Airworthiness Directives: Bombardier Model DHC-8-102, DHC-8-103, DHC-8-106, et al., Airplanes
Federal Register: November 25, 2009 (Volume 74, Number 226)
Rules and Regulations
Page 61501-61504
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
DOCID:fr25no09-1
Rules and Regulations
Federal Register
This section of the FEDERAL REGISTER contains regulatory documents having general applicability and legal effect, most of which are keyed to and codified in the Code of Federal Regulations, which is published under 50 titles pursuant to 44 U.S.C. 1510.
The Code of Federal Regulations is sold by the Superintendent of Documents.
Prices of new books are listed in the first FEDERAL REGISTER issue of each week.
Page 61501
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 39
Docket No. FAA-2009-1072; Directorate Identifier 2009-NM-169-AD;
Amendment 39-16099; AD 2008-09-25 R1
RIN 2120-AA64
Airworthiness Directives; Bombardier Model DHC-8-102, DHC-8-103,
DHC-8-106, DHC-8-201, DHC-8-202, DHC-8-301, DHC-8-311, and DHC-8-315
Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for comments.
SUMMARY: We are adopting a new airworthiness directive (AD) for the products listed above that would revise an existing AD. This AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Bombardier Aerospace has completed a system safety review of the aircraft fuel system against fuel tank safety standards introduced in Chapter 525 of the Airworthiness Manual through Notice of
Proposed Amendment (NPA) 2002-043. The identified non-compliances were then assessed using Transport Canada Policy Letter No. 525-001, to determine if mandatory corrective action is required.
The assessment showed that it is necessary to introduce Critical
Design Configuration Control Limitations (CDCCL), in order to preserve critical fuel tank system ignition source prevention features during configuration changes such as modifications and repairs, or during maintenance actions. Failure to preserve critical fuel tank system ignition source prevention features could result in a fuel tank explosion. * * *
This AD requires actions that are intended to address the unsafe condition described in the MCAI.
DATES: This AD becomes effective December 10, 2009.
On June 6, 2008 (73 FR 24157, May 2, 2008), the Director of the
Federal Register approved the incorporation by reference of certain publications listed in the AD.
We must receive comments on this AD by January 11, 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 W12-40, 1200 New
Jersey Avenue, SE., Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays.
For service information identified in this AD, contact Bombardier,
Inc., 400 C[ocirc]te-Vertu Road West, Dorval, Qu[eacute]bec H4S 1Y9,
Canada; telephone 514-855-5000; fax 514-855-7401; e-mail thd.qseries@aero.bombardier.com; Internet http://www.bombardier.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 Operations office 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 Operations 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: Mazdak Hobbi, Aerospace Engineer,
Airframe and Mechanical Systems Branch, ANE-171, FAA, New York Aircraft
Certification Office, 1600 Stewart Avenue, Suite 410, Westbury, New
York 11590; telephone (516) 228-7330; fax (516) 794-5531.
SUPPLEMENTARY INFORMATION:
Discussion
On April 24, 2008, we issued AD 2008-09-25, Amendment 39-15506 (73
FR 24157, May 2, 2008). That AD applied to all Bombardier Model DHC-8- 102, DHC-8-103, DHC-8-106, DHC-8-201, DHC-8-202, DHC-8-301, DHC-8-311, and DHC-8-315 airplanes. That AD required revising the Airworthiness
Limitations section (ALS) of the Instructions for Continued
Airworthiness to incorporate the critical design configuration control limitations (CDCCL) data specified in the applicable temporary revision
(TR) to the applicable maintenance program manual (MPM).
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.
Since we issued that AD, we have determined that it is necessary to clarify the AD's intended effect on spare and 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 ALS. But once the CDCCLs are incorporated into the ALS, future maintenance actions on components
Page 61502
must be done in accordance with those CDCCLs.
FAA's Determination
This product has been approved by the aviation authority of another country, and is approved for operation in the United States. 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 2008-09-25 allowed the use of later revisions of the ALS. 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 a later revision of the referenced service documents as an alternative method of compliance, under the provisions of paragraph (g)(1) of this
AD.
Differences Between the AD and the MCAI or Service Information
We have reviewed the MCAI and related service information and, in general, agree with their substance. But we might have found it necessary to use different words from those in the MCAI to ensure the
AD is clear for U.S. operators and is enforceable. In making these changes, we do not intend to differ substantively from the information provided in the MCAI and related service information.
We might also have required different actions in this AD from those in the MCAI in order to follow FAA policies. Any such differences are highlighted in a Note within the 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:
We estimate that this AD will affect about 118 products of U.S. registry. We also estimate that it will take about 1 work-hour per product to comply with the basic requirements of this AD. The average labor rate is $80 per work-hour. Based on these figures, we estimate the cost of this AD to the U.S. operators to be $9,440, or $80 per product.
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 precede it by notice and opportunity for public comment. We invite you to send any written relevant data, views, or arguments about this AD. Send your comments to an address listed under the ADDRESSES section. Include ``Docket No. FAA-2009-1072; Directorate
Identifier 2009-NM-169-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 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 this AD: 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.
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 removing amendment 39-15506 (73 FR 24157, May 2, 2008) and adding the following new AD: 2008-09-25 R1 Bombardier, Inc. (Formerly de Havilland, Inc.):
Amendment 39-16099. Docket No. FAA-2009-1072; Directorate Identifier 2009-NM-169-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective December 10, 2009.
Affected ADs
(b) This AD revises AD 2008-09-25, Amendment 39-15506.
Applicability
(c) This AD applies to all Bombardier Model DHC-8-102, DHC-8- 103, DHC-8-106, DHC-8-201, DHC-8-202, DHC-8-301, DHC-8-311, and DHC- 8-315 airplanes, certificated in any category, all serial numbers.
Subject
(d) Air Transport Association (ATA) of America Code 28: Fuel.
Page 61503
Reason
(e) The mandatory continuing airworthiness information (MCAI) states:
Bombardier Aerospace has completed a system safety review of the aircraft fuel system against fuel tank safety standards introduced in Chapter 525 of the Airworthiness Manual through Notice of
Proposed Amendment (NPA) 2002-043. The identified non-compliances were then assessed using Transport Canada Policy Letter No. 525-001, to determine if mandatory corrective action is required.
The assessment showed that it is necessary to introduce Critical
Design Configuration Control Limitations (CDCCL), in order to preserve critical fuel tank system ignition source prevention features during configuration changes such as modifications and repairs, or during maintenance actions. Failure to preserve critical fuel tank system ignition source prevention features could result in a fuel tank explosion. Revisions have been made to Part 2
``Airworthiness Limitations List'' of the Maintenance Program
Manuals of the affected aircraft models to introduce the required
CDCCL.
The corrective action is revising the Airworthiness Limitations section of the Instructions for Continued Airworthiness to include the CDCCL data.
Restatement of AD 2008-09-25, With Revised Compliance Method
Actions and Compliance
(f) Unless already done, do the following actions.
(1) For all airplanes: Within 60 days after June 6, 2008 (the effective date of AD 2008-09-25), revise the Airworthiness
Limitations section of the Instructions for Continued Airworthiness to incorporate the CDCCL data specified in the applicable temporary revision (TR) to the applicable maintenance program manual (MPM).
The TRs are listed in Table 1 of this AD.
Table 1--Temporary Revisions
Model
de Havilland TR
Maintenance program manual
DHC-8-102, DHC-8-103, and DHC-8-106
AWL-98, dated April 12,
Part 2, ``Airworthiness Limitations airplanes.
2006.
List,'' of de Havilland Dash 8 Series 100 MPM, Product Support Manual (PSM) 1- 8-7.
DHC-8-201, and DHC-8-202 airplanes...... AWL 2-35, dated April 12,
Part 2, ``Airworthiness Limitations 2006.
List,'' of de Havilland Dash 8 Series 200 MPM, PSM 1-82-7.
DHC-8-301, DHC-8[dash]311, and DHC-8-315 AWL 3-103, dated April 12, Part 2, ``Airworthiness Limitations airplanes.
2006.
List,'' of de Havilland Dash 8 Series 300 MPM, PSM 1-83-7.
Note 1: The revisions required by paragraph (f)(1) of this AD may be done by inserting a copy of the applicable TR into the applicable maintenance program manual. When the TR has been included in the general revision of the maintenance program, the general revision may be inserted into the maintenance program manual, provided the relevant information in the general revision is identical to that in the applicable TR, and the temporary revision may be removed.
(2) After accomplishing the actions specified in paragraph
(f)(1) of this AD, no alternative CDCCLs may be used unless the
CDCCLs are approved as an alternative method of compliance (AMOC) in accordance with the procedures specified in paragraph (g)(1) of this
AD.
New Information
Explanation of CDCCL Requirements
Note 2: 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 ALS, as required by paragraph (f)(1) of this AD, do not need to be reworked in accordance with the CDCCLs. However, once the ALS has been revised, future maintenance actions on these components must be done in accordance with the CDCCLs.
FAA AD Differences
Note 3: This AD differs from the MCAI and/or service information as follows: No differences.
Other FAA AD Provisions
(g) The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, New
York Aircraft Certification Office, 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: Mazdak Hobbi, Aerospace
Engineer, Airframe and Mechanical Systems Branch, ANE-171, FAA, New
York Aircraft Certification Office, 1600 Stewart Avenue, Suite 410,
Westbury, New York 11590; telephone (516) 228-7330; fax (516) 794- 5531. 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.
(2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered
FAA-approved if they are approved by the State of Design Authority
(or their delegated agent). You are required to assure the product is airworthy before it is returned to service.
(3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act (44
U.S.C. 3501 et seq.), the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned
OMB Control Number 2120-0056.
Related Information
(h) Refer to MCAI Canadian Airworthiness Directive CF-2008-03, dated January 3, 2008, and the TRs specified in Table 1 of this AD, for related information.
Material Incorporated by Reference
(i) You must use the service information contained in Table 2 of this AD to do the actions required by this AD, unless the AD specifies otherwise.
Table 2--Material Incorporated by Reference
de Havilland temporary revision--
Dated--
To--
AWL-98.................................. April 12, 2006............. Part 2, ``Airworthiness Limitations
List,'' of de Havilland Dash 8 Series 100 Maintenance Program Manual, Product
Support Manual 1-8-7.
AWL 2-35................................ April 12, 2006............. Part 2, ``Airworthiness Limitations
List,'' of de Havilland Dash 8 Series 200 Maintenance Program Manual, Product
Support Manual 1-82-7.
AWL 3-103............................... April 12, 2006............. Part 2, ``Airworthiness Limitations
List,'' of de Havilland Dash 8 Series 300 Maintenance Program Manual, Product
Support Manual 1-83-7.
Page 61504
(1) The Director of the Federal Register previously approved the incorporation by reference of this service information on June 6, 2008 (73 FR 24157, May 2, 2008).
(2) For service information identified in this AD, contact
Bombardier, Inc., 400 C[ocirc]te-Vertu Road West, Dorval,
Qu[eacute]bec H4S 1Y9, Canada; telephone 514-855-5000; fax 514-855- 7401; e-mail thd.qseries@aero.bombardier.com; Internet http:// www.bombardier.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 16, 2009.
Stephen P. Boyd,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
FR Doc. E9-28161 Filed 11-24-09; 8:45 am
BILLING CODE 4910-13-P
