Airworthiness Directives; Boeing Model 767-200, -300, and -400ER Series Airplanes, 37781-37783 [E8-14189]
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Federal Register / Vol. 73, No. 128 / Wednesday, July 2, 2008 / Rules and Regulations
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2008–0012; Directorate
Identifier 2007–NM–204–AD; Amendment
39–15584; AD 2008–13–21]
RIN 2120–AA64
Airworthiness Directives; Boeing
Model 767–200, –300, and –400ER
Series Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
mstockstill on PROD1PC66 with RULES
SUMMARY: We are adopting a new
airworthiness directive (AD) for certain
Boeing Model 767–200, –300, and
–400ER series airplanes. This AD
requires an inspection to determine the
manufacturer and manufacture date of
the oxygen masks in the passenger
service units and the flight attendant
and lavatory oxygen boxes, as
applicable. This AD also requires
related investigative/corrective actions
if necessary. This AD results from a
report that several passenger masks with
broken in-line flow indicators were
found following a mask deployment. We
are issuing this AD to prevent the inline flow indicators of the passenger
oxygen masks from fracturing and
separating, which could inhibit oxygen
flow to the masks and consequently
result in exposure of the passengers and
cabin attendants to hypoxia following a
depressurization event.
DATES: This AD is effective August 6,
2008.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of August 6, 2008.
ADDRESSES: For service information
identified in this AD, contact Boeing
Commercial Airplanes, P.O. Box 3707,
Seattle, Washington 98124–2207.
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 (telephone 800–647–5527)
is the 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.
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17:12 Jul 01, 2008
Jkt 214001
FOR FURTHER INFORMATION CONTACT:
Robert Hettman, Aerospace Engineer,
Cabin Safety and Environmental
Systems Branch, ANM–150S, FAA,
Seattle Aircraft Certification Office,
1601 Lind Avenue, SW., Renton,
Washington 98057–3356; telephone
(425) 917–6457; fax (425) 917–6590.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to include an airworthiness
directive (AD) that would apply to
certain Boeing Model 767–200, –300,
and –400ER series airplanes. That
NPRM was published in the Federal
Register on January 14, 2008 (73 FR
2190). That NPRM proposed to require
an inspection to determine the
manufacturer and manufacture date of
the oxygen masks in the passenger
service units and the flight attendant
and lavatory oxygen boxes, as
applicable. That NPRM also proposed to
require related investigative/corrective
actions if necessary.
Comments
We gave the public the opportunity to
participate in developing this AD. We
considered the comments received from
the two commenters.
Request To Revise the Relevant Service
Information Section
Boeing requests that we revise the
Relevant Service Information section of
the NPRM to include a general visual
inspection of the flow indicator to
determine whether the letter ‘‘W’’
appears on the right side of the
identification (ID) label. Boeing states
that this inspection should be included
in the NPRM, since the presence of the
letter ‘‘W’’ on the ID label indicates that
the corrective actions have already been
accomplished.
We agree to clarify the related
investigative and corrective actions
required by this AD. If the ID label on
the oxygen mask shows that the mask
was manufactured by B/E Aerospace
between January 1, 2002, and March 1,
2006, then the related investigative
action must be done. The related
investigative action includes doing a
general visual inspection of the flow
indicator to determine the color of the
flow direction mark and the word
‘‘flow’’ on the flow indicator, and to
determine whether the letter ‘‘W’’
appears on the right side of the ID label.
If the flow direction mark and the word
‘‘flow’’ on the flow indicator of the
oxygen mask are not green and the letter
‘‘W’’ is not shown on the right side of
the ID label, then the corrective action
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37781
must be done. The corrective action
includes replacing the oxygen mask
with one that was not manufactured by
B/E Aerospace between January 1, 2002,
and March 1, 2006, or with a modified
oxygen mask having an improved flow
indicator. We have revised paragraph (f)
of this AD accordingly. (Boeing Special
Attention Service Bulletin 767–35–
0054, dated July 6, 2006, refers to B/E
Aerospace Service Bulletin 174080–35–
01, dated February 6, 2006; and
Revision 1, dated May 1, 2006; as
additional sources of service
information for modifying the oxygen
mask assembly by replacing the flow
indicator with an improved flow
indicator.) The intent of this AD is to
accomplish all of the applicable actions
specified in the Accomplishment
Instructions of Boeing Special Attention
Service Bulletin 767–35–0054. Since the
Relevant Service Information section is
not retained in an AD, we have not
changed this AD in this regard.
Request To Revise the Discussion
Section
Boeing requests that we add a
statement to the Discussion section of
the NPRM clarifying that only masks
manufactured by B/E Aerospace
between January 1, 2002, and March 1,
2006, would require corrective action.
Boeing states that no further action is
required for oxygen masks
manufactured outside those dates or
manufactured by other suppliers.
Boeing also states that not including all
of the contents of Boeing Special
Attention Service Bulletin 767–35–0054
in this AD, and not clarifying the intent
of the AD, will generate many requests
for clarification from operators.
We have clarified the requirements of
this AD in our response to the previous
comment. No additional change to this
AD is necessary in this regard, since the
Discussion section of the NPRM is not
retained in this final rule.
Request To Delete Certain
Requirements or Add a Terminating
Action
British Airways states that it does not
agree with the proposed requirement to
replace a discrepant oxygen mask with
one having an improved flow indicator
because only the oxygen masks
identified in Boeing Special Attention
Service Bulletin 767–35–0054 are
potentially defective. The commenter
also states that it has inspected some of
its airplanes and replaced all discrepant
masks with new masks that do not fall
within the rejection criteria. The
commenter believes that it should not
have to re-inspect the oxygen masks
assemblies for the presence of an
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02JYR1
37782
Federal Register / Vol. 73, No. 128 / Wednesday, July 2, 2008 / Rules and Regulations
improved flow indicator after this AD is
issued. The commenter, therefore,
requests that we revise this AD in either
one of the following ways:
• Delete the phrase from paragraph (f)
of this AD that states ‘‘* * * except
where the service bulletin specifies
installing a new oxygen mask, replace
the oxygen mask with a new or
modified oxygen mask having an
improved flow indicator.’’
• Add a statement to this AD
specifying that inspections done in
accordance with Boeing Special
Attention Service Bulletin 767–35–0054
before issuance of this AD comply with
the intent of this AD and do not need
to be repeated.
We agree that inspections done in
accordance with Boeing Special
Attention Service Bulletin 767–35–0054
before the effective date of this AD do
not need to be accomplished again.
However, no change is necessary in this
regard, since a similar statement is
contained in paragraph (e) of this AD.
Further, as stated previously, we have
clarified the phrase regarding
replacement of the oxygen mask in
paragraph (f) of this AD. The intent of
that phrase is to provide the option of
replacing a discrepant oxygen mask
with one that was not manufactured by
B/E Aerospace between January 1, 2002,
and March 1, 2006, or with a modified
oxygen mask having an improved flow
indicator in accordance with B/E
Aerospace Service Bulletin 174080–35–
01.
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 change described previously.
We also determined that this change
will not increase the economic burden
on any operator or increase the scope of
the AD.
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Costs of Compliance
There are about 688 airplanes of the
affected design in the worldwide fleet.
This AD affects about 242 airplanes of
U.S. registry. The required actions take
about 53 work hours per airplane, with
an average of 360 oxygen masks per
airplane, at an average labor rate of $80
per work hour. Based on these figures,
the estimated cost of the AD for U.S.
operators is $1,026,080, or $4,240 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
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17:12 Jul 01, 2008
Jkt 214001
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), 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.
You can find our regulatory
evaluation and the estimated costs of
compliance in the AD Docket.
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 FAA amends § 39.13 by adding
the following new AD:
I
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2008–13–21 Boeing: Amendment 39–15584.
Docket No. FAA–2008–0012; Directorate
Identifier 2007–NM–204–AD.
Effective Date
(a) This airworthiness directive (AD) is
effective August 6, 2008.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Boeing Model 767–
200, –300, and –400ER series airplanes,
certificated in any category; as identified in
Boeing Special Attention Service Bulletin
767–35–0054, dated July 6, 2006.
Unsafe Condition
(d) This AD results from a report that
several passenger masks with broken in-line
flow indicators were found following a mask
deployment. We are issuing this AD to
prevent the in-line flow indicators of the
passenger oxygen masks from fracturing and
separating, which could inhibit oxygen flow
to the masks and consequently result in
exposure of the passengers and cabin
attendants to hypoxia following a
depressurization event.
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.
Inspection and Related Investigative/
Corrective Actions
(f) Within 60 months after the effective
date of this AD, do a general visual
inspection to determine the manufacturer
and manufacture date of the oxygen masks in
the passenger service units and the flight
attendant and lavatory oxygen boxes, as
applicable, and do the applicable related
investigative and corrective actions, by
accomplishing all of the applicable actions
specified in the Accomplishment
Instructions of Boeing Special Attention
Service Bulletin 767–35–0054, dated July 6,
2006; except where the service bulletin
specifies installing a new oxygen mask,
replace the oxygen mask with one that was
not manufactured by B/E Aerospace between
January 1, 2002, and March 1, 2006, or with
a modified oxygen mask having an improved
flow indicator. The related investigative and
corrective actions must be done before
further flight.
Note 1: The Boeing service bulletin refers
to B/E Aerospace Service Bulletin 174080–
35–01, dated February 6, 2006; and Revision
1, dated May 1, 2006; as additional sources
of service information for modifying the
oxygen mask assembly by replacing the flow
indicator with an improved flow indicator.
Alternative Methods of Compliance
(AMOCs)
(g)(1) The Manager, Seattle Aircraft
Certification Office, FAA, has the authority to
approve AMOCs for this AD, if requested in
accordance with the procedures found in 14
CFR 39.19.
(2) To request a different method of
compliance or a different compliance time
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02JYR1
Federal Register / Vol. 73, No. 128 / Wednesday, July 2, 2008 / Rules and Regulations
for this AD, follow the procedures in 14 CFR
39.19. Before using any approved AMOC on
any airplane to which the AMOC applies,
notify your appropriate principal inspector
(PI) in the FAA Flight Standards District
Office (FSDO), or lacking a PI, your local
FSDO.
Material Incorporated by Reference
(h) You must use Boeing Special Attention
Service Bulletin 767–35–0054, dated July 6,
2006, to do the actions required by this AD,
unless the AD specifies otherwise.
(1) The Director of the Federal Register
approved the incorporation by reference of
this service information under 5 U.S.C.
552(a) and 1 CFR part 51.
(2) For service information identified in
this AD, contact Boeing Commercial
Airplanes, P.O. Box 3707, Seattle,
Washington 98124–2207.
(3) You may review copies of the service
information incorporated by reference at the
FAA, Transport Airplane Directorate, 1601
Lind Avenue, SW., Renton, Washington; or at
the National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA, call
202–741–6030, or go to: https://
www.archives.gov/federal_register/
code_of_federal_regulations/
ibr_locations.html.
Issued in Renton, Washington, on June 8,
2008.
Michael Kaszycki,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. E8–14189 Filed 7–1–08; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2007–28434; Directorate
Identifier 2007–CE–053–AD; Amendment
39–15580; AD 2008–13–17]
RIN 2120–AA64
Airworthiness Directives; Hawker
Beechcraft Corporation (Type
Certificates No. 3A15, No. 3A16, No.
A23CE, and No. A30CE Previously
Held by Raytheon Aircraft Company)
F33 Series and Models G33, V35B, A36,
A36TC, B36TC, 95–B55, D55, E55,
A56TC, 58, 58P, 58TC, G58, and 77
Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
mstockstill on PROD1PC66 with RULES
AGENCY:
SUMMARY: The FAA adopts a new
airworthiness directive (AD) for certain
Hawker Beechcraft Corporation F33
series and Models G33, V35B, A36,
A36TC, B36TC, 95–B55, D55, E55,
A56TC, 58, 58P, 58TC, G58, and 77
airplanes. This AD requires you to
VerDate Aug<31>2005
18:15 Jul 01, 2008
Jkt 214001
replace certain circuit breaker toggle
switches with improved design circuit
breaker toggle switches. This AD results
from reports of certain circuit breaker
toggle switches used in various
electrical systems throughout the
affected airplanes overheating. We are
issuing this AD to prevent failure of the
circuit breaker toggle switch, which
could result in smoke in the cockpit and
the inability to turn off the switch.
DATES: This AD becomes effective on
August 6, 2008.
On August 6, 2008, the Director of the
Federal Register approved the
incorporation by reference of certain
publications listed in this AD.
ADDRESSES: To get the service
information identified in this AD,
contact Hawker Beechcraft Corporation,
9709 East Central, Wichita, Kansas
67291; telephone: (800) 429–5372 or
(316) 676–3140.
To view the AD docket, go to U.S.
Department of Transportation, Docket
Operations, M–30, West Building
Ground Floor, Room W12–140, 1200
New Jersey Avenue, SE., Washington,
DC 20590, or on the Internet at https://
www.regulations.gov. The docket
number is FAA–2007–28434;
Directorate Identifier 2007–CE–053–AD.
FOR FURTHER INFORMATION CONTACT: Jose
Flores, Aviation Safety Engineer,
Wichita Aircraft Certification Office,
1801 Airport Road, Room 100, Wichita,
Kansas 67209; telephone: (316) 946–
4132; fax: (316) 946–4107.
SUPPLEMENTARY INFORMATION:
Discussion
On June 29, 2007, we issued a
proposal to amend part 39 of the Federal
Aviation Regulations (14 CFR part 39) to
include an AD that would apply to
certain Hawker Beechcraft Corporation
F33 series and Models G33, V35B, A36,
A36TC, B36TC, 95–B55, D55, E55,
A56TC, 58, 58P, 58TC, G58, and 77
airplanes. This proposal was published
in the Federal Register as a notice of
proposed rulemaking (NPRM) on July 6,
2007 (72 FR 36912). The NPRM
proposed to require you to replace
certain circuit breaker toggle switches
with improved design circuit breaker
toggle switches.
Comments
We provided the public the
opportunity to participate in developing
this AD. The following presents the
comments received on the proposal and
FAA’s response to each comment:
Comment Issue No. 1: Reopen the
Comment Period
The American Bonanza Society and
six other commenters request more time
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37783
to further investigate and evaluate
replacing all circuit breaker switches in
numerous models of Hawker Beechcraft
piston airplanes. One commenter
requests the extension to better research
the number of service difficulty reports
(SDRs), the number of airplanes
affected, and the availability of
replacement switches.
We do not agree with the commenters.
The failure mode creates an internal
short circuit that will cause overheating.
Testing of the circuit breaker switches
revealed all the circuit breaker switches
are susceptible to the failure mode and
overheating.
We have identified an unsafe
condition and determined that
reopening the comment period will only
allow the unsafe condition to
potentially go undetected. If any owner/
operator identifies an alternative
method of compliance (AMOC) to this
AD that will provide a level of safety
acceptable to the FAA, they can apply
for an AMOC using the procedures
outlined in 14 CFR 39.19 and this AD.
We are not changing the final rule AD
action based on these comments.
Comment Issue No. 2: Change Required
Actions
James Blodgett and Adam Dagys
suggest that turning off the master
switch would better eliminate the
problem rather than replacing the
circuit breaker switches.
The commenters request that the FAA
change the proposed AD action to
mandate this change to prevent smoke
in the cockpit.
We do not agree with the commenters.
Turning off the master switch may
mitigate the overheating in some circuit
breaker switches. However, in certain
flight conditions, removing electrical
power could create a more hazardous
condition by disabling electrical
equipment required for continued safe
flight and landing, thus creating an
additional unsafe condition.
We are not changing the final rule AD
action based on these comments.
Comment Issue No. 3: AD Unwarranted
The American Bonanza Society, the
Bonanza Service Ltd., KT Graham Inc.,
and eight other commenters state that
the AD is unwarranted because failure
of the affected circuit breaker switches
is an uncommon occurrence and that
there is no imminent threat to airplane
occupants or the public.
The commenters state that they have
seen no or very few circuit breaker
switch failures in the field. Of the
thousands of affected airplanes and over
100,000 circuit breaker switches, none
of these resulted in a reportable mishap.
E:\FR\FM\02JYR1.SGM
02JYR1
Agencies
[Federal Register Volume 73, Number 128 (Wednesday, July 2, 2008)]
[Rules and Regulations]
[Pages 37781-37783]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E8-14189]
[[Page 37781]]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2008-0012; Directorate Identifier 2007-NM-204-AD;
Amendment 39-15584; AD 2008-13-21]
RIN 2120-AA64
Airworthiness Directives; Boeing Model 767-200, -300, and -400ER
Series Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Boeing Model 767-200, -300, and -400ER series airplanes. This AD
requires an inspection to determine the manufacturer and manufacture
date of the oxygen masks in the passenger service units and the flight
attendant and lavatory oxygen boxes, as applicable. This AD also
requires related investigative/corrective actions if necessary. This AD
results from a report that several passenger masks with broken in-line
flow indicators were found following a mask deployment. We are issuing
this AD to prevent the in-line flow indicators of the passenger oxygen
masks from fracturing and separating, which could inhibit oxygen flow
to the masks and consequently result in exposure of the passengers and
cabin attendants to hypoxia following a depressurization event.
DATES: This AD is effective August 6, 2008.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of August 6,
2008.
ADDRESSES: For service information identified in this AD, contact
Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124-
2207.
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 (telephone 800-647-5527) is the 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: Robert Hettman, Aerospace Engineer,
Cabin Safety and Environmental Systems Branch, ANM-150S, FAA, Seattle
Aircraft Certification Office, 1601 Lind Avenue, SW., Renton,
Washington 98057-3356; telephone (425) 917-6457; fax (425) 917-6590.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to include an airworthiness directive (AD) that would apply to
certain Boeing Model 767-200, -300, and -400ER series airplanes. That
NPRM was published in the Federal Register on January 14, 2008 (73 FR
2190). That NPRM proposed to require an inspection to determine the
manufacturer and manufacture date of the oxygen masks in the passenger
service units and the flight attendant and lavatory oxygen boxes, as
applicable. That NPRM also proposed to require related investigative/
corrective actions if necessary.
Comments
We gave the public the opportunity to participate in developing
this AD. We considered the comments received from the two commenters.
Request To Revise the Relevant Service Information Section
Boeing requests that we revise the Relevant Service Information
section of the NPRM to include a general visual inspection of the flow
indicator to determine whether the letter ``W'' appears on the right
side of the identification (ID) label. Boeing states that this
inspection should be included in the NPRM, since the presence of the
letter ``W'' on the ID label indicates that the corrective actions have
already been accomplished.
We agree to clarify the related investigative and corrective
actions required by this AD. If the ID label on the oxygen mask shows
that the mask was manufactured by B/E Aerospace between January 1,
2002, and March 1, 2006, then the related investigative action must be
done. The related investigative action includes doing a general visual
inspection of the flow indicator to determine the color of the flow
direction mark and the word ``flow'' on the flow indicator, and to
determine whether the letter ``W'' appears on the right side of the ID
label. If the flow direction mark and the word ``flow'' on the flow
indicator of the oxygen mask are not green and the letter ``W'' is not
shown on the right side of the ID label, then the corrective action
must be done. The corrective action includes replacing the oxygen mask
with one that was not manufactured by B/E Aerospace between January 1,
2002, and March 1, 2006, or with a modified oxygen mask having an
improved flow indicator. We have revised paragraph (f) of this AD
accordingly. (Boeing Special Attention Service Bulletin 767-35-0054,
dated July 6, 2006, refers to B/E Aerospace Service Bulletin 174080-35-
01, dated February 6, 2006; and Revision 1, dated May 1, 2006; as
additional sources of service information for modifying the oxygen mask
assembly by replacing the flow indicator with an improved flow
indicator.) The intent of this AD is to accomplish all of the
applicable actions specified in the Accomplishment Instructions of
Boeing Special Attention Service Bulletin 767-35-0054. Since the
Relevant Service Information section is not retained in an AD, we have
not changed this AD in this regard.
Request To Revise the Discussion Section
Boeing requests that we add a statement to the Discussion section
of the NPRM clarifying that only masks manufactured by B/E Aerospace
between January 1, 2002, and March 1, 2006, would require corrective
action. Boeing states that no further action is required for oxygen
masks manufactured outside those dates or manufactured by other
suppliers. Boeing also states that not including all of the contents of
Boeing Special Attention Service Bulletin 767-35-0054 in this AD, and
not clarifying the intent of the AD, will generate many requests for
clarification from operators.
We have clarified the requirements of this AD in our response to
the previous comment. No additional change to this AD is necessary in
this regard, since the Discussion section of the NPRM is not retained
in this final rule.
Request To Delete Certain Requirements or Add a Terminating Action
British Airways states that it does not agree with the proposed
requirement to replace a discrepant oxygen mask with one having an
improved flow indicator because only the oxygen masks identified in
Boeing Special Attention Service Bulletin 767-35-0054 are potentially
defective. The commenter also states that it has inspected some of its
airplanes and replaced all discrepant masks with new masks that do not
fall within the rejection criteria. The commenter believes that it
should not have to re-inspect the oxygen masks assemblies for the
presence of an
[[Page 37782]]
improved flow indicator after this AD is issued. The commenter,
therefore, requests that we revise this AD in either one of the
following ways:
Delete the phrase from paragraph (f) of this AD that
states ``* * * except where the service bulletin specifies installing a
new oxygen mask, replace the oxygen mask with a new or modified oxygen
mask having an improved flow indicator.''
Add a statement to this AD specifying that inspections
done in accordance with Boeing Special Attention Service Bulletin 767-
35-0054 before issuance of this AD comply with the intent of this AD
and do not need to be repeated.
We agree that inspections done in accordance with Boeing Special
Attention Service Bulletin 767-35-0054 before the effective date of
this AD do not need to be accomplished again. However, no change is
necessary in this regard, since a similar statement is contained in
paragraph (e) of this AD. Further, as stated previously, we have
clarified the phrase regarding replacement of the oxygen mask in
paragraph (f) of this AD. The intent of that phrase is to provide the
option of replacing a discrepant oxygen mask with one that was not
manufactured by B/E Aerospace between January 1, 2002, and March 1,
2006, or with a modified oxygen mask having an improved flow indicator
in accordance with B/E Aerospace Service Bulletin 174080-35-01.
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 change described previously. We also determined that
this change will not increase the economic burden on any operator or
increase the scope of the AD.
Costs of Compliance
There are about 688 airplanes of the affected design in the
worldwide fleet. This AD affects about 242 airplanes of U.S. registry.
The required actions take about 53 work hours per airplane, with an
average of 360 oxygen masks per airplane, at an average labor rate of
$80 per work hour. Based on these figures, the estimated cost of the AD
for U.S. operators is $1,026,080, or $4,240 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
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 under the criteria
of the Regulatory Flexibility Act.
You can find our regulatory evaluation and the estimated costs of
compliance in the AD Docket.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
0
Accordingly, under the authority delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new AD:
2008-13-21 Boeing: Amendment 39-15584. Docket No. FAA-2008-0012;
Directorate Identifier 2007-NM-204-AD.
Effective Date
(a) This airworthiness directive (AD) is effective August 6,
2008.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Boeing Model 767-200, -300, and -400ER
series airplanes, certificated in any category; as identified in
Boeing Special Attention Service Bulletin 767-35-0054, dated July 6,
2006.
Unsafe Condition
(d) This AD results from a report that several passenger masks
with broken in-line flow indicators were found following a mask
deployment. We are issuing this AD to prevent the in-line flow
indicators of the passenger oxygen masks from fracturing and
separating, which could inhibit oxygen flow to the masks and
consequently result in exposure of the passengers and cabin
attendants to hypoxia following a depressurization event.
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.
Inspection and Related Investigative/Corrective Actions
(f) Within 60 months after the effective date of this AD, do a
general visual inspection to determine the manufacturer and
manufacture date of the oxygen masks in the passenger service units
and the flight attendant and lavatory oxygen boxes, as applicable,
and do the applicable related investigative and corrective actions,
by accomplishing all of the applicable actions specified in the
Accomplishment Instructions of Boeing Special Attention Service
Bulletin 767-35-0054, dated July 6, 2006; except where the service
bulletin specifies installing a new oxygen mask, replace the oxygen
mask with one that was not manufactured by B/E Aerospace between
January 1, 2002, and March 1, 2006, or with a modified oxygen mask
having an improved flow indicator. The related investigative and
corrective actions must be done before further flight.
Note 1: The Boeing service bulletin refers to B/E Aerospace
Service Bulletin 174080-35-01, dated February 6, 2006; and Revision
1, dated May 1, 2006; as additional sources of service information
for modifying the oxygen mask assembly by replacing the flow
indicator with an improved flow indicator.
Alternative Methods of Compliance (AMOCs)
(g)(1) The Manager, Seattle Aircraft Certification Office, FAA,
has the authority to approve AMOCs for this AD, if requested in
accordance with the procedures found in 14 CFR 39.19.
(2) To request a different method of compliance or a different
compliance time
[[Page 37783]]
for this AD, follow the procedures in 14 CFR 39.19. Before using any
approved AMOC on any airplane to which the AMOC applies, notify your
appropriate principal inspector (PI) in the FAA Flight Standards
District Office (FSDO), or lacking a PI, your local FSDO.
Material Incorporated by Reference
(h) You must use Boeing Special Attention Service Bulletin 767-
35-0054, dated July 6, 2006, to do the actions required by this AD,
unless the AD specifies otherwise.
(1) The Director of the Federal Register approved the
incorporation by reference of this service information under 5
U.S.C. 552(a) and 1 CFR part 51.
(2) For service information identified in this AD, contact
Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington
98124-2207.
(3) You may review copies of the service information
incorporated by reference at the FAA, Transport Airplane
Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the
National Archives and Records Administration (NARA). For information
on the availability of this material at NARA, call 202-741-6030, or
go to: https://www.archives.gov/federal_register/code_of_federal_
regulations/ibr_locations.html.
Issued in Renton, Washington, on June 8, 2008.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E8-14189 Filed 7-1-08; 8:45 am]
BILLING CODE 4910-13-P