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时间:2011-02-12 08:57来源:蓝天飞行翻译 作者:admin
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R EFF : 001-049, 051-099, 101-149, 201-299,  08-10-00Page 607   May 01/05   CES


 (2)
 Weigh the aircraft on its wheels and calculate the position of the center of gravity.

 (a) Refer to the Weight and Balance Manual to weigh the aircraft and calculate the position of the center of gravity (Ref. WBM 1-80-05).

 (3)
 Weigh the aircraft on landing gear jacks and calculate the position of the center of gravity.


 NOTE : You can do this procedure with load cells on each jack or with
____ platform scales under each jack. The load cells or the platform scales must have a capacity of:
 -7000 daN min. at nose landing gear
 -30000 daN min. at main landing gear
 (a)
 Put the jacks and the weighing devices in position.

 (b)
 Jack up the aircraft (Ref. TASK 07-11-00-582-003).

 (c)
 Refer to the Weight and Balance Manual to weigh the aircraft and calculate the position of the center of gravity (Ref. WBM 1-80-04).


R **ON A/C 151-199, 401-499,
 Subtask 08-10-00-220-050-A
 A. Weigh the Aircraft and Calculate the Position of the Center of Gravity
 NOTE : You can weigh the aircraft with:
____
 -
the aircraft on jacks

 -
the aircraft on its wheels

 -
the aircraft on landing gear jacks


 (1) Weigh the aircraft on jacks and calculate the position of the center of gravity.
 NOTE : To weigh the aircraft on jacks, the aircraft must have a pitch
____
 attitude of zero deg..

 NOTE : You can refer to the Weight and Balance Manual to weigh the
____ aircraft and calculate the position of the center of gravity (Ref. WBM 1-80-05).
R EFF : 001-049, 051-099, 101-149, 151-199,  08-10-00Page 608 201-299, 401-499, Aug 01/05   CES  NOTE : You can do this procedure with load cells on each jack or with


____ platform scales under each jack. The load cells or the platform scales must have a capacity of:
 -7000 daN min. at nose landing gear
 -30000 daN min. at main landing gear
 (a)
 Put the jacks and the weighing devices in position.

 (b)
 Jack up the aircraft and make the aircraft level (Ref. TASK 08-21-00-200-001).

 (c)
 Calculate the aircraft weight W: W = RA + RV
 W = aircraft weight
 RA = reaction that you measure at the forward jack point.

 

 NOTE : If you use platform scales, you must subtract the weight
____
 of the jack.

 RV = sum of the reactions that you measure at the wing jack
 points.
 NOTE : If you use platform scales, you must subtract the weight
____
 of the jacks.

 RC = Reference Chord
 (d) Calculate the position of the center of gravity.
 To do this, use the formula:

 54.98 RV - 260.34 RA
 CG (% RC) =  -------------------W
 (e) Lower the aircraft on its wheels (Ref. TASK 07-11-00-586-002).
 (2)
 Weigh the aircraft on its wheels and calculate the position of the center of gravity.

 (a) Refer to the Weight and Balance Manual to weigh the aircraft and calculate the position of the center of gravity (Ref. WBM 1-80-04).

 (3)
 Weigh the aircraft on landing gear jacks and calculate the position of the center of gravity.


 NOTE : You can do this procedure with load cells on each jack or with
____ platform scales under each jack. The load cells or the platform scales must have a capacity of:
R EFF : 151-199, 401-499,  08-10-00Page 609   Aug 01/05   CES


 -7000 daN min. at nose landing gear
 -30000 daN min. at main landing gear
 (a)
 Put the jacks and the weighing devices in position.

 (b)
 Jack up the aircraft (Ref. TASK 07-11-00-582-003).

 (c)
 Refer to the Weight and Balance Manual to weigh the aircraft and calculate the position of the center of gravity (Ref. WBM 1-80-05).


 **ON A/C 301-399,
 Subtask 08-10-00-220-050-B
 A. Weigh the Aircraft and Calculate the Position of the Center of Gravity NOTE : You can weigh the aircraft with:
____
 -
the aircraft on jacks

 -
the aircraft on its wheels

 -
the aircraft on landing gear jacks


 (1) Weigh the aircraft on jacks and calculate the position of the center of gravity.
 NOTE : To weigh the aircraft on jacks, the aircraft must have a pitch
____
 attitude of zero deg..

 NOTE : You can refer to the Weight and Balance Manual to weigh the
 
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