

[Federal Register: February 19, 2008 (Volume 73, Number 33)]
[Proposed Rules]               
[Page 9055-9058]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr19fe08-12]                         

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2008-0179; Directorate Identifier 2007-NM-367-AD]
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), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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SUMMARY: We propose to adopt a new airworthiness directive (AD) for the 
products listed above. This proposed 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 * * *.
    [A]ssessment showed that supplemental maintenance tasks 
[inspections of fuel tank bonding jumpers, wiring harnesses, and 
drain valve components, among other items and actions; and 
applicable corrective actions] are required to prevent potential 
ignition sources inside the fuel system, which could result in a 
fuel tank explosion. * * *

    The proposed AD would require actions that are intended to address 
the unsafe condition described in the MCAI.

DATES: We must receive comments on this proposed AD by March 20, 2008.

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.


[[Page 9056]]

     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.

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 proposed 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: Rocco Viselli, Aerospace Engineer, 
Airframe and Propulsion Branch, ANE-171, FAA, New York Aircraft 
Certification Office, 1600 Stewart Avenue, Suite 410, Westbury, New 
York 11590; telephone (516) 228-7331; fax (516) 794-5531.

SUPPLEMENTARY INFORMATION: 

Comments Invited

    We invite you to send any written relevant data, views, or 
arguments about this proposed AD. Send your comments to an address 
listed under the ADDRESSES section. Include ``Docket No. FAA-2008-0179; 
Directorate Identifier 2007-NM-367-AD'' at the beginning of your 
comments. We specifically invite comments on the overall regulatory, 
economic, environmental, and energy aspects of this proposed AD. We 
will consider all comments received by the closing date and may amend 
this proposed AD based on 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 proposed AD.

Discussion

    Transport Canada Civil Aviation (TCCA), which is the aviation 
authority for Canada, has issued Canadian Airworthiness Directive CF-
2007-32, dated December 17, 2007 (referred to after this as ``the 
MCAI''), to correct an unsafe condition for the specified products. The 
MCAI states:

    Bombardier Aerospace has completed a system safety review of the 
aircraft fuel system against fuel tank 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 supplemental maintenance tasks 
[inspections of fuel tank bonding jumpers, wiring harnesses, and 
drain valve components, among other items and actions; and 
applicable corrective actions] are required to prevent potential 
ignition sources inside the fuel system, which could result in a 
fuel tank explosion. Revisions have been made to Part 2 
``Airworthiness Limitations List'' of the DHC-8 Maintenance Program 
Manuals to introduce the required maintenance tasks.

The corrective action is revising the Airworthiness Limitations Section 
of the Instructions for Continued Airworthiness to incorporate new 
limitations for fuel tank systems. You may obtain further information 
by examining the MCAI in the AD docket.
    The FAA has examined the underlying safety issues involved in fuel 
tank explosions on several large transport airplanes, including the 
adequacy of existing regulations, the service history of airplanes 
subject to those regulations, and existing maintenance practices for 
fuel tank systems. As a result of those findings, we issued a 
regulation titled ``Transport Airplane Fuel Tank System Design Review, 
Flammability Reduction and Maintenance and Inspection Requirements'' 
(66 FR 23086, May 7, 2001). In addition to new airworthiness standards 
for transport airplanes and new maintenance requirements, this rule 
included Special Federal Aviation Regulation No. 88 (``SFAR 88,'' 
Amendment 21-78, and subsequent Amendments 21-82 and 21-83).
    Among other actions, SFAR 88 requires certain type design (i.e., 
type certificate (TC) and supplemental type certificate (STC)) holders 
to substantiate that their fuel tank systems can prevent ignition 
sources in the fuel tanks. This requirement applies to type design 
holders for large turbine-powered transport airplanes and for 
subsequent modifications to those airplanes. It requires them to 
perform design reviews and to develop design changes and maintenance 
procedures if their designs do not meet the new fuel tank safety 
standards. As explained in the preamble to the rule, we intended to 
adopt airworthiness directives to mandate any changes found necessary 
to address unsafe conditions identified as a result of these reviews.
    In evaluating these design reviews, we have established four 
criteria intended to define the unsafe conditions associated with fuel 
tank systems that require corrective actions. The percentage of 
operating time during which fuel tanks are exposed to flammable 
conditions is one of these criteria. The other three criteria address 
the failure types under evaluation: Single failures, single failures in 
combination with a latent condition(s), and in-service failure 
experience. For all four criteria, the evaluations included 
consideration of previous actions taken that may mitigate the need for 
further action.
    We have determined that the actions identified in this AD are 
necessary to reduce the potential of ignition sources inside fuel 
tanks, which, in combination with flammable fuel vapors, could result 
in fuel tank explosions and consequent loss of the airplane.

Relevant Service Information

    Bombardier (de Havilland) has issued temporary revisions (TRs) to 
Part 2 ``Airworthiness Limitations List'' (AWL) of the de Havilland 
Dash 8 Series Maintenance Program Manuals (MPMs). The TRs are listed in 
the table titled ``TRs to the DHC-8 MPMs.''

                          TRs to the DHC-8 MPMs
------------------------------------------------------------------------
               MPM                      TR Nos.             TR date
------------------------------------------------------------------------
Dash 8 Series 100 Product         AWL-110...........  August 31, 2007.
 Support Manual 1-8-7.
Dash 8 Series 200 Product         AWL 2-43..........  August 31, 2007.
 Support Manual 1-82-7.
Dash 8 Series 300 Product         AWL 3-109           August 31, 2007.
 Support Manual 1-83-7.
------------------------------------------------------------------------


[[Page 9057]]

    The actions described in this service information are intended to 
correct the unsafe condition identified in the MCAI.

FAA's Determination and Requirements of This Proposed AD

    This product has been approved by the aviation authority of another 
country, and is approved for operation in the United States. Pursuant 
to our bilateral agreement with the State of Design Authority, we have 
been notified of the unsafe condition described in the MCAI and service 
information referenced above. We are proposing this AD because we 
evaluated all pertinent information and determined an unsafe condition 
exists and is likely to exist or develop on other products of the same 
type design.
    This proposed AD would also allow accomplishing the AWL revision in 
accordance with later revisions of the Maintenance Program Manual (MPM) 
as an acceptable method of compliance if the limit or interval is part 
of a later approved MPM revision or the limit or interval is approved 
as an alternative method of compliance (AMOC) in accordance with the 
procedures specified in paragraph (g) of this proposed AD.
    In most ADs, we adopt a compliance time allowing a specified amount 
of time after the AD's effective date. In this case, however, the FAA 
has already issued regulations that require operators to revise their 
maintenance/inspection programs to address fuel tank safety issues. The 
compliance date for these regulations is December 16, 2008. To provide 
for coordinated implementation of these regulations and this proposed 
AD, we are using this same compliance date in this proposed AD.

Differences Between This 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 proposed 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 proposed AD.

Costs of Compliance

    Based on the service information, we estimate that this proposed AD 
would affect about 122 products of U.S. registry. We also estimate that 
it would take about 1 work-hour per product to comply with the basic 
requirements of this proposed AD. The average labor rate is $80 per 
work-hour. Based on these figures, we estimate the cost of the proposed 
AD on U.S. operators to be $9,760, or $80 per product.

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 proposed AD would not have federalism 
implications under Executive Order 13132. This proposed AD would 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 proposed 
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 proposed AD and placed it in the AD docket.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Safety.

The Proposed Amendment

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

PART 39--AIRWORTHINESS DIRECTIVES

    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]

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

Bombardier, Inc. (Formerly de Havilland, Inc.): Docket No. FAA-2008-
0179; Directorate Identifier 2007-NM-367-AD.

Comments Due Date

    (a) We must receive comments by March 20, 2008.

Affected ADs

    (b) None.

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.

    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 according 
to paragraph (g) 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.

Subject

    (d) Air Transport Association (ATA) of America Code 28: Fuel.

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 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 supplemental maintenance tasks 
[inspections of fuel tank bonding jumpers, wiring harnesses, and 
drain valve components, among other items and actions; and 
applicable corrective actions] are required to prevent potential

[[Page 9058]]

ignition sources inside the fuel system, which could result in a 
fuel tank explosion. Revisions have been made to Part 2 
``Airworthiness Limitations List'' of the DHC-8 Maintenance Program 
Manuals to introduce the required maintenance tasks.

The corrective action is revising the Airworthiness Limitations 
Section of the Instructions for Continued Airworthiness to 
incorporate new limitations for fuel tank systems.

Actions and Compliance

    (f) Unless already done, do the following actions.
    (1) Within 60 days after the effective date of this AD, or 
before December 16, 2008, whichever occurs first, revise the 
Airworthiness Limitations Section (ALS) of the Instructions for 
Continued Airworthiness to incorporate the fuel system limitations 
tasks identified in the de Havilland temporary revisions (TRs) to 
Part 2 ``Airworthiness Limitations List'' of the Dash 8 Series 
Maintenance Program Manuals (``the MPMs''). The TRs are listed in 
Table 1 of this AD. For the tasks identified in the TRs, the initial 
compliance times start from the later of the times specified in 
paragraphs (f)(1)(i) and (f)(1)(ii) of this AD, and the repetitive 
inspections must be accomplished thereafter at the interval 
specified in the TRs to the MPM, except as provided by paragraphs 
(f)(2), (f)(3), (f)(4), and (g)(1) of this AD.
    (i) The effective date of this AD.
    (ii) The date of issuance of the original Canadian standard 
airworthiness certificate or the date of issuance of the original 
Canadian export certificate of airworthiness.

                      Table 1.--Temporary Revisions
------------------------------------------------------------------------
                                                          Maintenance
              Model                 de Havilland TR     Program Manual
                                                             (MPM)
------------------------------------------------------------------------
DHC-8-102, DHC-8-103, and DHC-8-  AWL-110, dated      Dash 8 Series 100
 106 airplanes.                    August 31, 2007.    MPM, Product
                                                       Support Manual
                                                       (PSM) 1-8-7, Part
                                                       2,
                                                       ``Airworthiness
                                                       Limitations
                                                       List''.
DHC-8-201, and DHC-8-202          AWL 2-43, dated     Dash 8 Series 200
 airplanes.                        August 31, 2007.    MPM, PSM 1-82-7,
                                                       Part 2,
                                                       ``Airworthiness
                                                       Limitations
                                                       List''.
DHC-8-301, DHC-8-311, and DHC-8-  AWL 3-109, dated    Dash 8 Series 300
 315 airplanes.                    August 31, 2007.    MPM, PSM 1-83-7,
                                                       Part 2,
                                                       ``Airworthiness
                                                       Limitations
                                                       List''.
------------------------------------------------------------------------


    Note 2: The actions required by paragraph (f)(1) of this AD may 
be done by inserting a copies of the applicable TR listed in Table 1 
of this AD into the Airworthiness Limitations section of the 
applicable MPM listed in Table 1 of this AD. When the applicable TR 
has been included in general revisions of the applicable MPM, the 
general revisions may be inserted in the MPM, provided the relevant 
information in the general revision is identical to that in the 
applicable TR.

    (2) For airplanes that have accumulated 4,000 total flight 
hours, or 24 months since new as of the effective date of this AD: 
For those tasks with 6,000 flight hours/36 month inspection 
intervals, do the initial inspection within 2,000 flight hours or 12 
months after the effective date of this AD, whichever occurs first. 
Thereafter, repeat the inspection at intervals not to exceed 6,000 
flight hours or 36 months, whichever occurs first.
    (3) For airplanes that have accumulated 12,000 total flight 
hours, or 72 months since new as of the effective date of this AD: 
For those tasks with 18,000 flight hours/108 month inspection 
intervals, do the initial inspection within 6,000 flight hours or 36 
months after the effective date of this AD, whichever occurs first. 
Thereafter, repeat the inspection at intervals not to exceed 18,000 
flight hours or 108 months, whichever occurs first.
    (4) After accomplishing the actions specified in paragraphs 
(f)(1), (f)(2), and (f)(3) of this AD, no alternative inspections or 
inspection intervals may be used unless the inspections or 
inspection intervals are part of a later revision of Part 2 
``Airworthiness Limitations List'' of the applicable de Havilland 
Dash 8 Series MPM listed in Table 2 of this AD, that is approved by 
the Manager, New York Aircraft Certification Office (ACO), FAA, or 
the Transport Canada Civil Aviation (TCCA) (or its delegated agent); 
or unless inspections or inspection intervals are approved as an 
alternative method of compliance (AMOC) in accordance with the 
procedures specified in paragraph (g)(1) of this AD.

                             Table 2.--MPMs
------------------------------------------------------------------------
                                            Maintenance Program Manual
                 Model                                (MPM)
------------------------------------------------------------------------
                                         ...............................
DHC-8-102, DHC-8-103, and DHC-8-106      Dash 8 Series 100 MPM, Product
 airplanes.                               Support Manual (PSM) 1-8-7,
                                          Part 2, ``Airworthiness
                                          Limitations List,'' Revision
                                          17, dated April 19, 2005.
DHC-8-201, and DHC-8-202 airplanes.....  Dash 8 Series 200 MPM, PSM 1-82-
                                          7, Part 2, ``Airworthiness
                                          Limitations List,'' Revision
                                          5, dated August 15, 2001.
DHC-8-301, DHC-8-311, and DHC-8-315      Dash 8 Series 300 MPM, PSM 1-83-
 airplanes.                               7, Part 2, ``Airworthiness
                                          Limitations List,'' Revision
                                          16, dated August 15, 2001.
------------------------------------------------------------------------

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 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: Rocco Viselli, Aerospace Engineer, Airframe and 
Propulsion Branch, ANE-171, FAA, New York Aircraft Certification 
Office, 1600 Stewart Avenue, Suite 410, Westbury, New York 11590; 
telephone (516) 228-7331; fax (516) 794-5531. 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.
    (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, 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-2007-32, 
dated December 17, 2007, and the temporary revisions listed in Table 
1 of this AD.

    Issued in Renton, Washington, on February 11, 2008.
Stephen P. Boyd,
Assistant Manager, Transport Airplane Directorate, Aircraft 
Certification Service.
 [FR Doc. E8-3000 Filed 2-15-08; 8:45 am]

BILLING CODE 4910-13-P
