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钻石20飞机飞行手册 DA 20 Airplane Flight Manual(40)

时间:2011-10-28 13:14来源:蓝天飞行翻译 作者:admin
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-Standard Setting, MSL Landing distance over a 50 ft (15 m) obstacle: approx. 1280 ft (390m) Landing roll distance: approx. 5 80 ft (1 77m)
Height above LMS  ft. (m)  0 (0)  0 ) 100 (305  0 ) 200 (610  0 5) 300 (91  400 22 0 (1 0)  500 (15 0 24)  600 (1 0 829)  700 (2 0 134) 
Landing Distance  ft. (m)  280 1 390  5130 398  2133 406  60 4 13 41  423 1388   14 4 18 32  1 4 449  42  1 4 481  51 
Lan ing Ro Distance d ll  ft. (m)  581 177  598 182  616 188  5 3 63 19  654 199  6 2 74 05  6 2 95 12  7 2 16 25 

Figure 5.11. Landing and Rolling Distances for Heights Above MSL
NOTE

Poor m aintenance condition of the airplane, deviation from the given procedures as well as unfavorable outside conditions (i. e .high temperature, rain,  unfavorable wind conditions, slippery runway) could increase the landing  dis tance co nsiderably.
NOTE

Aircraft with ground idle speed set  to 1 000 RPM, landing distance increased approx. 5% and ground roll increase d approx. 7%.
5.4. NOISE DA TA
Noise Measu odrement Meth  ropeller W69 3Sensenich P EK-6  wable Maximum Allo 
FAR36 A dix G ppen  B71.4 d A  75 dBA 
ICA Annex 1 ppend O 6, A ix 6  B74.1 d A  79.1 dBA 

Doc # DA202-C1  April 16, 2009  Page 5 - 13 
Revision 24  DOT Approved 

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CHAPTER 6

WEIGHT AND BALANCE / EQUIPMENT LIST

6.1. INTRODUCTION...............................................................................................................2


6.2. AIRPLANE WEIGHING.....................................................................................................3


6.3. WEIGHT AND BALANCE REPORT .................................................................................6


6.4. FLIGHT WEIGHT AND CENTER OF GRAVITY...............................................................8


6.5. EQUIPMENT LIST ..........................................................................................................12

 

6.1. INTRODUCTION
To obtain the performance, flight characteristics and safe operation described in this Flight Manual, the airplane must be operated within the permissible weight and balance envelope as described in Chapter 2.  It is the pilot's responsibility to adhere to the weight and balance limitations and to take into consideration the change of the center of gravity (CG) position due to fuel consumption.
The procedure for weighing the airplane and calculating the empty weight CG position are given in this Chapter.
The aircraft is weighed when new and should be reweighed in accordance with applicable air regulations.  Empty weight and the center of gravity are recorded in a Weighing Report and in the Weight & Balance Report, included at the back of this manual.
 
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