Diamond DA 42, Руководство по эксплуатации самолета

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Operating Limitations DA 42 AFM
Page 2 - 16 Rev. 8 15-Dec-2017
EASA
approved
Doc. No. 7.01.05-E
2.7 MASS (WEIGHT)
Value Mass (Weight)
Minimum flight mass 1250 kg 2756 lb
Maximum take-off
mass MÄM 42-088 not carried out 1700 kg 3748 lb
MÄM 42-088 carried out 1785 kg 3935 lb
Maximum zero fuel mass 1650 kg 3638 lb
Maximum zero fuel mass,
if OÄM 42-188 is carried out (see Note below)
1674 kg 3690 lb
Maximum zero fuel mass,
if OÄM 42-188 and OÄM 42-195 are carried out
(see Note below)
1730 kg 3814 lb
Maximum landing mass (see NOTE below) 1700 kg 3748 lb
Maximum landing mass,
if OÄM 42-195 is carried out
1785 kg 3935 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 baggage
extension 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.