[Federal Register: October 31, 2008 (Volume 73, Number 212)]
[Rules and Regulations]
[Page 64879-64881]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr31oc08-7]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2008-0848; Directorate Identifier 2008-NM-082-AD;
Amendment 39-15702; AD 2008-22-07]
RIN 2120-AA64
Airworthiness Directives; Saab AB, Saab Aerosystems Model SAAB
2000 Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
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SUMMARY: We are adopting a new airworthiness directive (AD) for the
products listed above. 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:
Subsequent to accidents involving Fuel Tank System explosions in
flight * * * and on ground, * * * Special Federal Aviation
Regulation 88 (SFAR88) * * * required * * * a design review against
explosion risks.
* * * * *
The unsafe condition is 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. We
are issuing this AD to require actions to correct the unsafe condition
on these products.
DATES: This AD becomes effective December 5, 2008.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of December 5,
2008.
ADDRESSES: You may examine the AD docket on the Internet at http://
www.regulations.gov or in person at the U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC.
FOR FURTHER INFORMATION CONTACT: Shahram Daneshmandi, Aerospace
Engineer, International Branch, ANM-116, Transport Airplane
Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 98057-3356;
telephone (425) 227-1112; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would apply to the specified products.
That NPRM was published in the Federal Register on August 7, 2008 (73
FR 45888). That NPRM proposed to correct an unsafe condition for the
specified products. The MCAI states:
Subsequent to accidents involving Fuel Tank System explosions in
flight * * * and on ground, the FAA has published Special Federal
Aviation Regulation 88 (SFAR88) in June 2001. In their Letters
referenced 04/00/02/07/01-L296 dated March 4th, 2002 and 04/00/02/
07/03-L024, dated February 3rd, 2003, the Joint Aviation Authorities
(JAA) recommended the application of a similar regulation to the
National Aviation Authorities (NAA).
Under current European Union regulation, all holders of type
certificates for passenger transport aircraft with either a
passenger capacity of 30 or more, or a payload capacity of 7,500
pounds (3,402 kg) or more, which have received their certification
after January 1st, 1958, are required to conduct a design review
against explosion risks.
This Airworthiness Directive (AD), which is the result of one of
these design reviews, requires a wiring modification of the FQIS
(Fuel Quantity Indication System) Signal conditioner 28VDC (volts
direct current) supply and replacement of the Fuel Pump harness
inside the wing tanks (both LH and RH (left- and right-hand)).
The unsafe condition is 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. The
corrective actions include functional and operational tests. You may
obtain further information by examining the MCAI in the AD docket.
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.
Explanation of Change to Applicability
We have revised the applicability of the existing AD to identify
the type certificate holder as published in the most recent type
certificate data sheet for the affected model.
Conclusion
We reviewed the available data and determined that air safety and
the
[[Page 64880]]
public interest require adopting the AD with the change described
previously. We determined that this change will not increase the
economic burden on any operator or increase the scope of the 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 required different actions in this AD from those
in the MCAI in order to follow our FAA policies. Any such differences
are highlighted in a NOTE within the AD.
Costs of Compliance
We estimate that this AD will affect about 6 products of U.S.
registry. We also estimate that it will take about 80 work-hours per
product to comply with the basic requirements of this AD. The average
labor rate is $80 per work-hour. Required parts will cost about $14,040
per product. Where the service information lists required parts costs
that are covered under warranty, we have assumed that there will be no
charge for these parts. As we do not control warranty coverage for
affected parties, some parties may incur costs higher than estimated
here. Based on these figures, we estimate the cost of this AD to the
U.S. operators to be $122,640, or $20,440 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 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.
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 the NPRM, 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.
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:
2008-22-07 Saab AB, Saab Aerosystems: Amendment 39-15702. Docket No.
FAA-2008-0848; Directorate Identifier 2008-NM-082-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective December
5, 2008.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Saab AB, Saab Aerosystems Model SAAB 2000
airplanes, certificated in any category, all serial numbers.
Subject
(d) Air Transport Association (ATA) of America Code 28: Fuel.
Reason
(e) The mandatory continuing airworthiness information (MCAI)
states:
Subsequent to accidents involving Fuel Tank System explosions in
flight * * * and on ground, the FAA has published Special Federal
Aviation Regulation 88 (SFAR88) in June 2001. In their Letters
referenced 04/00/02/07/01-L296 dated March 4th, 2002 and 04/00/02/
07/03-L024, dated February 3rd, 2003, the Joint Aviation Authorities
(JAA) recommended the application of a similar regulation to the
National Aviation Authorities (NAA).
Under current European Union regulation, all holders of type
certificates for passenger transport aircraft with either a
passenger capacity of 30 or more, or a payload capacity of 7,500
pounds (3,402 kg) or more, which have received their certification
after January 1st, 1958, are required to conduct a design review
against explosion risks.
This Airworthiness Directive (AD), which is the result of one of
these design reviews, requires a wiring modification of the FQIS
(Fuel Quantity Indication System) Signal conditioner 28VDC (volts
direct current) supply and replacement of the Fuel Pump harness
inside the wing tanks (both LH and RH (left- and right-hand)).
The unsafe condition is 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.
The corrective actions include functional and operational tests.
Actions and Compliance
(f) Unless already done, do the following actions.
(1) Within 72 months after the effective date of this AD,
replace the fuel pump harness inside each (both left- and right-
hand) inboard wing fuel tank in accordance with the Accomplishment
Instructions of Saab 2000 Service Bulletin 2000-28-013, dated
October 11, 2007 (Modification 6250), including a follow-up
functional test and operational test.
(2) Within 72 months after the effective date of this AD, modify
the wiring of the 28 VDC supply to the signal conditioner and the
132VP (feed-through connector) in accordance with the Accomplishment
Instructions of Saab 2000 Service Bulletin 2000-28-014, Revision 02,
dated January 23, 2008 (Modification 6251), including the follow-up
operational test.
(3) Actions done before the effective date of this AD in
accordance with Saab 2000 Service Bulletin 2000-28-014, Revision 01,
dated November 6, 2007, are acceptable for
[[Page 64881]]
compliance with the requirements of paragraph (f)(2) of this AD.
FAA AD Differences
Note: 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,
International Branch, ANM-116, Transport Airplane Directorate, 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:
Shahram Daneshmandi, Aerospace Engineer, International Branch, ANM-
116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW.,
Renton, Washington 98057-3356; telephone (425) 227-1112; fax (425)
227-1149. 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 European Aviation Safety Agency Airworthiness
Directive 2008-0031, dated February 15, 2008; Saab 2000 Service
Bulletin 2000-28-013, dated October 11, 2007; and Saab 2000 Service
Bulletin 2000-28-014, Revision 02, dated January 23, 2008; for
related information.
Material Incorporated by Reference
(i) You must use Saab 2000 Service Bulletin 2000-28-013, dated
October 11, 2007; and Saab 2000 Service Bulletin 2000-28-014,
Revision 02, dated January 23, 2008; as applicable; 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 Saab
Aircraft AB, SAAB Aerosystems, SE-581.88, Link[ouml]ping, Sweden;
telephone 011 46 13 18 5591; fax 011 46 13 18 4874; e-mail http://
www.saab2000.techsupport@saabgroup.com; Internet http://
www.saabgroup.com.
(3) You may review copies 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: http://www.archives.gov/federal_register/code_of_
federal_regulations/ibr_locations.html.
Issued in Renton, Washington, on October 9, 2008.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E8-25307 Filed 10-30-08; 8:45 am]
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