STEMME S12

DOCUMENT NUMBER:
L500-912.820 ISSUE JUL 20, 2016
AMENDMENT: 00
DATE: 
CHAPTERPAGE 525
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
9. Check backlash in ttings
of horizontal stabilizer when
installed.
X X X
7.3.1
10. Check holes of water tank in
the right shell of vertical tail.
Verify correct markings of
quantity.
X X
7.3.1
1 1. Check gap sealings and zigzag
tape on empennage.
X X
7.3.1
5.4.8 FUEL SYSTEM COMPONENTS IN THE 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 quick-release coupling
in fuel supply line.
X X X
7.4.6
2. Check condition of supply,
return and drain lines outside
the engine compartment, sup-
ply and return lines inside the
engine compartment.
X X X
7.4.6
3. Check condition, attachment
and function of electrical fuel
pumps.
X X X
7.4.6.2
4. Replace the main fuel pump –
every 1000 hours.
X
7.4.6.2
5. Check fuel valve, fuel check
valves and quick drains. Check
re-wall penetration assy. of
supply and return lines for
tight connection and leakage.
X X X
7.4.6.2
6. Check drain lines of carburetor
drip trays and airbox.
X X X
7.4.6.2
7. Check re protective sleeves
on fuel supply and return lines
in engine compartment.
X X X
7.4.8.2