Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 Airplanes, 3761-3764 [E7-1215]
Download as PDF
Federal Register / Vol. 72, No. 17 / Friday, January 26, 2007 / Proposed Rules
Applicability
(c) This AD applies to Airbus Model A330
airplanes, and Model A340–200 and –300
series airplanes, certificated in any category;
all serial numbers fitted with MLG (main
landing gear) retraction link Part Number
(PN) 201489311 (LH (left-hand) side) or PN
201489312 (RH (right-hand) side).
Reason
(d) The MCAI states that during full-scale
fatigue tests, the retraction link failed on the
latest growth production standard MLG
(main landing gear) prior to its expected life
limit. Investigations confirm that the root
cause of this premature fracture is due to
high lug stress. The retraction link is
included in the ALS (Airworthiness
Limitation section) Part 1—Safe Life
Airworthiness Limitation Item—and
currently limited to 35,200 flight cycles (FC).
Its fracture causes un-damped extension of
the MLG, potentially leading to loss of side
stay integrity and then MLG collapse, which
constitutes an unsafe condition. The aim of
the MCAI is to mandate the reduced
retraction link life limit and replacement of
any retraction link that has exceeded this
new limit.
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Actions and Compliance
(e) Unless already done, do the following
actions.
(1) Prior to the accumulation of 8,300 total
landings on the retraction link assembly or
within 39 days after the effective date of this
AD, whichever occurs later, replace the
retraction link assembly in accordance with
the instructions defined in Airbus All
Operators Telex A330–32A3208, dated
October 18, 2006; or Airbus All Operators
Telex A340–32A4252, dated October 18,
2006; as applicable.
(2) Within 39 days after the effective date
of this AD, report to Airbus the life
accumulation information of each retraction
link assembly affected by this AD in
accordance with Airbus All Operators Telex
A330–32A3208, dated October 18, 2006; or
Airbus All Operators Telex A340–32A4252,
dated October 18, 2006; as applicable.
Note 1: This reduced life limit will be
incorporated within the next revision of the
Airbus A330/A340 ALS Part 1.
Other FAA AD Provisions
(f) The following provisions also apply to
this AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, International
Branch, ANM–116, Transport Airplane
Directorate, FAA, ATTN: Tim Backman,
Aerospace Engineer, 1601 Lind Avenue, SW.,
Renton, Washington 98057–3356, has the
authority to approve AMOCs for this AD, if
requested using the procedures found in 14
CFR 39.19. 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.
(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.
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Corrective actions are considered FAAapproved 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
(g) Refer to MCAI European Aviation
Safety Agency Emergency Airworthiness
Directive 2006–0324–E, dated October 20,
2006; and Airbus All Operators Telex A330–
32A3208, dated October 18, 2006; and Airbus
All Operators Telex A340–32A4252, dated
October 18, 2006, for related information.
Issued in Renton, Washington, on January
12, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E7–1202 Filed 1–25–07; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2006–25419; Directorate
Identifier 2006–NM–055–AD]
RIN 2120–AA64
Airworthiness Directives; Empresa
Brasileira de Aeronautica S.A.
(EMBRAER) Model ERJ 170 Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Supplemental notice of
proposed rulemaking (NPRM);
reopening of comment period.
AGENCY:
SUMMARY: The FAA is revising an earlier
NPRM for an airworthiness directive
(AD) that applies to certain EMBRAER
Model ERJ 170 airplanes. The original
NPRM would have required replacing
the mini-latches on certain lavatory
waste compartment doors with new,
stronger latches, and other specified
actions. The original NPRM resulted
from reports of certain lavatory waste
compartment doors opening during
flight due to movement of the waste
compartment during takeoff, because
the mini-latches installed on the doors
of those compartments lose their
strength over time. This action revises
the original NPRM by adding airplanes
to the applicability. We are proposing
this supplemental NPRM to prevent the
inability of the waste compartment
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3761
doors to adequately contain a fire inside
the lavatory waste compartment, and
consequent uncontained fire and smoke
within a lavatory during flight.
DATES: We must receive comments on
this supplemental NPRM by February
20, 2007.
ADDRESSES: Use one of the following
addresses to submit comments on this
supplemental NPRM.
• DOT Docket Web site: Go to
https://dms.dot.gov and follow the
instructions for sending your comments
electronically.
• Government-wide rulemaking web
site: Go to https://www.regulations.gov
and follow the instructions for sending
your comments electronically.
• Mail: Docket Management Facility;
U.S. Department of Transportation, 400
Seventh Street, SW., Nassif Building,
Room PL–401, Washington, DC 20590.
• Fax: (202) 493–2251.
• Hand Delivery: Room PL–401 on
the plaza level of the Nassif Building,
400 Seventh Street, SW., Washington,
DC, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
Contact Empresa Brasileira de
Aeronautica S.A. (EMBRAER), P.O. Box
343—CEP 12.225, Sao Jose dos
Campos—SP, Brazil, for service
information identified in this proposed
AD.
FOR FURTHER INFORMATION CONTACT:
Todd Thompson, Aerospace Engineer,
International Branch, ANM–116,
Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton,
Washington 98057–3356; telephone
(425) 227–1175; fax (425) 227–1149.
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite you to submit any relevant
written data, views, or arguments
regarding this supplemental NPRM.
Send your comments to an address
listed in the ADDRESSES section. Include
the docket number ‘‘Docket No. FAA–
2006–25419; Directorate Identifier
2006–NM–055–AD’’ at the beginning of
your comments. We specifically invite
comments on the overall regulatory,
economic, environmental, and energy
aspects of this supplemental NPRM. We
will consider all comments received by
the closing date and may amend this
supplemental NPRM in light of those
comments.
We will post all comments submitted,
without change, to https://dms.dot.gov,
including any personal information you
provide. We will also post a report
summarizing each substantive verbal
contact with FAA personnel concerning
this supplemental NPRM. Using the
search function of that Web site, anyone
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can find and read the comments in any
of our dockets, including the name of
the individual who sent the comment
(or signed the comment on behalf of an
association, business, labor union, etc.).
You may review the DOT’s complete
Privacy Act Statement in the Federal
Register published on April 11, 2000
(65 FR 19477–78), or you may visit
https://dms.dot.gov.
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 in the Nassif Building at the DOT
street address stated in ADDRESSES.
Comments will be available in the AD
docket shortly after the Docket
Management System receives them.
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Discussion
We proposed to amend 14 CFR part
39 with a notice of proposed rulemaking
(NPRM) for an airworthiness directive
(AD) (the ‘‘original NPRM’’). The
original NPRM applies to certain
EMBRAER Model ERJ 170 airplanes.
The original NPRM was published in
the Federal Register on July 28, 2006
(71 FR 42776). The original NPRM
proposed to require replacing the minilatches on certain lavatory waste
compartment doors with new, stronger
latches, and other specified actions.
Since we issued the original NPRM,
we have received Revision 01 of
EMBRAER Service Bulletin 170–25–
0024, dated January 9, 2006. The
procedures in EMBRAER Service
Bulletin 170–25–0024, Revision 01, are
essentially identical to those in the
original issue of the service bulletin,
dated July 21, 2005, which we referred
to as the appropriate source of service
information for the proposed latch
replacement in the original NPRM.
EMBRAER issued Revision 01 of the
service bulletin to add airplanes to the
effectivity and to transmit Revision 1 of
C & D Aerospace Service Bulletin 170–
18616–25–023, dated November 29,
2005.
Accomplishing the actions specified
in the service information is intended to
adequately address the unsafe
condition.
Comments
We have considered the following
comments on the original NPRM.
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Request To Make Service Documents
Available to the Public by Incorporation
by Reference and Publication in DMS
The Modification and Replacement
Parts Association (MARPA) requests
that we incorporate by reference the
essential service documents in the
NPRM. MARPA states that ADs are
typically based upon service
information originating with the type
certificate holder or its suppliers.
MARPA asserts that, if a service
document is used as a mandatory
element of compliance, it should not
only be referred to, but also
incorporated into the AD. MARPA adds
that manufacturer’s service documents
are privately authored instruments,
generally having copyright protection
against duplication and distribution.
When a service document is
incorporated by reference into a public
document, such as an AD, pursuant to
5 U.S.C. 552(a) and 1 CFR part 51, it
loses its private, protected status and
becomes a public document. MARPA
notes that the NPRM is one of these
public documents, but does not
incorporate by reference that service
document. Therefore, the NPRM, as
proposed, attempts to require
compliance with a public law by
reference to a private writing. MARPA
believes that public laws, by definition,
should be public and that they cannot
rely on private writings.
We do not agree that documents
should be incorporated by reference
during the NPRM phase of rulemaking.
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. The final rule for this
action will incorporate 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.
MARPA also requests that essential
service documents be published in the
Docket Management System (DMS).
MARPA states that service documents
incorporated by reference should be
made available to the public by
publication in either the Federal
Register or DMS. MARPA also states
that the purpose of the incorporation by
reference method is brevity, to keep
from expanding the Federal Register
needlessly by publishing documents
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already in the hands of the affected
individuals. MARPA adds that,
traditionally, ‘‘affected individuals’’
means aircraft owners and operators,
who are generally provided service
information by the manufacturer.
MARPA further 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.
This new class includes maintenance
and repair organizations, component
servicing and repair shops, parts
purveyors and distributors, and/or
organizations repairing or servicing
alternatively certified parts under
section 21.303 (‘‘Parts Manufacturer
Approval’’) of the Federal Aviation
Regulations (14 CFR 21.303). MARPA
states that the concept of brevity is now
nearly archaic as documents exist more
frequently in electronic format than on
paper.
In regard to the commenter’s request
that service documents be made
available to the public by publication in
the Federal Register, we agree that
incorporation by reference was
authorized to reduce the volume of
material published in the Federal
Register and the Code of Federal
Regulations. However, as specified in
the Federal Register Document Drafting
Handbook, the Director of the Office of
the Federal Register (OFR) decides
when an agency may incorporate
material by reference. As the commenter
is aware, the OFR files documents for
public inspection on the workday before
the date of publication of the rule at its
office in Washington, DC. As stated in
the Federal Register Document Drafting
Handbook, when documents are filed
for public inspection, anyone may
inspect or copy filed documents during
the OFR’s hours of business. Further
questions regarding publication of
documents in the Federal Register or
incorporation by reference should be
directed to the OFR.
In regard to the commenter’s request
to post service bulletins on the
Department of Transportation’s DMS,
we are currently in the process of
reviewing issues surrounding the
posting of service bulletins on DMS as
part of an AD docket. 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. No change to the final rule is
necessary in response to this comment.
Request To Reference Parts
Manufacturer Approval (PMA) Parts
The same commenter, MARPA, also
requests that the language in the NPRM
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be changed to permit installation of
PMA equivalent parts. MARPA asserts
that mandating a certain part-numbered
part to the exclusion of all other parts,
in some cases, prevents installation of
perfectly good parts, while also
prohibiting development of new parts,
‘‘* * * permitted under [14 CFR]
21.303.’’ MARPA further asserts that
this prohibition risks removing the AD
out of the realm of safety and into the
realm of economics, since prohibiting
the development, sale, and use of a
perfectly good part has nothing to do
with safety. MARPA continues, stating
that the NPRM, as written, does not
comply with FAA Order 8040.2, which
allows replacement parts under section
21.303 of the Federal Aviation
Regulations (14 CFR 21.303) based on a
finding of identicality.
MARPA goes on to state that it
believes ‘‘* * * the practice of requiring
an [alternative method of compliance]
AMOC to install a PMA part should be
stopped.’’ It is ‘‘* * * tantamount to
illogically stating that all PMA parts are
inherently defective and that they all
require an additional layer of approval
when the [original equipment
manufacturer] OEM part is determined
to be defective.’’ MARPA further states
that, if the PMA part is deemed
defective, it must be deemed so in the
AD, not simply implied by a ‘‘catch-all
AMOC requirement.’’
In addition, MARPA refers to differing
language used in other ADs addressing
the use of PMA parts and asserts that,
because the NPRM differs in treatment
of PMA parts from other ADs, ‘‘* * *
the mandates contained in Section 1,
paragraph (b)(10) of Executive Order
12866 are not being met.’’ That
paragraph requires that all agencies act
uniformly on a given issue.
The NPRM did not address PMA
parts, as provided in draft FAA Order
8040.2, because the Order was only a
draft that was out for comment at the
time. After issuance of the NPRM, the
Order was revised and issued as FAA
Order 8040.5 with an effective date of
September 29, 2006.
FAA Order 8040.5 does not address
PMA parts in ADs. We acknowledge the
need to ensure that unsafe PMA parts
are identified and addressed in ADs
related to mandatory continuing
airworthiness information (MCAI). We
are currently examining all aspects of
this issue, including input from
industry. Once we have made a final
determination, we will consider how
our policy regarding PMA parts in ADs
needs to be revised. We consider that to
delay this AD action would be
inappropriate, since we have
determined that an unsafe condition
exists and that replacement of certain
parts must be accomplished to ensure
continued safety. Therefore, no change
has been made to the final rule in this
regard.
The FAA recognizes the need for
standardization of this issue and is
currently in the process of reviewing
issues that address the use of PMAs in
ADs at the national level. However, the
Transport Airplane Directorate
considers that to delay this particular
AD action would be inappropriate, since
we have determined that an unsafe
condition exists and that replacement of
certain parts must be accomplished to
ensure continued safety. Therefore, no
change has been made to the final rule
in this regard.
Request To Replace Only the Lavatory
Waste Compartment Latches
EMBRAER requests that we revise
paragraph (f) of the original NPRM to
require replacement of only the latches
for the lavatory waste compartment
door. EMBRAER asserts that only those
latches need to be replaced, because
none of the other doors identified in
EMBRAER Service Bulletin 170–25–
0024, dated July 21, 2005, affect fire
containment, the unsafe condition
addressed by this AD. EMBRAER states
that the wording in paragraph (f) of the
original NPRM, the mandatory
accomplishment of ‘‘* * * all the
actions, except for the forward and aft
lavatory mirror rework, specified in the
Accomplishment Instructions * * *,’’
will require replacement of several
latches that are not associated with the
identified unsafe condition. Therefore
EMBRAER suggests that we identify the
specific paragraphs of the
Accomplishment Instructions of the
service bulletin that need to be done to
replace just the latches for the lavatory
waste compartment.
We agree that only the latches for the
lavatory waste compartment need to be
replaced to address the subject unsafe
condition. Therefore, as EMBRAER
suggests, we have revised paragraph (f)
of this supplemental NPRM to refer to
the specific paragraphs of the
Accomplishment Instructions of the
service bulletin necessary to replace
only the latches for the lavatory waste
compartment door.
FAA’s Determination and Proposed
Requirements of the Supplemental
NPRM
The changes discussed above expand
the scope of the original NPRM;
therefore, we have determined that it is
necessary to reopen the comment period
to provide additional opportunity for
public comment on this supplemental
NPRM.
Costs of Compliance
The following table provides the
estimated costs for U.S. operators to
comply with this proposed AD.
ESTIMATED COSTS
Work hours
Average
labor rate
per hour
Parts
Cost per
airplane
Number of
U.S.-registered
airplanes
Fleet cost
Replacement of lavatory waste compartment door
latches ..........................................................................
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Action
2
$80
$0
$160
75
$12,000
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.
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15:24 Jan 25, 2007
Jkt 211001
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
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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.
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Federal Register / Vol. 72, No. 17 / Friday, January 26, 2007 / Proposed Rules
Regulatory Findings
We have 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 that the 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 supplemental NPRM 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, 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
Authority: 49 U.S.C. 106(g), 40113, 44701.
[Amended]
2. The Federal Aviation
Administration (FAA) amends § 39.13
by adding the following new
airworthiness directive (AD):
Empresa Brasileira De Aeronautica S.A.
(EMBRAER): Docket No. FAA–2006–
25419; Directorate Identifier 2006–NM–
055–AD.
mstockstill on PROD1PC62 with PROPOSALS
Comments Due Date
(a) The FAA must receive comments on
this AD action by February 20, 2007.
Affected ADs
(b) None.
Applicability
(c) This AD applies to EMBRAER Model
ERJ 170–100 LR, –100 STD, –100 SE, –100
SU, –200 LR, –200 STD, and –200 SU
airplanes, certificated in any category; as
identified in EMBRAER Service Bulletin
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15:24 Jan 25, 2007
Jkt 211001
Unsafe Condition
(d) This AD results from reports of certain
lavatory waste compartment doors opening
during flight due to movement of the waste
compartment during takeoff, because the
mini-latches installed on those doors lose
their strength over time. We are issuing this
AD to prevent the inability of the waste
compartment doors to adequately contain a
fire inside the lavatory waste compartment,
and consequent uncontained fire and smoke
within a lavatory during flight.
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.
Replacement of Mini-Latches on Certain
Lavatory Waste Compartment Doors
(f) Within 700 flight hours after the
effective date of this AD: Replace the minilatches for the forward and aft lavatory waste
compartment doors by accomplishing all the
actions, except for the forward and aft
lavatory mirror rework, specified in
paragraphs 3.B. and 3.G. of paragraph 4.,
‘‘Appendix 1,’’ of EMBRAER Service Bulletin
170–25–0024, Revision 01, dated January 9,
2006.
Note 1: EMBRAER Service Bulletin 170–
25–0024, Revision 01, dated January 9, 2006,
refers to C & D Aerospace Service Bulletin
170–18616–25–023, Revision 1, dated
November 29, 2005, as an additional source
of service information for replacing the minilatches on certain lavatory waste
compartment doors required by paragraph (f)
of this AD.
Credit for Actions Done Using Previous Issue
of Service Information
1. The authority citation for part 39
continues to read as follows:
§ 39.13
170–25–0024, Revision 01, dated January 9,
2006.
(g) Replacements done before the effective
date of this AD in accordance with
paragraphs 3.B. and 3.G. of paragraph 4.,
‘‘Appendix 1,’’ of EMBRAER Service Bulletin
170–25–0024, dated July 21, 2005, are
considered acceptable for compliance with
the corresponding action specified in this
AD.
Alternative Methods of Compliance
(AMOCs)
(h)(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.
Related Information
(i) Brazilian airworthiness directive 2005–
11–01, effective December 8, 2005, also
addresses the subject of this AD.
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Issued in Renton, Washington, on January
12, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E7–1215 Filed 1–25–07; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2007–27012; Directorate
Identifier 2006–NM–188–AD]
RIN 2120–AA64
Airworthiness Directives; Airbus Model
A300 B4–601, A300 B4–603, A300 B4–
605R, A300 C4–605R Variant F, A310–
204, A310–304, and A310–308
Airplanes Equipped With General
Electric CF6–80C2 Engines
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
SUMMARY: The FAA proposes to
supersede an existing airworthiness
directive (AD) that applies to certain
Airbus Model A300 B4–600, B4–600R,
C4–605R Variant F, and F4–600R
(collectively called A300–600) series
airplanes; and Model A310 series
airplanes. The existing AD currently
requires a one-time inspection for
damage of the integrated drive generator
(IDG) electrical harness and pyramid
arm, and repair if necessary. This
proposed AD would add new repetitive
inspections, which, when initiated,
would terminate the inspection required
by the existing AD. This proposed AD
would also require repairing damage
and protecting the harness. The
proposed AD would also provide for
optional terminating action for the
repetitive inspections. This proposed
AD also removes certain airplanes from
the applicability of the existing AD.
This proposed AD results from a report
of structural damage on the forward
pyramid arm of an engine pylon due to
chafing of the IDG electrical harness
against the structure of the pyramid
arm. We are proposing this AD to
prevent electrical arcing in the engine
pylon, which could result in loss of the
relevant alternating current (AC) bus
bar, reduced structural integrity of the
engine pylon, and possible loss of
control of the airplane.
DATES: We must receive comments on
this proposed AD by February 26, 2007.
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26JAP1
Agencies
[Federal Register Volume 72, Number 17 (Friday, January 26, 2007)]
[Proposed Rules]
[Pages 3761-3764]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E7-1215]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2006-25419; Directorate Identifier 2006-NM-055-AD]
RIN 2120-AA64
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A.
(EMBRAER) Model ERJ 170 Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Supplemental notice of proposed rulemaking (NPRM); reopening of
comment period.
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SUMMARY: The FAA is revising an earlier NPRM for an airworthiness
directive (AD) that applies to certain EMBRAER Model ERJ 170 airplanes.
The original NPRM would have required replacing the mini-latches on
certain lavatory waste compartment doors with new, stronger latches,
and other specified actions. The original NPRM resulted from reports of
certain lavatory waste compartment doors opening during flight due to
movement of the waste compartment during takeoff, because the mini-
latches installed on the doors of those compartments lose their
strength over time. This action revises the original NPRM by adding
airplanes to the applicability. We are proposing this supplemental NPRM
to prevent the inability of the waste compartment doors to adequately
contain a fire inside the lavatory waste compartment, and consequent
uncontained fire and smoke within a lavatory during flight.
DATES: We must receive comments on this supplemental NPRM by February
20, 2007.
ADDRESSES: Use one of the following addresses to submit comments on
this supplemental NPRM.
DOT Docket Web site: Go to https://dms.dot.gov and follow
the instructions for sending your comments electronically.
Government-wide rulemaking web site: Go to https://
www.regulations.gov and follow the instructions for sending your
comments electronically.
Mail: Docket Management Facility; U.S. Department of
Transportation, 400 Seventh Street, SW., Nassif Building, Room PL-401,
Washington, DC 20590.
Fax: (202) 493-2251.
Hand Delivery: Room PL-401 on the plaza level of the
Nassif Building, 400 Seventh Street, SW., Washington, DC, between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
Contact Empresa Brasileira de Aeronautica S.A. (EMBRAER), P.O. Box
343--CEP 12.225, Sao Jose dos Campos--SP, Brazil, for service
information identified in this proposed AD.
FOR FURTHER INFORMATION CONTACT: Todd Thompson, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425)
227-1175; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite you to submit any relevant written data, views, or
arguments regarding this supplemental NPRM. Send your comments to an
address listed in the ADDRESSES section. Include the docket number
``Docket No. FAA-2006-25419; Directorate Identifier 2006-NM-055-AD'' at
the beginning of your comments. We specifically invite comments on the
overall regulatory, economic, environmental, and energy aspects of this
supplemental NPRM. We will consider all comments received by the
closing date and may amend this supplemental NPRM in light of those
comments.
We will post all comments submitted, without change, to https://
dms.dot.gov, including any personal information you provide. We will
also post a report summarizing each substantive verbal contact with FAA
personnel concerning this supplemental NPRM. Using the search function
of that Web site, anyone
[[Page 3762]]
can find and read the comments in any of our dockets, including the
name of the individual who sent the comment (or signed the comment on
behalf of an association, business, labor union, etc.). You may review
the DOT's complete Privacy Act Statement in the Federal Register
published on April 11, 2000 (65 FR 19477-78), or you may visit https://
dms.dot.gov.
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 in the Nassif Building at the DOT
street address stated in ADDRESSES. Comments will be available in the
AD docket shortly after the Docket Management System receives them.
Discussion
We proposed to amend 14 CFR part 39 with a notice of proposed
rulemaking (NPRM) for an airworthiness directive (AD) (the ``original
NPRM''). The original NPRM applies to certain EMBRAER Model ERJ 170
airplanes. The original NPRM was published in the Federal Register on
July 28, 2006 (71 FR 42776). The original NPRM proposed to require
replacing the mini-latches on certain lavatory waste compartment doors
with new, stronger latches, and other specified actions.
Since we issued the original NPRM, we have received Revision 01 of
EMBRAER Service Bulletin 170-25-0024, dated January 9, 2006. The
procedures in EMBRAER Service Bulletin 170-25-0024, Revision 01, are
essentially identical to those in the original issue of the service
bulletin, dated July 21, 2005, which we referred to as the appropriate
source of service information for the proposed latch replacement in the
original NPRM. EMBRAER issued Revision 01 of the service bulletin to
add airplanes to the effectivity and to transmit Revision 1 of C & D
Aerospace Service Bulletin 170-18616-25-023, dated November 29, 2005.
Accomplishing the actions specified in the service information is
intended to adequately address the unsafe condition.
Comments
We have considered the following comments on the original NPRM.
Request To Make Service Documents Available to the Public by
Incorporation by Reference and Publication in DMS
The Modification and Replacement Parts Association (MARPA) requests
that we incorporate by reference the essential service documents in the
NPRM. MARPA states that ADs are typically based upon service
information originating with the type certificate holder or its
suppliers. MARPA asserts that, if a service document is used as a
mandatory element of compliance, it should not only be referred to, but
also incorporated into the AD. MARPA adds that manufacturer's service
documents are privately authored instruments, generally having
copyright protection against duplication and distribution. When a
service document is incorporated by reference into a public document,
such as an AD, pursuant to 5 U.S.C. 552(a) and 1 CFR part 51, it loses
its private, protected status and becomes a public document. MARPA
notes that the NPRM is one of these public documents, but does not
incorporate by reference that service document. Therefore, the NPRM, as
proposed, attempts to require compliance with a public law by reference
to a private writing. MARPA believes that public laws, by definition,
should be public and that they cannot rely on private writings.
We do not agree that documents should be incorporated by reference
during the NPRM phase of rulemaking. 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. The final rule for this action will
incorporate 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.
MARPA also requests that essential service documents be published
in the Docket Management System (DMS). MARPA states that service
documents incorporated by reference should be made available to the
public by publication in either the Federal Register or DMS. MARPA also
states that the 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.
MARPA adds that, traditionally, ``affected individuals'' means aircraft
owners and operators, who are generally provided service information by
the manufacturer. MARPA further 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. This new class includes maintenance and repair
organizations, component servicing and repair shops, parts purveyors
and distributors, and/or organizations repairing or servicing
alternatively certified parts under section 21.303 (``Parts
Manufacturer Approval'') of the Federal Aviation Regulations (14 CFR
21.303). MARPA states that the concept of brevity is now nearly archaic
as documents exist more frequently in electronic format than on paper.
In regard to the commenter's request that service documents be made
available to the public by publication in the Federal Register, we
agree that incorporation by reference was authorized to reduce the
volume of material published in the Federal Register and the Code of
Federal Regulations. However, as specified in the Federal Register
Document Drafting Handbook, the Director of the Office of the Federal
Register (OFR) decides when an agency may incorporate material by
reference. As the commenter is aware, the OFR files documents for
public inspection on the workday before the date of publication of the
rule at its office in Washington, DC. As stated in the Federal Register
Document Drafting Handbook, when documents are filed for public
inspection, anyone may inspect or copy filed documents during the OFR's
hours of business. Further questions regarding publication of documents
in the Federal Register or incorporation by reference should be
directed to the OFR.
In regard to the commenter's request to post service bulletins on
the Department of Transportation's DMS, we are currently in the process
of reviewing issues surrounding the posting of service bulletins on DMS
as part of an AD docket. 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. No change to the
final rule is necessary in response to this comment.
Request To Reference Parts Manufacturer Approval (PMA) Parts
The same commenter, MARPA, also requests that the language in the
NPRM
[[Page 3763]]
be changed to permit installation of PMA equivalent parts. MARPA
asserts that mandating a certain part-numbered part to the exclusion of
all other parts, in some cases, prevents installation of perfectly good
parts, while also prohibiting development of new parts, ``* * *
permitted under [14 CFR] 21.303.'' MARPA further asserts that this
prohibition risks removing the AD out of the realm of safety and into
the realm of economics, since prohibiting the development, sale, and
use of a perfectly good part has nothing to do with safety. MARPA
continues, stating that the NPRM, as written, does not comply with FAA
Order 8040.2, which allows replacement parts under section 21.303 of
the Federal Aviation Regulations (14 CFR 21.303) based on a finding of
identicality.
MARPA goes on to state that it believes ``* * * the practice of
requiring an [alternative method of compliance] AMOC to install a PMA
part should be stopped.'' It is ``* * * tantamount to illogically
stating that all PMA parts are inherently defective and that they all
require an additional layer of approval when the [original equipment
manufacturer] OEM part is determined to be defective.'' MARPA further
states that, if the PMA part is deemed defective, it must be deemed so
in the AD, not simply implied by a ``catch-all AMOC requirement.''
In addition, MARPA refers to differing language used in other ADs
addressing the use of PMA parts and asserts that, because the NPRM
differs in treatment of PMA parts from other ADs, ``* * * the mandates
contained in Section 1, paragraph (b)(10) of Executive Order 12866 are
not being met.'' That paragraph requires that all agencies act
uniformly on a given issue.
The NPRM did not address PMA parts, as provided in draft FAA Order
8040.2, because the Order was only a draft that was out for comment at
the time. After issuance of the NPRM, the Order was revised and issued
as FAA Order 8040.5 with an effective date of September 29, 2006.
FAA Order 8040.5 does not address PMA parts in ADs. We acknowledge
the need to ensure that unsafe PMA parts are identified and addressed
in ADs related to mandatory continuing airworthiness information
(MCAI). We are currently examining all aspects of this issue, including
input from industry. Once we have made a final determination, we will
consider how our policy regarding PMA parts in ADs needs to be revised.
We consider that to delay this AD action would be inappropriate, since
we have determined that an unsafe condition exists and that replacement
of certain parts must be accomplished to ensure continued safety.
Therefore, no change has been made to the final rule in this regard.
The FAA recognizes the need for standardization of this issue and
is currently in the process of reviewing issues that address the use of
PMAs in ADs at the national level. However, the Transport Airplane
Directorate considers that to delay this particular AD action would be
inappropriate, since we have determined that an unsafe condition exists
and that replacement of certain parts must be accomplished to ensure
continued safety. Therefore, no change has been made to the final rule
in this regard.
Request To Replace Only the Lavatory Waste Compartment Latches
EMBRAER requests that we revise paragraph (f) of the original NPRM
to require replacement of only the latches for the lavatory waste
compartment door. EMBRAER asserts that only those latches need to be
replaced, because none of the other doors identified in EMBRAER Service
Bulletin 170-25-0024, dated July 21, 2005, affect fire containment, the
unsafe condition addressed by this AD. EMBRAER states that the wording
in paragraph (f) of the original NPRM, the mandatory accomplishment of
``* * * all the actions, except for the forward and aft lavatory mirror
rework, specified in the Accomplishment Instructions * * *,'' will
require replacement of several latches that are not associated with the
identified unsafe condition. Therefore EMBRAER suggests that we
identify the specific paragraphs of the Accomplishment Instructions of
the service bulletin that need to be done to replace just the latches
for the lavatory waste compartment.
We agree that only the latches for the lavatory waste compartment
need to be replaced to address the subject unsafe condition. Therefore,
as EMBRAER suggests, we have revised paragraph (f) of this supplemental
NPRM to refer to the specific paragraphs of the Accomplishment
Instructions of the service bulletin necessary to replace only the
latches for the lavatory waste compartment door.
FAA's Determination and Proposed Requirements of the Supplemental NPRM
The changes discussed above expand the scope of the original NPRM;
therefore, we have determined that it is necessary to reopen the
comment period to provide additional opportunity for public comment on
this supplemental NPRM.
Costs of Compliance
The following table provides the estimated costs for U.S. operators
to comply with this proposed AD.
Estimated Costs
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Number of
Average Cost per U.S.-
Action Work hours labor rate Parts airplane registered Fleet cost
per hour airplanes
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Replacement of lavatory 2 $80 $0 $160 75 $12,000
waste compartment door
latches....................
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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, ``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.
[[Page 3764]]
Regulatory Findings
We have 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 that the 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 supplemental NPRM 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, 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 Federal Aviation Administration (FAA) amends Sec. 39.13 by
adding the following new airworthiness directive (AD):
Empresa Brasileira De Aeronautica S.A. (EMBRAER): Docket No. FAA-
2006-25419; Directorate Identifier 2006-NM-055-AD.
Comments Due Date
(a) The FAA must receive comments on this AD action by February
20, 2007.
Affected ADs
(b) None.
Applicability
(c) This AD applies to EMBRAER Model ERJ 170-100 LR, -100 STD, -
100 SE, -100 SU, -200 LR, -200 STD, and -200 SU airplanes,
certificated in any category; as identified in EMBRAER Service
Bulletin 170-25-0024, Revision 01, dated January 9, 2006.
Unsafe Condition
(d) This AD results from reports of certain lavatory waste
compartment doors opening during flight due to movement of the waste
compartment during takeoff, because the mini-latches installed on
those doors lose their strength over time. We are issuing this AD to
prevent the inability of the waste compartment doors to adequately
contain a fire inside the lavatory waste compartment, and consequent
uncontained fire and smoke within a lavatory during flight.
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.
Replacement of Mini-Latches on Certain Lavatory Waste Compartment Doors
(f) Within 700 flight hours after the effective date of this AD:
Replace the mini-latches for the forward and aft lavatory waste
compartment doors by accomplishing all the actions, except for the
forward and aft lavatory mirror rework, specified in paragraphs 3.B.
and 3.G. of paragraph 4., ``Appendix 1,'' of EMBRAER Service
Bulletin 170-25-0024, Revision 01, dated January 9, 2006.
Note 1: EMBRAER Service Bulletin 170-25-0024, Revision 01, dated
January 9, 2006, refers to C & D Aerospace Service Bulletin 170-
18616-25-023, Revision 1, dated November 29, 2005, as an additional
source of service information for replacing the mini-latches on
certain lavatory waste compartment doors required by paragraph (f)
of this AD.
Credit for Actions Done Using Previous Issue of Service Information
(g) Replacements done before the effective date of this AD in
accordance with paragraphs 3.B. and 3.G. of paragraph 4., ``Appendix
1,'' of EMBRAER Service Bulletin 170-25-0024, dated July 21, 2005,
are considered acceptable for compliance with the corresponding
action specified in this AD.
Alternative Methods of Compliance (AMOCs)
(h)(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
(i) Brazilian airworthiness directive 2005-11-01, effective
December 8, 2005, also addresses the subject of this AD.
Issued in Renton, Washington, on January 12, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E7-1215 Filed 1-25-07; 8:45 am]
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