82 FR 12755 - Airworthiness Directives; Honeywell International Inc. Turbofan Engines
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 82, Issue 43 (March 7, 2017)
Federal Aviation Administration
Federal Register Volume 82, Issue 43 (March 7, 2017)
| Page Range | 12755-12757 | |
| FR Document | 2017-04370 |
[Federal Register Volume 82, Number 43 (Tuesday, March 7, 2017)] [Proposed Rules] [Pages 12755-12757] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2017-04370] [[Page 12755]] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2016-9451; Directorate Identifier 2016-NE-24-AD] RIN 2120-AA64 Airworthiness Directives; Honeywell International Inc. Turbofan Engines AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). ----------------------------------------------------------------------- SUMMARY: We propose to adopt a new airworthiness directive (AD) for all Honeywell International Inc. TFE731-20 and TFE731-40 turbofan engines. This proposed AD was prompted by two fan disks found with a manufacturing-caused flaw. This proposed AD would require removing affected fan disks, performing a one-time inspection, and replacing fan disks that fail inspection. We are proposing this AD to correct the unsafe condition on these products. DATES: We must receive comments on this proposed AD by April 21, 2017. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods:Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments. Fax: 202-493-2251. Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590. Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For service information identified in this NPRM, contact Honeywell International Inc., 111 S. 34th Street, Phoenix, AZ 85034-2802; phone: 800-601-3099; Internet: https://myaerospace.honeywell.com/wps/portal/!ut/. You may view this service information at the FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA 01803. For information on the availability of this material at the FAA, call (781) 238-7125. 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- 9451; 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 proposed AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Office (phone: 800-647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. FOR FURTHER INFORMATION CONTACT: Joseph Costa, Aerospace Engineer, Los Angeles Aircraft Certification Office, FAA, Transport Airplane Directorate, 3960 Paramount Blvd., Lakewood, CA 90712-4137; phone: 562- 627-5246; fax: 562-627-5210; email: [email protected]. SUPPLEMENTARY INFORMATION: Comments Invited We invite you to send any written relevant data, views, or arguments about this NPRM. Send your comments to an address listed under the ADDRESSES section. Include ``Docket No. FAA-2016-9451; Directorate Identifier 2016-NE-24-AD'' at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this NPRM. We will consider all comments received by the closing date and may amend this NPRM because of those comments. We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this NPRM. Discussion We received reports of two fan disks with material rollover condition on the surface of the dovetail slot. The material rollover was caused by incomplete chamfering or edge-break of the fan disk dovetail slots after broaching and subsequent shot-peening. This material rollover was considered a crack-like stress riser that can cause reduction in fatigue life and cracking. This condition, if not corrected, could result in uncontained failure of the fan disk and damage to the engine and airplane. Related Service Information Under 1 CFR Part 51 We reviewed Honeywell Service Bulletin (SB) TFE731-72-5256, Revision 0, dated October 7, 2016. The SB identifies affected fan disks by serial number and describes procedures for removing, inspecting, and replacing the fan disks. 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. FAA's Determination We are proposing this AD because we evaluated all the relevant information and determined the unsafe condition described previously is likely to exist or develop in other products of the same type design. Proposed AD Requirements This proposed AD would require removing, inspecting, and replacing affected fan disks. Differences Between This Proposed AD and the Service Information Honeywell SB TFE731-72-5256, Revision 0, dated October 7, 2016 specifies a five year compliance time with no grace period. This NPRM proposes a tiered compliance time based on cycle accumulation. Also, Honeywell SB TFE731-72-5256 specifies compliance with two overhaul/ repair instructions (ORIs). Honeywell ORI T43374 addresses the fan disk material rollover condition and Honeywell ORI T43342 addresses additional material in the fan disk wings. This NPRM addresses only ORI T43374 corrective action for an unsafe condition. Costs of Compliance We estimate that this proposed AD affects 61 engines installed on airplanes of U.S. registry. We estimate the following costs to comply with this proposed AD: Estimated Costs ---------------------------------------------------------------------------------------------------------------- Cost per Cost on U.S. Action Labor cost Parts cost product operators ---------------------------------------------------------------------------------------------------------------- Remove fan disk.................... 8 work-hours x $85 per hour $0 $680.00 $41,480.00 = $680.00. Inspect fan disk................... 8 work-hours x $85 per hour $0 680.00 41,480.00 = $680.00. [[Page 12756]] Install reworked or new fan disk... 18 work-hours x $85 per $0 1,530.00 93,330.00 hour = $1,530.00. ---------------------------------------------------------------------------------------------------------------- We estimate the following costs to do any necessary disk replacements that would be required based on the results of the proposed inspection. We estimate that 6 engines will need this replacement: On-Condition Costs ---------------------------------------------------------------------------------------------------------------- Cost per Action Labor cost Parts cost product ---------------------------------------------------------------------------------------------------------------- Replace non-serviceable disks with new fan 1 work-hour x $85 per hour = $85.00 $50,000.00 $300,510.00 disk. ---------------------------------------------------------------------------------------------------------------- According to the manufacturer, some of the costs of this proposed 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 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 We determined that this proposed AD would not have federalism implications under Executive Order 13132. This proposed AD would 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 this proposed regulation: (1) Is not a ``significant regulatory action'' under Executive Order 12866, (2) Is not a ``significant rule'' under the 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. The Proposed Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA proposes to amend 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): Honeywell International Inc. (Type Certificate previously held by AlliedSignal Inc., Garrett Engine Division; Garrett Turbine Engine Company; and AiResearch Manufacturing Company of Arizona): Docket No. FAA-2016-9451; Directorate Identifier 2016-NE-24-AD. (a) Comments Due Date We must receive comments by April 21, 2017. (b) Affected ADs None. (c) Applicability This AD applies to all Honeywell International Inc. (Honeywell) TFE731-20 and TFE731-40 turbofan engines, with fan disk, part number (P/N) 3060287-2 and serial numbers (S/Ns) listed in Table 9 of Honeywell Service Bulletin (SB) TFE731-72-5256, Revision 0, dated October 7, 2016, that do not have ``T43374'' marked adjacent to the engine P/N or S/N. (d) Subject Joint Aircraft System Component (JASC) Code 7230, Turbine Engine Compressor Section. (e) Unsafe Condition This AD was prompted by a report of two fan disks found with surface rollovers in the dovetail slot area. We are issuing this AD to prevent uncontained failure of the fan disks and damage to the engine and airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Required Actions (1) Remove fan disks with 9,000 cycles-since-new (CSN) or more on the effective date of this AD, within 100 cycles-in-service (CIS), or at the next shop visit, or at next access, whichever occurs first, after the effective date of this AD. (2) Remove fan disks with between 8,000 and 8,999 CSN, inclusive, on the effective date of this AD, within 9,100 CSN or within 1,000 CIS, or at the next shop visit, or at next access, whichever occurs first, after the effective date of this AD. (3) Remove fan disks with fewer than 8,000 CSN, on the effective date of this AD, before exceeding 9,000 CSN, or at the next shop visit, or at next access, whichever occurs first, after the effective date of this AD. (4) Inspect removed fan disks in accordance with Paragraph 3.D.(2) in the Accomplishment Instructions of Honeywell SB TFE731- 72-5256, Revision 0, dated October 7, 2016. (5) Replace all removed fan disks with a part eligible for installation. [[Page 12757]] (h) Definitions (1) For the purposes of this AD, shop visit is defined as the removal of the tie-shaft nut from the engine. (2) For the purposes of this AD, access is defined as the removal of the fan rotor assembly from the engine. (3) For the purposes of this AD, parts eligible for installation are those fan disks that pass the inspections and are marked with ``T43374'' adjacent to the P/N or S/N. (i) Alternative Methods of Compliance (AMOCs) (1) The Manager, Los Angeles Aircraft Certification Office, FAA, may approve AMOCs for this AD. Use the procedures found in 14 CFR 39.19 to make your request. (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. (j) Related Information (1) For more information about this AD, contact Joseph Costa, Aerospace Engineer, Los Angeles Aircraft Certification Office, FAA, Transport Airplane Directorate, 3960 Paramount Blvd., Lakewood, CA 90712-4137; phone: 562-627-5246; fax: 562-627-5210; email: [email protected]. (2) For service information identified in this AD, contact Honeywell International Inc., 111 S. 34th Street, Phoenix, AZ 85034- 2802; phone: 800-601-3099; Internet: https://myaerospace.honeywell.com/wps/portal/!ut/. (3) For service information on returning the fan disk for inspection identified in SB TFE731-72-5256 of this AD, contact Honeywell International Inc., 111 S. 34th Street, Phoenix, AZ 85034- 2802; phone: 800-601-3099; Internet: https://myaerospace.honeywell.com/wps/portal/!ut/. (4) You may view this service information at the FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA. For information on the availability of this material at the FAA, call 781-238-7125. Issued in Burlington, Massachusetts on February 8, 2017. Carlos A. Pestana, Acting Manager, Engine & Propeller Directorate, Aircraft Certification Service. [FR Doc. 2017-04370 Filed 3-6-17; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 82, No. 43 / Tuesday, March 7, 2017 / Proposed Rules 12755
DEPARTMENT OF TRANSPORTATION material at the FAA, call (781) 238– subsequent shot-peening. This material
7125. rollover was considered a crack-like
Federal Aviation Administration stress riser that can cause reduction in
Examining the AD Docket
fatigue life and cracking. This condition,
14 CFR Part 39 You may examine the AD docket on if not corrected, could result in
the Internet at http:// uncontained failure of the fan disk and
[Docket No. FAA–2016–9451; Directorate www.regulations.gov by searching for damage to the engine and airplane.
Identifier 2016–NE–24–AD] and locating Docket No. FAA–2016–
9451; or in person at the Docket Related Service Information Under 1
RIN 2120–AA64 CFR Part 51
Management Facility between 9 a.m.
Airworthiness Directives; Honeywell and 5 p.m., Monday through Friday, We reviewed Honeywell Service
International Inc. Turbofan Engines except Federal holidays. The AD docket Bulletin (SB) TFE731–72–5256,
contains this proposed AD, the Revision 0, dated October 7, 2016. The
AGENCY: Federal Aviation regulatory evaluation, any comments SB identifies affected fan disks by serial
Administration (FAA), DOT. received, and other information. The number and describes procedures for
ACTION: Notice of proposed rulemaking street address for the Docket Office removing, inspecting, and replacing the
(NPRM). (phone: 800–647–5527) is in the fan disks. This service information is
ADDRESSES section. Comments will be reasonably available because the
SUMMARY: We propose to adopt a new available in the AD docket shortly after interested parties have access to it
airworthiness directive (AD) for all receipt. through their normal course of business
Honeywell International Inc. TFE731–
FOR FURTHER INFORMATION CONTACT: or by the means identified in the
20 and TFE731–40 turbofan engines.
Joseph Costa, Aerospace Engineer, Los ADDRESSES section.
This proposed AD was prompted by two
Angeles Aircraft Certification Office,
fan disks found with a manufacturing- FAA’s Determination
FAA, Transport Airplane Directorate,
caused flaw. This proposed AD would
3960 Paramount Blvd., Lakewood, CA We are proposing this AD because we
require removing affected fan disks,
90712–4137; phone: 562–627–5246; fax: evaluated all the relevant information
performing a one-time inspection, and
562–627–5210; email: joseph.costa@ and determined the unsafe condition
replacing fan disks that fail inspection.
faa.gov. described previously is likely to exist or
We are proposing this AD to correct the
SUPPLEMENTARY INFORMATION: develop in other products of the same
unsafe condition on these products.
type design.
DATES: We must receive comments on Comments Invited
this proposed AD by April 21, 2017. Proposed AD Requirements
We invite you to send any written
ADDRESSES: You may send comments, relevant data, views, or arguments about This proposed AD would require
using the procedures found in 14 CFR this NPRM. Send your comments to an removing, inspecting, and replacing
11.43 and 11.45, by any of the following address listed under the ADDRESSES affected fan disks.
methods: section. Include ‘‘Docket No. FAA– Differences Between This Proposed AD
• Federal eRulemaking Portal: Go to 2016–9451; Directorate Identifier 2016– and the Service Information
http://www.regulations.gov. Follow the NE–24–AD’’ at the beginning of your
instructions for submitting comments. comments. We specifically invite Honeywell SB TFE731–72–5256,
• Fax: 202–493–2251. comments on the overall regulatory, Revision 0, dated October 7, 2016
• Mail: U.S. Department of economic, environmental, and energy specifies a five year compliance time
Transportation, Docket Operations, M– aspects of this NPRM. We will consider with no grace period. This NPRM
30, West Building Ground Floor, Room all comments received by the closing proposes a tiered compliance time based
W12–140, 1200 New Jersey Avenue SE., date and may amend this NPRM on cycle accumulation. Also, Honeywell
Washington, DC 20590. because of those comments. SB TFE731–72–5256 specifies
• Hand Delivery: Deliver to Mail We will post all comments we compliance with two overhaul/repair
address above between 9 a.m. and 5 receive, without change, to http:// instructions (ORIs). Honeywell ORI
p.m., Monday through Friday, except www.regulations.gov, including any T43374 addresses the fan disk material
Federal holidays. personal information you provide. We rollover condition and Honeywell ORI
For service information identified in will also post a report summarizing each T43342 addresses additional material in
this NPRM, contact Honeywell substantive verbal contact we receive the fan disk wings. This NPRM
International Inc., 111 S. 34th Street, about this NPRM. addresses only ORI T43374 corrective
Phoenix, AZ 85034–2802; phone: 800– action for an unsafe condition.
601–3099; Internet: https:// Discussion
Costs of Compliance
myaerospace.honeywell.com/wps/ We received reports of two fan disks
portal/!ut/. You may view this service with material rollover condition on the We estimate that this proposed AD
information at the FAA, Engine & surface of the dovetail slot. The material affects 61 engines installed on airplanes
Propeller Directorate, 1200 District rollover was caused by incomplete of U.S. registry.
Avenue, Burlington, MA 01803. For chamfering or edge-break of the fan disk We estimate the following costs to
information on the availability of this dovetail slots after broaching and comply with this proposed AD:
jstallworth on DSK7TPTVN1PROD with PROPOSALS
ESTIMATED COSTS
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
Remove fan disk ..................... 8 work-hours × $85 per hour = $680.00 ................................ $0 $680.00 $41,480.00
Inspect fan disk ....................... 8 work-hours × $85 per hour = $680.00 ................................ $0 680.00 41,480.00
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ESTIMATED COSTS—Continued
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
Install reworked or new fan 18 work-hours × $85 per hour = $1,530.00 ........................... $0 1,530.00 93,330.00
disk.
We estimate the following costs to do would be required based on the results that 6 engines will need this
any necessary disk replacements that of the proposed inspection. We estimate replacement:
ON-CONDITION COSTS
Cost per
Action Labor cost Parts cost product
Replace non-serviceable disks with new fan disk ....... 1 work-hour × $85 per hour = $85.00 .......................... $50,000.00 $300,510.00
According to the manufacturer, some (2) Is not a ‘‘significant rule’’ under (c) Applicability
of the costs of this proposed AD may be the DOT Regulatory Policies and This AD applies to all Honeywell
covered under warranty, thereby Procedures (44 FR 11034, February 26, International Inc. (Honeywell) TFE731–20
reducing the cost impact on affected 1979), and TFE731–40 turbofan engines, with fan
individuals. We do not control warranty (3) Will not affect intrastate aviation disk, part number (P/N) 3060287–2 and serial
coverage for affected individuals. As a numbers (S/Ns) listed in Table 9 of
in Alaska, and
result, we have included all costs in our Honeywell Service Bulletin (SB) TFE731–72–
cost estimate. (4) Will not have a significant 5256, Revision 0, dated October 7, 2016, that
economic impact, positive or negative, do not have ‘‘T43374’’ marked adjacent to the
Authority for This Rulemaking on a substantial number of small entities engine P/N or S/N.
Title 49 of the United States Code under the criteria of the Regulatory (d) Subject
specifies the FAA’s authority to issue Flexibility Act.
Joint Aircraft System Component (JASC)
rules on aviation safety. Subtitle I, List of Subjects in 14 CFR Part 39 Code 7230, Turbine Engine Compressor
section 106, describes the authority of Section.
the FAA Administrator. Subtitle VII: Air transportation, Aircraft, Aviation
safety, Incorporation by reference, (e) Unsafe Condition
Aviation Programs, describes in more
detail the scope of the Agency’s Safety. This AD was prompted by a report of two
authority. fan disks found with surface rollovers in the
The Proposed Amendment dovetail slot area. We are issuing this AD to
We are issuing this rulemaking under
prevent uncontained failure of the fan disks
the authority described in Subtitle VII, Accordingly, under the authority and damage to the engine and airplane.
Part A, Subpart III, Section 44701: delegated to me by the Administrator,
‘‘General requirements.’’ Under that the FAA proposes to amend 14 CFR part (f) Compliance
section, Congress charges the FAA with 39 as follows: Comply with this AD within the
promoting safe flight of civil aircraft in compliance times specified, unless already
air commerce by prescribing regulations PART 39—AIRWORTHINESS done.
for practices, methods, and procedures DIRECTIVES
(g) Required Actions
the Administrator finds necessary for
safety in air commerce. This regulation ■ 1. The authority citation for part 39 (1) Remove fan disks with 9,000 cycles-
is within the scope of that authority since-new (CSN) or more on the effective
continues to read as follows:
date of this AD, within 100 cycles-in-service
because it addresses an unsafe condition Authority: 49 U.S.C. 106(g), 40113, 44701. (CIS), or at the next shop visit, or at next
that is likely to exist or develop on access, whichever occurs first, after the
products identified in this rulemaking § 39.13 [Amended] effective date of this AD.
action. (2) Remove fan disks with between 8,000
■ 2. The FAA amends § 39.13 by adding
Regulatory Findings the following new airworthiness and 8,999 CSN, inclusive, on the effective
directive (AD): date of this AD, within 9,100 CSN or within
We determined that this proposed AD 1,000 CIS, or at the next shop visit, or at next
would not have federalism implications Honeywell International Inc. (Type
access, whichever occurs first, after the
Certificate previously held by
under Executive Order 13132. This effective date of this AD.
AlliedSignal Inc., Garrett Engine
proposed AD would not have a Division; Garrett Turbine Engine
(3) Remove fan disks with fewer than 8,000
substantial direct effect on the States, on CSN, on the effective date of this AD, before
Company; and AiResearch
the relationship between the national Manufacturing Company of Arizona): exceeding 9,000 CSN, or at the next shop
jstallworth on DSK7TPTVN1PROD with PROPOSALS
Government and the States, or on the Docket No. FAA–2016–9451; Directorate visit, or at next access, whichever occurs
distribution of power and Identifier 2016–NE–24–AD. first, after the effective date of this AD.
(4) Inspect removed fan disks in
responsibilities among the various (a) Comments Due Date accordance with Paragraph 3.D.(2) in the
levels of government. Accomplishment Instructions of Honeywell
We must receive comments by April 21,
For the reasons discussed above, I 2017. SB TFE731–72–5256, Revision 0, dated
certify this proposed regulation: October 7, 2016.
(1) Is not a ‘‘significant regulatory (b) Affected ADs (5) Replace all removed fan disks with a
action’’ under Executive Order 12866, None. part eligible for installation.
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(h) Definitions SECURITIES AND EXCHANGE business days between the hours of
(1) For the purposes of this AD, shop visit COMMISSION 10:00 a.m. and 3:00 p.m. All comments
is defined as the removal of the tie-shaft nut received will be posted without change;
from the engine. 17 CFR Parts 210, 211, 229, 231 and the Commission does not edit personal
(2) For the purposes of this AD, access is 241 identifying information from
defined as the removal of the fan rotor [Release No. 33–10321; 34–80131; File No. submissions. You should submit only
assembly from the engine. S7–02–17] information that you wish to make
(3) For the purposes of this AD, parts available publicly.
eligible for installation are those fan disks RIN 3235–AL79
FOR FURTHER INFORMATION CONTACT:
that pass the inspections and are marked Lindsay McCord, Associate Chief
Request for Comment on Possible
with ‘‘T43374’’ adjacent to the P/N or S/N. Accountant in the Office of Chief
Changes to Industry Guide 3
(i) Alternative Methods of Compliance (Statistical Disclosure by Bank Holding Accountant, Division of Corporation
(AMOCs) Companies) Finance, at (202) 551–3400, U.S.
Securities and Exchange Commission,
(1) The Manager, Los Angeles Aircraft AGENCY: Securities and Exchange 100 F Street NE., Washington, DC
Certification Office, FAA, may approve Commission. 20549.
AMOCs for this AD. Use the procedures
ACTION: Request for comment. SUPPLEMENTARY INFORMATION:
found in 14 CFR 39.19 to make your request.
(2) Before using any approved AMOC, SUMMARY: The Commission is Table of Contents
notify your appropriate principal inspector, publishing this request for comment to
or lacking a principal inspector, the manager I. Introduction
seek public input as to the disclosures II. Applicable Disclosures
of the local flight standards district office/ called for by Industry Guide 3, A. Distribution of Assets, Liabilities and
certificate holding district office. Statistical Disclosure by Bank Holding Stockholders’ Equity; Interest Rate and
(j) Related Information Companies. The financial services Interest Differential (Average Balance,
industry has changed dramatically since Interest and Yield/Rate Analysis and
(1) For more information about this AD, Rate/Volume Analysis)
contact Joseph Costa, Aerospace Engineer,
Guide 3 was first published.
B. Investment Portfolio
Los Angeles Aircraft Certification Office, Consequently, our disclosure guidance
C. Loan Portfolio
FAA, Transport Airplane Directorate, 3960 may not in all cases reflect recent D. Summary of Loan Loss Experience
Paramount Blvd., Lakewood, CA 90712– industry developments or changes in E. Deposits
4137; phone: 562–627–5246; fax: 562–627– accounting standards related to F. Return on Equity and Assets
5210; email: joseph.costa@faa.gov. financial and other reporting G. Short-Term Borrowings
(2) For service information identified in requirements. H. Potential New Disclosures
III. Applicability of Disclosure Requirements
this AD, contact Honeywell International DATES: Comments should be received on A. Applicability to Registrants Other Than
Inc., 111 S. 34th Street, Phoenix, AZ 85034– or before May 8, 2017. Bank Holding Companies
2802; phone: 800–601–3099; Internet: https:// ADDRESSES: Comments may be B. Applicability to Foreign Registrants
myaerospace.honeywell.com/wps/portal/!ut/. submitted by any of the following C. Size Thresholds and Reporting Periods
(3) For service information on returning the methods: IV. Closing
fan disk for inspection identified in SB
TFE731–72–5256 of this AD, contact Electronic Comments I. Introduction
Honeywell International Inc., 111 S. 34th • Use the Commission’s Internet The Commission is considering
Street, Phoenix, AZ 85034–2802; phone: comment form (http://www.sec.gov/ possible revisions to its disclosure
800–601–3099; Internet: https:// rules/other.shtml); regime for bank holding companies.
myaerospace.honeywell.com/wps/portal/!ut/. • Send an email to rule-comments@ When we discuss current disclosure
(4) You may view this service information sec.gov. Please include File Number S7– guidance in this request for comment,
at the FAA, Engine & Propeller Directorate, 02–17 on the subject line; or we focus on the disclosures currently
1200 District Avenue, Burlington, MA. For • Use the Federal eRulemaking Portal called for by Industry Guide 3,
information on the availability of this (http://www.regulations.gov). Follow the Statistical Disclosure by Bank Holding
material at the FAA, call 781–238–7125. instructions for submitting comments. Companies (Guide 3).1 By its terms,
Issued in Burlington, Massachusetts on Guide 3 applies exclusively to bank
Paper Comments holding companies, although the staff
February 8, 2017.
Carlos A. Pestana, • Send paper comments to Secretary, has previously indicated that the
Securities and Exchange Commission, disclosures called for by Guide 3
Acting Manager, Engine & Propeller ‘‘should also be provided by other
100 F Street NE., Washington, DC
Directorate, Aircraft Certification Service.
20549–1090. registrants with material lending and
[FR Doc. 2017–04370 Filed 3–6–17; 8:45 am] deposit activities.’’ 2 In this request for
All submissions should refer to File
BILLING CODE 4910–13–P
Number S7–02–17. This file number comment, when we use the term ‘‘BHC
should be included on the subject line registrants,’’ we are referring to public
if email is used. To help us process and companies that apply Guide 3
review your comments more efficiently, disclosures. In light of developments in
please use only one method of
jstallworth on DSK7TPTVN1PROD with PROPOSALS
1 57 FR 36442.
submission. The Commission will post 2 Staff Accounting Bulletin Topic 11:K—
all comments on the Commission’s Web Application of Article 9 and Guide 3 (SAB 11:K).
site (http://www.sec.gov/rules/ The Industry Guides and SAB 11:K are not rules,
other.shtml). Comments also are regulations or statements of the Commission.
available for Web site viewing and Further, as with any staff guidance, the views of the
staff referenced in this request for comment are not
printing in the Commission’s Public rules or interpretations of the Commission. The
Reference Room, 100 F Street NE., Commission has neither approved nor disapproved
Washington, DC 20549, on official the views of the staff expressed herein.
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Document Created: 2018-02-01 14:48:51
Document Modified: 2018-02-01 14:48:51
| 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 | Proposed Rules | |
| Action | Notice of proposed rulemaking (NPRM). | |
| Dates | We must receive comments on this proposed AD by April 21, 2017. | |
| Contact | Joseph Costa, Aerospace Engineer, Los Angeles Aircraft Certification Office, FAA, Transport Airplane Directorate, 3960 Paramount Blvd., Lakewood, CA 90712-4137; phone: 562- 627-5246; fax: 562-627-5210; email: [email protected] | |
| FR Citation | 82 FR 12755 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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