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AutoGyro Calidus - Red End-Cap Rotor System Limitations; Rotor System II (Blue End Caps) Limitations

AutoGyro Calidus
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RSUK0060_POH_CD Revision 7.0, Issue Date17.01.2019 7
Limitations if fitted with red end-cap RotorSystemII under SB-039, or SB-039 is embodied
and Rotorsystem II TOPP variant is fitted (blue end caps)
Occupant warning (in front and rear cockpits) Fitted beside front
seat and back of front seat
Auxiliary socket (where fitted,
marked ‘12v 5A on the panel) Roll trim indicator (where fitted)
Coolant header tank Engine oil tank
OCCUPANT WARNING
This aircraft has not been certificated to an
International Requirement
L R
Roll Trim
Front seat back
straps limit stops
must be fitted if rear
stick is fitted
OPERATING LIMITATIONS
Aerobatic Limitations
Aerobatic manoeuvres are prohibited.
Manoeuvres involving a deliberate reduction in normal ‘g’ shall be avoided.
CG Range Limits (Gyroplane) – refer to Pilots Handbook data.
Airspeed Limitations
Maximum Indicated Airspeed (Vne): 120mph
Other Limitations
This aircraft shall be flown by day and under Visual Flight Rules only.
Smoking in the aircraft is prohibited
Coolant Header Tank.
Filled with 50/50
water/antifreeze
Oil tank
Capacity 3 ltrs.
Use Shell VSX or
equivalent Motorcycle
oil SF or SG

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