,i #aafth ,,congress #ast ,session ,h4 ,r4 #fge ,,in ,,the ,,house ,,of ,,representatives ,january #ag1 #bjai,mr4 ,neguse 7for himself and ,mr4 ,perlmutter7 introduced the following bill2 which was referred to the ,committee on ,ways and ,means ,a ,,bill ,to amend the ,internal ,revenue ,code of #aihf to provide for a credit against tax for improving the safety of fuel systems in emergency medical rotorcraft4 #a4 ,short title ,this ,act may be cited as the ,safe ,helicopters ,now ,act4 #b4 ,credit for improving safety of fuel systems in emergency medical rotorcraft 7a7 ,in general ,subpart ,b of part ,,iv of subchapter ,a of chapter #a of the ,internal ,revenue ,code of #aihf is amended by inserting after section #cj;,d the following new section3 #cj;,e4 ,improving safety of fuel systems in emergency medical rotorcraft 7a7 ,in general ,there shall be allowed as a credit against the tax imposed by this chapter for the taxable year an amount equal to #aj percent of the qualified fuel system improvement costs which are paid or incurred by the taxpayer during the taxable year4 7b7 ,definitions ,for purposes of this section-- 7#a7 ,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 an emergency medical rotorcraft that did not1 before such changes1 meet the requirements described in paragraph 7#b77;,a74 7#b7 ,qualified changes ,the term qualified changes means-- 7,a7 changes necessary to make a fuel system compliant with the requirements under-- 7i7 paragraphs 7#a71 7#b71 7#c71 7#e71 and 7#f7 of section #bg4ieb7;a71 section #bg4ieb7;c71 section #bg4ieb7;f71 section #bg4ieb7;g71 section #bg4ifc7;g7 7but allowing for a minimum puncture force of #bej pounds if successfully drop tested in-structure71 and section #bg4ige7;b7 of title #ad1 ,code of ,federal ,regulations as in effect on the date of enactment1 or 7ii7 paragraphs 7#a71 7#b71 7#c71 7#e71 and 7#f7 of section #bi4ieb7;a71 section #bi4ieb7;c71 section #bi4ieb7;f71 section #bi4ieb7;g71 section #bi4ifc7;b7 7but allowing for a minimum puncture force of #bej pounds if successfully drop tested in-structure71 and #bi4ige7;a77#g7 of such title as so in effect1 and 7,b7 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 7i7 or 7ii7 of subparagraph 7,a74 7#c7 ,emergency medical rotorcraft ,the term emergency medical rotorcraft means1 with respect to a taxable year1 a rotorcraft that is used for the provision of emergency medical services during such year4 4 7b7 ,clerical amendment ,the table of sections for such subpart ,a is amended by inserting after the item relating to section #cj;,d the following new item3 ,sec4 #cj;,e4 ,improving safety of fuel systems in emergency medical rotorcraft44 7c7 ,effective date ,the amendments made by this section shall apply to taxable years beginning after ,december #ca1 #bjah4