Airworthiness Directives; The Boeing Company Airplanes, 47330-47331 [2012-19244]

Download as PDF 47330 Federal Register / Vol. 77, No. 153 / Wednesday, August 8, 2012 / Proposed Rules 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 On October 19, 2009, we issued AD 2009–22–13, Amendment 39–16066 (74 FR 55755, October 29, 2009), for certain The Boeing Company Model 767–200, –300, –300F, and –400ER series airplanes. That AD requires an inspection to determine if certain motor operated valve actuators for the fuel tanks are installed, and related investigative and corrective actions if necessary. That AD resulted from fuel system reviews conducted by the manufacturer. We issued that AD to prevent an ignition source inside the fuel tanks, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane. Actions Since Existing AD (74 FR 55755, October 29, 2009) Was Issued Since we issued AD 2009–22–13, Amendment 39–16066 (74 FR 55755, October 29, 2009), we discovered that the corrective action addresses that safety concern, but also introduces a different unsafe condition. The manufacturer is developing a more complete solution to address both unsafe conditions. We will consider additional rulemaking to require a new solution once that solution is developed, approved, and available for accomplishment. FAA’s Conclusions Upon further consideration, we have determined that existing AD 2009–22– 13, Amendment 39–16066 (74 FR 55755, October 29, 2009), must be rescinded. Accordingly, this proposed AD would rescind AD 2009–22–13. Rescission of AD 2009–22–13 would not preclude the FAA from issuing another related action or commit the FAA to any course of action in the future. wreier-aviles on DSK5TPTVN1PROD with PROPOSALS Related Costs AD 2009–22–13, Amendment 39– 16066 (74 FR 55755, October 29, 2009), affects about 397 airplanes of U.S. registry. The estimated cost of the currently required actions for U.S. operators is between $67,490 and $134,980, or between $170 and $340 per airplane. Rescinding AD 2009–22–13 would eliminate those costs. VerDate Mar<15>2010 13:49 Aug 07, 2012 Jkt 226001 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. § 39.13 Regulatory Findings We have determined that this proposed AD would not have federalism implications under Executive Order 13132. This proposed AD would not have a substantial direct effect on the States, on the relationship between the national Government and the States, or on the distribution of power and responsibilities among the various levels of government. For the reasons discussed above, I certify that the proposed regulation: (1) Is not a ‘‘significant regulatory action’’ under Executive Order 12866; (2) Is not a ‘‘significant rule’’ under the DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); (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. Issued in Renton, Washington, on July 31, 2012. Michael Kaszycki, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, 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. PO 00000 Frm 00003 Fmt 4702 Sfmt 4702 [Amended] 2. The FAA amends § 39.13 by removing airworthiness directive (AD) 2009–22–13, Amendment 39–16066 (74 FR 55755, October 29, 2009), and adding the following new AD: The Boeing Company: Docket No. FAA– 2012–0805; Directorate Identifier 2012– NM–117–AD. Comments Due Date (a) The FAA must receive comments on this AD action by September 24, 2012. Affected ADs (b) This action rescinds AD 2009–22–13, Amendment 39–16066 (74 FR 55755, October 29, 2009). Applicability (c) This action applies to The Boeing Company Model 767–200, –300, –300F, and –400ER series airplanes, certificated in any category; as identified in Boeing Alert Service Bulletin 767–28A0090, dated July 3, 2008. [FR Doc. 2012–19238 Filed 8–7–12; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2011–0158; Directorate Identifier 2010–NM–118–AD] RIN 2120–AA64 Airworthiness Directives; The Boeing Company Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Proposed rule; withdrawal. AGENCY: The FAA withdraws a notice of proposed rulemaking (NPRM) that proposed to supersede an existing airworthiness directive (AD) that applies to certain The Boeing Company Model 767–200, –300, –300F, and –400ER series airplanes. The proposed AD would have continued to require an inspection to determine if certain motor operated valve actuators for the fuel tanks are installed, and related investigative and corrective actions if necessary. That proposed AD would have added airplanes and, for certain airplanes, required additional inspections to determine if certain motor operated valve actuators for the fuel tanks are installed, and related SUMMARY: E:\FR\FM\08AUP1.SGM 08AUP1 Federal Register / Vol. 77, No. 153 / Wednesday, August 8, 2012 / Proposed Rules investigative and corrective actions if necessary. Since the proposed AD was issued, we have received new data indicating that the existing AD addresses that safety concern, but also introduces a different unsafe condition. Accordingly, the proposed AD is withdrawn. 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 rule, the regulatory evaluation, any comments received, and other information. The address for the Docket Office (phone: 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. ADDRESSES: FOR FURTHER INFORMATION CONTACT: Rebel Nichols, Aerospace Engineer, Propulsion Branch, ANM–140S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue SW., Renton, WA 98057–3356; phone: (425) 917–6509; fax: (425) 917–6590; email: Rebel. Nichols@faa.gov. wreier-aviles on DSK5TPTVN1PROD with PROPOSALS Discussion We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 of with a notice of proposed rulemaking (NPRM) to supersede AD 2009–22–13, Amendment 39–16066 (74 FR 55755, October 29, 2009). That AD applies to the specified products. The NPRM published in the Federal Register on March 14, 2011 (76 FR 13534). That NPRM would have continued to require an inspection to determine if certain motor operated valve actuators for the fuel tanks are installed, and related investigative and corrective actions if necessary. That proposed AD would have added airplanes and, for certain airplanes, required additional inspections to determine if certain motor operated valve actuators for the fuel tanks are installed, and related investigative and corrective actions if necessary. That NPRM resulted from fuel system reviews conducted by the manufacturer. The proposed actions were intended to prevent an ignition source inside the fuel tanks, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane. 13:49 Aug 07, 2012 Jkt 226001 DEPARTMENT OF HOMELAND SECURITY Since we issued the NPRM (76 FR 13534, March 14, 2011), we discovered that the corrective action mandated by AD 2009–22–13, Amendment 39–16066 (74 FR 55755, October 29, 2009), and subsequently the corrective actions proposed by the NPRM, address that safety concern, but also introduce a different unsafe condition. The manufacturer is developing a more complete solution to address both unsafe conditions. Accordingly, we have determined that the NPRM (76 FR 13534, March 14, 2011), must be withdrawn. In addition, we are considering further rulemaking to rescind AD 2009–22–13, Amendment 39–16066 (74 FR 55755, October 29, 2009), and will consider requiring a new solution once it is developed, approved, and available for accomplishment. Coast Guard FAA’s Conclusions Upon further consideration, we have determined that the existing AD does not properly address the safety concern. Accordingly, the NPRM (76 FR 13534, March 14, 2011) is withdrawn. Withdrawal of the NPRM (76 FR 13534, March 14, 2011) does not preclude the FAA from issuing another related action or commit the FAA to any course of action in the future. SUPPLEMENTARY INFORMATION: VerDate Mar<15>2010 Actions Since NPRM (76 FR 13534, March 14, 2011) Was Issued 47331 Regulatory Impact Since this action only withdraws an NPRM (76 FR 13534, March 14, 2011), it is neither a proposed nor a final rule and therefore is not covered under Executive Order 12866, the Regulatory Flexibility Act, or DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979). List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. The Withdrawal Accordingly, we withdraw the NPRM, Docket No. FAA–2011–0158, Directorate Identifier 2010–NM–118–AD, which was published in the Federal Register on March 14, 2011 (76 FR 13534). Issued in Renton, Washington, on July 31, 2012. Michael Kaszycki, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2012–19244 Filed 8–7–12; 8:45 am] BILLING CODE 4910–13–P PO 00000 Frm 00004 Fmt 4702 Sfmt 4702 33 CFR Part 165 [Docket No. USCG–2012–0343] RIN 1625–AA11 Regulated Navigation Area—New Haven Harbor, Quinnipiac River, Mill River, New Haven, CT; Pearl Harbor Memorial Bridge (Interstate 95) Construction Coast Guard, DHS. Notice of proposed rulemaking. AGENCY: ACTION: The Coast Guard is proposing changes to the existing regulated navigation area in the navigable waters of New Haven Harbor, Quinnipiac River and Mill River. The current RNA pertains only to the operation of tugs and barges. The changes would allow periodic, temporary closure of the area which will be needed during construction of the new Pearl Harbor Memorial Bridge, and which could be needed at other times as well. This proposed revision would allow the Coast Guard to suspend all vessel traffic through the RNA during periods of temporary closure. This rule is necessary to provide for the safety of life in the regulated area. DATES: Comments and related material must be received by the Coast Guard on or before September 7, 2012. Requests for public meetings must be received by the Coast Guard on or before August 20, 2012. ADDRESSES: You may submit comments identified by docket number USCG– 2012–0343 using any one of the following methods: (1) Federal eRulemaking Portal: https://www.regulations.gov. (2) Fax: 202–493–2251. (3) Mail: Docket Management Facility (M–30), U.S. Department of Transportation, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE., Washington, DC 20590– 0001. (4) Hand delivery: Same as mail address above, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The telephone number is 202–366–9329. To avoid duplication, please use only one of these four methods. See the ‘‘Public Participation and Request for Comments’’ portion of the SUPPLEMENTARY INFORMATION section below for instructions on submitting comments. SUMMARY: E:\FR\FM\08AUP1.SGM 08AUP1

Agencies

[Federal Register Volume 77, Number 153 (Wednesday, August 8, 2012)]
[Proposed Rules]
[Pages 47330-47331]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2012-19244]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2011-0158; Directorate Identifier 2010-NM-118-AD]
RIN 2120-AA64


Airworthiness Directives; The Boeing Company Airplanes

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

ACTION: Proposed rule; withdrawal.

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

SUMMARY: The FAA withdraws a notice of proposed rulemaking (NPRM) that 
proposed to supersede an existing airworthiness directive (AD) that 
applies to certain The Boeing Company Model 767-200, -300, -300F, and -
400ER series airplanes. The proposed AD would have continued to require 
an inspection to determine if certain motor operated valve actuators 
for the fuel tanks are installed, and related investigative and 
corrective actions if necessary. That proposed AD would have added 
airplanes and, for certain airplanes, required additional inspections 
to determine if certain motor operated valve actuators for the fuel 
tanks are installed, and related

[[Page 47331]]

investigative and corrective actions if necessary. Since the proposed 
AD was issued, we have received new data indicating that the existing 
AD addresses that safety concern, but also introduces a different 
unsafe condition. Accordingly, the proposed AD is withdrawn.

ADDRESSES: 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 rule, the regulatory 
evaluation, any comments received, and other information. The address 
for the Docket Office (phone: 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: Rebel Nichols, Aerospace Engineer, 
Propulsion Branch, ANM-140S, FAA, Seattle Aircraft Certification 
Office, 1601 Lind Avenue SW., Renton, WA 98057-3356; phone: (425) 917-
6509; fax: (425) 917-6590; email: Rebel.Nichols@faa.gov.

SUPPLEMENTARY INFORMATION:

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR 
part 39 of with a notice of proposed rulemaking (NPRM) to supersede AD 
2009-22-13, Amendment 39-16066 (74 FR 55755, October 29, 2009). That AD 
applies to the specified products. The NPRM published in the Federal 
Register on March 14, 2011 (76 FR 13534). That NPRM would have 
continued to require an inspection to determine if certain motor 
operated valve actuators for the fuel tanks are installed, and related 
investigative and corrective actions if necessary. That proposed AD 
would have added airplanes and, for certain airplanes, required 
additional inspections to determine if certain motor operated valve 
actuators for the fuel tanks are installed, and related investigative 
and corrective actions if necessary. That NPRM resulted from fuel 
system reviews conducted by the manufacturer. The proposed actions were 
intended to prevent an ignition source inside the fuel tanks, which, in 
combination with flammable fuel vapors, could result in a fuel tank 
explosion and consequent loss of the airplane.

Actions Since NPRM (76 FR 13534, March 14, 2011) Was Issued

    Since we issued the NPRM (76 FR 13534, March 14, 2011), we 
discovered that the corrective action mandated by AD 2009-22-13, 
Amendment 39-16066 (74 FR 55755, October 29, 2009), and subsequently 
the corrective actions proposed by the NPRM, address that safety 
concern, but also introduce a different unsafe condition. The 
manufacturer is developing a more complete solution to address both 
unsafe conditions.
    Accordingly, we have determined that the NPRM (76 FR 13534, March 
14, 2011), must be withdrawn. In addition, we are considering further 
rulemaking to rescind AD 2009-22-13, Amendment 39-16066 (74 FR 55755, 
October 29, 2009), and will consider requiring a new solution once it 
is developed, approved, and available for accomplishment.

FAA's Conclusions

    Upon further consideration, we have determined that the existing AD 
does not properly address the safety concern. Accordingly, the NPRM (76 
FR 13534, March 14, 2011) is withdrawn.
    Withdrawal of the NPRM (76 FR 13534, March 14, 2011) does not 
preclude the FAA from issuing another related action or commit the FAA 
to any course of action in the future.

Regulatory Impact

    Since this action only withdraws an NPRM (76 FR 13534, March 14, 
2011), it is neither a proposed nor a final rule and therefore is not 
covered under Executive Order 12866, the Regulatory Flexibility Act, or 
DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 
1979).

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by 
reference, Safety.

The Withdrawal

    Accordingly, we withdraw the NPRM, Docket No. FAA-2011-0158, 
Directorate Identifier 2010-NM-118-AD, which was published in the 
Federal Register on March 14, 2011 (76 FR 13534).

    Issued in Renton, Washington, on July 31, 2012.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2012-19244 Filed 8-7-12; 8:45 am]
BILLING CODE 4910-13-P
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