80 FR 15947 - Airworthiness Directives; The Boeing Company Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 80, Issue 58 (March 26, 2015)
Federal Aviation Administration
Federal Register Volume 80, Issue 58 (March 26, 2015)
| Page Range | 15947-15951 | |
| FR Document | 2015-06745 |
[Federal Register Volume 80, Number 58 (Thursday, March 26, 2015)] [Proposed Rules] [Pages 15947-15951] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2015-06745] ======================================================================= ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2015-0249; Directorate Identifier 2014-NM-174-AD] RIN 2120-AA64 Airworthiness Directives; The Boeing Company Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). ----------------------------------------------------------------------- SUMMARY: We propose to supersede Airworthiness Directive (AD) 2012-18- 05, which applies to The Boeing Company Model DC-9-10, DC-9-20, DC-9- 30, DC-9-40, and DC-9-50 series airplanes; and Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), MD-88, and MD-90-30 airplanes; equipped with a center wing fuel tank and Boeing original equipment manufacturer-installed auxiliary fuel tanks. AD 2012-18-05 currently requires adding design features to detect electrical faults and to detect a pump running in an empty fuel tank. Since we issued AD 2012-18-05, we have determined that it is necessary to clarify the actions for airplanes on which the auxiliary fuel tanks are removed. This proposed AD would allow certain actions as optional methods of compliance. We are proposing this AD to reduce the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane. DATES: We must receive comments on this proposed AD by May 11, 2015. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods:Federal eRulemaking Portal: Go to http://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: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For service information identified in this proposed AD, contact Boeing Commercial Airplanes, Attention: Data & Services Management, 3855 [[Page 15948]] Lakewood Boulevard, MC D800-0019, Long Beach, CA 90846-0001; telephone 206-544-5000, extension 2; fax 206-766-5683; Internet https://www.myboeingfleet.com. You may view this referenced service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425-227-1221. It is also available on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2015- 0249. Examining the AD Docket You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2015- 0249; 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 (phone: 800-647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. FOR FURTHER INFORMATION CONTACT: S[eacute]rj Harutunian, Aerospace Engineer, Propulsion Branch, ANM-140L, FAA, Los Angeles Aircraft Certification Office (ACO), 3960 Paramount Boulevard, Lakewood, CA 90712-4137; phone: 562-627-5254; fax: 562-627-5210; email: [email protected]. 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-2015-0249; Directorate Identifier 2014-NM-174-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 http://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 August 6, 2012, we issued AD 2012-18-05, Amendment 39-17181 (77 FR 54793, September 6, 2012), for The Boeing Company Model DC-9-10, DC- 9-20, DC-9-30, DC-9-40, and DC-9-50 series airplanes; and Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), MD-88, and MD-90-30 airplanes; equipped with a center wing fuel tank and Boeing original equipment manufacturer-installed auxiliary fuel tanks. AD 2012-18-05 requires adding design features to detect electrical faults and to detect a pump running in an empty fuel tank. AD 2012-18-05 resulted from fuel system reviews conducted by the manufacturer. We issued AD 2012-18-05 to reduce the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane. Actions Since AD 2012-18-05, Amendment 39-17181 (77 FR 54793, September 6, 2012) Was Issued Since we issued AD 2012-18-05, Amendment 39-17181 (77 FR 54793, September 6, 2012), we have determined that it is necessary to clarify the actions for airplanes on which the auxiliary fuel tanks are removed. In addition, The Boeing Company has issued new service information for Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD- 83), DC-9-87 (MD-87), and Model MD-88 airplanes; and Model MD-90-30 airplanes, which provides a method of compliance for the actions required by AD 2012-18-05. Boeing has not yet issued corresponding service information for Boeing Model DC-9-10, DC-9-20, DC-9-30, DC-9- 40, and DC-9-50 series airplanes. The applicability of AD 2012-18-05 has not changed in this proposed AD. Related Service Information Under 1 CFR Part 51 We reviewed Boeing Service Bulletin MD80-28-228, dated September 27, 2013; and Boeing Service Bulletin MD90-28-013, dated September 27, 2013. The service information describes procedures for installing GFI relays that change fuel pump system wiring, installing a low fuel pressure indication system, and revising the inspection or maintenance program to include new limitations. We have also reviewed Appendixes B, C, and D of Boeing Special Compliance Item Report MDC-92K9145, Revision M, dated February 5, 2013, which includes Critical Design Configuration Control Limitations (CDCCLs), Airworthiness Limitations Instructions (ALIs), and short-term extensions. Boeing Service Bulletin MD80-28-228, dated September 27, 2013, specifies prior or concurrent accomplishment of the following concurrent service information. Boeing MD-80 Service Bulletin 28-53, Revision 1, dated April 16, 1992, which describes procedures for installing a low fuel pressure indication system. Boeing MD-80 Service Bulletin 28-63, Revision 2, dated April 8, 1992, which describes procedures for installing a low fuel pressure indication inhibit system. This service information is reasonably available; see ADDRESSES for ways to access this service information. Clarification of the Requirements for the Design Features In paragraph (c) of this proposed AD, we have added the text ``for airplanes on which auxiliary fuel tanks are removed, the AD action specified for the auxiliary fuel tanks are not required'' to clarify that the actions specified in this AD for the auxiliary fuel tanks are not required when the auxiliary fuel tanks are removed, but the AD actions for the center fuel tanks still apply. Revised Compliance Time We have determined that it is appropriate to allow additional time to accomplish the design features and requirements specified in this proposed AD. Therefore, we have added a compliance time of ``within 42 months after the effective date of this AD'' to paragraph (g) of this proposed AD. We have determined that this extension of the compliance time will provide an acceptable level of safety. FAA's Determination We are proposing this AD because we evaluated all the relevant information and determined the unsafe condition described previously is likely to exist or develop in other products of these same type designs. Proposed AD Requirements This proposed AD would retain all requirements of AD 2012-18-05, Amendment 39-17181 (77 FR 54793, September 6, 2012). This proposed AD would clarify the actions for airplanes on which the auxiliary fuel tanks are removed, that the actions specified for the auxiliary fuel tanks are not required. This proposed AD would also provide certain methods of compliance for the actions restated from AD 2012-18-05 (one option is accomplishing the actions [[Page 15949]] specified in the service information described previously, including revising the inspection or maintenance program, as applicable, to include new limitations; the other option is installing a supplemental type certificate (STC)). This proposed AD specifies to revise certain operator maintenance documents to include new actions (e.g., inspections) and CDCCLs. Compliance with these actions and CDCCLs is required by 14 CFR 91.403(c). For airplanes that have been previously modified, altered, or repaired in the areas addressed by this proposed AD, the operator may not be able to accomplish the actions described in the revisions. In this situation, to comply with 14 CFR 91.403(c), the operator must request approval for an alternative method of compliance according to paragraph (l) of this proposed AD. The request should include a description of changes to the required actions and CDCCLs that will ensure the continued operational safety of the airplane. Costs of Compliance We estimate that this proposed AD affects 809 airplanes of U.S. registry. We estimate the following costs to comply with this proposed AD: Estimated Costs ---------------------------------------------------------------------------------------------------------------- Cost per Cost on U.S. Action Labor cost Parts cost product operators ---------------------------------------------------------------------------------------------------------------- Installing design features for 50 work-hours x $85 per $35,000 $39,250 $10,322,750 airplanes with center wing and hour = $4,250. auxiliary tanks (263 airplanes), using a method approved by the FAA [retained actions from AD 2012[dash]18[dash]05, Amendment 39[dash]17181 (77 FR 54793, September 6, 2012)]. Installing design features for 35 work-hours x $85 per 17,000 19,975 10,906,350 airplanes with center wing tank (546 hour = $2,975. airplanes), using a method approved by the FAA [retained actions from AD 2012-18-05, Amendment 39[dash]17181 (77 FR 54793, September 6, 2012)]. ---------------------------------------------------------------------------------------------------------------- Estimated Costs: New Optional Actions for Installing Design Features ---------------------------------------------------------------------------------------------------------------- Cost per Action Labor cost Parts cost product ---------------------------------------------------------------------------------------------------------------- For airplanes with center wing and auxiliary 250 work-hours x $85 per hour = $69,000 $90,250 tanks, using service information specified in $21,250. paragraph (h) of this proposed AD (including revising the maintenance/inspection program). For airplanes with center wing tank, using 110 work-hours x $85 = 9,350.... 30,000 39,350 service information specified in paragraph (h) of this proposed AD (including revising the maintenance/inspection program). Installing STC specified in paragraph (i) of 35 work-hours x $85 per hour = 17,000 19,975 this proposed AD. $2,975. ---------------------------------------------------------------------------------------------------------------- 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 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. 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 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 removing Airworthiness Directive (AD) 2012-18-05, Amendment 39-17181 (77 FR 54793, September 6, 2012), and adding the following new AD: The Boeing Company: Docket No. FAA-2015-0249; Directorate Identifier 2014 NM-174-AD. (a) Comments Due Date The FAA must receive comments on this AD action by May 11, 2015. [[Page 15950]] (b) Affected ADs This AD replaces AD 2012-18-05, Amendment 39-17181 (77 FR 54793, September 6, 2012). (c) Applicability This AD applies to The Boeing Company airplanes identified in paragraphs (c)(1) through (c)(8) of this AD, certificated in any category, and equipped with center wing fuel tanks and Boeing original equipment manufacturer-installed auxiliary fuel tanks. For airplanes on which the auxiliary fuel tanks have been removed, the actions specified for the auxiliary fuel tanks are not required. (1) Model DC-9-11, DC-9-12, DC-9-13, DC-9-14, DC-9-15, and DC-9- 15F airplanes. (2) Model DC-9-21 airplanes. (3) Model DC-9-31, DC-9-32, DC-9-32 (VC-9C), DC-9-32F, DC-9-33F, DC-9-34, DC-9-34F, and DC-9-32F (C-9A, C 9B) airplanes. (4) Model DC-9-41 airplanes. (5) Model DC-9-51 airplanes. (6) Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and DC-9-87 (MD-87) airplanes. (7) Model MD-88 airplanes. (8) Model MD-90-30 airplanes. (d) Subject Air Transport Association (ATA) of America Code 28, Fuel. (e) Unsafe Condition This AD was prompted by fuel system reviews conducted by the manufacturer. We are issuing this AD to reduce the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Retained Criteria for Operation This paragraph restates the actions required by paragraph (g) of AD 2012-18-05, Amendment 39-17181 (77 FR 54793, September 6, 2012), with a new compliance time. Except as provided by paragraphs (h) and (i) of this AD: As of 42 months after the effective date of this AD, no person may operate any airplane affected by this AD unless an amended type certificate or supplemental type certificate that incorporates the design features and requirements described in paragraphs (g)(1) and (g)(2) of this AD has been approved by the Manager, Los Angeles Aircraft Certification Office (ACO), FAA, and those design features are installed on the airplane. (1) Each electrically powered fuel pump installed in the center wing tank or auxiliary fuel tank must have a protective device installed to detect electrical faults that can cause arcing and burn through the fuel pump housing. The same device must shut off the pump by automatically removing electrical power from the pump when such faults are detected. When a fuel pump is shut off as the result of detection of an electrical fault, the device must stay latched off until the fault is cleared through maintenance action and verified that the pump and the electrical power feed are safe for operation. (2) Additional design features must be installed to detect when any center wing tank or auxiliary fuel tank pump is running in an empty fuel tank. The prospective pump shutoff system must shut off each pump no later than 60 seconds after the fuel tank is emptied. The pump shutoff system design must preclude undetected running of a fuel pump in an empty tank, after the pump was commanded off manually or automatically. (h) New: Optional Methods of Compliance For Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC- 9-87 (MD-87), and Model MD-88 airplanes; and Model MD-90-30 airplanes: In lieu of doing the requirements of paragraph (g) of this AD, do the applicable actions specified in paragraphs (h)(1), (h)(2), and (h)(3) of this AD. (1) For Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and Model MD-88 airplanes: Do the applicable actions specified in paragraphs (h)(1)(i), (h)(1)(ii), and (h)(1)(iii) of this AD. (i) For all airplanes identified in paragraph (h)(1) of this AD: Within the compliance time specified in paragraph (g) of this AD, install ground fault interrupter (GFI) relays, in accordance with the Accomplishment Instructions of Boeing Service Bulletin MD80-28- 228, dated September 27, 2013. (ii) For airplanes identified in Boeing MD-80 Service Bulletin 28-53, Revision 1, dated April 16, 1992: Prior to or concurrently with accomplishing the action specified in paragraph (h)(1)(i) of this AD, install a low fuel pressure indication system, in accordance with the Accomplishment Instructions of Boeing MD-80 Service Bulletin 28-53, Revision 1, dated April 16, 1992. (iii) For airplanes identified in Boeing MD-80 Service Bulletin 28-63, Revision 2, dated April 8, 1992: Prior to or concurrently with accomplishing the action specified in paragraph (h)(1)(i) of this AD, install a low fuel pressure indication inhibition system, in accordance with the Accomplishment Instructions of Boeing MD-80 Service Bulletin 28-63, Revision 2, dated April 8, 1992. (2) For Model MD-90-30 airplanes: Within the compliance time specified in paragraph (g) of this AD, install brackets and mod block rails, and install GFI relays, in accordance with the Accomplishment Instructions of Boeing Service Bulletin MD90-28-013, dated September 27, 2013. (3) For all airplanes: Within 30 days after accomplishing the actions required by paragraph (h)(1) or (h)(2) of this AD or within 30 days after the effective date of this AD, whichever occurs later, revise the maintenance or inspection program, as applicable, to incorporate the Critical Design Configuration Control Limitations (CDCCLs), Airworthiness Limitations Instructions (ALIs), and short- term extensions specified in Appendixes B, C, and D of Boeing Special Compliance Item Report MDC-92K9145, Revision M, dated February 5, 2013. The initial compliance time for accomplishing the actions specified in the ALIs is at the later of the times in paragraphs (h)(3)(i) and (h)(3)(ii) of this AD. Doing the revision of the maintenance or inspection program, as applicable, required by this paragraph terminates the requirements in paragraphs (g) and (h) of AD 2008-11-15, Amendment 39-15538 (73 FR 30746, May 29, 2008). (i) At the applicable time specified in in Appendix C of Boeing Special Compliance Item Report MDC-92K9145, Revision M, dated February 5, 2013, except as provided by Appendix D, of Boeing Special Compliance Item Report MDC-92K9145, Revision M, dated February 5, 2013. (ii) Within 30 days after accomplishing the actions required by paragraph (h)(1) or (h)(2) of this AD, or within 30 days after the effective date of this AD, whichever occurs later. (i) New: Optional Universal Fault Interrupter (UFI) Installation In lieu of doing the requirements of paragraph (g) of this AD, within the compliance time specified in paragraph (g) of this AD install a TDG Aerospace Inc. UFI using a method approved in accordance with the procedures specified in paragraph (l) of this AD. Note 1 to paragraph (i) of this AD: TDG Aerospace STC ST02502LA ([http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0/ 4d132827a425d7de86257cd3004dfc02/$FILE/ST02502LA.pdf)] provides additional guidance for installing the TDG UFI. (j) No Alternative Actions, Intervals, and CDCCLs After the maintenance or inspection program, as applicable, has been revised as required by paragraph (h)(3) of this AD, no alternative actions (e.g., inspections), intervals, or CDCCLs may be used unless the actions, intervals, or CDCCLs are approved as an alternative method of compliance (AMOC) in accordance with the procedures specified in paragraph (l) of this AD. (k) Credit for Previous Actions This paragraph provides credit for the actions specified in paragraphs (h)(1)(ii) and (h)(1)(iii) of this AD, if those actions were performed before the effective date of this AD using any of the service information specified in paragraph (k)(1), (k)(2), or (k)(3) of this AD. (1) Boeing MD-80 Service Bulletin 28-53, dated April 8, 1991. (2) Boeing MD-80 Service Bulletin 28-63, dated, June 14, 1991. (3) Boeing MD-80 Service Bulletin 28-63, Revision 1, dated July 19, 1991. (l) Alternative Methods of Compliance (AMOCs) (1) The Manager, Los Angeles Aircraft Certification Office (ACO), FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the ACO, send it to the [[Page 15951]] attention of the person identified in paragraph (m)(1) of this AD. Information may be emailed to: [email protected]. (2) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. (3) An AMOC that provides an acceptable level of safety may be used for any repair required by this AD if it is approved by the Boeing Commercial Airplanes Organization Designation Authorization (ODA) that has been authorized by the Manager, Los Angeles ACO, to make those findings. For a repair method to be approved, the repair must meet the certification basis of the airplane, and the approval must specifically refer to this AD. (4) AMOCs approved for AD 2012-18-05, Amendment 39-17181 (77 FR 54793, September 6, 2012), are approved as AMOCs for the corresponding provisions of this AD. (m) Related Information (1) For more information about this AD, contact S[eacute]rj Harutunian, Aerospace Engineer, Propulsion Branch, ANM-140L, FAA, Los Angeles Aircraft Certification Office (ACO), 3960 Paramount Boulevard, Lakewood, CA 90712-4137; phone: 562-627-5254; fax: 562- 627-5210; email: [email protected]. (2) For service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Data & Services Management, 3855 Lakewood Boulevard, MC D800-0019, Long Beach, CA 90846-0001; telephone 206-544-5000, extension 2; fax 206-766-5683; Internet https://www.myboeingfleet.com. You may view this referenced service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425-227-1221. Issued in Renton, Washington, on February 11, 2015. Jeffrey E. Duven, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2015-06745 Filed 3-25-15; 8:45 am] BILLING CODE 4910-13-P
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(2) The report has been prepared in Securities Act. These filings include, DEPARTMENT OF TRANSPORTATION
accordance with all applicable statutory but are not limited to:
or regulatory requirements, and Federal Aviation Administration
(a) One paper and one electronic copy
(3) The information is true, accurate, of any offering circular, private
and complete to the best of signatories’ 14 CFR Part 39
placement memorandum, or
knowledge and belief. [Docket No. FAA–2015–0249; Directorate
information statement prepared in
(c) Distribution. The Corporation must Identifier 2014–NM–174–AD]
connection with the securities offering
distribute the signed report of condition
to all its shareholders within 90 days of at or before the time of the securities RIN 2120–AA64
its fiscal year-end. The Corporation offering.
(b) For securities backed by qualified Airworthiness Directives; The Boeing
must provide us one paper and one
Company Airplanes
electronic copy of every signed report loans as defined in section 8.0(9)(A) of
within 5 days of signing. If the report is the Act, one paper and one electronic AGENCY: Federal Aviation
the same as that filed with the SEC, the copy of the following within 1 business Administration (FAA), DOT.
Corporation may instead provide the day of the finalization of the transaction: ACTION: Notice of proposed rulemaking
signed reports to us only in electronic (1) The private placement memoranda (NPRM).
form and simultaneous with filing the for securities sold to investors; and
report with the SEC. SUMMARY: We propose to supersede
(1) The Corporation must publish a (2) The pooling and servicing Airworthiness Directive (AD) 2012–18–
copy of each report of condition on its agreement when the security is 05, which applies to The Boeing
Web site within 3 business days of filing purchased by the Corporation as Company Model DC–9–10, DC–9–20,
the report with us. The report must authorized by section 8.6(g) of the Act. DC–9–30, DC–9–40, and DC–9–50 series
remain on the Web site until the next (c) For securities backed by qualified airplanes; and Model DC–9–81 (MD–
report is posted. When the reports are loans as defined in section 8.0(9)(B) of 81), DC–9–82 (MD–82), DC–9–83 (MD–
the same as those filed with the SEC, the Act, the Corporation must provide 83), DC–9–87 (MD–87), MD–88, and
electronic links to the SEC filings Web summary information on such securities MD–90–30 airplanes; equipped with a
site, EDGAR, may be used in satisfaction issued during each calendar quarter in center wing fuel tank and Boeing
of this requirement. original equipment manufacturer-
the form prescribed by us. Such
(2) Upon receiving a request for an installed auxiliary fuel tanks. AD 2012–
summary information must be provided
annual report of condition from a 18–05 currently requires adding design
with each report of condition and
stockholder, investor, or the public, the features to detect electrical faults and to
performance filed pursuant to § 621.12, detect a pump running in an empty fuel
Corporation must promptly provide the
requester the most recent signed annual and at such other times as OSMO may tank. Since we issued AD 2012–18–05,
report issued in compliance with this require. we have determined that it is necessary
section. § 655.21 Filings and communications with to clarify the actions for airplanes on
the U.S. Treasury, the SEC, and NYSE. which the auxiliary fuel tanks are
§ 655.15 Interim reports, notices, and removed. This proposed AD would
proxy statements. (a) The Corporation must send us one allow certain actions as optional
(a) The Corporation must provide to paper and one electronic copy of every methods of compliance. We are
us one paper and one electronic copy of filing made with U.S. Treasury, the SEC, proposing this AD to reduce the
every interim report, notice, and proxy or NYSE, including financial statements potential of ignition sources inside fuel
statement filed with the SEC within 1 and related schedules, exhibits, and tanks, which, in combination with
business day of filing the item with the other documents that are a part of the flammable fuel vapors, could result in
SEC, including all papers and filing. Such copies must be filed with us fuel tank explosions and consequent
documents that are a part of the report, no later than 1 business day after any loss of the airplane.
notice, or statement. U.S. Treasury, SEC, or NYSE filing. If DATES: We must receive comments on
(b) The Corporation must publish a the filing is one addressed in subpart B this proposed AD by May 11, 2015.
copy of each interim report, notice, and of this part, no action under this ADDRESSES: You may send comments,
proxy statement on its Web site within
paragraph is required. using the procedures found in 14 CFR
5 business days of filing the
document(s) with the SEC. The interim (b) The Corporation must send us, 11.43 and 11.45, by any of the following
report, notice, or proxy statement must within 3 business days and according to methods:
remain on the Web site for 6 months or instructions provided by us, copies of • Federal eRulemaking Portal: Go to
until the next annual report of condition all substantive correspondence between http://www.regulations.gov. Follow the
is posted, whichever is later. Electronic the Corporation and the U.S. Treasury, instructions for submitting comments.
links to the SEC filings Web site, the SEC, or NYSE. • Fax: 202–493–2251.
• Mail: U.S. Department of
EDGAR, may be used in satisfaction of (c) The Corporation must notify us Transportation, Docket Operations, M–
this requirement. within 1 business day if it becomes 30, West Building Ground Floor, Room
Subpart C—Reports Relating to exempt or claims exemption from any W12–140, 1200 New Jersey Avenue SE.,
filing requirements of the Securities Act. Washington, DC 20590.
mstockstill on DSK4VPTVN1PROD with PROPOSALS
Securities Activities of the Federal
Agricultural Mortgage Corporation Dated: March 19, 2015. • Hand Delivery: Deliver to Mail
address above between 9 a.m. and 5
Dale L. Aultman,
§ 655.20 Securities not registered under p.m., Monday through Friday, except
the Securities Act. Secretary, Farm Credit Administration Board. Federal holidays.
The Corporation must make special [FR Doc. 2015–06755 Filed 3–25–15; 8:45 am] For service information identified in
filings with OSMO for securities either BILLING CODE 6705–01–P this proposed AD, contact Boeing
issued or guaranteed by the Corporation Commercial Airplanes, Attention: Data
that are not registered under the & Services Management, 3855
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specified in the service information required by 14 CFR 91.403(c). For request should include a description of
described previously, including revising airplanes that have been previously changes to the required actions and
the inspection or maintenance program, modified, altered, or repaired in the CDCCLs that will ensure the continued
as applicable, to include new areas addressed by this proposed AD, operational safety of the airplane.
limitations; the other option is installing the operator may not be able to
a supplemental type certificate (STC)). accomplish the actions described in the Costs of Compliance
This proposed AD specifies to revise revisions. In this situation, to comply
We estimate that this proposed AD
certain operator maintenance with 14 CFR 91.403(c), the operator
documents to include new actions (e.g., affects 809 airplanes of U.S. registry.
must request approval for an alternative
inspections) and CDCCLs. Compliance method of compliance according to We estimate the following costs to
with these actions and CDCCLs is paragraph (l) of this proposed AD. The comply with this proposed AD:
ESTIMATED COSTS
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
Installing design features for airplanes with center wing and 50 work-hours × $85 per hour $35,000 $39,250 $10,322,750
auxiliary tanks (263 airplanes), using a method approved = $4,250.
by the FAA [retained actions from AD 2012-18-05,
Amendment 39-17181 (77 FR 54793, September 6,
2012)].
Installing design features for airplanes with center wing tank 35 work-hours × $85 per hour 17,000 19,975 10,906,350
(546 airplanes), using a method approved by the FAA [re- = $2,975.
tained actions from AD 2012–18–05, Amendment
39-17181 (77 FR 54793, September 6, 2012)].
ESTIMATED COSTS: NEW OPTIONAL ACTIONS FOR INSTALLING DESIGN FEATURES
Cost per
Action Labor cost Parts cost product
For airplanes with center wing and auxiliary tanks, using service infor- 250 work-hours × $85 per hour = $69,000 $90,250
mation specified in paragraph (h) of this proposed AD (including re- $21,250.
vising the maintenance/inspection program).
For airplanes with center wing tank, using service information specified 110 work-hours × $85 = 9,350 ........ 30,000 39,350
in paragraph (h) of this proposed AD (including revising the mainte-
nance/inspection program).
Installing STC specified in paragraph (i) of this proposed AD .................. 35 work-hours × $85 per hour = 17,000 19,975
$2,975.
Authority for This Rulemaking implications under Executive Order The Proposed Amendment
Title 49 of the United States Code 13132. This proposed AD would not
have a substantial direct effect on the Accordingly, under the authority
specifies the FAA’s authority to issue delegated to me by the Administrator,
rules on aviation safety. Subtitle I, States, on the relationship between the
national Government and the States, or the FAA proposes to amend 14 CFR part
Section 106, describes the authority of
on the distribution of power and 39 as follows:
the FAA Administrator. Subtitle VII,
Aviation Programs, describes in more responsibilities among the various
levels of government. PART 39—AIRWORTHINESS
detail the scope of the Agency’s DIRECTIVES
authority. For the reasons discussed above, I
We are issuing this rulemaking under certify that the proposed regulation:
(1) Is not a ‘‘significant regulatory ■ 1. The authority citation for part 39
the authority described in Subtitle VII,
Part A, Subpart III, Section 44701, action’’ under Executive Order 12866, continues to read as follows:
‘‘General requirements.’’ Under that (2) Is not a ‘‘significant rule’’ under Authority: 49 U.S.C. 106(g), 40113, 44701.
section, Congress charges the FAA with the DOT Regulatory Policies and
promoting safe flight of civil aircraft in Procedures (44 FR 11034, February 26, § 39.13 [Amended]
air commerce by prescribing regulations 1979), ■ 2. The FAA amends § 39.13 by
for practices, methods, and procedures (3) Will not affect intrastate aviation removing Airworthiness Directive (AD)
the Administrator finds necessary for in Alaska, and 2012–18–05, Amendment 39–17181 (77
safety in air commerce. This regulation (4) Will not have a significant FR 54793, September 6, 2012), and
economic impact, positive or negative,
mstockstill on DSK4VPTVN1PROD with PROPOSALS
is within the scope of that authority adding the following new AD:
because it addresses an unsafe condition on a substantial number of small entities
that is likely to exist or develop on under the criteria of the Regulatory The Boeing Company: Docket No. FAA–
products identified in this rulemaking Flexibility Act. 2015–0249; Directorate Identifier 2014
action. NM–174–AD.
List of Subjects in 14 CFR Part 39
Regulatory Findings (a) Comments Due Date
Air transportation, Aircraft, Aviation
The FAA must receive comments on this
We have determined that this safety, Incorporation by reference,
AD action by May 11, 2015.
proposed AD would not have federalism Safety.
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![15950 Federal Register / Vol. 80, No. 58 / Thursday, March 26, 2015 / Proposed Rules
(b) Affected ADs device must stay latched off until the fault is initial compliance time for accomplishing the
This AD replaces AD 2012–18–05, cleared through maintenance action and actions specified in the ALIs is at the later
Amendment 39–17181 (77 FR 54793, verified that the pump and the electrical of the times in paragraphs (h)(3)(i) and
September 6, 2012). power feed are safe for operation. (h)(3)(ii) of this AD. Doing the revision of the
(2) Additional design features must be maintenance or inspection program, as
(c) Applicability installed to detect when any center wing tank applicable, required by this paragraph
This AD applies to The Boeing Company or auxiliary fuel tank pump is running in an terminates the requirements in paragraphs (g)
airplanes identified in paragraphs (c)(1) empty fuel tank. The prospective pump and (h) of AD 2008–11–15, Amendment 39–
through (c)(8) of this AD, certificated in any shutoff system must shut off each pump no 15538 (73 FR 30746, May 29, 2008).
category, and equipped with center wing fuel later than 60 seconds after the fuel tank is (i) At the applicable time specified in in
tanks and Boeing original equipment emptied. The pump shutoff system design Appendix C of Boeing Special Compliance
manufacturer-installed auxiliary fuel tanks. must preclude undetected running of a fuel Item Report MDC–92K9145, Revision M,
For airplanes on which the auxiliary fuel pump in an empty tank, after the pump was dated February 5, 2013, except as provided
tanks have been removed, the actions commanded off manually or automatically. by Appendix D, of Boeing Special
specified for the auxiliary fuel tanks are not Compliance Item Report MDC–92K9145,
(h) New: Optional Methods of Compliance Revision M, dated February 5, 2013.
required.
For Model DC–9–81 (MD–81), DC–9–82 (ii) Within 30 days after accomplishing the
(1) Model DC–9–11, DC–9–12, DC–9–13,
(MD–82), DC–9–83 (MD–83), DC–9–87 (MD– actions required by paragraph (h)(1) or (h)(2)
DC–9–14, DC–9–15, and DC–9–15F airplanes.
87), and Model MD–88 airplanes; and Model of this AD, or within 30 days after the
(2) Model DC–9–21 airplanes.
MD–90–30 airplanes: In lieu of doing the effective date of this AD, whichever occurs
(3) Model DC–9–31, DC–9–32, DC–9–32
requirements of paragraph (g) of this AD, do later.
(VC–9C), DC–9–32F, DC–9–33F, DC–9–34,
the applicable actions specified in
DC–9–34F, and DC–9–32F (C–9A, C 9B) (i) New: Optional Universal Fault
paragraphs (h)(1), (h)(2), and (h)(3) of this
airplanes. Interrupter (UFI) Installation
AD.
(4) Model DC–9–41 airplanes. In lieu of doing the requirements of
(1) For Model DC–9–81 (MD–81), DC–9–82
(5) Model DC–9–51 airplanes. paragraph (g) of this AD, within the
(MD–82), DC–9–83 (MD–83), DC–9–87 (MD–
(6) Model DC–9–81 (MD–81), DC–9–82 compliance time specified in paragraph (g) of
87), and Model MD–88 airplanes: Do the
(MD–82), DC–9–83 (MD–83), and DC–9–87 this AD install a TDG Aerospace Inc. UFI
applicable actions specified in paragraphs
(MD–87) airplanes. using a method approved in accordance with
(h)(1)(i), (h)(1)(ii), and (h)(1)(iii) of this AD.
(7) Model MD–88 airplanes. the procedures specified in paragraph (l) of
(i) For all airplanes identified in paragraph
(8) Model MD–90–30 airplanes. this AD.
(h)(1) of this AD: Within the compliance time
(d) Subject specified in paragraph (g) of this AD, install Note 1 to paragraph (i) of this AD: TDG
Air Transport Association (ATA) of ground fault interrupter (GFI) relays, in Aerospace STC ST02502LA ([http://
America Code 28, Fuel. accordance with the Accomplishment rgl.faa.gov/Regulatory_and_Guidance_
Instructions of Boeing Service Bulletin Library/rgstc.nsf/0/
(e) Unsafe Condition MD80–28–228, dated September 27, 2013. 4d132827a425d7de86257cd3004dfc02/
This AD was prompted by fuel system (ii) For airplanes identified in Boeing MD– $FILE/ST02502LA.pdf)] provides additional
reviews conducted by the manufacturer. We 80 Service Bulletin 28–53, Revision 1, dated guidance for installing the TDG UFI.
are issuing this AD to reduce the potential of April 16, 1992: Prior to or concurrently with
ignition sources inside fuel tanks, which, in accomplishing the action specified in (j) No Alternative Actions, Intervals, and
combination with flammable fuel vapors, paragraph (h)(1)(i) of this AD, install a low CDCCLs
could result in fuel tank explosions and fuel pressure indication system, in After the maintenance or inspection
consequent loss of the airplane. accordance with the Accomplishment program, as applicable, has been revised as
Instructions of Boeing MD–80 Service required by paragraph (h)(3) of this AD, no
(f) Compliance Bulletin 28–53, Revision 1, dated April 16, alternative actions (e.g., inspections),
Comply with this AD within the 1992. intervals, or CDCCLs may be used unless the
compliance times specified, unless already (iii) For airplanes identified in Boeing MD– actions, intervals, or CDCCLs are approved as
done. 80 Service Bulletin 28–63, Revision 2, dated an alternative method of compliance (AMOC)
April 8, 1992: Prior to or concurrently with in accordance with the procedures specified
(g) Retained Criteria for Operation accomplishing the action specified in in paragraph (l) of this AD.
This paragraph restates the actions paragraph (h)(1)(i) of this AD, install a low
required by paragraph (g) of AD 2012–18–05, fuel pressure indication inhibition system, in (k) Credit for Previous Actions
Amendment 39–17181 (77 FR 54793, accordance with the Accomplishment This paragraph provides credit for the
September 6, 2012), with a new compliance Instructions of Boeing MD–80 Service actions specified in paragraphs (h)(1)(ii) and
time. Except as provided by paragraphs (h) Bulletin 28–63, Revision 2, dated April 8, (h)(1)(iii) of this AD, if those actions were
and (i) of this AD: As of 42 months after the 1992. performed before the effective date of this AD
effective date of this AD, no person may (2) For Model MD–90–30 airplanes: Within using any of the service information specified
operate any airplane affected by this AD the compliance time specified in paragraph in paragraph (k)(1), (k)(2), or (k)(3) of this AD.
unless an amended type certificate or (g) of this AD, install brackets and mod block (1) Boeing MD–80 Service Bulletin 28–53,
supplemental type certificate that rails, and install GFI relays, in accordance dated April 8, 1991.
incorporates the design features and with the Accomplishment Instructions of (2) Boeing MD–80 Service Bulletin 28–63,
requirements described in paragraphs (g)(1) Boeing Service Bulletin MD90–28–013, dated dated, June 14, 1991.
and (g)(2) of this AD has been approved by September 27, 2013. (3) Boeing MD–80 Service Bulletin 28–63,
the Manager, Los Angeles Aircraft (3) For all airplanes: Within 30 days after Revision 1, dated July 19, 1991.
Certification Office (ACO), FAA, and those accomplishing the actions required by
design features are installed on the airplane. paragraph (h)(1) or (h)(2) of this AD or within (l) Alternative Methods of Compliance
(1) Each electrically powered fuel pump 30 days after the effective date of this AD, (AMOCs)
mstockstill on DSK4VPTVN1PROD with PROPOSALS
installed in the center wing tank or auxiliary whichever occurs later, revise the (1) The Manager, Los Angeles Aircraft
fuel tank must have a protective device maintenance or inspection program, as Certification Office (ACO), FAA, has the
installed to detect electrical faults that can applicable, to incorporate the Critical Design authority to approve AMOCs for this AD, if
cause arcing and burn through the fuel pump Configuration Control Limitations (CDCCLs), requested using the procedures found in 14
housing. The same device must shut off the Airworthiness Limitations Instructions CFR 39.19. In accordance with 14 CFR 39.19,
pump by automatically removing electrical (ALIs), and short-term extensions specified in send your request to your principal inspector
power from the pump when such faults are Appendixes B, C, and D of Boeing Special or local Flight Standards District Office, as
detected. When a fuel pump is shut off as the Compliance Item Report MDC–92K9145, appropriate. If sending information directly
result of detection of an electrical fault, the Revision M, dated February 5, 2013. The to the manager of the ACO, send it to the
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![Federal Register / Vol. 80, No. 58 / Thursday, March 26, 2015 / Proposed Rules 15951
attention of the person identified in enable DOJ investigative agencies to public docket, you must include the
paragraph (m)(1) of this AD. Information may collect and maintain records of potential phrase ‘‘PERSONALLY IDENTIFYING
be emailed to: 9-ANM-LAACO-AMOC- impeachment information and to INFORMATION’’ in the first paragraph
Requests@faa.gov. of your comment. You must also place
disclose such information to DOJ
(2) Before using any approved AMOC,
notify your appropriate principal inspector, prosecuting offices in order to ensure all the personally identifying
or lacking a principal inspector, the manager that prosecutors receive sufficient information you do not want posted
of the local flight standards district office/ information to meet their obligations online or made available in the public
certificate holding district office. under Giglio v. United States, 405 U.S. docket in the first paragraph of your
(3) An AMOC that provides an acceptable 150 (1972), as well as to enable DOJ comment and identify what information
level of safety may be used for any repair prosecuting offices to maintain records you want redacted.
required by this AD if it is approved by the of potential impeachment information If you want to submit confidential
Boeing Commercial Airplanes Organization business information as part of your
obtained from DOJ investigative
Designation Authorization (ODA) that has comment, but do not want it to be
been authorized by the Manager, Los Angeles agencies, other federal agencies, and
ACO, to make those findings. For a repair state and local agencies and to disclose posted online or made available in the
method to be approved, the repair must meet such information in accordance with the public docket, you must include the
the certification basis of the airplane, and the Giglio decision. For the reasons phrase ‘‘CONFIDENTIAL BUSINESS
approval must specifically refer to this AD. provided below, the Department INFORMATION’’ in the first paragraph
(4) AMOCs approved for AD 2012–18–05, proposes to amend its Privacy Act of your comment. You must also
Amendment 39–17181 (77 FR 54793, regulations by establishing an prominently identify confidential
September 6, 2012), are approved as AMOCs exemption for records in this system business information to be redacted
for the corresponding provisions of this AD. within the comment. If a comment has
from certain provisions of the Privacy
(m) Related Information Act pursuant to 5 U.S.C. 552a(j) and (k). so much confidential business
(1) For more information about this AD, DATES: Comments must be received by information that it cannot be effectively
contact Sérj Harutunian, Aerospace Engineer, April 27, 2015. redacted, all or part of that comment
Propulsion Branch, ANM–140L, FAA, Los may not be posted online or made
ADDRESSES: Address all comments to
Angeles Aircraft Certification Office (ACO), available in the public docket.
the Privacy Analyst, Office of Privacy Personally identifying information
3960 Paramount Boulevard, Lakewood, CA
90712–4137; phone: 562–627–5254; fax: 562– and Civil Liberties, National Place and confidential business information
627–5210; email: serj.harutunian@faa.gov. Building, 1331 Pennsylvania Avenue identified and located as set forth above
(2) For service information identified in NW., Suite 1000, Washington, DC will be redacted and the comment, in
this AD, contact Boeing Commercial 20530, or by facsimile to (202) 307– redacted form, will be posted online and
Airplanes, Attention: Data & Services 0693. To ensure proper handling, please placed in the Department’s public
Management, 3855 Lakewood Boulevard, MC reference the CPCLO Order Number on
D800–0019, Long Beach, CA 90846–0001; docket file. Please note that the Freedom
your correspondence. You may review of Information Act applies to all
telephone 206–544–5000, extension 2; fax an electronic version of the proposed
206–766–5683; Internet https:// comments received. If you wish to
rule at http://www.regulations.gov, and inspect the agency’s public docket file
www.myboeingfleet.com. You may view this
referenced service information at the FAA, you may also comment by using that in person by appointment, please see
Transport Airplane Directorate, 1601 Lind Web site’s comment form for this the FOR FURTHER INFORMATION CONTACT
Avenue SW., Renton, WA. For information regulation. Please include the CPCLO paragraph.
on the availability of this material at the Order Number in the subject box.
FAA, call 425–227–1221. Please note that the Department is FOR FURTHER INFORMATION CONTACT:
requesting that electronic comments be Tricia Francis, Executive Office for
Issued in Renton, Washington, on February
11, 2015. submitted before midnight Eastern Time United States Attorneys, FOIA/Privacy
on the day the comment period closes Act Staff, 600 E Street NW., Suite 7300,
Jeffrey E. Duven,
because this is when http:// Washington, DC 20530, or by facsimile
Manager, Transport Airplane Directorate,
www.regulations.gov terminates the at (202) 252–6047.
Aircraft Certification Service.
public’s ability to submit comments. SUPPLEMENTARY INFORMATION: In the
[FR Doc. 2015–06745 Filed 3–25–15; 8:45 am]
Commenters in time zones other than notices section of this issue of the
BILLING CODE 4910–13–P
Eastern Time may want to consider this Federal Register, the Department of
so that their electronic comments are Justice has published a system of
received. All comments sent via regular records notice for the system entitled,
DEPARTMENT OF JUSTICE or express mail will be considered ‘‘Department of Justice Giglio
timely if postmarked on or before the Information Files,’’ JUSTICE/DOJ–017.
28 CFR Part 16
day the comment period closes. This Department-wide system notice
[CPCLO Order No. 004–2014] Posting of Public Comments: Please replaces the notice for the system
note that all comments received are entitled, ‘‘United States Attorney’s
Privacy Act of 1974; Implementation considered part of the public record and Office, Giglio Information Files,’’
AGENCY: Department of Justice. made available for public inspection JUSTICE/USA–018, 65 FR 75308 (Dec.
ACTION: Notice of proposed rulemaking. online at http://www.regulations.gov 1, 2000). That system of records was
and in the Department’s public docket. exempt from certain provisions of the
SUMMARY: As described in the notice Such information includes personally Privacy Act pursuant to 5 U.S.C. 552a(j)
mstockstill on DSK4VPTVN1PROD with PROPOSALS
section of this issue of the Federal identifying information (such as your and (k). Those exemptions are codified
Register, the Department of Justice name, address, etc.) voluntarily in the Code of Federal Regulations
(Department or DOJ) has published a submitted by the commenter. (CFR) section for Exemption of United
notice of a new Department-wide If you want to submit personally States Attorneys Systems (28 CFR
Privacy Act system of records, identifying information (such as your 16.81(g) and (h)). The Department is
‘‘Department of Justice, Giglio name, address, etc.) as part of your now proposing to establish a new CFR
Information Files,’’ JUSTICE/DOJ–017. comment, but do not want it to be section for exemptions of the JUSTICE/
This system has been established to posted online or made available in the DOJ–017 system (28 CFR 16.136) and to
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Document Created: 2015-12-18 11:46:45
Document Modified: 2015-12-18 11:46:45
| Category | Regulatory Information | |
| Collection | Federal Register | |
| sudoc Class | AE 2.7: GS 4.107: AE 2.106: | |
| Publisher | Office of the Federal Register, National Archives and Records Administration | |
| Section | Proposed Rules | |
| Action | Notice of proposed rulemaking (NPRM). | |
| Dates | We must receive comments on this proposed AD by May 11, 2015. | |
| Contact | S[eacute]rj Harutunian, Aerospace Engineer, Propulsion Branch, ANM-140L, FAA, Los Angeles Aircraft Certification Office (ACO), 3960 Paramount Boulevard, Lakewood, CA 90712-4137; phone: 562-627-5254; fax: 562-627-5210; email: [email protected] | |
| FR Citation | 80 FR 15947 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft and Aviation Safety |
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