DA20-C1 Flight Manual
Supplement 4
Doc # DA202-C1 April 16, 2009 Page S4 - 2
Revision 24 DOT Approved
1. GENERAL
This supplement addresses the effects on the DA20-C1 of an increase in the gross weight from
750 kg (1653 lbs) to 800 kg (1764 lbs) and is applicable only to aircraft with the Sensenich
propeller. This increase of 50 kg (110 lbs) imposes no significant change to the control and
stability of the aircraft. Only the portions of the flight manual affected by this weight increase are
included in this supplement.
1.10. WEIGHT
Maximum Ramp Weight : 803 kg (1770 lbs)
Maximum Take-off Weight : 800 kg (1764 lbs)
Maximum Landing Weight : 800 kg (1764 lbs)
Empty Weight : See Chapter 6
Maximum Weight in Baggage Compartment : 44 lbs (20 kg)
only if restraining devices available
Wing Loading
At Maximum Take-off Weight : 14.11 lbs/sq.ft. (68.96 kg/m2)
Performance Load at Max. Take-off Weight : 14.11 lbs/hp (8.58 kg/kW)
2. OPERATING LIMITATIONS
2.7. WEIGHT
Maximum Ramp Weight : 803 kg (1770 lbs)
Maximum permissible weight : 800 kg (1764 lbs)
Maximum permissible weight in the baggage : 44 lbs (20 kg) only permissible
compartment (including baggage extension, with baggage harness
if fitted)
WARNING
EXCEEDING WEIGHT LIMITATIONS MAY LEAD TO
OVERLOADING OF THE AIRPLANE AND CAUSE LOSS OF
CONTROL OF THE AIRPLANE AND/OR STRUCTURAL
DAMAGE.
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