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钻石20系列飞机维护手册 DA 20 SERIES AIRPLANE MAINTENANCE MANUAL(70)

时间:2011-10-28 13:51来源:蓝天飞行翻译 作者:admin
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3.
EMERGENCY PROCEDURES................................................................................... S4-5


4.
NORMAL PROCEDURES .......................................................................................... S4-6


5.
PERFORMANCE ........................................................................................................ S4-6


6.
WEIGHT AND BALANCE ......................................................................................... S4-14


7.
DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS ....................................... S4-16


8.
HANDLING, PREVENTIVE AND CORRECTIVE MAINTENANCE........................... S4-16

 


1. GENERAL
This supplement addresses the effects on the DA20-C1 of an increase in the gross weight from 750 kg (1653 lbs) to 800 kg (1764 lbs) and is applicable only to aircraft with the Sensenich propeller. This increase of 50 kg (110 lbs) imposes no significant change to the control and stability of the aircraft.  Only the portions of the flight manual affected by this weight increase are
included in this supplement. 
1.10.  WEIGHT 
Maximum Ramp Weight  : 803 kg (1770 lbs) 
Maximum Take-off Weight  : 800 kg (1764 lbs) 
Maximum Landing Weight  : 800 kg (1764 lbs) 
Empty Weight  : See Chapter 6 
Maximum Weight in Baggage Compartment  : 44 lbs (20 kg) 
  only if restraining devices available 
Wing Loading 
At Maximum Take-off Weight  : 14.11 lbs/sq.ft. (68.96 kg/m2) 
Performance Load at Max. Take-off Weight  : 14.11 lbs/hp (8.58 kg/kW) 
2.  OPERATING LIMITATIONS 
2.7.  WEIGHT 
Maximum Ramp Weight  : 803 kg (1770 lbs) 
Maximum permissible weight  : 800 kg (1764 lbs) 
Maximum permissible weight in the baggage   : 44 lbs (20 kg) only permissible 
compartment (including baggage extension,  with baggage harness 
if fitted) 

WARNING

EXCEEDING WEIGHT LIMITATIONS MAY LEAD TO OVERLOADING OF THE AIRPLANE AND CAUSE LOSS OF CONTROL OF THE AIRPLANE AND/OR STRUCTURAL DAMAGE.

2.8. CENTER OF GRAVITY


Points  Gross Weight   Arm (aft of datum) 
(lbs)  (kgs)  (in)  (m) 
A  1653  750  7.95  .202 
B  1764  800  8.07  .205 
C  1764  800  12.16  .309 
D  1653  750  12.48  .317 

WARNING

EXCEEDING THE CENTER OF GRAVITY LIMITATIONS REDUCES THE MANOEUVRABILITY AND STABILITY OF THE AIRPLANE.
The procedure used to determine the center of gravity is described in Chapter 6.

2.9.  APPROVED MANEUVERS
 
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