Diamond DA 62, Руководство по эксплуатации самолета

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DA 62 AFM Operating Limitations
2.7 MASS (WEIGHT)
Value
Mass (Weight)
Minimum flight mass 1600 kg 3329 lb
Maximum take-off mass (if MÄM 62-001 is carried out) 2300 kg 5071 lb
Maximum take-off mass
(if MÄM 62-001 is NOT carried out
or if OÄM 62-018 AND MÄM 62-001 are carried out)
1999 kg 4407 lb
Maximum zero fuel mass 2036 kg 4489 lb
Maximum landing mass 2300 kg 5071 lb
Maximum zero fuel mass (if MÄM 62-063 is carried out) 2200 kg 4850 lb
Max. load in LH nose baggage compartment 30 kg 66 lb
Max. load in RH nose baggage compartment 30 kg 66 lb
Max. total load in rear baggage compartment 120 kg 265 lb
Max. load in section A of rear baggage compartment 6 kg 13 lb
Max. load in section B of rear baggage compartment 6 kg 13 lb
Max. load in section C of rear baggage compartment 68 kg 150 lb
Max. load in section D of rear baggage compartment 40 kg 88 lb
If OÄM
62-019
is carried
out
Max. load total load in rear baggage
compartment 46 kg 101 lb
Max. load in section E of rear baggage
compartment 6 kg 13 lb
Max. load in section F of rear baggage
compartment 40 kg 88 lb
WARNING
Exceeding the mass limits will lead to overstressing of the
airplane as well as to degradation of flight characteristics and
flight performance.
Doc. No. 11.01.05-E Rev. 0 11-Jan-2019
DOT
approved
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