| Title: | 2010-246 FAA AD 2010-17-14 Boeing Model 737-100 og -200 serier |
| Summary: | FAA AD 2010-17-14 træder i kraft den 7. oktober 2010 |
| Description: | |
| Keywords: | |
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Handle:
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Document-10588
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Owner:
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TL Luftfartøjscertificering (User-23, luftfartøjscertificering:DocuShare)DS
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| Create Date: | Monday, September 6, 2010 11:04:30 AM CEST |
| Modified Date: | Monday, September 6, 2010 11:04:30 AM CEST |
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Modified By:
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| Expiration Date: | |
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Locked By:
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| Abstract: | - This AD requires repetitive inspections for cracking and damaged fasteners of certain fuselage frames and stub beams, and corrective actions if necessary.
- For certain airplanes, this AD also requires repetitive inspections for cracking of the inboard chord fastener hole of the frame at body station 639, stringer S-16, and corrective actions if necessary.
- For airplanes with a certain short edge margin, this AD requires repetitive inspections for cracking, and corrective actions if necessary; replacing the lower chord terminates the repetitive inspections.
- For airplanes on which the modification or repair is done at certain body stations, this AD requires repetitive inspections for ...
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| Add Versions: | Allowed |
| Content Type: |
Adobe Portable Document Format (.pdf) - application/pdf
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| File name: | 2010-246 FAA AD 2010-17-14.pdf |
| Is Placeholder: | No |
| Max Versions: | 4 |
| Nr.: | FAA AD 2010-17-14 |
| Size: | 45875 |
| Ready for Declare: | No |
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Appears In:
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10) Liste over AD-noter fra 27. august til 23. september 2010
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B 737
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Preferred Version:
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2010-246 FAA AD 2010-17-14 Boeing Model 737-100 og -200 serier
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... 
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