Source: https://www.federalregister.gov/documents/2005/06/27/05-12514/airworthiness-directives-boeing-model-737-300--400-and--500-series-airplanes
Timestamp: 2018-04-25 17:33:02
Document Index: 79270009

Matched Legal Cases: ['art 39', 'art 2', 'art 3', 'art 2', 'art 3', 'art 2', 'art 3', 'art 3', 'art 51']

This AD becomes effective August 1, 2005.
70 FR 36821
Amendment 39-14164
AD 2005-13-27
05-12514
Request to Incorporate Revised Repair and Preventive Modification Procedures
Request to Fix Typographical Error
https://www.federalregister.gov/d/05-12514 https://www.federalregister.gov/d/05-12514
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 737-300, -400, and -500 series airplanes. This AD requires repetitive inspections for cracking of the crown area of the fuselage skin, and corrective actions if necessary. This AD is prompted by a Model 737 fuselage structure test and fatigue analysis that indicate fuselage skin cracking could occur between 21,000 and 42,000 total flight cycles. We are issuing this AD to detect and correct fatigue cracking of the fuselage skin, which could cause the fuselage skin to fracture and fail, and could result in rapid decompression of the airplane.
The incorporation by reference of a certain publication listed in the AD is approved by the Director of the Federal Register as of August 1, 2005.
Docket: The AD docket contains the proposed AD, comments, and any final disposition. You can examine the AD docket on the Internet at http://dms.dot.gov, or in person at the Docket Management Facility office between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The Docket Management Facility office (telephone (800) 647-5227) is located on the plaza level of the Nassif Building at the U.S. Department of Transportation, 400 Seventh Street SW., room PL-401, Washington, DC. This docket number is FAA-2004-19533; the directorate identifier for this docket is 2004-NM-31-AD.
The FAA proposed to amend 14 CFR part 39 with an AD for certain Boeing Model 737-300, -400, and -500 series airplanes. That action, published in the Federal Register on November 5, 2004 (69 FR 64534), proposed to require repetitive inspections for cracking of the crown area of the fuselage skin, and corrective actions if necessary.
One commenter, the airplane manufacturer, requests that the proposed AD be revised to include the instructions provided to airplane operators in Boeing Communication System Activity 1-VN5QD. This Boeing Communication revises the repair and preventive modification procedures in Boeing Special Attention Service Start Printed Page 36822Bulletin 737-53-1234, dated June 13, 2002 (which is cited as the appropriate source of service information for the proposed AD). The revised procedures reduce the number of fasteners common to the first fastener row at the tear straps. The commenter states that the fastener size and pattern in the tear straps that are part of the procedures in the original issue of the service bulletin will not be consistent with future structural repair manual (SRM) repairs. These SRM repairs are currently being developed for Model 737-300, -400, and -500 series airplanes, with 20-inch tear strap spacing. The commenter explains that the fastener pattern and size difference in the SRM is being incorporated in an effort to maximize the “fail safety” of the repair by increasing the net area across the tear strap at the critical rows of the repair. The commenter points out that the procedures in the original issue of the service bulletin are adequate and do not contain an unsafe repair; however, there is a potential inconsistency between the service bulletin and the SRM. The commenter feels that this inconsistency would not represent best design practices given the potential number of repairs that could be required if a significant amount of chem-mill cracking occurs. The commenter further states that it is planning to revise Boeing Special Attention Service Bulletin 737-53-1234 to incorporate the instructions in Boeing Communication System Activity 1-VN5QD.
We partially agree with the commenter. We agree with the request to incorporate best design practices for repairs to the fuselage, because mandating an action with known obsolete information ultimately requires additional work for the industry. However, we disagree with including a Boeing Communication as part of the AD, because multiple sources of AD-mandated instructions can increase the potential for misinterpretation and non-compliance. In addition, since the time the comments were made, the commenter (the airplane manufacturer) has revised the repair information in the service bulletin to include the information in Boeing Communication System Activity 1-VN5QD. We have included this revision of the service bulletin (Boeing Special Attention Service Bulletin 737-53-1234, Revision 1, dated March 31, 2005) in the final rule as the appropriate source of service information for accomplishing the AD actions. Revision 1 adds no further work to the original issue of the service bulletin, but incorporates the information in Boeing Communication System Activity 1-VN5QD. The final rule mandates the revised service bulletin. We have also added a new paragraph (l) to the final rule, which allows credit for actions done in accordance with the original issue of the service bulletin. We have re-identified subsequent paragraphs accordingly.
The same commenter requests that we fix the typographical error “appropriateaction” in paragraph (j) of the proposed AD.
We have changed paragraph (j) of the final rule to read “appropriate action” instead of “appropriateaction.”
We have revised paragraph (j) of the final rule to allow any crack in the subject area to be repaired according to data that conform to the airplane's type certificate and that are approved by an Authorized Representative for the Boeing Delegation Option Authorization Organization whom we have authorized to make such findings.
We have revised paragraphs (i)(1), (i)(2)(i), and (i)(2)(ii) of the final rule to remove references to the notes in Part 2 and Part 3 of the Work Instructions in the original issue of the service bulletin. The notes are no longer in those parts of Revision 1 of the service bulletin. The information in the referenced notes is still required by this AD, but in Revision 1 of the service bulletin this information has been incorporated into the procedures of Part 2 and Part 3.
(3) Will not have a significant economic impact, positive or negative, on a substantial number of small entities Start Printed Page 36823under the criteria of the Regulatory Flexibility Act.
2005-13-27 Boeing: Amendment 39-14164. Docket No. FAA-2004-19533; Directorate Identifier 2004-NM-31-AD.
(a) This AD becomes effective August 1, 2005.
(c) This AD applies to Boeing Model 737-300, -400, and -500 series airplanes, certificated in any category; as identified in Boeing Special Attention Service Bulletin 737-53-1234, Revision 1, dated March 31, 2005.
(d) This AD was prompted by a Model 737 fuselage structure test and fatigue analysis that indicate fuselage skin cracking could occur between 21,000 and 42,000 total flight cycles. We are issuing this AD to detect and correct fatigue cracking of the fuselage skin, which could cause the fuselage skin to fracture and fail, and could result in rapid decompression of the airplane.
(f) The term “service bulletin,” as used in this AD, means Boeing Special Attention Service Bulletin 737-53-1234, Revision 1, dated March 31, 2005.
(i) If any cracking is found during any inspection required by paragraph (g) or (h) of this AD, do the actions specified in paragraph (i)(1) or (i)(2) of this AD in accordance with the service bulletin, except as provided by paragraphs (j) and (k) of this AD.
(1) Before further flight, do a permanent repair (including related investigative actions and applicable corrective actions) in accordance with Part 2 of the Work Instructions of the service bulletin. Doing a permanent repair ends the repetitive inspections required by paragraph (h) of this AD for the repaired area only.
(i) Before further flight, do a time-limited repair (including related investigative actions and applicable corrective actions) in accordance with Part 3 of the Work Instructions of the service bulletin.
(ii) At the times specified in Figure 8 of the service bulletin, do the related investigative and corrective actions in accordance with Part 3 of the Work Instructions of the service bulletin.
(j) Where the service bulletin specifies to contact Boeing for appropriate action: Before further flight, repair according to a method approved by the Manager, Seattle Aircraft Certification Office (ACO), FAA; or according to data meeting the certification basis of the airplane approved by an Authorized Representative for the Boeing Delegation Option Authorization Organization who has been authorized by the Manager, Seattle ACO, to make those findings. For a repair method to be approved, the approval must specifically reference this AD.
(l) Actions done before the effective date of this AD in accordance with Boeing Special Attention Service Bulletin 737-53-1234, dated June 13, 2002, are acceptable for compliance with the corresponding actions required by this AD.
(m) The Manager, Seattle ACO, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19.
(n) You must use Boeing Special Attention Service Bulletin 737-53-1234, Revision 1, dated March 31, 2005, to perform the actions that are required by this AD, unless the AD specifies otherwise. The Director of the Federal Register approves the incorporation by reference of this document in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. To get copies of the service information, contact Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124-2207. To view the AD docket, go to the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street SW., room PL-401, Nassif Building, Washington, DC. To review copies of the service information, go to the National Archives and Records Administration (NARA). For information on the availability of this material at the NARA, call (202) 741-6030, or go to http://www.archives.gov/​federal_​register/​code_​of_​federal_​regulations/​ibr_​locations.html.
[FR Doc. 05-12514 Filed 6-24-05; 8:45 am]