通航信息_通航_通用航空_General Aviation

2.6.2 OTHER WARNING ALERTS
Warning alerts on the instrument panel
GEAR UNSAFE

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Illuminates if the landing gear is neither in the final up nor in WARNING LIGHT
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the down & locked position.
(red)
Audible warning alerts
GEAR

Resounds if the landing gear is retracted while the flapsRETRACTED
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move into position LDG or when the power lever is placed inCHIME TONE a position below 25%.
(repeating)
Page 2 - 14  Rev. 5  15-Nov-2007  Doc. No. 7.01.05-E 

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2.7 MASS (WEIGHT)

Value  Mass (Weight) 
Minimum flight mass  1250 kg  2756 lb 
Maximum take-off mass  M.M 42-088 not carried out  1700 kg  3748 lb 
M.M 42-088 carried out  1785 kg  3935 lb 
Maximum zero fuel mass  1650 kg  3638 lb 
Maximum landing mass (see NOTE below)  1700 kg  3748 lb 
Max. load in nose baggage compartment(in fuselage nose)  30 kg  66 lb 
Max. load in cabin baggage compartment(behind rear seats)  45 kg  100 lb 
Max. load in baggage extension(behind cabin baggage compartment)  18 kg  40 lb 
Max. load, cabin baggage compartment and baggageextension together  45 kg  100 lb 

WARNING
Exceeding the mass limits will lead to overstressing of the airplane as well as to degradation of flight characteristics and flight performance.
NOTE
In some countries the beginning of a flight is defined by starting the powerplant. In those countries a ramp mass of maximal MTOM + 8 kg (MTOM + 18 lb) is approved. At the time of lift-off the maximum permitted take-off mass must not be exceeded.
NOTE
If M.M 42-088 is carried out, a landing with a mass between 1700 kg (3748 lb) and 1785 kg (3935 lb) is admissible. It constitutes an abnormal operating procedure. A "Hard Landing Check" is only required after a hard landing, regardless of the actual landing mass.
Doc. No. 7.01.05-E  Rev. 5  15-Nov-2007  Page 2 - 15 

2.8 CENTER OF GRAVITY
Datum Plane
The Datum Plane (DP) is a plane which is normal to the airplane*s longitudinal axis and in front of the airplane as seen from the direction of flight. The airplane*s longitudinal axis is parallel with the floor of the nose baggage compartment. When the floor of the nose baggage compartment is aligned horizontally, the Datum Plane is vertical. The Datum Plane is located 2.196 meters (86.46 in) forward of the most forward point of the root rib on the stub wing (refer to figure in Section 6.2).
Center of gravity limitations
The center of gravity (CG position) for flight conditions must be between the following limits:
Most forward flight CG:
　
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