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
Br
eak
-in
Air
cr
af
t 100
hr
Engine 100
hr
Engine 200
hr
Engine 600 hr
Annual
Refer to
Section
Sign-off
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 fire warning.
X
X
X
7.4.7
4. Check ignition lock shorting
cables (aft firewall, 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
Br
eak
-in
Air
cr
af
t 100
hr
Engine 100
hr
Engine 200
hr
Engine 600 hr
Annual
Refer to
Section
Sign-off
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
fire protective paint. Repair if
required.
X
X
X
7.4.8.1
4. Check condition and function
of inlet and outlet cowl flaps.
X
X
X
7.4.9
5. Check fairing section aft of
outlet cowl flap.
X
X
X
7.4.9
6. Check openings of inlet cowl
flap (fully opened and fully
reduced aperture). Check if
flaps close properly when
nose-cone is closed.
X
X
X
7.4.9
7. Check condition of firewall
sheets.
X
X
X
7.4.8.3
Summary of Contents for S12
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Page 255: ...A FLIGHT CONTROLS PITCH CONTROL AND TRIM ...
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Page 257: ...B FLIGHT CONTROLS LATERAL CONTROL WING FLAP AILERON ...
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Page 259: ...C FLIGHT CONTROLS AIRBRAKE CONTROL ...
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Page 261: ...D FLIGHT CONTROLS RUDDER CONTROL ...
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