DOCUMENT NUMBER:
L500-912.820 ISSUE JUL 20, 2016
AMENDMENT: 00
DATE: --
APPROVED SECTION-PAGE 4-2
MAINTENANCE MANUAL STEMME S12
4.1 GENERAL
This chapter defines the mandatory overhaul (TBO – Time Between Overhaul), replacement
(TBR – Time Between Replacement), and inspection intervals for components of the STEMME S12.
The chapter also defines the structural inspection requirements for the STEMME S12 composite
airframe. It contains information about the lifetime of all STEMME designed parts or components
that must be overhauled, rebuilt, inspected, or replaced at either specific flight time limits or
specified calendar time limits or that require monitoring through scheduled maintenance.
Compliance with the specified times and intervals is mandatory for maintaining continuing
airworthiness of the aircraft.
For airworthiness limitations of other parts installed in the aircraft not designed by STEMME or
with separate TC refer to chapter »5« and respective manufacturer documentation as amended
from time to time.
4.2 MAINTENANCE LIMITATIONS
Be sure to verify compliance with chapter »4 Airworthiness Limitations« when performing
scheduled maintenance per chapter »5«.
The following requirements must be adhered to consistent with applicable national regulations.
4.2.1
PAINT FINISH
To ensure that the temperature of the composite structure is kept below 54°C / 130 °F, the airframe
must be painted white as approved. Only the nose cone may be a darker color. On the rest of the
airframe, you may only paint registration letters and numbers and placards in a color other than
white.
When re-painting is needed on a cowling, you must paint the engine side (interior side) of the
lower and side cowlings with aviation grade fire-resistant paint approved by STEMME.
Refer to P520-901.502 “Small Repairs of Composite Materials” (latest approved issue), Annex A
of this manual, for guidance on the paint approved for use by STEMME.
CAUTION
Aircraft control surface balance is critical to flight safety. Repair and removal or addition of any
paint or body filler to a control surface requires that the control surface is rebalanced according
Annex D of this manual.
Summary of Contents for S12
Page 1: ......
Page 3: ......
Page 97: ......
Page 238: ......
Page 240: ......
Page 242: ......
Page 244: ......
Page 246: ......
Page 248: ......
Page 250: ......
Page 255: ...A FLIGHT CONTROLS PITCH CONTROL AND TRIM ...
Page 256: ......
Page 257: ...B FLIGHT CONTROLS LATERAL CONTROL WING FLAP AILERON ...
Page 258: ......
Page 259: ...C FLIGHT CONTROLS AIRBRAKE CONTROL ...
Page 260: ......
Page 261: ...D FLIGHT CONTROLS RUDDER CONTROL ...
Page 262: ......
Page 263: ......
Page 264: ......
Page 265: ...E PROPULSION SYSTEM ...
Page 266: ......
Page 268: ......
Page 270: ......
Page 272: ......
Page 274: ......
Page 276: ......
Page 278: ......
Page 280: ......
Page 282: ......
Page 284: ......
Page 286: ......
Page 288: ......
Page 290: ......