,i #aaeth ,,congress #ast ,session ,h4 ,r4 #caej ,,in ,,the ,,house ,,of ,,representatives ,june #bi1 #bjag,mr4 ,perlmutter 7for himself and ,mr4 ,polis7 introduced the following bill2 which was referred to the ,committee on ,transportation and ,infrastructure ,a ,,bill ,to amend title #di1 ,united ,states ,code1 with respect to helicopter crash resistant fuel systems1 and for other purposes4 #a4 ,short title ,this ,act may be cited as the ,helicopter ,fuel ,system ,safety ,act4 #b4 ,helicopter crash resistant fuel systems 7a7 ,in general ,chapter #ddg of title #di1 ,united ,states ,code1 is amended by adding at the end the following3 #ddgcf4 ,fuel system crash resistance 7a7 ,prohibition 7#a7 ,in general ,a person may not operate a covered rotorcraft in ,united ,states airspace unless the design of the rotorcraft is certified by the ,administrator of the ,federal ,aviation ,administration to-- 7,a7 comply with the requirements under paragraphs 7#a71 7#b71 7#c71 7#e71 and 7#f7 of section #bg4ieb7;a7 and section #bg4ieb7;f7 or paragraphs 7#a71 7#b71 7#c71 7#e71 and 7#f7 of section #bi4ieb7;a7 and section #bi4ieb7;f7 of title #ad1 ,code of ,federal ,regulations1 applicable to the category of the rotorcraft2 or 7,b7 employ other means acceptable to the ,administrator to provide an equivalent level of fuel system crash resistance4 7#b7 ,covered rotorcraft defined ,in this subsection1 the term covered rotorcraft means a rotorcraft for which manufacture was completed1 as determined by the ,administrator1 on or after the date that is #a year after the date of enactment of this section4 7b7 ,administrative provisions ,the ,administrator shall-- 7#a7 expedite the certification and validation of ,united ,states and foreign type designs and retrofit kits that improve fuel system crashworthiness2 and 7#b7 not later than #ahj days after the date of enactment of this section1 and periodically thereafter1 issue a bulletin to-- 7,a7 inform rotorcraft owners and operators of available modifications to improve fuel system crashworthiness2 and 7,b7 urge that such modifications be installed as soon as practicable4 7c7 ,rule of construction ,nothing in this section may be construed to affect the operation of a rotorcraft by the ,department of ,defense4 4 7b7 ,clerical amendment ,the analysis for chapter #ddg of title #di1 ,united ,states ,code1 is amended by adding at the end the following3 #ddgcf4 ,fuel system crash resistance4 4