EasyManua.ls Logo

STEMME S12

STEMME S12
290 pages
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
DOCUMENT NUMBER:
L500-912.820 ISSUE JUL 20, 2016
AMENDMENT: 00
DATE: 
CHAPTERPAGE 69
MAINTENANCE MANUAL STEMME S12
6.4.1.2 FRICTION IN CONTROL SYSTEM
MEASURING POINT
At the operating lever / control stick, mid of the grip.
If installed temporarily disconnect autopilot actuators.
Elevator 5 ± 2 N (1.1 ± 0.45 lbf)
Aileron 15
+5
/
-8
N (3.4
+1.1
/
-1.8
lbf)
Rudder (Tail wheel o the ground!) 25
+5
/
-8
N (5.6
+1.1
/
-1.8
lbf)
6.4.1.3 PILOT FORCES
Following rated forces apply for approx. 20°C, measured on ground. Measuring points for airbrake
and wing ap forces are the respective handles, for down-spring / trim spring forces the uppermost
nger notch of the control stick handle.
If installed temporarily disconnect autopilot actuators for elevator.
Air brake over-center lock and unlock 150 + 50 N (34 + 11 lbf)
Wing Flap: Counter force in position L
125 ± 25 N (28 ± 6 lbf)
Elevator: Down-Spring / Trim-Spring
Force at uppermost nger notch of
stick, stick full forward, trim setting
fully “nose down.
40 ± 5 N (9 ± 1.1 lbf)
Elevator: Down-Spring / Trim-Spring
Force at uppermost nger notch of
stick, stick full aft, trim setting fully
“nose down.
60 ± 5 N (13.5 ± 1.1 lbf)

Table of Contents

Related product manuals