Eagle ICA-D212-725, Instructions Manual

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ICA-D212-725 (52
)
Page 44 of 54
CHAPTER 52 – DOORS AND WINDOWS (52-00-00)
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COPYRIGHT
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2007 BY DART AEROSPACE LTD.
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THIS DOCUMENT IS PRIVATE AND CONFIDENTIAL AND IS SUPPLIED ON THE EXPRESS CONDITION THAT IT IS NOT TO BE USED FOR ANY PURPOSE OR COPIED OR COMMUNICATED TO
ANY OTHER PERSON WITHOUT WRITTEN PERMISSION FROM DART AEROSPACE LTD.
Revision: 4
Date: 11.06.01
Scratches and pits may polished out to the extent that vision is not distorted. Distortion of vision is cause
for replacement. Cracks, holes or other damage may be temporarily repaired, if vision of crew members
will not be impaired by stop drilling, patching or other approved methods (refer to FAA Advisory Circular
43.13-1B. Aircraft Inspection and Repair), but window must be replaced at the earliest opportunity.
Scratches and pits are permitted in this area provided they are not so numerous or form such a pattern as
to be objectionable to the viewer. Cracks, holes or other damage may be temporarily repaired by stop
drilling, patching or other approved methods (refer to FAA Advisory Circular 43.13-1B. Aircraft Inspection
and Repair), but window must be replaced at the earliest opportunity.
Scratches and pits are permitted in this area providing the structural integrity of the window is not impaired.
Cracks, holes or other damage may be repaired by stop drilling, patching or other approved methods
provided structural integrity is not impaired (refer to FAA Advisory Circular 43.13-1B. Aircraft Inspection
and Repair.)
Figure 52-12. Windshield and Window Damage Limits