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Federal Register / Vol. 86, No. 171 / Wednesday, September 8, 2021 / Proposed Rules PART 39AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:

Authority: 49 U.S.C. 106g, 40113, 44701.
39.13

Amended
2. The FAA amends 39.13 by adding the following new airworthiness directive:

Leonardo S.p.a.: Docket No. FAA2021
0720; Project Identifier 2019SW079
AD.
a Comments Due Date The FAA must receive comments on this airworthiness directive AD by October 25, 2021.
b Affected ADs None.
c Applicability This AD applies to Leonardo S.p.a. Model AW109SP helicopters, certificated in any category, with an affected part as identified in European Union Aviation Safety Agency EASA AD 20190213, dated August 29, 2019 EASA AD 20190213.
d Subject Joint Aircraft Service Component JASC
Codes: 2913, Hydraulic Pump Elect/Eng, Main.
e Unsafe Condition This AD was prompted by reports of the ineligible installation of hydraulic pump part number P/N 109076042103 on Model AW109SP helicopters resulting in the applicable instructions for continued airworthiness not being available. The FAA
is issuing this AD to address this unsafe condition. The unsafe condition, if not addressed, could result in failure of the hydraulic pump and subsequent loss of control of the helicopter.
f Compliance Comply with this AD within the compliance times specified, unless already done.

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h Exceptions to EASA AD 20190213
1 Where EASA AD 20190213 requires compliance in terms of flight hours, this AD
requires using hours time-in-service.
2 Where EASA AD 20190213 requires compliance from its effective date, this AD
requires using the effective date of this AD.
3 Where paragraph 2 of EASA AD 2019
0213 specifies to replace a part if any discrepancy is detected during the inspection, this AD requires removing that part from service.
4 Where paragraph 3 of EASA AD 2019
0213 specifies to replace a part before exceeding 1,600 flight hours since first
VerDate Sep<11>2014

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installation on a helicopter, this AD requires removing that part from service before 1600
hours time in service since first installation on a helicopter.
5 Where the service information required by EASA AD 20190213 specifies discarding the o-ring and gasket, this AD requires removing those parts from service.
6 Where the service information required by EASA AD 20190213 specifies recording compliance with the service bulletin in the helicopter logbook, this AD does not include that requirement.
7 This AD does not require the Remarks section of EASA AD 20190213.

Issued on August 26, 2021.
Gaetano A. Sciortino, Deputy Director for Strategic Initiatives, Compliance & Airworthiness Division, Aircraft Certification Service.

i No Reporting Requirement
Docket No. FAA20210725; Project Identifier MCAI202001402T

Although the service information referenced in EASA AD 20190213 specifies to submit certain information to the manufacturer, this AD does not include that requirement.
j Special Flight Permit
k Alternative Methods of Compliance AMOCs 1 The Manager, International Validation 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 International Validation Branch, send it to the attention of the person identified in paragraph l2 of this AD.
Information may be emailed to: 9-AVS-AIR730-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.
1 For EASA AD 20190213, contact EASA, Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221 8999
000; email ADs@easa.europa.eu; internet www.easa.europa.eu. You may find this EASA AD on the EASA website at https
ad.easa.europa.eu. You may view this material at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N321, Fort Worth, TX 76177.
For information on the availability of this material at the FAA, call 817 2225110.
This material may be found in the AD docket at https www.regulations.gov by searching for and locating Docket No. FAA20210720.
2 For more information about this AD, contact Darren Gassetto, Aerospace Engineer, COS Program Management Section, Operational Safety Branch, Compliance &
Airworthiness Division, FAA, 1600 Stewart Ave., Suite 410, Westbury, NY 11590;
telephone 516 2287323; email Darren.Gassetto@faa.gov.

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FR Doc. 202119254 Filed 9721; 8:45 am BILLING CODE 491013P

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 39

RIN 2120AA64

Airworthiness Directives; Bombardier, Inc., Airplanes Federal Aviation Administration FAA, DOT.
ACTION: Notice of proposed rulemaking NPRM.
AGENCY:

Special flight permits, as described in 14
CFR 21.197 and 21.199, are prohibited.

l Related Information
g Requirements Except as specified in paragraph h of this AD: Comply with all required actions and compliance times specified in, and in accordance with, EASA AD 20190213.

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The FAA proposes to supersede Airworthiness Directive AD
20172206, which applies to certain Bombardier, Inc., Model CL6002B16
6013A, 6013R, and 604 Variants airplanes. AD 20172206 requires repetitive inspections for fuel leakage at the engine and auxiliary power unit APU fuel pumps, and related investigative and corrective actions if necessary. Since the FAA issued AD
20172206, terminating actions have been developed and additional airplanes have been determined to be affected by the unsafe condition. This proposed AD would retain the requirements of AD 20172206, and require an inspection of the APU, repair if necessary, and modification of the engine electrical fuel pump EFP
installation. This proposed AD would also add airplanes to the applicability.
The FAA is proposing this AD to address the unsafe condition on these products.

SUMMARY:

The FAA must receive comments on this proposed AD by October 25, 2021.

DATES:

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: 2024932251.
Mail: U.S. Department of Transportation, Docket Operations, M
30, West Building Ground Floor, Room W12140, 1200 New Jersey Avenue SE, Washington, DC 20590.

ADDRESSES:

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