81 FR 94956 - Airworthiness Directives; The Boeing Company Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 81, Issue 248 (December 27, 2016)
Federal Aviation Administration
Federal Register Volume 81, Issue 248 (December 27, 2016)
| Page Range | 94956-94958 | |
| FR Document | 2016-30278 |
[Federal Register Volume 81, Number 248 (Tuesday, December 27, 2016)] [Rules and Regulations] [Pages 94956-94958] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2016-30278] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2016-8850; Directorate Identifier 2016-NM-031-AD; Amendment 39-18755; AD 2016-25-29] 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 767-200 and -300 series airplanes. This AD was prompted by a report of a fire in the bilge area of the cargo compartment that burned through the insulation blankets that were intended to prevent smoke from migrating behind the cargo compartment sidewall liners and upward into the main cabin. This AD requires replacing the cargo compartment insulation blankets on the left and right sides with new insulation blankets that incorporate fire stops. We are issuing this AD to address the unsafe condition on these products. DATES: This AD is effective January 31, 2017. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of January 31, 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-2016- 8850. Examining the AD Docket You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016- 8850; 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, [[Page 94957]] Cabin Safety & Environmental Control Systems, ANM-150S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue SW., Renton, WA 98057- 3356; phone: 425-917-6596; fax: 425-917-6590; email: [email protected]. SUPPLEMENTARY INFORMATION: Discussion We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to certain The Boeing Company Model 767-200 and -300 series airplanes. The NPRM published in the Federal Register on August 30, 2016 (81 FR 59549) (``the NPRM''). The NPRM was prompted by a report of a fire in the bilge area of the cargo compartment that burned through the insulation blankets that were intended to prevent smoke from migrating behind the cargo compartment sidewall liners and upward into the main cabin. The NPRM proposed to require replacing the cargo compartment insulation blankets on the left and right sides with new insulation blankets that incorporate fire stops. We are issuing this AD to prevent a fire in the bilge area of the cargo compartment burning through the insulation blankets and consequently allowing smoke to migrate behind the cargo compartment sidewall liners and upward into the main cabin. 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 and United Airlines expressed support for the NPRM. Effect of Winglets on Accomplishment of the Proposed Actions Aviation Partners Boeing stated that the installation of winglets per Supplemental Type Certificate (STC) ST01920SE does not affect the accomplishment of the manufacturer's service instructions. We agree with the commenter that STC ST01920SE does not affect the accomplishment of the manufacturer's service instructions. Therefore, the installation of STC ST01920SE does not affect the ability to accomplish the actions required by this AD. We have not changed this AD in this regard. 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. We also determined that these changes will not increase the economic burden on any operator or increase the scope of this AD. Related Service Information Under 1 CFR part 51 We reviewed Boeing Special Attention Service Bulletin 767-25-0550, dated January 30, 2015. The service information describes procedures for replacing the cargo compartment insulation blankets on the left and right sides between stringers 29 and 33 with new insulation blankets that incorporate fire stops. 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 26 airplanes of U.S. registry. We estimate the following costs to comply with this AD: Estimated Costs ---------------------------------------------------------------------------------------------------------------- Action Labor cost Parts cost Cost per product Cost on U.S. operators ---------------------------------------------------------------------------------------------------------------- Replacement.............. Up to 54 work- (\1\) Up to $4,590............. Up to $119,340. hours x $85 per hour = $4,590. ---------------------------------------------------------------------------------------------------------------- \1\ We have received no definitive data that will enable us to provide parts cost estimates for the actions specified in this AD. According to the manufacturer, some of the costs of this AD may be covered under warranty, thereby reducing the cost impact on affected individuals. We do not control warranty coverage for affected individuals. As a result, we have included all available costs in our cost estimate. Authority for This Rulemaking Title 49 of the United States Code specifies the FAA's authority to issue rules on aviation safety. Subtitle I, section 106, describes the authority of the FAA Administrator. Subtitle VII: Aviation Programs, describes in more detail the scope of the Agency's authority. We are issuing this rulemaking under the authority described in Subtitle VII, Part A, Subpart III, Section 44701: ``General requirements.'' Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on 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, the FAA amends 14 CFR part 39 as follows: [[Page 94958]] 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): 2016-25-29 The Boeing Company: Amendment 39-18755; Docket No. FAA- 2016-8850; Directorate Identifier 2016-NM-031-AD. (a) Effective Date This AD is effective January 31, 2017. (b) Affected ADs None. (c) Applicability This AD applies to The Boeing Company Model 767-200 and -300 series airplanes, certificated in any category, as identified in Boeing Special Attention Service Bulletin 767-25-0550, dated January 30, 2015. (d) Subject Air Transport Association (ATA) of America Code 25; Equipment/ furnishings. (e) Unsafe Condition This AD was prompted by a report of a fire in the bilge area of the cargo compartment that burned through the insulation blankets that were intended to prevent smoke from migrating behind the cargo compartment sidewall liners and upward into the main cabin. We are issuing this AD to prevent a fire in the bilge area of the cargo compartment burning through the insulation blankets and consequently allowing smoke to migrate behind the cargo compartment sidewall liners and upward into the main cabin. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Insulation Blanket Replacement Within 36 months after the effective date of this AD: Replace the cargo compartment insulation blankets on the left and right sides between stringers 29 and 33 with new insulation blankets that incorporate fire stops, in accordance with the Accomplishment Instructions of Boeing Special Attention Service Bulletin 767-25- 0550, dated January 30, 2015. For Groups 1 through 4, Configurations 1 and 2, airplanes identified in Boeing Special Attention Service Bulletin 767-25-0550, dated January 30, 2015, no action is required by this AD. (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: [email protected]. (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. (4) For service information that contains steps that are labeled as Required for Compliance (RC), the provisions of paragraphs (h)(4)(i) and (h)(4)(ii) of this AD apply. (i) The steps labeled as RC, including substeps under an RC step and any figures identified in an RC step, must be done to comply with the AD. An AMOC is required for any deviations to RC steps, including substeps and identified figures. (ii) Steps not labeled as RC may be deviated from using accepted methods in accordance with the operator's maintenance or inspection program without obtaining approval of an AMOC, provided the RC steps, including substeps and identified figures, can still be done as specified, and the airplane can be put back in an airworthy condition. (i) Related Information For more information about this AD, contact Francis Smith, Aerospace Engineer, Cabin Safety & Environmental Control Systems, ANM-150S, FAA, Seattle ACO, 1601 Lind Avenue SW., Renton, WA 98057- 3356; phone: 425-917-6596; fax: 425-917-6590; email: [email protected]. (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 767-25-0550, dated January 30, 2015. (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 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 December 9, 2016. Dionne Palermo, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2016-30278 Filed 12-23-16; 8:45 am] BILLING CODE 4910-13-P
![94956 Federal Register / Vol. 81, No. 248 / Tuesday, December 27, 2016 / Rules and Regulations
(b) Unsafe Condition (d) Compliance gearbox, whichever comes first; and
This AD defines the unsafe condition as a You are responsible for performing each thereafter at intervals not to exceed the
action required by this AD within the compliance times shown in Table 1 to
crack in a bi-directional cross-bar, which
specified compliance time unless it has paragraph (e) of this AD, inspect each cross-
could result in failure of a cross-bar and loss bar for a crack. For purposes of this AD, a
already been accomplished prior to that time.
of control of the helicopter. torque cycle is defined as one landing with
(e) Required Actions or without stopping the rotor or one external
(c) Effective Date
(1) Within the initial inspection times load-carrying operation; an external load-
This AD becomes effective January 31, shown in Table 1 to paragraph (e) of this AD carrying operation occurs each time a
2017. or the next time maintenance of the helicopter picks up an external load and
helicopter involves removing the main drops it off.
TABLE 1 TO PARAGRAPH (e)
Helicopter model Initial and recurrent inspection interval
AS350B, AS350BA, AS350B1, AS350B2, AS350C, AS350D, and 4,500 hours time-in-service (TIS) or 60,000 torque cycles, whichever
AS350D1. occurs first.
AS350B3, AS355E, AS355F, AS355F1, AS355F2, AS355N, and 3,300 hours TIS or 60,000 torque cycles, whichever occurs first.
AS355 NP.
EC130B4 ..................................................................................................
EC130T2 ................................................................................................... 3,300 hours TIS or 40,000 torque cycles, whichever occurs first.
(2) If there is a crack, before further flight, (i) Subject DATES: This AD is effective January 31,
replace the cross-bar. Joint Aircraft Service Component (JASC) 2017.
(f) Special Flight Permits Code: 6300, Main Rotor Drive System. The Director of the Federal Register
Issued in Fort Worth, Texas, on December approved the incorporation by reference
Special flight permits are prohibited.
6, 2016. of a certain publication listed in this AD
(g) Alternative Methods of Compliance Scott A. Horn, as of January 31, 2017.
(AMOCs) ADDRESSES: For service information
Acting Manager, Rotorcraft Directorate,
(1) The Manager, Safety Management Aircraft Certification Service. identified in this final rule, contact
Group, FAA, may approve AMOCs for this Boeing Commercial Airplanes,
[FR Doc. 2016–30048 Filed 12–23–16; 8:45 am]
AD. Send your proposal to: Robert Grant, Attention: Contractual & Data Services
BILLING CODE 4910–13–P
Aviation Safety Engineer, Safety Management (C&DS), 2600 Westminster Blvd., MC
Group, FAA, 10101 Hillwood Pkwy, Fort 110–SK57, Seal Beach, CA 90740–5600;
Worth, TX 76177; telephone (817) 222–5110; telephone 562–797–1717; Internet
email 9-ASW-FTW-AMOC-Requests@faa.gov. DEPARTMENT OF TRANSPORTATION
https://www.myboeingfleet.com. You
(2) For operations conducted under a 14
CFR part 119 operating certificate or under Federal Aviation Administration may view this referenced service
14 CFR part 91, subpart K, we suggest that information at the FAA, Transport
you notify your principal inspector, or 14 CFR Part 39 Airplane Directorate, 1601 Lind Avenue
lacking a principal inspector, the manager of SW., Renton, WA. For information on
[Docket No. FAA–2016–8850; Directorate
the local flight standards district office or Identifier 2016–NM–031–AD; Amendment
the availability of this material at the
certificate holding district office, before 39–18755; AD 2016–25–29] FAA, call 425–227–1221. It is also
operating any aircraft complying with this available on the Internet at http://
AD through an AMOC. RIN 2120–AA64 www.regulations.gov by searching for
(h) Additional Information and locating Docket No. FAA–2016–
Airworthiness Directives; The Boeing 8850.
(1) Airbus Helicopters Alert Service Company Airplanes
Bulletin No. EC130–05A021, No. EC130– Examining the AD Docket
05A022, No. AS350–05.00.84, and No. AGENCY: Federal Aviation
Administration (FAA), DOT. You may examine the AD docket on
AS355–05.00.73, all Revision 0 and all dated
ACTION: Final rule.
the Internet at http://
May 21, 2015, which are not incorporated by
reference, contain additional information
www.regulations.gov by searching for
about the subject of this final rule. For SUMMARY: We are adopting a new and locating Docket No. FAA–2016–
service information identified in this final airworthiness directive (AD) for certain 8850; or in person at the Docket
rule, contact Airbus Helicopters, 2701 N. The Boeing Company Model 767–200 Management Facility between 9 a.m.
Forum Drive, Grand Prairie, TX 75052; and –300 series airplanes. This AD was and 5 p.m., Monday through Friday,
telephone (972) 641–0000 or (800) 232–0323; prompted by a report of a fire in the except Federal holidays. The AD docket
fax (972) 641–3775; or at http:// bilge area of the cargo compartment that contains this AD, the regulatory
www.airbushelicopters.com/techpub. You burned through the insulation blankets evaluation, any comments received, and
may review the referenced service that were intended to prevent smoke other information. The address for the
information at the FAA, Office of the from migrating behind the cargo Docket Office (phone: 800–647–5527) is
asabaliauskas on DSK3SPTVN1PROD with RULES
Regional Counsel, Southwest Region, 10101 compartment sidewall liners and Docket Management Facility, U.S.
Hillwood Pkwy, Room 6N–321, Fort Worth, Department of Transportation, Docket
upward into the main cabin. This AD
TX 76177.
requires replacing the cargo Operations, M–30, West Building
(2) The subject of this AD is addressed in
compartment insulation blankets on the Ground Floor, Room W12–140, 1200
European Aviation Safety Agency (EASA) AD
No. 2015–0094, dated May 29, 2015. You left and right sides with new insulation New Jersey Avenue SE., Washington,
may view the EASA AD on the Internet at blankets that incorporate fire stops. We DC 20590.
http://www.regulations.gov in Docket No. are issuing this AD to address the unsafe FOR FURTHER INFORMATION CONTACT:
FAA–2015–3929. condition on these products. Francis Smith, Aerospace Engineer,
VerDate Sep<11>2014 19:06 Dec 23, 2016 Jkt 241001 PO 00000 Frm 00048 Fmt 4700 Sfmt 4700 E:\FR\FM\27DER1.SGM 27DER1](https://thefederalregister.org/doc/81_FR_95204/page/1.svg)
![94958 Federal Register / Vol. 81, No. 248 / Tuesday, December 27, 2016 / Rules and Regulations
PART 39—AIRWORTHINESS send your request to your principal inspector Lind Avenue SW., Renton, WA. For
DIRECTIVES or local Flight Standards District Office, as information on the availability of this
appropriate. If sending information directly material at the FAA, call 425–227–1221.
■ 1. The authority citation for part 39 to the manager of the ACO, send it to the (5) You may view this service information
continues to read as follows: attention of the person identified in that is incorporated by reference at the
paragraph (i) of this AD. Information may be National Archives and Records
Authority: 49 U.S.C. 106(g), 40113, 44701. emailed to: 9-ANM-Seattle-ACO-AMOC- Administration (NARA). For information on
Requests@faa.gov. the availability of this material at NARA, call
§ 39.13 [Amended] (2) Before using any approved AMOC, 202–741–6030, or go to: http://
■ 2. The FAA amends § 39.13 by adding notify your appropriate principal inspector, www.archives.gov/federal-register/cfr/ibr-
the following new airworthiness or lacking a principal inspector, the manager locations.html.
directive (AD): of the local flight standards district office/
Issued in Renton, Washington, on
certificate holding district office.
2016–25–29 The Boeing Company: December 9, 2016.
(3) An AMOC that provides an acceptable
Amendment 39–18755; Docket No. level of safety may be used for any repair, Dionne Palermo,
FAA–2016–8850; Directorate Identifier modification, or alteration required by this Acting Manager, Transport Airplane
2016–NM–031–AD. AD if it is approved by the Boeing Directorate, Aircraft Certification Service.
(a) Effective Date Commercial Airplanes Organization [FR Doc. 2016–30278 Filed 12–23–16; 8:45 am]
Designation Authorization (ODA) that has
This AD is effective January 31, 2017. BILLING CODE 4910–13–P
been authorized by the Manager, Seattle
(b) Affected ADs ACO, to make those findings. To be
None. approved, the repair method, modification
DEPARTMENT OF TRANSPORTATION
deviation, or alteration deviation must meet
(c) Applicability the certification basis of the airplane, and the
Federal Aviation Administration
This AD applies to The Boeing Company approval must specifically refer to this AD.
Model 767–200 and –300 series airplanes, (4) For service information that contains
steps that are labeled as Required for 14 CFR Part 91
certificated in any category, as identified in
Boeing Special Attention Service Bulletin Compliance (RC), the provisions of [Docket No. FAA–2014–0708; Amendment
767–25–0550, dated January 30, 2015. paragraphs (h)(4)(i) and (h)(4)(ii) of this AD No. 91–334A]
apply.
(d) Subject (i) The steps labeled as RC, including RIN 2120–AK93
substeps under an RC step and any figures
Air Transport Association (ATA) of Extension of the Prohibition Against
identified in an RC step, must be done to
America Code 25; Equipment/furnishings.
comply with the AD. An AMOC is required Certain Flights Within the Damascus
(e) Unsafe Condition for any deviations to RC steps, including (OSTT) Flight Information Region (FIR)
This AD was prompted by a report of a fire substeps and identified figures.
(ii) Steps not labeled as RC may be AGENCY: Federal Aviation
in the bilge area of the cargo compartment
that burned through the insulation blankets deviated from using accepted methods in Administration (FAA), Department of
that were intended to prevent smoke from accordance with the operator’s maintenance Transportation (DOT).
migrating behind the cargo compartment or inspection program without obtaining ACTION: Final rule.
sidewall liners and upward into the main approval of an AMOC, provided the RC steps,
cabin. We are issuing this AD to prevent a including substeps and identified figures, can SUMMARY: This action extends the
fire in the bilge area of the cargo still be done as specified, and the airplane prohibition of certain flight operations
compartment burning through the insulation can be put back in an airworthy condition. in the Damascus (OSTT) Flight
blankets and consequently allowing smoke to (i) Related Information Information Region (FIR) by all U.S. air
migrate behind the cargo compartment carriers; U.S. commercial operators;
sidewall liners and upward into the main For more information about this AD,
contact Francis Smith, Aerospace Engineer, persons exercising the privileges of a
cabin.
Cabin Safety & Environmental Control U.S. airman certificate, except when
(f) Compliance Systems, ANM–150S, FAA, Seattle ACO, such persons are operating a U.S.-
Comply with this AD within the 1601 Lind Avenue SW., Renton, WA 98057– registered aircraft for a foreign air
compliance times specified, unless already 3356; phone: 425–917–6596; fax: 425–917– carrier; and operators of U.S.-registered
done. 6590; email: francis.smith@faa.gov. civil aircraft, except when such
(g) Insulation Blanket Replacement (j) Material Incorporated by Reference operators are foreign air carriers. The
Within 36 months after the effective date (1) The Director of the Federal Register FAA finds that this action continues to
of this AD: Replace the cargo compartment approved the incorporation by reference be necessary to address a potential
insulation blankets on the left and right sides (IBR) of the service information listed in this hazard to persons and aircraft engaged
between stringers 29 and 33 with new paragraph under 5 U.S.C. 552(a) and 1 CFR in such flight operations.
insulation blankets that incorporate fire part 51. DATES: This final rule is effective on
stops, in accordance with the (2) You must use this service information December 30, 2016.
Accomplishment Instructions of Boeing as applicable to do the actions required by
Special Attention Service Bulletin 767–25– this AD, unless the AD specifies otherwise. FOR FURTHER INFORMATION CONTACT:
0550, dated January 30, 2015. For Groups 1 (i) Boeing Special Attention Service Michael Filippell, Air Transportation
through 4, Configurations 1 and 2, airplanes Bulletin 767–25–0550, dated January 30, Division, AFS–220, Flight Standards
identified in Boeing Special Attention 2015. Service, Federal Aviation
Service Bulletin 767–25–0550, dated January (ii) Reserved. Administration, 800 Independence
asabaliauskas on DSK3SPTVN1PROD with RULES
30, 2015, no action is required by this AD. (3) For service information identified in Avenue SW., Washington, DC 20591;
this AD, contact Boeing Commercial telephone: 202–267–8166; email:
(h) Alternative Methods of Compliance Airplanes, Attention: Contractual & Data
(AMOCs) Michael.e.filippell@faa.gov.
Services (C&DS), 2600 Westminster Blvd.,
(1) The Manager, Seattle Aircraft MC 110–SK57, Seal Beach, CA 90740–5600; SUPPLEMENTARY INFORMATION:
Certification Office (ACO), FAA, has the telephone 562–797–1717; Internet https:// I. Executive Summary
authority to approve AMOCs for this AD, if www.myboeingfleet.com.
requested using the procedures found in 14 (4) You may view this service information This action continues the prohibition
CFR 39.19. In accordance with 14 CFR 39.19, at FAA, Transport Airplane Directorate, 1601 against certain flight operations in the
VerDate Sep<11>2014 19:06 Dec 23, 2016 Jkt 241001 PO 00000 Frm 00050 Fmt 4700 Sfmt 4700 E:\FR\FM\27DER1.SGM 27DER1](https://thefederalregister.org/doc/81_FR_95204/page/3.svg)
Document Created: 2018-02-14 09:13:13
Document Modified: 2018-02-14 09:13:13
| 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 January 31, 2017. | |
| Contact | Francis Smith, Aerospace Engineer, Cabin Safety & Environmental Control Systems, ANM-150S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue SW., Renton, WA 98057- 3356; phone: 425-917-6596; fax: 425-917-6590; email: [email protected] | |
| FR Citation | 81 FR 94956 | |
| 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