Flight and Operational Manual
TL- 96 STAR s/n 99 S 25
Notice! The information contained in this document is for reference and information only.
The pilot is the final and only responsible party for the safe operation of this aircraft.
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7.7.Periodical revision after every 300hours
This revision is made after every 295-305 flight hours or after three years of operating. The
diagnostics of all stressed parts of the construction is made and also its detailed range is
prescribed by the internal rule of the producer by the detected state. We introduce here basic
tasks for your information:
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revision after 100hours
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taking off the airscrew and the engine
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revision of the construction
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revision of the interior of the body and the cabin
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the outer revision of the whole airframe
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pilotage revision
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replacement of intended parts
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flight test by the probationary pilot
ATTENTION!
This revision is made only by the service center of the producer.
7.8.Jacking points on the plane
The jacking points made by the low inside buckles of the engine bed to the body partition
are made for lifting the front undercarriage. These jacking points are approachable after taking
off the low part of the engine hood. Do not forget about ensuring the wheels of the main
undercarriage by the wedges on both sides while supporting the airplane on these points.
The jacking points prescribed for the lifting are placed on the low part of the wings in the
distance of 190cm from the body. The supporting mean must be made of a hard construction, it
must be at least 100mm wide and 1000mm long. This supporting part, which supports the wing
must have a soft, 20mm thick felt cover, which enables the weight of the supporting part of the
airplane to disintegrate to its whole area.
After interposing the support under the supporting area, we lift the wing on its low end part by
arms the way to let the lifting force disintegrate on its whole length.
The main undercarriage wheels can be supported by the low parts of the spring constituting the
main undercarriage.
7.9.List of labels and their placing
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the producer label of the body is placed on the inner left side of the airplane in the area
behind the pilot’s seat.
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producer label is placed on the partition behind the seat of the fellow-traveler
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the label introducing the maximum weight of the crew and the load in the dependency
of filling the fuel tank is sticked inside on the left front part of the cabin
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the label indicating used engine oil is on the control tap of the upper cover of the
engine