83 FR 59290 - Airworthiness Directives; Zodiac Aero Evacuation Systems (also known as Air Cruisers Company)
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 83, Issue 226 (November 23, 2018)
Federal Aviation Administration
Federal Register Volume 83, Issue 226 (November 23, 2018)
| Page Range | 59290-59295 | |
| FR Document | 2018-25003 |
[Federal Register Volume 83, Number 226 (Friday, November 23, 2018)] [Rules and Regulations] [Pages 59290-59295] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2018-25003] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2016-9392; Product Identifier 2016-NM-003-AD; Amendment 39-19499; AD 2018-23-12] RIN 2120-AA64 Airworthiness Directives; Zodiac Aero Evacuation Systems (also known as Air Cruisers Company) AGENCY: Federal Aviation Administration (FAA), DOT. [[Page 59291]] ACTION: Final rule. ----------------------------------------------------------------------- SUMMARY: We are adopting a new airworthiness directive (AD) for Zodiac Aero Evacuation Systems (also known as Air Cruisers Company) fusible plugs installed on emergency evacuation equipment for various transport category airplanes. This AD was prompted by reports indicating that affected fusible plugs activated (vented gas) below the rated temperature. This AD requires an inspection of the fusible plugs to determine the part number and lot number, and replacement of all affected fusible plugs. We are issuing this AD to address the unsafe condition on these products. DATES: This AD is effective December 28, 2018. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of December 28, 2018. ADDRESSES: For service information identified in this final rule, contact Air Cruisers, 1747 State Route 34, Wall Township, NJ 07727- 3935; phone 732-681-3527; email [email protected]. You may view this service information at the FAA, Transport Standards Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. It is also available on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-9392. 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-2016- 9392; or in person at Docket Operations between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this final rule, the regulatory evaluation, any comments received, and other information. The address for Docket Operations (phone: 800-647- 5527) is 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: Darren Gassetto, Aerospace Engineer, Mechanical Systems and Admin Services Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7323; fax 516-794-5531; email [email protected]. SUPPLEMENTARY INFORMATION: Discussion We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to Zodiac Aero Evacuation Systems (also known as Air Cruisers Company) fusible plugs installed on emergency evacuation equipment for various transport category airplanes. The NPRM published in the Federal Register on November 18, 2016 (81 FR 81709). The NPRM was prompted by reports indicating that affected fusible plugs activated (vented gas) below the rated temperature. The NPRM proposed to require an inspection of the fusible plugs to determine the part number and lot number, and replacement of all affected fusible plugs. We subsequently issued a supplemental NPRM (SNPRM) that was published in the Federal Register on January 24, 2018 (83 FR 3283). The SNPRM proposed to extend the compliance time, clarify the applicability, and clarify certain requirements. We are issuing this AD to address fusible plugs that might activate below the rated temperature and render the evacuation system unusable. Comments We gave the public the opportunity to participate in developing this final rule. The following presents the comments received on the SNPRM and the FAA's response to each comment. Request to Extend Compliance Time Airlines for America (A4A), on behalf of its members, requested that we extend the compliance time specified in paragraph (h) of the proposed AD (in the SNPRM). A4A stated that the extended compliance time of 42 months after the effective date (in paragraph (g) of the proposed AD (in the SNPRM)) had an unintended consequence in the re- worded compliance paragraph (h) of the proposed AD (in the SNPRM). A4A noted that while the allowance for maintenance records inspection was added, the words ``[b]efore further flight'' remained. A4A concluded that the current version means that either a planeside finding or a maintenance records discovery will each require action before further flight. A4A stated that while a finding by direct inspection will happen only in a shop and not affect operation of any aircraft, the accommodation for records review could immediately ground an in-service aircraft. A4A requested that we allow 42 months for the replacement if a records review was done. We agree to revise the compliance time in paragraph (h) of this AD because we have determined that a compliance time of 42 months to replace the affected part addresses the unsafe condition and provides an acceptable level of safety. We have revised paragraph (h) of the AD to specify a 42-month compliance time for the replacement. Request To Specify Serial Numbers All Nippon Airways (ANA) requested that we revise paragraph (c) of the proposed AD (in the SNPRM) to refer to service information that specifies the serial numbers and not only the part numbers of the affected emergency equipment. ANA stated that identifying affected [parts] by only the part number means that even after expiration of the compliance time specified in the proposed AD, the inspection must be continued every time the affected emergency equipment is purchased. ANA stated that the serial number of the affected emergency equipment should be specified in the service information listed in paragraph (c) of the proposed AD (in the SNPRM) in order to prevent endless inspections. We do not agree because specific serial numbers for the affected emergency equipment have not been identified. In addition, since the fusible plugs are rotable we cannot limit the applicability to only the known emergency equipment on which the fusible plugs were initially installed. Therefore, in order to address the identified unsafe condition, all fusible plugs installed on emergency evacuation equipment identified in the service information specified in paragraph (c) of this AD must be inspected as specified in paragraph (g) of this AD. When installing new equipment on an airplane, operators must ensure the newly installed part is not one of the affected parts by complying with the parts installation prohibition specified in paragraph (i) of this AD. We have not changed this AD in this regard. Request To Refer to Service Information Southwest Airlines (SWA) and A4A, on behalf of its members, requested that we refer to service information for accomplishing the actions specified in paragraph (g) of the proposed AD (in the SNPRM). SWA stated that the Air Cruisers service bulletins listed in paragraphs (c)(1) through (c)(16) of the proposed AD (in the SNPRM) have steps to inspect for the affected fusible plugs and to remove fusible plugs that are stamped with Lot PA-21 or PA-22. SWA noted that the service bulletins have been incorporated into the various [[Page 59292]] Air Cruisers component maintenance manuals (CMMs). A4A stated that the service bulletins and CMMs specify an inspection for the suspect fusible plug lot numbers and replacement if found. A4A and SWA also stated that maintenance records would not indicate the level of detail of the fusible plug part numbers and lot numbers installed. SWA stated that the revision of the CMM used to make the components serviceable is noted on FAA Form 8130-3. A4A also stated that access to the fusible plug part number and lot number is not achievable planeside, and noted that the equipment manufacturer recommends the system to be unpacked and inspected in the slide shop. SWA and A4A requested that paragraph (g) of the proposed AD (in the SNPRM) be revised to specify accomplishing the inspection in accordance with the applicable service information specified in paragraphs (c)(1) through (c)(16) of the proposed AD (in the SNPRM) and/or the applicable component maintenance manuals. We do not agree with revising paragraph (g) of this AD to mandate service information because this AD does not require operators to accomplish the inspection using a specific method. However, we do agree that operators should be aware of the service information that can be used to do the inspection specified in paragraph (g) of this AD. Therefore, we have added Note 1 to paragraph (g) of this AD to specify service bulletins and CMMs that provide guidance for performing the inspection. We have redesignated subsequent notes in this AD accordingly. We also acknowledge the commenters' statement that the records review might not be conclusive. As stated in paragraph (g) of this AD, the records review is allowed only if operators can conclusively determine the part number and lot number. For operators that do not have records that can conclusively determine the part number and lot number, the inspection must be done. Request To Remove Paragraph (h) of the Proposed AD (in the SNPRM) SWA requested that we remove paragraph (h) of the proposed AD (in the SNPRM). SWA stated that paragraph (h) of the proposed AD (in the SNPRM) would require immediate removal of the emergency equipment if an inspection or a records review determines an affected part is installed. SWA suggested that paragraph (h) of the proposed AD (in the SNPRM) be deleted because it is unnecessary. SWA stated the emergency equipment must be removed from the aircraft in order to inspect for the affected fusible plug. SWA noted the component maintenance documents do not provide the level of detail of the fusible plug part numbers and lot numbers installed. We do not agree with removing paragraph (h) of this AD because in order to address the unsafe condition the affected fusible plug must not only be removed but must also be replaced as required by paragraph (h) of this AD. We have not changed this AD in this regard. However, as stated previously, we have revised the compliance time in paragraph (h) of this AD to specify replacing within 42 months instead of requiring immediate action. Request for Credit for Actions Done Using Certain Service Information SWA requested that we give credit for inspections of the affected fusible plugs previously done per Air Cruisers service bulletins and/or CMMs incorporating the requirements of the Air Cruisers service bulletins. We agree to clarify. We have not mandated specific service information for accomplishing the actions specified in paragraphs (g) and (h) of this AD; therefore, it is not necessary to give credit for using specific service information. For operators that have already accomplished the actions required by paragraphs (g) and (h) of this AD, credit is given as specified in paragraph (f) of this AD, which states to accomplish the required actions within the compliance times specified, ``unless already done.'' Therefore, if operators have accomplished the actions required for compliance with paragraphs (g) and (h) of this AD before the effective date of this AD, no further action is necessary. Request To Revise Parts Installation Prohibition A4A, on behalf of its members, requested that we revise paragraph (i) of the proposed AD (in the SNPRM) to specify that no person may install on any airplane any slide, slide/raft, or off-wing escape system unless the inspection of the fusible plug has been done per the applicable service information specified in paragraphs (c)(1) through (c)(16) of the proposed AD (in the SNPRM) and/or the applicable CMM listed in Air Cruisers Service Information Letter (SIL) 25-246, Rev. No. 2, dated January 24, 2017. A4A stated that paragraph (i) of the proposed AD (in the SNPRM) does not sufficiently close the door on direct inspection of the plug, which can only be accomplished by unpacking slides and complete disassembly. A4A stated that only the inspection of records (including service bulletin accomplishment information directly stamped on the slide) can reasonably accomplish the intention of the proposed AD in a practical manner. We do not agree because we have not mandated the service information specified by the commenter. In order to comply with paragraph (i) of this AD, operators must prevent the installation of an affected part on an airplane. Paragraph (i) of this AD does not mandate a specific method for operators to follow to ensure the affected part is not installed. We have not changed this AD in this regard. Request To Revise Cost Estimate A4A, on behalf of its members, requested that we revise the cost estimate. A4A stated that the NPRM assumes one hour of labor per aircraft. A4A noted that because the actions need to be done at an appropriate facility (off wing and often not the operator's own shop), the cost should be per system, and include all facets from uninstalling through reinstallation. A4A stated the operator's actions will consume closer to 4 hours per slide (at $85/hour), with the addition of $500 each way shipping, and the vendor cost (Zodiac's typical billing is $2,900 per slide). We agree with revising the cost estimate because operators that cannot do a records review will need to remove the affected emergency equipment to accomplish the inspection. We disagree with including the shipping and vendor costs because not all operators will need to ship the equipment in order to do the inspection or records review. We have revised the Costs of Compliance section in this final rule to specify up to 4 work-hours for the inspection. Clarification of Replacement Part In paragraph (h) of the proposed AD (in the SNPRM), we specified to replace the fusible plug with a new part that does not have P/N B13984- 3, stamped with Lot PA-21 or PA-22. However, we have determined that it is not necessary for the replacement part to be a new part. Therefore, we have revised paragraph (h) of this AD to specify to replace the fusible plug with a serviceable fusible plug P/N B13984-3 that is not stamped with Lot PA-21 or PA-22. Additional Affected Parts--Other Related Service Information We have reviewed Air Cruisers Service Information Letter (SIL) 25- 246, Rev. No. 2, dated January 24, 2017, which indicates additional fusible plugs [[Page 59293]] might be affected by the identified unsafe condition. We have determined that to delay this action in order to allow the public to comment on the merits of inspecting the additional fusible plugs would be inappropriate, since we have determined that an unsafe condition exists and that inspections must be conducted to ensure continued safety. We are considering additional rulemaking to address additional fusible plugs. Clarification of Manufacturer's Name In the Summary of the SNPRM, we noted that Zodiac Aero Evacuation Systems was formerly known as Air Cruisers. However, Zodiac Aero Evacuation Systems is also known as Air Cruisers Company. For clarity, we have referred to the manufacturer as Zodiac Aero Evacuation Systems (also known as Air Cruisers Company) throughout this final rule. Conclusion We reviewed the relevant data, considered the comments received, and determined that air safety and the public interest require adopting this final rule with the changes described previously and minor editorial changes. We have determined that these minor changes:Are consistent with the intent that was proposed in the SNPRM for addressing the unsafe condition; and Do not add any additional burden upon the public than was already proposed in the SNPRM. We also determined that these changes will not increase the economic burden on any operator or increase the scope of this final rule. Related Service Information Under 1 CFR Part 51 We reviewed the following Air Cruisers service information. The service information identifies the affected fusible plugs. In addition, it describes procedures for inspecting and replacing affected fusible plugs. These documents are distinct since they apply to different airplane models or configurations. Air Cruisers Service Bulletin 737 103-25-50, dated August 27, 2010. Air Cruisers Service Bulletin 757 105-25-80, dated August 27, 2010. Air Cruisers Service Bulletin 757 105-25-81, dated August 27, 2010. Air Cruisers Service Bulletin 767 106-25-10, Rev. No. 1, dated October 15, 2010. Air Cruisers Service Bulletin 777 107-25-29, Rev. No. 1, dated July 8, 2011. Air Cruisers Service Bulletin A300/A310 001-25-19, dated August 27, 2010. Air Cruisers Service Bulletin A300/A310 003-25-33, dated August 27, 2010. Air Cruisers Service Bulletin A310 002-25-08, dated August 27, 2010. Air Cruisers Service Bulletin A320 004-25-87, Rev. No. 2, dated January 7, 2011. Air Cruisers Service Bulletin A321 005-25-21, dated August 27, 2010. Air Cruisers Service Bulletin BAe 146 201-25-23, dated December 10, 2010. Air Cruisers Service Bulletin F28 352-25-02, dated December 10, 2010. Air Cruisers Service Bulletin F100 351-25-07, dated December 10, 2010. Air Cruisers Service Bulletin Liferaft 35-25-79, dated August 27, 2010. Air Cruisers Service Bulletin MD11 305-25-35, dated August 27, 2010. Air Cruisers Service Bulletin MD80/90/717 304-25-45, dated August 27, 2010. This service information is reasonably available because the interested parties have access to it through their normal course of business or by the means identified in the ADDRESSES section. Costs of Compliance We estimate that this AD affects 3,384 airplanes of U.S. registry. We estimate the following costs to comply with this AD: Estimated Costs ---------------------------------------------------------------------------------------------------------------- Cost on U.S. Action Labor cost Parts cost Cost per product operators ---------------------------------------------------------------------------------------------------------------- Determination of part and lot Up to 4 work-hours $0 Up to $340......... Up to $1,150,560. number. x $85 per hour = Up to $340. ---------------------------------------------------------------------------------------------------------------- We estimate the following costs per slide to do any necessary replacement of the fusible plug that would be required based on the results of the inspection. We have no way of determining the number of aircraft that might need these replacements: On-Condition Cost ---------------------------------------------------------------------------------------------------------------- Cost per Action Labor cost Parts cost product ---------------------------------------------------------------------------------------------------------------- Replacement............................. 1 work-hour x $85 per hour Not available............. $85 = $85. ---------------------------------------------------------------------------------------------------------------- According to the manufacturer, some of the costs of this AD may be covered under warranty, thereby reducing the cost impact on affected individuals. We do not control warranty coverage for affected individuals. As a result, we have included all available costs in our cost estimate. 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 [[Page 59294]] products identified in this rulemaking action. This AD is issued in accordance with authority delegated by the Executive Director, Aircraft Certification Service, as authorized by FAA Order 8000.51C. In accordance with that order, issuance of ADs is normally a function of the Compliance and Airworthiness Division, but during this transition period, the Executive Director has delegated the authority to issue ADs applicable to transport category airplanes and associated appliances to the Director of the System Oversight Division. Regulatory Findings 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), (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. Adoption of the Amendment 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 FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD): 2018-23-12 Zodiac Aero Evacuation Systems (also known as Air Cruisers Company): Amendment 39-19499; Docket No. FAA-2016-9392; Product Identifier 2016-NM-003-AD. (a) Effective Date This AD is effective December 28, 2018. (b) Affected ADs None. (c) Applicability This AD applies to Zodiac Aero Evacuation Systems (also known as Air Cruisers Company) fusible plugs installed on emergency evacuation equipment identified in the service information specified in paragraphs (c)(1) through (c)(16) of this AD. These affected fusible plugs might be installed on the emergency evacuation equipment of the following manufacturers' airplanes: Airbus, The Boeing Company, BAE Systems (Operations) Limited, and Fokker Services B.V. (1) Air Cruisers Service Bulletin 737 103-25-50, dated August 27, 2010. (2) Air Cruisers Service Bulletin 757 105-25-80, dated August 27, 2010. (3) Air Cruisers Service Bulletin 757 105-25-81, dated August 27, 2010. (4) Air Cruisers Service Bulletin 767 106-25-10, Rev. No. 1, dated October 15, 2010. (5) Air Cruisers Service Bulletin 777 107-25-29, Rev. No. 1, dated July 8, 2011. (6) Air Cruisers Service Bulletin A300/A310 001-25-19, dated August 27, 2010. (7) Air Cruisers Service Bulletin A300/A310 003-25-33, dated August 27, 2010. (8) Air Cruisers Service Bulletin A310 002-25-08, dated August 27, 2010. (9) Air Cruisers Service Bulletin A320 004-25-87, Rev. No. 2, dated January 7, 2011. (10) Air Cruisers Service Bulletin A321 005-25-21, dated August 27, 2010. (11) Air Cruisers Service Bulletin BAe 146 201-25-23, dated December 10, 2010. (12) Air Cruisers Service Bulletin F28 352-25-02, dated December 10, 2010. (13) Air Cruisers Service Bulletin F100 351-25-07, dated December 10, 2010. (14) Air Cruisers Service Bulletin Liferaft 35-25-79, dated August 27, 2010. (15) Air Cruisers Service Bulletin MD11 305-25-35, dated August 27, 2010. (16) Air Cruisers Service Bulletin MD80/90/717 304-25-45, dated August 27, 2010. (d) Subject Air Transport Association (ATA) of America Code 25, Equipment/ furnishings. (e) Unsafe Condition This AD was prompted by reports indicating that affected fusible plugs activated (vented gas) below the rated temperature. We are issuing this AD to address fusible plugs that might activate below the rated temperature and render the evacuation system unusable. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Fusible Plug Identification Within 42 months after the effective date of this AD, do an inspection to determine if any fusible plug has part number (P/N) B13984-3, stamped with Lot PA-21 or PA-22. A review of the airplane maintenance records is acceptable to make this determination if it can be conclusively determined from that review that a part not having P/N B13984-3, stamped with Lot PA-21 or PA-22, has been installed. Note 1 to paragraph (g) of this AD: Guidance for performing the inspection specified in paragraph (g) of this AD can be found in applicable service information specified in paragraphs (c)(1) through (c)(16) of this AD and the applicable component maintenance manuals (CMMs) that have incorporated the appropriate Air Cruisers service information. (h) Replacement of Affected Fusible Plug If, during the inspection or records review required by paragraph (g) of this AD, it is determined that any fusible plug has part number (P/N) B13984-3, stamped with Lot PA-21 or PA-22: Within 42 months after the effective date of this AD, replace that fusible plug with a serviceable fusible plug P/N B13984-3 that is not stamped with Lot PA-21 or PA-22. Note 2 to paragraph (h) of this AD: Guidance can be found in the applicable CMM for the replacement. In addition, Air Cruisers Service Information Letter (SIL) 25-246, Rev. No. 1, dated February 21, 2014, provides information regarding affected fusible plugs and guidance on the replacement. (i) Parts Installation Prohibition As of the effective date of this AD, no person may install on any airplane any fusible plug having P/N B13984-3, stamped with Lot PA-21 or PA-22. (j) Alternative Methods of Compliance (AMOCs) (1) The Manager, New York ACO Branch, 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 certification office, send it to ATTN: Program Manager, Continuing Operational Safety, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone: 516-228-7300; fax: 516- 794-5531. (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. (k) Related Information (1) For more information about this AD, contact Darren Gassetto, Aerospace Engineer, Mechanical Systems and Admin Services Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7323; fax 516-794-5531; email [email protected]. (2) Service information identified in this AD that is not incorporated by reference is available at the addresses specified in paragraphs (l)(3) and (l)(4) of this AD. (l) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this [[Page 59295]] paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to determine parts that are affected by this AD, unless the AD specifies otherwise. (i) Air Cruisers Service Bulletin 737 103-25-50, dated August 27, 2010. (ii) Air Cruisers Service Bulletin 757 105-25-80, dated August 27, 2010. (iii) Air Cruisers Service Bulletin 757 105-25-81, dated August 27, 2010. (iv) Air Cruisers Service Bulletin 767 106-25-10, Rev. No. 1, dated October 15, 2010. (v) Air Cruisers Service Bulletin 777 107-25-29, Rev. No. 1, dated July 8, 2011. (vi) Air Cruisers Service Bulletin A300/A310 001-25-19, dated August 27, 2010. (vii) Air Cruisers Service Bulletin A300/A310 003-25-33, dated August 27, 2010. (viii) Air Cruisers Service Bulletin A310 002-25-08, dated August 27, 2010. (ix) Air Cruisers Service Bulletin A320 004-25-87, Rev. No. 2, dated January 7, 2011. (x) Air Cruisers Service Bulletin A321 005-25-21, dated August 27, 2010. (xi) Air Cruisers Service Bulletin BAe 146 201-25-23, dated December 10, 2010. (xii) Air Cruisers Service Bulletin F28 352-25-02, dated December 10, 2010. (xiii) Air Cruisers Service Bulletin F100 351-25-07, dated December 10, 2010. (xiv) Air Cruisers Service Bulletin Liferaft 35-25-79, dated August 27, 2010. (xv) Air Cruisers Service Bulletin MD11 305-25-35, dated August 27, 2010. (xvi) Air Cruisers Service Bulletin MD80/90/717 304-25-45, dated August 27, 2010. (3) For service information identified in this AD, contact Air Cruisers, 1747 State Route 34, Wall Township, NJ 07727-3935; phone 732-681-3527; email [email protected]. (4) You may view this service information at the FAA, Transport Standards Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. (5) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html. Issued in Des Moines, Washington, on November 8, 2018. Chris Spangenberg, Acting Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2018-25003 Filed 11-21-18; 8:45 am] BILLING CODE 4910-13-P
![59290 Federal Register / Vol. 83, No. 226 / Friday, November 23, 2018 / Rules and Regulations
(1) Is not a ‘‘significant regulatory (g) Required Actions (k) Related Information
action’’ under Executive Order 12866, (1) Before exceeding 2,500 flight cycles (1) For more information about this AD,
(2) Is not a ‘‘significant rule’’ under (FCs), or within 100 FCs after the effective contact Dorie Resnik, Aerospace Engineer,
the DOT Regulatory Policies and date of this AD, whichever occurs later, Boston ACO Branch, FAA, 1200 District
Procedures (44 FR 11034, February 26, inspect the seat pan structure in both Avenue, Burlington, MA, 01803; phone: 781–
1979), deployed and stowed positions using 238–7693; fax: 781–238–7199; email:
(3) Will not affect intrastate aviation paragraph 2.A., Accomplishment dorie.resnik@faa.gov.
Instructions, of Zodiac Seats France Service (2) Refer to MCAI EASA AD 2017–0001,
in Alaska, and dated January 6, 2017, for more information.
(4) Will not have a significant Bulletin (SB) No. 536–25–003, Rev. 3, dated
June 2, 2017. You may examine the MCAI in the AD
economic impact, positive or negative, docket on the internet at http://
(2) If cracks are found, before the next
on a substantial number of small entities flight: www.regulations.gov by searching for and
under the criteria of the Regulatory (i) Replace seat pan with reinforced seat locating it in Docket No. FAA–2017–0632.
Flexibility Act. pan, P/N F0511530, using paragraph 2.B., (l) Material Incorporated by Reference
List of Subjects in 14 CFR Part 39 Accomplishment Instructions, of Zodiac
(1) The Director of the Federal Register
Seats France SB No. 536–25–003, Rev. 3,
Air transportation, Aircraft, Aviation approved the incorporation by reference
dated June 2, 2017.
safety, Incorporation by reference, (IBR) of the service information listed in this
(ii) Re-mark the seat using paragraph 2.C.,
paragraph under 5 U.S.C. 552(a) and 1 CFR
Safety. Accomplishment Instructions, of Zodiac
part 51.
Seats France SB No. 536–25–003, Rev. 3, (2) You must use this service information
Adoption of the Amendment dated June 2, 2017. as applicable to do the actions required by
Accordingly, under the authority (3) If no cracks are found, do the following: this AD, unless the AD specifies otherwise.
delegated to me by the Administrator, (i) Re-mark the seat using paragraph 2.C., (i) Zodiac Seats France Service Bulletin
the FAA amends 14 CFR part 39 as Accomplishment Instructions, of Zodiac No. 536–25–003, Rev. 3, dated June 2, 2017.
follows: Seats France SB No. 536–25–003, Rev. 3, (ii) [Reserved.]
dated June 2, 2017. (3) For Zodiac Seats France service
PART 39—AIRWORTHINESS (ii) Reinspect the seat pan every 100 FCs information identified in this AD, contact
since last inspection, or replace seat pan with Zodiac Seats France, Rue Robert Marechal
DIRECTIVES
reinforced seat pan, P/N F0511530, using Senior B.P. 69, 36100 Issoudun, France;
■ 1. The authority citation for part 39 paragraph 2.B., Accomplishment. phone: +33 (0) 2 54 03 39 39; fax: +33 (0) 2
Instructions, of Zodiac Seats France SB No. 54 03 39 00; email: zs.tac@
continues to read as follows:
536–25–003, Rev. 3, dated June 2, 2017. zodiacaerospace.com; internet: https://
Authority: 49 U.S.C. 106(g), 40113, 44701. (4) After the effective date of this AD, and services.zodiacaerospace.com.
until compliance with this AD is (4) You may view this service information
§ 39.13 [Amended] accomplished, stow and secure an affected at FAA, Engine & Propeller Standards
■ 2. The FAA amends § 39.13 by adding attendant seat in the retracted position to Branch, 1200 District Avenue, Burlington,
the following new airworthiness prevent occupancy, in accordance with the MA, 01803. For information on the
directive (AD): provisions and limitations of the applicable availability of this material at the FAA, call
Master Minimum Equipment List item. 781–238–7759.
2018–23–01 Zodiac Seats France (formerly (5) You may view this service information
SICMA Aero Seat): Amendment 39–19487; (h) Optional Terminating Action
that is incorporated by reference at the
Docket No. FAA–2017–0632; Product Installation of a reinforced seat pan, P/N National Archives and Records
Identifier 2017–NE–16–AD. F0511530, using paragraph 2.B., Administration (NARA). For information on
(a) Effective Date Accomplishment Instructions, of Zodiac the availability of this material at NARA, call
Seats France SB No. 536–25–003, Rev. 3, 202–741–6030, or go to: http://
This AD is effective December 28, 2018. dated June 2, 2017, is terminating action to www.archives.gov/federal-register/cfr/ibr-
(b) Affected ADs this AD. locations.html.
None. (i) Credit for Previous Actions Issued in Burlington, Massachusetts, on
You may take credit for inspections and November 16, 2018.
(c) Applicability
modifications performed in accordance with Robert J. Ganley,
(1) This AD applies to all Zodiac Seats
Zodiac Seats France SB No. 536–25–003, Manager, Engine and Propeller Standards
France Cabin Attendant Seats, 536 Series,
Rev. 2, dated September 16, 2016, or earlier Branch, Aircraft Certification Service.
part numbers (P/N) 53600, all dash numbers,
versions, if you performed these actions [FR Doc. 2018–25436 Filed 11–21–18; 8:45 am]
and all serial numbers, with seat pan P/N
before the effective date of this AD.
F0433453, installed. BILLING CODE 4910–13–P
(2) These appliances are installed on, but (j) Alternative Methods of Compliance
not limited to, ATR 42 and ATR 72 airplanes (AMOCs)
of U.S. registry. DEPARTMENT OF TRANSPORTATION
(1) The Manager, Boston ACO Branch,
(d) Subject FAA, has the authority to approve AMOCs
for this AD, if requested using the procedures Federal Aviation Administration
Joint Aircraft System Component (JASC)
Code 2500, Cabin Equipment/Furnishings. found in 14 CFR 39.19. In accordance with
14 CFR 39.19, send your request to your 14 CFR Part 39
(e) Unsafe Condition principal inspector or local Flight Standards
[Docket No. FAA–2016–9392; Product
This AD was prompted by cracks found in District Office, as appropriate. If sending
Identifier 2016–NM–003–AD; Amendment
a highly concentrated stress area of the seat information directly to the manager of the
39–19499; AD 2018–23–12]
pan hinges. We are issuing this AD to prevent ACO Branch, send it to the attention of the
failure of affected seats. The unsafe person identified in paragraph (k)(1) of this RIN 2120–AA64
amozie on DSK3GDR082PROD with RULES
condition, if not addressed, could result in AD. You may email your request to: 9-ane-
injury to the seat occupants. boston-aco-amocrequests@faa.gov. Airworthiness Directives; Zodiac Aero
(2) Before using any approved AMOC, Evacuation Systems (also known as
(f) Compliance notify your appropriate principal inspector, Air Cruisers Company)
Comply with this AD within the or lacking a principal inspector, the manager
compliance times specified, unless already of the local flight standards district office/ AGENCY:Federal Aviation
done. certificate holding district office. Administration (FAA), DOT.
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![Federal Register / Vol. 83, No. 226 / Friday, November 23, 2018 / Rules and Regulations 59291
ACTION: Final rule. Discussion we have determined that a compliance
We issued a notice of proposed time of 42 months to replace the
SUMMARY: We are adopting a new affected part addresses the unsafe
rulemaking (NPRM) to amend 14 CFR
airworthiness directive (AD) for Zodiac condition and provides an acceptable
part 39 by adding an AD that would
Aero Evacuation Systems (also known level of safety. We have revised
apply to Zodiac Aero Evacuation
as Air Cruisers Company) fusible plugs Systems (also known as Air Cruisers paragraph (h) of the AD to specify a 42-
installed on emergency evacuation Company) fusible plugs installed on month compliance time for the
equipment for various transport emergency evacuation equipment for replacement.
category airplanes. This AD was various transport category airplanes.
prompted by reports indicating that Request To Specify Serial Numbers
The NPRM published in the Federal
affected fusible plugs activated (vented All Nippon Airways (ANA) requested
Register on November 18, 2016 (81 FR
gas) below the rated temperature. This that we revise paragraph (c) of the
81709). The NPRM was prompted by
AD requires an inspection of the fusible proposed AD (in the SNPRM) to refer to
reports indicating that affected fusible
plugs to determine the part number and service information that specifies the
plugs activated (vented gas) below the
lot number, and replacement of all serial numbers and not only the part
rated temperature. The NPRM proposed
affected fusible plugs. We are issuing numbers of the affected emergency
to require an inspection of the fusible
this AD to address the unsafe condition equipment. ANA stated that identifying
plugs to determine the part number and
on these products. affected [parts] by only the part number
lot number, and replacement of all
means that even after expiration of the
DATES: This AD is effective December affected fusible plugs.
We subsequently issued a compliance time specified in the
28, 2018.
supplemental NPRM (SNPRM) that was proposed AD, the inspection must be
The Director of the Federal Register continued every time the affected
approved the incorporation by reference published in the Federal Register on
January 24, 2018 (83 FR 3283). The emergency equipment is purchased.
of certain publications listed in this AD ANA stated that the serial number of the
as of December 28, 2018. SNPRM proposed to extend the
compliance time, clarify the affected emergency equipment should
ADDRESSES: For service information be specified in the service information
applicability, and clarify certain
identified in this final rule, contact Air requirements. listed in paragraph (c) of the proposed
Cruisers, 1747 State Route 34, Wall We are issuing this AD to address AD (in the SNPRM) in order to prevent
Township, NJ 07727–3935; phone 732– fusible plugs that might activate below endless inspections.
681–3527; email technicalpublications@ the rated temperature and render the We do not agree because specific
zodiacaerospace.com. You may view evacuation system unusable. serial numbers for the affected
this service information at the FAA, emergency equipment have not been
Transport Standards Branch, 2200 Comments identified. In addition, since the fusible
South 216th St., Des Moines, WA. For We gave the public the opportunity to plugs are rotable we cannot limit the
information on the availability of this participate in developing this final rule. applicability to only the known
material at the FAA, call 206–231–3195. The following presents the comments emergency equipment on which the
It is also available on the internet at received on the SNPRM and the FAA’s fusible plugs were initially installed.
http://www.regulations.gov by searching response to each comment. Therefore, in order to address the
for and locating Docket No. FAA–2016– identified unsafe condition, all fusible
9392. Request to Extend Compliance Time plugs installed on emergency
Airlines for America (A4A), on behalf evacuation equipment identified in the
Examining the AD Docket of its members, requested that we service information specified in
You may examine the AD docket on extend the compliance time specified in paragraph (c) of this AD must be
the internet at http:// paragraph (h) of the proposed AD (in the inspected as specified in paragraph (g)
www.regulations.gov by searching for SNPRM). A4A stated that the extended of this AD. When installing new
and locating Docket No. FAA–2016– compliance time of 42 months after the equipment on an airplane, operators
9392; or in person at Docket Operations effective date (in paragraph (g) of the must ensure the newly installed part is
between 9 a.m. and 5 p.m., Monday proposed AD (in the SNPRM)) had an not one of the affected parts by
through Friday, except Federal holidays. unintended consequence in the re- complying with the parts installation
The AD docket contains this final rule, worded compliance paragraph (h) of the prohibition specified in paragraph (i) of
the regulatory evaluation, any proposed AD (in the SNPRM). A4A this AD. We have not changed this AD
comments received, and other noted that while the allowance for in this regard.
information. The address for Docket maintenance records inspection was
added, the words ‘‘[b]efore further Request To Refer to Service
Operations (phone: 800–647–5527) is Information
U.S. Department of Transportation, flight’’ remained. A4A concluded that
Docket Operations, M–30, West the current version means that either a Southwest Airlines (SWA) and A4A,
Building Ground Floor, Room W12–140, planeside finding or a maintenance on behalf of its members, requested that
1200 New Jersey Avenue SE, records discovery will each require we refer to service information for
Washington, DC 20590. action before further flight. A4A stated accomplishing the actions specified in
that while a finding by direct inspection paragraph (g) of the proposed AD (in the
FOR FURTHER INFORMATION CONTACT: SNPRM). SWA stated that the Air
will happen only in a shop and not
Darren Gassetto, Aerospace Engineer, affect operation of any aircraft, the Cruisers service bulletins listed in
Mechanical Systems and Admin accommodation for records review paragraphs (c)(1) through (c)(16) of the
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Services Section, FAA, New York ACO could immediately ground an in-service proposed AD (in the SNPRM) have steps
Branch, 1600 Stewart Avenue, Suite aircraft. A4A requested that we allow 42 to inspect for the affected fusible plugs
410, Westbury, NY 11590; telephone months for the replacement if a records and to remove fusible plugs that are
516–228–7323; fax 516–794–5531; email review was done. stamped with Lot PA–21 or PA–22.
9-avs-nyaco-cos@faa.gov. We agree to revise the compliance SWA noted that the service bulletins
SUPPLEMENTARY INFORMATION: time in paragraph (h) of this AD because have been incorporated into the various
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![59294 Federal Register / Vol. 83, No. 226 / Friday, November 23, 2018 / Rules and Regulations
products identified in this rulemaking (a) Effective Date determination if it can be conclusively
action. This AD is effective December 28, 2018. determined from that review that a part not
This AD is issued in accordance with having P/N B13984–3, stamped with Lot PA–
(b) Affected ADs 21 or PA–22, has been installed.
authority delegated by the Executive
None. Note 1 to paragraph (g) of this AD:
Director, Aircraft Certification Service, Guidance for performing the inspection
as authorized by FAA Order 8000.51C. (c) Applicability specified in paragraph (g) of this AD can be
In accordance with that order, issuance This AD applies to Zodiac Aero Evacuation found in applicable service information
of ADs is normally a function of the Systems (also known as Air Cruisers specified in paragraphs (c)(1) through (c)(16)
Compliance and Airworthiness Company) fusible plugs installed on of this AD and the applicable component
Division, but during this transition emergency evacuation equipment identified maintenance manuals (CMMs) that have
period, the Executive Director has in the service information specified in incorporated the appropriate Air Cruisers
delegated the authority to issue ADs paragraphs (c)(1) through (c)(16) of this AD. service information.
These affected fusible plugs might be
applicable to transport category installed on the emergency evacuation
(h) Replacement of Affected Fusible Plug
airplanes and associated appliances to equipment of the following manufacturers’ If, during the inspection or records review
the Director of the System Oversight airplanes: Airbus, The Boeing Company, BAE required by paragraph (g) of this AD, it is
Division. Systems (Operations) Limited, and Fokker determined that any fusible plug has part
Services B.V. number (P/N) B13984–3, stamped with Lot
Regulatory Findings (1) Air Cruisers Service Bulletin 737 103– PA–21 or PA–22: Within 42 months after the
This AD will not have federalism 25–50, dated August 27, 2010. effective date of this AD, replace that fusible
implications under Executive Order (2) Air Cruisers Service Bulletin 757 105– plug with a serviceable fusible plug P/N
25–80, dated August 27, 2010. B13984–3 that is not stamped with Lot PA–
13132. This AD will not have a 21 or PA–22.
(3) Air Cruisers Service Bulletin 757 105–
substantial direct effect on the States, on Note 2 to paragraph (h) of this AD:
25–81, dated August 27, 2010.
the relationship between the national (4) Air Cruisers Service Bulletin 767 106– Guidance can be found in the applicable
government and the States, or on the 25–10, Rev. No. 1, dated October 15, 2010. CMM for the replacement. In addition, Air
distribution of power and (5) Air Cruisers Service Bulletin 777 107– Cruisers Service Information Letter (SIL) 25–
responsibilities among the various 25–29, Rev. No. 1, dated July 8, 2011. 246, Rev. No. 1, dated February 21, 2014,
levels of government. (6) Air Cruisers Service Bulletin A300/ provides information regarding affected
For the reasons discussed above, I A310 001–25–19, dated August 27, 2010. fusible plugs and guidance on the
certify that this AD: (7) Air Cruisers Service Bulletin A300/ replacement.
(1) Is not a ‘‘significant regulatory A310 003–25–33, dated August 27, 2010. (i) Parts Installation Prohibition
(8) Air Cruisers Service Bulletin A310 002–
action’’ under Executive Order 12866, As of the effective date of this AD, no
25–08, dated August 27, 2010.
(2) Is not a ‘‘significant rule’’ under (9) Air Cruisers Service Bulletin A320 004– person may install on any airplane any
DOT Regulatory Policies and Procedures 25–87, Rev. No. 2, dated January 7, 2011. fusible plug having P/N B13984–3, stamped
(44 FR 11034, February 26, 1979), (10) Air Cruisers Service Bulletin A321 with Lot PA–21 or PA–22.
(3) Will not affect intrastate aviation 005–25–21, dated August 27, 2010. (j) Alternative Methods of Compliance
in Alaska, and (11) Air Cruisers Service Bulletin BAe 146 (AMOCs)
(4) Will not have a significant 201–25–23, dated December 10, 2010.
(12) Air Cruisers Service Bulletin F28 352– (1) The Manager, New York ACO Branch,
economic impact, positive or negative, FAA, has the authority to approve AMOCs
on a substantial number of small entities 25–02, dated December 10, 2010.
(13) Air Cruisers Service Bulletin F100 for this AD, if requested using the procedures
under the criteria of the Regulatory found in 14 CFR 39.19. In accordance with
351–25–07, dated December 10, 2010.
Flexibility Act. (14) Air Cruisers Service Bulletin Liferaft 14 CFR 39.19, send your request to your
35–25–79, dated August 27, 2010. principal inspector or local Flight Standards
List of Subjects in 14 CFR Part 39 District Office, as appropriate. If sending
(15) Air Cruisers Service Bulletin MD11
Air transportation, Aircraft, Aviation 305–25–35, dated August 27, 2010. information directly to the certification
safety, Incorporation by reference, (16) Air Cruisers Service Bulletin MD80/ office, send it to ATTN: Program Manager,
Safety. 90/717 304–25–45, dated August 27, 2010. Continuing Operational Safety, FAA, New
York ACO Branch, 1600 Stewart Avenue,
Adoption of the Amendment (d) Subject Suite 410, Westbury, NY 11590; telephone:
Air Transport Association (ATA) of 516–228–7300; fax: 516–794–5531.
Accordingly, under the authority (2) Before using any approved AMOC,
America Code 25, Equipment/furnishings.
delegated to me by the Administrator, notify your appropriate principal inspector,
the FAA amends 14 CFR part 39 as (e) Unsafe Condition or lacking a principal inspector, the manager
follows: This AD was prompted by reports of the local flight standards district office/
indicating that affected fusible plugs certificate holding district office.
PART 39—AIRWORTHINESS activated (vented gas) below the rated (k) Related Information
DIRECTIVES temperature. We are issuing this AD to
address fusible plugs that might activate (1) For more information about this AD,
■ 1. The authority citation for part 39 below the rated temperature and render the contact Darren Gassetto, Aerospace Engineer,
continues to read as follows: evacuation system unusable. Mechanical Systems and Admin Services
Section, FAA, New York ACO Branch, 1600
Authority: 49 U.S.C. 106(g), 40113, 44701. (f) Compliance Stewart Avenue, Suite 410, Westbury, NY
Comply with this AD within the 11590; telephone 516–228–7323; fax 516–
§ 39.13 [Amended] compliance times specified, unless already 794–5531; email 9-avs-nyaco-cos@faa.gov.
■ 2. The FAA amends § 39.13 by adding done. (2) Service information identified in this
the following new airworthiness AD that is not incorporated by reference is
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(g) Fusible Plug Identification available at the addresses specified in
directive (AD): Within 42 months after the effective date paragraphs (l)(3) and (l)(4) of this AD.
2018–23–12 Zodiac Aero Evacuation of this AD, do an inspection to determine if
Systems (also known as Air Cruisers any fusible plug has part number (P/N) (l) Material Incorporated by Reference
Company): Amendment 39–19499; B13984–3, stamped with Lot PA–21 or PA– (1) The Director of the Federal Register
Docket No. FAA–2016–9392; Product 22. A review of the airplane maintenance approved the incorporation by reference
Identifier 2016–NM–003–AD. records is acceptable to make this (IBR) of the service information listed in this
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![Federal Register / Vol. 83, No. 226 / Friday, November 23, 2018 / Rules and Regulations 59295
paragraph under 5 U.S.C. 552(a) and 1 CFR DEPARTMENT OF ENERGY Jobs Act of 2017.1 The Commission also
part 51. addresses the accounting and
(2) You must use this service information Federal Energy Regulatory ratemaking treatment of ADIT following
as applicable to determine parts that are Commission the sale or retirement of an asset.
affected by this AD, unless the AD specifies
otherwise. 18 CFR Parts 35, 101, 154, 201, and 352 I. Background
(i) Air Cruisers Service Bulletin 737 103– A. Tax Cuts and Jobs Act
25–50, dated August 27, 2010. [Docket No. PL19–2–000]
(ii) Air Cruisers Service Bulletin 757 105–
2. On December 22, 2017, the
25–80, dated August 27, 2010. President signed into law the Tax Cuts
Accounting and Ratemaking Treatment and Jobs Act. The Tax Cuts and Jobs
(iii) Air Cruisers Service Bulletin 757 105– of Accumulated Deferred Income
25–81, dated August 27, 2010. Act, among other things, reduced the
Taxes and Treatment Following the federal corporate income tax rate from
(iv) Air Cruisers Service Bulletin 767 106– Sale or Retirement of an Asset
25–10, Rev. No. 1, dated October 15, 2010. 35 percent to 21 percent, effective
(v) Air Cruisers Service Bulletin 777 107– AGENCY: Federal Energy Regulatory January 1, 2018.2 This means that,
25–29, Rev. No. 1, dated July 8, 2011. Commission, Department of Energy. beginning January 1, 2018, companies
(vi) Air Cruisers Service Bulletin A300/ subject to the Commission’s jurisdiction
ACTION: Policy statement.
A310 001–25–19, dated August 27, 2010. will compute income taxes owed to the
(vii) Air Cruisers Service Bulletin A300/ SUMMARY: In this Policy Statement, the Internal Revenue Service (IRS) based on
A310 003–25–33, dated August 27, 2010. Federal Energy Regulatory Commission a 21 percent tax rate. The tax rate
(viii) Air Cruisers Service Bulletin A310 (Commission) states its policy regarding reduction will result in less corporate
002–25–08, dated August 27, 2010. the treatment of Accumulated Deferred income tax expense going forward.
(ix) Air Cruisers Service Bulletin A320 Income Taxes for both accounting and 3. Importantly, the tax rate reduction
004–25–87, Rev. No. 2, dated January 7, ratemaking purposes as to Commission- will also result in a reduction in ADIT
2011. jurisdictional public utilities, natural liabilities and ADIT assets on the books
(x) Air Cruisers Service Bulletin A321 005– gas pipelines and oil pipelines, in light of rate-regulated companies. ADIT
25–21, dated August 27, 2010. of the Tax Cuts and Jobs Act of 2017. In balances are accumulated on the
(xi) Air Cruisers Service Bulletin BAe 146 addition, the Commission addresses the regulated books and records of such
201–25–23, dated December 10, 2010. accounting and ratemaking treatment of regulated companies based on the
(xii) Air Cruisers Service Bulletin F28 352– Accumulated Deferred Income Taxes requirements of the Uniform System of
25–02, dated December 10, 2010. following the sale or retirement of an Accounts (USofA).3 ADIT arises from
(xiii) Air Cruisers Service Bulletin F100 asset. timing differences between the method
351–25–07, dated December 10, 2010. of computing taxable income for
(xiv) Air Cruisers Service Bulletin Liferaft DATES: This Policy Statement will reporting to the IRS and the method of
35–25–79, dated August 27, 2010. become applicable November 23, 2018. computing income for regulatory
(xv) Air Cruisers Service Bulletin MD11 FOR FURTHER INFORMATION CONTACT: accounting and ratemaking purposes.4
305–25–35, dated August 27, 2010. Sharli Silva (Legal Information), Office As a result of the Tax Cuts and Jobs Act
(xvi) Air Cruisers Service Bulletin MD80/ of the General Counsel, 888 First reducing the federal corporate income
90/717 304–25–45, dated August 27, 2010. Street NE, Washington, DC 20426, tax rate from 35 percent to 21 percent,
(3) For service information identified in (202) 502–8719, Sharli.Silva@ferc.gov. a portion of an ADIT liability that was
this AD, contact Air Cruisers, 1747 State collected from customers will no longer
Bryan Wheeler (Technical Information),
Route 34, Wall Township, NJ 07727–3935; be due from public utilities, natural gas
Office of Energy Markets Regulation,
phone 732–681–3527; email technical pipelines and oil pipelines to the IRS
Federal Energy Regulatory
publications@zodiacaerospace.com. and is considered excess ADIT.
Commission, 888 First Street NE,
(4) You may view this service information
at the FAA, Transport Standards Branch,
Washington, DC 20426, (202) 502– B. Order No. 144
2200 South 216th St., Des Moines, WA. For
8497, Bryan.Wheeler@ferc.gov.
4. The purpose of tax normalization is
information on the availability of this Monil Patel (Technical Information),
to match the tax effects of costs and
material at the FAA, call 206–231–3195. Office of Energy Markets Regulation,
revenues with the recovery in rates of
(5) You may view this service information Federal Energy Regulatory
those same costs and revenues.5 As
that is incorporated by reference at the Commission, 888 First Street NE,
National Archives and Records Washington, DC 20426, (202) 502– 1 An Act to provide for reconciliation pursuant to
Administration (NARA). For information on 8296, Monil.Patel@ferc.gov. titles II and V of the concurrent resolution on the
the availability of this material at NARA, call Kimberly Horner (Technical budget for fiscal year 2018, Public Law 115–97, 131
Information), Office of Enforcement, Stat. 2054 (2017) (Tax Cuts and Jobs Act).
202–741–6030, or go to: http:// 2 Id. Sec. 13001, 131 Stat. at 2096.
www.archives.gov/federal-register/cfr/ibr- Federal Energy Regulatory 3 See Definition of Accounts 182.3 and Account
locations.html. Commission, 888 First Street NE, 254, 18 CFR part 101, Uniform System of Accounts
Washington, DC 20426, (202) 502– Prescribed for Public Utilities and Licensees Subject
Issued in Des Moines, Washington, on
8623, Kimberly.Horner@ferc.gov. to the Provisions of the Federal Power Act; see
November 8, 2018. Definition of Accounts 182.3 and Account 254, 18
SUPPLEMENTARY INFORMATION: CFR part 201, Uniform System of Accounts
Chris Spangenberg,
1. In this Policy Statement, the Prescribed for Natural Gas Companies Subject to
Acting Director, System Oversight Division, the Provisions of the Natural Gas Act; see General
Aircraft Certification Service.
Federal Energy Regulatory Commission
Instructions 1–12, Accounting for Income Taxes, 18
(Commission) states its policy regarding
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[FR Doc. 2018–25003 Filed 11–21–18; 8:45 am] CFR part 352, Uniform Systems of Accounts
the treatment of Accumulated Deferred Prescribed for Oil Pipeline Companies Subject to
BILLING CODE 4910–13–P Income Taxes (ADIT) for both the Provisions of the Interstate Commerce Act.
accounting and ratemaking purposes as 4 See 18 CFR 35.24(d)(2) (2018).
5 Tax Normalization for Certain Items Reflecting
to Commission-jurisdictional public
Timing Differences in the Recognition of Expenses
utilities, natural gas pipelines, and oil or Revenues for Ratemaking and Income Tax
pipelines, in light of the Tax Cuts and Continued
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Document Created: 2018-11-27 12:58:48
Document Modified: 2018-11-27 12:58:48
| 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 | Rules and Regulations | |
| Action | Final rule. | |
| Dates | This AD is effective December 28, 2018. | |
| Contact | Darren Gassetto, Aerospace Engineer, Mechanical Systems and Admin Services Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7323; fax 516-794-5531; email [email protected] | |
| FR Citation | 83 FR 59290 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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