STEMME S12 User Manual

DOCUMENT NUMBER:
L500-912.820 ISSUE JUL 20, 2016
AMENDMENT: 00
DATE: 
CHAPTERPAGE 524
MAINTENANCE MANUAL STEMME S12
5.4.6 TAIL BOOM
Type and Subject of Inspection
Break-in Aircraft 100 hr Engine 100 hr Engine 200 hr Engine 600 hr Annual
Refer to
Section
Sign-o
1. Check elevator control lever in
lower vertical n.
X X
7.3.3
2. Check swaged terminals of all
control rods in tail boom.
X X
7.3
3. Check rudder control cables in
forward tail boom.
X X X
7.3.3
4. Check trim system (actuator /
springs).
X
5.4.7 EMPENNAGE
Type and Subject of Inspection
Break-in Aircraft 100 hr Engine 100 hr Engine 200 hr Engine 600 hr Annual
Refer to
Section
Sign-o
1. Check rudder ttings.
X X X
7.1.3
2. Check connection of COM
antenna cable (bottom of
rudder).
X X
7.1.3
3. Check adjustment and condi-
tion of rudder control.
X X X
7.3.3
4. Check free movement of rud-
der, especially in case of tail
wheel blockage.
X X X
7.3.1
5. Check front tting of horizon-
tal stabilizer for spring ten-
sion, backlash of bolt, fatigue
cracks and corrosion.
X X X
7.3.1
6. Check rear tting of horizon-
tal stabilizer for wear of pins,
fatigue cracks, axial and radial
backlash and corrosion.
X X X
7.3.1
7. Check tight t of screw con-
nections of both horizontal
stabilizer ttings.
X X X
7.3.1
8. Check connection of elevator
control rod to rear tting of
elevator.
X X X
7.3.1

STEMME S12 Specifications

General

Brand	STEMME
Model	S12
Category	Aircrafts
Language	English