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2021-24-04 BELL TEXTRON CANADA LIMITED (TYPE CERTIFICATE PREVIOUSLY HELD BY BELL HELICOPTER TEXTRON CANADA LIMITED): Amendment 39-21825; Docket No. FAA-2021-0783; Project Identifier 2019-SW-009-AD.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) is effective January 13, 2022.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD  applies to  Bell Helicopter Textron Canada Limited (type cer-
    tificate previously  held by  Bell Helicopter  Textron Canada Limited)
    Model  505  helicopters  having serial  number  65011  and subsequent,
    certificated 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 determination that reducing the  pressure
    altitude limitations for certain fuel  types is necessary. The FAA  is
    issuing this AD  to address unsatisfactory  flight performance of  the
    engine above pressure altitude limitations  for Jet B and JP-4  fuels.
    The  unsafe condition,  if  not  addressed, could  result in  low fuel
    pressure, engine flame-out, or engine power interruption.

(f) COMPLIANCE

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

(g) REQUIRED ACTIONS

    Within 30 calendar  days after the  effective date of  this AD, revise
    the Limitations Section of the existing Rotorcraft Flight Manual (RFM)
    for your  helicopter by  replacing Figure  1-6. with  Figure 1-6. Fuel
    Operating Envelope (Sheet 1 of 1) of Bell 505 Rotorcraft Flight Manual
    BHT-505-FM-1, Revision 3, dated  July 25, 2018 (BHT-505-FM-1  Revision
    3). Using a different document  with information identical to that  in
    Figure 1-6.  Fuel Operating  Envelope (Sheet  1 of  1) of BHT-505-FM-1
    Revision 3 is acceptable for compliance with the requirements of  this
    AD. The  action required  by this  paragraph 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 14 CFR 43.9(a)(1)  through (4) and 14  CFR
    91.417(a)(2)(v). The record must be  maintained as required by 14  CFR
    91.417, 121.380, or 135.439.

(h) 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 (i)(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.

(i) RELATED INFORMATION

(1) For more information about this AD,  contact Rao Edupuganti, Aerospace
    Engineer, Dynamic Systems Section, Technical Innovation Policy Branch,
    Policy & Innovation Division, FAA, 10101 Hillwood Pkwy, Fort Worth, TX
    76177; telephone (817) 222-5110; email rao.edupuganti@faa.gov.

(2) The subject of this AD is addressed in Transport Canada AD CF-2019-08,
    dated March 5, 2019.  You may view the Transport Canada AD at https://
    www.regulations.gov in Docket No. FAA-2021-0783.

(j) 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) Figure 1-6.  Fuel Operating Envelope (Sheet 1 of 1) of Bell 505 Rotor-
    craft Flight Manual BHT-505-FM-1, Revision 3, dated July 25, 2018.

(ii) [Reserved]

(3) For service information identified  in this AD,  contact  Bell Textron
    Canada  Limited,  12,800  Rue de l'Avenir,  Mirabel,  Quebec  J7J 1R4,
    Canada; telephone 1-450-437-2862 or 1-800-363-8023; fax 1-450-433-0272
    email productsupport@bellflight.com; or at https://www.bellflight.com/
    support/contact-support.

(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: fr.
    inspection@nara.gov,   or  go  to:  https://www.archives.gov/federal-
    register/cfr/ibr-locations.html.

Issued on November 12, 2021.  Gaetano A. Sciortino,  Deputy  Director  for
Strategic Initiatives,  Compliance & Airworthiness Division, Aircraft Cer-
tification Service.

FOR FURTHER INFORMATION CONTACT:   Rao  Edupuganti,   Aerospace  Engineer,
Dynamic Systems Section,  Technical  Innovation  Policy  Branch,  Policy &
Innovation Division, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; tel-
ephone (817) 222-5110; email rao.edupuganti@faa.gov.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2021-0783; Project Identifier 2019-SW-009-AD; Amendment
39-21825; AD 2021-24-04]
RIN 2120-AA64

Airworthiness Directives; Bell Textron Canada Limited (Type
Certificate Previously Held by Bell Helicopter Textron Canada Limited)
Helicopters

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Bell Textron Canada Limited (type certificate previously held
by Bell Helicopter Textron Canada Limited) Model 505 helicopters. This
AD was prompted by the determination that reducing the pressure
altitude limitations for certain fuel types is necessary. 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 January 13, 2022.
The Director of the Federal Register approved the incorporation by
reference of a certain document listed in this AD as of January 13,
2022.

ADDRESSES: For service information identified in this final rule,
contact Bell Textron Canada Limited, 12,800 Rue de l'Avenir, Mirabel,
Quebec J7J 1R4, Canada; telephone 1-450-437-2862 or 1-800-363-8023; fax
1-450-433-0272; email productsupport@bellflight.com; or at https://www.bellflight.com/support/contact-support. 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. For information on the availability of this material at the FAA,
call (817) 222-5110. It is also available at https://www.regulations.gov by searching
for and locating Docket No. FAA-2021-0783.

Examining the AD Docket

You may examine the AD docket at https://www.regulations.gov by
searching for and locating Docket No. FAA-2021-0783; 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
Transport Canada 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: Rao Edupuganti, Aerospace Engineer,
Dynamic Systems Section, Technical Innovation Policy Branch, Policy &
Innovation Division, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177;
telephone (817) 222-5110; email rao.edupuganti@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 certain Bell Textron
Canada Limited (type certificate previously held by Bell Helicopter
Textron Canada Limited) Model 505 helicopters. The NPRM published in
the Federal Register on September 20, 2021 (86 FR 52109). In the NPRM,
the FAA proposed to require revising the existing RFM for your
helicopter. Incorporating the RFM revision 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 14 CFR 43.9(a)(1) through (4) and 14 CFR
91.417(a)(2)(v). The record must be maintained as required by 14 CFR
91.417, 121.380, or 135.439. This is an exception to the FAA's standard
maintenance regulations.
The NPRM was prompted by Canadian AD CF-2019-08, dated March 5,
2019 (Canadian AD CF-2019-08), issued by Transport Canada, which is the
aviation authority for Canada, to correct an unsafe condition for Bell
Helicopter Textron Canada Limited Model 505 helicopters serial numbers
65011 and subsequent. Transport Canada advises of the need to reduce
the altitude limitations for Jet B and JP-4 wide-cut fuels following
unsatisfactory performance of the engine at the original higher
altitude limitations with these wide-cut fuels. This condition, if not
addressed, could result in low fuel pressure, engine flame-out, or
engine power interruption (a change in any engine performance
parameter--including but not limited to gas generator speed, power
turbine speed, main gas temperature, or output torque--outside its
normal limits for the prevailing operating conditions).
Accordingly, Canadian AD CF-2019-08 requires revising the RFM to
reflect the reduced altitude operating limitations for Jet B and JP-4
wide-cut fuels.

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 the aviation authority of
Canada and are approved for operation in the United States. Pursuant to
the FAA's bilateral agreement with Canada, Transport Canada, its
technical representative, has notified the FAA of 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. Except for minor editorial changes, this AD is adopted as
proposed in the NPRM.

Related Service Information Under 1 CFR Part 51

The FAA reviewed Figure 1-6. Fuel Operating Envelope (Sheet 1 of 1)
of Bell 505 Rotorcraft Flight Manual BHT-505-FM-1, Revision 3, dated
July 25, 2018, which specifies limitations, normal and emergency
procedures, performance data, weight and balance information, and
provides a list of approved optional equipment supplements. This
revision of the service information includes an updated figure of the
fuel operating envelope showing the reduced pressure altitude
limitations for Jet B and JP-4 fuels.
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 Transport Canada AD

Canadian AD CF-2019-08 requires updating the RFM to Bell 505 RFM
BHT-505-FM-1 Revision 3 or later revisions approved by Transport
Canada, whereas this AD requires revising the Limitations Section of
the RFM for your helicopter by replacing the existing Figure 1-6. with
Figure 1-6. Fuel Operating Envelope (Sheet 1 of 1) of Bell 505 RFM BHT-
505-FM-1, Revision 3, dated July 25, 2018.

Costs of Compliance

The FAA estimates that this AD affects 73 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 would take about 0.5
work-hour for an estimated cost of $43 per helicopter or $3,139 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 products 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: