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钻石40飞机飞行手册 DA 40 Airplane Flight Manual(16)

时间:2011-10-28 12:56来源:蓝天飞行翻译 作者:admin
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3.5  EMERGENCY LANDINGS .............................. 3-24

3.5.1  EMERGENCY LANDING WITH ENGINE OFF .......... 3-24

3.5.2  LANDING WITH A DEFECTIVE TIRE ON THE MAIN LANDING GEAR ......................................... 3-25
3.5.3  LANDING WITH DEFECTIVE BRAKES ............... 3-26

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Doc. No. 6.01.05-E  Revision 1  03-Mar-2003  Page 3 - 1 


3.6 RECOVERY FROM AN UNINTENTIONAL SPIN ............. 3-27

3.7 OTHER EMERGENCIES ............................... 3-28

3.7.1 ICING ......................................... 3-28

3.7.2 FAILURES IN THE ELECTRICAL SYSTEM ............ 3-29

3.7.3 SUSPICION OF CARBON MONOXIDE CONTAMINATION IN THE
CABIN ......................................... 3-30
% 3.7.4 'DOOR'-WARNING LIGHT ON ...................... 3-31

NOTE
Procedures for uncritical system faults are given in Chapter 4B - ABNORMAL OPERATING PROCEDURES.
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Doc. No. 6.01.05-E  Revision 3  26-May-2003  Page 3 - 2 


3.1 INTRODUCTION
3.1.1 GENERAL
This Chapter contains checklists as well as the description of recommended procedures to be followed in the event of an emergency. Engine failure or other airplane-related emergencies are most unlikely to occur if the prescribed procedures for pre-flight checks and airplane maintenance are followed.
If, nonetheless, an emergency does arise, the guidelines given here should be followed and applied in order to clear the problem.
As it is impossible to foresee all kinds of emergencies and cover them in this Airplane Flight Manual, a thorough understanding of the airplane by the pilot is, in addition to his knowledge and experience, an essential factor in the solution of any problems which may arise.
WARNING
In each emergency, control over the flight attitude and the preparation of a possible emergency landing have priority over attempts to solve the current problem ("first fly the aircraft"). Prior to the flight the pilot must consider the suitability of the terrain for an emergency landing for each phase of the flight. For a safe flight the pilot must constantly keep a safe minimum flight altitude. Solutions for various adverse scenarios should be thought over in advance. Thus it should be guaranteed that the pilot is at no time shocked by an engine failure and that he can act calmly and with determination.


3.1.2 CERTAIN AIRSPEEDS IN EMERGENCIES

Event  850 kg 1874 lb  1000 kg 2205 lb  1150 kg 2535 lb 
Engine failure after take-off (Flaps T/O)  59 KIAS  66 KIAS  72 KIAS 
Airspeed for best glide angle (Flaps UP)  60 KIAS  68 KIAS  73 KIAS 
Emergency landing with engine off  Flaps UP  60 KIAS  68 KIAS  73 KIAS 
Flaps T/O  59 KIAS  66 KIAS  72 KIAS 
Flaps LDG  58 KIAS  63 KIAS  71 KIAS 
 
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