8-2
Date of Issue: 04/2008
Revision: 1.0
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.
All repairs and maintenance should be made in accordance with AC
43.13-1B.
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 SECTION 6 and up-date
the placard showing weights in the cockpit.
8.4 Ground handling
8.4.1
Towing
To handle the airplane on the ground, use the Tow Bar, or the fuselage
rear pushed down in the place of a bulkhead.
CAUTION
Avoid excessive pressure at the airplane airframe-especially at control
surfaces. Keep all safety precautions, especially in the propeller area.
