通航信息_通航_通用航空_General Aviation

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Doc. No. 6.01.05-E
Revision 2 30-Apr-2003
Page 1 - 2

This Airplane Flight Manual must be kept on board the airplane at all times. Its designated place is the side bag of the forward left seat.
CAUTION
The DA 40 D is a single engine airplane. When the operating limitations and maintenance requirements are complied with, it has the high degree of reliability which is required by the certification basis. Nevertheless, an engine failure is not completely impossible. For this reason, flights during the night, on top, under instrument meteorological conditions (IMC), or above terrain which is unsuitable for a landing, constitute a risk. It is therefore highly recommended to select flight times and flight routes such that this risk is minimized.

1.2 CERTIFICATION BASIS
This airplane has been type certified in accordance with the JAA JC/VP procedure. The certification basis is JAR-23, published on 11-Mar-1994, including Amdt.1, and additional requirements as laid down in CRI A-01.
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Doc. No. 6.01.05-E
Revision 1 03-Mar-2003
Page 1 - 3

1.3 WARNINGS, CAUTIONS AND NOTES
Special statements in the Airplane Flight Manual concerning the safety or operation of the airplane are highlighted by being prefixed by one of the following terms:
WARNING
means that the non-observation of the corresponding procedure leads to an immediate or important degradation in flight safety.
CAUTION
means that the non-observation of the corresponding procedure leads to a minor or to a more or less long term degradation in flight safety.
NOTE
draws the attention to any special item not directly related to safety but which is important or unusual.
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Doc. No. 6.01.05-E  Revision 1  03-Mar-2003  Page 1 - 4 

1.4 DIMENSIONS 
Overall dimensions 
Span Length Height  : : :  appr. 11.94 m appr. 8.06 m appr. 1.97 m  appr. 39 ft 2 in appr. 26 ft 5 in appr. 6 ft 6 in 
Wing 
Airfoil Wing Area Mean aerodynamic chord (MAC) Aspect ratio Dihedral Leading edge sweep  : : : : : :  Wortmann FX 63-137/20 - W4 appr. 13.54 m2 appr. 145.7 sq.ft. appr. 1.121 m appr. 3 ft 8.1 in appr. 10.53 appr. 5° appr. 1° 
Aileron 
Area (total, left + right)  :  appr. 0.654 m2  appr.  7.0 sq.ft. 
Wing flaps 
Area (total, left + right)  :  appr. 1.56 m2  appr. 16.8 sq.ft. 
Horizontal tail 
Area Elevator area Angle of incidence  : : :  appr. 2.34 m2 appr. 25.2 sq.ft. appr. 0.665 m2 appr. 7.2 sq.ft. appr. -3.0° relative to longitudinal axis of airplane 
　
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