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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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