AVIATION
Artur Trendak
FLIGHT MANUAL
Restrictions
Chapter 2
Page 2-4
Document no.: TERCEL-AFM-001-EN
Edition 1
21 Aug 2014
Change no.:
WARNING!
Load Factor below 1g during flight cause the rotor rotational speed to fall
and if maintained, it can lead to disaster.
2.6
Rotor Tachometer Markings
Marking
Value or range
[rpm]
Notes
Red arch
0
÷
200
Warning range
Green arch
200
÷
420
Normal range
Red arch
420
÷500
Warning range
2.7
Weights
Maximum take-off weight (MTOW)
560kg
1234 lb
Nominal proper weight *
326 kg
718lb
Minimum crew weight
60 kg
132 lb
Maximum crew weight
220 kg
485 lb
Maximum one person weight
110 kg
243 lb
Maximum fuel weight
93 kg
205 lb
* - the actual proper weight for a particular model is written in the current weighing report and in
subsection 6.4 of this manual.
The current take-off weight is equal to the sum of the empty gyrocopter weight and the
weights of the crew, luggage and fuel. Under no circumstances, do not exceed the approved
maximum take-off weight (MTOW) equal to 560 kg (1234 lb). Proposed load sheet is presented
below.
Weight Minimum Maximum
Empty weight
----------- ----------
Crew weight
Fuel weight
Luggage weight
Total
WARNING!
Exceeding the maximum weight published is prohibited.
