Airworthiness Directives: McDonnell Douglas Corporation Model DC 10 10 and DC 10 10F Airplanes, et al.
Federal Register: November 25, 2009 (Volume 74, Number 226)
Rules and Regulations
Page 61504-61506
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
DOCID:fr25no09-2
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 39
Docket No. FAA-2009-1071; Directorate Identifier 2009-NM-160-AD;
Amendment 39-16100; AD 2008-06-21 R1
RIN 2120-AA64
Airworthiness Directives; McDonnell Douglas Corporation Model DC- 10-10 and DC-10-10F Airplanes, Model DC-10-15 Airplanes, Model DC-10-30 and DC-10-30F (KC-10A and KDC-10) Airplanes, Model DC-10-40 and DC-10- 40F Airplanes, Model MD-10-10F and MD-10-30F Airplanes, and Model MD-11 and MD-11F Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for comments.
SUMMARY: The FAA is revising an existing airworthiness directive (AD), which applies to all McDonnell Douglas Corporation airplane models identified above. That AD currently requires revising the FAA-approved maintenance program, or the Airworthiness Limitations (AWLs) section of the Instructions for Continued Airworthiness, as applicable, to incorporate new AWLs for fuel tank systems to satisfy Special Federal
Aviation Regulation No. 88 requirements. For certain airplanes, this AD also requires the initial accomplishment of a certain repetitive AWL inspection to phase in that inspection, and repair if necessary. This
AD clarifies the intended effect of the AD on spare and on-airplane fuel tank system components. This AD results from a design review of the fuel tank system. We are issuing this AD to prevent the potential for ignition sources inside fuel tanks caused by latent failures, alterations, repairs, or maintenance actions, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane.
DATES: This AD is effective December 10, 2009.
On April 23, 2008 (73 FR 14673, March 19, 2008), the Director of the Federal Register approved the incorporation by reference of a certain publication listed in the AD.
We must receive any comments on this AD by January 25, 2010.
ADDRESSES: You may send comments by any of the following methods:
Federal eRulemaking Portal: Go to http:// www.regulations.gov. Follow the instructions for submitting comments.
Fax: 202-493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue, SE., Washington, DC 20590.
Hand Delivery: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue, SE., Washington, DC 20590, between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.
For service information identified in this AD, contact Boeing
Commercial Airplanes, Attention: Data & Services Management, 3855
Lakewood Boulevard, MC D800 0019, Long Beach, California 90846-0001; telephone 206-544-5000, extension 2; fax 206-766-5683; e-mail dse.boecom@boeing.com; Internet https://www.myboeingfleet.com.
Examining the AD Docket
You may examine the AD docket on the Internet at http:// 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 street address for the Docket Office (telephone 800-647-5527) is in the ADDRESSES section.
Comments will be available in the AD docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT: Philip C. Kush, Aerospace Engineer,
Propulsion Branch, ANM-140L, Los Angeles Aircraft Certification Office,
FAA, 3960 Paramount Boulevard, Lakewood, California 90712-4137; telephone (562) 627-5263; fax (562) 627-5210.
SUPPLEMENTARY INFORMATION:
Discussion
On March 9, 2008, we issued AD 2008-06-21, Amendment 39-15433 (73
FR 14673, March 19, 2008). That AD applied to all McDonnell Douglas
Model DC-10-10 and DC-10-10F airplanes, Model DC-10-15 airplanes, Model
DC-10-30 and DC-10-30F (KC-10A and KDC-10) airplanes, Model DC-10-40 and DC-10-40F airplanes, Model MD-10-10F and MD-10-30F airplanes, and
Model MD-11 and MD-11F airplanes. That AD required revising the FAA- approved maintenance program, or the Airworthiness Limitations (AWLs) section of the Instructions for Continued Airworthiness, as applicable, to incorporate new AWLs for fuel tank systems to satisfy Special
Federal Aviation Regulation No. 88 requirements. For certain airplanes, that AD also required the initial accomplishment of a certain repetitive AWL inspection to phase in that inspection, and repair if necessary. That AD resulted from a design review of the fuel tank systems. The actions specified in that AD are intended to prevent the potential for ignition sources inside fuel tanks caused by latent failures, alterations, repairs, or maintenance actions, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane.
Critical design configuration control limitations (CDCCLs) are limitation requirements to preserve a critical ignition source prevention feature of the fuel tank system design that is necessary to prevent the occurrence of an unsafe condition. The purpose of a CDCCL is to provide instruction to retain the critical ignition source prevention feature during configuration change that may be caused by alterations, repairs, or maintenance actions. A CDCCL is not a periodic inspection.
Actions Since AD Was Issued
Since we issued that AD, we have determined that it is necessary to clarify the AD's intended effect on spare and
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on-airplane fuel tank system components, regarding the use of maintenance manuals and instructions for continued airworthiness.
Section 91.403(c) of the Federal Aviation Regulations (14 CFR 91.403(c)) specifies the following:
No person may operate an aircraft for which a manufacturer's maintenance manual or instructions for continued airworthiness has been issued that contains an airworthiness limitation section unless the mandatory * * * procedures * * * have been complied with.
Some operators have questioned whether existing components affected by the new CDCCLs must be reworked. We did not intend for the AD to retroactively require rework of components that had been maintained using acceptable methods before the effective date of the AD. Owners and operators of the affected airplanes therefore are not required to rework affected components identified as airworthy or installed on the affected airplanes before the required revisions of the FAA-approved maintenance program, or the AWLs section, as applicable. But once the
CDCCLs are incorporated into the FAA-approved maintenance program or the AWLs section, as applicable, future maintenance actions on components must be done in accordance with those CDCCLs.
FAA's Determination and Requirements of This AD
The unsafe condition described previously is likely to exist or develop on other airplanes of the same type design. For this reason, we are issuing this AD to revise AD 2008-06-21. This new AD retains the requirements of the existing AD, and adds a new note to clarify the intended effect of the AD on spare and on-airplane fuel tank system components.
Explanation of Additional Change to AD
AD 2008-06-21 allowed the use of later revisions of Appendixes B,
C, and D of Report MDC-02K1003. That provision has been removed from this AD. Allowing the use of ``a later revision'' of specific service documents violates Office of the Federal Register policies for approving materials that are incorporated by reference. Affected operators, however, may request approval to use an alternative CDCCL that is part of a later revision of the referenced service documents as an alternative method of compliance, under the provisions of paragraph
(l) of this AD.
Costs of Compliance
This revision imposes no additional economic burden. The current costs for this AD are repeated for the convenience of affected operators, as follows:
There are about 300 airplanes of the affected design in the worldwide fleet. This AD affects about 180 airplanes of U.S. registry.
The required actions take about 1 work hour per airplane, at an average labor rate of $80 per work hour. Based on these figures, the estimated cost of the AD for U.S. operators is $14,400, or $80 per airplane.
FAA's Justification and Determination of the Effective Date
This revision merely clarifies the intended effect on spare and on- airplane fuel tank system components, and makes no substantive change to the AD's requirements. For this reason, it is found that notice and opportunity for prior public comment for this action are unnecessary, and good cause exists for making this amendment effective in less than 30 days.
Comments Invited
This AD is a final rule that involves requirements affecting flight safety, and we did not provide you with notice and an opportunity to provide your comments before it becomes effective. However, we invite you to send any written data, views, or arguments about this AD. Send your comments to an address listed under the ADDRESSES section. Include
``Docket No. FAA-2009-1071; Directorate Identifier 2009-NM-160-AD'' at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this
AD. We will consider all comments received by the closing date and may amend this AD because of those comments.
We will post all comments we receive, without change, to http:// www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this AD.
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
We have determined that 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 the regulation: 1. Is not a ``significant regulatory action'' under Executive Order 12866; 2. Is not a ``significant rule'' under the 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.
We prepared a regulatory evaluation of the estimated costs to comply with this AD and placed it in the AD docket. See the ADDRESSES section for a location to examine the regulatory evaluation.
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 part 39 of the Federal Aviation Regulations (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 removing Amendment 39-15433 (73 FR 14673, March 19, 2008) and adding the following new AD: 2008-06-21 R1 McDonnell Douglas Corporation: Amendment 39-16100.
Docket No. FAA-2009-1071; Directorate Identifier 2009-NM-160-AD.
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Effective Date
(a) This airworthiness directive (AD) is effective December 10, 2009.
Affected ADs
(b) This AD revises AD 2008-06-21, Amendment 39-15433.
Applicability
(c) This AD applies to all McDonnell Douglas Corporation Model
DC-10-10 and DC-10-10F airplanes, Model DC-10-15 airplanes, Model
DC-10-30 and DC-10-30F (KC-10A and KDC-10) airplanes, Model DC-10-40 and DC-10-40F airplanes, Model MD-10-10F and MD-10-30F airplanes, and Model MD-11 and MD-11F airplanes; certificated in any category.
Note 1: This AD requires revisions to certain operator maintenance documents to include new inspections. Compliance with these inspections is required by 14 CFR 91.403(c). For airplanes that have been previously modified, altered, or repaired in the areas addressed by these inspections, the operator may not be able to accomplish the inspections described in the revisions. In this situation, to comply with 14 CFR 91.403(c), the operator must request approval for an alternative method of compliance (AMOC) in accordance with paragraph (l) of this AD. The request should include a description of changes to the required inspections that will ensure the continued operational safety of the airplane.
Unsafe Condition
(d) This AD results from a design review of the fuel tank systems. We are issuing this AD to prevent the potential for ignition sources inside fuel tanks caused by latent failures, alterations, repairs, or maintenance actions, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane.
Compliance
(e) You are responsible for having the actions required by this
AD performed within the compliance times specified, unless the actions have already been done.
Service Information Reference
(f) The term ``Report MDC-02K1003'' as used in this AD, means the Boeing Trijet Special Compliance Item Report, MDC-02K1003,
Revision C, dated July 24, 2007.
Restatement of Requirements of AD 2008-06-21, With Changes to
Compliance Method
Revise the FAA-Approved Maintenance Program
(g) For Model DC-10-10 and DC-10-10F airplanes, Model DC-10-15 airplanes, Model DC-10-30 and DC-10-30F (KC-10A and KDC-10) airplanes, and Model DC-10-40 and DC-10-40F airplanes: Before
December 16, 2008, revise the FAA-approved maintenance program to incorporate the information specified in Appendixes B, C, and D of
Report MDC-02K1003.
Revise the Airworthiness Limitations (AWLs) Section
(h) For Model MD-10-10F and MD-10-30F airplanes, and Model MD-11 and MD-11F airplanes: Before December 16, 2008, revise the AWLs section of the Instructions for Continued Airworthiness to incorporate the information specified in Appendixes B, C, and D of
Report MDC-02K1003, except that the initial inspection required by paragraph (i) of this AD must be done at the applicable compliance time specified in that paragraph.
Initial Inspection and Repair if Necessary
(i) For Model MD-11 and MD-11F airplanes: Within 60 months after
April 23, 2008 (the effective date AD 2008-06-21), do a detailed inspection of the metallic overbraiding and red-wrap tape installed on the tail tank fuel quantity indication system (FQIS) wiring to verify if the metallic overbraiding or red-wrap tape is damaged or shows signs of deterioration, in accordance with ALI 20-2 of
Appendix C of Report MDC-02K1003. If any discrepancy is found during the inspection, repair the discrepancy before further flight in accordance with ALI 20-2 of Appendix C of Report MDC-02K1003.
Note 2 : For the purposes of this AD, a detailed inspection is:
``An intensive examination of a specific item, installation, or assembly to detect damage, failure, or irregularity. Available lighting is normally supplemented with a direct source of good lighting at an intensity deemed appropriate. Inspection aids such as mirror, magnifying lenses, etc., may be necessary. Surface cleaning and elaborate procedures may be required.''
No Reporting Requirement
(j) Although Report MDC-02K1003 specifies to submit certain information to the manufacturer, this AD does not require that action.
No Alternative Inspections, Inspection Intervals, or Critical Design
Configuration Control Limitations (CDCCLs)
(k) After accomplishing the applicable actions specified in paragraphs (g), (h), and (i) of this AD, no alternative inspections, inspection intervals, or CDCCLs may be used unless the inspections, intervals, or CDCCLs are approved as an AMOC in accordance with the procedures specified in paragraph (l) of this AD.
New Information
Explanation of CDCCL Requirements
Note 3: Notwithstanding any other maintenance or operational requirements, components that have been identified as airworthy or installed on the affected airplanes before the revision of the FAA- approved maintenance program, or the AWLs section, as required by paragraphs (g) and (h) of this AD, do not need to be reworked in accordance with the CDCCLs. However, once the FAA-approved maintenance program, or the AWLs section, as applicable, has been revised, future maintenance actions on these components must be done in accordance with the CDCCLs.
Alternative Methods of Compliance (AMOCs)
(l)(1) The Manager, Los Angeles Aircraft Certification Office
(ACO), FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Philip C. Kush, Aerospace Engineer, Propulsion
Branch, ANM-140L, FAA, Los Angeles ACO, 3960 Paramount Boulevard,
Lakewood, California 90712-4137; telephone (562) 627-5263; fax (562) 627-5210.
(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 principal maintenance inspector (PMI) or principal avionics inspector (PAI), as appropriate, or lacking a principal inspector, your local Flight Standards District Office.
The AMOC approval letter must specifically reference this AD.
(3) AMOCs approved previously in accordance with AD 2008-06-21,
Amendment 39-15433, are approved as AMOCs for the corresponding provisions of this AD.
Material Incorporated by Reference
(m) You must use Boeing Trijet Special Compliance Item Report,
MDC-02K1003, Revision C, dated July 24, 2007, to do the actions required by this AD, unless the AD specifies otherwise.
(1) The Director of the Federal Register previously approved the incorporation by reference of Boeing Trijet Special Compliance Item
Report, MDC-02K1003, Revision C, dated July 24, 2007, on April 23, 2008 (73 FR 14673, March 19, 2008).
(2) For service information identified in this AD, contact
Boeing Commercial Airplanes, Attention: Data & Services Management, 3855 Lakewood Boulevard, MC D800 0019, Long Beach, California 90846- 0001; telephone 206-544-5000, extension 2; fax 206-766-5683; e-mail dse.boecom@boeing.com; Internet https://www.myboeingfleet.com.
(3) You may review copies of the service information at the FAA,
Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton,
Washington. For information on the availability of this material at the FAA, call 425-227-1221 or 425-227-1152.
(4) You may also review copies of the service information that is incorporated by reference 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: http:// www.archives.gov/federal_register/code_of_federal_regulations/ ibr_locations.html.
Issued in Renton, Washington, on November 12, 2009.
Stephen P. Boyd,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
FR Doc. E9-28163 Filed 11-24-09; 8:45 am
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