Zlin Aviation
Section 1
Maintenance Manual Aircraft Maintenance Manual
Issued: 01/02/2006
QAP-AMM-Rev02
Date of latest Revision: 23/01/2013
Page Number: 1-33
1.2.5
100 Hours or Annual Condition Inspection
(Whichever comes first)
Note:
make sure that after the inspections, aircraft is free of any tools, parts and debris, and
reinstall all access doors, fairing, seats and so on, removed for the inspection.
Complete entries in log book, or any other required records
In addition to all the inspections required at 50 hours, the following must also be inspected.
General
Level of
certification
Control log books and flying books for any records
Owner
Fuselage-Wings
1
Clean the entire aircraft and open all panels to allow access for
inspection.
Owner
2
Check aircraft external covering for rents, tears, in the fabric covered
parts.
LSRMA
3
Check windscreen and all windows for condition. Verify all glasses
correctly open and close, and ensure door hinges are in good condition.
Grease hinges.
Owner
4
Check wing support attachment pins and bolts for correct torque and
no abnormal play
LSRMA
5
Inspect wing covering, check leading and trailing edges for damage
or deformation.
LSRMA
6
Inspect aileron and flap hinges and attachments. Check attachment
pins for security and locking.
LSRMA
7
Inspect spar compression rod attachments. These attachments are
fastened with steel bolts which must be inspected for wear or corrosion.
Even in the case of minute wear, replacement must be carried out
immediately.
LSRMA
8
Check wing compression rods attachment plates for wear or
corrosion.
LSRMA
9
Verify the tail surface attachment pins and supporting struts are
secure and in good condition.
LSRMA
10
Inspect the fuselage lower beam adjacent to the tail for corrosion
damage or deformity through heavy landing.
LSRMA
