Section X
Safety Information
~ft
Twin
Engine (Piston)
Salvaged airplane parts, reworked parts obtained from non-
BEECHCRAFT approved sources or parts, components, or
structural assemblies, the service history of which is
unknown or cannot be authenticated, may have been sub-
jected to unacceptable stresses or temperatures or have
other hidden damage not discernible through routine visual
or usual nondestructive testing techniques. This may render
the part, component or structural assembly
I even though
originally manufactured by BEECHCRAFT, unsuitable and
unsafe for airplane use.
BEECHCRAFT expressly disclaims any responsibility for
malfunctions, failures, damage or injury caused by use of
non-BEECHCRAFT parts.
Airplanes operated for Air Taxi or other than normal opera-
tion, and airplanes operated in humid tropics, or cold and
damp climates, etc., may need more frequent inspections for
wear, corrosion and/or lack of lubrication. In these areas,
periodic inspections
should be performed until the operator
can set his own inspection periods based on experience.
NOTE
The required periods do not constitute a
guarantee that the item will' reach the period
without malfunction, as the aforementioned
factors cannot be controlled by the manufac-
turer.
Corrosion and its effects must be treated at the earliest pos-
sible opportunity. A clean,
dry surface is virtually immune to
corrosion. Make sure that all drain holes remain unob-
structed. Protective films and sealants help to keep corro-
sive agents from contacting metallic surfaces. Corrosion
inspections should be made most frequently under high-
corrosion-risk operating conditions, such as in areas of
10-18
May, 1994
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