Airworthiness Directives; The Boeing Company Airplanes, 41045-41047 [2012-15893]
Download as PDF
Federal Register / Vol. 77, No. 134 / Thursday, July 12, 2012 / Rules and Regulations
Accomplishment Instructions of Boeing
Service Bulletin 747–30–2081, Revision 3,
dated December 5, 2011, and repeat the
detailed inspection thereafter at the
applicable intervals specified in paragraph
(g)(1) or (g)(2) of this AD. Doing the
replacement specified in paragraph (j) of this
AD terminates the repetitive inspection
requirements of this paragraph for the
replaced flightdeck window 1.
(i) Window 1 Conditional Replacement
If, during the inspection required by
paragraph (g) or (h) of this AD, a screw is
found crossthreaded, do the applicable
corrective actions specified in paragraph
(i)(1) or (i)(2) of this AD.
(1) If the connector is loose and cannot be
tightened by applying the correct torque,
before further flight, replace that window 1
in accordance with the Accomplishment
Instructions of Boeing Service Bulletin 747–
30–2081, Revision 3, dated December 5,
2011.
(2) If the connector is tight or can be
tightened by applying the correct torque,
replace that window 1 within 500 flight
hours after the inspection, in accordance
with the Accomplishment Instructions of
Boeing Service Bulletin 747–30–2081,
Revision 3, dated December 5, 2011.
(j) Optional Terminating Action
Replacing a flightdeck window 1 that uses
screw and connector for the electrical heat
connection with a flightdeck window 1 that
uses pin and socket for the electrical
connection, in accordance with Work
Package 3 or 4 of the Accomplishment
Instructions of Boeing Service Bulletin 747–
30–2081, Revision 3, dated December 5,
2011, ends the repetitive inspection
requirements of this AD for that window 1
only.
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(k) Credit for Previous Actions
This paragraph provides credit for the
inspections and corrective actions required
by this AD, and for the window replacement
specified in paragraph (j) of this AD for the
replaced window 1 only, if the corresponding
actions were performed before the effective
date of this AD using the service information
identified in paragraph (k)(1), (k)(2), or (k)(3)
of this AD.
(1) Boeing Special Attention Service
Bulletin 747–30–2081, dated August 8, 2006.
(2) Boeing Special Attention Service
Bulletin 747–30–2081, Revision 1, dated
August 20, 2008.
(3) Boeing Special Attention Service
Bulletin 747–30–2081, Revision 2, dated
March 10, 2010.
(l) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, Seattle Aircraft
Certification Office (ACO), FAA, has the
authority to approve AMOCs for this AD, if
requested using the procedures found in 14
CFR 39.19. In accordance with 14 CFR 39.19,
send your request to your principal inspector
or local Flight Standards District Office, as
appropriate. If sending information directly
to the manager of the ACO, send it to the
attention of the person identified in the
Related Information section of this AD.
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Information may be emailed to: 9-ANMSeattle-ACO-AMOC-Requests@faa.gov.
(2) Before using any approved AMOC,
notify your Principal Maintenance Inspector
or Principal Avionics Inspector, as
appropriate, or lacking a principal inspector,
your local Flight Standards District Office.
(m) Related Information
For more information about this AD,
contact Louis Natsiopoulos, Aerospace
Engineer, Systems and Equipment Branch,
ANM–130S, FAA, Seattle Aircraft
Certification Office, 1601 Lind Avenue SW.,
Renton, Washington 98057–3356; phone:
425–917–6478; fax: 425–917–6590; email:
Elias.Natsiopoulos@faa.gov.
(n) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) of the following service information
under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use the following service
information to do the actions required by this
AD, unless the AD specifies otherwise.
(i) Boeing Service Bulletin 747–30–2081,
Revision 3, dated December 5, 2011.
(3) For service information identified in
this AD, contact Boeing Commercial
Airplanes, Attention: Data & Services
Management, P.O. Box 3707, MC 2H–65,
Seattle, Washington 98124–2207; telephone
206–544–5000, extension 1; fax 206–766–
5680; Internet https://
www.myboeingfleet.com.
(4) You may review copies of the service
information at the FAA, Transport Airplane
Directorate, 1601 Lind Avenue SW., Renton,
Washington. For information on the
availability of this material at the FAA, call
425–227–1221.
(5) You may also review copies of the
service information that is incorporated by
reference at the National Archives and
Records Administration (NARA). For
information on the availability of this
material at NARA, call 202–741–6030, or go
to: https://www.archives.gov/federal-register/
cfr/ibr-locations.html.
Issued in Renton, Washington, on June 27,
2012.
Kalene C. Yanamura,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 2012–16333 Filed 7–11–12; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2012–0104; Directorate
Identifier 2011–NM–279–AD; Amendment
39–17107; AD 2012–13–05]
RIN 2120–AA64
Airworthiness Directives; The Boeing
Company Airplanes
Federal Aviation
Administration (FAA), DOT.
AGENCY:
PO 00000
Frm 00005
Fmt 4700
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ACTION:
41045
Final rule.
We are adopting a new
airworthiness directive (AD) for certain
The Boeing Company Model 777–200,
–200LR, –300, –300ER, and 777F series
airplanes. This AD was prompted by a
report indicating that a fire originated
near the first officer’s area, which
caused extensive damage to the flight
deck. This AD requires replacing the
low-pressure oxygen hoses with nonconductive low-pressure oxygen hoses
in the flight compartment. We are
issuing this AD to prevent electrical
current from passing through the lowpressure oxygen hose internal anticollapse spring, which can cause the
low-pressure oxygen hose to melt or
burn, and a consequent oxygen-fed fire
in the flight compartment.
DATES: This AD is effective August 16,
2012.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in the AD
as of August 16, 2012.
ADDRESSES: For service information
identified in this AD, contact Boeing
Commercial Airplanes, Attention: Data
& Services Management, P.O. Box 3707,
MC 2H–65, Seattle, Washington 98124–
2207; telephone 206–544–5000,
extension 1; fax 206–766–5680; Internet
https://www.myboeingfleet.com. You
may review copies of the referenced
service information at the FAA,
Transport Airplane Directorate, 1601
Lind Avenue SW., Renton, WA 98057–
3356. For information on the availability
of this material at the FAA, call (425)
227–1221.
SUMMARY:
Examining the AD Docket
You may examine the AD docket on
the Internet at https://
www.regulations.gov; or in person at the
Docket Management Facility between 9
a.m. and 5 p.m., Monday through
Friday, except Federal holidays. The AD
docket contains this AD, the regulatory
evaluation, any comments received, and
other information. The address for the
Docket Office (phone: 800–647–5527) is
Document Management Facility, U.S.
Department of Transportation, Docket
Operations, M–30, West Building
Ground Floor, Room W12–140, 1200
New Jersey Avenue SE., Washington,
DC 20590.
FOR FURTHER INFORMATION CONTACT:
Susan Monroe, Aerospace Engineer,
Cabin Safety and Environmental
Systems Branch, ANM–150S, FAA,
Seattle Aircraft Certification Office,
1601 Lind Avenue SW., Renton, WA
98057–3356; phone: 425–917–6457; fax:
425–917–6590; email:
susan.l.monroe@faa.gov.
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41046
Federal Register / Vol. 77, No. 134 / Thursday, July 12, 2012 / Rules and Regulations
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would
apply to the specified products. That
NPRM published in the Federal
Register on February 8, 2012 (77 FR
6518). That NPRM proposed to require
replacing the low-pressure oxygen hoses
with non-conductive low-pressure
oxygen hoses in the flight compartment.
Relevant Service Information
Since we issued the NPRM (77 FR
6518, February 8, 2012), Boeing has
issued Alert Service Bulletin 777–
35A0027, Revision 1, dated April 19,
2012. This service information was
issued to remove airplanes from the
effectivity that have had certain changes
incorporated in production, update
warranty information, and material
price information. No additional work is
necessary for airplanes changed in
accordance with Boeing Alert Service
Bulletin 777–35A0027, dated December
15, 2011. We have changed the final
rule to reference Boeing Alert Service
Bulletin 777–35A0027, Revision 1,
dated April 19, 2012. Additionally, we
have updated the Costs of Compliance
section of the final rule regarding the
parts cost and warranty information.
Comments
We gave the public the opportunity to
participate in developing this AD. The
following presents the comments
received on the proposal (77 FR 6518,
February 8, 2012) and the FAA’s
response to each comment.
Support for the NPRM (77 FR 6518,
February 8, 2012)
The Air Line Pilots Association
(ALPA) stated it supports the NPRM (77
FR 6518, February 8, 2012).
pmangrum on DSK3VPTVN1PROD with RULES
Request To Shorten Compliance Time
The ALPA requested we shorten the
compliance time for the replacement of
the oxygen hoses from 18 months to 12
months. The commenter based this
request on the impact that an oxygen fed
fire on the flight deck would have on
flight safety.
We disagree. In developing the
proposed compliance time, we
considered the safety implications, parts
availability, and normal maintenance
schedules for the timely
accomplishment of replacement of the
oxygen hoses. Further, the proposed
compliance time is in keeping with the
manufacturers’ recommended
compliance time. In consideration of all
these factors, operators are always
permitted to accomplish the
requirements of an AD at a time earlier
than the specified compliance time. If
additional data are presented that would
justify a shorter compliance time, we
may consider further rulemaking on this
issue. We have not changed the AD in
this regard.
Request To Increase Compliance Time
United Airlines requested we increase
the compliance time for the replacement
of the oxygen hoses from 18 months to
24 months. The commenter stated that
based on parts availability and its
normal maintenance schedule, it
believes that 24 months would be an
appropriate interval for the timely
accomplishment of the actions while
maintaining an adequate level of safety.
We disagree with increasing the
compliance time. As stated previously,
in developing the proposed compliance
time, we considered the safety
implications, parts availability, and
normal maintenance schedules for a
timely accomplishment of replacement
of the oxygen hoses. Further, the
proposed compliance time is in keeping
with the manufacturers’ recommended
compliance time. However, under the
provisions of paragraph (i) of the final
rule, we may approve requests for
adjustments to the compliance time if
data are submitted to substantiate that
such an adjustment would provide an
acceptable level of safety. We have not
changed the AD in this regard.
Request To Add Applicability Language
Boeing requested that we add
language to paragraph (h) of the NPRM
(77 FR 6518, February 8, 2012), stating
that this paragraph applies only to any
airplane ‘‘affected by this AD.’’
We do not agree with the commenter’s
request. The applicability statement in
all AD actions lists all airplanes affected
by that AD. All of the requirements
stated in an AD are applicable only to
the airplanes listed in the applicability.
We find no justification for making the
requested change. We have not changed
the AD in this regard.
Request for Clarification of Parts
Installation Requirement
American Airlines (American)
requested clarification of the
requirement in paragraph (h) of the
NPRM (77 FR 6518, February 8, 2012)
that prohibits installing certain oxygen
hoses after the effective date of the AD.
American stated that the compliance
time of paragraph (h) of the NPRM is
prior to the compliance date of the lowpressure oxygen hose removal, and if a
maintenance procedure is accomplished
which would require the removal of the
low-pressure oxygen hose, the same
low-pressure oxygen hose cannot be reinstalled.
We agree to clarify the requirement.
Once we have determined that an
unsafe condition exists, we generally
specify not to allow that condition to be
introduced into the fleet. Although the
word ‘‘install’’ is generally considered
to be broader than the word ‘‘replace,’’
for this AD operators can interpret it as
meaning ‘‘replace’’ while remaining
within the intent of the ‘‘Parts
Installation’’ paragraph (paragraph (h) of
this AD). By simply reinstalling a part
removed during maintenance, the
operator is not ‘‘installing’’ a different
part. Therefore, removing a part to gain
access and then reinstalling that same
part for other maintenance activities not
associated with the AD is acceptable.
We have not changed the AD in this
regard.
Conclusion
We reviewed the relevant data,
considered the comments received, and
determined that air safety and the
public interest require adopting the AD
with the changes described previously.
We also determined that these
changes will not increase the economic
burden on any operator or increase the
scope of the AD.
Costs of Compliance
We estimate that this AD affects 169
airplanes of U.S. registry.
We estimate the following costs to
comply with this AD:
ESTIMATED COSTS
Action
Labor cost
Parts cost
Cost per
product
Cost on U.S.
operators
Replacement ...................................................
18 work-hours × $85 per hour = $1,530 ........
$1,066
$2,596
$438,724
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Federal Register / Vol. 77, No. 134 / Thursday, July 12, 2012 / Rules and Regulations
According to the manufacturer, some
of the costs of this AD may be covered
under warranty, thereby reducing the
cost impact on affected individuals. We
do not control warranty coverage for
affected individuals. As a result, we
have included all costs in our cost
estimate.
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive (AD):
■
Authority for This Rulemaking
Title 49 of the United States Code
specifies the FAA’s authority to issue
rules on aviation safety. Subtitle I,
section 106, describes the authority of
the FAA Administrator. Subtitle VII:
Aviation Programs, describes in more
detail the scope of the Agency’s
authority.
We are issuing this rulemaking under
the authority described in Subtitle VII,
Part A, Subpart III, Section 44701:
‘‘General requirements.’’ Under that
section, Congress charges the FAA with
promoting safe flight of civil aircraft in
air commerce by prescribing regulations
for practices, methods, and procedures
the Administrator finds necessary for
safety in air commerce. This regulation
is within the scope of that authority
because it addresses an unsafe condition
that is likely to exist or develop on
products identified in this rulemaking
action.
Regulatory Findings
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),
(3) Will not affect intrastate aviation
in Alaska, and
(4) 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.
2012–13–05 The Boeing Company:
Amendment 39–17107; Docket No.
FAA–2012–0104; Directorate Identifier
2011–NM–279–AD.
(a) Effective Date
This AD is effective August 16, 2012.
(b) Affected ADs
None.
(c) Applicability
This AD applies to The Boeing Company
Model 777–200, –200LR, –300, –300ER, and
777F series airplanes; certificated in any
category; as identified in Boeing Alert
Service Bulletin 777–35A0027, Revision 1,
dated April 19, 2012.
(d) Subject
Joint Aircraft System Component (JASC)/
Air Transport Association (ATA) of America
Code 35, Oxygen.
(e) Unsafe Condition
This AD was prompted by a report
indicating that a fire originated near the first
officer’s area, which caused extensive
damage to the flight deck. We are issuing this
AD to prevent electrical current from passing
through the low-pressure oxygen hose
internal anti-collapse spring, which can
cause the low-pressure oxygen hose to melt
or burn, and a consequent oxygen-fed fire in
the flight compartment.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Replacement
Within 18 months after the effective date
of this AD: Replace the low-pressure oxygen
hoses with non-conductive low-pressure
oxygen hoses in the flight compartment, in
accordance with the Accomplishment
Instructions of Boeing Alert Service Bulletin
777–35A0027, dated December 15, 2011, or
Boeing Alert Service Bulletin 777–35A0027,
Revision 1, dated April 19, 2012.
Adoption of the Amendment
(h) Parts Installation Prohibition
As of the effective date of this AD, no
person may install in the airplane flight
compartment oxygen system on any airplane,
a low-pressure oxygen hose having part
number 57034–81220, 57034–81320, or
57034–91100.
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
(i) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, Seattle Aircraft
Certification Office (ACO), FAA, has the
List of Subjects in 14 CFR Part 39
pmangrum on DSK3VPTVN1PROD with RULES
PART 39—AIRWORTHINESS
DIRECTIVES
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
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41047
authority to approve AMOCs for this AD, if
requested using the procedures found in 14
CFR 39.19. In accordance with 14 CFR 39.19,
send your request to your principal inspector
or local Flight Standards District Office, as
appropriate. If sending information directly
to the manager of the ACO, send it to the
attention of the person identified in the
Related Information section of this AD.
Information may be emailed to: 9-ANMSeattle-ACO-AMOC-Requests@faa.gov.
(2) Before using any approved AMOC,
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
of the local flight standards district office/
certificate holding district office.
(j) Related Information
For more information about this AD,
contact Susan Monroe, Aerospace Engineer,
Cabin Safety and Environmental Systems
Branch, ANM–150S, FAA, Seattle Aircraft
Certification Office, 1601 Lind Avenue SW.,
Renton, WA 98057–3356; phone: (425) 917–
6457; fax: (425) 917–6590; email:
susan.l.monroe@faa.gov.
(k) Material Incorporated by Reference
(1) You must use the following service
information to do the actions required by this
AD, unless the AD specifies otherwise. The
Director of the Federal Register approved the
incorporation by reference (IBR) of the
following service information under 5 U.S.C.
552(a) and 1 CFR part 51.
(i) Boeing Alert Service Bulletin 777–
35A0027, dated December 15, 2011.
(ii) Boeing Alert Service Bulletin 777–
35A0027, Revision 1, dated April 19, 2012.
(2) For service information identified in
this AD, Boeing Commercial Airplanes,
Attention: Data & Services Management, P.O.
Box 3707, MC 2H–65, Seattle, Washington
98124–2207; telephone 206–544–5000,
extension 1; fax 206–766–5680; Internet
https://www.myboeingfleet.com.
(3) You may review copies of the
referenced service information at the FAA,
Transport Airplane Directorate, 1601 Lind
Avenue SW., Renton, WA 98057–3356. For
information on the availability of this
material at the FAA, call (425) 227–1221.
(4) You may also review copies of the
service information that is incorporated by
reference at the National Archives and
Records Administration (NARA). For
information on the availability of this
material at NARA, call 202–741–6030, or go
to: https://www.archives.gov/federal-register/
cfr/ibr-locations.html.
Issued in Renton, Washington, on June 21,
2012.
John Piccola,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 2012–15893 Filed 7–11–12; 8:45 am]
BILLING CODE 4910–13–P
E:\FR\FM\12JYR1.SGM
12JYR1
Agencies
[Federal Register Volume 77, Number 134 (Thursday, July 12, 2012)]
[Rules and Regulations]
[Pages 41045-41047]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2012-15893]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2012-0104; Directorate Identifier 2011-NM-279-AD;
Amendment 39-17107; AD 2012-13-05]
RIN 2120-AA64
Airworthiness Directives; The Boeing Company Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for certain
The Boeing Company Model 777-200, -200LR, -300, -300ER, and 777F series
airplanes. This AD was prompted by a report indicating that a fire
originated near the first officer's area, which caused extensive damage
to the flight deck. This AD requires replacing the low-pressure oxygen
hoses with non-conductive low-pressure oxygen hoses in the flight
compartment. We are issuing this AD to prevent electrical current from
passing through the low-pressure oxygen hose internal anti-collapse
spring, which can cause the low-pressure oxygen hose to melt or burn,
and a consequent oxygen-fed fire in the flight compartment.
DATES: This AD is effective August 16, 2012.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in the AD as of August 16,
2012.
ADDRESSES: For service information identified in this AD, contact
Boeing Commercial Airplanes, Attention: Data & Services Management,
P.O. Box 3707, MC 2H-65, Seattle, Washington 98124-2207; telephone 206-
544-5000, extension 1; fax 206-766-5680; Internet https://www.myboeingfleet.com. You may review copies of the referenced service
information at the FAA, Transport Airplane Directorate, 1601 Lind
Avenue SW., Renton, WA 98057-3356. For information on the availability
of this material at the FAA, call (425) 227-1221.
Examining the AD Docket
You may examine the AD docket on the Internet at https://www.regulations.gov; or in person at the Docket Management Facility
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains this AD, the regulatory evaluation,
any comments received, and other information. The address for the
Docket Office (phone: 800-647-5527) is Document Management Facility,
U.S. Department of Transportation, Docket Operations, M-30, West
Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE.,
Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Susan Monroe, Aerospace Engineer,
Cabin Safety and Environmental Systems Branch, ANM-150S, FAA, Seattle
Aircraft Certification Office, 1601 Lind Avenue SW., Renton, WA 98057-
3356; phone: 425-917-6457; fax: 425-917-6590; email:
susan.l.monroe@faa.gov.
[[Page 41046]]
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would apply to the specified products.
That NPRM published in the Federal Register on February 8, 2012 (77 FR
6518). That NPRM proposed to require replacing the low-pressure oxygen
hoses with non-conductive low-pressure oxygen hoses in the flight
compartment.
Relevant Service Information
Since we issued the NPRM (77 FR 6518, February 8, 2012), Boeing has
issued Alert Service Bulletin 777-35A0027, Revision 1, dated April 19,
2012. This service information was issued to remove airplanes from the
effectivity that have had certain changes incorporated in production,
update warranty information, and material price information. No
additional work is necessary for airplanes changed in accordance with
Boeing Alert Service Bulletin 777-35A0027, dated December 15, 2011. We
have changed the final rule to reference Boeing Alert Service Bulletin
777-35A0027, Revision 1, dated April 19, 2012. Additionally, we have
updated the Costs of Compliance section of the final rule regarding the
parts cost and warranty information.
Comments
We gave the public the opportunity to participate in developing
this AD. The following presents the comments received on the proposal
(77 FR 6518, February 8, 2012) and the FAA's response to each comment.
Support for the NPRM (77 FR 6518, February 8, 2012)
The Air Line Pilots Association (ALPA) stated it supports the NPRM
(77 FR 6518, February 8, 2012).
Request To Shorten Compliance Time
The ALPA requested we shorten the compliance time for the
replacement of the oxygen hoses from 18 months to 12 months. The
commenter based this request on the impact that an oxygen fed fire on
the flight deck would have on flight safety.
We disagree. In developing the proposed compliance time, we
considered the safety implications, parts availability, and normal
maintenance schedules for the timely accomplishment of replacement of
the oxygen hoses. Further, the proposed compliance time is in keeping
with the manufacturers' recommended compliance time. In consideration
of all these factors, operators are always permitted to accomplish the
requirements of an AD at a time earlier than the specified compliance
time. If additional data are presented that would justify a shorter
compliance time, we may consider further rulemaking on this issue. We
have not changed the AD in this regard.
Request To Increase Compliance Time
United Airlines requested we increase the compliance time for the
replacement of the oxygen hoses from 18 months to 24 months. The
commenter stated that based on parts availability and its normal
maintenance schedule, it believes that 24 months would be an
appropriate interval for the timely accomplishment of the actions while
maintaining an adequate level of safety.
We disagree with increasing the compliance time. As stated
previously, in developing the proposed compliance time, we considered
the safety implications, parts availability, and normal maintenance
schedules for a timely accomplishment of replacement of the oxygen
hoses. Further, the proposed compliance time is in keeping with the
manufacturers' recommended compliance time. However, under the
provisions of paragraph (i) of the final rule, we may approve requests
for adjustments to the compliance time if data are submitted to
substantiate that such an adjustment would provide an acceptable level
of safety. We have not changed the AD in this regard.
Request To Add Applicability Language
Boeing requested that we add language to paragraph (h) of the NPRM
(77 FR 6518, February 8, 2012), stating that this paragraph applies
only to any airplane ``affected by this AD.''
We do not agree with the commenter's request. The applicability
statement in all AD actions lists all airplanes affected by that AD.
All of the requirements stated in an AD are applicable only to the
airplanes listed in the applicability. We find no justification for
making the requested change. We have not changed the AD in this regard.
Request for Clarification of Parts Installation Requirement
American Airlines (American) requested clarification of the
requirement in paragraph (h) of the NPRM (77 FR 6518, February 8, 2012)
that prohibits installing certain oxygen hoses after the effective date
of the AD. American stated that the compliance time of paragraph (h) of
the NPRM is prior to the compliance date of the low-pressure oxygen
hose removal, and if a maintenance procedure is accomplished which
would require the removal of the low-pressure oxygen hose, the same
low-pressure oxygen hose cannot be re-installed.
We agree to clarify the requirement. Once we have determined that
an unsafe condition exists, we generally specify not to allow that
condition to be introduced into the fleet. Although the word
``install'' is generally considered to be broader than the word
``replace,'' for this AD operators can interpret it as meaning
``replace'' while remaining within the intent of the ``Parts
Installation'' paragraph (paragraph (h) of this AD). By simply
reinstalling a part removed during maintenance, the operator is not
``installing'' a different part. Therefore, removing a part to gain
access and then reinstalling that same part for other maintenance
activities not associated with the AD is acceptable. We have not
changed the AD in this regard.
Conclusion
We reviewed the relevant data, considered the comments received,
and determined that air safety and the public interest require adopting
the AD with the changes described previously.
We also determined that these changes will not increase the
economic burden on any operator or increase the scope of the AD.
Costs of Compliance
We estimate that this AD affects 169 airplanes of U.S. registry.
We estimate the following costs to comply with this AD:
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
Replacement......................... 18 work-hours x $85 per $1,066 $2,596 $438,724
hour = $1,530.
----------------------------------------------------------------------------------------------------------------
[[Page 41047]]
According to the manufacturer, some of the costs of this AD may be
covered under warranty, thereby reducing the cost impact on affected
individuals. We do not control warranty coverage for affected
individuals. As a result, we have included all costs in our cost
estimate.
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
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),
(3) Will not affect intrastate aviation in Alaska, and
(4) 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.
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:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive (AD):
2012-13-05 The Boeing Company: Amendment 39-17107; Docket No. FAA-
2012-0104; Directorate Identifier 2011-NM-279-AD.
(a) Effective Date
This AD is effective August 16, 2012.
(b) Affected ADs
None.
(c) Applicability
This AD applies to The Boeing Company Model 777-200, -200LR, -
300, -300ER, and 777F series airplanes; certificated in any
category; as identified in Boeing Alert Service Bulletin 777-
35A0027, Revision 1, dated April 19, 2012.
(d) Subject
Joint Aircraft System Component (JASC)/Air Transport Association
(ATA) of America Code 35, Oxygen.
(e) Unsafe Condition
This AD was prompted by a report indicating that a fire
originated near the first officer's area, which caused extensive
damage to the flight deck. We are issuing this AD to prevent
electrical current from passing through the low-pressure oxygen hose
internal anti-collapse spring, which can cause the low-pressure
oxygen hose to melt or burn, and a consequent oxygen-fed fire in the
flight compartment.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Replacement
Within 18 months after the effective date of this AD: Replace
the low-pressure oxygen hoses with non-conductive low-pressure
oxygen hoses in the flight compartment, in accordance with the
Accomplishment Instructions of Boeing Alert Service Bulletin 777-
35A0027, dated December 15, 2011, or Boeing Alert Service Bulletin
777-35A0027, Revision 1, dated April 19, 2012.
(h) Parts Installation Prohibition
As of the effective date of this AD, no person may install in
the airplane flight compartment oxygen system on any airplane, a
low-pressure oxygen hose having part number 57034-81220, 57034-
81320, or 57034-91100.
(i) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Seattle Aircraft Certification Office (ACO),
FAA, has the authority to approve AMOCs for this AD, if requested
using the procedures found in 14 CFR 39.19. In accordance with 14
CFR 39.19, send your request to your principal inspector or local
Flight Standards District Office, as appropriate. If sending
information directly to the manager of the ACO, send it to the
attention of the person identified in the Related Information
section of this AD. Information may be emailed to: 9-ANM-Seattle-ACO-AMOC-Requests@faa.gov.
(2) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the local flight standards district office/certificate holding
district office.
(j) Related Information
For more information about this AD, contact Susan Monroe,
Aerospace Engineer, Cabin Safety and Environmental Systems Branch,
ANM-150S, FAA, Seattle Aircraft Certification Office, 1601 Lind
Avenue SW., Renton, WA 98057-3356; phone: (425) 917-6457; fax: (425)
917-6590; email: susan.l.monroe@faa.gov.
(k) Material Incorporated by Reference
(1) You must use the following service information to do the
actions required by this AD, unless the AD specifies otherwise. The
Director of the Federal Register approved the incorporation by
reference (IBR) of the following service information under 5 U.S.C.
552(a) and 1 CFR part 51.
(i) Boeing Alert Service Bulletin 777-35A0027, dated December
15, 2011.
(ii) Boeing Alert Service Bulletin 777-35A0027, Revision 1,
dated April 19, 2012.
(2) For service information identified in this AD, Boeing
Commercial Airplanes, Attention: Data & Services Management, P.O.
Box 3707, MC 2H-65, Seattle, Washington 98124-2207; telephone 206-
544-5000, extension 1; fax 206-766-5680; Internet https://www.myboeingfleet.com.
(3) You may review copies of the referenced service information
at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW.,
Renton, WA 98057-3356. For information on the availability of this
material at the FAA, call (425) 227-1221.
(4) You may also review copies of the service information that
is incorporated by reference at the National Archives and Records
Administration (NARA). For information on the availability of this
material at NARA, call 202-741-6030, or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Renton, Washington, on June 21, 2012.
John Piccola,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2012-15893 Filed 7-11-12; 8:45 am]
BILLING CODE 4910-13-P