[Federal Register Volume 84, Number 97 (Monday, May 20, 2019)]
[Proposed Rules]
[Pages 22743-22744]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2019-10232]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2019-0268; Product Identifier 2019-NE-08-AD]
RIN 2120-AA64
Airworthiness Directives; International Aero Engines AG Turbofan
Engines
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: We propose to adopt a new airworthiness directive (AD) for
certain International Aero Engines AG (IAE) V2500 model turbofan
engines. This proposed AD was prompted by an inspection that determined
that material anomalies exist in certain low-pressure turbine (LPT)
stage 6 disks. This proposed AD would require removal from service of
the affected LPT stage 6 disks and their replacement with a part
eligible for installation. We are proposing this AD to address the
unsafe condition on these products.
DATES: We must receive comments on this proposed AD by July 5, 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 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
International Aero Engines AG, 400 Main Street, East Hartford, CT
06118; phone: 800-565-0140; email: [email protected]; internet: http://fleetcare.pw.utc.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.
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-2019-
0268; 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 (phone: 800-647-
5527) is listed above. Comments will be available in the AD docket
shortly after receipt.
FOR FURTHER INFORMATION CONTACT: Scott Hopper, Aerospace Engineer, ECO
Branch, FAA, 1200 District Avenue, Burlington, MA 01803; phone: 781-
238-7154; fax: 781-238-7199; email: [email protected].
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite 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-2019-0268;
Product Identifier 2019-NE-08-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 based on an inspection of material anomalies in
certain LPT stage 6 disks. A manufacturer produced 18 V2500 LPT stage 6
disks from ATI, a supplier of material ingots, in late 2017. Six of
those disks were rejected prior to shipment by MTU Aero Engines, a disk
supplier, for melt defects at final inspection. The other twelve disks
that initially passed inspection are now considered suspect. Four disk
were recovered and quarantined prior to entering into service. This AD
addresses the eight remaining affected disks. The material anomaly may
reduce the life of the LPT stage 6 disks; therefore, all affected disks
must be removed from service within the times specified in this AD.
This condition, if not addressed, could result in failure of the LPT,
uncontained release of the LPT stage 6 disk, damage to the engine, and
damage to the airplane.
Related Service Information
We reviewed IAE Alert Service Bulletin (ASB) V2500-ENG-72-A0697,
Revision No. 1, dated November 27, 2018. The ASB describes procedures
for removal of the affected LPT stage 6 disks.
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 removal and replacement of the
affected LPT stage 6 disks.
Costs of Compliance
We estimate that this proposed AD affects 1 engine installed on
airplanes of U.S. registry.
We estimate the following costs to comply with this proposed AD:
[[Page 22744]]
Estimated Costs
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Cost per Cost on U.S.
Action Labor cost Parts cost product operators
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Replace the disk...................... 130 work-hours x $85 per $155,560 $166,610 $166,610
hour = $11,050.
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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.
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.
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.
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):
International Aero Engines AG: Docket No. FAA-2019-0268; Product
Identifier 2019-NE-08-AD.
(a) Comments Due Date
We must receive comments by July 5, 2019.
(b) Affected ADs
None.
(c) Applicability
This AD applies to International Aero Engines AG (IAE) V2522-A5,
V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, and V2533-A5
model turbofan engines with the following engine serial numbers:
V10631, V12329, V12494, V13107, V18679, V18681, V18684, and V18690.
(d) Subject
Joint Aircraft System Component (JASC) Code 7250, Turbine
Section.
(e) Unsafe Condition
This AD was prompted by an inspection that determined that
material anomalies exist in certain low-pressure turbine (LPT) stage
6 disks. We are issuing this AD to prevent failure of the LPT stage
6 disk. The unsafe condition, if not addressed, could result in
uncontained release of the LPT stage 6 disk, 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
At the next piece part exposure after the effective date of this
AD, but not to exceed 5,000 cycles from new, remove from service LPT
stage 6 disks, part number 3A2996, and with any of the following
serial numbers: MAP04258; MAP04259; MAP04260, MAP04430, MAP04431,
MAP08718, MAP08719; and MAP08721. Replace the affected LPT stage 6
disk with a part eligible for installation.
(h) Definition
For the purpose of this AD, piece-part exposure is when the LPT
stage 6 disk is removed from the engine and completely disassembled.
(i) Alternative Methods of Compliance (AMOCs)
(1) The Manager, ECO, 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)(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.
(j) Related Information
(1) For more information about this AD, contact Scott Hopper,
Aerospace Engineer, ECO Branch, FAA, 1200 District Avenue,
Burlington, MA 01803; phone: 781-238-7154; 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]; internet:
http://fleetcare.pw.utc.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.
Issued in Burlington, Massachusetts, on May 13, 2019.
Robert J. Ganley,
Manager, Engine and Propeller Standards Branch, Aircraft Certification
Service.
[FR Doc. 2019-10232 Filed 5-17-19; 8:45 am]
BILLING CODE 4910-13-P