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3.
EMERGENCY PROCEDURES................................................................................... S4-5
4.
NORMAL PROCEDURES .......................................................................................... S4-6
5.
PERFORMANCE ........................................................................................................ S4-6
6.
WEIGHT AND BALANCE ......................................................................................... S4-14
7.
DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS ....................................... S4-16
8.
HANDLING, PREVENTIVE AND CORRECTIVE MAINTENANCE........................... S4-16
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.
2.8. CENTER OF GRAVITY
Points Gross Weight Arm (aft of datum)
(lbs) (kgs) (in) (m)
A 1653 750 7.95 .202
B 1764 800 8.07 .205
C 1764 800 12.16 .309
D 1653 750 12.48 .317
WARNING
EXCEEDING THE CENTER OF GRAVITY LIMITATIONS REDUCES THE MANOEUVRABILITY AND STABILITY OF THE AIRPLANE.
The procedure used to determine the center of gravity is described in Chapter 6.
2.9. APPROVED MANEUVERS
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