[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 [www.gpo.gov]
[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