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时间:2011-03-27 08:58来源:蓝天飞行翻译 作者:admin
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 2_ Scratches
 (Ref. Fig. 619/TASK 56-11-12-991-046)
 NOTE : If you see scratches, you must do a check of the depth____
 of the scratches:
 - with your finger nail or
 - with the MITUTOYO surface tester SJ201 (Ref. TASK 56-
10-00-200-004). 

R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 56-11-12Page 623 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1


 Acrylic Fixed Window - Burn Spot Inspection Procedure
 Figure 616/TASK 56-11-12-991-043

R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 56-11-12Page 624 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1


 Acrylic Fixed Window - Crazing Inspection Procedure
 Figure 617/TASK 56-11-12-991-044

R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 56-11-12Page 625 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1


 Glass Fixed Window - Permitted Damage
 Figure 618/TASK 56-11-12-991-045

R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 56-11-12Page 626 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1


 Glass Fixed Window - Permitted Damage
 Figure 619/TASK 56-11-12-991-046

R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 56-11-12Page 627 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1 3 Chips


_ (Ref. Fig. 620/TASK 56-11-12-991-048)
 4 Delamination
_ (Ref. Fig. 621/TASK 56-11-12-991-047)
 5 Bubbles
_ (Ref. Fig. 622/TASK 56-11-12-991-049)
 6 Discoloration
_ (Ref. Fig. 622/TASK 56-11-12-991-049)
 7 Transparency
_ (Ref. Fig. 622/TASK 56-11-12-991-049)
 8 Interlayer microflakes
_ (Ref. Fig. 623/TASK 56-11-12-991-051)
 9 Burn spots
_ (Ref. Fig. 624/TASK 56-11-12-991-050)
 (b) Do a check for burn spots. (Ref. Fig. 625/TASK 56-11-12-991-052)
 1_ Put a light source at 45 deg. to the outer surface of the
 window panel.
 2_ Do a check of the bus bar for burn spots.
 5. Close-up________

 Subtask 56-11-12-865-064
 A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1DG1, 4DG1, 5DG1, 1DG2, 4DG2, 5DG2, 5SQ1, 5SQ2.
 Subtask 56-11-12-942-056
 B. Get Access
 (1)
 Put the access platform in position at the zone 210.

 (2)
 Clean the fixed windows (Ref. TASK 56-10-00-110-002).


R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 56-11-12Page 628 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1


 Glass Fixed Window - Permitted Damage
 Figure 620/TASK 56-11-12-991-048

R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 56-11-12Page 629 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1


 Glass Fixed Window - Permitted Damage
 Figure 621/TASK 56-11-12-991-047

R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 56-11-12Page 630 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1


 Glass Fixed Window - Permitted Damage
 Figure 622/TASK 56-11-12-991-049

R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 56-11-12Page 631 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1


 Glass Fixed Window - Permitted Damage
 Figure 623/TASK 56-11-12-991-051

R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 56-11-12Page 632 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1


 Glass Fixed Window - Permitted Damage
 Figure 624/TASK 56-11-12-991-050

R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 56-11-12Page 633 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1


 Glass Fixed Window - Burn Spot Inspection Procedure
 Figure 625/TASK 56-11-12-991-052

R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 56-11-12Page 634 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1


 SLIDING WINDOWS - DESCRIPTION AND OPERATION
___________________________________________
 1. General
_______
 A. Sliding Windows The cockpit includes two sliding windows (left and right) installed between FR5 and FR8. The crew can use these sliding windows as emergency exits.
 B. Sliding Window Panels Each panel is installed in a frame. The frames permit the panels to move on the rails which are fixed to the aircraft structure.
 1EFF : ALL 1 56-12-00Page 1 1 1 Feb 01/98 1 1 1CES 1


 2. Description
___________
 A. General R **ON A/C 001-049, 101-149, 151-199, 201-299, 301-399, 401-499,
 (Ref. Fig. 001)
 **ON A/C 051-099,

 (Ref. Fig. 001A)
 **ON A/C ALL

 (1) Each sliding window includes:
 (a)
 A panel which has an anti-icing and defogging system. This panel is installed in a frame.

 (b)
 The opening/closing mechanism.


 B. Composition of Panels
 
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