SAMPLE
8-1
Document No.:
Z601XLFMEN
Date of Issue:
12/2002
Revision:
8.1 Introduction
This section contains factory-recommended procedures for proper ground
handling and servicing of the airplane. It also identifies certain inspection
and maintenance requirements which must be followed if the airplane is to
retain that new-plane performance and dependability.
8.2
Aircraft inspection periods
Periods of overall checks and contingent maintenance depends on the
condition of the operation and on overall condition of the airplane.
Inspections and revisions should be carried out in the following periods, at
least:
a) after the first 25 flight hours
b) after every 50 flight hours
c) after every 100 flight hours or at least annual inspection
Refer to the Engine Operator's Manual for engine maintenance.
Maintain the prop according to its manual.
Refer to the Technical Description, Operating, Maintenance and Repair
Manual for
Z
Z
E
E
N
N
A
A
I
I
R
R
C
C
H
H
6
6
0
0
1
1
Z
Z
O
O
D
D
I
I
A
A
C
C
microlight to see more details on
maintenance.
8.3
Aircraft alterations or repairs
It is recommended to contact the airplane manufacturer prior to any
alternations to the aircraft to ensure that the airworthiness of the aircraft is
not violated. Always use only the original spare parts produced by the
airplane (engine, prop) manufacturer.
If the aircraft weight is affected by that alternation, a new weighing is
necessary, then record the new empty weight into the Weight and Balance
record / Permitted payload range in 6.2 and up-date the placard showing
weights in the cockpit.
Refer to the Technical Description, Operating, Maintenance and Repair
Manual for
Z
Z
E
E
N
N
A
A
I
I
R
R
C
C
H
H
6
6
0
0
1
1
Z
Z
O
O
D
D
I
I
A
A
C
C
microlight to see more details on
repairs
.
.
