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2010-09-23
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Airworthiness Directives; Boeing Model 737-100, -200, and -200C Series Airplanes
Rules and Regulations
D09002ee1bde31471
D09002ee1bde3190a
United States
Department of Transportation
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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 certain Boeing Model 737-100, -200, and -200C series airplanes. This AD requires a one-time detailed inspection for cracking of the lugs of the inboard attach fittings of the wing leading edge slat tracks at slat numbers 2 and 5; prior or concurrent actions for certain airplanes; repetitive high-frequency eddy current (HFEC) inspections for cracking of the lug surfaces of those inboard attach fittings if necessary; and replacement of the attach fittings with new, improved fittings. This AD results from reports of damage to the lugs of certain inboard attach fittings of the leading edge slat tracks. We are issuing this AD to prevent a lifted slat, which, if the airplane performs any non-normal maneuver during takeoff or landing at very high angles of attack, could lead to the loss of the slat and reduced control of the airplane.
70 FR 58005
https://www.govinfo.gov/app/details/FR-2005-10-05/05-19871
05-19871
fr05oc05-7
RIN 2120-AA64
4910-13-P
Docket No. FAA-2005-21138
Directorate Identifier 2004-NM-131-AD
Amendment 39-14310
AD 2005-20-16
https://www.govinfo.gov/app/details/FR-2005-10-05/05-19871
https://www.govinfo.gov/content/pkg/FR-2005-10-05/html/05-19871.htm
https://www.govinfo.gov/content/pkg/FR-2005-10-05/pdf/05-19871.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
3 p.
58005
58007
70 FR 58005
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Boeing Model 737-100, -200, and -200C Series Airplanes; Federal Register Vol. 70, Issue
RULE
05-19871
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2005-11-09
Docket No. FAA-2005-21138
Directorate Identifier 2004-NM-131-AD
Amendment 39-14310
AD 2005-20-16
4910-13-P
05-19871
Final rule.
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 737-100, -200, and -200C series airplanes. This AD requires a one-time detailed inspection for cracking of the lugs of the inboard attach fittings of the wing leading edge slat tracks at slat numbers 2 and 5; prior or concurrent actions for certain airplanes; repetitive high-frequency eddy current (HFEC) inspections for cracking of the lug surfaces of those inboard attach fittings if necessary; and replacement of the attach fittings with new, improved fittings. This AD results from reports of damage to the lugs of certain inboard attach fittings of the leading edge slat tracks. We are issuing this AD to prevent a lifted slat, which, if the airplane performs any non-normal maneuver during takeoff or landing at very high angles of attack, could lead to the loss of the slat and reduced control of the airplane.
This AD becomes effective November 9, 2005.
Nancy Marsh, Aerospace Engineer, Airframe Branch, ANM-120S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 917-6440; 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/cfr/ibr-locations.html
Federal Register
Vol. 70, no. 192
Office of the Federal Register, National Archives and Records Administration
2005-10-05
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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
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57993
58289
DGPO
2010-09-23
2023-05-03
FR-2005-10-05
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FR-2005-10-05
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