56-11-21
ALL ú ú B06 Page 604 ú Jul 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
ú (b) Scratches on the inner pane if they are larger than the ú specified limits. ú ú~...............................................................................
ú| Scratch | Max Length | Max Cumulative |
ú| Depth | of Each | Length of All |
ú| (in.) | Scratch (in.) | Scratches (in.) |
ú................................................................................. ú| 0.005 | 1.0 | 5.0 | ú2.......................…..........................…............................1 ú
S 356-005-B00
(4) Polish the scratches in the window surface (Ref 56-11-21/801).
NOTE: It is not necessary to polish small scratches, 0.001 inch or
____ less. These scratches are not very important.
Scratches on the inner pane are not permitted if they are more than these limits. They cannot be more than 0.005 inch deep, one inch in length or more than 5 inches total of all scratches.
Do not polish the window pane to less than the thickness
shown.
~.............................................. | Outer Pane | Inner Pane*[1] | ................................................ | 0.400 inch | 0.230 inch | 2....................….........................1 *[1] Refer to the Overhaul Manual for Repair
S 216-006-B00
(5) Examine the window for crazing.
(a)
Crazing in an inner stretched acrylic pane.
(b)
Surface crazing in the outer stretched acrylic pane, other than at the routed edge.
NOTE: Replace the window if the crazing is more than these
____ limits.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
56-11-21
ALL ú ú B04.1 Page 605 ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
~.............................................. | Max Depth (in.) | Max Local Area | ................................................ | 0.040 | 2.0 inch dia | | 0.030 | Over entire surface | 2....................….........................1
S 216-007-B00
(6) Examine the window for chips.
(a)
Chips in the outer stretched acrylic pane larger than these limits.
~.............................................. | Max Chip | Max, Size of | Min Distance | | Depth | Delamination | Between Chips | | (inch) | Due to Chip | (inches) | ................................................ | 0.05 | 0.50 dia. | 1.00 | 2............…...............….................1
(b)
Chips on the inner surface of the inner pane or along the edge if they are more than 0.06 inch in depth.
NOTE: To remove edge chips and delaminations, chamfer the edge
____ of the pane. Refer to the Overhaul Manual.
S 216-008-B00
(7) Examine the window for delaminations (in-plane cracks) (Fig. 602).
(a)
Delaminations, if the visual quality of the window is not good.
(b)
Delaminations larger than these limits.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
56-11-21
ú ALL ú
ú ú ú B01.101 ú BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. Page 606Jul 12/02
A
737-300/400/500MAINTENANCE MANUAL
~.............................................................................. | Edge *[1] | Max Extension | Max Length | Min Distance | Max No. | Max No. | | | in from Edge | at Edge | Between Defects | per Edge| per Pane| ................................................................................
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊(cè) WINDOWS(28)
