(c)
The applicant must apply for a type certi.cate, in the transport category, for the aircraft.
(d)
The applicant must hold a U.S. type certi.cate for at least one other aircraft in the same transport category as the subject aircraft.
(e)
The FAA’s o.cial .ight test program or the .ight test program conducted by the authorities of the country in which the aircraft was manufactured, with respect to the issue of a type certi.cate for that aircraft, must be in progress.
(f)
The applicantor,in the case of aforeign manufactured aircraft, the countryin which the aircraft was manufactured, must certify that–
(1)
The aircraft has been designed and constructed in accordance with the air-worthiness requirements applicable to the issue of the type certi.cate applied for;
(2)
The aircraft substantially complies with the applicable .ight characteristic requirements for the type certi.cate applied for; and
(3)
The aircraftcanbe operated safely under the appropriate operatinglimitations in this subchapter.
(g)
The applicant must submit a report showing that the aircraft has been .own in all maneuvers necessary to show compliance with the .ight requirements for the issue of the type certi.cate and to establish that the aircraft can be operated safely in accordance with the limitations in this subchapter.
(h)
The applicant must prepare a provisional aircraft .ight manual containing all li-mitations required for the issue of the type certi.cate applied for, including limi-tations on weights, speeds, .ight maneuvers, loading, and operation of controls and equipment unless,for eachlimitation not so established, appropriate operating restrictions are established for the aircraft.
(i)
The applicant must establish an inspection and maintenance program for the conti-nued airworthiness of the aircraft.
(j)
The applicant must show that a prototype aircraft has been .own for at least 100 hours. In the case of an amendment to a provisional type certi.cate, the Adminis-trator may reduce the number of required .ight hours.
Amdt. 21-66, E.. 8/18/90
FAR 21.85 : Provisional amendments to type certi.cates.
(a)
An applicant who manufactures aircraft within the United States is entitled to a provisionalamendment to a type certi.cateifhe shows compliance with this section andtheAdministrator .ndsthatthereisnofeature, characteristic,orconditionthat would make the aircraft unsafe when operated under the appropriate limitations contained in this subchapter.
(b)
An applicant who manufactures aircraft in a foreign country with which the United States has an agreement for the acceptance of those aircraft for export and import is entitled to aprovisional amendmentto atype certi.cateif the country in which the aircraft was manufactured certi.es that the applicant has shown compliance with this section,thatthe aircraft meetsthe requirements ofparagraph(e) of this section and that there is no feature, characteristic, or condition that would make the aircraft unsafe when operated under the appropriate limitations contained in this subchapter.
(c)
The applicant must apply for an amendment to the type certi.cate.
(d)
The FAA’s o.cial .ight test program or the .ight test program conducted by the authorities of the country in which the aircraft was manufactured, with respect to the amendment of the type certi.cate, must be in progress.
(e)
The applicant or, in the case of foreign manufactured aircraft, the country in which the aircraft was manufactured, must certify that–
(1)
The modi.cation involved in the amendment to the type certi.cate has been designed and constructed in accordance with the airworthiness requirements applicable to the issue of the type certi.cate for the aircraft;
(2)
The aircraft substantially complies with the applicable .ight characteristic requirements for the type certi.cate; and
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本文链接地址：FAA规章 美国联邦航空规章 Federal Aviation Regulations 1(82)
