DOCUMENT NUMBER:
L500-912.820 ISSUE JUL 20, 2016
AMENDMENT: 00
DATE: 
CHAPTERPAGE 522
MAINTENANCE MANUAL STEMME S12
5.4.4 COCKPIT
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. Inspect canopy for damage
and proper function of locking
mechanism, grease canopy
locks. Check tension of the
metal wire rope in locking
mechanism. Check and ad-
just the wire rope to ensure
uniform locking/unlocking at
each side.
X X X
7.2.1
2. Canopy emergency jettison:
Check function and gas spring
force (minimum 150 ± 30 N / 34
± 7 lbf compressed).
X
7.2.1
3. Check function of lateral gas
springs of canopy (canopy
must remain in open position).
X X
7.2.1
4. Check seat belts and attach-
ment points.
X
7.2.2
5. Check throttle and choke lever
assy. in cockpit. Check stops
of throttle lever. Check choke
lever adjustment. Check throt-
tle valve positions by means
of the ROTAX communication
program.
X X X
7.4.7
6. Check controls in front fuse-
lage for foreign objects, proper
condition and installation.
X X X
7.3.1
7. Check swagged terminals of
all control rods in fuselage.
X X
7.3
8. Check condition and attach-
ment of instruments, switches,
circuit breakers, fuses and wir-
ing. Check re warning light.
X X X
7.2.2
9. Check cockpit ventilation ex-
ible hoses.
X X X
7.2.2
10. Check rudder pedals and ca-
bles, check pedal adjustment.
X X X
7.3.1
1 1. Check condition, attachment
and adjustment mechanism of
seats.
X X
7.2.2