STEMME S12 User Manual

DOCUMENT NUMBER:
L500-912.820 ISSUE JUL 20, 2016
AMENDMENT: 00
DATE: 
CHAPTERPAGE 521
MAINTENANCE MANUAL STEMME S12
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
12. Inspect L’Hotellier-connectors
of aileron control rod accord-
ing to manufacturer instruc-
tions (Annex A). Check un-
loose-able fastening of safety
pin.
X X X
7.3.2
13. Check bell-crank levers and
adjacent components of wing
aps and aileron system in
wing.
X
7.3.2
14. Check swaged terminals of all
control rods in wing.
X X
7.3
15. Check condition of air brakes.
X X
7.3.2
5.4.3 FORWARD FUSELAGE
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 safe locking of
nose-cone.
X X
7.1.2.3
2. Check condition and backlash
(3 mm / 0.12 in at nose-cone
tip) of nose-cone.
X x
7.1.2.3

STEMME S12 Specifications

General

Brand	STEMME
Model	S12
Category	Aircrafts
Language	English