Airworthiness Directives; Airbus Model A300 Airplanes; A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model A300 C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes); and A310 Airplanes, 5160-5164 [E7-1602]
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into the FAA-approved maintenance program
to specify an inspection for breaks of the
bottom flange of the RAT swivel coupling
yoke fitting after each RAT retraction; and
replacement of the RAT swivel coupling yoke
fitting with a new aluminum or steel part as
applicable; in accordance with a method
approved by the Manager, International
Branch, ANM–116, Transport Airplane
´ ´
Directorate, FAA; or the Direction Generale
de l’Aviation Civile (or its delegated agent);
or European Aviation Safety Agency (or its
delegated agent). The page blocks specified
in paragraphs (c)(1), (c)(2), and (c)(3) of this
AD, as applicable, are one approved method
for the actions required by paragraph (c) of
this AD. Thereafter, except as provided by
paragraph (d) of this AD, no alternative
inspection intervals may be approved for the
bottom flange of the RAT swivel coupling
yoke fitting.
(1) Airbus A300–600 AMM, Chapter 29–
25–00, Page Block 301, dated June 1, 2005.
(2) Airbus A310 AMM, Chapter 29–25–00,
Page Block 301, dated June 1, 2005.
(3) Airbus A300 AMM Chapter 29–25–00,
Page Block 301, dated March 1, 2006.
Note 2: After revising the maintenance
program to include the required periodic
inspections according to this paragraph,
operators do not need to make a maintenance
log entry to show compliance with this AD
every time those inspections are
accomplished thereafter.
Note 3: 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 (d) of this AD. The request
should include a description of changes to
the required inspections that will ensure the
continued damage tolerance of the affected
structure. The FAA has provided guidance
for this determination in Advisory Circular
(AC) 25–1529–1.
Alternative Methods of Compliance
(d)(1) In accordance with 14 CFR 39.19, the
Manager, International Branch, ANM–116, is
authorized to approve alternative methods of
compliance for this AD.
(2) Before using any AMOC approved in
accordance with § 39.19 on any airplane to
which the AMOC applies, notify the
appropriate principal inspector in the FAA
Flight Standards Certificate Holding District
Office.
Note 4: The subject of this AD is addressed
in French airworthiness directives F–2005–
089, dated June 8, 2005; and F–2005–090 R1,
dated July 6, 2005.
Incorporation by Reference
(e) Unless otherwise specified in this AD,
the actions must be done in accordance with
the applicable service information specified
in Table 1 of this AD. This incorporation by
reference was approved by the Director of the
Federal Register in accordance with 5 U.S.C.
552(a) and 1 CFR part 51. To get copies of
this service information, contact Airbus, 1
Rond Point Maurice Bellonte, 31707 Blagnac
Cedex, France. To inspect copies of this
service information, go to the FAA, Transport
Airplane Directorate, 1601 Lind Avenue,
SW., Renton, Washington; or to the National
Archives and Records Administration
(NARA). For information on the availability
of this material at the NARA, call (202) 741–
6030, or go to https://www.archives.gov/
federal_register/code_of_federal_regulations/
ibr_locations.html.
TABLE 1.—MATERIAL INCORPORATED BY REFERENCE
Revision
level
Service information
Airbus
Airbus
Airbus
Airbus
Airbus
A300–600 All Operators Telex 57A6096 ....................................................................................
A310 All Operators Telex 57A2085 ............................................................................................
Service Bulletin A300–57–0244 ..................................................................................................
Service Bulletin A300–57–6099 ..................................................................................................
Service Bulletin A310–57–2086 ..................................................................................................
Effective Date
DEPARTMENT OF TRANSPORTATION
(f) This amendment becomes effective on
March 12, 2007.
Federal Aviation Administration
Issued in Renton, Washington, on January
24, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E7–1601 Filed 2–2–07; 8:45 am]
14 CFR Part 39
BILLING CODE 4910–13–P
Airworthiness Directives; Airbus Model
A300 Airplanes; A300 B4–600, B4–
600R, and F4–600R Series Airplanes,
and Model A300 C4–605R Variant F
Airplanes (Collectively Called A300–
600 Series Airplanes); and A310
Airplanes
[Docket No. FAA–2006–24289; Directorate
Identifier 2005–NM–186–AD; Amendment
39–14921; AD 2007–03–10]
RIN 2120–AA64
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
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AGENCY:
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for all
Airbus airplanes identified above. This
AD requires improving the routing of
certain electrical wire bundles in certain
airplane zones, as applicable to the
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01 ................
01 ................
Original ........
Original ........
Original ........
Date
April 11, 2005.
April 11, 2005.
March 4, 2005.
February 23, 2005.
March 1, 2005.
airplane model. This AD results from
fuel system reviews conducted by the
manufacturer. We are issuing this AD 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.
DATES: This AD becomes effective
March 12, 2007.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in the AD
as of March 12, 2007.
ADDRESSES: You may examine the AD
docket on the Internet at https://
dms.dot.gov or in person at the Docket
Management Facility, U.S. Department
of Transportation, 400 Seventh Street,
SW., Nassif Building, Room PL–401,
Washington, DC.
Contact Airbus, 1 Rond Point Maurice
Bellonte, 31707 Blagnac Cedex, France,
for service information identified in this
AD.
FOR FURTHER INFORMATION CONTACT:
Thomas Stafford, Aerospace Engineer,
International Branch, ANM–116,
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Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton,
Washington 98057–3356; telephone
(425) 227–1622; fax (425) 227–1149.
SUPPLEMENTARY INFORMATION:
Examining the Docket
You may examine the AD docket on
the Internet at https://dms.dot.gov or in
person at the Docket Management
Facility office between 9 a.m. and 5
p.m., Monday through Friday, except
Federal holidays. The Docket
Management Facility office (telephone
(800) 647–5227) is located on the plaza
level of the Nassif Building at the street
address stated in the ADDRESSES section.
Discussion
The FAA issued a supplemental
notice of proposed rulemaking (NPRM)
to amend 14 CFR part 39 to include an
AD that would apply to all Airbus
Model A300 airplanes; A300 B4–600,
B4–600R, and F4–600R series airplanes,
and Model A300 C4–605R Variant F
airplanes (collectively called A300–600
series airplanes); and A310 airplanes.
That supplemental NPRM was
published in the Federal Register on
September 11, 2006 (71 FR 53341). That
supplemental NPRM proposed to
require the actions in the original
NPRM, which were improving the
routing of certain electrical wire
bundles in certain airplane zones, as
applicable to the airplane model. That
supplemental NPRM also revised the
original NPRM by removing certain
proposed requirements, and extending
the compliance time for a certain
replacement. That supplemental NPRM
5161
also specified that the actions are
considered interim until a terminating
action for the removed proposed
requirements is approved and available.
Relevant Service Information
Since we issued the supplemental
NPRM, we have reviewed and approved
the service bulletins listed in the
following table. We referred to earlier
revisions of these service bulletins as
appropriate sources of service
information for accomplishing certain
actions in the supplemental NPRM. We
have changed paragraphs (f)(2), (g),
(h)(1), and (h)(2), and Table 1 of this AD
to include references to these new
revisions, and to give credit for
accomplishment of previous revisions.
The changes in the service information
do not change the scope of the AD.
NEW REVISIONS OF CERTAIN SERVICE BULLETINS
Airbus Service Bulletin—
Was Issued to—
A300–24–6004, Revision 04, dated November 15, 2005 ........................
• Change the manufacturer’s serial numbers in Paragraph 1.A.
‘‘Effectivity.’’
• Specify that the service bulletin has been rendered mandatory in
France.
• Give the European Aviation Safety Agency (EASA) designation organization approval number.
• Include references to certain other documents.
• Update certain access and test information.
• Include a note regarding the removal of a certain clamp.
• Change the manufacturer’s serial numbers in Paragraph 1.A.
‘‘Effectivity.’’
• Revise manpower estimates.
• Include references to certain other documents.
• Revise materials description.
• Add a note regarding the size of certain clamps.
• Change the manufacturer’s serial numbers in Paragraph 1.A.
‘‘Effectivity.’’
• Specify that the service bulletin is part of the fuel safety assessment
program.
• Specify that the service bulletin has been rendered mandatory in
France.
• Include references to certain other documents.
• Update material, price, and industry support information.
• Update certain access and part number information.
• Change the manufacturer’s serial numbers in Paragraph 1.A.
‘‘Effectivity.’’
• Specify that the service bulletin has been rendered mandatory in
France.
• Give the EASA designation organization approval number.
• Include references to certain other documents.
• Update certain access and test information.
• Include a note regarding the removal of a certain clamp.
A300–24–6043, Revision 07, dated October 11, 2006 ............................
A300–28–6056, Revision 01, dated January 20, 2006 ............................
A310–24–2009, Revision 04, dated November 15, 2005 ........................
Comments
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We provided the public the
opportunity to participate in the
development of this AD. We have
considered the comment received.
Request To Change Incorporation of
Certain Information
The Modification and Replacement
Parts Association (MARPA) states that,
typically, airworthiness directives are
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14:24 Feb 02, 2007
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based on service information originating
with the type certificate holder or its
suppliers. MARPA adds that
manufacturer service documents are
privately authored instruments
generally having copyright protection
against duplication and distribution.
MARPA notes that when a service
document is incorporated by reference
into a public document, such as an
airworthiness directive, it loses its
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private, protected status and becomes a
public document. MARPA adds that if
a service document is used as a
mandatory element of compliance, it
should not simply be referenced, but
should be incorporated into the
regulatory document; by definition,
public laws must be public, which
means they cannot rely upon private
writings. MARPA is concerned that the
failure to incorporate essential service
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information could result in a court
decision invalidating the AD.
MARPA adds that incorporated by
reference service documents should be
made available to the public by
publication in the Docket Management
System (DMS), keyed to the action that
incorporates them. MARPA notes that
the stated purpose of the incorporation
by reference method is brevity, to keep
from expanding the Federal Register
needlessly by publishing documents
already in the hands of the affected
individuals; traditionally, ‘‘affected
individuals’’ means aircraft owners and
operators, who are generally provided
service information by the
manufacturer. MARPA adds that a new
class of affected individuals has
emerged, since the majority of aircraft
maintenance is now performed by
specialty shops instead of aircraft
owners and operators. MARPA notes
that this new class includes
maintenance and repair organizations,
component servicing and repair shops,
parts purveyors and distributors, and
organizations manufacturing or
servicing alternatively certified parts
under part 21 of the Federal Aviation
Regulations (14 CFR part 21), § 21.303
(parts manufacturer approval) (PMA).
MARPA adds that the concept of brevity
is now nearly archaic as documents
exist more frequently in electronic
format than on paper. Therefore,
MARPA asks that the service documents
deemed essential to the accomplishment
of the NPRM be incorporated by
reference into the regulatory instrument,
and published in the DMS.
We understand MARPAs comment
concerning incorporation by reference.
The Office of the Federal Register (OFR)
requires that documents that are
necessary to accomplish the
requirements of the AD be incorporated
by reference during the final rule phase
of rulemaking. This final rule
incorporates by reference the document
necessary for the accomplishment of the
requirements mandated by this AD.
Further, we point out that while
documents that are incorporated by
reference do become public information,
they do not lose their copyright
protection. For that reason, we advise
the public to contact the manufacturer
to obtain copies of the referenced
service information.
Additionally, we do not publish
service documents in DMS. We are
currently reviewing our practice of
publishing proprietary service
information. Once we have thoroughly
examined all aspects of this issue, and
have made a final determination, we
will consider whether our current
practice needs to be revised. However,
we consider that to delay this AD action
for that reason would be inappropriate,
since we have determined that an
unsafe condition exists and that the
requirements in this AD must be
accomplished to ensure continued
safety. Therefore, we have not changed
the AD in this regard.
Clarification of Paragraph (f)(2)
We have clarified paragraph (f)(2) of
this AD to specify the intended
paragraph identifier referenced in that
paragraph.
Conclusion
We have carefully reviewed the
available data, including the comment
received, and determined that air safety
and the public interest require adopting
the AD with the change described
previously. We have determined that
these changes will neither increase the
economic burden on any operator nor
increase the scope of the AD.
Interim Action
We consider this AD interim action.
The EASA, which is the airworthiness
authority for the European Union, has
informed us that the manufacturer is
currently developing an additional
modification that will address the
unsafe condition identified in this AD.
Once this modification is developed,
approved, and available, we may
consider additional rulemaking.
Costs of Compliance
The following table provides the
estimated costs for U.S. operators to
comply with this AD.
This AD affects about 169 airplanes of
U.S. registry. The following table
provides the estimated costs for U.S.
operators to comply with this AD. The
average labor rate is $80 per work hour.
ESTIMATED COSTS
Work
hours
For airplanes on which this action is required—
Action 3, Modify the retaining and protection system ...............................................
Action 4, Modify the electrical wiring of routes 1P and 2P .......................................
Action 5, Inspect the wire looms on the wing trailing edge ......................................
Action 6, Replace the nylon clamps of the electrical routes in the hydraulic compartment and in the shroud box.
Based on these figures, the estimated
cost of the AD for U.S. operators is up
to $2,939,924, or up to $17,396 per
airplane.
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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,
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14:24 Feb 02, 2007
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Parts
4 to 16 .....
2 ...............
8 ..............
44 to 98 ...
$836 to $1,056 ..........
$720 ..........................
Operator Supplied .....
$100 to $5,700 ..........
‘‘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
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Cost per
airplane
$1,156 to $2,336.
$880.
$640.
$3,620 to $13,540.
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
E:\FR\FM\05FER1.SGM
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Federal Register / Vol. 72, No. 23 / Monday, February 5, 2007 / Rules and Regulations
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
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
I
PART 39—AIRWORTHINESS
DIRECTIVES
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 Federal Aviation
Administration (FAA) amends § 39.13
by adding the following new
airworthiness directive (AD):
I
2007–03–10 Airbus: Amendment 39–14921.
Docket No. FAA–2006–24289;
Directorate Identifier 2005–NM–186–AD.
Effective Date
(a) This AD becomes effective March 12,
2007.
Affected ADs
(b) None.
Applicability
(c) This AD applies to all Airbus Model
A300 airplanes; A300 B4–601, B4–603, B4–
620, B4–622, B4–605R, B4–622R, A300 F4–
605R, F4–622R, and C4–605R Variant F
airplanes; and A310 airplanes; certificated in
any category.
Unsafe Condition
(d) This AD results from fuel system
reviews conducted by the manufacturer. We
are issuing this AD 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.
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.
Action 3—Modify the Retaining and
Protection System
(f) For all airplanes identified in
paragraphs (f)(1) and (f)(2) of this AD: Within
26 months after the effective date of this AD,
modify the retaining and protection system
for the electrical bundles located at the wingto-fuselage junction, under the flap control
screw jack.
(1) For Model A300 airplanes: Do the
actions specified in paragraph (f) of this AD
in accordance with the Accomplishment
Instructions of Airbus Service Bulletin A300–
24–0085, Revision 06, dated October 13,
2005.
(2) For Model A300 B4–601, B4–603, B4–
620, B4–622, B4–605R, B4–622R, A300 F4–
605R, F4–622R, and C4–605R Variant F
airplanes, except those on which Airbus
Modification 10505 has been done: Do the
actions specified in paragraph (f) of this AD
in accordance with the Accomplishment
Instructions of Airbus Service Bulletin A300–
24–6043, Revision 07, dated October 11,
2006.
Action 4—Modify the Electrical Wiring of
Routes 1P and 2P
(g) For Model A300 B4–601, B4–603, B4–
620, B4–622, B4–605R, B4–622R, A300 F4–
605R, F4–622R, and C4–605R Variant F
airplanes; except those on which Airbus
Modification 11741 has been done: Within 26
months after the effective date of this AD,
modify the electrical wiring of routes 1P and
2P (along the top panel of the shroud box and
the rear spars of the wings) by extending the
protective conduits up to the next support,
and replace the two existing clamps on this
support with new, improved clamps. Do all
actions in accordance with the
Accomplishment Instructions of Airbus
Service Bulletin A300–28–6056, Revision 01,
dated January 20, 2006.
Action 5—Inspect the Wire Looms
(h) For all airplanes identified in
paragraphs (h)(1) and (h)(2) of this AD:
Within 26 months after the effective date of
this AD, do a general visual inspection of the
wire looms on the wing trailing edge for
improperly held wires in the clamps, restore
the electrical bundles to good condition, and
replace the affected nylon clamps with
metallic clamps that have an elastomer
lining. Do all applicable corrective action
before further flight. Repeat the inspection
thereafter at intervals not to exceed 26
months until all clamps have been replaced.
(1) For Model A300 B4–601, B4–603, B4–
620, B4–622, B4–605R, B4–622R, A300 F4–
605R, F4–622R, and C4–605R Variant F
airplanes; except those on which Airbus
Modification 6478 has been done: Do the
actions specified in paragraph (h) of this AD
in accordance with the Accomplishment
Instructions of Airbus Service Bulletin A300–
24–6004, Revision 04, dated November 15,
2005.
(2) For Model A310 airplanes, except those
on which Airbus Modification 6478 has been
done: Do the actions specified in paragraph
(h) of this AD in accordance with the
Accomplishment Instructions of Airbus
Service Bulletin A310–24–2009, Revision 04,
dated November 15, 2005.
Action 6—Improve the Quality of the
Electrical Routes
(i) For all airplanes identified in
paragraphs (i)(1), (i)(2), and (i)(3) of this AD:
Within 26 months after the effective date of
this AD, replace the nylon clamps of the
electrical routes in the hydraulic
compartment and in the shroud box with
new metallic clamps that have white silicone
lining (for airplanes identified in paragraph
(i)(1) of this AD); and/or replace the nylon
clamps and change the location of routes 1P
and 2P to improve the retention of the wiring
loom (for airplanes identified in paragraphs
(i)(2) and (i)(3) of this AD); as applicable.
(1) For Model A300 airplanes; except those
on which Airbus Modification 11763 has
been done: Do the actions specified in
paragraph (i) of this AD in accordance with
the Accomplishment Instructions of Airbus
Service Bulletin A300–24–0100, dated April
7, 2005.
(2) For Model A300 B4–601, B4–603, B4–
620, B4–622, B4–605R, B4–622R, A300 F4–
605R, F4–622R, and C4–605R Variant F
airplanes; except those on which Airbus
Modifications 11763 and 12995 have been
done: Do the actions specified in paragraph
(i) of this AD in accordance with the
Accomplishment Instructions of Airbus
Service Bulletin A300–24–6084, Revision 01,
dated June 28, 2005.
(3) For Model A310 airplanes, except those
on which Airbus Modification 11763 has
been done: Do the actions specified in
paragraph (i) of this AD in accordance with
the Accomplishment Instructions of Airbus
Service Bulletin A310–24–2091, dated March
4, 2005.
Parts Installation
(j) After the effective date of this AD, no
person may install on any airplane plate
assemblies with part numbers
A5351088000000 or A5351088000100 unless
they have been modified in accordance with
paragraph (f) of this AD.
Actions Accomplished According to
Previous Revisions of Service Bulletins
(k) Actions done before the effective date
of this AD in accordance with the service
bulletins identified in Table 1 of this AD are
acceptable for compliance with the
corresponding requirements in this AD.
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TABLE 1.—PREVIOUS REVISIONS OF SERVICE BULLETINS
Airbus Service Bulletin
A300–24–0085
A300–24–0085
A300–24–0085
A300–24–0085
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Revision level
.................................................................................................
.................................................................................................
.................................................................................................
.................................................................................................
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Date
Original ...............................................
03 .......................................................
04 .......................................................
05 .......................................................
Sfmt 4700
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05FER1
December 12, 1994.
January 17, 1996.
July 23, 1996.
March 6, 2001.
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TABLE 1.—PREVIOUS REVISIONS OF SERVICE BULLETINS—Continued
Airbus Service Bulletin
A300–24–6004
A300–24–6004
A300–24–6004
A300–24–6043
A300–24–6043
A300–24–6043
A300–24–6043
A300–24–6043
A300–24–6043
A300–24–6043
A300–24–6084
A300–28–6056
A310–24–2009
A310–24–2009
A310–24–2009
A310–24–2009
Revision level
.................................................................................................
.................................................................................................
.................................................................................................
.................................................................................................
.................................................................................................
.................................................................................................
.................................................................................................
.................................................................................................
.................................................................................................
.................................................................................................
.................................................................................................
.................................................................................................
.................................................................................................
.................................................................................................
.................................................................................................
.................................................................................................
Alternative Methods of Compliance
(AMOCs)
(l)(1) The Manager, International Branch,
ANM–116, Transport Airplane Directorate,
FAA, has the authority to approve AMOCs
for this AD, if requested in accordance with
the procedures found in 14 CFR 39.19.
(2) Before using any AMOC approved in
accordance with § 39.19 on any airplane to
which the AMOC applies, notify the
appropriate principal inspector in the FAA
Flight Standards Certificate Holding District
Office.
Date
1 .........................................................
2 .........................................................
03 .......................................................
Original ...............................................
01 .......................................................
02 .......................................................
03 .......................................................
04 .......................................................
05 .......................................................
06 .......................................................
Original ...............................................
Original ...............................................
Original ...............................................
1 .........................................................
2 .........................................................
03 .......................................................
Related Information
(m) European Aviation Safety Agency
airworthiness directive 2006–0074, dated
April 3, 2006, also addresses the subject of
this AD.
Material Incorporated by Reference
(n) You must use the service information
specified in Table 2 of this AD to perform the
actions that are required by this AD, unless
the AD specifies otherwise. The Director of
the Federal Register approved the
incorporation by reference of these
documents in accordance with 5 U.S.C.
552(a) and 1 CFR part 51. Contact Airbus, 1
January 28, 1988.
February 24, 1995.
June 30, 1998.
December 12, 1994.
February 7, 1995.
May 10, 1995.
January 17, 1996.
March 6, 2001.
August 30, 2001.
October 13, 2005.
March 4, 2005.
February 18, 1998.
May 31, 1985.
January 28, 1988.
February 24, 1995.
June 30, 1998.
Rond Point Maurice Bellonte, 31707 Blagnac
Cedex, France, for a copy of this service
information. You may review copies at the
Docket Management Facility, U.S.
Department of Transportation, 400 Seventh
Street SW., Room PL–401, Nassif Building,
Washington, DC; on the Internet at https://
dms.dot.gov; or at the National Archives and
Records Administration (NARA). For
information on the availability of this
material at the NARA, call (202) 741–6030,
or go to https://www.archives.gov/
federal_register/code_of_federal_regulations/
ibr_locations.html.
TABLE 2.—MATERIAL INCORPORATED BY REFERENCE
Revision
level
Airbus Service Bulletin
A300–24–0085
A300–24–0100
A300–24–6004
A300–24–6043
A300–24–6084
A300–28–6056
A310–24–2009
A310–24–2091
.................................................................................................
.................................................................................................
.................................................................................................
.................................................................................................
.................................................................................................
.................................................................................................
.................................................................................................
.................................................................................................
Issued in Renton, Washington, on January
24, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E7–1602 Filed 2–2–07; 8:45 am]
BILLING CODE 4910–13–P
06 .......................................................
Original ...............................................
04 .......................................................
07 .......................................................
01 .......................................................
01 .......................................................
04 .......................................................
Original ...............................................
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2006–26046; Directorate
Identifier 2006–NM–172–AD; Amendment
39–14922; AD 2007–03–11]
mstockstill on PROD1PC66 with RULES
RIN 2120–AA64
Airworthiness Directives; Bombardier
Model CL–600–2B19 (Regional Jet
Series 100 & 440) Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
VerDate Aug<31>2005
14:24 Feb 02, 2007
Jkt 211001
PO 00000
Frm 00014
Fmt 4700
Date
Sfmt 4700
October 13, 2005.
April 7, 2005.
November 15, 2005.
October 11, 2006.
June 28, 2005.
January 20, 2006.
November 15, 2005.
March 4, 2005.
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for certain
Bombardier Model CL–600–2B19
(Regional Jet Series 100 & 440)
airplanes. This AD requires inspecting
for discrepancies of the activation
mechanism of certain chemical oxygen
generators, and corrective action if
necessary. This AD results from several
incidents, on certain airplane models, of
incorrect installation of the release pin
into the safety pin hole of the activation
mechanism of the chemical oxygen
generator; this resulted in failure to
activate the chemical oxygen generator
when required. A separate incident
occurred on a different airplane model
during deployment of the cabin oxygen
system, which resulted in failure of the
E:\FR\FM\05FER1.SGM
05FER1
]]>Agencies
[Federal Register Volume 72, Number 23 (Monday, February 5, 2007)]
[Rules and Regulations]
[Pages 5160-5164]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E7-1602]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2006-24289; Directorate Identifier 2005-NM-186-AD;
Amendment 39-14921; AD 2007-03-10]
RIN 2120-AA64
Airworthiness Directives; Airbus Model A300 Airplanes; A300 B4-
600, B4-600R, and F4-600R Series Airplanes, and Model A300 C4-605R
Variant F Airplanes (Collectively Called A300-600 Series Airplanes);
and A310 Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
Airbus airplanes identified above. This AD requires improving the
routing of certain electrical wire bundles in certain airplane zones,
as applicable to the airplane model. This AD results from fuel system
reviews conducted by the manufacturer. We are issuing this AD 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.
DATES: This AD becomes effective March 12, 2007.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in the AD as of March 12,
2007.
ADDRESSES: You may examine the AD docket on the Internet at https://
dms.dot.gov or in person at the Docket Management Facility, U.S.
Department of Transportation, 400 Seventh Street, SW., Nassif Building,
Room PL-401, Washington, DC.
Contact Airbus, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex,
France, for service information identified in this AD.
FOR FURTHER INFORMATION CONTACT: Thomas Stafford, Aerospace Engineer,
International Branch, ANM-116,
[[Page 5161]]
Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton,
Washington 98057-3356; telephone (425) 227-1622; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
Examining the Docket
You may examine the AD docket on the Internet at https://dms.dot.gov
or in person at the Docket Management Facility office between 9 a.m.
and 5 p.m., Monday through Friday, except Federal holidays. The Docket
Management Facility office (telephone (800) 647-5227) is located on the
plaza level of the Nassif Building at the street address stated in the
ADDRESSES section.
Discussion
The FAA issued a supplemental notice of proposed rulemaking (NPRM)
to amend 14 CFR part 39 to include an AD that would apply to all Airbus
Model A300 airplanes; A300 B4-600, B4-600R, and F4-600R series
airplanes, and Model A300 C4-605R Variant F airplanes (collectively
called A300-600 series airplanes); and A310 airplanes. That
supplemental NPRM was published in the Federal Register on September
11, 2006 (71 FR 53341). That supplemental NPRM proposed to require the
actions in the original NPRM, which were improving the routing of
certain electrical wire bundles in certain airplane zones, as
applicable to the airplane model. That supplemental NPRM also revised
the original NPRM by removing certain proposed requirements, and
extending the compliance time for a certain replacement. That
supplemental NPRM also specified that the actions are considered
interim until a terminating action for the removed proposed
requirements is approved and available.
Relevant Service Information
Since we issued the supplemental NPRM, we have reviewed and
approved the service bulletins listed in the following table. We
referred to earlier revisions of these service bulletins as appropriate
sources of service information for accomplishing certain actions in the
supplemental NPRM. We have changed paragraphs (f)(2), (g), (h)(1), and
(h)(2), and Table 1 of this AD to include references to these new
revisions, and to give credit for accomplishment of previous revisions.
The changes in the service information do not change the scope of the
AD.
New Revisions of Certain Service Bulletins
------------------------------------------------------------------------
Airbus Service Bulletin-- Was Issued to--
------------------------------------------------------------------------
A300-24-6004, Revision 04, dated Change the
November 15, 2005. manufacturer's serial numbers
in Paragraph 1.A.
``Effectivity.''
Specify that the
service bulletin has been
rendered mandatory in France.
Give the European
Aviation Safety Agency (EASA)
designation organization
approval number.
Include references to
certain other documents.
Update certain access
and test information.
Include a note
regarding the removal of a
certain clamp.
A300-24-6043, Revision 07, dated Change the
October 11, 2006. manufacturer's serial numbers
in Paragraph 1.A.
``Effectivity.''
Revise manpower
estimates.
Include references to
certain other documents.
Revise materials
description.
Add a note regarding
the size of certain clamps.
A300-28-6056, Revision 01, dated Change the
January 20, 2006. manufacturer's serial numbers
in Paragraph 1.A.
``Effectivity.''
Specify that the
service bulletin is part of
the fuel safety assessment
program.
Specify that the
service bulletin has been
rendered mandatory in France.
Include references to
certain other documents.
Update material,
price, and industry support
information.
Update certain access
and part number information.
A310-24-2009, Revision 04, dated Change the
November 15, 2005. manufacturer's serial numbers
in Paragraph 1.A.
``Effectivity.''
Specify that the
service bulletin has been
rendered mandatory in France.
Give the EASA
designation organization
approval number.
Include references to
certain other documents.
Update certain access
and test information.
Include a note
regarding the removal of a
certain clamp.
------------------------------------------------------------------------
Comments
We provided the public the opportunity to participate in the
development of this AD. We have considered the comment received.
Request To Change Incorporation of Certain Information
The Modification and Replacement Parts Association (MARPA) states
that, typically, airworthiness directives are based on service
information originating with the type certificate holder or its
suppliers. MARPA adds that manufacturer service documents are privately
authored instruments generally having copyright protection against
duplication and distribution. MARPA notes that when a service document
is incorporated by reference into a public document, such as an
airworthiness directive, it loses its private, protected status and
becomes a public document. MARPA adds that if a service document is
used as a mandatory element of compliance, it should not simply be
referenced, but should be incorporated into the regulatory document; by
definition, public laws must be public, which means they cannot rely
upon private writings. MARPA is concerned that the failure to
incorporate essential service
[[Page 5162]]
information could result in a court decision invalidating the AD.
MARPA adds that incorporated by reference service documents should
be made available to the public by publication in the Docket Management
System (DMS), keyed to the action that incorporates them. MARPA notes
that the stated purpose of the incorporation by reference method is
brevity, to keep from expanding the Federal Register needlessly by
publishing documents already in the hands of the affected individuals;
traditionally, ``affected individuals'' means aircraft owners and
operators, who are generally provided service information by the
manufacturer. MARPA adds that a new class of affected individuals has
emerged, since the majority of aircraft maintenance is now performed by
specialty shops instead of aircraft owners and operators. MARPA notes
that this new class includes maintenance and repair organizations,
component servicing and repair shops, parts purveyors and distributors,
and organizations manufacturing or servicing alternatively certified
parts under part 21 of the Federal Aviation Regulations (14 CFR part
21), Sec. 21.303 (parts manufacturer approval) (PMA). MARPA adds that
the concept of brevity is now nearly archaic as documents exist more
frequently in electronic format than on paper. Therefore, MARPA asks
that the service documents deemed essential to the accomplishment of
the NPRM be incorporated by reference into the regulatory instrument,
and published in the DMS.
We understand MARPAs comment concerning incorporation by reference.
The Office of the Federal Register (OFR) requires that documents that
are necessary to accomplish the requirements of the AD be incorporated
by reference during the final rule phase of rulemaking. This final rule
incorporates by reference the document necessary for the accomplishment
of the requirements mandated by this AD. Further, we point out that
while documents that are incorporated by reference do become public
information, they do not lose their copyright protection. For that
reason, we advise the public to contact the manufacturer to obtain
copies of the referenced service information.
Additionally, we do not publish service documents in DMS. We are
currently reviewing our practice of publishing proprietary service
information. Once we have thoroughly examined all aspects of this
issue, and have made a final determination, we will consider whether
our current practice needs to be revised. However, we consider that to
delay this AD action for that reason would be inappropriate, since we
have determined that an unsafe condition exists and that the
requirements in this AD must be accomplished to ensure continued
safety. Therefore, we have not changed the AD in this regard.
Clarification of Paragraph (f)(2)
We have clarified paragraph (f)(2) of this AD to specify the
intended paragraph identifier referenced in that paragraph.
Conclusion
We have carefully reviewed the available data, including the
comment received, and determined that air safety and the public
interest require adopting the AD with the change described previously.
We have determined that these changes will neither increase the
economic burden on any operator nor increase the scope of the AD.
Interim Action
We consider this AD interim action. The EASA, which is the
airworthiness authority for the European Union, has informed us that
the manufacturer is currently developing an additional modification
that will address the unsafe condition identified in this AD. Once this
modification is developed, approved, and available, we may consider
additional rulemaking.
Costs of Compliance
The following table provides the estimated costs for U.S. operators
to comply with this AD.
This AD affects about 169 airplanes of U.S. registry. The following
table provides the estimated costs for U.S. operators to comply with
this AD. The average labor rate is $80 per work hour.
Estimated Costs
----------------------------------------------------------------------------------------------------------------
For airplanes on which this
action is required-- Work hours Parts Cost per airplane
----------------------------------------------------------------------------------------------------------------
Action 3, Modify the retaining 4 to 16......... $836 to $1,056............... $1,156 to $2,336.
and protection system.
Action 4, Modify the electrical 2............... $720......................... $880.
wiring of routes 1P and 2P.
Action 5, Inspect the wire looms 8............... Operator Supplied............ $640.
on the wing trailing edge.
Action 6, Replace the nylon 44 to 98........ $100 to $5,700............... $3,620 to $13,540.
clamps of the electrical routes
in the hydraulic compartment
and in the shroud box.
----------------------------------------------------------------------------------------------------------------
Based on these figures, the estimated cost of the AD for U.S.
operators is up to $2,939,924, or up to $17,396 per airplane.
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 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
[[Page 5163]]
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 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 Federal Aviation Administration (FAA) amends Sec. 39.13 by
adding the following new airworthiness directive (AD):
2007-03-10 Airbus: Amendment 39-14921. Docket No. FAA-2006-24289;
Directorate Identifier 2005-NM-186-AD.
Effective Date
(a) This AD becomes effective March 12, 2007.
Affected ADs
(b) None.
Applicability
(c) This AD applies to all Airbus Model A300 airplanes; A300 B4-
601, B4-603, B4-620, B4-622, B4-605R, B4-622R, A300 F4-605R, F4-
622R, and C4-605R Variant F airplanes; and A310 airplanes;
certificated in any category.
Unsafe Condition
(d) This AD results from fuel system reviews conducted by the
manufacturer. We are issuing this AD 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.
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.
Action 3--Modify the Retaining and Protection System
(f) For all airplanes identified in paragraphs (f)(1) and (f)(2)
of this AD: Within 26 months after the effective date of this AD,
modify the retaining and protection system for the electrical
bundles located at the wing-to-fuselage junction, under the flap
control screw jack.
(1) For Model A300 airplanes: Do the actions specified in
paragraph (f) of this AD in accordance with the Accomplishment
Instructions of Airbus Service Bulletin A300-24-0085, Revision 06,
dated October 13, 2005.
(2) For Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R, B4-
622R, A300 F4-605R, F4-622R, and C4-605R Variant F airplanes, except
those on which Airbus Modification 10505 has been done: Do the
actions specified in paragraph (f) of this AD in accordance with the
Accomplishment Instructions of Airbus Service Bulletin A300-24-6043,
Revision 07, dated October 11, 2006.
Action 4--Modify the Electrical Wiring of Routes 1P and 2P
(g) For Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R, B4-
622R, A300 F4-605R, F4-622R, and C4-605R Variant F airplanes; except
those on which Airbus Modification 11741 has been done: Within 26
months after the effective date of this AD, modify the electrical
wiring of routes 1P and 2P (along the top panel of the shroud box
and the rear spars of the wings) by extending the protective
conduits up to the next support, and replace the two existing clamps
on this support with new, improved clamps. Do all actions in
accordance with the Accomplishment Instructions of Airbus Service
Bulletin A300-28-6056, Revision 01, dated January 20, 2006.
Action 5--Inspect the Wire Looms
(h) For all airplanes identified in paragraphs (h)(1) and (h)(2)
of this AD: Within 26 months after the effective date of this AD, do
a general visual inspection of the wire looms on the wing trailing
edge for improperly held wires in the clamps, restore the electrical
bundles to good condition, and replace the affected nylon clamps
with metallic clamps that have an elastomer lining. Do all
applicable corrective action before further flight. Repeat the
inspection thereafter at intervals not to exceed 26 months until all
clamps have been replaced.
(1) For Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R, B4-
622R, A300 F4-605R, F4-622R, and C4-605R Variant F airplanes; except
those on which Airbus Modification 6478 has been done: Do the
actions specified in paragraph (h) of this AD in accordance with the
Accomplishment Instructions of Airbus Service Bulletin A300-24-6004,
Revision 04, dated November 15, 2005.
(2) For Model A310 airplanes, except those on which Airbus
Modification 6478 has been done: Do the actions specified in
paragraph (h) of this AD in accordance with the Accomplishment
Instructions of Airbus Service Bulletin A310-24-2009, Revision 04,
dated November 15, 2005.
Action 6--Improve the Quality of the Electrical Routes
(i) For all airplanes identified in paragraphs (i)(1), (i)(2),
and (i)(3) of this AD: Within 26 months after the effective date of
this AD, replace the nylon clamps of the electrical routes in the
hydraulic compartment and in the shroud box with new metallic clamps
that have white silicone lining (for airplanes identified in
paragraph (i)(1) of this AD); and/or replace the nylon clamps and
change the location of routes 1P and 2P to improve the retention of
the wiring loom (for airplanes identified in paragraphs (i)(2) and
(i)(3) of this AD); as applicable.
(1) For Model A300 airplanes; except those on which Airbus
Modification 11763 has been done: Do the actions specified in
paragraph (i) of this AD in accordance with the Accomplishment
Instructions of Airbus Service Bulletin A300-24-0100, dated April 7,
2005.
(2) For Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R, B4-
622R, A300 F4-605R, F4-622R, and C4-605R Variant F airplanes; except
those on which Airbus Modifications 11763 and 12995 have been done:
Do the actions specified in paragraph (i) of this AD in accordance
with the Accomplishment Instructions of Airbus Service Bulletin
A300-24-6084, Revision 01, dated June 28, 2005.
(3) For Model A310 airplanes, except those on which Airbus
Modification 11763 has been done: Do the actions specified in
paragraph (i) of this AD in accordance with the Accomplishment
Instructions of Airbus Service Bulletin A310-24-2091, dated March 4,
2005.
Parts Installation
(j) After the effective date of this AD, no person may install
on any airplane plate assemblies with part numbers A5351088000000 or
A5351088000100 unless they have been modified in accordance with
paragraph (f) of this AD.
Actions Accomplished According to Previous Revisions of Service
Bulletins
(k) Actions done before the effective date of this AD in
accordance with the service bulletins identified in Table 1 of this
AD are acceptable for compliance with the corresponding requirements
in this AD.
Table 1.--Previous Revisions of Service Bulletins
----------------------------------------------------------------------------------------------------------------
Airbus Service Bulletin Revision level Date
----------------------------------------------------------------------------------------------------------------
A300-24-0085........................... Original.................. December 12, 1994.
A300-24-0085........................... 03........................ January 17, 1996.
A300-24-0085........................... 04........................ July 23, 1996.
A300-24-0085........................... 05........................ March 6, 2001.
[[Page 5164]]
A300-24-6004........................... 1......................... January 28, 1988.
A300-24-6004........................... 2......................... February 24, 1995.
A300-24-6004........................... 03........................ June 30, 1998.
A300-24-6043........................... Original.................. December 12, 1994.
A300-24-6043........................... 01........................ February 7, 1995.
A300-24-6043........................... 02........................ May 10, 1995.
A300-24-6043........................... 03........................ January 17, 1996.
A300-24-6043........................... 04........................ March 6, 2001.
A300-24-6043........................... 05........................ August 30, 2001.
A300-24-6043........................... 06........................ October 13, 2005.
A300-24-6084........................... Original.................. March 4, 2005.
A300-28-6056........................... Original.................. February 18, 1998.
A310-24-2009........................... Original.................. May 31, 1985.
A310-24-2009........................... 1......................... January 28, 1988.
A310-24-2009........................... 2......................... February 24, 1995.
A310-24-2009........................... 03........................ June 30, 1998.
----------------------------------------------------------------------------------------------------------------
Alternative Methods of Compliance (AMOCs)
(l)(1) The Manager, International Branch, ANM-116, Transport
Airplane Directorate, FAA, has the authority to approve AMOCs for
this AD, if requested in accordance with the procedures found in 14
CFR 39.19.
(2) Before using any AMOC approved in accordance with Sec.
39.19 on any airplane to which the AMOC applies, notify the
appropriate principal inspector in the FAA Flight Standards
Certificate Holding District Office.
Related Information
(m) European Aviation Safety Agency airworthiness directive
2006-0074, dated April 3, 2006, also addresses the subject of this
AD.
Material Incorporated by Reference
(n) You must use the service information specified in Table 2 of
this AD to perform the actions that are required by this AD, unless
the AD specifies otherwise. The Director of the Federal Register
approved the incorporation by reference of these documents in
accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact Airbus, 1
Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France, for a copy
of this service information. You may review copies at the Docket
Management Facility, U.S. Department of Transportation, 400 Seventh
Street SW., Room PL-401, Nassif Building, Washington, DC; on the
Internet at https://dms.dot.gov; or at the National Archives and
Records Administration (NARA). For information on the availability
of this material at the NARA, call (202) 741-6030, or go to https://
www.archives.gov/federal_register/code_of_federal_regulations/
ibr_locations.html.
Table 2.--Material Incorporated by Reference
----------------------------------------------------------------------------------------------------------------
Airbus Service Bulletin Revision level Date
----------------------------------------------------------------------------------------------------------------
A300-24-0085........................... 06........................ October 13, 2005.
A300-24-0100........................... Original.................. April 7, 2005.
A300-24-6004........................... 04........................ November 15, 2005.
A300-24-6043........................... 07........................ October 11, 2006.
A300-24-6084........................... 01........................ June 28, 2005.
A300-28-6056........................... 01........................ January 20, 2006.
A310-24-2009........................... 04........................ November 15, 2005.
A310-24-2091........................... Original.................. March 4, 2005.
----------------------------------------------------------------------------------------------------------------
Issued in Renton, Washington, on January 24, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E7-1602 Filed 2-2-07; 8:45 am]
BILLING CODE 4910-13-P
