117 HR 7521 IH: Helicopter Passenger Protection Act U.S. House of Representatives 2022-04-14 text/xml EN Pursuant to Title 17 Section 105 of the United States Code, this file is not subject to copyright protection and is in the public domain.

I117th CONGRESS2d SessionH. R. 7521IN THE HOUSE OF REPRESENTATIVESApril 14, 2022Mr. Neguse (for himself, Mr. Perlmutter, Mr. Carson, Ms. Norton, Mrs. Carolyn B. Maloney of New York, and Mr. Cohen) introduced the following bill; which was referred to the Committee on Ways and Means, and in addition to the Committee on Transportation and Infrastructure, for a period to be subsequently determined by the Speaker, in each case for consideration of such provisions as fall within the jurisdiction of the committee concernedA BILLTo 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.

1.

Short title

This Act may be cited as the Helicopter Passenger Protection Act.

2.

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. .

3.

Credit for improving safety of fuel systems in rotorcraft

(a)

In general

Subpart B of part IV of subchapter A of chapter 1 of the Internal Revenue Code of 1986 is amended by inserting after section 30D the following new section:

30E.

Improving safety of fuel systems in rotorcraft

(a)

In general

There shall be allowed as a credit against the tax imposed by this chapter for the taxable year an amount equal to 10 percent of the qualified fuel system improvement costs which are paid or incurred by the taxpayer during the taxable year.(b)

Definitions

For purposes of this section—(1)

Qualified fuel system improvement costs

The term qualified fuel system improvement costs means costs paid or incurred to make qualified changes to a fuel system in a rotorcraft that did not, before such changes, meet the requirements described in paragraph (2)(A).(2)

Qualified changes

The term qualified changes means—(A)changes necessary to make a fuel system compliant with the requirements under—(i)paragraphs (1), (2), (3), (5), and (6) of section 27.952(a), section 27.952(c), section 27.952(f), section 27.952(g), section 27.963(g) (but allowing for a minimum puncture force of 250 pounds if successfully drop tested in-structure), and section 27.975(b) of title 14, Code of Federal Regulations as in effect on the date of enactment of this section, or(ii)paragraphs (1), (2), (3), (5), and (6) of section 29.952(a), section 29.952(c), section 29.952(f), section 29.952(g), section 29.963(b) (but allowing for a minimum puncture force of 250 pounds if successfully drop tested in-structure), and 29.975(a)(7) of such title as so in effect, and(B)such changes as the Secretary determines are necessary to result in a fuel system that has equivalent crash resistance to a fuel system compliant with the requirements under clause (i) or (ii) of subparagraph (A).

.(b)

Clerical amendment

The table of sections for such subpart A is amended by inserting after the item relating to section 30D the following new item:Sec. 30E. Improving safety of fuel systems in rotorcraft..(c)

Effective date

The amendments made by this section shall apply to taxable years beginning after December 31, 2022.