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2021-13-13 LEONARDO S.P.A.: Amendment 39-21618; Docket No. FAA-2021-0302; Project Identifier MCAI-2020-01596-R.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) is effective August 24, 2021.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies to Leonardo S.p.a.  Model AW189 helicopters,  certifi-
    cated in any category.

(d) SUBJECT

    Joint Aircraft Service Component (JASC)  Code:  7300,  Engine fuel and
    control.

(e) UNSAFE CONDITION

    This AD was prompted  by the identification  of misleading information
    in the emergency  procedure for the  "1(2) FUEL LOW"  caution message.
    The FAA  is issuing  this AD  to prevent  the wrong  estimation of the
    remaining flight time in a  low fuel condition. The unsafe  condition,
    if  not addressed,  could result  in an  uncommanded engine  in-flight
    shut-down and forced landing, with subsequent damage to the helicopter
    or injury to the occupants.

(f) COMPLIANCE

    Comply with this AD within the compliance times specified,  unless al-
    ready done.

(g) REQUIRED ACTIONS

    Within 14 hours time-in-service  after the effective date  of this AD,
    revise page 3-118 of Section 3,  Emergency and Malfunction Procedures,
    of the existing Rotorcraft Flight Manual for your helicopter by adding
    page 3-118, Temporary Revision 3-1 Rev. A, of AW189-RFM,  Document No.
    189G0290X002,  Record of Temporary Revisions,  dated May 24, 2019,  as
    contained in Annex A of Leonardo Helicopters Document No. 189G0257A061
    "AW189-MAF for EASA RFM Issue 2 TR 3-1,  Low Fuel  Caution Procedure,"
    Issue B, dated May 22, 2019 (TR 3-1 Rev A). Using a different document
    with information identical to the information  in page 3-118 of TR 3-1
    Rev A is acceptable for compliance  with the requirement of this para-
    graph.  This action  may be performed  by  the  owner/operator (pilot)
    holding at least a private pilot certificate  and must be entered into
    the aircraft records showing compliance  with this  AD  in  accordance
    with Sec. 43.9(a)(1) through (4) and Sec. 91.417(a)(2)(v).  The record
    must be maintained as required by Sec. 91.417,  Sec. 121.380,  or Sec.
    135.439.

(h) SPECIAL FLIGHT PERMITS

    Special flight permits are prohibited.

(i) 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 (j)(1)  of this AD. Information may  be
    emailed to: 9-AVS-AIR-730-AMOC@faa.gov.

(2) Before using any approved AMOC,  notify your appropriate principal in-
    spector, 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  Mitch Soth,  Flight Test
    Engineer, Southwest Section, Flight Test Branch, Compliance & Airworth
    -iness Division, FAA, 10101 Hillwood Pkwy, Fort Worth, TX 76177; tele-
    phone (817) 222-5110; email mitch.soth@faa.gov.

(2) The subject of this AD is addressed  in European Union Aviation Safety
    Agency (EASA) AD 2019-0136, dated June 11, 2019. You may view the EASA
    AD at https://www.regulations.gov in Docket No. FAA-2021-0302.

(k) MATERIAL INCORPORATED BY REFERENCE

(1) The Director of the Federal Register  approved  the  incorporation  by
    reference of the service information listed  in this paragraph under 5
    U.S.C. 552(a) and 1 CFR part 51.

(2) You must use  this service information as applicable to do the actions
    required by this AD, unless the AD specifies otherwise.

(i) AW189-RFM,  Document No. 189G0290X002,  Record of Temporary Revisions,
    dated May 24, 2019, as contained  in  Annex A  of Leonardo Helicopters
    Document No. 189G0257A061, "AW189-MAF for EASA RFM Issue 2 TR 3-1, Low
    Fuel Caution Procedure," Issue B, dated May 22, 2019.

(ii) [Reserved]

(3) For service information identified in this AD, contact Leonardo S.p.A.
    Helicopters,  Emanuele Bufano,  Head of Airworthiness,  Viale G.Agusta
    520, 21017 C.Costa di Samarate (Va) Italy;  telephone +39-0331-225074;
    fax +39-0331-229046; or at https://customerportal.leonardocompany.com/
    en-US/.

(4) You may view  this  service  information  at  the  FAA,  Office of the
    Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-321,
    Fort Worth, TX 76177.  For  information  on  the  availability of this
    material at the FAA, call (817) 222-5110.

(5) You may view this service information  that is incorporated  by refer-
    ence at the National  Archives and Records Administration  (NARA). For
    information  on  the availability  of  this material  at  NARA, email:
    fedreg.legal@nara.gov,  or  go  to:  https://www.archives.gov/federal-
    register/cfr/ibr-locations.html.

Issued on July 9, 2021. Gaetano A Sciortino, Deputy Director for Strategic
Initiatives,  Compliance & Airworthiness Division,  Aircraft Certification
Service.

FOR FURTHER INFORMATION CONTACT:  Mitch Soth, Flight Test Engineer, South-
west Section, Flight Test Branch, Compliance & Airworthiness Division, FAA
10101 Hillwood Pkwy, Fort Worth, TX 76177; telephone (817) 222-5110; email
mitch.soth@faa.gov.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2021-0302; Project Identifier MCAI-2020-01596-R;
Amendment 39-21618; AD 2021-13-13]
RIN 2120-AA64

Airworthiness Directives; Leonardo S.p.a. Helicopters

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
Leonardo S.p.a. Model AW189 helicopters. This AD was prompted by the
identification of misleading information in the emergency procedure for
the ``1(2) FUEL LOW'' caution message. This AD requires revising the
existing Rotorcraft Flight Manual (RFM) for your helicopter. The FAA is
issuing this AD to address the unsafe condition on these products.

DATES: This AD is effective August 24, 2021.
The Director of the Federal Register approved the incorporation by
reference of a certain document listed in this AD as of August 24,
2021.

ADDRESSES: For service information identified in this final rule,
contact Leonardo S.p.A. Helicopters, Emanuele Bufano, Head of
Airworthiness, Viale G.Agusta 520, 21017 C.Costa di Samarate (Va)
Italy; telephone +39-0331-225074; fax +39-0331-229046; or at https://customerportal.leonardocompany.com/en-US/. You may view the referenced
service information at the FAA, Office of the Regional Counsel,
Southwest Region, 10101 Hillwood Pkwy., Room 6N-321, Fort Worth, TX
76177. It is also available at https://www.regulations.gov by searching
for and locating Docket No. FAA-2021-0302.

Examining the AD Docket


You may examine the AD docket at https://www.regulations.gov by
searching for and locating Docket No. FAA-2021-0302; 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
European Union Aviation Safety Agency (EASA) AD, any comments received,
and other information. The street address for Docket Operations is U.S.
Department of Transportation, Docket Operations, M-30, West Building
Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC
20590.

FOR FURTHER INFORMATION CONTACT
: Mitch Soth, Flight Test Engineer,
Southwest Section, Flight Test Branch, Compliance & Airworthiness
Division, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone
(817) 222-5110; email mitch.soth@faa.gov.

SUPPLEMENTARY INFORMATION:

Background

The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to Leonardo S.p.a. Model
AW189 helicopters. The NPRM published in the Federal Register on April
19, 2021 (86 FR 20336). In the NPRM, the FAA proposed to require
revising page 3-118 of Section 3, Emergency and Malfunction Procedures,
of the existing RFM for your helicopter to add remaining flight times
(minutes) based on TQ value (%) and conditions that further reduce the
remaining flight times. The NPRM was prompted by EASA AD 2019-0136,
dated June 11, 2019 (EASA AD 2019-0136), issued by EASA, which is the
Technical Agent for the Member States of the European Union, to correct
an unsafe condition for Leonardo S.p.A. (formerly Finmeccanica
Helicopter Division, AgustaWestland) Model AW189 helicopters. EASA
advises of the identification of misleading information in the AW189
RFM Emergency procedure associated with the ``1(2) FUEL LOW'' caution
message. In particular, the procedure at issue instructs the pilot to
land as soon as practicable within 20 minutes. However, this remaining
flight time is guaranteed only if a constant torque value of 50% is
maintained. The correct time limit depends on the fuel consumption at
different engine power settings. Accordingly, EASA AD 2019-0136
requires amending section 3 of the AW189 RFM, ``Emergency and
malfunction procedures,'' informing all flight crews, and thereafter,
operating the helicopter accordingly. This condition, if not addressed,
could result in the wrong estimation of the remaining flight time in a
low fuel condition, possibly resulting in an uncommanded engine in-
flight shut-down and forced landing, with consequent damage to the
helicopter or injury to occupants.
EASA initially issued EASA AD 2019-0103, dated May 9, 2019 (EASA AD
2019-0103), to address this unsafe condition. EASA issued EASA AD 2019-
0136 to supersede EASA AD 2019-0103 to require using the corrected
amendment of the AW189 RFM.

Discussion of Final Airworthiness Directive

Comments

The FAA received no comments on the NPRM or on the determination of
the costs.

Conclusion

These helicopters have been approved by EASA and are approved for
operation in the United States. Pursuant to the FAA's bilateral
agreement with the European Union, EASA has notified the FAA about the
unsafe condition described in its AD. The FAA reviewed the relevant
data and determined that air safety requires adopting this AD as
proposed. Accordingly, the FAA is issuing this AD to address the unsafe
condition on these helicopters. Since the FAA issued the NPRM, the
website address for Leonardo S.p.a. has changed. This AD updates that
contact information to obtain service documentation. Additionally, the
FAA made edits to clarify that AW189--RFM, Document No. 189G0290X002,
Record of Temporary Revisions, TR No. 3-1, Revision A, dated May 24,
2019 (TR 3-1 Rev A) is included in Annex A of Leonardo Helicopters
Document No. 189G0257A061, ``AW189--MAF for EASA RFM Issue 2 TR 3-1,
Low Fuel Caution Procedure,'' Issue B, dated May 22, 2019. This AD is
otherwise adopted as proposed in the NPRM.

Related Service Information Under 1 CFR Part 51

The FAA reviewed TR 3-1 Rev A, which specifies remaining flight
times (minutes) based on TQ value (%) if the XFEED is closed or if the
XFEED is open with both fuel pumps ON. TR 3-1 Rev A also specifies that
the remaining flight times (minutes) are further reduced if the XFEED
is open, both fuel pumps are ON and one tank has emptied, and the 2
engines are supplied from the remaining tank.
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.

Differences Between This AD and the EASA AD

EASA AD 2019-0136 requires revising the existing RFM for your
helicopter within 14 days, whereas this AD requires that action within
14 hours time-in-service after the effective date of this AD instead.
EASA AD 2019-0136 requires removing the RFM changes previously required
by EASA AD 2019-0103, whereas this AD does not.

Costs of Compliance

The FAA estimates that this AD affects 4 helicopters of U.S.
Registry. Labor rates are estimated at $85 per work-hour. Based on
these numbers, the FAA estimates the following costs to comply with
this AD.
Revising the existing RFM for your helicopter takes about 0.25
work-hour for an estimated cost of $21 per helicopter and $84 for the
U.S. fleet.

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 helicopters identified in this rulemaking action.

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,
(2) Will not affect intrastate aviation in Alaska, and
(3) 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 Amendment

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

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.

Sec. 39.13 [Amended]

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