Edition 1 21 Aug 2014
Change no.:
Document no.: TERCEL-AFM-001-EN
Page
TERCEL
PILOT OPERATING HANDBOOK
13
Chapter 2
Restrictions
2.10 Manoeuver Load Factor
Admissible manoeuver load factor:
0/+3
2.11 Crew
The
TERCEL
is a side by side two-seater gyrocopter with an option of a single,
or double flight control system. The minimum crew is one pilot. The pilot’s seat
on a solo flight will depend upon the configuration of the cockpit instrument
panel and the position of the wheel brake lever.
2.12 Sorts of Usage
This gyrocopter can be used for leisure, sports, display purposes and training
practice and other reasons, but not including air carriage. Flights can only be
performed in Visual Meteorological Conditions (VMC) under by Visual Flight
Rules (VFR). The specific use of the gyrocopter is described in the Certificate
of Registration given by the Aviation Authority of country of registration.
2.13 Fuel
•
Capacity of the fuel tanks
120 ltr
•
Admissible quantity of fuel in the tanks
120 ltr
•
Including usable fuel
118 ltr
•
Non-usable fuel
2 ltr
2.14 Wind speed restrictions
The admissible values of wind speed during flight and landing:
•
Headwind
60 km/h
•
Crosswind (90º)
30 km/h
•
Tailwind
0 km/h
