CESSNA AIRCRAFT
COMPANY
SINGLE ENGINE
STRUCTURAL REPA
IR MANUAL
AUXILIARY SPAR REPAIRS
1. General
A. The auxiliary spar is constructed of formed sheet metal, and is behind the trailing edge ribs from
approximately WS 100.50 to 208.00. The auxiliary spar is attached to upper skins, lower skins and
other wing str
ucture using rivets.
2. Auxiliary Spar Damage
A. Damage to the a
uxiliary spar can be divided into three major categories and is detailed in Wing
Damage Classification.
3. Auxiliary Spa
r Repair
A. Repairs to the auxiliary spar are illustrated in Figure 801.
57-24-00 Page 801
© Cessna Aircraft Company Jun 1/2005
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