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Regulatory Information
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2010-09-23
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Airworthiness Directives; Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes
Rules and Regulations
D09002ee1bde5c900
D09002ee1bde5cba6
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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org
United States Government Agency or Subagency
This document corrects a typographical error that appeared in airworthiness directive (AD) 2004-19-10 that was published in the Federal Register on September 27, 2004 (69 FR 57632). The typographical error resulted in the omission of the AD number in one location of the document. This AD is applicable to certain Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This AD requires repetitive inspections for corrosion and cracking of the pivot hinge pins of the horizontal stabilizer, certain follow-on inspections, and replacement of the hinge pins with new or serviceable pins if necessary.
69 FR 62399
https://www.govinfo.gov/app/details/FR-2004-10-26/04-23928
04-23928
fr26oc04-4
RIN 2120-AA64
4910-13-P
Docket No. 2003-NM-90-AD
Amendment 39-13804
AD 2004-19-10
https://www.govinfo.gov/app/details/FR-2004-10-26/04-23928
https://www.govinfo.gov/content/pkg/FR-2004-10-26/html/04-23928.htm
https://www.govinfo.gov/content/pkg/FR-2004-10-26/pdf/04-23928.pdf
1 p.
62399
62399
69 FR 62399
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, -200C, -300, -400, and -500 Series Airplanes; Federal Register Vol. 69, Issue
RULE
04-23928
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2004-11-01
Docket No. 2003-NM-90-AD
Amendment 39-13804
AD 2004-19-10
4910-13-P
04-23928
Final rule; correction.
This document corrects a typographical error that appeared in airworthiness directive (AD) 2004-19-10 that was published in the Federal Register on September 27, 2004 (69 FR 57632). The typographical error resulted in the omission of the AD number in one location of the document. This AD is applicable to certain Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This AD requires repetitive inspections for corrosion and cracking of the pivot hinge pins of the horizontal stabilizer, certain follow-on inspections, and replacement of the hinge pins with new or serviceable pins if necessary.
Effective November 1, 2004.
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.
Airworthiness directives:
Boeing; correction,
Federal Register
Vol. 69, no. 206
Office of the Federal Register, National Archives and Records Administration
2004-10-26
continuing
daily
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170 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2004-10-26
P0b002ee18098120e
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr26oc04
https://www.govinfo.gov/app/details/FR-2004-10-26
https://www.govinfo.gov/content/pkg/FR-2004-10-26/pdf/FR-2004-10-26.pdf
https://www.govinfo.gov/content/pkg/FR-2004-10-26/xml/FR-2004-10-26.xml
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62393
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DGPO
2010-09-23
2023-05-03
FR-2004-10-26
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eng
FR
FR-2004-10-26
69
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