STEMME S12 User Manual

DOCUMENT NUMBER:
L500-912.820 ISSUE JUL 20, 2016
AMENDMENT: 00
DATE: 
CHAPTERPAGE 534
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
14. Check landing gear position
indication and warning (visual
and acoustic, during function
test).
X X X
7.5.1
15. Check function of emergency
gear extension.
X X
7.5.1
5.4.18 TAIL WHEEL
Type and Subject of Inspection
Break-in Aircraft 100h Engine 100h Engine 200h Engine 600h Annual
Refer to
Section
Sign-o
1. Tail wheel: Check ease of op-
eration, clearance to fairing,
backlash.
X X X
7.5.2
2. Check tire condition, pressure
2.8 ± 0.2 bar / 40.6 ± 2.9 p.s.i
X X X
7.5.2
3. Check wheel fork for cracks
and deformation.
X X
7.5.2
4. Check bearing of tail wheel
fork.
X X
7.5.2
5. Check spring coupling assy.
between tail wheel and rudder.
X X X
7.5.2
5.4.19 FLIGHT INSTRUMENTATION AND PITOT / STATIC SYSTEMS
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 condition of Pitot / Stat-
ic system and renew lters/
water separators if required.
X X X
7.6.2
2. Check condition and function
- service life limits if applica-
ble- of ight instrumentation
(refer to equipment list).
X X
7.6

STEMME S12 Specifications

General

Brand	STEMME
Model	S12
Category	Aircrafts
Language	English