Airworthiness Directives; Boeing Model 707 Airplanes, and Model 720 and 720B Series Airplanes, 50703-50705 [E8-19136]

Download as PDF Federal Register / Vol. 73, No. 168 / Thursday, August 28, 2008 / Rules and Regulations agencies, in general, to provide the public the option of communicating electronically with the government to the maximum extent possible. The Agency will ensure that all forms used by the establishments are made available electronically. Additional Public Notification Public awareness of all segments of rulemaking and policy development is important. Consequently, in an effort to ensure that minorities, women, and persons with disabilities are aware of this final rule, FSIS will announce it online through the FSIS Web page located at https://www.fsis.usda.gov/ Regulations_&_Policies/2008_Interim_& _Final_Rules_Index/index.asp. FSIS will also make copies of this Federal Register publication available through the FSIS Constituent Update, which is used to provide information regarding FSIS policies, procedures, regulations, Federal Register notices, FSIS public meetings, and other types of information that could affect or would be of interest to constituents and stakeholders. The Update is communicated via Listserv, a free electronic mail subscription service for industry, trade groups, consumer interest groups, health professionals, and other individuals who have asked to be included. The Update is also available on the FSIS Web page. Through the Listserv and Web page, FSIS is able to provide information to a much broader and more diverse audience. In addition, FSIS offers an email subscription service which provides automatic and customized access to selected food safety news and information. This service is available at https://www.fsis.usda.gov/news_and_ events/email_subscription/. Options range from recalls to export information to regulations, directives and notices. Customers can add or delete subscriptions themselves, and have the option to password protect their accounts. 9 CFR Part 317 Food labeling, Meat inspection. mstockstill on PROD1PC66 with RULES 9 CFR Part 381 Food labeling, Poultry and poultry products. I For the reasons discussed in the preamble, FSIS is amending 9 CFR Chapter III as follows: PART 317—LABELING, MARKING DEVICES, AND CONTAINERS 1. The authority citation for part 317 continues to read as follows: I 16:19 Aug 27, 2008 2. Section 317.5(b) is amended as follows: I a. In paragraph (b)(1) after ‘‘geographical origin claims’’ add the following parenthetical phrase: ‘‘(except as provided by paragraph (b)(9)(xxv) of this section),’’ I b. In paragraph (b)(2) after ‘‘geographical origin claims’’ add the following parenthetical phrase: ‘‘(except as provided by paragraph (b)(9)(xxv) of this section),’’ I c. A new paragraph (b)(9)(xxv) is added to read as follows: I § 317.5 Generically approved labeling. * * * * * (b) * * * (9) * * * (xxv) A country of origin statement on any product label described in § 317.8(b)(40) that complies with the requirements in that paragraph. I 3. In § 317.8, a new paragraph (b)(40) is added to read as follows: § 317.8 False or misleading labeling or practices generally; specific prohibitions and requirements for labels and containers. * * * * * (b) * * * (40) A country of origin statement on the label of any meat ‘‘covered commodity’’ as defined in 7 CFR Part 65, Subpart A, that is to be sold by a ‘‘retailer,’’ as defined in 7 CFR 65.240, must comply with the requirements in 7 CFR 65.300 and 65.400. PART 381—POULTRY PRODUCTS INSPECTION REGULATIONS 4. The authority citation for part 381 continues to read as follows: I Authority: 7 U.S.C. 138f, 450; 21 U.S.C. 451–470; 7 CFR 2.18, 2.53. 5. In § 381.129, a new paragraph (f) is added to read as follows: I § 381.129 False or misleading labeling or containers. * List of Subjects VerDate Aug<31>2005 Authority: 21 U.S.C. 601–695; 7 CFR 2.18, 2.53. Jkt 214001 * * * * (f) A country of origin statement on the label of any poultry product ‘‘covered commodity’’ as defined in 7 CFR Part 65, Subpart A, that is to be sold by a ‘‘retailer,’’ as defined in 7 CFR 65.240, must comply with the requirements in 7 CFR 65.300 and 65.400. I 6. § 381.133(b) is amended as follows: I a. In paragraph (b)(1) after ‘‘geographical origin claims’’ add the following parenthetical phrase: ‘‘(except as provided by paragraph (b)(9)(xxviii) of this section),’’ I b. In paragraph (b)(2) after ‘‘geographical origin claims’’ add the PO 00000 Frm 00003 Fmt 4700 Sfmt 4700 50703 following parenthetical phrase: ‘‘(except as provided by paragraph (b)(9)(xxviii) of this section),’’ I c. A new paragraph (b)(9)(xxviii) is added to read as follows: § 381.133 Generically approved labeling. * * * * * (b) * * * (9) * * * (xxviii) A country of origin statement on any product label described in § 381.129(f) that complies with the requirements in that paragraph. Done in Washington, DC, on August 22, 2008. Alfred V. Almanza, Administrator. [FR Doc. E8–19882 Filed 8–27–08; 8:45 am] BILLING CODE 3410–DM–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2008–0523; Directorate Identifier 2008–NM–049–AD; Amendment 39–15648; AD 2008–17–10] RIN 2120–AA64 Airworthiness Directives; Boeing Model 707 Airplanes, and Model 720 and 720B Series Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Final rule. AGENCY: SUMMARY: We are adopting a new airworthiness directive (AD) for certain Boeing Model 707 airplanes, and Model 720 and 720B series airplanes. This AD requires repetitive detailed inspections to detect cracks and corrosion on any existing repairs and at certain body stations of the visible surfaces of the wing to body terminal fittings including the web, flanges, and ribs; and applicable related investigative and corrective actions. This AD results from reports of cracks found in the wing to body terminal fittings during routine inspections. We are issuing this AD to prevent cracks and corrosion in the body terminal fittings, which could cause loss of support for the wing and could adversely affect the structural integrity of the airplane. DATES: This AD is effective October 2, 2008. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of October 2, 2008. ADDRESSES: For service information identified in this AD, contact Boeing E:\FR\FM\28AUR1.SGM 28AUR1 50704 Federal Register / Vol. 73, No. 168 / Thursday, August 28, 2008 / Rules and Regulations Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124–2207. Examining the AD Docket You may examine the AD docket on the Internet at https:// www.regulations.gov; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD, the regulatory evaluation, any comments received, and other information. The address for the Docket Office (telephone 800–647–5527) is the Document Management Facility, U.S. Department of Transportation, Docket Operations, M–30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue, SE., Washington, DC 20590. FOR FURTHER INFORMATION CONTACT: Berhane Alazar, Aerospace Engineer, Airframe Branch, ANM–120S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98057–3356; telephone (425) 917–6577; fax (425) 917–6590. SUPPLEMENTARY INFORMATION: Discussion We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to include an airworthiness directive (AD) that would apply to certain Boeing Model 707 airplanes, and Model 720 and 720B series airplanes. That NPRM was published in the Federal Register on May 8, 2008 (73 FR 26043). That NPRM proposed to require repetitive detailed inspections to detect cracks and corrosion on any existing repairs and at certain body stations of the visible surfaces of the wing to body terminal fittings including the web, flanges, and ribs; and applicable related investigative and corrective actions. Comments We gave the public the opportunity to participate in developing this AD. We received no comments on the NPRM or on the determination of the cost to the public. Conclusion We reviewed the relevant data and determined that air safety and the public interest require adopting the AD as proposed. Costs of Compliance We estimate that this AD affects 5 airplanes of U.S. registry. The following table provides the estimated costs for U.S. operators to comply with this AD. ESTIMATED COSTS Action Work hours Average labor rate per hour Cost per product Number of U.S.-registered airplanes Fleet cost Inspections ............................ 20 $80 $1,600, per inspection cycle 5 $8,000, per inspection cycle. mstockstill on PROD1PC66 with RULES Authority for This Rulemaking Title 49 of the United States Code specifies the FAA’s authority to issue rules on aviation safety. Subtitle I, section 106, describes the authority of the FAA Administrator. ‘‘Subtitle VII: Aviation Programs,’’ describes in more detail the scope of the Agency’s authority. We are issuing this rulemaking under the authority described in ‘‘Subtitle VII, Part A, Subpart III, Section 44701: General requirements.’’ Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. (1) Is not a ‘‘significant regulatory action’’ under Executive Order 12866, (2) Is not a ‘‘significant rule’’ under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979), and (3) Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. You can find our regulatory evaluation and the estimated costs of compliance in the AD Docket. Regulatory Findings This AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government. For the reasons discussed above, I certify that this AD: PART 39—AIRWORTHINESS DIRECTIVES VerDate Aug<31>2005 16:19 Aug 27, 2008 Jkt 214001 List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: I 1. The authority citation for part 39 continues to read as follows: I Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Amended] 2. The FAA amends § 39.13 by adding the following new AD: I 2008–17–10 Boeing: Amendment 39–15648. Docket No. FAA–2008–0523; Directorate Identifier 2008–NM–049–AD. PO 00000 Frm 00004 Fmt 4700 Sfmt 4700 Effective Date (a) This airworthiness directive (AD) is effective October 2, 2008. Affected ADs (b) None. Applicability (c) This AD applies to Model 707–100 long body, –200, –100B long body, and –100B short body series airplanes; Model 707–300, –300B, –300C, and –400 series airplanes; and Model 720 and 720B series airplanes, certificated in any category; as identified in Boeing 707 Special Attention Service Bulletin 3524, dated July 18, 2007. Unsafe Condition (d) This AD results from reports of cracks found in the wing to body terminal fittings during routine inspections. We are issuing this AD to prevent cracks and corrosion in the body terminal fittings, which could cause loss of support for the wing and could adversely affect the structural integrity of the airplane. Compliance (e) Comply with this AD within the compliance times specified, unless already done. Inspections and Corrective Actions (f) Within 24 months after the effective date of this AD, do detailed inspections and applicable related investigative and corrective actions, by accomplishing all the actions specified in the Accomplishment Instructions of Boeing 707 Special Attention Service Bulletin 3524, dated July 18, 2007, except as provided by paragraph (g) of this AD. Repeat the detailed inspections E:\FR\FM\28AUR1.SGM 28AUR1 Federal Register / Vol. 73, No. 168 / Thursday, August 28, 2008 / Rules and Regulations thereafter at intervals not to exceed 24 months. Do all applicable related investigative and corrective actions before further flight. (g) If any crack or corrosion is found during any inspection required by paragraph (f) of this AD, and Boeing 707 Special Attention Service Bulletin 3524, dated July 18, 2007, specifies to contact Boeing for appropriate action: Before further flight, repair the terminal fittings using a method approved in accordance with the procedures specified in paragraph (i) of this AD. No Information Submission (h) Although Boeing 707 Special Attention Service Bulletin 3524, dated July 18, 2007, specifies to submit information to the manufacturer, this AD does not include that requirement. mstockstill on PROD1PC66 with RULES Alternative Methods of Compliance (AMOCs) (i)(1) The Manager, Seattle Aircraft Certification Office (ACO), FAA, ATTN: Berhane Alazar, Aerospace Engineer, Airframe Branch, ANM–120S, 1601 Lind Avenue SW., Renton, Washington 98057– 3356; telephone (425) 917–6577; fax (425) 917–6590; has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. (2) To request a different method of compliance or a different compliance time for this AD, follow the procedures in 14 CFR 39.19. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO. (3) An AMOC that provides an acceptable level of safety may be used for any repair required by this AD, if it is approved by an Authorized Representative for the Boeing Commercial Airplanes 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 repair must meet the certification basis of the airplane, and the approval must specifically refer to this AD. Material Incorporated by Reference (j) You must use Boeing 707 Special Attention Service Bulletin 3524, dated July 18, 2007, to do the actions required by this AD, unless the AD specifies otherwise. (1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124–2207. (3) You may review copies of the service information incorporated by reference at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington; or at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202–741–6030, or go to: https:// www.archives.gov/federal_register/ code_of_federal_regulations/ ibr_locations.html. VerDate Aug<31>2005 16:19 Aug 27, 2008 Jkt 214001 Issued in Renton, Washington, on August 6, 2008. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E8–19136 Filed 8–27–08; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2007–0223; Directorate Identifier 2007–NM–156–AD; Amendment 39–15652; AD 2008–17–14] RIN 2120–AA64 Airworthiness Directives; Boeing Model 727 Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. AGENCY: The FAA is superseding an existing airworthiness directive (AD), which applies to certain Boeing Model 727 series airplanes. That AD currently requires repetitive inspections to detect cracks and loose brackets of the elevator rear spar, and corrective actions if necessary. The existing AD also provides for an optional terminating action for the repetitive inspections. This new AD reduces the repetitive intervals of the inspections, mandates the previously optional terminating action for the repetitive inspections, and no longer allows stop-drilling. This AD results from new reports of cracks, elongated fastener holes, and loose fittings of the elevator rear spar. We are issuing this AD to prevent cracking of the elevator rear spar at the tab hinge locations, which could cause excessive freeplay of the elevator control tab and possible tab flutter, and consequent loss of control of the airplane. DATES: This AD becomes effective October 2, 2008. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in the AD as of October 2, 2008. On April 22, 1996 (61 FR 11529, March 21, 1996), the Director of the Federal Register approved the incorporation by reference of Boeing Service Bulletin 727–55–0089, dated June 29, 1995. ADDRESSES: For service information identified in this AD, contact Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124–2207. SUMMARY: PO 00000 Frm 00005 Fmt 4700 Sfmt 4700 50705 Examining the AD Docket You may examine the AD docket on the Internet at https:// www.regulations.gov; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD, the regulatory evaluation, any comments received, and other information. The address for the Docket Office (telephone 800–647–5527) is the Document Management Facility, U.S. Department of Transportation, Docket Operations, M–30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue, SE., Washington, DC 20590. FOR FURTHER INFORMATION CONTACT: Berhane Alazar, Aerospace Engineer, Airframe Branch, ANM–120S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98057–3356; telephone (425) 917–6577; fax (425) 917–6590. SUPPLEMENTARY INFORMATION: Discussion The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to include an AD that supersedes AD 96–06–05, amendment 39–9542 (61 FR 11529, March 21, 1996). The existing AD applies to certain Boeing Model 727 series airplanes. That NPRM was published in the Federal Register on November 23, 2007 (72 FR 65678). That NPRM proposed to require repetitive inspections to detect cracks and loose brackets of the elevator rear spar, and corrective actions if necessary. The NPRM also proposed to reduce the repetitive intervals of the inspections, mandate the previously optional terminating action for the repetitive inspection, and no longer allow stopdrilling. Comments We provided the public the opportunity to participate in the development of this AD. We have considered the comments that have been received on the NPRM. Request To Extend Compliance Time for Terminating Action (Spar Replacement) Several commenters (Boeing, Champion Air, DHL, FedEx, and ReadyJetGo) request that we extend the compliance time (18 months) for the terminating action specified in the NPRM. Boeing, Champion Air, and ReadyJetGo request an extension from 18 months to 24 months; DHL requests 36 months; and FedEx requests 36 months or 3,600 flight hours, whichever E:\FR\FM\28AUR1.SGM 28AUR1

Agencies

[Federal Register Volume 73, Number 168 (Thursday, August 28, 2008)]
[Rules and Regulations]
[Pages 50703-50705]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E8-19136]


=======================================================================
-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2008-0523; Directorate Identifier 2008-NM-049-AD; 
Amendment 39-15648; AD 2008-17-10]
RIN 2120-AA64


Airworthiness Directives; Boeing Model 707 Airplanes, and Model 
720 and 720B Series Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: We are adopting a new airworthiness directive (AD) for certain 
Boeing Model 707 airplanes, and Model 720 and 720B series airplanes. 
This AD requires repetitive detailed inspections to detect cracks and 
corrosion on any existing repairs and at certain body stations of the 
visible surfaces of the wing to body terminal fittings including the 
web, flanges, and ribs; and applicable related investigative and 
corrective actions. This AD results from reports of cracks found in the 
wing to body terminal fittings during routine inspections. We are 
issuing this AD to prevent cracks and corrosion in the body terminal 
fittings, which could cause loss of support for the wing and could 
adversely affect the structural integrity of the airplane.

DATES: This AD is effective October 2, 2008.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of October 2, 
2008.

ADDRESSES: For service information identified in this AD, contact 
Boeing

[[Page 50704]]

Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124-2207.

Examining the AD Docket

    You may examine the AD docket on the Internet at https://
www.regulations.gov; or in person at the Docket Management Facility 
between 9 a.m. and 5 p.m., Monday through Friday, except Federal 
holidays. The AD docket contains this AD, the regulatory evaluation, 
any comments received, and other information. The address for the 
Docket Office (telephone 800-647-5527) is the Document Management 
Facility, U.S. Department of Transportation, Docket Operations, M-30, 
West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., 
Washington, DC 20590.

FOR FURTHER INFORMATION CONTACT: Berhane Alazar, Aerospace Engineer, 
Airframe Branch, ANM-120S, FAA, Seattle Aircraft Certification Office, 
1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425) 
917-6577; fax (425) 917-6590.

SUPPLEMENTARY INFORMATION:

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR 
part 39 to include an airworthiness directive (AD) that would apply to 
certain Boeing Model 707 airplanes, and Model 720 and 720B series 
airplanes. That NPRM was published in the Federal Register on May 8, 
2008 (73 FR 26043). That NPRM proposed to require repetitive detailed 
inspections to detect cracks and corrosion on any existing repairs and 
at certain body stations of the visible surfaces of the wing to body 
terminal fittings including the web, flanges, and ribs; and applicable 
related investigative and corrective actions.

Comments

    We gave the public the opportunity to participate in developing 
this AD. We received no comments on the NPRM or on the determination of 
the cost to the public.

Conclusion

    We reviewed the relevant data and determined that air safety and 
the public interest require adopting the AD as proposed.

Costs of Compliance

    We estimate that this AD affects 5 airplanes of U.S. registry. The 
following table provides the estimated costs for U.S. operators to 
comply with this AD.

                                                                     Estimated Costs
--------------------------------------------------------------------------------------------------------------------------------------------------------
                                                                                                           Number of U.S.-
                  Action                      Work hours     Average labor         Cost per product           registered             Fleet cost
                                                             rate per hour                                    airplanes
--------------------------------------------------------------------------------------------------------------------------------------------------------
Inspections..............................              20              $80   $1,600, per inspection cycle               5   $8,000, per inspection
                                                                                                                             cycle.
--------------------------------------------------------------------------------------------------------------------------------------------------------

Authority for This Rulemaking

    Title 49 of the United States Code specifies the FAA's authority to 
issue rules on aviation safety. Subtitle I, section 106, describes the 
authority of the FAA Administrator. ``Subtitle VII: Aviation 
Programs,'' describes in more detail the scope of the Agency's 
authority.
    We are issuing this rulemaking under the authority described in 
``Subtitle VII, Part A, Subpart III, Section 44701: General 
requirements.'' Under that section, Congress charges the FAA with 
promoting safe flight of civil aircraft in air commerce by prescribing 
regulations for practices, methods, and procedures the Administrator 
finds necessary for safety in air commerce. This regulation is within 
the scope of that authority because it addresses an unsafe condition 
that is likely to exist or develop on products identified in this 
rulemaking action.

Regulatory Findings

    This AD will not have federalism implications under Executive Order 
13132. This AD will not have a substantial direct effect on the States, 
on the relationship between the national government and the States, or 
on the distribution of power and responsibilities among the various 
levels of government.
    For the reasons discussed above, I certify that this AD:
    (1) Is not a ``significant regulatory action'' under Executive 
Order 12866,
    (2) Is not a ``significant rule'' under DOT Regulatory Policies and 
Procedures (44 FR 11034, February 26, 1979), and
    (3) Will not have a significant economic impact, positive or 
negative, on a substantial number of small entities under the criteria 
of the Regulatory Flexibility Act.
    You can find our regulatory evaluation and the estimated costs of 
compliance in the AD Docket.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by 
reference, Safety.

Adoption of the Amendment

0
Accordingly, under the authority delegated to me by the Administrator, 
the FAA amends 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:

    Authority: 49 U.S.C. 106(g), 40113, 44701.


Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by adding the following new AD:

2008-17-10 Boeing: Amendment 39-15648. Docket No. FAA-2008-0523; 
Directorate Identifier 2008-NM-049-AD.

Effective Date

    (a) This airworthiness directive (AD) is effective October 2, 
2008.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to Model 707-100 long body, -200, -100B long 
body, and -100B short body series airplanes; Model 707-300, -300B, -
300C, and -400 series airplanes; and Model 720 and 720B series 
airplanes, certificated in any category; as identified in Boeing 707 
Special Attention Service Bulletin 3524, dated July 18, 2007.

Unsafe Condition

    (d) This AD results from reports of cracks found in the wing to 
body terminal fittings during routine inspections. We are issuing 
this AD to prevent cracks and corrosion in the body terminal 
fittings, which could cause loss of support for the wing and could 
adversely affect the structural integrity of the airplane.

Compliance

    (e) Comply with this AD within the compliance times specified, 
unless already done.

Inspections and Corrective Actions

    (f) Within 24 months after the effective date of this AD, do 
detailed inspections and applicable related investigative and 
corrective actions, by accomplishing all the actions specified in 
the Accomplishment Instructions of Boeing 707 Special Attention 
Service Bulletin 3524, dated July 18, 2007, except as provided by 
paragraph (g) of this AD. Repeat the detailed inspections

[[Page 50705]]

thereafter at intervals not to exceed 24 months. Do all applicable 
related investigative and corrective actions before further flight.
    (g) If any crack or corrosion is found during any inspection 
required by paragraph (f) of this AD, and Boeing 707 Special 
Attention Service Bulletin 3524, dated July 18, 2007, specifies to 
contact Boeing for appropriate action: Before further flight, repair 
the terminal fittings using a method approved in accordance with the 
procedures specified in paragraph (i) of this AD.

No Information Submission

    (h) Although Boeing 707 Special Attention Service Bulletin 3524, 
dated July 18, 2007, specifies to submit information to the 
manufacturer, this AD does not include that requirement.

Alternative Methods of Compliance (AMOCs)

    (i)(1) The Manager, Seattle Aircraft Certification Office (ACO), 
FAA, ATTN: Berhane Alazar, Aerospace Engineer, Airframe Branch, ANM-
120S, 1601 Lind Avenue SW., Renton, Washington 98057-3356; telephone 
(425) 917-6577; fax (425) 917-6590; has the authority to approve 
AMOCs for this AD, if requested using the procedures found in 14 CFR 
39.19.
    (2) To request a different method of compliance or a different 
compliance time for this AD, follow the procedures in 14 CFR 39.19. 
Before using any approved AMOC on any airplane to which the AMOC 
applies, notify your appropriate principal inspector (PI) in the FAA 
Flight Standards District Office (FSDO), or lacking a PI, your local 
FSDO.
    (3) An AMOC that provides an acceptable level of safety may be 
used for any repair required by this AD, if it is approved by an 
Authorized Representative for the Boeing Commercial Airplanes 
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 repair must meet the certification basis 
of the airplane, and the approval must specifically refer to this 
AD.

Material Incorporated by Reference

    (j) You must use Boeing 707 Special Attention Service Bulletin 
3524, dated July 18, 2007, to do the actions required by this AD, 
unless the AD specifies otherwise.
    (1) The Director of the Federal Register approved the 
incorporation by reference of this service information under 5 
U.S.C. 552(a) and 1 CFR part 51.
    (2) For service information identified in this AD, contact 
Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 
98124-2207.
    (3) You may review copies of the service information 
incorporated by reference at the FAA, Transport Airplane 
Directorate, 1601 Lind Avenue SW., Renton, Washington; or at the 
National Archives and Records Administration (NARA). For information 
on the availability of this material at NARA, call 202-741-6030, or 
go to: https://www.archives.gov/federal_register/code_of_federal_
regulations/ibr_locations.html.

    Issued in Renton, Washington, on August 6, 2008.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. E8-19136 Filed 8-27-08; 8:45 am]
BILLING CODE 4910-13-P

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