81 FR 69666 - Airworthiness Directives; The Boeing Company Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 81, Issue 195 (October 7, 2016)
Federal Aviation Administration
Federal Register Volume 81, Issue 195 (October 7, 2016)
| Page Range | 69666-69668 | |
| FR Document | 2016-22707 |
[Federal Register Volume 81, Number 195 (Friday, October 7, 2016)] [Rules and Regulations] [Pages 69666-69668] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2016-22707] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2016-3986; Directorate Identifier 2015-NM-147-AD; Amendment 39-18661; AD 2016-19-12] 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 certain The Boeing Company Model 747-400, 747-400D, and 747-400F series airplanes. This AD was prompted by a determination that a certain fastener type in the fuel tank walls has insufficient bond to the structure, and an electrical wiring short could cause arcing to occur at the ends of fasteners in the fuel tanks. This AD requires the installation of new clamps and polytetrafluoroethylene (TFE) sleeves on the wire bundles of the front spars and rear spars of the wings. This AD also requires inspecting the existing TFE sleeves under the wire bundle clamps for correct installation, and replacement if necessary. We are issuing this AD to prevent potential ignition sources in the fuel tank in the event of a lightning strike or high-powered short circuit, and consequent fire or explosion. DATES: This AD is effective November 14, 2016. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of November 14, 2016. ADDRESSES: For service information identified in this final rule, contact Boeing Commercial Airplanes, Attention: Data & Services Management, P.O. Box 3707, MC 2H-65, Seattle, WA 98124-2207; telephone: 206-544-5000, extension 1; fax: 206-766-5680; 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-2016- 3986. Examining the AD Docket You may examine the AD docket on the Internet at http:// [[Page 69667]] www.regulations.gov by searching for and locating Docket No. FAA-2016- 3986; 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: Tung Tran, Aerospace Engineer, Propulsion Branch, ANM-140S, FAA, Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue SW., Renton, WA 98057-3356; phone: 425-917- 6505; fax: 425-917-6590; email: Tung.Tran@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 certain The Boeing Company Model 747-400, 747-400D, and 747-400F series airplanes. The NPRM published in the Federal Register on March 1, 2016 (81 FR 10537) (``the NPRM''). The NPRM was prompted by a determination that a certain fastener type in the fuel tank walls has insufficient bond to the structure, and an electrical wiring short could cause arcing to occur at the ends of fasteners in the fuel tanks. The NPRM proposed to require the installation of new clamps and TFE sleeves on the wire bundles of the front spars and rear spars of the wings. The NPRM also proposed to require inspecting the existing TFE sleeves under the wire bundle clamps for correct installation, and replacement if necessary. We are issuing this AD to prevent potential ignition sources in the fuel tank in the event of a lightning strike or high-powered short circuit, and consequent fire or explosion. Comments We gave the public the opportunity to participate in developing this AD. The following presents the comments received on the NPRM and the FAA's response to each comment. Support for the NPRM Boeing supported the content of the NPRM. United Airlines had no objection to the NPRM. Conclusion We reviewed the relevant data, considered the comments received, and determined that air safety and the public interest require adopting this AD 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 correcting 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 Special Attention Service Bulletin 747-28-2324, Revision 1, dated July 27, 2015. The service information describes procedures for installing new clamps and TFE sleeves on the wire bundles of the front spars and rear spars of the wings. The service information also describes procedures for inspecting TFE sleeves under the wire bundle clamps that were installed using the procedures specified in Boeing Special Attention Service Bulletin 747-28-2324, dated November 3, 2014, for correct installation, and replacing them if necessary. 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 135 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 ---------------------------------------------------------------------------------------------------------------- Installation of wire bundle Up to 7 work-hours x $85 $138 Up to $733......... Up to $98,955. clamps. per hour = $595. Inspection...................... Up to 5 work-hours x $85 0 Up to $425......... Up to $57,375. per hour = $425. ---------------------------------------------------------------------------------------------------------------- We have received no definitive data that enables us to provide cost estimates for the on-condition actions specified in this AD. Authority for This Rulemaking Title 49 of the United States Code specifies the FAA's authority to issue rules on aviation safety. Subtitle I, section 106, describes the authority of the FAA Administrator. Subtitle VII: Aviation Programs, describes in more detail the scope of the Agency's authority. We are issuing this rulemaking under the authority described in Subtitle VII, Part A, Subpart III, Section 44701: ``General requirements.'' Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. Regulatory Findings 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, [[Page 69668]] 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): 2016-19-12 The Boeing Company: Amendment 39-18661; Docket No. FAA- 2016-3986; Directorate Identifier 2015-NM-147-AD. (a) Effective Date This AD is effective November 14, 2016. (b) Affected ADs None. (c) Applicability This AD applies to The Boeing Company Model 747-400, 747-400D, and 747-400F series airplanes, certificated in any category, as identified in Boeing Special Attention Service Bulletin 747-28-2324, Revision 1, dated July 27, 2015. (d) Subject Air Transport Association (ATA) of America Code 28, Fuel. (e) Unsafe Condition This AD was prompted by a determination that a certain fastener type in the fuel tank walls has insufficient bond to the structure, and an electrical wiring short could cause arcing to occur at the ends of fasteners in the fuel tanks. We are issuing this AD to prevent potential ignition sources in the fuel tank in the event of a lightning strike or high-powered short circuit, and consequent fire or explosion. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Installation/Inspection Within 60 months after the effective date of this AD, do the actions specified in paragraph (g)(1) or (g)(2) of this AD, as applicable. (1) For airplanes on which the modification specified in Boeing Special Attention Service Bulletin 747-28-2324, dated November 3, 2014, has not been done as of the effective date of this AD: Install new clamps and polytetrafluoroethylene (TFE) sleeves on the wire bundles of the front spars and rear spars of the wings, in accordance with the Accomplishment Instructions of Boeing Special Attention Service Bulletin 747-28-2324, Revision 1, dated July 27, 2015. (2) For airplanes on which the modification specified in Boeing Special Attention Service Bulletin 747-28-2324, dated November 3, 2014, has been done as of the effective date of this AD: Do a detailed inspection of the TFE sleeves under the wire bundle clamps for correct installation, and replace the sleeves if not correctly installed, in accordance with the Accomplishment Instructions of Boeing Special Attention Service Bulletin 747-28-2324, Revision 1, dated July 27, 2015. (h) 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 (i) of this AD. Information may be emailed to: 9-ANM-Seattle-ACO-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, alteration, or modification 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. For a repair method 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. (i) Related Information For more information about this AD, contact Tung Tran, Aerospace Engineer, Propulsion Branch, ANM-140S, FAA, Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue SW., Renton, WA 98057- 3356; phone: 425-917-6505; fax: 425-917-6590; email: Tung.Tran@faa.gov. (j) 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 Special Attention Service Bulletin 747-28-2324, Revision 1, dated July 27, 2015. (ii) Reserved. (3) For service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Data & Services Management, P. O. Box 3707, MC 2H-65, Seattle, WA 98124-2207; telephone: 206- 544-5000, extension 1; fax: 206-766-5680; Internet: https://www.myboeingfleet.com. (4) 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. (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 Renton, Washington, on September 13, 2016. Michael Kaszycki, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2016-22707 Filed 10-6-16; 8:45 am] BILLING CODE 4910-13-P
![69666 Federal Register / Vol. 81, No. 195 / Friday, October 7, 2016 / Rules and Regulations
Lithium battery installations on the i. The ICAW must contain DEPARTMENT OF TRANSPORTATION
Model A36 airplanes must be designed recommended manufacturer’s
and installed as follows: maintenance and inspection Federal Aviation Administration
a. Safe cell temperatures and requirements to ensure that batteries,
pressures must be maintained during including single cells, meet a 14 CFR Part 39
any probable charging or discharging functionally safe level essential to the [Docket No. FAA–2016–3986; Directorate
condition, or during any failure of the aircraft’s continued airworthiness. Identifier 2015–NM–147–AD; Amendment
charging or battery monitoring system (1) The ICAW must contain operating 39–18661; AD 2016–19–12]
not shown to be extremely remote. The instructions and equipment limitations RIN 2120–AA64
lithium battery installation must be in an installation maintenance manual.
designed to preclude explosion or fire in Airworthiness Directives; The Boeing
the event of those failures. (2) The ICAW must contain
installation procedures and limitations Company Airplanes
b. Lithium batteries must be designed
to preclude the occurrence of self- in a maintenance manual, sufficient to AGENCY: Federal Aviation
sustaining, uncontrolled increases in ensure that cells or batteries, when Administration (FAA), DOT.
temperature or pressure. installed according to the installation ACTION: Final rule.
c. No explosive or toxic gasses procedures, still meet safety functional
levels essential to the aircraft’s SUMMARY: We are adopting a new
emitted by any lithium battery in
continued airworthiness. The airworthiness directive (AD) for certain
normal operation or as the result of any
limitations must identify any unique The Boeing Company Model 747–400,
failure of the battery charging or 747–400D, and 747–400F series
monitoring system, or battery aspects of the installation.
airplanes. This AD was prompted by a
installation not shown to be extremely (3) The ICAW must contain corrective
determination that a certain fastener
remote, may accumulate in hazardous maintenance procedures to check
type in the fuel tank walls has
quantities within the airplane. battery capacity at manufacturer’s
insufficient bond to the structure, and
d. Lithium batteries that contain recommended inspection intervals.
an electrical wiring short could cause
flammable fluids must comply with the (4) The ICAW must contain scheduled arcing to occur at the ends of fasteners
flammable fluid fire protection servicing information to replace in the fuel tanks. This AD requires the
requirements of 14 CFR 23.863(a) batteries at manufacturer’s installation of new clamps and
through (d). recommended replacement time. polytetrafluoroethylene (TFE) sleeves on
e. No corrosive fluids or gases that the wire bundles of the front spars and
(5) The ICAW must contain
may escape from any lithium battery rear spars of the wings. This AD also
maintenance and inspection
may damage airplane structure or requires inspecting the existing TFE
requirements how to check visually for
essential equipment. sleeves under the wire bundle clamps
battery and charger degradation.
f. Each lithium battery installation for correct installation, and replacement
must have provisions to prevent any j. Batteries in a rotating stock (spares) if necessary. We are issuing this AD to
hazardous effect on structure or that have degraded charge retention prevent potential ignition sources in the
essential systems that may be caused by capability or other damage due to fuel tank in the event of a lightning
the maximum amount of heat the prolonged storage must be checked at strike or high-powered short circuit, and
battery can generate during a short manufacturer’s recommended consequent fire or explosion.
circuit of the battery or of its individual inspection intervals.
DATES: This AD is effective November
cells. k. If the lithium battery application 14, 2016.
g. Lithium battery installations must contains software and/or complex The Director of the Federal Register
have— hardware, in accordance with AC 20– approved the incorporation by reference
(1) A system to control the charging 115 5 and AC 20–152,6 they should be of a certain publication listed in this AD
rate of the battery automatically to developed to the standards of DO–178 as of November 14, 2016.
prevent battery overheating or for software and DO–254 for complex ADDRESSES: For service information
overcharging, or hardware. identified in this final rule, contact
(2) A battery temperature sensing and Compliance with the requirements of Boeing Commercial Airplanes,
over-temperature warning system with a this Special Condition must be shown Attention: Data & Services Management,
means for automatically disconnecting by test or analysis, with the concurrence P.O. Box 3707, MC 2H–65, Seattle, WA
the battery from its charging source in of the New York Aircraft Certification 98124–2207; telephone: 206–544–5000,
the event of an over-temperature Office. extension 1; fax: 206–766–5680;
condition or, Internet: https://
(3) A battery failure sensing and Issued in Kansas City, Missouri on
www.myboeingfleet.com. You may view
warning system with a means for September 28, 2016.
this referenced service information at
automatically disconnecting the battery William Schinstock, the FAA, Transport Airplane
from its charging source in the event of Acting Manager, Small Airplane Directorate, Directorate, 1601 Lind Avenue SW.,
battery failure. Aircraft Certification Service. Renton, WA. For information on the
h. Any lithium battery installation [FR Doc. 2016–24343 Filed 10–6–16; 8:45 am] availability of this material at the FAA,
functionally required for safe operation BILLING CODE 4910–13–P call 425–227–1221. It is also available
of the airplane, must incorporate a on the Internet at http://
mstockstill on DSK3G9T082PROD with RULES
monitoring and warning feature that 5 http://rgl.faa.gov/Regulatory_and_Guidance_ www.regulations.gov by searching for
will provide an indication to the Library/rgAdvisoryCircular.nsf/0/E35FBC0060 and locating Docket No. FAA–2016–
appropriate flight crewmembers, E2159186257BBE00719FB3?OpenDocument& 3986.
whenever the capacity and state of Highlight=ac%2020–115b.
charge of the batteries have fallen below
6 http://rgl.faa.gov/Regulatory_and_Guidance_
Examining the AD Docket
Library/rgAdvisoryCircular.nsf/0/6D4AE0BF
levels considered acceptable for 1BDE3579862570360055D119?Open You may examine the AD docket on
dispatch of the airplane. Document&Highlight=ac%2020–152. the Internet at http://
VerDate Sep<11>2014 18:29 Oct 06, 2016 Jkt 241001 PO 00000 Frm 00008 Fmt 4700 Sfmt 4700 E:\FR\FM\07OCR1.SGM 07OCR1](https://thefederalregister.org/doc/81_FR_69861/page/1.svg)
![69668 Federal Register / Vol. 81, No. 195 / Friday, October 7, 2016 / Rules and Regulations
the FAA amends 14 CFR part 39 as of the effective date of this AD: Do a detailed (5) You may view this service information
follows: inspection of the TFE sleeves under the wire that is incorporated by reference at the
bundle clamps for correct installation, and National Archives and Records
PART 39—AIRWORTHINESS replace the sleeves if not correctly installed, Administration (NARA). For information on
DIRECTIVES in accordance with the Accomplishment the availability of this material at NARA, call
Instructions of Boeing Special Attention 202–741–6030, or go to: http://
■ 1. The authority citation for part 39 Service Bulletin 747–28–2324, Revision 1, www.archives.gov/federal-register/cfr/ibr-
dated July 27, 2015. locations.html.
continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701. (h) Alternative Methods of Compliance
Issued in Renton, Washington, on
(AMOCs)
September 13, 2016.
§ 39.13 [Amended] (1) The Manager, Seattle Aircraft Michael Kaszycki,
■ 2. The FAA amends § 39.13 by adding Certification Office (ACO), FAA, has the
authority to approve AMOCs for this AD, if Acting Manager, Transport Airplane
the following new airworthiness Directorate, Aircraft Certification Service.
requested using the procedures found in 14
directive (AD): CFR 39.19. In accordance with 14 CFR 39.19, [FR Doc. 2016–22707 Filed 10–6–16; 8:45 am]
2016–19–12 The Boeing Company: send your request to your principal inspector BILLING CODE 4910–13–P
Amendment 39–18661; Docket No. or local Flight Standards District Office, as
FAA–2016–3986; Directorate Identifier appropriate. If sending information directly
2015–NM–147–AD. to the manager of the ACO, send it to the
attention of the person identified in DEPARTMENT OF HEALTH AND
(a) Effective Date paragraph (i) of this AD. Information may be HUMAN SERVICES
This AD is effective November 14, 2016. emailed to: 9-ANM-Seattle-ACO-AMOC-
Requests@faa.gov. Food and Drug Administration
(b) Affected ADs
(2) Before using any approved AMOC,
None. notify your appropriate principal inspector, 21 CFR Part 216
(c) Applicability or lacking a principal inspector, the manager
of the local flight standards district office/ [Docket No. FDA–1999–N–0194 (Formerly
This AD applies to The Boeing Company certificate holding district office. 99N–4490)]
Model 747–400, 747–400D, and 747–400F (3) An AMOC that provides an acceptable RIN 0910–AH08
series airplanes, certificated in any category, level of safety may be used for any repair,
as identified in Boeing Special Attention alteration, or modification required by this
Service Bulletin 747–28–2324, Revision 1,
Additions and Modifications to the List
AD if it is approved by the Boeing of Drug Products That Have Been
dated July 27, 2015. Commercial Airplanes Organization
Designation Authorization (ODA) that has
Withdrawn or Removed From the
(d) Subject Market for Reasons of Safety or
been authorized by the Manager, Seattle
Air Transport Association (ATA) of ACO, to make those findings. For a repair Effectiveness
America Code 28, Fuel. method to be approved, the repair method,
modification deviation, or alteration
AGENCY: Food and Drug Administration,
(e) Unsafe Condition HHS.
deviation must meet the certification basis of
This AD was prompted by a determination the airplane, and the approval must ACTION: Final rule.
that a certain fastener type in the fuel tank specifically refer to this AD.
walls has insufficient bond to the structure, SUMMARY: The Food and Drug
and an electrical wiring short could cause (i) Related Information Administration (FDA or the Agency) is
arcing to occur at the ends of fasteners in the For more information about this AD, amending its regulations to revise the
fuel tanks. We are issuing this AD to prevent contact Tung Tran, Aerospace Engineer, list of drug products that have been
potential ignition sources in the fuel tank in Propulsion Branch, ANM–140S, FAA, Seattle
the event of a lightning strike or high- withdrawn or removed from the market
Aircraft Certification Office (ACO), 1601 Lind
powered short circuit, and consequent fire or Avenue SW., Renton, WA 98057–3356;
because the drug products or
explosion. phone: 425–917–6505; fax: 425–917–6590; components of such drug products have
email: Tung.Tran@faa.gov. been found to be unsafe or not effective.
(f) Compliance
Drugs appearing on this list may not be
Comply with this AD within the (j) Material Incorporated by Reference compounded under the exemptions
compliance times specified, unless already (1) The Director of the Federal Register provided by sections 503A and 503B of
done. approved the incorporation by reference the Federal Food, Drug, and Cosmetic
(IBR) of the service information listed in this
(g) Installation/Inspection Act (the FD&C Act). Specifically, the
paragraph under 5 U.S.C. 552(a) and 1 CFR
Within 60 months after the effective date part 51. rule adds 24 entries to this list of drug
of this AD, do the actions specified in (2) You must use this service information products, modifies the description of
paragraph (g)(1) or (g)(2) of this AD, as as applicable to do the actions required by one entry on this list, and revises the
applicable. this AD, unless the AD specifies otherwise. list’s title and introductory language.
(1) For airplanes on which the (i) Boeing Special Attention Service These revisions are necessary because
modification specified in Boeing Special Bulletin 747–28–2324, Revision 1, dated July information has come to the Agency’s
Attention Service Bulletin 747–28–2324, 27, 2015. attention since March 8, 1999, when
dated November 3, 2014, has not been done (ii) Reserved.
as of the effective date of this AD: Install new FDA published the original list as a final
(3) For service information identified in
clamps and polytetrafluoroethylene (TFE) this AD, contact Boeing Commercial rule.
sleeves on the wire bundles of the front spars Airplanes, Attention: Data & Services DATES: This rule is effective November
and rear spars of the wings, in accordance Management, P. O. Box 3707, MC 2H–65, 7, 2016.
mstockstill on DSK3G9T082PROD with RULES
with the Accomplishment Instructions of Seattle, WA 98124–2207; telephone: 206– FOR FURTHER INFORMATION CONTACT:
Boeing Special Attention Service Bulletin 544–5000, extension 1; fax: 206–766–5680; Edisa Gozun, Center for Drug Evaluation
747–28–2324, Revision 1, dated July 27, Internet: https://www.myboeingfleet.com.
2015. (4) You may view this referenced service
and Research (HFD–310), Food and
(2) For airplanes on which the information at the FAA, Transport Airplane Drug Administration, 10903 New
modification specified in Boeing Special Directorate, 1601 Lind Avenue SW., Renton, Hampshire Ave., Bldg. 51, Rm. 5199,
Attention Service Bulletin 747–28–2324, WA. For information on the availability of Silver Spring, MD 20993–0002, 301–
dated November 3, 2014, has been done as this material at the FAA, call 425–227–1221. 796–3110.
VerDate Sep<11>2014 18:29 Oct 06, 2016 Jkt 241001 PO 00000 Frm 00010 Fmt 4700 Sfmt 4700 E:\FR\FM\07OCR1.SGM 07OCR1](https://thefederalregister.org/doc/81_FR_69861/page/3.svg)
Document Created: 2018-02-13 16:32:07
Document Modified: 2018-02-13 16:32:07
| 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 14, 2016. | |
| Contact | Tung Tran, Aerospace Engineer, Propulsion Branch, ANM-140S, FAA, Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue SW., Renton, WA 98057-3356; phone: 425-917- 6505; fax: 425-917-6590; email: [email protected] | |
| FR Citation | 81 FR 69666 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
2025 Federal Register | Disclaimer | Privacy Policy
USC | CFR | eCFR