83 FR 48708 - Airworthiness Directives; The Boeing Company Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 83, Issue 188 (September 27, 2018)
Federal Aviation Administration
Federal Register Volume 83, Issue 188 (September 27, 2018)
| Page Range | 48708-48711 | |
| FR Document | 2018-20631 |
[Federal Register Volume 83, Number 188 (Thursday, September 27, 2018)] [Rules and Regulations] [Pages 48708-48711] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2018-20631] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2017-1026; Product Identifier 2017-NM-097-AD; Amendment 39-19422; AD 2018-19-21] RIN 2120-AA64 Airworthiness Directives; The Boeing Company Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. ----------------------------------------------------------------------- SUMMARY: We are adopting a new airworthiness directive (AD) for all The Boeing Company Model 707 airplanes, and Model 720 and 720B series airplanes. This AD was prompted by fuel system reviews conducted by the manufacturer. This AD requires revising the maintenance or inspection program to include new airworthiness limitations. We are issuing this AD to address the unsafe condition on these products. DATES: This AD is effective November 1, 2018. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of November 1, 2018. 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 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-2017- 1026. 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-2017- 1026; 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 Docket Operations, U.S. Department of Transportation, Docket Operations, [[Page 48709]] M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590. FOR FURTHER INFORMATION CONTACT: Samuel Lee, Aerospace Engineer, Propulsion Section, FAA, Los Angeles ACO Branch, 3960 Paramount Boulevard, Lakewood, CA 90712-4137; phone: 562-627-5262; fax: 562-627- 5210; email: samuel.lee@faa.gov. 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 all The Boeing Company Model 707 airplanes, and Model 720 and 720B series airplanes. The NPRM published in the Federal Register on November 20, 2017 (82 FR 55057). The NPRM was prompted by fuel system reviews conducted by the manufacturer. The NPRM proposed to require revising the maintenance or inspection program to include new airworthiness limitations. We are issuing this AD to detect and correct potential ignition sources inside fuel tanks caused by latent failures, alterations, repairs, or maintenance actions, which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane. Comments We gave the public the opportunity to participate in developing this final rule. We have considered the comment received. Boeing supported the NPRM. Clarification of Alternative Wire Types and Sleeving Paragraph (h) of this AD allows alternative wire types and sleeving materials for certain wire types and sleeving materials identified in AWL No. 28-AWL-03. AWL No. 28-AWL-03 was originally mandated by AD 2008-04-11 R1, Amendment 39-16147 (74 FR 68505, December 28, 2009) (``AD 2008-04-11 R1''). Since the issuance of AD 2008-04-11 R1, which is terminated by this AD, we received numerous requests for approval of alternative methods of compliance (AMOCs) from operators and supplemental type certificate (STC) holders (or applicants) to allow the installation of the alternative wire types and sleeving. We evaluated certain attributes of those alternative wire types and sleeving for each installation, and issued numerous AMOC approvals for AD 2008-04-11 R1, based on our determination that the installation of those wire types and sleeving would provide an acceptable level of safety. The alternative wire types and sleeving specified in paragraph (h) of this AD were previously approved as an AMOC for AD 2008-04-11 R1. Although paragraph (h) of this AD provides certain allowances, it does not provide approval of alternative wire types and sleeving that are installed as part of an aircraft design change. Each applicant for any design change is responsible to show that the installation of alternative wire types and sleeving identified in paragraphs (h)(l) and (h)(2) of this AD complies with all applicable regulatory requirements. This responsibility includes, but is not limited to, substantiation of compliance with flammability requirements, and substantiation to show that sleeve installation, including the selection of sleeve thickness, is adequate to protect wires from chafing for the life of installation. Conclusion We reviewed the relevant data, considered the comment received, and determined that air safety and the public interest require adopting this final rule as proposed, except for minor editorial changes. We have determined that these minor changes:Are consistent with the intent that was proposed in the NPRM for addressing the unsafe condition; and Do not add any additional burden upon the public than was already proposed in the NPRM. Related Service Information Under 1 CFR Part 51 We reviewed Boeing 707/720 Airworthiness Limitations (AWLs), D6- 7552-AWL, dated October 2016, which addresses fuel systems ignition prevention and impact-resistant fuel tank access doors. 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 9 airplanes of U.S. registry. We estimate the following costs to comply with this AD: We have determined that revising the maintenance or inspection program takes an average of 90 work-hours per operator, although we recognize that this number may vary from operator to operator. In the past, we have estimated that this action takes 1 work-hour per airplane. Since operators incorporate maintenance or inspection program changes for their affected fleet(s), we have determined that a per- operator estimate is more accurate than a per-airplane estimate. Therefore, we estimate the total cost per operator to be $7,650 (90 work-hours x $85 per work-hour). Authority for This Rulemaking Title 49 of the United States Code specifies the FAA's authority to issue rules on aviation safety. Subtitle I, section 106, describes the authority of the FAA Administrator. Subtitle VII: Aviation Programs, describes in more detail the scope of the Agency's authority. We are issuing this rulemaking under the authority described in Subtitle VII, Part A, Subpart III, Section 44701: ``General requirements.'' Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. 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. [[Page 48710]] 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): 2018-19-21 The Boeing Company: Amendment 39-19422; Docket No. FAA- 2017-1026; Product Identifier 2017-NM-097-AD. (a) Effective Date This AD is effective November 1, 2018. (b) Affected ADs This AD affects the ADs specified in paragraphs (b)(1) and (b)(2) of this AD. (1) AD 2008-04-11 R1, Amendment 39-16147 (74 FR 68505, December 28, 2009) (``AD 2008-04-11 R1''). (2) AD 2013-24-07, Amendment 39-17681 (78 FR 72550, December 3, 2013) (``AD 2013-24-07''). (c) Applicability This AD applies to all The Boeing Company airplanes, certificated in any category, identified in paragraphs (c)(1) and (c)(2) of this AD. (1) Model 707-100 long body, -200, -100B long body, -100B short body, -300, -300B, -300C, and -400 series airplanes. (2) Model 720 and 720B series airplanes. (d) Subject Air Transport Association (ATA) of America Code 28, Fuel. (e) Unsafe Condition This AD was prompted by fuel system reviews conducted by the manufacturer. We are issuing this AD to detect and correct potential ignition sources inside fuel tanks caused by latent failures, alterations, repairs, or maintenance actions, which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Revision of Maintenance or Inspection Program Within 60 days after the effective date of this AD, revise the maintenance or inspection program, as applicable, to incorporate the information in Section A, including Subsections A.1, A.2, and Appendix A, as specified in Boeing 707/720 Airworthiness Limitations (AWLs), D6-7552-AWL, dated October 2016; except as provided in paragraph (h) of this AD. The initial compliance times for the AWL tasks are within the applicable compliance times specified in paragraphs (g)(1) through (g)(5) of this AD. (1) AWL No. 28-AWL-01, External Wires Over Center Fuel Tank, as specified in Boeing 707/720 Airworthiness Limitations (AWLs), D6- 7552-AWL, dated October 2016. The initial compliance time for accomplishment of the actions specified by AWL No. 28-AWL-01 is specified in paragraph (g)(1)(i) or (g)(1)(ii) of this AD, as applicable. (i) For airplanes that have been previously inspected as specified in 28-AWL-01 as of the effective date of this AD: Conduct the inspection within 120 months after the most recent inspection. (ii) For airplanes that have not been inspected as specified in 28-AWL-01 as of the effective date of this AD: Conduct the inspection within 12 months after the effective date of this AD. (2) AWL No. 28-AWL-18, AC Fuel Boost Pump Bonding Installation, as specified in Boeing 707/720 Airworthiness Limitations (AWLs), D6- 7552-AWL, dated October 2016. The initial compliance time for accomplishment of the actions specified by AWL No. 28-AWL-18 is specified in paragraph (g)(2)(i) or (g)(2)(ii) of this AD, as applicable. (i) For airplanes that have been previously inspected as specified in 28-AWL-18 as of the effective date of this AD: Conduct the inspection within 72 months after the most recent inspection. (ii) For airplanes that have not been inspected as specified in 28-AWL-18 as of the effective date of this AD: Conduct the inspection within 12 months after the effective date of this AD. (3) AWL No. 28-AWL-19, Fuel Valve Bonding Jumper Installation-- Engine Fuel Shutoff, Defuel, Reserve Tank Transfer, Fuel Dump, and Fuel Manifold Valves, as specified in Boeing 707/720 Airworthiness Limitations (AWLs), D6-7552-AWL, dated October 2016. The initial compliance time for accomplishment of the actions specified by AWL No. 28-AWL-19 is specified in paragraph (g)(3)(i) or (g)(3)(ii) of this AD, as applicable. (i) For airplanes that have been previously inspected as specified in 28-AWL-19 as of the effective date of this AD: Conduct the inspection within 72 months after the most recent inspection. (ii) For airplanes that have not been inspected as specified in 28-AWL-19 as of the effective date of this AD: Conduct the inspection within 12 months after the effective date of this AD. (4) AWL No. 28-AWL-21, Dry Bay Fuel Manifold Assembly--Bonding Jumper Installation, as specified in Boeing 707/720 Airworthiness Limitations (AWLs), D6-7552-AWL, dated October 2016. The initial compliance time for accomplishment of the actions specified by AWL No. 28-AWL-21 is specified in paragraph (g)(4)(i) or (g)(4)(ii) of this AD, as applicable. (i) For airplanes that have been previously inspected as specified in 28-AWL-21 as of the effective date of this AD: Conduct the inspection within 72 months after the most recent inspection. (ii) For airplanes that have not been inspected as specified in 28-AWL-21 as of the effective date of this AD: Conduct the inspection within 12 months after the effective date of this AD. (5) AWL No. 28-AWL-23, Reserve Tank Transfer Piping Assembly-- Bonding Jumper Installation, as specified in Boeing 707/720 Airworthiness Limitations (AWLs), D6-7552-AWL, dated October 2016. The initial compliance time for accomplishment of the actions specified by AWL No. 28-AWL-23 is specified in paragraph (g)(5)(i) or (g)(5)(ii) of this AD, as applicable. (i) For airplanes that have been previously inspected as specified in 28-AWL-23 as of the effective date of this AD: Conduct the inspection within 72 months after the most recent inspection. (ii) For airplanes that have not been inspected as specified in 28-AWL-23 as of the effective date of this AD: Conduct the inspection within 12 months after the effective date of this AD. (h) Additional Acceptable Wire Types and Sleeving As an option, when accomplishing the actions required by paragraph (g) of this AD, the changes specified in paragraphs (h)(1) and (h)(2) of this AD are acceptable. (1) Where AWL No. 28-AWL-03 identifies wire types BMS 13-48, BMS 13-58, and BMS 13-60, the following wire types are acceptable: MIL- W-22759/16, SAE AS22759/16 (M22759/16), MIL-W-22759/32, SAE AS22759/ 32 (M22759/32), MIL-W-22759/34, SAE AS22759/34 (M22759/34), MIL-W- 22759/41, SAE AS22759/41 (M22759/41), MIL-W-22759/86, SAE AS22759/86 (M22759/86), MIL-W-22759/87, SAE AS22759/87 (M22759/87), MIL-W- 22759/92 and SAE AS22759/92 (M22759/92); and MIL-C-27500 and NEMA WC 27500 cables constructed from these military or SAE specification wire types identified above. (2) Where AWL No. 28-AWL-03 identifies TFE-2X Standard wall for wire sleeving, the following sleeving materials are acceptable: Roundit 2000NX and Varglas Type HO, HP, or HM. (i) No Alternative Actions and Intervals Except as provided in paragraph (h) of this AD, after the maintenance or inspection program has been revised as required by paragraph (g) of this AD, no alternative actions (e.g., inspections) or intervals may be used unless the actions or intervals are approved as an alternative method of compliance (AMOC) in accordance with the procedures specified in paragraph (k) of this AD. (j) Terminating Action for Other ADs (1) Accomplishment of the actions required by paragraph (g) of this AD terminates all requirements of AD 2008-04-11 R1. [[Page 48711]] (2) Accomplishment of the actions required by paragraph (g) of this AD terminates the requirements of paragraph (h) of AD 2013-24- 07. (k) Alternative Methods of Compliance (AMOCs) (1) The Manager, Los Angeles 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 manager of the certification office, send it to the attention of the person identified in paragraph (l) of this AD. Information may be emailed to: 9-AWP-LAACO-ADS@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, Los Angeles ACO Branch, 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. (l) Related Information For more information about this AD, contact Samuel Lee, Aerospace Engineer, Propulsion Section, FAA, Los Angeles ACO Branch, 3960 Paramount Boulevard, Lakewood, CA 90712-4137; phone: 562-627- 5262; fax: 562-627-5210; email: samuel.lee@faa.gov. (m) 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. (i) Boeing 707/720 Airworthiness Limitations (AWLs), D6-7552- AWL, dated October 2016. (Subsection A.2 of this document includes pages 33 and 34, which are not identified in the Table of Contents.) (ii) Reserved. (3) 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. (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 September 10, 2018. Michael Kaszycki, Acting Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2018-20631 Filed 9-26-18; 8:45 am] BILLING CODE 4910-13-P
![48708 Federal Register / Vol. 83, No. 188 / Thursday, September 27, 2018 / Rules and Regulations
(d) Subject Dassault Aviation’s EASA Design DEPARTMENT OF TRANSPORTATION
Air Transport Association (ATA) of Organization Approval (DOA). If approved by
America Code 30, Ice and Rain Protection. the DOA, the approval must include the Federal Aviation Administration
DOA-authorized signature.
(e) Reason
(j) Related Information
14 CFR Part 39
This AD was prompted by reports of
metallic debris found in the wing slat piccolo (1) Refer to Mandatory Continuing [Docket No. FAA–2017–1026; Product
tubes; investigation revealed that the debris Airworthiness Information (MCAI) EASA AD Identifier 2017–NM–097–AD; Amendment
originated from the flow guide of the ball 39–19422; AD 2018–19–21]
2018–0022, dated January 29, 2018, for
joint located downstream of the wing anti-ice related information. This MCAI may be RIN 2120–AA64
valve. We are issuing this AD to address
found in the AD docket on the internet at
restricted airflow of the piccolo tubes, Airworthiness Directives; The Boeing
leading to insufficient wing anti-ice http://www.regulations.gov by searching for
capability and significant undetected ice and locating Docket No. FAA–2018–0496. Company Airplanes
accretion on the wing, which could result in (2) For more information about this AD,
AGENCY: Federal Aviation
loss of control of the airplane. contact Tom Rodriguez, Aerospace Engineer,
Administration (FAA), DOT.
International Section, Transport Standards
(f) Compliance ACTION: Final rule.
Branch, FAA, 2200 South 216th Street, Des
Comply with this AD within the Moines, WA 98198; telephone and fax 206–
compliance times specified, unless already SUMMARY: We are adopting a new
231–3226.
done. airworthiness directive (AD) for all The
(k) Material Incorporated by Reference Boeing Company Model 707 airplanes,
(g) Repetitive Inspections and Corrective
(1) The Director of the Federal Register and Model 720 and 720B series
Actions
approved the incorporation by reference airplanes. This AD was prompted by
Within 25 months after the effective date fuel system reviews conducted by the
of this AD: Perform a detailed inspection for (IBR) of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR manufacturer. This AD requires revising
discrepancies of the flow guide of the ball
joint located downstream of the wing anti-ice part 51. the maintenance or inspection program
valve, and do all applicable related (2) You must use this service information to include new airworthiness
investigative and corrective actions, in as applicable to do the actions required by limitations. We are issuing this AD to
accordance with the Accomplishment this AD, unless this AD specifies otherwise. address the unsafe condition on these
Instructions of Dassault Aviation Service (i) Dassault Aviation Service Bulletin products.
Bulletin F2000–441, dated June 20, 2017; or F2000–441, dated June 20, 2017.
Dassault Aviation Service Bulletin F2000EX–
DATES: This AD is effective November 1,
(ii) Dassault Aviation Service Bulletin 2018.
413, dated July 10, 2017; as applicable.
F2000EX–413, dated July 10, 2017. The Director of the Federal Register
Repeat the detailed inspection thereafter at
(3) For service information identified in approved the incorporation by reference
intervals not to exceed 25 months. Do all
applicable corrective actions before further this AD, contact Dassault Falcon Jet of a certain publication listed in this AD
flight. Corporation, Teterboro Airport, P.O. Box as of November 1, 2018.
2000, South Hackensack, NJ 07606;
(h) No Reporting Requirement ADDRESSES: For service information
telephone 201–440–6700; internet http://
Although the service information identified in this final rule, contact
www.dassaultfalcon.com.
identified in paragraph (g) of this AD (4) You may view this service information
Boeing Commercial Airplanes,
specifies to submit certain information to the at the FAA, Transport Standards Branch,
Attention: Contractual & Data Services
manufacturer, this AD does not include that 2200 South 216th St., Des Moines, WA. For (C&DS), 2600 Westminster Blvd., MC
requirement.
information on the availability of this 110–SK57, Seal Beach, CA 90740–5600;
(i) Other FAA AD Provisions material at the FAA, call 206–231–3195. telephone: 562–797–1717; internet:
(5) You may view this service information https://www.myboeingfleet.com. You
The following provisions also apply to this
that is incorporated by reference at the may view this service information at the
AD:
(1) Alternative Methods of Compliance National Archives and Records FAA, Transport Standards Branch, 2200
(AMOCs): The Manager, International Administration (NARA). For information on South 216th St., Des Moines, WA. For
Section, Transport Standards Branch, FAA, the availability of this material at NARA, call information on the availability of this
has the authority to approve AMOCs for this 202–741–6030, or go to: http:// material at the FAA, call 206–231–3195.
AD, if requested using the procedures found www.archives.gov/federal-register/cfr/ibr- It is also available on the internet at
in 14 CFR 39.19. In accordance with 14 CFR locations.html. http://www.regulations.gov by searching
39.19, send your request to your principal for and locating Docket No. FAA–2017–
inspector or local Flight Standards District Issued in Des Moines, Washington, on
1026.
Office, as appropriate. If sending information September 7, 2018.
directly to the International Section, send it Michael Kaszycki, Examining the AD Docket
to the attention of the person identified in
paragraph (j)(2) of this AD. Information may Acting Director, System Oversight Division, You may examine the AD docket on
be emailed to: 9-ANM-116-AMOC- Aircraft Certification Service. the internet at http://
REQUESTS@faa.gov. Before using any [FR Doc. 2018–20630 Filed 9–26–18; 8:45 am] www.regulations.gov by searching for
approved AMOC, notify your appropriate BILLING CODE 4910–13–P and locating Docket No. FAA–2017–
principal inspector, or lacking a principal 1026; or in person at Docket Operations
inspector, the manager of the local flight between 9 a.m. and 5 p.m., Monday
standards district office/certificate holding through Friday, except Federal holidays.
district office. The AD docket contains this final rule,
daltland on DSKBBV9HB2PROD with RULES
(2) Contacting the Manufacturer: For any the regulatory evaluation, any
requirement in this AD to obtain corrective
actions from a manufacturer, the action must
comments received, and other
be accomplished using a method approved information. The address for Docket
by the Manager, International Section, Operations (phone: 800–647–5527) is
Transport Standards Branch, FAA; or the Docket Operations, U.S. Department of
European Aviation Safety Agency (EASA); or Transportation, Docket Operations,
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List of Subjects in 14 CFR Part 39 program, as applicable, to incorporate the actions specified by AWL No. 28–AWL–21 is
information in Section A, including specified in paragraph (g)(4)(i) or (g)(4)(ii) of
Air transportation, Aircraft, Aviation Subsections A.1, A.2, and Appendix A, as this AD, as applicable.
safety, Incorporation by reference, specified in Boeing 707/720 Airworthiness (i) For airplanes that have been previously
Safety. Limitations (AWLs), D6–7552–AWL, dated inspected as specified in 28–AWL–21 as of
October 2016; except as provided in the effective date of this AD: Conduct the
Adoption of the Amendment paragraph (h) of this AD. The initial inspection within 72 months after the most
Accordingly, under the authority compliance times for the AWL tasks are recent inspection.
delegated to me by the Administrator, within the applicable compliance times (ii) For airplanes that have not been
the FAA amends 14 CFR part 39 as specified in paragraphs (g)(1) through (g)(5) inspected as specified in 28–AWL–21 as of
of this AD. the effective date of this AD: Conduct the
follows:
(1) AWL No. 28–AWL–01, External Wires inspection within 12 months after the
Over Center Fuel Tank, as specified in effective date of this AD.
PART 39—AIRWORTHINESS
Boeing 707/720 Airworthiness Limitations (5) AWL No. 28–AWL–23, Reserve Tank
DIRECTIVES (AWLs), D6–7552–AWL, dated October 2016. Transfer Piping Assembly—Bonding Jumper
The initial compliance time for Installation, as specified in Boeing 707/720
■ 1. The authority citation for part 39 Airworthiness Limitations (AWLs), D6–
accomplishment of the actions specified by
continues to read as follows: AWL No. 28–AWL–01 is specified in 7552–AWL, dated October 2016. The initial
Authority: 49 U.S.C. 106(g), 40113, 44701. paragraph (g)(1)(i) or (g)(1)(ii) of this AD, as compliance time for accomplishment of the
applicable. actions specified by AWL No. 28–AWL–23 is
§ 39.13 [Amended] (i) For airplanes that have been previously specified in paragraph (g)(5)(i) or (g)(5)(ii) of
■ 2. The FAA amends § 39.13 by adding inspected as specified in 28–AWL–01 as of this AD, as applicable.
the effective date of this AD: Conduct the (i) For airplanes that have been previously
the following new airworthiness inspected as specified in 28–AWL–23 as of
inspection within 120 months after the most
directive (AD): recent inspection. the effective date of this AD: Conduct the
2018–19–21 The Boeing Company: (ii) For airplanes that have not been inspection within 72 months after the most
Amendment 39–19422; Docket No. inspected as specified in 28–AWL–01 as of recent inspection.
FAA–2017–1026; Product Identifier the effective date of this AD: Conduct the (ii) For airplanes that have not been
2017–NM–097–AD. inspection within 12 months after the inspected as specified in 28–AWL–23 as of
effective date of this AD. the effective date of this AD: Conduct the
(a) Effective Date inspection within 12 months after the
(2) AWL No. 28–AWL–18, AC Fuel Boost
This AD is effective November 1, 2018. Pump Bonding Installation, as specified in effective date of this AD.
(b) Affected ADs Boeing 707/720 Airworthiness Limitations (h) Additional Acceptable Wire Types and
(AWLs), D6–7552–AWL, dated October 2016. Sleeving
This AD affects the ADs specified in The initial compliance time for
paragraphs (b)(1) and (b)(2) of this AD. accomplishment of the actions specified by As an option, when accomplishing the
(1) AD 2008–04–11 R1, Amendment 39– AWL No. 28–AWL–18 is specified in actions required by paragraph (g) of this AD,
16147 (74 FR 68505, December 28, 2009) paragraph (g)(2)(i) or (g)(2)(ii) of this AD, as the changes specified in paragraphs (h)(1)
(‘‘AD 2008–04–11 R1’’). applicable. and (h)(2) of this AD are acceptable.
(2) AD 2013–24–07, Amendment 39–17681 (i) For airplanes that have been previously (1) Where AWL No. 28–AWL–03 identifies
(78 FR 72550, December 3, 2013) (‘‘AD 2013– inspected as specified in 28–AWL–18 as of wire types BMS 13–48, BMS 13–58, and BMS
24–07’’). the effective date of this AD: Conduct the 13–60, the following wire types are
inspection within 72 months after the most acceptable: MIL–W–22759/16, SAE
(c) Applicability AS22759/16 (M22759/16), MIL–W–22759/32,
recent inspection.
This AD applies to all The Boeing SAE AS22759/32 (M22759/32), MIL–W–
(ii) For airplanes that have not been
Company airplanes, certificated in any 22759/34, SAE AS22759/34 (M22759/34),
inspected as specified in 28–AWL–18 as of
category, identified in paragraphs (c)(1) and MIL–W–22759/41, SAE AS22759/41
the effective date of this AD: Conduct the
(c)(2) of this AD. (M22759/41), MIL–W–22759/86, SAE
inspection within 12 months after the
(1) Model 707–100 long body, –200, –100B AS22759/86 (M22759/86), MIL–W–22759/87,
effective date of this AD.
long body, –100B short body, –300, –300B, SAE AS22759/87 (M22759/87), MIL–W–
(3) AWL No. 28–AWL–19, Fuel Valve
–300C, and –400 series airplanes. 22759/92 and SAE AS22759/92 (M22759/92);
Bonding Jumper Installation—Engine Fuel
(2) Model 720 and 720B series airplanes. and MIL–C–27500 and NEMA WC 27500
Shutoff, Defuel, Reserve Tank Transfer, Fuel
cables constructed from these military or
(d) Subject Dump, and Fuel Manifold Valves, as SAE specification wire types identified
Air Transport Association (ATA) of specified in Boeing 707/720 Airworthiness above.
America Code 28, Fuel. Limitations (AWLs), D6–7552–AWL, dated (2) Where AWL No. 28–AWL–03 identifies
October 2016. The initial compliance time for TFE–2X Standard wall for wire sleeving, the
(e) Unsafe Condition accomplishment of the actions specified by following sleeving materials are acceptable:
This AD was prompted by fuel system AWL No. 28–AWL–19 is specified in Roundit 2000NX and Varglas Type HO, HP,
reviews conducted by the manufacturer. We paragraph (g)(3)(i) or (g)(3)(ii) of this AD, as or HM.
are issuing this AD to detect and correct applicable.
potential ignition sources inside fuel tanks (i) For airplanes that have been previously (i) No Alternative Actions and Intervals
caused by latent failures, alterations, repairs, inspected as specified in 28–AWL–19 as of Except as provided in paragraph (h) of this
or maintenance actions, which, in the effective date of this AD: Conduct the AD, after the maintenance or inspection
combination with flammable fuel vapors, inspection within 72 months after the most program has been revised as required by
could result in fuel tank explosions and recent inspection. paragraph (g) of this AD, no alternative
consequent loss of the airplane. (ii) For airplanes that have not been actions (e.g., inspections) or intervals may be
inspected as specified in 28–AWL–19 as of used unless the actions or intervals are
(f) Compliance the effective date of this AD: Conduct the approved as an alternative method of
Comply with this AD within the inspection within 12 months after the compliance (AMOC) in accordance with the
daltland on DSKBBV9HB2PROD with RULES
compliance times specified, unless already effective date of this AD. procedures specified in paragraph (k) of this
done. (4) AWL No. 28–AWL–21, Dry Bay Fuel AD.
Manifold Assembly—Bonding Jumper
(g) Revision of Maintenance or Inspection Installation, as specified in Boeing 707/720 (j) Terminating Action for Other ADs
Program Airworthiness Limitations (AWLs), D6– (1) Accomplishment of the actions required
Within 60 days after the effective date of 7552–AWL, dated October 2016. The initial by paragraph (g) of this AD terminates all
this AD, revise the maintenance or inspection compliance time for accomplishment of the requirements of AD 2008–04–11 R1.
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![Federal Register / Vol. 83, No. 188 / Thursday, September 27, 2018 / Rules and Regulations 48711
(2) Accomplishment of the actions required the availability of this material at NARA, call SUPPLEMENTARY INFORMATION:
by paragraph (g) of this AD terminates the 202–741–6030, or go to: http://
requirements of paragraph (h) of AD 2013– www.archives.gov/federal-register/cfr/ibr- I. Background
24–07. locations.html. The Federal Food, Drug, and Cosmetic
(k) Alternative Methods of Compliance Issued in Des Moines, Washington, on Act (FD&C Act), as amended, establishes
(AMOCs) September 10, 2018. a comprehensive system for the
(1) The Manager, Los Angeles ACO Branch, Michael Kaszycki, regulation of medical devices intended
FAA, has the authority to approve AMOCs Acting Director, System Oversight Division, for human use. Section 513 of the FD&C
for this AD, if requested using the procedures Aircraft Certification Service. Act (21 U.S.C. 360c) established three
found in 14 CFR 39.19. In accordance with [FR Doc. 2018–20631 Filed 9–26–18; 8:45 am] categories (classes) of devices, reflecting
14 CFR 39.19, send your request to your the regulatory controls needed to
BILLING CODE 4910–13–P
principal inspector or local Flight Standards provide reasonable assurance of their
District Office, as appropriate. If sending
safety and effectiveness. The three
information directly to the manager of the
certification office, send it to the attention of DEPARTMENT OF HEALTH AND categories of devices are class I (general
the person identified in paragraph (l) of this HUMAN SERVICES controls), class II (special controls), and
AD. Information may be emailed to: 9-AWP- class III (premarket approval).
LAACO-ADS@faa.gov. Food and Drug Administration Devices that were not in commercial
(2) Before using any approved AMOC, distribution prior to May 28, 1976
notify your appropriate principal inspector, 21 CFR Part 884 (generally referred to as
or lacking a principal inspector, the manager postamendments devices) are
of the local flight standards district office/ [Docket No. FDA–2017–N–6538] automatically classified by section
certificate holding district office. 513(f)(1) of the FD&C Act into class III
(3) An AMOC that provides an acceptable Obstetrical and Gynecological
level of safety may be used for any repair, Devices; Reclassification of Single-Use without any FDA rulemaking process.
modification, or alteration required by this Female Condom, To Be Renamed Those devices remain in class III and
AD if it is approved by the Boeing Single-Use Internal Condom require premarket approval unless, and
Commercial Airplanes Organization until, the device is reclassified into class
Designation Authorization (ODA) that has AGENCY: Food and Drug Administration, I or II, or FDA issues an order finding
been authorized by the Manager, Los Angeles HHS. the device to be substantially
ACO Branch, to make those findings. To be ACTION: Final order. equivalent, in accordance with section
approved, the repair method, modification 513(i) of the FD&C Act, to a predicate
deviation, or alteration deviation must meet The Food and Drug
SUMMARY: device that does not require premarket
the certification basis of the airplane, and theAdministration (FDA or the Agency) is
approval must specifically refer to this AD.
approval. The Agency determines
issuing a final order to reclassify single- whether new devices are substantially
(l) Related Information use female condoms, renaming the equivalent to predicate devices by
For more information about this AD, device to ‘‘single-use internal condom,’’ means of premarket notification
contact Samuel Lee, Aerospace Engineer, a postamendments class III device procedures in section 510(k) of the
Propulsion Section, FAA, Los Angeles ACO (regulated under product code MBU), FD&C Act (21 U.S.C. 360(k)) and 21 CFR
Branch, 3960 Paramount Boulevard, into class II (special controls) subject to part 807.
Lakewood, CA 90712–4137; phone: 562–627– premarket notification (510(k)). FDA is A postamendments device that has
5262; fax: 562–627–5210; email: samuel.lee@ also identifying the special controls that been initially classified in class III
faa.gov. the Agency believes are necessary to under section 513(f)(1) of the FD&C Act
(m) Material Incorporated by Reference provide a reasonable assurance of safety may be reclassified into class I or class
(1) The Director of the Federal Register and effectiveness of the device. FDA is II under section 513(f)(3) of the FD&C
approved the incorporation by reference finalizing this reclassification on its Act. Section 513(f)(3) of the FD&C Act
(IBR) of the service information listed in this own initiative based on new provides that FDA acting by order can
paragraph under 5 U.S.C. 552(a) and 1 CFR information. FDA is also amending the reclassify the device into class I or class
part 51. existing device identification for II on its own initiative, or in response
(2) You must use this service information ‘‘female condom,’’ a preamendments
as applicable to do the actions required by
to a petition from the manufacturer or
class III device (product code OBY), by importer of the device. To change the
this AD, unless the AD specifies otherwise.
renaming the device ‘‘multiple-use classification of the device, the
(i) Boeing 707/720 Airworthiness
Limitations (AWLs), D6–7552–AWL, dated female condom,’’ to distinguish it from proposed new class must have sufficient
October 2016. (Subsection A.2 of this the ‘‘single-use internal condom.’’ This regulatory controls to provide
document includes pages 33 and 34, which order reclassifies single-use internal reasonable assurance of the safety and
are not identified in the Table of Contents.) condoms from class III to class II and effectiveness of the device for its
(ii) Reserved. reduces regulatory burden because these intended use.
(3) For service information identified in types of devices will no longer be Reevaluation of the data previously
this AD, contact Boeing Commercial required to submit a premarket approval
Airplanes, Attention: Contractual & Data
before the Agency is an appropriate
application (PMA), but can instead basis for subsequent action where the
Services (C&DS), 2600 Westminster Blvd.,
MC 110–SK57, Seal Beach, CA 90740–5600;
submit a less burdensome 510(k) before reevaluation is made in light of newly
telephone: 562–797–1717; internet: https:// marketing their device. available regulatory authority (see Bell
www.myboeingfleet.com. DATES: This order is effective October v. Goddard, 366 F.2d 177, 181 (7th Cir.
(4) You may view this service information 29, 2018. 1966); Ethicon, Inc. v. FDA, 762 F.
at the FAA, Transport Standards Branch, FOR FURTHER INFORMATION CONTACT: Supp. 382, 388–391 (D.D.C. 1991)), or in
daltland on DSKBBV9HB2PROD with RULES
2200 South 216th St., Des Moines, WA. For Monica Garcia, Center for Devices and light of changes in ‘‘medical science’’
information on the availability of this
material at the FAA, call 206–231–3195.
Radiological Health, Food and Drug (Upjohn Co. v. Finch, 422 F.2d 944, 951
(5) You may view this service information Administration, 10903 New Hampshire (6th Cir. 1970)). Whether data before the
that is incorporated by reference at the Ave., Bldg. 66, Rm. G215, Silver Spring, Agency are old or new, the ‘‘new
National Archives and Records MD 20993, 240–402–2791, information’’ to support reclassification
Administration (NARA). For information on monica.garcia@fda.hhs.gov. under section 513(f)(3) must be ‘‘valid
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Document Created: 2018-09-27 01:04:12
Document Modified: 2018-09-27 01:04:12
| 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 November 1, 2018. | |
| Contact | Samuel Lee, Aerospace Engineer, Propulsion Section, FAA, Los Angeles ACO Branch, 3960 Paramount Boulevard, Lakewood, CA 90712-4137; phone: 562-627-5262; fax: 562-627- 5210; email: [email protected] | |
| FR Citation | 83 FR 48708 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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