Federal Aviation Administration, DOT

Section 21.213

water, or over land areas where adequate landing facilities or appropriate
fuel is not available. The excess weight
that may be authorized under this
paragraph is limited to the additional
fuel, fuel-carrying facilities, and navigation equipment necessary for the
flight.
(c) Upon application, as prescribed in
SectionSection 91.1017 or 119.51 of this chapter, a special flight permit with a continuing authorization may be issued for aircraft
that may not meet applicable airworthiness requirements, but are capable of safe flight for the purpose of flying aircraft to a base where maintenance or alterations are to be performed. The permit issued under this
paragraph is an authorization, including conditions and limitations for
flight, which is set forth in the certificate holder-s operations specifications.
The permit issued under this paragraph
may be issued to - 
(1) Certificate holders authorized to
conduct operations under part 119 of
this chapter, that have an approved
program for continuing flight authorization; or
(2) Management specification holders
authorized to conduct operations under
part 91, subpart K of this chapter for
those aircraft they operate and maintain under a continuous airworthiness
maintenance program prescribed by
Section 91.1411 of this chapter.
[Doc. No. 5085, 29 FR 14570, Oct. 24, 1964, as
amended by Amdt. 21-21, 33 FR 6859, May 7,
1968; Amdt. 21-51, 45 FR 60170, Sept. 11, 1980;
Amdt. 21-54, 46 FR 37878, July 23, 1981; Amdt.
21-79, 66 FR 21066, Apr. 27, 2001; Amdt. 21-84,
68 FR 54559, Sept. 17, 2003; Amdt. 21-87, 71 FR
536, Jan. 4, 2006; Amdt. 21-92, 74 FR 53389, Oct.
16, 2009]

spaschal on DSK3GDR082PROD with CFR

Section 21.199

Issue of special flight permits.

(a) Except as provided in Section 21.197(c),
an applicant for a special flight permit
must submit a statement in a form and
manner prescribed by the FAA, indicating - 
(1) The purpose of the flight.
(2) The proposed itinerary.
(3) The crew required to operate the
aircraft and its equipment, e.g., pilot,
co-pilot, navigator, etc.
(4) The ways, if any, in which the aircraft does not comply with the applicable airworthiness requirements.

(5) Any restriction the applicant considers necessary for safe operation of
the aircraft.
(6) Any other information considered
necessary by the FAA for the purpose
of prescribing operating limitations.
(b) The FAA may make, or require
the applicant to make appropriate inspections or tests necessary for safety.
[Doc. No. 5085, 29 FR 14570, Oct. 24, 1964, as
amended by Amdt. 21-21, 33 FR 6859, May 7,
1968; Amdt. 21-22, 33 FR 11901, Aug. 22, 1968]

Subpart I - Provisional
Airworthiness Certificates
SOURCE: Docket No. 5085, 29 FR 14571, Oct.
24, 1964, unless otherwise noted.

Section 21.211

Applicability.

This subpart prescribes procedural
requirements for the issue of provisional airworthiness certificates.
Section 21.213

Eligibility.

(a) A manufacturer who is a United
States citizen may apply for a Class I
or Class II provisional airworthiness
certificate for aircraft manufactured
by him within the U.S.
(b) Any holder of an air carrier operating certificate under Part 121 of this
chapter who is a United States citizen
may apply for a Class II provisional
airworthiness certificate for transport
category aircraft that meet either of
the following:
(1) The aircraft has a current Class II
provisional type certificate or an
amendment thereto.
(2) The aircraft has a current provisional amendment to a type certificate
that was preceded by a corresponding
Class II provisional type certificate.
(c) An aircraft engine manufacturer
who is a United States citizen and who
has altered a type certificated aircraft
by installing different type certificated
engines, manufactured by him within
the United States, may apply for a
Class I provisional airworthiness certificate for that aircraft, if the basic
aircraft, before alteration, was type

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