COMCO IKARUS
Maintenance Manual C42 Series
MaintenanceManual C42-
Series_Issue_VII_18.02.2014.doc
Revison No.:1 62 from 107
No. Description
Inspection
Ref.
Chapter
Signature
every
50
hours
very
100
hours
145
146 Fuselage
147 Frame
148
Check metal frame (fuselage tube, A/B/C columns, canopy roof
frame, struts, fittings, etc.):
- screw connections
- rivet connections
- welded connections
- joints
- deformations
x x
149 Skin
150
Check condition of all glass-fibre and carbon-fibre shells, fairings and
cowlings for damage, cracks, deformation, etc.; repair or replace any
damaged elements
x x
151
Check functionality of fuselage shell attachments and that none are
missing
x x
152 Check proper attachment of mounted parts such as antennas, etc.
x x
153
Check rubber sealing around the opening of the ballistic recovery
system
x x
154
Check proper functioning of the Camloc locks in the baggage bin
cover
x x
155 Towing mechanism (if installed)
156
Maintenance in accordance with the appropriate documents (tow
hook E85)
in accordance
with COMCO
IKARUS GmbH
instructions
operating
manual
157
Check Bowden cable for freedom of movement and damage near the
release lever and near tow hook; this check should be carried out
before every flight
x x
158
Check release force at the release lever when the tow hook is
unloaded (< 13 daN); this check should also be carried out every 200
tows
x
159
Clean and grease Bowden cable at the adjustment screws near the
release lever and the tow hook; this check should also be carried out
every 200 tows
x
160
161 Doors and windscreen
162
Check the front door attachment bolts for cracks near the attachment
screws
x x
163 Check seals for damage and porosity
x x
164
Check glass for cracks, scratches; repair or replace damage elements
as required
x x
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