AD 2004-03-34 R1

final rule

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

AD Number
2004-03-34 R1
Status
final_rule
Effective Date
Product Category
aircraft
Docket
2004-NM-29-AD
FR Citation
(Federal Register: June 16, 2004 (Volume 69, Number 115))

Applicability

TypeManufacturerModelDetails
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

The existing screw, nut, and washers that attach the latch cable assembly to the latch block assembly of the door mounted escape slides may fail, which could result in improper operation of the escape slides.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Replace existing screw, nut, and washers with new, improved screw, nut, and washers.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Effective July 21, 2004

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

Door mounted escape slides

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - 040334R1.pdf
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DetailsAttachments/Public Comments
AD Number:
2004-03-34 R1
Document Type:
AD Final Rules
Docket Number:
2004-NM-29-AD
Subject Heading:
Airworthiness Directives; Boeing Model 737-100, -200, -200C, - 300, -400, and -500 Series Airplanes
Subject:
Door mounted escape slides
Status:
Current
Citation:
(Federal Register: June 16, 2004 (Volume 69, Number 115))
Citation Publish Date:
06/16/2004
Effective Date:
07/21/2004
Make:
The Boeing Company
Model:
737-100 Series | 737-200 Series | 737-200C Series | 737-300 Series | 737-400 Series | 737-500 Series
Product Type:
Aircraft
Product Subtype:
Large Airplane
Affected AD:
Superseded AD:
2004-03-34
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
CORRECTION: (Federal Register: July 8, 2004 (Volume 69, Number 130); Page 41189;\nwww.access.gpo.gov/su_docs/aces/aces140.html) Go to the attached "pd... ...Show more
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[Federal Register: July 8, 2004 (Volume 69, Number 130)]


[Rules and Regulations]


[Page 41189]


From the Federal Register Online via GPO Access [wais.access.gpo.gov]


[DOCID:fr08jy04-3]


–––––––––––––––––––––––––––––––––––


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.


–––––––––––––––––––––––––––––––––––


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.
2


The effective date of this AD remains July 21, 2004.


PART 39–AIRWORTHINESS DIRECTIVES


§ 39.13 [Corrected]


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

Document Text

Show stored source text (verify against official source)
AD Final Rules - 040334R1.pdf
Copy URL
Document Versions
 Feedback
DetailsAttachments/Public Comments
AD Number:
2004-03-34 R1
Document Type:
AD Final Rules
Docket Number:
2004-NM-29-AD
Subject Heading:
Airworthiness Directives; Boeing Model 737-100, -200, -200C, - 300, -400, and -500 Series Airplanes
Subject:
Door mounted escape slides
Status:
Current
Citation:
(Federal Register: June 16, 2004 (Volume 69, Number 115))
Citation Publish Date:
06/16/2004
Effective Date:
07/21/2004
Make:
The Boeing Company
Model:
737-100 Series | 737-200 Series | 737-200C Series | 737-300 Series | 737-400 Series | 737-500 Series
Product Type:
Aircraft
Product Subtype:
Large Airplane
Affected AD:
Superseded AD:
2004-03-34
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
CORRECTION: (Federal Register: July 8, 2004 (Volume 69, Number 130); Page 41189;\nwww.access.gpo.gov/su_docs/aces/aces140.html) Go to the attached "pd... ...Show more
Automatic Zoom
Actual Size
Page Fit
Page Width
⁨50⁩%
⁨75⁩%
⁨100⁩%
⁨125⁩%
⁨150⁩%
⁨200⁩%
⁨300⁩%
⁨400⁩%
125%
of ⁨7⁩
1


[Federal Register: July 8, 2004 (Volume 69, Number 130)]


[Rules and Regulations]


[Page 41189]


From the Federal Register Online via GPO Access [wais.access.gpo.gov]


[DOCID:fr08jy04-3]


–––––––––––––––––––––––––––––––––––


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.


–––––––––––––––––––––––––––––––––––


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.
2


The effective date of this AD remains July 21, 2004.


PART 39–AIRWORTHINESS DIRECTIVES


§ 39.13 [Corrected]


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

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.