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时间:2010-05-17 21:12来源:蓝天飞行翻译 作者:admin
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Centre of Gravity Limits (MTOW 48,200 lb)
Figure 02−03−1


 

 
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*+,-.,+/0.1.2345
+67/0.26./4869
,234:826486;2;
<.,:244.926432;-+6.

LIMITATIONS
Centre of Gravity
02−03−2
1. CENTRE OF GRAVITY LIMITS (MTOW 48,200 LB) (CONT’D)
On airplanes 5301 to 5547, 5549 and 5550 NOT incorporating Service Bulletin 604−28−007
and airplanes 5301 to 5571 NOT incorporating Service Bulletin 604−27−009 or 604−27−012:
The maximum permissible centre of gravity (CG) limits are as shown in Figure 02−03−2.
The airplane including interior payload, passengers and fuel (refer to Figure 02−05−2) must be
loaded such that the airplane weight and centre of gravity are maintained within the specified limits
(including variations due to fuel consumption, passenger movement, retraction of landing gear,
etc.).

CL-604 Airplane Flight Manual
PSP 604−1
DOT Approved
Centre of Gravity Limits (MTOW 48,200 lb)
Airplanes 5301 to 5547, 5549 and 5550 NOT incorporating Service Bulletin 604−28−007 and
airplanes 5301 to 5571 NOT incorporating Service Bulletin 604−27−009 or 604−27−012
Figure 02−03−2


     










 



 


 
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*+,-.,+/0.1.2345
+67/0.26./4869
,234:826486;2;
<.,:244.926432;-+6.

REV 58, Dec 05/05
LIMITATIONS
Centre of Gravity
02−03−3
2. CENTRE OF GRAVITY LIMITS (MTOW 47,600 LB)
(Airplanes 5301 to 5639 NOT Incorporating Service Bulletin 604−11−001)
The maximum permissible centre of gravity (CG) limits are as shown in Figure 02−03−3.
The airplane including interior payload, passengers and fuel (refer to Figure 02−05−2) must be
loaded such that the airplane weight and centre of gravity are maintained within the specified limits
(including variations due to fuel consumption, passenger movement, retraction of landing gear,
etc.).
The stabilizer trim setting must be in accordance with Figure 04−10−1.

CL-604 Airplane Flight Manual
PSP 604−1
DOT Approved


     










 



 


  

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Centre of Gravity Limits (MTOW 47,600 lb)
Figure 02−03−3
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*+,-.,+/0.1.2345
+67/0.26./4869
,234:826486;2;
<.,:244.926432;-+6.

REV 58, Dec 05/05
LIMITATIONS
Centre of Gravity
02−03−4
2. CENTRE OF GRAVITY LIMITS (MTOW 47,600 LB) (CONT’D)
(Airplanes 5301 to 5639 NOT Incorporating Service Bulletin 604−11−001
On airplanes 5301 to 5547, 5549 and 5550 NOT incorporating Service Bulletin 604−28−007
 
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