AD 2004-19-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 737-100 Series | Airworthiness Directives; Boeing Model 737-100, -200, -200C, - 300, -400, and -500 Series Airplanes |
| aircraft | The Boeing Company | 737-200 Series | Airworthiness Directives; Boeing Model 737-100, -200, -200C, - 300, -400, and -500 Series Airplanes |
| aircraft | The Boeing Company | 737-200C Series | Airworthiness Directives; Boeing Model 737-100, -200, -200C, - 300, -400, and -500 Series Airplanes |
| aircraft | The Boeing Company | 737-300 Series | Airworthiness Directives; Boeing Model 737-100, -200, -200C, - 300, -400, and -500 Series Airplanes |
| aircraft | The Boeing Company | 737-400 Series | Airworthiness Directives; Boeing Model 737-100, -200, -200C, - 300, -400, and -500 Series Airplanes |
| aircraft | The Boeing Company | 737-500 Series | Airworthiness Directives; Boeing Model 737-100, -200, -200C, - 300, -400, and -500 Series Airplanes |
Unsafe Condition
Corrosion and cracking of the pivot hinge pins of the horizontal stabilizer.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct repetitive inspections for corrosion and cracking of the pivot hinge pins of the horizontal stabilizer. Perform certain follow-on inspections. Replace the hinge pins with new or serviceable pins if necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight after the effective date.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
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.
Document Text
Show stored source text (verify against official source)
[Federal Register Volume 69, Number 206 (Tuesday, October 26, 2004)]
[Rules and Regulations]
[Page 62399]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 04-23928]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2003-NM-90-AD; Amendment 39-13804; AD 2004-19-10]
RIN 2120-AA64
Airworthiness Directives; Boeing Model 737-100, -200, -200C, -
300, -400, and -500 Series Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: 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.
DATES: Effective November 1, 2004.
FOR FURTHER INFORMATION CONTACT: 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.
SUPPLEMENTARY INFORMATION: Airworthiness Directive (AD) 2004-19-10,
amendment 39-13804, applicable to certain Boeing Model 737-100, -200, -
200C, -300, -400, and -500 series airplanes, was published in the
Federal Register on September 27, 2004 (69 FR 57632). That 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.
As published, the AD number is missing in the Product
Identification line in the regulatory text of the AD. The correct AD
number is 2004-19-10. The AD number is referenced correctly throughout
the remainder of the AD.
Since no other part of the regulatory information has been changed,
the final rule is not being republished in the Federal Register.
The effective date of this AD remains November 1, 2004.
Sec. 39.13 [Corrected]
0
On page 57634, in the third column, the Product Identification line of
AD 2004-19-10 is corrected to read as follows:
* * * * *
2004-19-10 Boeing: Amendment 39-13804. Docket 2003-NM-90-AD.
* * * * *
Issued in Renton, Washington, on October 18, 2004.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 04-23928 Filed 10-25-04; 8:45 am]
BILLING CODE 4910-13-P
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.
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