82 FR 10860 - Airworthiness Directives; The Boeing Company Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 82, Issue 31 (February 16, 2017)
Federal Aviation Administration
Federal Register Volume 82, Issue 31 (February 16, 2017)
| Page Range | 10860-10863 | |
| FR Document | 2017-03028 |
[Federal Register Volume 82, Number 31 (Thursday, February 16, 2017)] [Rules and Regulations] [Pages 10860-10863] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2017-03028] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2013-0797; Directorate Identifier 2013-NM-007-AD; Amendment 39-18776; AD 2017-01-09] RIN 2120-AA64 Airworthiness Directives; The Boeing Company Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; correction. ----------------------------------------------------------------------- [[Page 10861]] SUMMARY: The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to certain The Boeing Company Model 767-300 and 767-300F airplanes. Certain service information citations in the preamble and regulatory text are incorrect. This document corrects those errors. In all other respects, the original document remains the same. DATES: This final rule is effective February 21, 2017. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of February 21, 2017 (82 FR 4778, January 17, 2017). ADDRESSES: For service information identified in this final rule, contact Boeing Commercial Airplanes, Attention: Contractual & Data Services (C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA 90740-5600; telephone: 562-797-1717; 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-2013- 0797. Examining the AD Docket You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD, the regulatory evaluation, any comments received, and other information. The address for the Docket Office (phone: 800-647-5527) is Docket Management Facility, U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590. FOR FURTHER INFORMATION CONTACT: Francis Smith, Aerospace Engineer, Cabin Safety and Environmental Controls Branch, ANM-150S, FAA, Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue SW., Renton, WA 98057-3356; phone: 425-917-6596; fax: 425-917-6590; email: francis.smith@faa.gov. SUPPLEMENTARY INFORMATION: Airworthiness Directive 2017-01-09, amendment 39-18776 (82 FR 4778, January 17, 2017), requires modification and installation of components in the main equipment center for certain Model 767-300 and 767-300F series airplanes. For certain airplanes, AD 2017-01-09 also requires modification, replacement, and installation of flight deck air relief system (FDARS) components. Need for the Correction As published, certain service information citations in the preamble and regulatory text were incorrect. The incorrectly specified citation in the preamble and regulatory text was Boeing Service Bulletin 767-27- 0244, Revision 1, dated March 8, 2010 (``SB 767-27-0244, R1''); the correct citation is Boeing Service Bulletin 767-21-0244, Revision 1, dated March 8, 2010 (``SB 767-21-0244, R1''). Related Service Information Under 1 CFR Part 51 We reviewed the following service information.Boeing Service Bulletin 767-21-0235, dated October 8, 2009; and Revision 1, dated July 29, 2011 (``SB 767-21-0235, R1''). The service information describes procedures for a relay installation and related wiring changes (which change (modify) the 3-way valve control logic for the cooling system for the flight deck display equipment on freighter airplanes). Boeing Service Bulletin 767-21-0244, Revision 1, dated March 8, 2010 (``SB 767-21-0244, R1''). The service information describes procedures for changing (modifying) the 3-way valve control logic and installing a cooling system for the flight deck display equipment. Boeing Alert Service Bulletin 767-21A0245, Revision 2, dated September 27, 2013 (``ASB 767-21A0245, R2''); and Boeing Alert Service Bulletin 767-21A0247, Revision 1, dated April 9, 2013 (``ASB 767-21A0247, R1''). The service information describes procedures for changing (modifying) the 3-way valve control logic and main cargo air distribution system (MCADS), and installing an FDARS. These documents are distinct since they apply to different airplane models. Boeing Alert Service Bulletin 767-21A0253, dated October 12, 2012. The service information describes procedures for replacing the existing duct, installing an FDARS, changing (modifying) the 3-way valve control logic, and installing a new altitude switch and pitot tube. Boeing Alert Service Bulletin 767-21A0254, dated June 7, 2013. The service information describes procedures for replacing the duct with a new duct; installing an FDARS (including the installation of mounting brackets, ducts, orifice, outlet valve, and screen); and activating the 3-way valve logic (including modification of the associated wiring and related actions). Boeing Service Bulletin 767-31-0073, dated October 12, 1995. The service information describes procedures for installing a maintenance data selection system for the engine indication and crew alerting system. 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. Correction of Publication This document corrects errors in the citation of certain service information and correctly adds the AD as an amendment to 14 CFR 39.13. Although no other part of the preamble or regulatory information has been corrected, we are publishing the entire rule in the Federal Register. The effective date of this AD remains February 21, 2017. Since this action only corrects errors in the citation of certain service information, it has no adverse economic impact and imposes no additional burden on any person. Therefore, we have determined that notice and public procedures are unnecessary. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Correction Accordingly, pursuant to the authority delegated to me by the Administrator, the Federal Aviation Administration amends part 39 of the Federal Aviation Regulations (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 [Corrected] 0 2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD): 2017-01-09 The Boeing Company: Amendment 39-18776; Docket No. FAA- 2013-0797; Directorate Identifier 2013-NM-007-AD. (a) Effective Date This AD is effective February 21, 2017. (b) Affected ADs None. [[Page 10862]] (c) Applicability This AD applies to The Boeing Company Model 767-300 and 767-300F series airplanes, certificated in any category; as identified in the service information specified in paragraphs (c)(1) through (c)(5) of this AD. This AD does not apply to The Boeing Company Model 767-300 (passenger) series airplanes. (1) Boeing Service Bulletin 767-21-0244, Revision 1, dated March 8, 2010 (``SB 767-21-0244, R1''). (2) Boeing Alert Service Bulletin 767-21A0245, Revision 2, dated September 27, 2013 (``ASB 767-21A0245, R2''). (3) Boeing Alert Service Bulletin 767-21A0247, Revision 1, dated April 9, 2013 (``ASB 767-21A0247, R1''). (4) Boeing Alert Service Bulletin 767-21A0253, dated October 12, 2012. (5) Boeing Alert Service Bulletin 767-21A0254, dated June 7, 2013. (d) Subject Air Transport Association (ATA) of America Code 21, Air Conditioning. (e) Unsafe Condition This AD was prompted by reports of malfunctions in the flight deck display units, which resulted in blanking, blurring, or loss of color on the display. We are issuing this AD to prevent malfunctions of the flight deck display units, which could affect the ability of the flight crew to read the displays for airplane attitude, altitude, or airspeed, and consequently reduce the ability of the flight crew to maintain control of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Installation of Flight Deck Air Relief System (FDARS) and 3-Way Valve Logic Change or Activation (1) For Model 767-300F series airplanes, as identified in Boeing Alert Service Bulletin 767-21A0253, dated October 12, 2012: Within 72 months after the effective date of this AD, in the main equipment center and the area under the left and right sides of the flight deck floor, replace the existing duct with a new duct; install an FDARS (including the installation of mounting brackets, ducts, orifice, outlet valve, and screen); change the 3-way valve logic (including modification of the associated wiring and related actions); and install a new altitude switch and pitot tube; in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin 767-21A0253, dated October 12, 2012. (2) For Model 767-300F series airplanes, as identified in Boeing Alert Service Bulletin 767-21A0254, dated June 7, 2013: Within 72 months after the effective date of this AD, in the main equipment center and the area under the left and right sides of the flight deck floor, replace the duct with a new duct; install an FDARS (including the installation of mounting brackets, ducts, orifice, outlet valve, and screen); and activate the 3-way valve logic (including modification of the associated wiring and related actions); in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin 767-21A0254, dated June 7, 2013. (h) Installation of FDARS and a 3-Way Valve Control Logic and Main Cargo Air Distribution System Change (1) For Model 767-300F series airplanes, as identified in ASB 767-21A0245, R2: Within 72 months after the effective date of this AD, in the main equipment center and the area under the left and right sides of the flight deck floor, change (modify) the 3-way valve control logic and main cargo air distribution system (MCADS), and install an FDARS, in accordance with the Accomplishment Instruction of ASB 767-21A0245, R2, except as provided by paragraph (j) of this AD. (2) For Model 767-300F series airplanes, as identified in ASB 767-21A0247, R1: Within 72 months after the effective date of this AD, change (modify) the 3-way valve control logic and MCADS, and install an FDARS, in accordance with the Accomplishment Instructions of ASB 767-21A0247, R1. (i) Installation of a Flight Deck Display Equipment Cooling System and a 3-Way Valve Logic Change For Model 767-300 series airplanes that have been converted by Boeing to Model 767-300BCF (Boeing Converted Freighter) airplanes, as identified in SB 767-21-0244, R1: Within 72 months after the effective date of this AD, change (modify) the 3-way valve control logic and install a flight deck display equipment cooling system, in accordance with the Accomplishment Instructions of SB 767-21-0244, R1. (j) Exception to Paragraph (h)(1) of This AD For Model 767-300F series airplanes, as identified in ASB 767- 21A0245, R2: If the 3 way valve control logic change (modification) specified in Boeing Service Bulletin 767-21-0235, dated October 8, 2009; or Revision 1, dated July 29, 2011 (``SB 767-21-0235, R1''); is done prior to or concurrent with the actions required by paragraph (h)(1) of this AD, operators need to do only the functional test, FDARS installation, and flex duct change, in accordance with the Accomplishment Instructions of ASB 767-21A0245, R2. Operators do not need to do the other actions specified in the Accomplishment Instructions of ASB 767-21A0245, R2, if the actions in the Accomplishment Instructions of Boeing Service Bulletin 767- 21-0235, dated October 8, 2009; or SB 767-21-0235, R1; are done concurrently. If the functional test fails, before further flight, do corrective actions that are approved in accordance with the procedures specified in paragraph (l) of this AD. (k) Concurrent Requirements (1) For Groups 1 and 3 airplanes, as identified in ASB 767- 21A0245, R2: Prior to or concurrently with accomplishing the requirements of paragraph (h)(1) of this AD, do the relay installation and related wiring changes specified in, and in accordance with, the Accomplishment Instructions of Boeing Service Bulletin 767-21-0235, dated October 8, 2009; or SB 767-21-0235, R1. (2) For Group 1 airplanes, as identified in ASB 767-21A0247, R1: Prior to or concurrently with accomplishing the requirements of paragraph (h)(2) of this AD, do the relay installation and related wiring changes specified in the Accomplishment Instructions of Boeing Service Bulletin 767-21-0235, dated October 8, 2009; or SB 767-21-0235, R1. (3) For Model 767-300 series airplanes that have been converted by Boeing to Model 767-300BCF airplanes, as identified in SB 767-21- 0244, R1: Prior to or concurrently with accomplishing the requirements of paragraph (i) of this AD, do all the actions (installation) specified in the Accomplishment Instructions of Boeing Service Bulletin 767-31-0073, dated October 12, 1995. (l) Alternative Methods of Compliance (AMOCs) (1) The Manager, Seattle 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 attention of the person identified in paragraph (m) of this AD. Information may be emailed to: 9-ANM-SeattleACO-AMOC-Requests@faa.gov. (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, modification, or alteration required by this AD if it is approved by the Boeing Commercial Airplanes Organization Designation Authorization (ODA) that has been authorized by the Manager, Seattle ACO, to make those findings. To be approved, the repair method, modification deviation, or alteration deviation must meet the certification basis of the airplane and the approval must specifically refer to this AD. (m) Related Information For more information about this AD, contact Francis Smith, Aerospace Engineer, Cabin Safety and Environmental Controls Branch, ANM-150S, FAA, Seattle ACO, 1601 Lind Avenue SW., Renton, WA 98057- 3356; phone: 425-917-6596; fax:425 917-6590; email: francis.smith@faa.gov. (n) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise. (3) The following service information was approved for IBR on February 21, 2017 (82 FR 4778, January 17, 2017). (i) Boeing Service Bulletin 767-21-0235, dated October 8, 2009. [[Page 10863]] (ii) Boeing Service Bulletin 767-21-0235, Revision 1, dated July 29, 2011. (iii) Boeing Service Bulletin 767-21-0244, Revision 1, dated March 8, 2010. (iv) Boeing Alert Service Bulletin 767-21A0245, Revision 2, dated September 27, 2013. (v) Boeing Alert Service Bulletin 767-21A0247, Revision 1, dated April 9, 2013. (vi) Boeing Alert Service Bulletin 767-21A0253, dated October 12, 2012. (vii) Boeing Alert Service Bulletin 767-21A0254, dated June 7, 2013. (viii) Boeing Service Bulletin 767-31-0073, dated October 12, 1995. (4) For service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Contractual & Data Services (C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA 90740- 5600; telephone: 562-797-1717; Internet: https://www.myboeingfleet.com. (5) You may view this 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. (6) 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 Renton, Washington, on February 2, 2017. Michael Kaszycki, Assistant Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2017-03028 Filed 2-15-17; 8:45 am] BILLING CODE 4910-13-P
![10860 Federal Register / Vol. 82, No. 31 / Thursday, February 16, 2017 / Rules and Regulations
(a) Effective Date (3) Only authorized Pilatus Service Centers paragraph under 5 U.S.C. 552(a) and 1 CFR
This airworthiness directive (AD) is can do the Supplemental Structural part 51.
effective February 9, 2017. Inspection Document (SSID) as required by (2) You must use this service information
the documents in paragraphs (f)(1)(i) and (ii) as applicable to do the actions required by
(b) Affected ADs of this AD because deviations from the type this AD, unless the AD specifies otherwise.
This AD replaces AD 2014–22–01, 39– design in critical locations could make the (i) STRUCTURAL, COMPONENT AND
18005 (79 FR 67343, November 13, 2014). airplane ineligible for this life extension. MISCELLANEOUS—AIRWORTHINESS
(4) If no compliance time is specified in the LIMITATIONS, Data module code 12–A–04–
(c) Applicability documents listed in paragraphs (f)(1)(i) and 00–00–00A–000A–A, dated July 12, 2016, of
This AD applies to PILATUS AIRCRAFT (ii) of this AD when doing any corrective the Pilatus Model type—PC–12, PC–12/45,
LTD. Models PC–12, PC–12/45, PC–12/47, actions where discrepancies are found as PC–12/47 MSN–101–888, Aircraft
and PC–12/47E airplanes, all manufacturer required in paragraph (f)(2)(iii) of this AD, do Maintenance Manual (AMM), Document No.
serial numbers (MSNs), certificated in any these corrective actions before further flight 02049, 12–A–AM–00–00–00–I, revision 32,
category. after doing the applicable maintenance task. dated July 18, 2016.
(5) During the accomplishment of the (ii) STRUCTURAL AND COMPONENT
(d) Subject actions required in paragraph (f)(2) of this LIMITATIONS—AIRWORTHINESS
Air Transport Association of America AD, including all subparagraphs, if a LIMITATIONS, Data module code 12–B–04–
(ATA) Code 5: Time Limits. discrepancy is found that is not identified in 00–00–00A–000A–A, dated July 19, 2016, of
the documents listed in paragraphs (f)(1)(i) the Pilatus Model type—PC–12/47E MSN–
(e) Reason
and (ii) of this AD, before further flight after 1001–UP, Aircraft Maintenance Manual
This AD was prompted by mandatory finding the discrepancy, contact PILATUS (AMM), Document No. 02300, 12–B–AM–00–
continuing airworthiness information (MCAI) AIRCRAFT LTD. at the address specified in 00–00–I, revision 15, dated July 30, 2016.
originated by an aviation authority of another paragraph (h) of this AD for a repair scheme (3) For PILATUS AIRCRAFT LTD. service
country to identify and correct an unsafe and incorporate that repair scheme. information identified in this AD, contact
condition on an aviation product. The MCAI (6) Before or upon accumulating 6 years PILATUS AIRCRAFT LTD., Customer Service
describes the unsafe condition as a need to time-in-service (TIS) on the MLG attachment Manager, CH–6371 STANS, Switzerland;
incorporate new revisions into the bolts or within the next 3 months TIS after telephone: +41 (0) 41 619 33 33; fax: +41 (0)
Limitations section, Chapter 4, of the FAA- February 9, 2017 (the effective date of this 41 619 73 11; Internet: http://www.pilatus-
approved maintenance program (e.g., AD), whichever occurs later, inspect the MLG aircraft.com or email: SupportPC12@pilatus-
maintenance manual). The limitations were attachment bolts for cracks and corrosion and
revised to include repetitive inspections of aircraft.com.
before further flight take all necessary (4) You may view this service information
the main landing gear (MLG) attachment corrective actions.
bolts. These actions are required to ensure at FAA, FAA, Small Airplane Directorate,
the continued operational safety of the (g) Other FAA AD Provisions 901 Locust, Kansas City, Missouri 64106. For
affected airplanes. information on the availability of this
The following provisions also apply to this
material at the FAA, call (816) 329–4148. In
AD:
(f) Actions and Compliance addition, you can access this service
(1) Alternative Methods of Compliance
Unless already done, do the actions in (AMOCs): The Manager, Standards Office, information on the Internet at http://
paragraphs (f)(1) through (6) of this AD: FAA, has the authority to approve AMOCs www.regulations.gov by searching for and
(1) Before further flight after February 9, for this AD, if requested using the procedures locating Docket No. FAA–2016–7003.
2017 (the effective date of this AD), insert the found in 14 CFR 39.19. Send information to (5) You may view this service information
following revisions into the Limitations ATTN: Doug Rudolph, Aerospace Engineer, that is incorporated by reference at the
section of the FAA-approved maintenance FAA, Small Airplane Directorate, 901 Locust, National Archives and Records
program (e.g., maintenance manual). Room 301, Kansas City, Missouri 64106; Administration (NARA). For information on
Compliance with an electronic version of the telephone: (816) 329–4059; fax: (816) 329– the availability of this material at NARA, call
Limitations section is acceptable provided 4090; email: doug.rudolph@faa.gov. 202–741–6030, or go to: http://
the specifically referenced sections are (i) Before using any approved AMOC on www.archives.gov/federal-register/cfr/ibr-
followed even though there may be any airplane to which the AMOC applies, locations.html.
differences with the pagination: notify your appropriate principal inspector Issued in Kansas City, Missouri, on January
(i) STRUCTURAL, COMPONENT AND (PI) in the FAA Flight Standards District 24, 2017.
MISCELLANEOUS—AIRWORTHINESS Office (FSDO), or lacking a PI, your local
LIMITATIONS, Data module code 12–A–04– Melvin Johnson,
FSDO.
00–00–00A–000A–A, dated July 12, 2016, of (ii) AMOCs approved for AD 2014–22–01, Acting Manager, Small Airplane Directorate,
the Pilatus Model type—PC–12, PC–12/45, 39–18005 (79 FR 67343, November 13, 2014) Aircraft Certification Service.
PC–12/47 MSN–101–888, Aircraft are not approved as AMOCs for this AD. [FR Doc. 2017–02772 Filed 2–15–17; 8:45 am]
Maintenance Manual (AMM), Document No. (2) Airworthy Product: For any requirement BILLING CODE 4910–13–P
02049, 12–A–AM–00–00–00–I, revision 32, in this AD to obtain corrective actions from
dated July 18, 2016; and a manufacturer or other source, use these
(ii) STRUCTURAL AND COMPONENT actions if they are FAA-approved. Corrective
LIMITATIONS—AIRWORTHINESS
DEPARTMENT OF TRANSPORTATION
actions are considered FAA-approved if they
LIMITATIONS, Data module code 12–B–04– are approved by the State of Design Authority
00–00–00A–000A–A, dated July 19, 2016, of
Federal Aviation Administration
(or their delegated agent). You are required
the Pilatus Model type—PC–12/47E MSN– to assure the product is airworthy before it
1001–UP, Aircraft Maintenance Manual is returned to service. 14 CFR Part 39
(AMM), Document No. 02300, 12–B–AM–00– [Docket No. FAA–2013–0797; Directorate
00–00–I, revision 15, dated July 30, 2016. (h) Related Information
Identifier 2013–NM–007–AD; Amendment
(2) The new limitations section revisions Refer to MCAI European Aviation Safety 39–18776; AD 2017–01–09]
listed in paragraphs (f)(1)(i) and (ii) of this Agency (EASA) AD No. 2016–0083, dated
AD specify the following: April 28, 2016, for related information. You RIN 2120–AA64
jstallworth on DSK7TPTVN1PROD with RULES
(i) Establish inspections of the MLG may examine the MCAI on the Internet at
attachment bolts, https://www.regulations.gov/ Airworthiness Directives; The Boeing
(ii) Specify replacement of components document?D=FAA-2016-7003-0002. Company Airplanes
before or upon reaching the applicable life
limit, and (i) Material Incorporated by Reference AGENCY: Federal Aviation
(iii) Specify accomplishment of all (1) The Director of the Federal Register Administration (FAA), DOT.
applicable maintenance tasks within certain approved the incorporation by reference
ACTION: Final rule; correction.
thresholds and intervals. (IBR) of the service information listed in this
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![Federal Register / Vol. 82, No. 31 / Thursday, February 16, 2017 / Rules and Regulations 10861
SUMMARY: The FAA is correcting an main equipment center for certain (including the installation of mounting
airworthiness directive (AD) that Model 767–300 and 767–300F series brackets, ducts, orifice, outlet valve, and
published in the Federal Register. That airplanes. For certain airplanes, AD screen); and activating the 3-way valve
AD applies to certain The Boeing 2017–01–09 also requires modification, logic (including modification of the
Company Model 767–300 and 767–300F replacement, and installation of flight associated wiring and related actions).
airplanes. Certain service information deck air relief system (FDARS) • Boeing Service Bulletin 767–31–
citations in the preamble and regulatory components. 0073, dated October 12, 1995. The
text are incorrect. This document service information describes
Need for the Correction procedures for installing a maintenance
corrects those errors. In all other
respects, the original document remains As published, certain service data selection system for the engine
the same. information citations in the preamble indication and crew alerting system.
DATES: This final rule is effective and regulatory text were incorrect. The This service information is reasonably
February 21, 2017. incorrectly specified citation in the available because the interested parties
The Director of the Federal Register preamble and regulatory text was have access to it through their normal
approved the incorporation by reference Boeing Service Bulletin 767–27–0244, course of business or by the means
of certain publications listed in this AD Revision 1, dated March 8, 2010 (‘‘SB identified in the ADDRESSES section.
as of February 21, 2017 (82 FR 4778, 767–27–0244, R1’’); the correct citation
is Boeing Service Bulletin 767–21–0244, Correction of Publication
January 17, 2017).
Revision 1, dated March 8, 2010 (‘‘SB This document corrects errors in the
ADDRESSES: For service information
767–21–0244, R1’’). citation of certain service information
identified in this final rule, contact
and correctly adds the AD as an
Boeing Commercial Airplanes, Related Service Information Under 1 amendment to 14 CFR 39.13. Although
Attention: Contractual & Data Services CFR Part 51 no other part of the preamble or
(C&DS), 2600 Westminster Blvd., MC We reviewed the following service regulatory information has been
110–SK57, Seal Beach, CA 90740–5600; information. corrected, we are publishing the entire
telephone: 562–797–1717; Internet: • Boeing Service Bulletin 767–21– rule in the Federal Register.
https://www.myboeingfleet.com. You 0235, dated October 8, 2009; and The effective date of this AD remains
may view this referenced service Revision 1, dated July 29, 2011 (‘‘SB February 21, 2017.
information at the FAA, Transport 767–21–0235, R1’’). The service Since this action only corrects errors
Airplane Directorate, 1601 Lind Avenue information describes procedures for a in the citation of certain service
SW., Renton, WA. For information on relay installation and related wiring information, it has no adverse economic
the availability of this material at the changes (which change (modify) the 3- impact and imposes no additional
FAA, call 425–227–1221. It is also way valve control logic for the cooling burden on any person. Therefore, we
available on the Internet at http:// system for the flight deck display have determined that notice and public
www.regulations.gov by searching for equipment on freighter airplanes). procedures are unnecessary.
and locating Docket No. FAA–2013– • Boeing Service Bulletin 767–21–
0797. 0244, Revision 1, dated March 8, 2010 List of Subjects in 14 CFR Part 39
Examining the AD Docket (‘‘SB 767–21–0244, R1’’). The service Air transportation, Aircraft, Aviation
information describes procedures for safety, Incorporation by reference,
You may examine the AD docket on Safety.
changing (modifying) the 3-way valve
the Internet at http://
control logic and installing a cooling Adoption of the Correction
www.regulations.gov; or in person at the
system for the flight deck display
Docket Management Facility between 9 Accordingly, pursuant to the
equipment.
a.m. and 5 p.m., Monday through • Boeing Alert Service Bulletin 767– authority delegated to me by the
Friday, except Federal holidays. The AD 21A0245, Revision 2, dated September Administrator, the Federal Aviation
docket contains this AD, the regulatory 27, 2013 (‘‘ASB 767–21A0245, R2’’); and Administration amends part 39 of the
evaluation, any comments received, and Boeing Alert Service Bulletin 767– Federal Aviation Regulations (14 CFR
other information. The address for the 21A0247, Revision 1, dated April 9, part 39) as follows:
Docket Office (phone: 800–647–5527) is 2013 (‘‘ASB 767–21A0247, R1’’). The
Docket Management Facility, U.S. service information describes PART 39—AIRWORTHINESS
Department of Transportation, Docket procedures for changing (modifying) the DIRECTIVES
Operations, M–30, West Building 3-way valve control logic and main
Ground Floor, Room W12–140, 1200 ■ 1. The authority citation for part 39
cargo air distribution system (MCADS), continues to read as follows:
New Jersey Avenue SE., Washington, and installing an FDARS. These
DC 20590. documents are distinct since they apply Authority: 49 U.S.C. 106(g), 40113, 44701.
FOR FURTHER INFORMATION CONTACT: to different airplane models. § 39.13 [Corrected]
Francis Smith, Aerospace Engineer, • Boeing Alert Service Bulletin 767–
Cabin Safety and Environmental 21A0253, dated October 12, 2012. The ■ 2. The FAA amends § 39.13 by adding
Controls Branch, ANM–150S, FAA, service information describes the following new airworthiness
Seattle Aircraft Certification Office procedures for replacing the existing directive (AD):
(ACO), 1601 Lind Avenue SW., Renton, duct, installing an FDARS, changing 2017–01–09 The Boeing Company:
WA 98057–3356; phone: 425–917–6596; (modifying) the 3-way valve control Amendment 39–18776; Docket No.
jstallworth on DSK7TPTVN1PROD with RULES
fax: 425–917–6590; email: logic, and installing a new altitude FAA–2013–0797; Directorate Identifier
francis.smith@faa.gov. switch and pitot tube. 2013–NM–007–AD.
SUPPLEMENTARY INFORMATION: • Boeing Alert Service Bulletin 767– (a) Effective Date
Airworthiness Directive 2017–01–09, 21A0254, dated June 7, 2013. The This AD is effective February 21, 2017.
amendment 39–18776 (82 FR 4778, service information describes
January 17, 2017), requires modification procedures for replacing the duct with (b) Affected ADs
and installation of components in the a new duct; installing an FDARS None.
VerDate Sep<11>2014 11:26 Feb 15, 2017 Jkt 241001 PO 00000 Frm 00007 Fmt 4700 Sfmt 4700 E:\FR\FM\16FER1.SGM 16FER1](https://thefederalregister.org/doc/82_FR_10891/page/2.svg)
![Federal Register / Vol. 82, No. 31 / Thursday, February 16, 2017 / Rules and Regulations 10863
(ii) Boeing Service Bulletin 767–21–0235, at 82 FR 654, is delayed from March 6, Services Administration (SAMHSA)
Revision 1, dated July 29, 2011. 2017, to March 21, 2017. published a final rule on Confidentiality
(iii) Boeing Service Bulletin 767–21–0244, of Substance Use Disorder Patient
FOR FURTHER INFORMATION CONTACT:
Revision 1, dated March 8, 2010. Records. That rule is scheduled to take
(iv) Boeing Alert Service Bulletin 767– Christopher Kuczynski, Assistant Legal
21A0245, Revision 2, dated September 27, Counsel, (202) 663–4665, or Aaron effect on February 17, 2017. In
2013. Konopasky, Senior Attorney-Advisor, accordance with the memorandum of
(v) Boeing Alert Service Bulletin 767– (202) 663–4127 (voice), or (202) 663– January 20, 2017, from the Assistant to
21A0247, Revision 1, dated April 9, 2013. 7026 (TTY), Office of Legal Counsel, the President and Chief of Staff, entitled
(vi) Boeing Alert Service Bulletin 767– U.S. Equal Employment Opportunity ‘‘Regulatory Freeze Pending Review,’’
21A0253, dated October 12, 2012. Commission. (These are not toll free published in the Federal Register on
(vii) Boeing Alert Service Bulletin 767– numbers.) Requests for this document in January 24, 2017 (82 FR 8346), this
21A0254, dated June 7, 2013. action delays for 60 days from the date
(viii) Boeing Service Bulletin 767–31–0073,
an alternative format should be made to
the Office of Communications and of the memorandum the effective date of
dated October 12, 1995. the rule entitled ‘‘Confidentiality of
(4) For service information identified in Legislative Affairs at (202) 663–4191
this AD, contact Boeing Commercial (voice) or (202) 663–4494 (TTY). (These Substance Use Disorder Patient
Airplanes, Attention: Contractual & Data are not toll free numbers.) Records’’ published in the Federal
Services (C&DS), 2600 Westminster Blvd., Register on January 18, 2017 (82 FR
SUPPLEMENTARY INFORMATION: On
MC 110–SK57, Seal Beach, CA 90740–5600; 6052).
January 3, 2017, the EEOC published a
telephone: 562–797–1717; Internet: https:// DATES: The effective date of the
www.myboeingfleet.com.
final rule amending 29 CFR 1614.203 to
clarify the affirmative action obligations Confidentiality of Substance Use
(5) You may view this service information
that Section 501 of the Rehabilitation Disorder Patient Records final rule,
at the FAA, Transport Airplane Directorate,
1601 Lind Avenue SW., Renton, WA. For Act of 1973, 29 U.S.C. 791, imposes on published in the Federal Register on
information on the availability of this federal agencies as employers. As January 18, 2017 (82 FR 6052) is
material at the FAA, call 425–227–1221. clarified in a correction published on delayed from February 17, 2017, to a
(6) You may view this service information January 11, 2017, at 32 FR 3170, the rule new effective date of March 21, 2017.
that is incorporated by reference at the was to become effective on March 6, FOR FURTHER INFORMATION CONTACT:
National Archives and Records 2017. On January 20, 2017, the White Danielle Tarino, Telephone number:
Administration (NARA). For information on (240) 276–2857, Email address:
the availability of this material at NARA, call
House issued a memorandum
instructing Federal agencies to postpone PrivacyRegulations@samhsa.hhs.gov.
202–741–6030, or go to: http://
www.archives.gov/federal-register/cfr/ibr- until 60 days after January 20, 2017, the SUPPLEMENTARY INFORMATION: The
locations.html. effective dates of any regulations that Confidentiality of Substance Use
had been published in the Federal Disorder Patient Records Final Rule
Issued in Renton, Washington, on February
2, 2017. Register but had not yet taken effect, for updates and modernizes the
the purpose of ‘‘reviewing questions of Confidentiality of Alcohol and Drug
Michael Kaszycki,
fact, law, and policy they raise.’’ The Abuse Patient Records regulations (42
Assistant Manager, Transport Airplane CFR part 2) to facilitate integration of
Directorate, Aircraft Certification Service.
EEOC is, therefore, delaying the
effective date of its final rule published care and new health care delivery
[FR Doc. 2017–03028 Filed 2–15–17; 8:45 am] models while protecting the privacy of
on January 3, 2017, at 82 FR 654, until
BILLING CODE 4910–13–P
March 21, 2017. patients diagnosed, treated, or referred
for treatment for a substance use
For the Commission.
disorder. To the extent that 5 U.S.C. 553
Dated: February 10, 2017.
EQUAL EMPLOYMENT OPPORTUNITY applies to this action to delay the rule’s
COMMISSION Victoria A. Lipnic, effective date, it is exempt from notice
Acting Chair. and comment because it constitutes a
29 CFR Part 1614 [FR Doc. 2017–03146 Filed 2–15–17; 8:45 am] rule of procedure under 5 U.S.C.
BILLING CODE 6570–01–P 553(b)(A). Alternatively, the
RIN 3046–AA94
Department’s implementation of this
Affirmative Action for Individuals With rule without opportunity for public
Disabilities in Federal Employment DEPARTMENT OF HEALTH AND comment, effective immediately upon
HUMAN SERVICES publication today in the Federal
AGENCY: Equal Employment Register, is based on the good cause
Opportunity Commission. Office of the Secretary exception in 5 U.S.C. 553(b)(B) in that
ACTION: Final rule; delay of effective seeking public comment is
date. 42 CFR Part 2 impracticable, unnecessary and contrary
[SAMHSA–4162–20] to the public interest. The 60-day delay
SUMMARY: In accordance with the in effective date is necessary to give
Presidential directive in the RIN 0930–AA21 Department officials the opportunity for
memorandum from the Assistant to the further review and consideration of new
President and Chief of Staff, dated Confidentiality of Substance Use
regulations, consistent with the
January 20, 2017, and entitled Disorder Patient Records; Delay of
Assistant to the President’s
‘‘Regulatory Freeze Pending Review,’’ Effective Date
memorandum of January 20, 2017. This
jstallworth on DSK7TPTVN1PROD with RULES
the U.S. Equal Employment AGENCY: Substance Abuse and Mental memorandum instructed federal
Opportunity Commission (‘‘EEOC’’) is Health Services Administration, HHS. agencies to delay the effective date of
delaying the effective date of a final rule rules published in the Federal Register,
ACTION: Final rule; delay of effective
published in the Federal Register on but which have not yet taken effect, for
date.
January 3, 2017. a period of 60-days from the date of the
DATES: The effective date of the EEOC SUMMARY: On January 18, 2017, the memorandum. Given the imminence of
final rule published on January 3, 2017, Substance Abuse and Mental Health the effective date, seeking prior public
VerDate Sep<11>2014 11:26 Feb 15, 2017 Jkt 241001 PO 00000 Frm 00009 Fmt 4700 Sfmt 4700 E:\FR\FM\16FER1.SGM 16FER1](https://thefederalregister.org/doc/82_FR_10891/page/4.svg)
Document Created: 2018-02-01 15:02:18
Document Modified: 2018-02-01 15:02:18
| 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; correction. | |
| Dates | This final rule is effective February 21, 2017. | |
| Contact | Francis Smith, Aerospace Engineer, Cabin Safety and Environmental Controls Branch, ANM-150S, FAA, Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue SW., Renton, WA 98057-3356; phone: 425-917-6596; fax: 425-917-6590; email: [email protected] | |
| FR Citation | 82 FR 10860 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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