[Congressional Bills 118th Congress]
[From the U.S. Government Publishing Office]
[H.R. 8393 Introduced in House (IH)]
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118th CONGRESS
2d Session
H. R. 8393
To amend title 49, United States Code, to require that certain
rotorcraft manufactured before April 5, 2020, comply with requirements
relating to fuel system crash resistance, and for other purposes.
_______________________________________________________________________
IN THE HOUSE OF REPRESENTATIVES
May 14, 2024
Mr. Neguse introduced the following bill; which was referred to the
Committee on Transportation and Infrastructure
_______________________________________________________________________
A BILL
To amend title 49, United States Code, to require that certain
rotorcraft manufactured before April 5, 2020, comply with requirements
relating to fuel system crash resistance, and for other purposes.
Be it enacted by the Senate and House of Representatives of the
United States of America in Congress assembled,
SECTION 1. SHORT TITLE.
This Act may be cited as the ``Helicopter Passenger Protection
Act''.
SEC. 2. CRASH-RESISTANT FUEL SYSTEMS IN ROTORCRAFT.
(a) In General.--The Administrator of the Federal Aviation
Administration shall task the Aviation Rulemaking Advisory Committee
to--
(1) review the data analysis conducted and the
recommendations developed by the Aviation Rulemaking Advisory
Committee Rotorcraft Occupant Protection Working Group of the
Administration;
(2) update the 2018 report of such working group on
rotorcraft occupant protection by--
(A) reviewing National Transportation Safety Board
data from 2016 through 2023 on post-crash fires in
helicopter accidents; and
(B) determining whether and to what extent crash-
resistant fuel systems could have prevented fatalities;
and
(3) develop recommendations for either the Administrator or
the helicopter industry to encourage helicopter owners and
operators to expedite the installation of crash-resistant fuel
systems in the aircraft of such owners and operators regardless
of original certification and manufacture date.
(b) Schedule.--
(1) Deadline.--Not later than 18 months after the
Administrator tasks the Aviation Rulemaking Advisory Committee
under subsection (a), the Committee shall submit the
recommendations developed under subsection (a)(2) to the
Administrator.
(2) Implementation.--If applicable, and not later than 180
days after receiving the recommendations under paragraph (1),
the Administrator shall--
(A) begin implementing, as appropriate, any
consensus safety recommendations the Administrator
receives from the Aviation Rulemaking Advisory
Committee, and brief the Committee on Transportation
and Infrastructure of the House of Representatives and
the Committee on Commerce, Science, and Transportation
of the Senate on any recommendations the Administrator
does not implement; and
(B) partner with the United States Helicopter
Safety Team, as appropriate, to facilitate
implementation of any recommendations for the
helicopter industry pursuant to subsection (a)(2).
SEC. 3. HELICOPTER FUEL SYSTEM SAFETY.
Section 44737 of title 49, United States Code, is amended--
(1) in subsection (a)(2) by striking ``the date that is 18
months after the date of enactment of this section'' and
inserting ``April 5, 2020'';
(2) by redesignating subsections (b) and (c) as subsections
(c) and (d), respectively; and
(3) by inserting after subsection (a) the following:
``(b) Prohibition for Rotorcraft Manufactured Before April 5,
2020.--
``(1) In general.--Not later than 5 years after the date of
enactment of this subsection, a person may not operate in
United States airspace a rotorcraft manufactured before April
5, 2020, for which the Administrator of the Federal Aviation
Administration has issued a standard airworthiness certificate,
unless such rotorcraft includes a fuel system that is certified
by the Administrator to--
``(A) comply with the requirements applicable to
the category of the rotorcraft under paragraphs (1),
(2), (3), (5), and (6) of section 27.952(a), section
27.952(f), and section 27.963(g) (but allowing for a
minimum puncture force of 250 pounds) or paragraphs
(1), (2), (3), (5), and (6) of section 29.952(a),
section 29.952(f), and section 29.963(b) (but allowing
for a minimum puncture force of 250 pounds) of title
14, Code of Federal Regulations, as in effect on the
date of enactment of this subsection; or
``(B) employ other means acceptable to the
Administrator to provide an equivalent level of fuel
system crash resistance.
``(2) Exception.--This subsection shall not apply to an
unmanned aircraft that does not carry any occupants.''.
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