TL Ultralight TL-3000 Sirius, Руководство по эксплуатации и полетам

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Flight and operational manual
TL 3000 SIRIUS
Page 53
8.2.2 Engine periodical inspections
See the engine operating and maintenance manual published by the
engine manufacturer.
8.2.3 Propeller periodical inspections
See the operating and maintenance manual published by the propeller
manufacturer.
8.3 Airframe service life
The initial airframe life span is defined up to 8.000 hours or 5 years from the
production date. It will be adjusted according to the operational experience and
airframe actual status as determined during the manufacturer service centre
inspection.
8.4 Aircraft modifications and repairs
WARNING:
It is necessary to contact the aircraft manufacturer before every aircraft
modification as well as
the LAA CR
before each significant modification or repair
(influencing airworthiness).
CAUTION:
If the modification influences the weight, it is necessary to perform a new
weighing and empty aircraft centre of gravity determination procedure
according to section 6 and record the empty aircraft centre of gravity
position in the table shown in section 2.8, update the weighing and centre of
gravity position determination protocol and update the placards placed in the
aircraft.
8.4.1. Bolt connections repairs
In cases of corrosion, bending, cracking or callosity, such bolt must be
changed immediately. In case of a stripped thread, both the bolt and nut
must be changed. The bolts can be replaced only by the same quality and
norm bolts. Nylon insert self ‐ locking nuts are designed for one ‐ time use
only. Full metal nuts can be used maximum 3 times after compressing
the locking ring with pliers.