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nd
Edition – Rev 0
O6-10
INSPECTION CAPS
06-10 INSPECTION CAPS
An index number has been assigned to each opening for identifying the access. All access
plates and panels are secured by either metal fasteners or screws and are identified as follows:
(1) The suffix is the zone location, namely
C: cabin
CF: cabin floor
E: engine nacelle
F: fuselage
W: wing
L: light
(2) The second suffix consists of a number
The access and inspection caps for the airplane are shown in the following Figures.
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