Pelegrin Tarragon, Руководство по эксплуатации и полетной документации для пилотов, Страница: 7 / 76

Pilots Operating Handbook
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YL-MFG
Revision 7, Issue 1 6-Apr-16
1 General
1.1 Introduction
This Pilot’s Operating Handbook (POH) has been prepared as a guide to help you get the most out
of your airplane. It contains information about your airplane’s equipment, operating procedures,
performance and suggested service and care. Please study it carefully and use it as a reference.
The POH contains 8 sections. It also contains supplemental data supplied by Pelegrin Ltd.
The Appendix provides basic data and information of general interest. It also contains definitions or
explanations of symbols, abbreviations, and terminology used in the POH.
Throughout the Handbook, warnings, cautions and notes pertaining to airplane handling and
operations are utilized. These adjuncts to the text are used to highlight or emphasize important
points:
WARNING: Operating procedures, techniques, etc., which can result in personal injury
or loss of life if not carefully followed.
CAUTION: Operating procedures, techniques, etc., which can result in damage to equipment
if not carefully followed.
NOTE
: An operating procedure, technique etc., considered essential to emphasize.
1.2 Basic Description
The Tarragon is an all-carbon-composite, tandem-seat, low-wing Aircraft, designed to set new
standards for safety, weight and performance.
The Tarragon has been designed and calculated ground-up by C.F.M. Air, in Turino, an Italian
Aerospace Design Company, under the guidance of Maurizio Cheli, former Astronaut and chief test
pilot for ALENIA.
The prepreg carbon components are manufactured by www.nexusprojectes.com, an accredited
producer of carbon structures in Barcelona/Spain.
The fuselage consists of a stressed skin monocoque structure in carbon fiber with bulkheads that
also form the seats.
The aerodynamic components, wings, tail plane and rudder, are constructed of carbon fiber spars
and ribs, bonded with carbon fibe r external stressed skin.
The wing can only be detached from the fuselage as a complete unit, thereby eliminating the
weight of a wing - panel detach option and guaranteeing superior structural integrity.
The retracting landing gear is electrically actuated and is constructed of strong but lightweight
material including titanium