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2010-09-23
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Airworthiness Directives; Boeing Model 727 Airplanes
Rules and Regulations
D09002ee1bde31470
D09002ee1bde31909
United States
Department of Transportation
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org
United States Government Agency or Subagency
United States
Federal Aviation Administration
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United States Government Agency or Subagency
The FAA is adopting a new airworthiness directive (AD) for all Boeing Model 727 airplanes. This AD requires a one-time inspection of the lower lobe frames of body section 43 to find open holes between stringers 17L and 17R and to record their location; repetitive high frequency eddy current (HFEC) inspections for cracks of all open holes; and related investigative and corrective actions if necessary. This AD also includes an optional terminating action of installing rivets in all open tooling holes and all unused lining holes, which would terminate the repetitive open-hole HFEC inspections once a hole is plugged with a rivet. This AD results from reports of cracks at open tooling holes in the lower lobe frames of body section 43. We are issuing this AD to detect and correct cracks in the frames, which could result in cracks in the skin panels and rapid decompression of the airplane.
70 FR 58002
https://www.govinfo.gov/app/details/FR-2005-10-05/05-19842
05-19842
fr05oc05-6
RIN 2120-AA64
4910-13-P
Docket No. FAA-2005-21085
Directorate Identifier 2004-NM-252-AD
Amendment 39-14307
AD 2005-20-13
https://www.govinfo.gov/app/details/FR-2005-10-05/05-19842
https://www.govinfo.gov/content/pkg/FR-2005-10-05/html/05-19842.htm
https://www.govinfo.gov/content/pkg/FR-2005-10-05/pdf/05-19842.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
4 p.
58002
58005
70 FR 58002
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Boeing Model 727 Airplanes; Federal Register Vol. 70, Issue
RULE
05-19842
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2005-11-09
Docket No. FAA-2005-21085
Directorate Identifier 2004-NM-252-AD
Amendment 39-14307
AD 2005-20-13
4910-13-P
05-19842
Final rule.
The FAA is adopting a new airworthiness directive (AD) for all Boeing Model 727 airplanes. This AD requires a one-time inspection of the lower lobe frames of body section 43 to find open holes between stringers 17L and 17R and to record their location; repetitive high frequency eddy current (HFEC) inspections for cracks of all open holes; and related investigative and corrective actions if necessary. This AD also includes an optional terminating action of installing rivets in all open tooling holes and all unused lining holes, which would terminate the repetitive open-hole HFEC inspections once a hole is plugged with a rivet. This AD results from reports of cracks at open tooling holes in the lower lobe frames of body section 43. We are issuing this AD to detect and correct cracks in the frames, which could result in cracks in the skin panels and rapid decompression of the airplane.
This AD becomes effective November 9, 2005.
Daniel F. Kutz, Aerospace Engineer, Airframe Branch, ANM-120S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 917-6456; fax (425) 917-6590.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness directives:
Boeing,
http://dms.dot.gov
http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html
Federal Register
Vol. 70, no. 192
Office of the Federal Register, National Archives and Records Administration
2005-10-05
continuing
daily
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born digital
306 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2005-10-05
P0b002ee1809892d2
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr05oc05
https://www.govinfo.gov/app/details/FR-2005-10-05
https://www.govinfo.gov/content/pkg/FR-2005-10-05/pdf/FR-2005-10-05.pdf
https://www.govinfo.gov/content/pkg/FR-2005-10-05/xml/FR-2005-10-05.xml
fdlp
57993
58289
DGPO
2010-09-23
2023-05-03
FR-2005-10-05
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eng
FR
FR-2005-10-05
70
192