Airworthiness Directives; CFM International S.A. Turbofan Engines, 49487-49490 [2019-20054]
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Federal Register / Vol. 84, No. 183 / Friday, September 20, 2019 / Proposed Rules
670BA–25–100, Revision C, dated May 11,
2017.
(i) For airplanes with the accumulation of
780 total flight hours or more as of December
15, 2015 (the effective date of AD 2015–24–
04): Inspect within 100 flight hours after
December 15, 2015.
(ii) For airplanes that have accumulated
less than 780 total flight hours as of
December 15, 2015 (the effective date of AD
2015–24–04): Inspect before accumulating
880 total flight hours after December 15,
2015.
(2) Within 30 days after the effective date
of this AD, revise the existing maintenance
or inspection program, as applicable, to
incorporate the information specified in Task
255000–208, ‘‘Detailed Inspection of the Aft
Cargo Compartment Window-Louver Panel
Assembly and Blowout Panels Along with
Their Respective Cage Assemblies,’’ as
specified in Bombardier CRJ Regional Jet TR
MRB–0079, dated May 29, 2017, to Part 1 of
the Bombardier CRJ Series Regional Jet MRM,
CSP B–053. The initial compliance time for
accomplishing the task is within 880 flight
hours from the last inspection performed in
accordance with Bombardier Service Bulletin
670BA–25–100, Revision C, dated May 11,
2017. Accomplishing the actions required by
this paragraph terminates the inspection
requirement in paragraph (h)(1) of this AD.
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(i) Credit for Previous Actions
(1) This paragraph provides credit for
actions required by paragraph (g)(1) of this
AD, if those actions were performed before
the effective date of this AD using the service
information identified in paragraphs (i)(1)(i)
through (iii) of this AD.
(i) Bombardier Service Bulletin 601R–25–
201, dated July 21, 2015.
(ii) Bombardier Service Bulletin 601R–25–
201, Revision A, dated October 21, 2015.
(iii) Bombardier Service Bulletin 601R–25–
201, Revision B, dated February 2, 2016.
(2) This paragraph provides credit for
actions required by paragraph (h)(1) of this
AD, if those actions were performed before
the effective date of this AD using the service
information identified in paragraphs (i)(2)(i)
through (iii) of this AD.
(i) Bombardier Service Bulletin 670BA–25–
100, dated July 21, 2015.
(ii) Bombardier Service Bulletin 670BA–
25–100, Revision A, dated October 21, 2015.
(iii) Bombardier Service Bulletin 670BA–
25–100, Revision B, dated February 2, 2016.
(j) Other FAA AD Provisions
(1) Alternative Methods of Compliance
(AMOCs): The Manager, New York 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 ATTN: Program Manager,
Continuing Operational Safety, FAA, New
York ACO Branch, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590; telephone
516–228–7300; fax 516–794–5531.
(2) Contacting the Manufacturer: For any
requirement in this AD to obtain corrective
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actions from a manufacturer, the action must
be accomplished using a method approved
by the Manager, New York ACO Branch,
FAA; or Transport Canada Civil Aviation
(TCCA); or Bombardier, Inc.’s TCCA Design
Approval Organization (DAO). If approved by
the DAO, the approval must include the
DAO-authorized signature.
(k) Related Information
(1) Refer to Mandatory Continuing
Airworthiness Information (MCAI) Canadian
AD CF–2015–28R2, dated February 4, 2019;
for related information. This MCAI may be
found in the AD docket on the internet at
https://www.regulations.gov by searching for
and locating Docket No. FAA–2019–0526.
(2) For more information about this AD,
contact Darren Gassetto, Aerospace Engineer,
Mechanical Systems and Administrative
Services Section, FAA, New York ACO
Branch, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516–228–
7323; fax 516–794–5531; email 9-avs-nyacocos@faa.gov.
(3) For service information identified in
this AD, contact Bombardier, Inc., 400 CoˆteVertu Road West, Dorval, Que´bec H4S 1Y9,
Canada; Widebody Customer Response
Center North America toll-free telephone 1–
866–538–1247 or direct-dial telephone 1–
514–855–2999; fax 514–855–7401; email
ac.yul@aero.bombardier.com; internet https://
www.bombardier.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.
Issued in Des Moines, Washington, on
September 16, 2019.
Suzanne Masterson,
Acting Director, System Oversight Division,
Aircraft Certification Service.
[FR Doc. 2019–20333 Filed 9–19–19; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2019–0568; Product
Identifier 2019–NE–20–AD]
RIN 2120–AA64
Airworthiness Directives; CFM
International S.A. Turbofan Engines
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
The FAA proposes to adopt a
new airworthiness directive (AD) for all
CFM International, S.A. (CFM) CFM56–
5B and CFM56–7B model turbofan
engines with a certain high-pressure
turbine (HPT) inner stationary seal
installed. This proposed AD was
SUMMARY:
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49487
prompted by cracks found in the
rotating air HPT front seal. This
proposed AD would require removal,
inspection, and replacement of the
affected HPT inner stationary seal, and
depending on the findings, removal and
replacement of the rotating air HPT
front seal. The FAA is proposing this
AD to address the unsafe condition on
these products.
DATES: The FAA must receive comments
on this proposed AD by November 4,
2019.
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
https://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 CFM International
Inc., Aviation Operations Center, 1
Neumann Way, M/D Room 285,
Cincinnati, OH 45125; phone: 877–432–
3272; fax: 877–432–3329; email:
aviation.fleetsupport@ge.com. You may
view this service information at the
FAA, Engine and Propeller Standards
Branch, 1200 District Avenue,
Burlington, MA 01803. For information
on the availability of this material at the
FAA, call 781–238–7759.
ADDRESSES:
Examining the AD Docket
You may examine the AD docket on
the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2019–
0568; 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 NPRM, the
regulatory evaluation, any comments
received, and other information. The
street address for Docket Operations is
listed above. Comments will be
available in the AD docket shortly after
receipt.
FOR FURTHER INFORMATION CONTACT:
Christopher McGuire, Aerospace
Engineer, ECO Branch, FAA, 1200
District Avenue, Burlington, MA 01803;
phone: 781–238–7120; fax: 781–238–
7199; email: chris.mcguire@faa.gov.
SUPPLEMENTARY INFORMATION:
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Federal Register / Vol. 84, No. 183 / Friday, September 20, 2019 / Proposed Rules
Comments Invited
The FAA invites you to send any
written relevant data, views, or
arguments about this proposal. Send
your comments to an address listed
under the ADDRESSES section. Include
‘‘Docket No. FAA–2019–0568; Product
Identifier 2019–NE–20–AD’’ at the
beginning of your comments. The FAA
specifically invites comments on the
overall regulatory, economic,
environmental, and energy aspects of
this NPRM. The FAA will consider all
comments received by the closing date
and may amend this NPRM because of
those comments.
The FAA will post all comments
received, without change, to https://
www.regulations.gov, including any
personal information you provide. The
FAA will also post a report
summarizing each substantive verbal
contact received about this NPRM.
Discussion
The FAA received a report that two
cracks were discovered on a CFM
CFM56–5B model turbofan engine
rotating air HPT front seal during a
routine engine shop visit. After
investigation, CFM determined that the
HPT inner stationary seal, part number
1808M56G01, may not have received
the correct braze heat treat cycle at the
time of the honeycomb replacement. As
a result, the affected HPT inner
stationary seal could lead to a localized
separation of the replaced honeycomb,
which may affect the life of the rotating
air HPT front seal. This condition, if not
addressed, could result in an
uncontained release of the rotating air
HPT front seal, damage to the engine,
and damage to the airplane.
Related Service Information Under 1
CFR Part 51
The FAA reviewed CFM Service
Bulletin (SB) CFM56–5B S/B 72–0952,
dated April 23, 2019, and CFM SB
CFM56–7B S/B 72–1054, dated April
23, 2019. CFM SB CFM56–5B S/B 72–
0952, dated April 23, 2019, describes
procedures for repairing the CFM56–5B
turbofan engine HPT inner stationary
seal honeycomb. CFM SB CFM56–7B
S/B 72–1054, dated April 23, 2019,
describes procedures for repairing the
CFM56–7B turbofan engine HPT inner
stationary seal honeycomb. 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
The FAA is proposing this AD
because it 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
removal, inspection, and replacement of
the affected HPT inner stationary seal
and, depending on the findings, removal
and replacement of the rotating air HPT
front seal with a part eligible for
installation.
Costs of Compliance
The FAA estimates that this proposed
AD affects 210 engines installed on
airplanes of U.S. registry. Operators
have the option to replace or repair the
affected HPT inner stationary seal. The
part cost is for replacement with a
repaired HPT inner stationary seal.
The FAA estimates the following
costs to comply with this proposed AD:
ESTIMATED COSTS
Action
Labor cost
Replace HPT inner stationary seal .................
Inspect HPT inner stationary seal ..................
1 work-hour × $85 per hour = $85 .................
1 work-hour × $85 per hour = $85 .................
The FAA estimates the following
costs to do any necessary replacements
that would be required based on the
Parts cost
results of the proposed inspection. The
FAA has no way of determining the
$7,910
0
Cost per
product
$7,995
85
Cost on U.S.
operators
$1,678,950
17,850
number of engines that might need these
replacements:
ON-CONDITION COSTS
Action
Labor cost
Replace rotating air HPT front seal ..............................
Inspect HPT rotor blade internal cavities .....................
Replace HPT rotor blade (pair) ....................................
Replace No. 3 ball bearing ...........................................
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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.
The FAA is issuing this rulemaking
under the authority described in
Subtitle VII, Part A, Subpart III, Section
44701: ‘‘General requirements.’’ Under
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16:49 Sep 19, 2019
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1
1
1
1
work-hour
work-hour
work-hour
work-hour
×
×
×
×
$85
$85
$85
$85
per
per
per
per
hour
hour
hour
hour
=
=
=
=
$85
$85
$85
$85
Parts cost
...............................
...............................
...............................
...............................
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
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$344,600
0
31,000
30,000
Cost per
product
$344,685
85
31,085
30,085
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 engines, propellers, and
associated appliances to the Manager,
Engine and Propeller Standards Branch,
Policy and Innovation Division.
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Federal Register / Vol. 84, No. 183 / Friday, September 20, 2019 / Proposed Rules
Regulatory Findings
The FAA 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) Will not affect intrastate aviation
in Alaska, and
(3) 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
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive (AD):
■
CFM International, S.A.: Docket No. FAA–
2019–0568; Product Identifier 2019–NE–
20–AD.
(a) Comments Due Date
The FAA must receive comments by
November 4, 2019.
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(b) Affected ADs
None.
(c) Applicability
(1) This AD applies to all CFM
International, S.A. (CFM) CFM56–5B1, –5B1/
2P, –5B1/3, –5B1/P, –5B2, –5B2/2P, –5B2/3,
–5B2/P, –5B3/2P, –5B3/2P1, –5B3/3, –5B3/
3B1, –5B3/P, –5B3/P1, –5B4, –5B4/2P, –5B4/
2P1, –5B4/3, –5B4/3B1, –5B4/P, –5B4/P1,
–5B5, –5B5/3, –5B5/P, –5B6, –5B6/2P, –5B6/
3, –5B6/P, –5B7, –5B7/3, –5B7/P, –5B8/3,
–5B8/P, –5B9/2P, –5B9/3, –5B9/P, CFM56–
7B20, –7B20/2, –7B20/3, –7B20E, –7B22,
–7B22/2, –7B22/3, –7B22/3B1, –7B22/B1,
–7B22E, –7B22E/B1, –7B24, –7B24/2, –7B24/
3, –7B24/3B1, –7B24/B1, –7B24E, –7B24E/
B1, –7B26, –7B26/2, –7B26/3, –7B26/3B1,
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Jkt 247001
–7B26/3B2, –7B26/3B2F, –7B26/3F, –7B26/
B1, –7B26/B2, –7B26E, –7B26E/B1, –7B26E/
B2, –7B26E/B2F, –7B26E/F, –7B27, –7B27/2,
–7B27/3, –7B27/3B1, –7B27/3B1F, –7B27/
3B3, –7B27/3F, –7B27/B1, –7B27/B3,
–7B27A, –7B27A/3, –7B27AE, –7B27E,
–7B27E/B1, –7B27E/B1F, –7B27E/B3, and
–7B27E/F model turbofan engines with a
high-pressure turbine (HPT) inner stationary
seal, part number (P/N) 1808M56G01
installed that has a serial number (S/N) listed
in Planning Information, Paragraph 1.A.,
Table 1, of CFM Service Bulletin (SB)
CFM56–5B S/B 72–0952, dated April 23,
2019, or in Planning Information, Paragraph
1.A., Table 1, CFM SB CFM56–7B S/B 72–
1054, dated April 23, 2019, installed.
(2) This AD does not apply to affected CFM
CFM56–5B and CFM56–7B model turbofan
engines with the affected HPT inner
stationary seal installed if the seal has been
repaired as specified in CFM56–5B Engine
Shop Manual (ESM), 72–41–03, REPAIR 003,
or CFM56–7B ESM, 72–41–03, REPAIR 003,
after the year listed in Paragraph 1.A., Table
1, of CFM SB CFM56–5B S/B 72–0952 dated
April 23, 2019, or Paragraph 1.A., Table 1,
CFM SB CFM56–7B S/B 72–1054, dated
April 23, 2019.
(d) Subject
Joint Aircraft System Component (JASC)
Code 7230, Turbine Engine Compressor
Section.
(e) Unsafe Condition
This AD was prompted by cracks found in
the rotating air HPT front seal. The FAA is
issuing this AD to prevent failure of the HPT
inner stationary seal and the rotating air HPT
front seal. The unsafe condition, if not
addressed, could result in uncontained
release of the rotating air HPT front seal,
damage to the engine, and damage to the
airplane.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Required Actions
(1) At the next engine shop visit after the
effective date of this AD, remove the affected
HPT inner stationary seal from service and
replace with a HPT inner stationary seal (that
is not listed in Planning Information,
Paragraph 1.A., Table 1, of CFM SB CFM56–
5B S/B 72–0952, dated April 23, 2019, or in
Planning Information, Paragraph 1.A., Table
1, CFM SB CFM56–7B S/B 72–1054, dated
April 23, 2019) or a repaired HPT inner
stationary seal that is eligible for installation
per the definition in paragraph (h)(2) of this
AD.
(2) After removing the affected HPT inner
stationary seal required by paragraph (g)(1),
inspect the removed HPT inner stationary
seal for honeycomb separation, as defined in
the Accomplishment Instructions, paragraph
3.C.(1), in CFM SB CFM56–5B S/B 72–0952,
dated April 23, 2019, or in CFM SB CFM56–
7B S/B 72–1054, dated April 23, 2019.
(3) If honeycomb separation is found
during the inspection required by paragraph
(g)(2) of this AD, before further flight:
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49489
(i) Remove the rotating air HPT front seal
from service and replace with a part eligible
for installation.
(ii) Inspect the HPT rotor blade internal
cavities for honeycomb metal debris per the
Accomplishment Instructions, paragraph
3.C.(1)(a)(4), of CFM SB CFM56–5B S/B 72–
0952, dated April 23, 2019, or CFM SB
CFM56–7B S/B 72–1054, dated April 23,
2019. If honeycomb metal debris is found,
remove the HPT rotor blade from service and
replace with a part eligible for installation.
(iii) Remove the No. 3 ball bearing from
service and replace with a part eligible for
installation.
(h) Definition
(1) For the purpose of this AD, an ‘‘engine
shop visit’’ is the induction of an engine into
the shop for maintenance involving the
separation of pairs of major mating engine
case flanges, except that the separation of
engine flanges solely for the purposes of
transportation without subsequent
maintenance does not constitute an engine
shop visit.
(2) For the purpose of this AD, a repaired
HPT inner stationary seal that is eligible for
installation is any HPT inner stationary seal,
P/N 1808M56G01 and with a S/N listed in
Paragraph 1.A., Table 1, of CFM SB CFM56–
5B S/B 72–0952, dated April 23, 2019, or
Paragraph 1.A., Table 1, CFM SB CFM56–7B
S/B 72–1054, dated April 23, 2019 that has
been repaired per CFM56–5B ESM, 72–41–
03, REPAIR 003, or CFM56–7B ESM, 72–41–
03, REPAIR 003, after the year listed in
Paragraph 1.A., Table 1, of CFM SB CFM56–
5B S/B 72–0952, dated April 23, 2019, or
Paragraph 1.A., Table 1, CFM SB CFM56–7B
S/B 72–1054, dated April 23, 2019.
(i) No Reporting Requirement
The reporting requirements contained
within the SBs referenced in paragraph (g) of
this AD are not required by this AD.
(j) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, ECO 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 (k)(1) of this AD. You
may email your request to: ANE-AD-AMOC@
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.
(k) Related Information
(1) For more information about this AD,
contact Christopher McGuire, Aerospace
Engineer, ECO Branch, FAA, 1200 District
Avenue, Burlington, MA 01803; phone: 781–
238–7120; fax: 781–238–7199; email:
chris.mcguire@faa.gov.
(2) For service information identified in
this AD, contact CFM International Inc.,
Aviation Operations Center, 1 Neumann
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Federal Register / Vol. 84, No. 183 / Friday, September 20, 2019 / Proposed Rules
Way, M/D Room 285, Cincinnati, OH 45125;
phone: 877–432–3272; fax: 877–432–3329;
email: aviation.fleetsupport@ge.com. You
may view this referenced service information
at the FAA, Engine & Propeller Standards
Branch, 1200 District Avenue, Burlington,
MA 01803. For information on the
availability of this material at the FAA, call
781–238–7759.
Issued in Burlington, Massachusetts, on
September 11, 2019.
Robert J. Ganley,
Manager, Engine and Propeller Standards
Branch, Aircraft Certification Service.
[FR Doc. 2019–20054 Filed 9–19–19; 8:45 am]
BILLING CODE 4910–13–P
COMMODITY FUTURES TRADING
COMMISSION
17 CFR Part 13
RIN Number 3038–AE90
Public Rulemaking Procedures
Commodity Futures Trading
Commission.
ACTION: Notice of proposed rulemaking.
AGENCY:
The Commodity Futures
Trading Commission (the
‘‘Commission’’) is proposing to amend
part 13 of its regulations to eliminate the
provisions that set forth the procedure
for the formulation, amendment, or
repeal of rules or regulations. Because
the Administrative Procedure Act
(‘‘APA’’) governs the Commission’s
rulemaking process, the Commission
believes that it is unnecessary to codify
the rulemaking process in a Commission
regulation. Part 13, as amended, will be
comprised solely of the procedure for
filing petitions for rulemakings as the
APA does not address this process.
DATES: Comments must be received on
or before October 21, 2019.
ADDRESSES: You may submit comments,
identified by RIN number 3038–AE90,
by any of the following methods:
• Agency Website: https://
comments.cftc.gov;
• Mail: Secretary of the Commission,
Commodity Futures Trading
Commission, Three Lafayette Centre,
1155 21st Street NW, Washington, DC
20581;
• Hand Delivery/Courier: Same as
Mail, above.
• Federal eRulemaking Portal: https://
www.regulations.gov. Follow
instructions for submitting comments.
All comments must be submitted in
English, or if not, accompanied by an
English translation. Comments will be
posted as received to https://
www.cftc.gov. You should submit only
information that you wish to make
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SUMMARY:
VerDate Sep<11>2014
16:49 Sep 19, 2019
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available publicly. If you wish the
Commission to consider information
that may be exempt from disclosure
under the Freedom of Information Act,
a petition for confidential treatment of
the exempt information may be
submitted according to the procedures
established in CFTC regulations at 17
CFR part 145.
The Commission reserves the right,
but shall have no obligation, to review,
pre-screen, filter, redact, refuse or
remove any or all of your submission
from https://www.cftc.gov that it may
deem to be inappropriate for
publication, such as obscene language.
All submissions that have been redacted
or removed that contain comments on
the merits of the rulemaking will be
retained in the public comment file and
will be considered as required under the
Administrative Procedure Act and other
applicable laws, and may be accessible
under the Freedom of Information Act.
FOR FURTHER INFORMATION CONTACT:
Herminio Castro, Senior Special
Counsel, (202) 418–6705, hcastro@
cftc.gov; Dhaval Patel, Counsel, (202)
418–5125, dpatel@cftc.gov; Office of the
General Counsel, Commodity Futures
Trading Commission, 1155 21st Street
NW, Washington, DC 20581.
SUPPLEMENTARY INFORMATION:
I. Discussion
Part 13 sets forth procedures for the
formulation, amendment, or repeal of
rules or regulations insofar as those
procedures directly affect the public.1
The Commission promulgated part 13
pursuant to former section 4a(j) of the
Commodity Exchange Act (‘‘CEA’’),2
which is currently section 2(a)(12) of the
CEA.3 Section 2(a)(12) states that the
Commission is authorized to promulgate
such rules and regulations as it deems
necessary to govern the operating
procedures and conduct of business of
the Commission. This section
authorizes, but does not require, the
Commission to promulgate regulations
governing its rulemaking process. The
Commission first adopted part 13 in
1976 and has not revised part 13 since.
The Commission would eliminate the
provisions in part 13 that set forth the
process for rulemakings.4 As originally
adopted, part 13 was intended to track
the APA rulemaking process. However,
in its current form, part 13 does not
fully conform to the APA, which may
1 17
CFR part 13.
41 FR 17536 (Apr. 27, 1976); Public Law
93–463, Sec. 101(a)(11), 88 Stat. 1391, 7 U.S.C. 4a(j).
3 7 U.S.C. 2(a)(12).
4 The provisions being eliminated are 17 CFR
13.1, 13.3, 13.4, 13.5, and 13.6. 17 CFR 13.2 is being
retained and renumbered as 17 CFR 13.1.
2 See
PO 00000
Frm 00008
Fmt 4702
Sfmt 4702
create ambiguity and confusion about
the procedures to be followed by the
Commission in rulemakings.5 To be
clear, the APA governs Commission
rulemakings. Specifically, section 553 of
the APA provides for the procedures to
be followed by the Commission when
promulgating formal and informal
rulemakings.6 Because the APA governs
the Commission’s rulemaking process,
the Commission believes that it is
unnecessary to codify the rulemaking
process in a Commission regulation that
would be duplicative of the APA.
The Commission would retain
regulation 13.2, which is supplemental
to the APA. Regulation 13.2 describes
the procedures by which anyone who
wishes the Commission to consider the
issuance, amendment, or repeal of a rule
may petition the Commission.
Specifically, regulation 13.2 provides
instructions as to where the petition
should be sent, what information should
be included in the petition, and
prescribes the manner in which the
Commission must respond to such
petition. The Commission believes that
retaining this provision is necessary as
the APA does not address this process.
Furthermore, a formalized process for
petitions would promote consistency
and transparency in the way that the
Commission handles petitions for
rulemakings.
Accordingly, this proposed
rulemaking would remove regulations
13.1, 13.3, 13.4, 13.5, and 13.6 from part
13 and retain and renumber regulation
13.2 as regulation 13.1. In addition, the
Commission would revise the authority
citation for part 13. The current
authority cited for part 13, 7 U.S.C. 4a(j),
is incorrect due to subsequent
renumbering and is being changed to 7
U.S.C. 2(a)(12).
II. Related Matters
A. Regulatory Flexibility Act
The Regulatory Flexibility Act 7
requires federal agencies to consider
whether the rules they propose will
have a significant economic impact on
a substantial number of small entities
and, if so, to provide a regulatory
flexibility analysis regarding the
economic impact on those entities. This
rule would remove unnecessary and
potentially confusing provisions of part
13 and update the authority cited. As
5 For example, section 13.4(b) allows formal
rulemakings to be conducted through oral
presentation or written submissions; in contrast,
APA sections 556 and 557 require a trial-like
process to be followed for formal rulemakings.
6 See 5 U.S.C. 551 et seq.; Attorney General’s
Manual on the Administrative Procedure Act 9
(1947).
7 5 U.S.C. 601 et seq.
E:\FR\FM\20SEP1.SGM
20SEP1
Agencies
[Federal Register Volume 84, Number 183 (Friday, September 20, 2019)]
[Proposed Rules]
[Pages 49487-49490]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2019-20054]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2019-0568; Product Identifier 2019-NE-20-AD]
RIN 2120-AA64
Airworthiness Directives; CFM International S.A. Turbofan Engines
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for all CFM International, S.A. (CFM) CFM56-5B and CFM56-7B model
turbofan engines with a certain high-pressure turbine (HPT) inner
stationary seal installed. This proposed AD was prompted by cracks
found in the rotating air HPT front seal. This proposed AD would
require removal, inspection, and replacement of the affected HPT inner
stationary seal, and depending on the findings, removal and replacement
of the rotating air HPT front seal. The FAA is proposing this AD to
address the unsafe condition on these products.
DATES: The FAA must receive comments on this proposed AD by November 4,
2019.
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 https://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 CFM
International Inc., Aviation Operations Center, 1 Neumann Way, M/D Room
285, Cincinnati, OH 45125; phone: 877-432-3272; fax: 877-432-3329;
email: [email protected]. You may view this service
information at the FAA, Engine and Propeller Standards Branch, 1200
District Avenue, Burlington, MA 01803. For information on the
availability of this material at the FAA, call 781-238-7759.
Examining the AD Docket
You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2019-
0568; 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 NPRM, the regulatory evaluation, any comments received, and other
information. The street address for Docket Operations is listed above.
Comments will be available in the AD docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT: Christopher McGuire, Aerospace
Engineer, ECO Branch, FAA, 1200 District Avenue, Burlington, MA 01803;
phone: 781-238-7120; fax: 781-238-7199; email: [email protected].
SUPPLEMENTARY INFORMATION:
[[Page 49488]]
Comments Invited
The FAA invites you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under the ADDRESSES section. Include ``Docket No. FAA-2019-0568;
Product Identifier 2019-NE-20-AD'' at the beginning of your comments.
The FAA specifically invites comments on the overall regulatory,
economic, environmental, and energy aspects of this NPRM. The FAA will
consider all comments received by the closing date and may amend this
NPRM because of those comments.
The FAA will post all comments received, without change, to https://www.regulations.gov, including any personal information you provide.
The FAA will also post a report summarizing each substantive verbal
contact received about this NPRM.
Discussion
The FAA received a report that two cracks were discovered on a CFM
CFM56-5B model turbofan engine rotating air HPT front seal during a
routine engine shop visit. After investigation, CFM determined that the
HPT inner stationary seal, part number 1808M56G01, may not have
received the correct braze heat treat cycle at the time of the
honeycomb replacement. As a result, the affected HPT inner stationary
seal could lead to a localized separation of the replaced honeycomb,
which may affect the life of the rotating air HPT front seal. This
condition, if not addressed, could result in an uncontained release of
the rotating air HPT front seal, damage to the engine, and damage to
the airplane.
Related Service Information Under 1 CFR Part 51
The FAA reviewed CFM Service Bulletin (SB) CFM56-5B S/B 72-0952,
dated April 23, 2019, and CFM SB CFM56-7B S/B 72-1054, dated April 23,
2019. CFM SB CFM56-5B S/B 72-0952, dated April 23, 2019, describes
procedures for repairing the CFM56-5B turbofan engine HPT inner
stationary seal honeycomb. CFM SB CFM56-7B S/B 72-1054, dated April 23,
2019, describes procedures for repairing the CFM56-7B turbofan engine
HPT inner stationary seal honeycomb. 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
The FAA is proposing this AD because it 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 removal, inspection, and replacement
of the affected HPT inner stationary seal and, depending on the
findings, removal and replacement of the rotating air HPT front seal
with a part eligible for installation.
Costs of Compliance
The FAA estimates that this proposed AD affects 210 engines
installed on airplanes of U.S. registry. Operators have the option to
replace or repair the affected HPT inner stationary seal. The part cost
is for replacement with a repaired HPT inner stationary seal.
The FAA estimates the following costs to comply with this proposed
AD:
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
Replace HPT inner stationary seal..... 1 work-hour x $85 per $7,910 $7,995 $1,678,950
hour = $85.
Inspect HPT inner stationary seal..... 1 work-hour x $85 per 0 85 17,850
hour = $85.
----------------------------------------------------------------------------------------------------------------
The FAA estimates the following costs to do any necessary
replacements that would be required based on the results of the
proposed inspection. The FAA has no way of determining the number of
engines that might need these replacements:
On-Condition Costs
----------------------------------------------------------------------------------------------------------------
Cost per
Action Labor cost Parts cost product
----------------------------------------------------------------------------------------------------------------
Replace rotating air HPT front seal........... 1 work-hour x $85 per hour = $85 $344,600 $344,685
Inspect HPT rotor blade internal cavities..... 1 work-hour x $85 per hour = $85 0 85
Replace HPT rotor blade (pair)................ 1 work-hour x $85 per hour = $85 31,000 31,085
Replace No. 3 ball bearing.................... 1 work-hour x $85 per hour = $85 30,000 30,085
----------------------------------------------------------------------------------------------------------------
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.
The FAA is 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 engines, propellers, and
associated appliances to the Manager, Engine and Propeller Standards
Branch, Policy and Innovation Division.
[[Page 49489]]
Regulatory Findings
The FAA 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) Will not affect intrastate aviation in Alaska, and
(3) 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):
CFM International, S.A.: Docket No. FAA-2019-0568; Product
Identifier 2019-NE-20-AD.
(a) Comments Due Date
The FAA must receive comments by November 4, 2019.
(b) Affected ADs
None.
(c) Applicability
(1) This AD applies to all CFM International, S.A. (CFM) CFM56-
5B1, -5B1/2P, -5B1/3, -5B1/P, -5B2, -5B2/2P, -5B2/3, -5B2/P, -5B3/
2P, -5B3/2P1, -5B3/3, -5B3/3B1, -5B3/P, -5B3/P1, -5B4, -5B4/2P, -
5B4/2P1, -5B4/3, -5B4/3B1, -5B4/P, -5B4/P1, -5B5, -5B5/3, -5B5/P, -
5B6, -5B6/2P, -5B6/3, -5B6/P, -5B7, -5B7/3, -5B7/P, -5B8/3, -5B8/P,
-5B9/2P, -5B9/3, -5B9/P, CFM56-7B20, -7B20/2, -7B20/3, -7B20E, -
7B22, -7B22/2, -7B22/3, -7B22/3B1, -7B22/B1, -7B22E, -7B22E/B1, -
7B24, -7B24/2, -7B24/3, -7B24/3B1, -7B24/B1, -7B24E, -7B24E/B1, -
7B26, -7B26/2, -7B26/3, -7B26/3B1, -7B26/3B2, -7B26/3B2F, -7B26/3F,
-7B26/B1, -7B26/B2, -7B26E, -7B26E/B1, -7B26E/B2, -7B26E/B2F, -
7B26E/F, -7B27, -7B27/2, -7B27/3, -7B27/3B1, -7B27/3B1F, -7B27/3B3,
-7B27/3F, -7B27/B1, -7B27/B3, -7B27A, -7B27A/3, -7B27AE, -7B27E, -
7B27E/B1, -7B27E/B1F, -7B27E/B3, and -7B27E/F model turbofan engines
with a high-pressure turbine (HPT) inner stationary seal, part
number (P/N) 1808M56G01 installed that has a serial number (S/N)
listed in Planning Information, Paragraph 1.A., Table 1, of CFM
Service Bulletin (SB) CFM56-5B S/B 72-0952, dated April 23, 2019, or
in Planning Information, Paragraph 1.A., Table 1, CFM SB CFM56-7B S/
B 72-1054, dated April 23, 2019, installed.
(2) This AD does not apply to affected CFM CFM56-5B and CFM56-7B
model turbofan engines with the affected HPT inner stationary seal
installed if the seal has been repaired as specified in CFM56-5B
Engine Shop Manual (ESM), 72-41-03, REPAIR 003, or CFM56-7B ESM, 72-
41-03, REPAIR 003, after the year listed in Paragraph 1.A., Table 1,
of CFM SB CFM56-5B S/B 72-0952 dated April 23, 2019, or Paragraph
1.A., Table 1, CFM SB CFM56-7B S/B 72-1054, dated April 23, 2019.
(d) Subject
Joint Aircraft System Component (JASC) Code 7230, Turbine Engine
Compressor Section.
(e) Unsafe Condition
This AD was prompted by cracks found in the rotating air HPT
front seal. The FAA is issuing this AD to prevent failure of the HPT
inner stationary seal and the rotating air HPT front seal. The
unsafe condition, if not addressed, could result in uncontained
release of the rotating air HPT front seal, damage to the engine,
and damage to the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
(1) At the next engine shop visit after the effective date of
this AD, remove the affected HPT inner stationary seal from service
and replace with a HPT inner stationary seal (that is not listed in
Planning Information, Paragraph 1.A., Table 1, of CFM SB CFM56-5B S/
B 72-0952, dated April 23, 2019, or in Planning Information,
Paragraph 1.A., Table 1, CFM SB CFM56-7B S/B 72-1054, dated April
23, 2019) or a repaired HPT inner stationary seal that is eligible
for installation per the definition in paragraph (h)(2) of this AD.
(2) After removing the affected HPT inner stationary seal
required by paragraph (g)(1), inspect the removed HPT inner
stationary seal for honeycomb separation, as defined in the
Accomplishment Instructions, paragraph 3.C.(1), in CFM SB CFM56-5B
S/B 72-0952, dated April 23, 2019, or in CFM SB CFM56-7B S/B 72-
1054, dated April 23, 2019.
(3) If honeycomb separation is found during the inspection
required by paragraph (g)(2) of this AD, before further flight:
(i) Remove the rotating air HPT front seal from service and
replace with a part eligible for installation.
(ii) Inspect the HPT rotor blade internal cavities for honeycomb
metal debris per the Accomplishment Instructions, paragraph
3.C.(1)(a)(4), of CFM SB CFM56-5B S/B 72-0952, dated April 23, 2019,
or CFM SB CFM56-7B S/B 72-1054, dated April 23, 2019. If honeycomb
metal debris is found, remove the HPT rotor blade from service and
replace with a part eligible for installation.
(iii) Remove the No. 3 ball bearing from service and replace
with a part eligible for installation.
(h) Definition
(1) For the purpose of this AD, an ``engine shop visit'' is the
induction of an engine into the shop for maintenance involving the
separation of pairs of major mating engine case flanges, except that
the separation of engine flanges solely for the purposes of
transportation without subsequent maintenance does not constitute an
engine shop visit.
(2) For the purpose of this AD, a repaired HPT inner stationary
seal that is eligible for installation is any HPT inner stationary
seal, P/N 1808M56G01 and with a S/N listed in Paragraph 1.A., Table
1, of CFM SB CFM56-5B S/B 72-0952, dated April 23, 2019, or
Paragraph 1.A., Table 1, CFM SB CFM56-7B S/B 72-1054, dated April
23, 2019 that has been repaired per CFM56-5B ESM, 72-41-03, REPAIR
003, or CFM56-7B ESM, 72-41-03, REPAIR 003, after the year listed in
Paragraph 1.A., Table 1, of CFM SB CFM56-5B S/B 72-0952, dated April
23, 2019, or Paragraph 1.A., Table 1, CFM SB CFM56-7B S/B 72-1054,
dated April 23, 2019.
(i) No Reporting Requirement
The reporting requirements contained within the SBs referenced
in paragraph (g) of this AD are not required by this AD.
(j) Alternative Methods of Compliance (AMOCs)
(1) The Manager, ECO 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 (k)(1) of this AD. You may email your
request 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.
(k) Related Information
(1) For more information about this AD, contact Christopher
McGuire, Aerospace Engineer, ECO Branch, FAA, 1200 District Avenue,
Burlington, MA 01803; phone: 781-238-7120; fax: 781-238-7199; email:
[email protected].
(2) For service information identified in this AD, contact CFM
International Inc., Aviation Operations Center, 1 Neumann
[[Page 49490]]
Way, M/D Room 285, Cincinnati, OH 45125; phone: 877-432-3272; fax:
877-432-3329; email: [email protected]. You may view this
referenced service information at the FAA, Engine & Propeller
Standards Branch, 1200 District Avenue, Burlington, MA 01803. For
information on the availability of this material at the FAA, call
781-238-7759.
Issued in Burlington, Massachusetts, on September 11, 2019.
Robert J. Ganley,
Manager, Engine and Propeller Standards Branch, Aircraft Certification
Service.
[FR Doc. 2019-20054 Filed 9-19-19; 8:45 am]
BILLING CODE 4910-13-P