STEMME S12 User Manual

DOCUMENT NUMBER:
L500-912.820 ISSUE JUL 20, 2016
AMENDMENT: 00
DATE: 
CHAPTERPAGE 530
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
2. Check condition of TCU and
waste-gate-servo assy.
X X X
7.4.7
3. Check sensors for oil pressure,
oil temperature, cylinder cool-
ant temperature, exhaust gas
temperature (if installed), fuel
pressure and re warning.
X X X
7.4.7
4. Check ignition lock shorting
cables (aft rewall, lower LH
side)
X X
7.4.7
5. Check function of ignition
retarder module.
X X
7.4.7
6. Check function of engine in-
strumentation.
X X X
7.4.7
5.4.14 CENTER FUSELAGE FAIRING, ENGINE COWLINGS AND FIREWALL
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 upper cen-
ter fuselage fairing, including
oil service access.
X X X
7.4.9
2. Check condition of LH and RH
Cowling.
X X X
7.4.9
3. Check condition of cowling
re protective paint. Repair if
required.
X X X
7.4.8.1
4. Check condition and function
of inlet and outlet cowl aps.
X X X
7.4.9
5. Check fairing section aft of
outlet cowl ap.
X X X
7.4.9
6. Check openings of inlet cowl
ap (fully opened and fully
reduced aperture). Check if
aps close properly when
nose-cone is closed.
X X X
7.4.9
7. Check condition of rewall
sheets.
X X X
7.4.8.3

STEMME S12 Specifications

General

Brand	STEMME
Model	S12
Category	Aircrafts
Language	English