Federal Aviation Administration, DOT

Section 91.1603

(10) For all models of the McDonnell
Douglas DC-10, the flight cycle implementation time is 30,000 flights.
(11) For all models of the Lockheed
L-1011, the flight cycle implementation
time is 27,000 flights.
(12) For the Fokker F-28 Mark 1000,
2000, 3000, and 4000, the flight cycle implementation time is 60,000 flights.
(b) [Reserved]

kpayne on VMOFRWIN702 with $$_JOB

[Doc. No. 29104, 65 FR 24125, Apr. 25, 2000; 65
FR 35703, June 5, 2000; 65 FR 50744, Aug. 21,
2000, as amended by Amdt. 91-266, 66 FR
23130, May 7, 2001; Amdt. 91-277, 67 FR 72834,
Dec. 9, 2002; Amdt. 91-283, 69 FR 45941, July
30, 2004. Redesignated and amended by Amdt.
91-297, 72 FR 63410, Nov. 8, 2007; Docket FAA-
2018-0119, Amdt. 91-350, 83 FR 9171, Mar. 5,
2018]

Section 91.1507 Fuel tank system inspection
program.
(a) Except as provided in paragraph
(g) of this section, this section applies
to transport category, turbine-powered
airplanes with a type certificate issued
after January 1, 1958, that, as a result
of original type certification or later
increase in capacity, have - 
(1) A maximum type-certificated passenger capacity of 30 or more, or
(2) A maximum payload capacity of
7,500 pounds or more.
(b) For each airplane on which an
auxiliary fuel tank is installed under a
field approval, before June 16, 2008, the
operator must submit to the responsible Aircraft Certification Service Office proposed maintenance instructions
for the tank that meet the requirements of Special Federal Aviation Regulation No. 88 (SFAR 88) of this chapter.
(c) After December 16, 2008, no operator may operate an airplane identified
in paragraph (a) of this section unless
the inspection program for that airplane has been revised to include applicable inspections, procedures, and limitations for fuel tank systems.
(d) The proposed fuel tank system inspection program revisions specified in
paragraph (c) of this section must be
based on fuel tank system Instructions
for Continued Airworthiness (ICA) that
have been developed in accordance
with the applicable provisions of SFAR
88 of this chapter or Section 25.1529 and part
25, Appendix H, of this chapter, in effect on June 6, 2001 (including those de-

veloped for auxiliary fuel tanks, if any,
installed under supplemental type certificates or other design approval) and
that have been approved by the responsible Aircraft Certification Service Office.
(e) After December 16, 2008, before returning an airplane to service after any
alterations for which fuel tank ICA are
developed under SFAR 88, or under
Section 25.1529 in effect on June 6, 2001, the operator must include in the inspection
program for the airplane inspections
and procedures for the fuel tank system based on those ICA.
(f) The fuel tank system inspection
program changes identified in paragraphs (d) and (e) of this section and
any later fuel tank system revisions
must be submitted to the Flight Standards office responsible for review and
approval.
(g) This section does not apply to the
following airplane models:
(1) Bombardier CL-44
(2) Concorde
(3) deHavilland D.H. 106 Comet 4C
(4) VFW-Vereinigte Flugtechnische
Werk VFW-614
(5) Illyushin Aviation IL 96T
(6) Bristol Aircraft Britannia 305
(7) Handley Page Herald Type 300
(8) Avions Marcel Dassault - Breguet
Aviation Mercure 100C
(9) Airbus Caravelle
(10) Lockheed L-300
[Amdt. 91-297, 72 FR 63410, Nov. 8, 2007, as
amended by Docket FAA-2018-0119, Amdt. 91-
350, 83 FR 9172, Mar. 5, 2018]

Subpart M - Special Federal
Aviation Regulations
Section 91.1603 Special Federal Aviation Regulation
No.
112 - Prohibition
Against Certain Flights in the Tripoli (HLLL) Flight Information Region (FIR).
(a) Applicability. This section applies
to the following persons:
(1) All U.S. air carriers and U.S. commercial operators;
(2) All persons exercising the privileges of an airman certificate issued by
the FAA, except when such persons are
operating a U.S.-registered aircraft for
a foreign air carrier; and

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