Section 129.113

14 CFR Ch. I (1-1-19 Edition)

(2) For airplanes subject to Section 25.1729 of
this chapter, the EWIS ICA must comply with paragraph H25.4 and all of
paragraph H25.5.
(d) After March 10, 2011, before returning a U.S.-registered airplane to
service after any alterations for which
EWIS ICA are developed, the foreign
person or foreign air carrier must include in the maintenance program for
that airplane inspections and procedures for EWIS based on those ICA.
(e) The EWIS maintenance program
changes identified in paragraphs (c)
and (d) of this section and any later
EWIS revisions must be submitted to
the Principal Inspector or Flight
Standards office responsible for review
and approval.
(f) This section does not apply to the
following airplane models:
(1) Lockheed L-188
(2) Bombardier CL-44
(3) Mitsubishi YS-11
(4) British Aerospace BAC 1-11
(5) Concorde
(6) deHavilland D.H. 106 Comet 4C
(7) VFW-Vereinigte Flugtechnische
Werk VFW-614
(8) Illyushin Aviation IL 96T
(9) Bristol Aircraft Britannia 305
(10) Handley Page Herald Type 300
(11) Avions Marcel Dassault - Breguet
Aviation Mercure 100C
(12) Airbus Caravelle
(13) Lockheed L-300
[Amdt. 129-43, 72 FR 63413, Nov. 8, 2007, as
amended by Docket FAA-2018-0119, Amdt.
129-53, 83 FR 9174, Mar. 5, 2018]

Section 129.113 Fuel tank system maintenance 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
7500 pounds or more.
(b) For each U.S.-registered airplane
on which an auxiliary fuel tank is installed under a field approval, before
June 16, 2008, the foreign person or foreign air carrier operating the airplane
must submit to the responsible Air-

craft 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 foreign person or foreign air carrier may
operate a U.S.-registered airplane identified in paragraph (a) of this section
unless the maintenance program for
that airplane has been revised to include applicable inspections, procedures, and limitations for fuel tank
systems.
(d) The proposed fuel tank system
maintenance program revisions 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 developed 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 a U.S.-registered airplane to
service after any alteration for which
fuel tank ICA are developed under
SFAR 88, or under Section 25.1529 in effect on
June 6, 2001, the foreign person or foreign air carrier must include in the
maintenance program for the airplane
inspections and procedures for the fuel
tank system based on those ICA.
(f) The fuel tank system maintenance
program changes identified in paragraphs (d) and (e) of this section and
any later fuel tank system revisions
must be submitted to the Principal Inspector or 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

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