1.1 Introduction
This manual has been written to provide pilots and engineers with information essential for
safe and effective operation on gyrocopter. The manual also contains basic guidelines
from the gyrocopter manufacturer and also legal requirements concerning the performance of
flights.
The manual is not a substitute for theoretical and
practical training in respect of piloting gyrocopters.
gyrocopter pilots must hold a qualification certificate or a valid licence for ultralight
aircrafts with specialization for gyrocopters. Before flight pilots must become acquainted with the
uniqueness of the gyrocopter. We recommend you read both the Flight Manual and the Service
Manual to be fully familiar with the structure, all the equipment and the driving unit of the
gyrocopter.
The gyrocopter can only be used for flight when it is technically operative and holds a valid
authorization to perform flights. An authorization to perform flights is entered into the ultralight
aircraft book, which is a document identifying an ultralight aircraft and its units as well as
containing details about the history of usage.
The utilized gyrocopter should be entered into aircraft records kept by the Civil Aviation
Authority as well as hold current air third-party insurance.
1.2 Basis for Airworthiness Acknowledgment
The legal basis for operating a gyroplane is provided by national law and its respective
regulations. The instructions and conditions contained have to be considered when operating the
gyroplane. All documented performance data and operating procedures have been identified within
the certification processes for this gyroplane by means of flight test and analysis.
gyrocopter meet German and Polish Civil Airworthiness Requirements. They
comprise requirements and constitute the basis for the issue of Certificates, Permits and Approvals
in accordance with the Air Navigation Order.
1.3 Description of the Gyrocopter
is a two-seat ultralight gyrocopter. The main structural component is the fuselage
which is constructed with composite material. Two metal tail booms are attached from the lower part
of the fuselage to a twin vertical tail unit. This consist of twin stabilizers and rudders on which a
horizontal stabilizer is attached complete with winglets of constructed composite material. A metal
mast is affixed to the fuselage structure, on which the control head with the rotor is mounted.
The two-blade rotor of metal structure is manufactured and delivered as a set (blades plus a
hub) by the AVIATION Artur Trendak Company. The blades, made from drawn aluminium, are
entirely anodized and perfectly balanced.
