Airworthiness Directives; International Aero Engines AG Turbofan Engines, 55624-55627 [2020-19749]
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55624
Federal Register / Vol. 85, No. 175 / Wednesday, September 9, 2020 / Proposed Rules
Revision 39, dated October 26, 2018; which
can be found on the Flight Standards
Information Management System (FSIMS)
website, https://fsims.faa.gov/
PICResults.aspx?mode=Publication
&doctype=MMELByModel.
(i) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, Seattle ACO Branch,
FAA, has the authority to approve AMOCs
for this AD, if requested using the procedures
found in 14 CFR 39.19. In accordance with
14 CFR 39.19, send your request to your
principal inspector or local Flight Standards
District Office, as appropriate. If sending
information directly to the manager of the
certification office, send it to the attention of
the person identified in paragraph (j) of this
AD. Information may be emailed to: 9-ANMSeattle-ACO-AMOC-Requests@faa.gov.
(2) Before using any approved AMOC,
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
of the local flight standards district office/
certificate holding district office.
(3) An AMOC that provides an acceptable
level of safety may be used for any repair,
modification, or alteration required by this
AD if it is approved by The Boeing Company
Organization Designation Authorization
(ODA) that has been authorized by the
Manager, Seattle ACO Branch, FAA, 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.
(j) Related Information
For more information about this AD,
contact Jeffrey Rothman, Aerospace Engineer,
Propulsion Section, FAA, Seattle ACO
Branch, 2200 South 216th St., Des Moines,
WA 98190; phone and fax: 206–231–3558;
jeffrey.rothman@faa.gov.
Issued on August 21, 2020.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives,
Compliance & Airworthiness Division,
Aircraft Certification Service.
[FR Doc. 2020–19583 Filed 9–8–20; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2020–0700; Project
Identifier AD–2020–00238–E]
RIN 2120–AA64
Airworthiness Directives; International
Aero Engines AG Turbofan Engines
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
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The FAA proposes to
supersede Airworthiness Directive (AD)
2019–06–06, which applies to all
International Aero Engines AG (IAE)
V2500–A1, V2522–A5, V2524–A5,
V2525–D5, V2527–A5, V2527E–A5,
V2527M–A5, V2528–D5, V2530–A5,
V2533–A5 model turbofan engines. AD
2019–06–06 requires initial and
repetitive borescope inspections (BSIs)
of the diffuser case M-flange and, if it
fails the inspection, replacement of the
diffuser case with a part eligible for
installation. Since the FAA issued AD
2019–06–06, the manufacturer
performed an updated safety risk
analysis, which reduced the diffuser
case M-flange inspection intervals and
added the performance of a replacement
of the diffuser case M-flange. This
proposed AD would require an initial
BSI of the diffuser case M-flange and, if
it fails the inspection, repetitive BSIs of
the diffuser case M-flange until
replacement of the diffuser case Mflange is performed. 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 October 26,
2020.
SUMMARY:
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 International Aero
Engines AG, 400 Main Street, East
Hartford, CT 06118; phone: 800–565–
0140; email: help24@pw.utc.com;
website: https://fleetcare.pw.utc.com.
You may view this service information
at the FAA, Airworthiness Products
Section, Operational Safety 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–2020–
0700; or in person at Docket Operations
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between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
The AD docket contains this NPRM, 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:
Nicholas Paine, Aerospace Engineer,
ECO Branch, FAA, 1200 District
Avenue, Burlington, MA 01803; phone:
781–238–7742; fax: 781–238–7199;
email: nicholas.j.paine@faa.gov.
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any
written relevant data, views, or
arguments about this proposed AD.
Send your comments to an address
listed under the ADDRESSES section.
Include ‘‘Docket No. FAA–2020–0700;
Project Identifier AD–2020–00238–E’’ at
the beginning of your comments. The
most helpful comments reference a
specific portion of the proposal, explain
the reason for any recommended
change, and include supporting data.
The FAA will consider all comments
received by the closing date and may
amend this NPRM because of those
comments.
Except for Confidential Business
Information as described in the
following paragraph, and other
information as described in 14 CFR
11.35, the FAA will post all comments
received, without change, to https://
www.regulations.gov, including any
personal information you provide. The
agency will also post a report
summarizing each substantive verbal
contact received about this proposal.
Confidential Business Information
Confidential Business Information
(CBI) is commercial or financial
information that is both customarily and
actually treated as private by its owner.
Under the Freedom of Information Act
(FOIA) (5 U.S.C. 552), CBI is exempt
from public disclosure. If your
comments responsive to this NPRM
contain commercial or financial
information that is customarily treated
as private, that you actually treat as
private, and that is relevant or
responsive to this NPRM, it is important
that you clearly designate the submitted
comments as CBI. Please mark each
page of your submission containing CBI
as ‘‘PROPIN.’’ The FAA will treat such
marked submissions as confidential
under the FOIA, and they will not be
placed in the public docket of this
NPRM. Submissions containing CBI
should be sent to Nicholas Paine,
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Federal Register / Vol. 85, No. 175 / Wednesday, September 9, 2020 / Proposed Rules
Aerospace Engineer, ECO Branch, FAA,
1200 District Avenue, Burlington, MA
01803. Any commentary that the FAA
receives which is not specifically
designated as CBI will be placed in the
public docket for this rulemaking.
Background
The FAA issued AD 2019–06–06,
Amendment 39–19604 (84 FR 11642,
March 28, 2019) (‘‘AD 2019–06–06’’), for
all IAE V2500–A1, V2522–A5, V2524–
A5, V2525–D5, V2527–A5, V2527E–A5,
V2527M–A5, V2528–D5, V2530–A5,
V2533–A5 model turbofan engines. AD
2019–06–06 requires initial and
repetitive BSIs of the diffuser case Mflange and, if it fails the inspection,
replacement of the diffuser case with a
part eligible for installation. AD 2019–
06–06 resulted from a crack found at the
diffuser case M-flange during overhaul
inspection. The FAA issued AD 2019–
06–06 to prevent failure of the diffuser
case.
Actions Since AD 2019–06–06 Was
Issued
Since the FAA issued AD 2019–06–
06, the manufacturer performed an
updated safety risk analysis, which
resulted in reducing the diffuser case Mflange inspection intervals and adding
the performance of a replacement of the
diffuser case M-flange, which terminates
the need for repetitive BSIs of the
diffuser case M-flange.
FAA’s Determination
The FAA is issuing this NPRM
because the agency has determined that
the unsafe condition described
previously is likely to exist or develop
in other products of the same type
design.
Service Information Incorporated by
Reference Under 1 CFR Part 51
The FAA reviewed IAE NonModification Alert Service Bulletin
(NMASB) V2500–ENG–72–A0706,
Revision 2, dated November 7, 2019.
IAE NMASB V2500–ENG–72–A0706,
Revision 2, describes procedures for
inspecting the diffuser case M-flange.
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.
Other Related Service Information
The FAA reviewed IAE Service
Bulletin (SB) V2500–ENG–72–0709,
dated December 13, 2019. IAE SB
V2500–ENG–72–0709 describes
procedures for replacing the diffuser
case M-flange.
Proposed AD Requirements in This
NPRM
This proposed AD would retain
certain requirements of AD 2019–06–06.
This proposed AD would require an
initial BSI of the diffuser case M-flange
and, if it fails the inspection, repetitive
BSIs of the diffuser case M-flange until
replacement of the diffuser case Mflange is performed.
Costs of Compliance
The FAA estimates that this AD, as
proposed, would affect 1,654 engines
installed on airplanes of U.S. registry.
The FAA estimates the following
costs to comply with this proposed AD:
ESTIMATED COSTS
Action
Labor cost
BSI of diffuser case M-flange .........................
Replace the diffuser case M-flange ................
2 work-hours × $85 per hour = $170 .............
40 work-hours × $85 per hour = $3,400 ........
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. The FAA does not control
warranty coverage for affected
individuals. As a result, the FAA has
included all costs in its 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.
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
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Parts cost
Cost per
product
$0
20,000
Cost on U.S.
operators
$170
23,400
$281,180
38,703,600
that authority because it addresses an
unsafe condition that is likely to exist or
develop on products identified in this
rulemaking action.
List of Subjects in 14 CFR Part 39
Regulatory Findings
The Proposed Amendment
The FAA has 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 that the proposed regulation:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866,
(2) Would not affect intrastate
aviation in Alaska, and
(3) Would not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
Accordingly, under the authority
delegated to me by the Administrator,
the FAA proposes to amend 14 CFR part
39 as follows:
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Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
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:
a. Removing Airworthiness Directive
(AD) 2019–06–06, Amendment 39–
19604 (84 FR 11642, March 28, 2019);
and
■ b. Adding the following new AD:
■
■
International Aero Engines AG: Docket No.
FAA–2020–0700; Project Identifier AD–
2020–00238–E.
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Federal Register / Vol. 85, No. 175 / Wednesday, September 9, 2020 / Proposed Rules
(a) Comments Due Date
The FAA must receive comments on this
AD action by October 26, 2020.
(b) Affected ADs
This AD replaces AD 2019–06–06,
Amendment 39–19604 (84 FR 11642, March
28, 2019).
(c) Applicability
This AD applies to all International Aero
Engines AG (IAE) V2500–A1, V2522–A5,
V2524–A5, V2525–D5, V2527–A5, V2527E–
A5, V2527M–A5, V2528–D5, V2530–A5, and
V2533–A5 model turbofan engines.
(e) Unsafe Condition
(g) Required Actions
This AD was prompted by a crack found
at the diffuser case M-flange during overhaul
inspection. The FAA is issuing this AD to
prevent failure of the diffuser case. The
unsafe condition, if not addressed, could
result in uncontained diffuser case rupture,
damage to the engine, and damage to the
airplane.
(1) Borescope Inspection of Diffuser Case MFlange
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(d) Subject
Joint Aircraft System Component (JASC)
Code 7250, Turbine Section.
(ii) For engines with a diffuser case Mflange that has fewer than 19,000 CSN on the
effective date of this AD, perform the BSI of
the diffuser case M-flange before
accumulating 20,300 CSN.
(iii) For engines with a diffuser case Mflange in which the CSN is unknown,
perform the BSI of the diffuser case M-flange
within 250 cycles after the effective date of
this AD.
(iv) Use the Accomplishment Instructions,
paragraphs 2.A. through 2.G. of IAE NonModification Alert Service Bulletin (NMASB)
V2500–ENG–72–A0706, Revision 2, dated
November 7, 2019 (‘‘the NMASB’’), to
perform the initial BSI.
(v) If no crack is found as a result of the
inspections required by paragraphs (g)(1)(i)
through (iii) of this AD, repeat the BSI of
zones 1, 2, and 3 of the diffuser case M-flange
at intervals not to exceed 2,100 cycles since
the previous BSI.
(vi) If a crack is found as a result of the
inspections required by paragraphs (g)(1)(i)
through (iii) of this AD, replace the diffuser
case M-flange or repeat the BSI of zones 1,
2, and 3 of the diffuser case M-flange as
specified by either ‘‘Table 2: Fly on Limits’’
or ‘‘Table 4: Fly on Limits,’’ in paragraph 2,
Accomplishment Instructions, of the NMASB
as appropriate for the affected the engine
model.
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(2) Replacement of the Diffuser Case MFlange
(i) At the next engine shop visit after the
effective date of this AD or before the diffuser
case M-flange accumulates 20,000 CSN,
whichever occurs later, replace the diffuser
case M-flange.
Note 1 to paragraph (g)(2)(i): Guidance on
performing the replacement of the diffuser
case M-flange can be found in the
Accomplishment Instructions, paragraphs
1.A. and B., of IAE SB V2500–ENG–72–0709,
dated December 13, 2019.
(ii) Thereafter, repeat the replacement of
the diffuser case M-flange before
accumulating 20,000 cycles since the
previous replacement.
(iii) Replacement of the diffuser case Mflange is the terminating action for the
repetitive BSIs required by paragraph (g)(1) of
this AD.
(h) Installation Prohibition
After the effective date of this AD, do not
install a diffuser case onto any engine if the
diffuser case M-flange has more than 20,000
CSN.
(i) Credit for Previous Actions
You may take credit for the initial BSIs that
are required by paragraphs (g)(1)(i) through
(iii) of this AD, or the replacement of the
diffuser case M-flange required by paragraph
(g)(2) of this AD, if you performed those
actions before the effective date of this AD
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For engines with a diffuser case assembly,
part number 2A0051, 2A2081–01, 2A2581–
01, 2A2883–01, 2A2885–01, 2A2889–01,
2A2891–01, 2A2896–01, 2A2897–01, or
2A3132 installed, perform an initial
borescope inspection (BSI) of zones 1, 2, and
3 of the diffuser case M-flange as follows:
(i) For engines with a diffuser case Mflange that has 19,000 or more cycles since
new (CSN) on the effective date of this AD,
perform the BSI of the diffuser case M-flange
before accumulating the ‘‘Inspect within
(Cycles)’’ in Table 1 to paragraph (g)(1) of this
AD. If the CSLFPI is unknown, use the CSN
of the diffuser case M-flange.
using IAE NMASB V2500–ENG–72–A0706,
Revision 1, dated June 28, 2019, or Original
Issue, dated February 14, 2019; IAE V2500
Special Instruction (SI) No. 341F–18, dated
November 19, 2018; IAE V2500 SI No. 350F–
18, Rev. 1, dated December 17, 2018; IAE
V2500 SI No. 356F–18, Rev. 1, dated January
9, 2019; IAE V2500 SI No. 372F–18, dated
January 8, 2019; or IAE V2500 Special SI No.
04F–19, dated January 14, 2019.
(j) Definition
For the purpose of this AD, an ‘‘engine
shop visit’’ is the induction of the engine into
the shop for maintenance involving the
separation of pairs of major mating engine
flanges.
(k) 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 (l)(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
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Federal Register / Vol. 85, No. 175 / Wednesday, September 9, 2020 / Proposed Rules
of the local flight standards district office/
certificate holding district office.
management of instrument flight rules
(IFR) operations in the area.
(l) Related Information
DATES: Comments must be received on
or before October 26, 2020.
(1) For more information about this AD,
contact Nicholas Paine, Aerospace Engineer,
ADDRESSES: Send comments on this
ECO Branch, FAA, 1200 District Avenue,
proposal to: The U.S. Department of
Burlington, MA 01803; phone: 781–238–
Transportation, Docket Operations, 1200
7742; fax: 781–238–7199; email:
New Jersey Avenue SE, West Building
nicholas.j.paine@faa.gov.
Ground Floor, Room W12–140,
(2) For service information identified in
Washington, DC 20590–0001;
this AD, contact International Aero Engines
Telephone: (800) 647–5527, or (202)
AG, 400 Main Street, East Hartford, CT
06118; phone: 800–565–0140; email: help24@ 366–9826. You must identify the Docket
pw.utc.com; website: https://
No. FAA–2020–0701; Airspace Docket
fleetcare.pw.utc.com. You may view this
No. 20–ASO–19, at the beginning of
referenced service information at the FAA,
your comments. You may also submit
Airworthiness Products Section, Operational
comments through the internet at
Safety Branch, 1200 District Avenue,
https://www.regulations.gov.
Burlington, MA 01803. For information on
FAA Order 7400.11D, Airspace
the availability of this material at the FAA,
Designations and Reporting Points, and
call 781–238–7759.
subsequent amendments can be viewed
Issued on September 1, 2020.
on line at https://www.faa.gov/air_
Lance T. Gant,
traffic/publications/. For further
Director, Compliance & Airworthiness
information, you can contact the
Division, Aircraft Certification Service.
Airspace Policy Group, Federal Aviation
[FR Doc. 2020–19749 Filed 9–8–20; 8:45 am]
Administration, 800 Independence
BILLING CODE 4910–13–P
Avenue SW, Washington, DC, 20591;
Telephone: (202) 267–8783. The Order
is also available for inspection at the
DEPARTMENT OF TRANSPORTATION
National Archives and Records
Administration (NARA). For
Federal Aviation Administration
information on the availability of FAA
Order 7400.11D at NARA, email
14 CFR Part 71
fedreg.legal@nara.gov or go to https://
[Docket No. FAA–2020–0701; Airspace
www.archives.gov/federal-register/cfr/
Docket No. 20–ASO–19]
ibr-locations.html.
RIN 2120–AA66
FOR FURTHER INFORMATION CONTACT: John
Fornito, Operations Support Group,
Proposed Establishment of Class D
Eastern Service Center, Federal Aviation
and Class E Airspace and Proposed
Administration, 1701 Columbia Avenue,
Amendment of Class E Airspace;
College Park, GA 30337; Telephone
Nashville, TN
(404) 305–6364.
SUPPLEMENTARY INFORMATION:
AGENCY: Federal Aviation
Administration (FAA), DOT.
Authority for This Rulemaking
ACTION: Notice of proposed rulemaking
The FAA’s authority to issue rules
(NPRM).
regarding aviation safety is found in
Title 49 of the United States Code.
SUMMARY: This action proposes to
Subtitle I, Section 106 describes the
establish Class D and Class E airspace
designated as an extension to Class D or authority of the FAA Administrator.
Subtitle VII, Aviation Programs,
E surface area, and amend Class E
describes in more detail the scope of the
airspace extending upward from 700
agency’s authority. This rulemaking is
feet above the surface for John C. Tune
promulgated under the authority
Airport, Nashville, TN, as a new air
described in Subtitle VII, Part A,
traffic control tower shall service the
Subpart I, Section 40103. Under that
airport. This action would also update
section, the FAA is charged with
the geographic coordinates of the
prescribing regulations to assign the use
airport, as well as Sumner County
of airspace necessary to ensure the
Regional Airport, and Lebanon
safety of aircraft and the efficient use of
Municipal Airport, and Murfreesboro
airspace. This regulation is within the
Municipal Airport. In addition, this
scope of that authority as it would
action would establish Class E airspace
establish Class D and Class E airspace,
extending upward from 700 feet above
and amend Class E airspace for John C.
the surface for Vanderbilt University
Tune Airport, and establish Class E
Hospital Heliport, as instrument
airspace for Vanderbilt University
approaches have been designed for the
Hospital Heliport, Nashville, TN, to
heliport. Controlled airspace is
support IFR operations in the area.
necessary for the safety and
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Comments Invited
Interested persons are invited to
comment on this proposed rulemaking
by submitting such written data, views,
or arguments, as they may desire.
Comments that provide the factual basis
supporting the views and suggestions
presented are particularly helpful in
developing reasoned regulatory
decisions on the proposal. Comments
are specifically invited on the overall
regulatory, aeronautical, economic,
environmental, and energy-related
aspects of the proposal.
Communications should identify both
docket numbers (Docket No. FAA–
2020–0701 and Airspace Docket No. 20–
ASO–19) and be submitted in triplicate
to DOT Docket Operations (see
ADDRESSES section for the address and
phone number). You may also submit
comments through the internet at
https://www.regulations.gov.
Persons wishing the FAA to
acknowledge receipt of their comments
on this action must submit with those
comments a self-addressed stamped
postcard on which the following
statement is made: ‘‘Comments to FAA
Docket No. FAA–2020–0701; Airspace
Docket No. 20–ASO–19’’. The postcard
will be date/time stamped and returned
to the commenter.
All communications received before
the specified closing date for comments
will be considered before taking action
on the proposed rule. The proposal
contained in this document may be
changed in light of the comments
received. All comments submitted will
be available for examination in the
public docket both before and after the
comment closing date. A report
summarizing each substantive public
contact with FAA personnel concerned
with this rulemaking will be filed in the
docket.
Availability of NPRMs
An electronic copy of this document
may be downloaded through the
internet at https://www.regulations.gov.
Recently published rulemaking
documents can also be accessed through
the FAA’s web page at https://
www.faa.gov/air_traffic/publications/
airspace_amendments/.
You may review the public docket
containing the proposal, any comments
received and any final disposition in
person in the Dockets Office (see the
ADDRESSES section for address and
phone number) between 9:00 a.m. and
5:00 p.m., Monday through Friday,
except federal holidays. An informal
docket may also be examined between
8:00 a.m. and 4:30 p.m., Monday
through Friday, except federal holidays
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Agencies
[Federal Register Volume 85, Number 175 (Wednesday, September 9, 2020)]
[Proposed Rules]
[Pages 55624-55627]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2020-19749]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2020-0700; Project Identifier AD-2020-00238-E]
RIN 2120-AA64
Airworthiness Directives; International Aero Engines AG Turbofan
Engines
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD)
2019-06-06, which applies to all International Aero Engines AG (IAE)
V2500-A1, V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5,
V2528-D5, V2530-A5, V2533-A5 model turbofan engines. AD 2019-06-06
requires initial and repetitive borescope inspections (BSIs) of the
diffuser case M-flange and, if it fails the inspection, replacement of
the diffuser case with a part eligible for installation. Since the FAA
issued AD 2019-06-06, the manufacturer performed an updated safety risk
analysis, which reduced the diffuser case M-flange inspection intervals
and added the performance of a replacement of the diffuser case M-
flange. This proposed AD would require an initial BSI of the diffuser
case M-flange and, if it fails the inspection, repetitive BSIs of the
diffuser case M-flange until replacement of the diffuser case M-flange
is performed. 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 October 26,
2020.
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
International Aero Engines AG, 400 Main Street, East Hartford, CT
06118; phone: 800-565-0140; email: [email protected]; website: https://fleetcare.pw.utc.com. You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety 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-2020-
0700; 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, 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: Nicholas Paine, Aerospace Engineer,
ECO Branch, FAA, 1200 District Avenue, Burlington, MA 01803; phone:
781-238-7742; fax: 781-238-7199; email: [email protected].
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any written relevant data, views, or
arguments about this proposed AD. Send your comments to an address
listed under the ADDRESSES section. Include ``Docket No. FAA-2020-0700;
Project Identifier AD-2020-00238-E'' at the beginning of your comments.
The most helpful comments reference a specific portion of the proposal,
explain the reason for any recommended change, and include supporting
data. The FAA will consider all comments received by the closing date
and may amend this NPRM because of those comments.
Except for Confidential Business Information as described in the
following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
https://www.regulations.gov, including any personal information you
provide. The agency will also post a report summarizing each
substantive verbal contact received about this proposal.
Confidential Business Information
Confidential Business Information (CBI) is commercial or financial
information that is both customarily and actually treated as private by
its owner. Under the Freedom of Information Act (FOIA) (5 U.S.C. 552),
CBI is exempt from public disclosure. If your comments responsive to
this NPRM contain commercial or financial information that is
customarily treated as private, that you actually treat as private, and
that is relevant or responsive to this NPRM, it is important that you
clearly designate the submitted comments as CBI. Please mark each page
of your submission containing CBI as ``PROPIN.'' The FAA will treat
such marked submissions as confidential under the FOIA, and they will
not be placed in the public docket of this NPRM. Submissions containing
CBI should be sent to Nicholas Paine,
[[Page 55625]]
Aerospace Engineer, ECO Branch, FAA, 1200 District Avenue, Burlington,
MA 01803. Any commentary that the FAA receives which is not
specifically designated as CBI will be placed in the public docket for
this rulemaking.
Background
The FAA issued AD 2019-06-06, Amendment 39-19604 (84 FR 11642,
March 28, 2019) (``AD 2019-06-06''), for all IAE V2500-A1, V2522-A5,
V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5,
V2533-A5 model turbofan engines. AD 2019-06-06 requires initial and
repetitive BSIs of the diffuser case M-flange and, if it fails the
inspection, replacement of the diffuser case with a part eligible for
installation. AD 2019-06-06 resulted from a crack found at the diffuser
case M-flange during overhaul inspection. The FAA issued AD 2019-06-06
to prevent failure of the diffuser case.
Actions Since AD 2019-06-06 Was Issued
Since the FAA issued AD 2019-06-06, the manufacturer performed an
updated safety risk analysis, which resulted in reducing the diffuser
case M-flange inspection intervals and adding the performance of a
replacement of the diffuser case M-flange, which terminates the need
for repetitive BSIs of the diffuser case M-flange.
FAA's Determination
The FAA is issuing this NPRM because the agency has determined that
the unsafe condition described previously is likely to exist or develop
in other products of the same type design.
Service Information Incorporated by Reference Under 1 CFR Part 51
The FAA reviewed IAE Non-Modification Alert Service Bulletin
(NMASB) V2500-ENG-72-A0706, Revision 2, dated November 7, 2019. IAE
NMASB V2500-ENG-72-A0706, Revision 2, describes procedures for
inspecting the diffuser case M-flange. 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.
Other Related Service Information
The FAA reviewed IAE Service Bulletin (SB) V2500-ENG-72-0709, dated
December 13, 2019. IAE SB V2500-ENG-72-0709 describes procedures for
replacing the diffuser case M-flange.
Proposed AD Requirements in This NPRM
This proposed AD would retain certain requirements of AD 2019-06-
06. This proposed AD would require an initial BSI of the diffuser case
M-flange and, if it fails the inspection, repetitive BSIs of the
diffuser case M-flange until replacement of the diffuser case M-flange
is performed.
Costs of Compliance
The FAA estimates that this AD, as proposed, would affect 1,654
engines installed on airplanes of U.S. registry.
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
----------------------------------------------------------------------------------------------------------------
BSI of diffuser case M-flange......... 2 work-hours x $85 per $0 $170 $281,180
hour = $170.
Replace the diffuser case M-flange.... 40 work-hours x $85 per 20,000 23,400 38,703,600
hour = $3,400.
----------------------------------------------------------------------------------------------------------------
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. The FAA does not control warranty coverage for
affected individuals. As a result, the FAA has included all costs in
its 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.
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.
Regulatory Findings
The FAA has 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 that the proposed
regulation:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Would not affect intrastate aviation in Alaska, and
(3) Would 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:
0
a. Removing Airworthiness Directive (AD) 2019-06-06, Amendment 39-19604
(84 FR 11642, March 28, 2019); and
0
b. Adding the following new AD:
International Aero Engines AG: Docket No. FAA-2020-0700; Project
Identifier AD-2020-00238-E.
[[Page 55626]]
(a) Comments Due Date
The FAA must receive comments on this AD action by October 26,
2020.
(b) Affected ADs
This AD replaces AD 2019-06-06, Amendment 39-19604 (84 FR 11642,
March 28, 2019).
(c) Applicability
This AD applies to all International Aero Engines AG (IAE)
V2500-A1, V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-
A5, V2528-D5, V2530-A5, and V2533-A5 model turbofan engines.
(d) Subject
Joint Aircraft System Component (JASC) Code 7250, Turbine
Section.
(e) Unsafe Condition
This AD was prompted by a crack found at the diffuser case M-
flange during overhaul inspection. The FAA is issuing this AD to
prevent failure of the diffuser case. The unsafe condition, if not
addressed, could result in uncontained diffuser case rupture, 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) Borescope Inspection of Diffuser Case M-Flange
For engines with a diffuser case assembly, part number 2A0051,
2A2081-01, 2A2581-01, 2A2883-01, 2A2885-01, 2A2889-01, 2A2891-01,
2A2896-01, 2A2897-01, or 2A3132 installed, perform an initial
borescope inspection (BSI) of zones 1, 2, and 3 of the diffuser case
M-flange as follows:
(i) For engines with a diffuser case M-flange that has 19,000 or
more cycles since new (CSN) on the effective date of this AD,
perform the BSI of the diffuser case M-flange before accumulating
the ``Inspect within (Cycles)'' in Table 1 to paragraph (g)(1) of
this AD. If the CSLFPI is unknown, use the CSN of the diffuser case
M-flange.
[GRAPHIC] [TIFF OMITTED] TP09SE20.006
(ii) For engines with a diffuser case M-flange that has fewer
than 19,000 CSN on the effective date of this AD, perform the BSI of
the diffuser case M-flange before accumulating 20,300 CSN.
(iii) For engines with a diffuser case M-flange in which the CSN
is unknown, perform the BSI of the diffuser case M-flange within 250
cycles after the effective date of this AD.
(iv) Use the Accomplishment Instructions, paragraphs 2.A.
through 2.G. of IAE Non-Modification Alert Service Bulletin (NMASB)
V2500-ENG-72-A0706, Revision 2, dated November 7, 2019 (``the
NMASB''), to perform the initial BSI.
(v) If no crack is found as a result of the inspections required
by paragraphs (g)(1)(i) through (iii) of this AD, repeat the BSI of
zones 1, 2, and 3 of the diffuser case M-flange at intervals not to
exceed 2,100 cycles since the previous BSI.
(vi) If a crack is found as a result of the inspections required
by paragraphs (g)(1)(i) through (iii) of this AD, replace the
diffuser case M-flange or repeat the BSI of zones 1, 2, and 3 of the
diffuser case M-flange as specified by either ``Table 2: Fly on
Limits'' or ``Table 4: Fly on Limits,'' in paragraph 2,
Accomplishment Instructions, of the NMASB as appropriate for the
affected the engine model.
(2) Replacement of the Diffuser Case M-Flange
(i) At the next engine shop visit after the effective date of
this AD or before the diffuser case M-flange accumulates 20,000 CSN,
whichever occurs later, replace the diffuser case M-flange.
Note 1 to paragraph (g)(2)(i): Guidance on performing the
replacement of the diffuser case M-flange can be found in the
Accomplishment Instructions, paragraphs 1.A. and B., of IAE SB
V2500-ENG-72-0709, dated December 13, 2019.
(ii) Thereafter, repeat the replacement of the diffuser case M-
flange before accumulating 20,000 cycles since the previous
replacement.
(iii) Replacement of the diffuser case M-flange is the
terminating action for the repetitive BSIs required by paragraph
(g)(1) of this AD.
(h) Installation Prohibition
After the effective date of this AD, do not install a diffuser
case onto any engine if the diffuser case M-flange has more than
20,000 CSN.
(i) Credit for Previous Actions
You may take credit for the initial BSIs that are required by
paragraphs (g)(1)(i) through (iii) of this AD, or the replacement of
the diffuser case M-flange required by paragraph (g)(2) of this AD,
if you performed those actions before the effective date of this AD
using IAE NMASB V2500-ENG-72-A0706, Revision 1, dated June 28, 2019,
or Original Issue, dated February 14, 2019; IAE V2500 Special
Instruction (SI) No. 341F-18, dated November 19, 2018; IAE V2500 SI
No. 350F-18, Rev. 1, dated December 17, 2018; IAE V2500 SI No. 356F-
18, Rev. 1, dated January 9, 2019; IAE V2500 SI No. 372F-18, dated
January 8, 2019; or IAE V2500 Special SI No. 04F-19, dated January
14, 2019.
(j) Definition
For the purpose of this AD, an ``engine shop visit'' is the
induction of the engine into the shop for maintenance involving the
separation of pairs of major mating engine flanges.
(k) 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 (l)(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
[[Page 55627]]
of the local flight standards district office/certificate holding
district office.
(l) Related Information
(1) For more information about this AD, contact Nicholas Paine,
Aerospace Engineer, ECO Branch, FAA, 1200 District Avenue,
Burlington, MA 01803; phone: 781-238-7742; fax: 781-238-7199; email:
[email protected].
(2) For service information identified in this AD, contact
International Aero Engines AG, 400 Main Street, East Hartford, CT
06118; phone: 800-565-0140; email: [email protected]; website:
https://fleetcare.pw.utc.com. You may view this referenced service
information at the FAA, Airworthiness Products Section, Operational
Safety Branch, 1200 District Avenue, Burlington, MA 01803. For
information on the availability of this material at the FAA, call
781-238-7759.
Issued on September 1, 2020.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2020-19749 Filed 9-8-20; 8:45 am]
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