83_FR_4631 83 FR 4609 - Airworthiness Directives; Rolls-Royce Corporation Turboshaft Engines

83 FR 4609 - Airworthiness Directives; Rolls-Royce Corporation Turboshaft Engines

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration

Federal Register Volume 83, Issue 22 (February 1, 2018)

Page Range4609-4610
FR Document2018-01900

We propose to adopt a new airworthiness directive (AD) for certain Rolls-Royce Corporation (RRC) model 250-C turboshaft engines. This proposed AD was prompted by several reports of engine power loss, one of which resulted in a fatal helicopter accident. This proposed AD would require removal of the bearing assembly, part number (P/N) 2544198, in the power turbine governor (PTG) and its replacement with a bearing assembly eligible for installation. We are proposing this AD to address the unsafe condition on these products.

Federal Register, Volume 83 Issue 22 (Thursday, February 1, 2018) 
[Federal Register Volume 83, Number 22 (Thursday, February 1, 2018)]
[Proposed Rules]
[Pages 4609-4610]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2018-01900]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2017-1118; Product Identifier 2017-NE-40-AD]
RIN 2120-AA64


Airworthiness Directives; Rolls-Royce Corporation Turboshaft 
Engines

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: We propose to adopt a new airworthiness directive (AD) for 
certain Rolls-Royce Corporation (RRC) model 250-C turboshaft engines. 
This proposed AD was prompted by several reports of engine power loss, 
one of which resulted in a fatal helicopter accident. This proposed AD 
would require removal of the bearing assembly, part number (P/N) 
2544198, in the power turbine governor (PTG) and its replacement with a 
bearing assembly 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 March 19, 2018.

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 Rolls-
Royce Corporation, 450 South Meridian Street, Mail Code NB-02-05, 
Indianapolis, IN 46225; phone: 317-230-3774; email: 
royce.com">indy.pubs.services@rolls-royce.com; internet: www.rolls-royce.com. You 
may view this service information at the FAA, Engine and Propeller 
Standards Branch, 1200 District Avenue, Burlington, MA. 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-2017-
1118; 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 in the ADDRESSES section. Comments will be available in the AD 
docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: John Tallarovic, Aerospace Engineer, 
Chicago ACO Branch, FAA, 2300 E. Devon Ave., Des Plaines, IL 60018; 
phone: 847-294-8180; fax: 847-294-7834; 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-2017-1118; 
Product Identifier 2017-NE-40-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 were prompted to issue this NPRM based upon several reports of 
loss of engine power on certain RRC model 250-C turboshaft engines 
installed on single-engine helicopters. One of these instances of power 
loss resulted in a fatal helicopter accident on May 4, 2016.
    During the course of the investigation of the 2016 fatal accident, 
RRC determined that the root cause of this engine power loss was the 
failure of the bearing assembly, P/N 2544198, in the PTG, due to lack 
of lubrication. Although RRC had issued a service bulletin in 2009 to 
address the failure of this bearing assembly, our risk assessment had 
not supported issuance of an AD at that time. Based on more recent 
service experience, and the fatal accident in 2016, we are now 
proposing an AD to remove the affected bearing assembly in the PTG and 
replace it with a bearing assembly with a new design. This condition, 
if not addressed, could result in failure of the PTG, failure of the 
engine, in-flight shutdown, and forced autorotation landing or 
accident.

Related Service Information

    We reviewed Rolls-Royce Corporation Commercial Engine Bulletin 
(CEB) 1402, Revision 2, dated February 4, 2009. The CEB provides 
guidance on replacing the P/N 2544198 bearing assembly in the PTG with 
a bearing assembly eligible for installation.

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 of the affected bearing 
assembly in the PTG and its replacement with a bearing assembly 
eligible for installation.

Costs of Compliance

    We estimate that this proposed AD affects 2,928 engines installed 
on airplanes of U.S. registry.
    We estimate the following costs to comply with this proposed AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                     Cost per      Cost on U.S.
                Action                         Labor cost           Parts cost        product        operators
----------------------------------------------------------------------------------------------------------------
Remove and replace PTG bearing          8 work-hours x $85 per            $1,700          $2,380      $6,968,640
 assembly.                               hour = $680.
----------------------------------------------------------------------------------------------------------------


[[Page 4610]]

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):

Roll-Royce Corporation (Type Certificate previously held by Allison 
Engine Company): Docket No. FAA-2017-1118; Product Identifier 2017-
NE-40-AD.

(a) Comments Due Date

    We must receive comments by March 19, 2018.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Rolls-Royce Corporation (RRC) model 250-C10D, 
250-C18, 250-C18A, 250-C18B, 250-C18C, 250-C19, 250-C20, 250-C20B, 
250-C20C, 250-C20F, 250-C20J, 250-C20R, 250-C20R/1, 250-C20R/2, 250-
C20R/4, 250-C20S, 250-C20W, 250-C28, 250-C28B, 250-C28C, 250-C30, 
250-C30G, 250-C30G/2, 250-C30M, 250-C30P, 250-C30S, and 250-C30U 
turboshaft engines.

(d) Subject

    Joint Aircraft System Component (JASC) Code 7323, Turbine 
Governor.

(e) Unsafe Condition

    This AD was prompted by several reports of loss of power, one of 
which resulted in a fatal helicopter accident. We are issuing this 
AD to prevent failure of the bearing assembly in the power turbine 
governor (PTG). The unsafe condition, if not addressed, could result 
in failure of the PTG, failure of the engine, in-flight shutdown, 
and forced autorotation landing or accident.

(f) Compliance

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

(g) Required Actions

    (1) Remove the bearing assembly, part number 2544198, from the 
PTG in accordance with the compliance times in Figure 1 to paragraph 
(g) of this AD, or within 90 days after the effective date of this 
AD, whichever occurs later.

               Figure 1 to Paragraph (g)--Compliance Times
------------------------------------------------------------------------
 PTG operational hours (time since new/
        time since last overhaul)                 Compliance time
------------------------------------------------------------------------
0 to 750................................  Not later than 750 hours.
751 to 1000.............................  Not later than 1,000 hours.
1001 to 1250............................  Not later than 1,250 hours.
1251 to 1500............................  Not later than 1,500 hours.
1501 or greater.........................  At the next removal of the PTG
                                           for any reason.
------------------------------------------------------------------------

    (2) After such removal, replace the affected bearing assembly in 
the PTG with a part eligible for installation before further flight.

(h) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, Chicago 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 Chicago ACO Branch, send it to the attention of the 
person identified in paragraph (i)(1) of this AD.
    (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.

(i) Related Information

    (1) For more information about this AD, contact John Tallarovic, 
Aerospace Engineer, Chicago ACO Branch, FAA, 2300 E Devon Ave., Des 
Plaines, IL 60018; phone: 847-294-8180; fax: 847-294-7834; email: 
[email protected].
    (2) For service information identified in this AD, contact 
Rolls-Royce Corporation, 450 South Meridian Street, Mail Code NB-02-
05, Indianapolis, IN 46225; phone: 317-230-3774; email: 
royce.com">indy.pubs.services@rolls-royce.com; internet: www.rolls-royce.com. 
You may view this referenced 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 January 25, 2018.
Robert J. Ganley,
Manager, Engine and Propeller Standards Branch, Aircraft Certification 
Service.
[FR Doc. 2018-01900 Filed 1-31-18; 8:45 am]
 BILLING CODE 4910-13-P

Federal Register / Vol. 83, No. 22 / Thursday, February 1, 2018 / Proposed Rules 4609 Issued in Kansas City, Missouri, on January For service information identified in Discussion 24, 2018. this NPRM, contact Rolls-Royce Pat Mullen, We were prompted to issue this Corporation, 450 South Meridian Street, NPRM based upon several reports of Acting Deputy Director, Policy & Innovation Mail Code NB–02–05, Indianapolis, IN Division, Aircraft Certification Service. loss of engine power on certain RRC 46225; phone: 317–230–3774; email: model 250–C turboshaft engines [FR Doc. 2018–01923 Filed 1–31–18; 8:45 am] indy.pubs.services@rolls-royce.com; installed on single-engine helicopters. BILLING CODE 4910–13–P internet: www.rolls-royce.com. You may One of these instances of power loss view this service information at the resulted in a fatal helicopter accident on FAA, Engine and Propeller Standards May 4, 2016. DEPARTMENT OF TRANSPORTATION Branch, 1200 District Avenue, During the course of the investigation Burlington, MA. For information on the Federal Aviation Administration of the 2016 fatal accident, RRC availability of this material at the FAA, determined that the root cause of this call 781–238–7759. 14 CFR Part 39 engine power loss was the failure of the Examining the AD Docket bearing assembly, P/N 2544198, in the [Docket No. FAA–2017–1118; Product PTG, due to lack of lubrication. Identifier 2017–NE–40–AD] You may examine the AD docket on the internet at http:// Although RRC had issued a service RIN 2120–AA64 www.regulations.gov by searching for bulletin in 2009 to address the failure of and locating Docket No. FAA–2017– this bearing assembly, our risk Airworthiness Directives; Rolls-Royce assessment had not supported issuance 1118; or in person at Docket Operations Corporation Turboshaft Engines of an AD at that time. Based on more between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. recent service experience, and the fatal AGENCY: Federal Aviation accident in 2016, we are now proposing Administration (FAA), DOT. The AD docket contains this NPRM, the regulatory evaluation, any comments an AD to remove the affected bearing ACTION: Notice of proposed rulemaking assembly in the PTG and replace it with (NPRM). received, and other information. The street address for Docket Operations a bearing assembly with a new design. (phone: 800–647–5527) is in the This condition, if not addressed, could SUMMARY: We propose to adopt a new ADDRESSES section. Comments will be result in failure of the PTG, failure of airworthiness directive (AD) for certain available in the AD docket shortly after the engine, in-flight shutdown, and Rolls-Royce Corporation (RRC) model receipt. forced autorotation landing or accident. 250–C turboshaft engines. This proposed AD was prompted by several FOR FURTHER INFORMATION CONTACT: John Related Service Information reports of engine power loss, one of Tallarovic, Aerospace Engineer, Chicago We reviewed Rolls-Royce Corporation which resulted in a fatal helicopter ACO Branch, FAA, 2300 E. Devon Ave., Commercial Engine Bulletin (CEB) 1402, accident. This proposed AD would Des Plaines, IL 60018; phone: 847–294– Revision 2, dated February 4, 2009. The require removal of the bearing assembly, 8180; fax: 847–294–7834; email: CEB provides guidance on replacing the part number (P/N) 2544198, in the john.tallarovic@faa.gov. P/N 2544198 bearing assembly in the power turbine governor (PTG) and its SUPPLEMENTARY INFORMATION: PTG with a bearing assembly eligible for replacement with a bearing assembly installation. eligible for installation. We are Comments Invited proposing this AD to address the unsafe We invite you to send any written FAA’s Determination condition on these products. relevant data, views, or arguments about We are proposing this AD because we DATES: We must receive comments on this proposal. Send your comments to evaluated all the relevant information this proposed AD by March 19, 2018. an address listed under the ADDRESSES and determined the unsafe condition ADDRESSES: You may send comments, section. Include ‘‘Docket No. FAA– described previously is likely to exist or using the procedures found in 14 CFR 2017–1118; Product Identifier 2017– develop in other products of the same 11.43 and 11.45, by any of the following NE–40–AD’’ at the beginning of your type design. methods: comments. We specifically invite Proposed AD Requirements • Federal eRulemaking Portal: Go to comments on the overall regulatory, http://www.regulations.gov. Follow the economic, environmental, and energy This proposed AD would require instructions for submitting comments. aspects of this NPRM. We will consider removal of the affected bearing assembly • Fax: 202–493–2251. all comments received by the closing in the PTG and its replacement with a • Mail: U.S. Department of date and may amend this NPRM bearing assembly eligible for Transportation, Docket Operations, because of those comments. installation. M–30, West Building Ground Floor, We will post all comments we Costs of Compliance Room W12–140, 1200 New Jersey receive, without change, to http:// Avenue SE, Washington, DC 20590. www.regulations.gov, including any We estimate that this proposed AD • Hand Delivery: Deliver to Mail personal information you provide. We affects 2,928 engines installed on address above between 9 a.m. and 5 will also post a report summarizing each airplanes of U.S. registry. p.m., Monday through Friday, except substantive verbal contact we receive We estimate the following costs to Federal holidays. about this NPRM. comply with this proposed AD: daltland on DSKBBV9HB2PROD with PROPOSALS ESTIMATED COSTS Cost per Cost on U.S. Action Labor cost Parts cost product operators Remove and replace PTG bearing assembly 8 work-hours × $85 per hour = $680 ............. $1,700 $2,380 $6,968,640 VerDate Sep<11>2014 16:25 Jan 31, 2018 Jkt 244001 PO 00000 Frm 00005 Fmt 4702 Sfmt 4702 E:\FR\FM\01FEP1.SGM 01FEP1

4610 Federal Register / Vol. 83, No. 22 / Thursday, February 1, 2018 / Proposed Rules Authority for This Rulemaking List of Subjects in 14 CFR Part 39 FIGURE 1 TO PARAGRAPH (g)— Air transportation, Aircraft, Aviation COMPLIANCE TIMES Title 49 of the United States Code specifies the FAA’s authority to issue safety, Incorporation by reference, PTG operational hours rules on aviation safety. Subtitle I, Safety. (time since new/time Compliance time since last overhaul) section 106, describes the authority of The Proposed Amendment the FAA Administrator. Subtitle VII: 0 to 750 ....................... Not later than 750 hours. Aviation Programs, describes in more Accordingly, under the authority 751 to 1000 ................. Not later than 1,000 hours. detail the scope of the Agency’s delegated to me by the Administrator, 1001 to 1250 ............... Not later than 1,250 hours. authority. the FAA proposes to amend 14 CFR part 1251 to 1500 ............... Not later than 1,500 hours. We are issuing this rulemaking under 39 as follows: 1501 or greater ............ At the next removal of the PTG for any reason. the authority described in Subtitle VII, PART 39—AIRWORTHINESS Part A, Subpart III, Section 44701: DIRECTIVES (2) After such removal, replace the affected ‘‘General requirements.’’ Under that bearing assembly in the PTG with a part section, Congress charges the FAA with ■ 1. The authority citation for part 39 eligible for installation before further flight. promoting safe flight of civil aircraft in continues to read as follows: (h) Alternative Methods of Compliance air commerce by prescribing regulations Authority: 49 U.S.C. 106(g), 40113, 44701. (AMOCs) for practices, methods, and procedures the Administrator finds necessary for (1) The Manager, Chicago ACO Branch, § 39.13 [Amended] safety in air commerce. This regulation FAA, has the authority to approve AMOCs is within the scope of that authority ■ 2. The FAA amends § 39.13 by adding for this AD, if requested using the procedures because it addresses an unsafe condition the following new airworthiness found in 14 CFR 39.19. In accordance with that is likely to exist or develop on directive (AD): 14 CFR 39.19, send your request to your products identified in this rulemaking Roll-Royce Corporation (Type Certificate principal inspector or local Flight Standards action. previously held by Allison Engine District Office, as appropriate. If sending Company): Docket No. FAA–2017–1118; information directly to the manager of the This AD is issued in accordance with Product Identifier 2017–NE–40–AD. Chicago ACO Branch, send it to the attention authority delegated by the Executive of the person identified in paragraph (i)(1) of Director, Aircraft Certification Service, (a) Comments Due Date this AD. as authorized by FAA Order 8000.51C. We must receive comments by March 19, (2) Before using any approved AMOC, In accordance with that order, issuance 2018. notify your appropriate principal inspector, of ADs is normally a function of the (b) Affected ADs or lacking a principal inspector, the manager Compliance and Airworthiness None. of the local flight standards district office/ Division, but during this transition certificate holding district office. period, the Executive Director has (c) Applicability delegated the authority to issue ADs This AD applies to Rolls-Royce (i) Related Information applicable to engines, propellers, and Corporation (RRC) model 250–C10D, 250– (1) For more information about this AD, associated appliances to the Manager, C18, 250–C18A, 250–C18B, 250–C18C, 250– contact John Tallarovic, Aerospace Engineer, Engine and Propeller Standards Branch, C19, 250–C20, 250–C20B, 250–C20C, 250– Chicago ACO Branch, FAA, 2300 E Devon C20F, 250–C20J, 250–C20R, 250–C20R/1, Ave., Des Plaines, IL 60018; phone: 847–294– Policy and Innovation Division. 250–C20R/2, 250–C20R/4, 250–C20S, 250– 8180; fax: 847–294–7834; email: Regulatory Findings C20W, 250–C28, 250–C28B, 250–C28C, 250– john.tallarovic@faa.gov. C30, 250–C30G, 250–C30G/2, 250–C30M, 250–C30P, 250–C30S, and 250–C30U (2) For service information identified in We determined that this proposed AD turboshaft engines. this AD, contact Rolls-Royce Corporation, would not have federalism implications 450 South Meridian Street, Mail Code NB– under Executive Order 13132. This (d) Subject 02–05, Indianapolis, IN 46225; phone: 317– proposed AD would not have a Joint Aircraft System Component (JASC) 230–3774; email: indy.pubs.services@rolls- substantial direct effect on the States, on Code 7323, Turbine Governor. royce.com; internet: www.rolls-royce.com. the relationship between the national You may view this referenced service Government and the States, or on the (e) Unsafe Condition information at the FAA, Engine and Propeller distribution of power and This AD was prompted by several reports Standards Branch, 1200 District Avenue, responsibilities among the various of loss of power, one of which resulted in a fatal helicopter accident. We are issuing this Burlington, MA 01803. For information on levels of government. the availability of this material at the FAA, AD to prevent failure of the bearing assembly For the reasons discussed above, I in the power turbine governor (PTG). The call 781–238–7759. certify this proposed regulation: unsafe condition, if not addressed, could Issued in Burlington, Massachusetts, on (1) Is not a ‘‘significant regulatory result in failure of the PTG, failure of the January 25, 2018. engine, in-flight shutdown, and forced action’’ under Executive Order 12866, Robert J. Ganley, autorotation landing or accident. (2) Is not a ‘‘significant rule’’ under Manager, Engine and Propeller Standards (f) Compliance the DOT Regulatory Policies and Branch, Aircraft Certification Service. Procedures (44 FR 11034, February 26, Comply with this AD within the [FR Doc. 2018–01900 Filed 1–31–18; 8:45 am] 1979), compliance times specified, unless already daltland on DSKBBV9HB2PROD with PROPOSALS done. BILLING CODE 4910–13–P (3) Will not affect intrastate aviation in Alaska, and (g) Required Actions (1) Remove the bearing assembly, part (4) Will not have a significant number 2544198, from the PTG in economic impact, positive or negative, accordance with the compliance times in on a substantial number of small entities Figure 1 to paragraph (g) of this AD, or under the criteria of the Regulatory within 90 days after the effective date of this Flexibility Act. AD, whichever occurs later. VerDate Sep<11>2014 16:25 Jan 31, 2018 Jkt 244001 PO 00000 Frm 00006 Fmt 4702 Sfmt 9990 E:\FR\FM\01FEP1.SGM 01FEP1


Document Created: 2018-10-26 13:47:39
Document Modified: 2018-10-26 13:47:39
CategoryRegulatory Information
CollectionFederal Register
sudoc ClassAE 2.7:
GS 4.107:
AE 2.106:
PublisherOffice of the Federal Register, National Archives and Records Administration
SectionProposed Rules
ActionNotice of proposed rulemaking (NPRM).
DatesWe must receive comments on this proposed AD by March 19, 2018.
ContactJohn Tallarovic, Aerospace Engineer, Chicago ACO Branch, FAA, 2300 E. Devon Ave., Des Plaines, IL 60018; phone: 847-294-8180; fax: 847-294-7834; email: [email protected]
FR Citation83 FR 4609 
RIN Number2120-AA64
CFR AssociatedAir Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety
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