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Federal Register/Vol. 66, No. 42/Friday, March 2, 2001

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Federal Register/Vol. 66, No. 42/Friday, March 2, 2001 Federal Register / Vol. 66, No. 42 / Friday, March 2, 2001 / Proposed Rules 13189 Model/Series STC number Docket number Boeing 767–200 ................................................................................................................................... ST09022AC–D 2000–NM–243–AD Boeing 747SP ...................................................................................................................................... ST09097AC–D 2000–NM–244–AD Boeing 747–400 ................................................................................................................................... SA8843SW 2000–NM–245–AD Airbus A340–211 .................................................................................................................................. ST0902AC–D 2000–NM–246–AD Cost Impact location provided under the caption and remove the system from the airplane, in ADDRESSES. accordance with Hollingsead International There are approximately 6 airplanes Service Bulletin 2526–2332–001, dated July of the affected design in the worldwide List of Subjects in 14 CFR Part 39 19, 2000. fleet. The FAA estimates that 3 Air transportation, Aircraft, Aviation Spares airplanes of U.S. registry would be safety, Safety. affected by this proposed AD, that it (b) As of the effective date of this AD, no would take approximately 4 work hours The Proposed Amendment person shall install an IFE system in accordance with STC SA8026NM on any per airplane to accomplish the proposed Accordingly, pursuant to the airplane. actions, and that the average labor rate authority delegated to me by the is $60 per work hour. Based on these Administrator, the Federal Aviation Alternative Methods of Compliance figures, the cost impact of the proposed Administration proposes to amend part (c) An alternative method of compliance or AD on U.S. operators is estimated to be 39 of the Federal Aviation Regulations adjustment of the compliance time that $720, or $240 per airplane. (14 CFR part 39) as follows: provides an acceptable level of safety may be The cost impact figure discussed used if approved by the Manager, Los Angeles Aircraft Certification Office (ACO), above is based on assumptions that no PART 39—AIRWORTHINESS DIRECTIVES FAA. Operators shall submit their requests operator has yet accomplished any of through an appropriate FAA Principal the proposed requirements of this AD 1. The authority citation for part 39 Maintenance Inspector, who may add action, and that no operator would continues to read as follows: comments and then send it to the Manager, accomplish those actions in the future if Los Angeles ACO. Authority: 19 U.S.C. 106(g), 40113, 44701. this proposed AD were not adopted. The Note 2: Information concerning the cost impact figures discussed in AD § 39.13 [Amended] existence of approved alternative methods of rulemaking actions represent only the 2. Section 39.13 is amended by compliance with this AD, if any, may be obtained from the Los Angeles ACO. time necessary to perform the specific adding the following new airworthiness actions actually required by the AD. directive: Special Flight Permits These figures typically do not include McDonnell Douglas: Docket 2000–NM–229– incidental costs, such as the time (d) Special flight permits may be issued in AD. accordance with §§ 21.197 and 21.199 of the required to gain access and close up, Applicability: Model DC–9–51 and DC–9– Federal Aviation Regulations (14 CFR 21.197 planning time, or time necessitated by 83 series airplanes modified by and 21.199) to operate the airplane to a other administrative actions. Supplemental Type Certificate (STC) location where the requirements of this AD Regulatory Impact SA8026NM, certificated in any category. can be accomplished. Note 1: This AD applies to each airplane Issued in Renton, Washington, on February The regulations proposed herein identified in the preceding applicability 23, 2001. would not have a substantial direct provision, regardless of whether it has been Donald L. Riggin, effect on the States, on the relationship otherwise modified, altered, or repaired in the area subject to the requirements of this Acting Manager, Transport Airplane between the national Government and Directorate, Aircraft Certification Service. the States, or on the distribution of AD. For airplanes that have been modified, [FR Doc. 01–4941 Filed 3–1–01; 8:45 am] power and responsibilities among the altered, or repaired so that the performance of the requirements of this AD is affected, the BILLING CODE 4910–13–P various levels of government. Therefore, owner/operator must request approval for an it is determined that this proposal alternative method of compliance in would not have federalism implications accordance with paragraph (c) of this AD. DEPARTMENT OF TRANSPORTATION under Executive Order 13132. The request should include an assessment of For the reasons discussed above, I the effect of the modification, alteration, or Federal Aviation Administration certify that this proposed regulation (1) repair on the unsafe condition addressed by is not a ‘‘significant regulatory action’’ this AD; and, if the unsafe condition has not been eliminated, the request should include 14 CFR Part 39 under Executive Order 12866; (2) is not specific proposed actions to address it. [Docket No. 2000–NM–231–AD] a ‘‘significant rule’’ under the DOT Compliance: Required as indicated, unless Regulatory Policies and Procedures (44 accomplished previously. RIN 2120–AA64 FR 11034, February 26, 1979); and (3) if To prevent the inability of the flight crew promulgated, will not have a significant to remove power from the in-flight Airworthiness Directives; McDonnell economic impact, positive or negative, entertainment (IFE) system when necessary; Douglas Model DC–10–30 Series on a substantial number of small entities which, during a non-normal or emergency Airplanes Modified by Supplemental under the criteria of the Regulatory situation, could result in inability to control Type Certificate ST00054SE Flexibility Act. A copy of the draft smoke or fumes in the airplane flight deck or cabin; accomplish the following: AGENCY: Federal Aviation regulatory evaluation prepared for this Administration, DOT. action is contained in the Rules Docket. Deactivation and Removal ACTION: Notice of proposed rulemaking A copy of it may be obtained by (a) Within 18 months after the effective (NPRM). contacting the Rules Docket at the date of this AD, deactivate the IFE system VerDate 11<MAY>2000 16:49 Mar 01, 2001 Jkt 194001 PO 00000 Frm 00007 Fmt 4701 Sfmt 4702 E:\FR\FM\02MRP2.SGM pfrm01 PsN: 02MRP2 13190 Federal Register / Vol. 66, No. 42 / Friday, March 2, 2001 / Proposed Rules SUMMARY: This document proposes the Submit comments using the following total passenger seats were also adoption of a new airworthiness format: considered for the review. The types of directive (AD) that is applicable to all • Organize comments issue-by-issue. IFE systems not considered for review McDonnell Douglas Model DC–10–30 For example, discuss a request to include systems that provide only audio series airplanes modified by change the compliance time and a signals to each passenger seat, ordinary supplemental type certificate (STC) request to change the service bulletin in-flight telephone systems (e.g., one ST00054SE. This proposal would reference as two separate issues. telephone handset per group of seats or require removal of the in-flight • For each issue, state what specific bulkhead-mounted telephones), systems entertainment (IFE) system installed by change to the proposed AD is being that only have a video monitor on the that STC. This action is necessary to requested. forward bulkhead(s) (or a projection • prevent inability of the flight crew to Include justification (e.g., reasons or system) to provide passengers with remove power from the IFE system data) for each request. basic airplane and flight information, when necessary. Inability to remove Comments are specifically invited on and in-seat power supply systems that power from the IFE system during a the overall regulatory, economic, provide power to less than 20 percent of non-normal or emergency situation environmental, and energy aspects of the total passenger seats. could result in inability to control the proposed rule. All comments Items considered during the review smoke or fumes in the airplane flight submitted will be available, both before include the following: deck or cabin. This action is intended to and after the closing date for comments, • Can the electrical bus(es) supplying address the identified unsafe condition. in the Rules Docket for examination by power to the IFE system be deenergized interested persons. A report when necessary without removing DATES: Comments must be received by summarizing each FAA-public contact April 16, 2001. power from systems that may be concerned with the substance of this required for continued safe flight and ADDRESSES: Submit comments in proposal will be filed in the Rules landing? triplicate to the Federal Aviation Docket. • Can IFE system power be removed Administration (FAA), Transport Commenters wishing the FAA to when required without pulling IFE Airplane Directorate, ANM–114, acknowledge receipt of their comments system circuit breakers? [i.e., is there a Attention: Rules Docket No. 2000–NM– submitted in response to this action switch (dedicated to the IFE system or 231–AD, 1601 Lind Avenue, SW., must submit a self-addressed, stamped a combination of loads) located in the Renton, Washington
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