measured as follows: measuring point at the operating lever / control stick, mid of the
grip; measure the force being reached when the system sets going - three times in both directions. The
average of the higher values from each measurement is to be entered.
Elevator
5 ± 2 N
[N]
Aileron
15
+5
/
-8
N
[N]
Rudder (tailwheel off the ground)
25
+5
/
-8
N
[N]
Pilot Force required to unlock the Airbrakes:
Airbrake lock/unlock
150 + 50 N at 20°C
[N]
at [°C]
wing flap: counterforce in Pos. L
125 ± 25 N at 20°C
[N]
at [°C]
wing flap: damping perceptible in both
directions when jerkily operated
 yes no