Airworthiness Directives; Boeing Model 767 Airplanes, 32252-32253 [E8-12684]
Download as PDF
32252
Federal Register / Vol. 73, No. 110 / Friday, June 6, 2008 / Proposed Rules
using the procedures found in 14 CFR 39.19.
Send information to ATTN: Vladimir
Ulyanov, Aerospace Engineer, International
Branch, ANM–116, Transport Airplane
Directorate, FAA, 1601 Lind Avenue, SW.,
Renton, Washington 98057–3356; telephone
(425) 227–1138; fax (425) 227–1149. Before
using any approved AMOC on any airplane
to which the AMOC applies, notify your
appropriate principal inspector (PI) in the
FAA Flight Standards District Office (FSDO),
or lacking a PI, your local FSDO.
(2) Airworthy Product: For any requirement
in this AD to obtain corrective actions from
a manufacturer or other source, use these
actions if they are FAA-approved. Corrective
actions are considered FAA-approved if they
are approved by the State of Design Authority
(or their delegated agent). You are required
to assure the product is airworthy before it
is returned to service.
(3) Reporting Requirements: For any
reporting requirement in this AD, under the
provisions of the Paperwork Reduction Act,
the Office of Management and Budget (OMB)
has approved the information collection
requirements and has assigned OMB Control
Number 2120–0056.
Related Information
(h) Refer to MCAI European Aviation
Safety Agency Airworthiness Directive 2008–
0055, dated March 5, 2008, and Airbus
Service Bulletin A300–28A6096, Revision 01,
dated April 16, 2008, for related information.
Issued in Renton, Washington, on May 29,
2008.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E8–12727 Filed 6–5–08; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2008–0616; Directorate
Identifier 2007–NM–353–AD]
RIN 2120–AA64
Airworthiness Directives; Boeing
Model 767 Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
We propose to adopt a new
airworthiness directive (AD) for all
Boeing Model 767 airplanes. This
proposed AD would require performing
repetitive operational tests of the engine
fuel suction feed of the fuel system, and
other related testing if necessary. This
proposed AD results from a report of inservice occurrences of loss of fuel
system suction feed capability, followed
by total loss of pressure of the fuel feed
dwashington3 on PRODPC61 with PROPOSALS
SUMMARY:
VerDate Aug<31>2005
11:59 Jun 05, 2008
Jkt 214001
system. We are proposing this AD to
detect and correct failure of the engine
fuel suction feed of the fuel system,
which could result in dual engine
flameout, inability to restart the engines,
and consequent forced landing of the
airplane.
DATES: We must receive comments on
this proposed AD by July 21, 2008.
ADDRESSES: You may send comments by
any of the following methods:
• Federal eRulemaking Portal: Go to
https://www.regulations.gov. Follow the
instructions for submitting comments.
• Fax: 202–493–2251.
• Mail: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue, SE.,
Washington, DC 20590.
• Hand Delivery: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue, SE.,
Washington, DC 20590, between 9 a.m.
and 5 p.m., Monday through Friday,
except Federal holidays.
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 proposed AD, the
regulatory evaluation, any comments
received, and other information. The
street address for the Docket Office
(telephone 800–647–5527) is in the
ADDRESSES section. Comments will be
available in the AD docket shortly after
receipt.
FOR FURTHER INFORMATION CONTACT: Sue
Lucier, Aerospace Engineer, Propulsion
Branch, ANM–140S, FAA, Seattle
Aircraft Certification Office, 1601 Lind
Avenue, SW., Renton, Washington
98057–3356; telephone (425) 917–6438;
fax (425) 917–6590.
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite you to send any written
relevant data, views, or arguments about
this proposed AD. Send your comments
to an address listed under the
ADDRESSES section. Include ‘‘Docket No.
FAA–2008–0616; Directorate Identifier
2007–NM–353–AD’’ at the beginning of
your comments. We specifically invite
comments on the overall regulatory,
economic, environmental, and energy
aspects of this proposed AD. We will
PO 00000
Frm 00010
Fmt 4702
Sfmt 4702
consider all comments received by the
closing date and may amend this
proposed AD because of those
comments.
We will post all comments we
receive, without change, to https://
www.regulations.gov, including any
personal information you provide. We
will also post a report summarizing each
substantive verbal contact we receive
about this proposed AD.
Discussion
We have received a report of inservice occurrences of loss of fuel
system suction feed capability, followed
by total loss of pressure of the fuel feed
system. This condition, if not corrected,
could result in dual engine flameout,
inability to restart the engines, and
consequent forced landing of the
airplane.
FAA’s Conclusions
We have determined that it is
necessary to require an operational test
of the engine fuel suction feed of the
fuel system, and other related testing, as
applicable. Procedures for doing the
operational test can be found in the
maintenance manual. The other related
testing is for airplanes on which one or
both of the engines stop idling in less
than five minutes after starting the test.
Failure of the engine fuel suction feed
of the fuel system could result in the
unsafe condition described previously.
FAA’s Determination and Requirements
of This Proposed AD
We are proposing this AD because we
have evaluated all pertinent information
and identified an unsafe condition that
is likely to exist or develop on other
airplanes of this same type design. This
proposed AD would require performing
repetitive operational tests of the engine
fuel suction feed of the fuel system, and
other related testing if necessary.
Costs of Compliance
We estimate that this proposed AD
would affect 416 airplanes of U.S.
registry. We also estimate that it would
take 1 work-hour per product, per test,
to comply with this proposed AD. The
average labor rate is $80 per work-hour.
Based on these figures, we estimate the
cost of this proposed AD to the U.S.
operators to be $33,280, or $80 per
product, per test.
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
E:\FR\FM\06JNP1.SGM
06JNP1
Federal Register / Vol. 73, No. 110 / Friday, June 6, 2008 / Proposed Rules
detail the scope of the Agency’s
authority.
We are issuing this rulemaking under
the authority described in ‘‘Subtitle VII,
Part A, Subpart III, Section 44701:
General requirements.’’ Under that
section, Congress charges the FAA with
promoting safe flight of civil aircraft in
air commerce by prescribing regulations
for practices, methods, and procedures
the Administrator finds necessary for
safety in air commerce. This regulation
is within the scope of that authority
because it addresses an unsafe condition
that is likely to exist or develop on
products identified in this rulemaking
action.
Regulatory Findings
We determined that this 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 this 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.
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, 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:
dwashington3 on PRODPC61 with PROPOSALS
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.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new AD:
Boeing: Docket No. FAA–2008–0616;
Directorate Identifier 2007–NM–353–AD.
VerDate Aug<31>2005
11:59 Jun 05, 2008
Jkt 214001
32253
Comments Due Date
(a) We must receive comments by July 21,
2008.
DEPARTMENT OF TRANSPORTATION
Affected ADs
(b) None.
14 CFR Part 39
Applicability
(c) This AD applies to all Boeing Model
767–200, –300, –300F, and –400ER series
airplanes, certificated in any category.
Unsafe Condition
(d) This AD results from a report of inservice occurrences of loss of fuel system
suction feed capability, followed by total loss
of pressure of the fuel feed system. We are
issuing this AD to detect and correct failure
of the engine fuel suction feed of the fuel
system, which could result in dual engine
flameout, inability to restart the engines, and
consequent forced landing of the airplane.
Compliance
(e) Comply with this AD within the
compliance times specified, unless already
done.
Operational Test/Other Related Testing
(f) Within 7,500 flight hours after the
effective date of this AD, perform an
operational test of the engine fuel suction
feed of the fuel system, and perform all other
related testing, as applicable, before further
flight, according to a method approved by the
Manager, Seattle Aircraft Certification Office
(ACO), FAA. One approved method is the
operational test in Section 28–22–00, titled
‘‘Engine Fuel Feed System—Description and
Operation,’’ of the Boeing 767 Maintenance
Manual; and Boeing 767 Task Card 28–018–
02, titled ‘‘Engine Fuel Suction Feed
System,’’ dated August 22, 2007. Repeat the
operational test thereafter at intervals not to
exceed 7,500 flight hours. Thereafter, except
as provided in paragraph (g) of this AD, no
alternative procedure or repeat test intervals
will be allowed.
Alternative Methods of Compliance
(AMOCs)
(g)(1) The Manager, Seattle ACO, FAA,
ATTN: Sue Lucier, Aerospace Engineer,
Propulsion Branch, ANM–140S, 1601 Lind
Avenue, SW., Renton, Washington 98057–
3356; telephone (425) 917–6438; fax (425)
917–6590, has the authority to approve
AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19.
(2) To request a different method of
compliance or a different compliance time
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.
Issued in Renton, Washington, on May 16,
2008.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E8–12684 Filed 6–5–08; 8:45 am]
BILLING CODE 4910–13–P
PO 00000
Frm 00011
Fmt 4702
Sfmt 4702
Federal Aviation Administration
[Docket No. FAA–2008–0618; Directorate
Identifier 2007–NM–355–AD]
RIN 2120–AA64
Airworthiness Directives; Boeing
Model 777 Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
SUMMARY: We propose to adopt a new
airworthiness directive (AD) for all
Boeing Model 777 airplanes. This
proposed AD would require performing
repetitive operational tests of the engine
fuel suction feed of the fuel system, and
other related testing if necessary. This
proposed AD results from a report of inservice occurrences of loss of fuel
system suction feed capability, followed
by total loss of pressure of the fuel feed
system. We are proposing this AD to
detect and correct failure of the engine
fuel suction feed of the fuel system,
which could result in dual engine
flameout, inability to restart the engines,
and consequent forced landing of the
airplane.
We must receive comments on
this proposed AD by July 21, 2008.
ADDRESSES: You may send comments by
any of the following methods:
• Federal eRulemaking Portal: Go to
https://www.regulations.gov. Follow the
instructions for submitting comments.
• Fax: 202–493–2251.
• Mail: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue, SE.,
Washington, DC 20590.
• Hand Delivery: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue, SE.,
Washington, DC 20590, between 9 a.m.
and 5 p.m., Monday through Friday,
except Federal holidays.
For service information identified in
this AD, contact Boeing Commercial
Airplanes, P.O. Box 3707, Seattle,
Washington 98124–2207.
DATES:
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 proposed AD, the
E:\FR\FM\06JNP1.SGM
06JNP1
Agencies
[Federal Register Volume 73, Number 110 (Friday, June 6, 2008)]
[Proposed Rules]
[Pages 32252-32253]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E8-12684]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2008-0616; Directorate Identifier 2007-NM-353-AD]
RIN 2120-AA64
Airworthiness Directives; Boeing Model 767 Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: We propose to adopt a new airworthiness directive (AD) for all
Boeing Model 767 airplanes. This proposed AD would require performing
repetitive operational tests of the engine fuel suction feed of the
fuel system, and other related testing if necessary. This proposed AD
results from a report of in-service occurrences of loss of fuel system
suction feed capability, followed by total loss of pressure of the fuel
feed system. We are proposing this AD to detect and correct failure of
the engine fuel suction feed of the fuel system, which could result in
dual engine flameout, inability to restart the engines, and consequent
forced landing of the airplane.
DATES: We must receive comments on this proposed AD by July 21, 2008.
ADDRESSES: You may send comments by any of the following methods:
Federal eRulemaking Portal: Go to https://
www.regulations.gov. Follow the instructions for submitting comments.
Fax: 202-493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue, SE., Washington, DC 20590.
Hand Delivery: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue, SE., Washington, DC 20590, between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.
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 proposed AD, the regulatory
evaluation, any comments received, and other information. The street
address for the Docket Office (telephone 800-647-5527) is in the
ADDRESSES section. Comments will be available in the AD docket shortly
after receipt.
FOR FURTHER INFORMATION CONTACT: Sue Lucier, Aerospace Engineer,
Propulsion Branch, ANM-140S, FAA, Seattle Aircraft Certification
Office, 1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone
(425) 917-6438; fax (425) 917-6590.
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite you to send any written relevant data, views, or
arguments about this proposed AD. Send your comments to an address
listed under the ADDRESSES section. Include ``Docket No. FAA-2008-0616;
Directorate Identifier 2007-NM-353-AD'' at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of this proposed AD. We
will consider all comments received by the closing date and may amend
this proposed AD because of those comments.
We will post all comments we receive, without change, to https://
www.regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this proposed AD.
Discussion
We have received a report of in-service occurrences of loss of fuel
system suction feed capability, followed by total loss of pressure of
the fuel feed system. This condition, if not corrected, could result in
dual engine flameout, inability to restart the engines, and consequent
forced landing of the airplane.
FAA's Conclusions
We have determined that it is necessary to require an operational
test of the engine fuel suction feed of the fuel system, and other
related testing, as applicable. Procedures for doing the operational
test can be found in the maintenance manual. The other related testing
is for airplanes on which one or both of the engines stop idling in
less than five minutes after starting the test. Failure of the engine
fuel suction feed of the fuel system could result in the unsafe
condition described previously.
FAA's Determination and Requirements of This Proposed AD
We are proposing this AD because we have evaluated all pertinent
information and identified an unsafe condition that is likely to exist
or develop on other airplanes of this same type design. This proposed
AD would require performing repetitive operational tests of the engine
fuel suction feed of the fuel system, and other related testing if
necessary.
Costs of Compliance
We estimate that this proposed AD would affect 416 airplanes of
U.S. registry. We also estimate that it would take 1 work-hour per
product, per test, to comply with this proposed AD. The average labor
rate is $80 per work-hour. Based on these figures, we estimate the cost
of this proposed AD to the U.S. operators to be $33,280, or $80 per
product, per test.
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
[[Page 32253]]
detail the scope of the Agency's authority.
We are issuing this rulemaking under the authority described in
``Subtitle VII, Part A, Subpart III, Section 44701: General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.
Regulatory Findings
We determined that this 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 this 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.
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, 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 FAA amends Sec. 39.13 by adding the following new AD:
Boeing: Docket No. FAA-2008-0616; Directorate Identifier 2007-NM-
353-AD.
Comments Due Date
(a) We must receive comments by July 21, 2008.
Affected ADs
(b) None.
Applicability
(c) This AD applies to all Boeing Model 767-200, -300, -300F,
and -400ER series airplanes, certificated in any category.
Unsafe Condition
(d) This AD results from a report of in-service occurrences of
loss of fuel system suction feed capability, followed by total loss
of pressure of the fuel feed system. We are issuing this AD to
detect and correct failure of the engine fuel suction feed of the
fuel system, which could result in dual engine flameout, inability
to restart the engines, and consequent forced landing of the
airplane.
Compliance
(e) Comply with this AD within the compliance times specified,
unless already done.
Operational Test/Other Related Testing
(f) Within 7,500 flight hours after the effective date of this
AD, perform an operational test of the engine fuel suction feed of
the fuel system, and perform all other related testing, as
applicable, before further flight, according to a method approved by
the Manager, Seattle Aircraft Certification Office (ACO), FAA. One
approved method is the operational test in Section 28-22-00, titled
``Engine Fuel Feed System--Description and Operation,'' of the
Boeing 767 Maintenance Manual; and Boeing 767 Task Card 28-018-02,
titled ``Engine Fuel Suction Feed System,'' dated August 22, 2007.
Repeat the operational test thereafter at intervals not to exceed
7,500 flight hours. Thereafter, except as provided in paragraph (g)
of this AD, no alternative procedure or repeat test intervals will
be allowed.
Alternative Methods of Compliance (AMOCs)
(g)(1) The Manager, Seattle ACO, FAA, ATTN: Sue Lucier,
Aerospace Engineer, Propulsion Branch, ANM-140S, 1601 Lind Avenue,
SW., Renton, Washington 98057-3356; telephone (425) 917-6438; fax
(425) 917-6590, has the authority to approve AMOCs for this AD, if
requested using the procedures found in 14 CFR 39.19.
(2) To request a different method of compliance or a different
compliance time 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.
Issued in Renton, Washington, on May 16, 2008.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E8-12684 Filed 6-5-08; 8:45 am]
BILLING CODE 4910-13-P