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钻石20飞机飞行手册 DA 20 Airplane Flight Manual(36)

时间:2011-10-28 13:14来源:蓝天飞行翻译 作者:admin
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4.4.17. Idle Power Operations
NOTE

Turn fuel pump on for all low throttle operations, including taxiing and all flight operations when engine speed could fall below 1400 RPM (eg. stalls, descents, spins, landings, etc.).
1.
 Fuel Pump ON

2.
 Mixture FULL RICH

3.
Throttle IDLE


NOTE

For aircraft with altitude compensating fuel system minimum recommended flight idle is 1400 RPM, during idle power flight conditions and maneuvres.

CHAPTER 5

PERFORMANCE

5.1. INTRODUCTION...............................................................................................................2


5.2. USE OF PERFORMANCE TABLES AND DIAGRAMS ....................................................2


5.3. PERFORMANCE TABLE AND DIAGRAMS.....................................................................3


5.3.1. Airspeed System Calibration.....................................................................................3


5.3.2. Cruising Performance................................................................................................4


5.3.3. Stall Speeds..............................................................................................................5


5.3.4. Wind Components.....................................................................................................6


5.3.5. Take-off Distance......................................................................................................7


5.3.6. Climb Performance / Cruising Altitudes.....................................................................8


5.3.7. Climb Performance / Take off....................................................................................9


5.3.8. Cruising Speed (True Airspeed)..............................................................................10


5.3.9. Maximum Flight Duration ........................................................................................10


5.3.10. Climb Performance / Balked Landing......................................................................12


5.3.11. Landing Distance.....................................................................................................13


5.4. NOISE DATA ..................................................................................................................13

 

5.1. INTRODUCTION
This chapter contains the performance data required by the basis of certification.  This data which has been approved by Transport Canada is marked ‘DOT Approved’ in the footer of the page. Where additional performance data has been provided, beyond the basis for certification, it has not been reviewed or approved by Transport Canada.
The performance data contained in the following pages has been prepared to illustrate the performance you may expect from your airplane and to assist you in precise flight planning. The data presented has been derived from test-flights using an airplane and engine in good operating condition.  The data is corrected to standard atmospheric conditions 59° F (15° C) and
 
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