Airworthiness Directives; Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes

[Federal Register Volume 69, Number 130 (Thursday, July 8, 2004)]
[Rules and Regulations]
[Page 41189]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 04-15365]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2004-NM-29-AD; Amendment 39-13673; AD 2004-03-34 R1]
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.

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SUMMARY: This document corrects a typographical error that appeared in 
airworthiness directive (AD) 2004-03-34 R1 that was published in the 
Federal Register on June 16, 2004 (69 FR 33555). A reference to the 
amendment number was inadvertently omitted from a heading in the AD. 
This AD is applicable to certain Boeing Model 737-100, -200, -200C, -
300, -400, and -500 series airplanes. This AD requires replacing 
existing screw, nut, and washers that attach the latch cable assembly 
to the latch block assembly of the door mounted escape slides, with 
new, improved screw, nut, and washers.

DATES: Effective July 21, 2004.

FOR FURTHER INFORMATION CONTACT: Keith Ladderud, Aerospace Engineer, 
Cabin Safety and Environmental Systems Branch, ANM-150S, FAA, Seattle 
Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, 
Washington 98055-4056; telephone (425) 917-6435; fax (425) 917-6590.

SUPPLEMENTARY INFORMATION: Airworthiness Directive (AD) 2004-03-34 R1, 
amendment 39-13673, applicable to certain Boeing Model 737-100, -200, -
200C, -300, -400, and -500 series airplanes, was published in the 
Federal Register on June 16, 2004 (69 FR 33555). That AD requires 
replacing existing screw, nut, and washers that attach the latch cable 
assembly to the latch block assembly of the door mounted escape slides, 
with new, improved screw, nut, and washers.
    As published, the heading preceding the ``Applicability'' paragraph 
has a typographical error. That airworthiness directive reads as 
``2004-03-34 R1 Boeing: Docket 2004-NM-29-AD. Revises AD 2004-03-34, 
Amendment 39-13478.'' However, the new amendment number, 39-13673, was 
inadvertently omitted. That airworthiness directive should have read 
``2004-03-34 R1 Boeing: amendment 39-13673. Docket 2004-NM-29-AD. 
Revises AD 2004-03-34, Amendment 39-13478.''
    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 July 21, 2004.

PART 39--AIRWORTHINESS DIRECTIVES


Sec.  39.13  [Corrected]

0
On page 33556, in the third column, the section preceding the 
``Applicability'' paragraph of AD 2004-03-34 R1 is corrected to read as 
follows:
* * * * *

2004-03-34 R1 Boeing: Amendment 39-13673. Docket 2004-NM-29-AD. 
Revises AD 2004-03-34, Amendment 39-13478.

* * * * *

    Issued in Renton, Washington, on June 29, 2004.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 04-15365 Filed 7-7-04; 8:45 am]
BILLING CODE 4910-13-P

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