Document ID: FAA-2019-0393-0001
Agency: faa
Document Type: Rule
Title: Airworthiness Directives: International Aero Engines Turbofan Engines
Posted Date: 2019-06-13T04:00Z

[Federal Register Volume 84, Number 114 (Thursday, June 13, 2019)]
[Rules and Regulations]
[Pages 27511-27513]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2019-12360]

[[Page 27511]]

-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2019-0393; Product Identifier 2019-NE-14-AD; Amendment 
39-19654; AD 2019-11-08]
RIN 2120-AA64

Airworthiness Directives; International Aero Engines Turbofan 
Engines

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; request for comments.

-----------------------------------------------------------------------

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all 
International Aero Engines, LLC (IAE) PW1133G-JM, PW1133GA-JM, PW1130G-
JM, PW1129G-JM, PW1127G-JM, PW1127GA-JM, PW1127G1-JM, PW1124G-JM, 
PW1124G1-JM, and PW1122G-JM model turbofan engines. This AD requires 
the removal of the main gearbox (MGB) assembly and electronic engine 
control (EEC) software and the installation of a part and software 
version eligible for installation. This AD was prompted by multiple 
reports of in-flight engine shutdowns (IFSDs) as the result of high-
cycle fatigue causing fracture of certain parts of the MGB assembly. 
The FAA is issuing this AD to address the unsafe condition on these 
products.

DATES: This AD is effective June 28, 2019.
    The FAA must receive comments on this AD by July 29, 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: U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue SE, Washington, DC 20590, between 9 a.m. and 5 p.m., 
Monday through Friday, except Federal holidays.
    For service information identified in this final rule, contact 
International Aero Engines, LLC, 400 Main Street, East Hartford, CT 
06118; phone: 800-565-0140; email: help24@pw.utc.com; 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. It is also available on the 
internet at http://www.regulations.gov by searching for and locating 
Docket No. FAA-2019-0393.

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-
0393; 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 final rule, the regulatory evaluation, any comments received, and 
other information. The street address for the Docket Operations is 
listed above. Comments will be available in the AD docket shortly after 
receipt.

FOR FURTHER INFORMATION CONTACT: Kevin M. Clark, Aerospace Engineer, 
ECO Branch, FAA, 1200 District Avenue, Burlington, MA 01803; phone: 
781-238-7088; fax: 781-238-7199; email: kevin.m.clark@faa.gov.

SUPPLEMENTARY INFORMATION:

Discussion

    The FAA learned of 13 IFSD events on certain IAE PW1100G-JM model 
turbofan engines beginning in October, 2018. After further analysis, 
IAE determined that the integrated drive generator (IDG) oil pump drive 
gearshaft assembly in the MGB assembly fractured during engine 
operation as a result of high-cycle fatigue. In response, IAE 
subsequently redesigned the IDG oil pump drive gearshaft assembly in 
the MGB assembly with an axially thicker gear web, a radially thicker 
gear rim, and an improved tooth tip relief to improve MGB assembly 
durability and reliability. IAE also redesigned the EEC software to 
restrict engine operation to certain parameters. This condition, if not 
addressed, could result in failure of one or more engines, loss of 
thrust control, and loss of the airplane. The FAA is issuing this AD to 
address the unsafe condition on these products.

Related Service Information

    The FAA reviewed PW Service Bulletin (SB) PW1000G-C-72-00-0129-00A-
930A-D, Original Issue, dated April 18, 2019, and PW SB PW1000G-C-73-
00-0037-00A-930A-D, Original Issue, dated May 28, 2019. PW SB PW1000G-
C-72-00-0129-00A-930A-D, Original Issue, dated April 18, 2019, 
describes procedures for replacing the IDG oil pump drive gearshaft 
assembly in the MGB assembly. PW SB PW1000G-C-73-00-0037-00A-930A-D, 
Original Issue, dated May 28, 2019, describes procedures for replacing 
the EEC software to incorporate FCS 5.0 software.

FAA's Determination

    The FAA is issuing 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.

AD Requirements

    This AD requires the removal of the MGB assembly and EEC software 
and the installation parts and software versions eligible for 
installation.

Interim Action

    These actions are interim actions, and the FAA may do additional 
rulemaking in the future for removal and replacement of the MGB 
assembly on the engines that do not operate on 180-minute or 120-minute 
extended operations (ETOPS) flights.

FAA's Justification and Determination of the Effective Date

    An unsafe condition exists that requires the immediate adoption of 
this AD without providing an opportunity for public comments prior to 
adoption. The FAA has found that the risk to the flying public 
justifies waiving notice and comment prior to adoption of this rule. 
Multiple IAE PW1100G-JM model turbofan engines experienced MGB assembly 
failures recently, which resulted in IFSDs. The MGB assemblies must be 
removed for ETOPS operators within 90 or 120 days after the effective 
date of this AD, depending on the length of the operator's ETOPS 
flights, to ensure the MGB assemblies are replaced before fractures 
develop that could result in the failure of both MGB assemblies and a 
dual IFSD event. Therefore, the FAA finds good cause that notice and 
opportunity for prior public comment are impracticable. In addition, 
for the reason stated above, the FAA finds that good cause exists for 
making this amendment effective in less than 30 days.

Comments Invited

    This AD is a final rule that involves requirements affecting flight 
safety and was not preceded by notice and an opportunity for public 
comment. However, the FAA invites you to send any written data, views, 
or arguments about this final rule. Send your

[[Page 27512]]

comments to an address listed under the ADDRESSES section. Include the 
docket number FAA-2019-0393 and Product Identifier 2019-NE-14-AD at the 
beginning of your comments. The FAA specifically invites comments on 
the overall regulatory, economic, environmental, and energy aspects of 
this final rule. The FAA will consider all comments received by the 
closing date and may amend this final rule because of those comments.
    The FAA will post all comments received, without change, to http://www.regulations.gov, including any personal information you provide. 
The FAA will also post a report summarizing each substantive verbal 
contact received about this final rule.

Regulatory Flexibility Act

    The requirements of the Regulatory Flexibility Act (RFA) do not 
apply when an agency finds good cause pursuant to 5 U.S.C. 553 to adopt 
a rule without prior notice and comment. Because the FAA has determined 
that it has good cause to adopt this rule without notice and comment, 
RFA analysis is not required.

Costs of Compliance

    The FAA estimates that this AD affects 72 engines installed on 
airplanes of U.S. registry.
    The FAA estimates the following costs to comply with this AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                     Cost per      Cost on U.S.
                Action                         Labor cost           Parts cost        product        operators
----------------------------------------------------------------------------------------------------------------
Replace the MGB assembly..............  13 work-hours x $85 per          $75,000         $76,105      $5,479,560
                                         hour = $1,105.
Replace the EEC software..............  3 work-hours x $85 per                 0             255          18,360
                                         hour = $255.
----------------------------------------------------------------------------------------------------------------

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.

Regulatory Findings

    This AD will not have federalism implications under Executive Order 
13132. This AD will not have a substantial direct effect on the States, 
on the relationship between the national government and the States, or 
on the distribution of power and responsibilities among the various 
levels of government.
    For the reasons discussed above, I certify that this AD:
    (1) Is not a ``significant regulatory action'' under Executive 
Order 12866, and
    (2) Will not affect intrastate aviation in Alaska.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by 
reference, Safety.

Adoption of the Amendment

    Accordingly, under the authority delegated to me by the 
Administrator, the FAA amends 14 CFR part 39 as follows:

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):

2019-11-08 International Aero Engines: Amendment 39-19654; Docket 
No. FAA-2019-0393; Product Identifier 2019-NE-14-AD.

(a) Effective Date

    This AD is effective June 28, 2019.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to all International Aero Engines, LLC (IAE) 
PW1133G-JM, PW1133GA-JM, PW1130G-JM, PW1129G-JM, PW1127G-JM, 
PW1127GA-JM, PW1127G1-JM, PW1124G-JM, PW1124G1-JM, and PW1122G-JM 
model turbofan engines.

(d) Subject

    Joint Aircraft System Component (JASC) Code 7260, Turbine Engine 
Accessory Drive.

(e) Unsafe Condition

    This AD was prompted by multiple reports of in-flight engine 
shutdowns as the result of high-cycle fatigue causing fracture of 
certain parts of the main gearbox (MGB) assembly. The FAA is issuing 
this AD to prevent failure of the MGB assembly. The unsafe 
condition, if not addressed, could result in failure of one or more 
engines, loss of thrust control, and loss of the airplane.

(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

(g) Required Actions

    (1) Remove the MGB assembly, part number (P/N) 5322505, and 
install a part eligible for installation as follows:
    (i) For engines that operate on 180-minute extended operations 
(ETOPS) flights, within 90 days from the effective date of this AD;
    (ii) For engines that operate on 120-minute ETOPS flights, 
within 120 days from the effective date of this AD.
    (2) For engines with MGB assembly P/N 5322505, within 120 days 
from the effective date of this AD, remove electronic engine control 
(EEC) software earlier than FCS 5.0 from the engine and load EEC 
software that is eligible for installation.

(h) Installation Prohibition

    (1) After the effective date of this AD, do not install 
integrated drive generator (IDG) oil pump drive gearshaft assembly, 
P/N 5322630-01, into an MGB assembly.
    (2) After the effective date of this AD, do not load EEC 
software earlier than FCS 5.0 on any engine identified in paragraph 
(c) of this AD with an MGB assembly, P/N 5322505.

[[Page 27513]]

(i) Definitions

    (1) For the purpose of this AD, a ``part eligible for 
installation'' is an MGB assembly with an IDG oil pump drive 
gearshaft assembly other than P/N 5322630-01.
    (2) For the purpose of this AD, ``EEC software that is eligible 
for installation'' is EEC software FCS 5.0 and later.

(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) 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

    For more information about this AD, contact Kevin M. Clark, 
Aerospace Engineer, ECO Branch, FAA, 1200 District Avenue, 
Burlington, MA 01803; phone: 781-238-7088; fax: 781-238-7199; email: 
kevin.m.clark@faa.gov.

(l) Material Incorporated by Reference

    None.

    Issued in Burlington, Massachusetts, on June 6, 2019.
Robert J. Ganley,
Manager, Engine & Propeller Standards Branch, Aircraft Certification 
Service.
[FR Doc. 2019-12360 Filed 6-12-19; 8:45 am]
 BILLING CODE 4910-13-P