Airworthiness Directives; Boeing Model 727 Airplanes, 67644-67645 [05-22214]

Download as PDF 67644 Federal Register / Vol. 70, No. 215 / Tuesday, November 8, 2005 / Rules and Regulations Individual, into a position that requires access to Sensitive Information except in accordance with paragraph (c) below. (c) Access to Sensitive Information. (1) Generally. The Board will grant access to Sensitive Information only in accordance with the Board’s rules and policies regarding access to Sensitive Information and, if applicable, the rules and policies of the FOMC. (2) FOMC Information. (i) Access by a Non-Citizen from a country on the Country List. 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(ii) Access by a Non-Citizen from a country not on the Country List. An Employee, other than a Protected Individual, who, on the date the Employee begins employment with the Federal Reserve System, is a NonCitizen from a country that is not on the Country List: (A) Shall not be granted access to Class I FOMC Information, and (B) shall be granted access to Class II FOMC Information only upon the recommendation of the Employee’s Division Director after six years of residence in the United States, at least two of which include satisfactory employment by the Board and/or one or more of the Federal Reserve Banks, and a background investigation acceptable to the Board. (3) Classified Information. Access to Classified Information is limited to those persons who are permitted access to Classified Information pursuant to the applicable executive orders and any subsequent amendments or superseding orders that the President of the United States may issue from time to time. (4) Confidential Supervisory Information. Access to Confidential VerDate Aug<31>2005 16:28 Nov 07, 2005 Jkt 208001 Supervisory Information is limited to Protected Individuals with a need to know employed by the Board or by a Federal Reserve Bank. By order of the Board of Governors of the Federal Reserve System. Dated: November 2, 2005. Jennifer J. Johnson, Secretary of the Board. [FR Doc. 05–22223 Filed 11–7–05; 8:45 am] BILLING CODE 6210–01–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2005–21975; Directorate Identifier 2005–NM–122–AD; Amendment 39–14365; AD 2005–23–07] RIN 2120–AA64 Airworthiness Directives; Boeing Model 727 Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. AGENCY: SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all Boeing Model 727 airplanes. This AD requires revising the Limitations section of the airplane flight manual to prohibit resetting a tripped circuit breaker for a fuel pump. This AD results from fuel system reviews conducted by the manufacturer. We are issuing this AD to prohibit the resetting of a tripped circuit breaker for a fuel pump, which could allow an electrical fault to override the protective features of the circuit breaker, and could result in sparks inside the fuel tank, ignition of fuel vapors, and consequent fire or explosion. DATES: This AD becomes effective December 13, 2005. ADDRESSES: You may examine the AD docket on the Internet at https:// dms.dot.gov or in person at the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street, SW., Nassif Building, room PL–401, Washington, DC. Contact Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124–2207, for service information identified in this AD. FOR FURTHER INFORMATION CONTACT: Sulmo Mariano, Aerospace Engineer, Propulsion Branch, ANM–140S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98055–4056; telephone (425) 917–6501; fax (425) 917–6590. PO 00000 Frm 00004 Fmt 4700 Sfmt 4700 SUPPLEMENTARY INFORMATION: Examining the Docket You may examine the airworthiness directive (AD) docket on the Internet at https://dms.dot.gov or in person at the Docket Management Facility office between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The Docket Management Facility office (telephone (800) 647–5227) is located on the plaza level of the Nassif Building at the street address stated in the ADDRESSES section. Discussion The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to include an AD that would apply to all Boeing Model 727 airplanes. That NPRM was published in the Federal Register on July 29, 2005 (70 FR 43802). That NPRM proposed to require revising the Limitations section of the airplane flight manual to prohibit resetting a tripped circuit breaker for a fuel pump. Comments We provided the public the opportunity to participate in the development of this AD. We have considered the one comment received. The commenter supports the NPRM. Clarification of Alternative Method of Compliance (AMOC) Paragraph We have revised this action to clarify the appropriate procedure for notifying the principal inspector before using any approved AMOC on any airplane to which the AMOC applies. Conclusion We have carefully reviewed the available data, including the comment received, and determined that air safety and the public interest require adopting the AD with the change described previously. We have determined that this change will neither increase the economic burden on any operator nor increase the scope of the AD. Costs of Compliance There are about 600 airplanes of the affected design in the worldwide fleet. This AD affects about 300 airplanes of U.S. registry. The action in this AD takes about 1 work hour per airplane, at an average labor rate of $65 per work hour. Based on these figures, the estimated cost of the AD for U.S. operators is $19,500, or $65 per airplane. Authority for This Rulemaking Title 49 of the United States Code specifies the FAA’s authority to issue E:\FR\FM\08NOR1.SGM 08NOR1 Federal Register / Vol. 70, No. 215 / Tuesday, November 8, 2005 / Rules and Regulations rules on aviation safety. Subtitle I, section 106, describes the authority of the FAA Administrator. Subtitle VII, Aviation Programs, describes in more detail the scope of the Agency’s authority. We are issuing this rulemaking under the authority described in subtitle VII, part A, subpart III, section 44701, ‘‘General requirements.’’ Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. Regulatory Findings We have determined that this AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the National Government and the States, or on the distribution of power and responsibilities among the various levels of government. For the reasons discussed above, I certify that this AD: (1) Is not a ‘‘significant regulatory action’’ under Executive Order 12866; (2) Is not a ‘‘significant rule’’ under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); and (3) Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. We prepared a regulatory evaluation of the estimated costs to comply with this AD and placed it in the AD docket. See the ADDRESSES section for a location to examine the regulatory evaluation. by adding the following new airworthiness directive (AD): DEPARTMENT OF COMMERCE 2005–23–07 Boeing: Amendment 39–14365. Docket No. FAA–2005–21975; Directorate Identifier 2005–NM–122–AD. International Trade Administration Effective Date Office of Insular Affairs (a) This AD becomes effective December 13, 2005. 15 CFR Part 303 Affected ADs Applicability RIN 0625–AA68 (c) This AD applies to all Boeing Model 727, 727C, 727–100, 727–100C, 727–200, and 727–200F series airplanes; certificated in any category. Changes in the Insular Possessions Watch, Watch Movement and Jewelry Programs Unsafe Condition AGENCIES: (d) This AD results from fuel system reviews conducted by the manufacturer. We are issuing this AD to prohibit the resetting of a tripped circuit breaker for a fuel pump, which could allow an electrical fault to override the protective features of the circuit breaker, and could result in sparks inside the fuel tank, ignition of fuel vapors, and consequent fire or explosion. 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. Revise the Airplane Flight Manual (AFM) (f) Within 30 days after the effective date of this AD, revise the Limitations section of the Boeing 727 AFM to include the following statement. This may be done by inserting a copy of this AD into the AFM. ‘‘Do not reset a tripped fuel pump circuit breaker.’’ Note 1: When a statement identical to that in paragraph (f) of this AD has been included in the general revisions of the AFM, the general revisions may be inserted into the AFM, and the copy of this AD may be removed from the AFM. Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: PART 39—AIRWORTHINESS DIRECTIVES Material Incorporated by Reference (h) None. 1. The authority citation for part 39 continues to read as follows: Issued in Renton, Washington, on October 26, 2005. Kalene C. Yanamura, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 05–22214 Filed 11–7–05; 8:45 am] Adoption of the Amendment I I Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Amended] 2. The Federal Aviation Administration (FAA) amends § 39.13 I VerDate Aug<31>2005 16:28 Nov 07, 2005 Jkt 208001 DEPARTMENT OF THE INTERIOR [Docket No. 050613157–5219–02] (b) None. 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) Before using any AMOC approved in accordance with 14 CFR 39.19 on any airplane to which the AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Certificate Holding District Office. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Safety. 67645 BILLING CODE 4910–13–P PO 00000 Frm 00005 Fmt 4700 Sfmt 4700 Import Administration, International Trade Administration, Department of Commerce; Office of Insular Affairs, Department of the Interior. ACTION: Final rule. SUMMARY: The Departments of Commerce and the Interior (the Departments) amend their regulations governing watch duty-exemption allocations and the watch and jewelry duty-refund benefits for producers in the United States insular possessions (the U.S. Virgin Islands, Guam, American Samoa and the Commonwealth of the Northern Mariana Islands). The rule amends the regulations by making technical changes required by passage of the Miscellaneous Trade and Technical Corrections Act of 2004; extending the duty refund benefits to include the value of usual and customary health insurance, life insurance and pension benefits; raising the ceiling on the amount of jewelry that qualifies for the duty refund benefit; allowing new insular jewelry producers to assemble jewelry and have such jewelry treated as an article of the insular possessions for up to 18 months after the jewelry company commences assembly operations; allowing duty refund certificate holders to secure a duty refund on any articles that are imported into the customs territory of the United States by the certificate holder duty paid; providing a more comprehensive definition of ‘‘unit;’’ adjusting the amount of watch repairs that are eligible for the duty refund; providing compensation to insular watch producers if tariffs on watches and watch movements are reduced; and clarifying which wages are eligible for purposes of determining the duty refund and identifying which records are needed for the audit. DATES: This rule is effective December 8, 2005. E:\FR\FM\08NOR1.SGM 08NOR1

Agencies

[Federal Register Volume 70, Number 215 (Tuesday, November 8, 2005)]
[Rules and Regulations]
[Pages 67644-67645]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-22214]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2005-21975; Directorate Identifier 2005-NM-122-AD; 
Amendment 39-14365; AD 2005-23-07]
RIN 2120-AA64


Airworthiness Directives; Boeing Model 727 Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all 
Boeing Model 727 airplanes. This AD requires revising the Limitations 
section of the airplane flight manual to prohibit resetting a tripped 
circuit breaker for a fuel pump. This AD results from fuel system 
reviews conducted by the manufacturer. We are issuing this AD to 
prohibit the resetting of a tripped circuit breaker for a fuel pump, 
which could allow an electrical fault to override the protective 
features of the circuit breaker, and could result in sparks inside the 
fuel tank, ignition of fuel vapors, and consequent fire or explosion.

DATES: This AD becomes effective December 13, 2005.

ADDRESSES: You may examine the AD docket on the Internet at https://
dms.dot.gov or in person at the Docket Management Facility, U.S. 
Department of Transportation, 400 Seventh Street, SW., Nassif Building, 
room PL-401, Washington, DC.
    Contact Boeing Commercial Airplanes, P.O. Box 3707, Seattle, 
Washington 98124-2207, for service information identified in this AD.

FOR FURTHER INFORMATION CONTACT: Sulmo Mariano, Aerospace Engineer, 
Propulsion Branch, ANM-140S, FAA, Seattle Aircraft Certification 
Office, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone 
(425) 917-6501; fax (425) 917-6590.

SUPPLEMENTARY INFORMATION:

Examining the Docket

    You may examine the airworthiness directive (AD) docket on the 
Internet at https://dms.dot.gov or in person at the Docket Management 
Facility office between 9 a.m. and 5 p.m., Monday through Friday, 
except Federal holidays. The Docket Management Facility office 
(telephone (800) 647-5227) is located on the plaza level of the Nassif 
Building at the street address stated in the ADDRESSES section.

Discussion

    The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 
CFR part 39 to include an AD that would apply to all Boeing Model 727 
airplanes. That NPRM was published in the Federal Register on July 29, 
2005 (70 FR 43802). That NPRM proposed to require revising the 
Limitations section of the airplane flight manual to prohibit resetting 
a tripped circuit breaker for a fuel pump.

Comments

    We provided the public the opportunity to participate in the 
development of this AD. We have considered the one comment received. 
The commenter supports the NPRM.

Clarification of Alternative Method of Compliance (AMOC) Paragraph

    We have revised this action to clarify the appropriate procedure 
for notifying the principal inspector before using any approved AMOC on 
any airplane to which the AMOC applies.

Conclusion

    We have carefully reviewed the available data, including the 
comment received, and determined that air safety and the public 
interest require adopting the AD with the change described previously. 
We have determined that this change will neither increase the economic 
burden on any operator nor increase the scope of the AD.

Costs of Compliance

    There are about 600 airplanes of the affected design in the 
worldwide fleet. This AD affects about 300 airplanes of U.S. registry. 
The action in this AD takes about 1 work hour per airplane, at an 
average labor rate of $65 per work hour. Based on these figures, the 
estimated cost of the AD for U.S. operators is $19,500, or $65 per 
airplane.

Authority for This Rulemaking

    Title 49 of the United States Code specifies the FAA's authority to 
issue

[[Page 67645]]

rules on aviation safety. Subtitle I, section 106, describes the 
authority of the FAA Administrator. Subtitle VII, Aviation Programs, 
describes in more detail the scope of the Agency's authority.
    We are issuing this rulemaking under the authority described in 
subtitle VII, part A, subpart III, section 44701, ``General 
requirements.'' Under that section, Congress charges the FAA with 
promoting safe flight of civil aircraft in air commerce by prescribing 
regulations for practices, methods, and procedures the Administrator 
finds necessary for safety in air commerce. This regulation is within 
the scope of that authority because it addresses an unsafe condition 
that is likely to exist or develop on products identified in this 
rulemaking action.

Regulatory Findings

    We have determined that this AD will not have federalism 
implications under Executive Order 13132. This AD will not have a 
substantial direct effect on the States, on the relationship between 
the National Government and the States, or on the distribution of power 
and responsibilities among the various levels of government.
    For the reasons discussed above, I certify that this AD:
    (1) Is not a ``significant regulatory action'' under Executive 
Order 12866;
    (2) Is not a ``significant rule'' under DOT Regulatory Policies and 
Procedures (44 FR 11034, February 26, 1979); and
    (3) Will not have a significant economic impact, positive or 
negative, on a substantial number of small entities under the criteria 
of the Regulatory Flexibility Act.
    We prepared a regulatory evaluation of the estimated costs to 
comply with this AD and placed it in the AD docket. See the ADDRESSES 
section for a location to examine the regulatory evaluation.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Safety.

Adoption of the Amendment

0
Accordingly, under the authority delegated to me by the Administrator, 
the FAA amends 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:

    Authority: 49 U.S.C. 106(g), 40113, 44701.


Sec.  39.13  [Amended]

0
2. The Federal Aviation Administration (FAA) amends Sec.  39.13 by 
adding the following new airworthiness directive (AD):

2005-23-07 Boeing: Amendment 39-14365. Docket No. FAA-2005-21975; 
Directorate Identifier 2005-NM-122-AD.

Effective Date

    (a) This AD becomes effective December 13, 2005.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to all Boeing Model 727, 727C, 727-100, 727-
100C, 727-200, and 727-200F series airplanes; certificated in any 
category.

Unsafe Condition

    (d) This AD results from fuel system reviews conducted by the 
manufacturer. We are issuing this AD to prohibit the resetting of a 
tripped circuit breaker for a fuel pump, which could allow an 
electrical fault to override the protective features of the circuit 
breaker, and could result in sparks inside the fuel tank, ignition 
of fuel vapors, and consequent fire or explosion.

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.

Revise the Airplane Flight Manual (AFM)

    (f) Within 30 days after the effective date of this AD, revise 
the Limitations section of the Boeing 727 AFM to include the 
following statement. This may be done by inserting a copy of this AD 
into the AFM.
    ``Do not reset a tripped fuel pump circuit breaker.''

    Note 1: When a statement identical to that in paragraph (f) of 
this AD has been included in the general revisions of the AFM, the 
general revisions may be inserted into the AFM, and the copy of this 
AD may be removed from the AFM.

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) Before using any AMOC approved in accordance with 14 CFR 
39.19 on any airplane to which the AMOC applies, notify the 
appropriate principal inspector in the FAA Flight Standards 
Certificate Holding District Office.

Material Incorporated by Reference

    (h) None.

    Issued in Renton, Washington, on October 26, 2005.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 05-22214 Filed 11-7-05; 8:45 am]
BILLING CODE 4910-13-P
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