09/01/2013
RANS S-20 RAVEN
TEXT MANUAL
00-20
(4) Instruments—for poor condition, mounting, marking, and (where practicable)
improper operation.
(5) Flight and engine controls—for improper installation and improper
operation. (6) Batteries—for improper installation and improper
charge.
(7) All systems—for improper installation, poor general condition, apparent
and obvious defects, and insecurity of attachment.
(d) Each person performing an annual or 100-hour inspection shall
inspect (where applicable) components of the engine and nacelle group
as follows:
(1) Engine section—for visual evidence of excessive oil, fuel, or hydraulic
leaks, and sources of such leaks.
(2) Studs and nuts—for improper torquing and obvious defects.
(3) Internal engine—for cylinder compression and for metal particles or foreign
matter on screens and sump drain plugs. If there is weak cylinder
compression, for improper internal condition and improper internal tolerances.
(4) Engine mount - for cracks, looseness of mounting, and looseness of engine
to mount.
(5) Flexible vibration dampeners—for poor condition and deterioration.
(6) Engine controls—for defects, improper travel, and improper safetying.
(7) Lines, hoses, and clamps—for leaks, improper condition, and
looseness.
(8) Exhaust stacks—for cracks, defects, and improper attachment.
(9) Accessories—for apparent defects in security of mounting.
(10) All systems—for improper installation, poor general condition, defects,
and insecure attachment.
(11) Cowling—for cracks, and defects.
(e) Each person performing an annual or 100-hour inspection shall
inspect (where applicable) the following components of the landing gear
group:
(1) All units—for poor condition and insecurity of
attachment.
(2) Shock absorbing devices—for improper oleo
fluid level.
