14CFR vol1 part26 - 16 pages

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14 CFR Ch. I (1-1-18 Edition)
(f) The ice accretion that has the most adverse effect on ha...
PART 26 - CONTINUED AIRWORTHINESS AND SAFETY IMPROVEMENTS FO...
Subpart A - General
26.1 Purpose and scope.
26.3 Definitions.
26.5 Applicability table.
Subpart B - Enhanced Airworthiness
26.11 Electrical wiring interconnection systems (EWIS) maint...
Subpart C - Aging Airplane Safety - 
26.21
26.23
Subpart D - Fuel Tank Flammability
26.31 Definitions.
26.33 Holders of type certificates: Fuel tank
26.35 Changes to type certificates affecting
26.37 Pending type certification projects:
26.39 Newly produced airplanes: Fuel tank
Subpart E - Aging Airplane Safety - Damage Tolerance Data fo...
26.41 Definitions.
26.43 Holders of and applicants for type certificates - Repa...
...
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Section 26.11
Section 26.5 Applicability table.
Subpart B EAPAS/FTS
Subpart C widespread
Subpart D fuel tank
26.11 ...........................
26.21 ...........................
26.33 ...........................
26.11 ...........................
26.11 ...........................
26.21 ...........................
26.21 ...........................
26.21 ...........................
26.37 ...........................
26.35 ...........................
26.35 ...........................
26.11 ...........................
26.21 ...........................
26.35 ...........................
26.39 ...........................
Subpart E damage
...
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Section 26.21
14 CFR Ch. I (1-1-18 Edition)
(b) or (c) of this section, as applicable,
(e) Each person identified in paragraphs (d)(1), (d)(2), and...
(b) of this subchapter in effect on December 10, 2007, and a...
(f) Each person specified in paragraph
(e) must implement the compliance
(e) of this section.
(g) This section does not apply to the
68618, Dec. 5, 2007]
Subpart C - Aging Airplane Safety - Widespread Fatigue Damag...
69782, Nov. 15, 2010, unless otherwise noted.
Section 26.21
(a) Applicability. Except as provided
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Section 26.21
(b) Limit of validity. Each person identified in paragraph (...
(i) All model variations and derivatives approved under the ...
(i) For those maintenance actions for
(c) Persons who must comply and compliance dates. The follow...
(i) January 14, 2016;
(c)(7) of this section, if the original TC
(i) January 14, 2016;
(c)(7) of this section, if the application
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Section 26.21
14 CFR Ch. I (1-1-18 Edition)
(i) January 14, 2016;
(i) July 14, 2012;
(i) July 14, 2012;
(d) Compliance plan. Each person
(e) Compliance dates for compliance
2011.
(f) Compliance plan implementation.
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Section 26.21
(g) Exceptions. This section does not
300-50A01
14, 2011)
717 ...........................................................
727 (all series) ..............................................
737 (Classics): 737-100, -200, -200C, -300, -400, -500 ........
737 (NG): 737-600, -700, -700C, -800, -900, -900ER ............
747 (Classics): 747-100, -100B, -100B SUD, -200B, -200C, -20...
747-400: 747-400, -400D, -400F ................................
757 ...........................................................
767 ...........................................................
...
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Section 26.23
14 CFR Ch. I (1-1-18 Edition)
15, 2010, as amended at 77 FR 30878, May 24,
2012]
Section 26.23
(a) Applicability. Any person may
(b) Extended limit of validity. Each person applying for an ...
(i) All model variations and derivatives approved under the ...
Subpart D - Fuel Tank
42499, July 21, 2008, unless otherwise noted.
Section 26.31
(a) Fleet Average Flammability Exposure has the meaning defi...
(b) Normally Emptied means a fuel
25.981(b).
Section 26.33 Holders of type certificates:
(a) Applicability. This section applies
1992, that, as a result of original type
7,500 pounds or more.
(b) Flammability Exposure Analysis. (1)
25 of this chapter.
11:00 Mar 08, 2018
...
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Section 26.33
(i) Fuel tanks for which the type certificate holder has not...
(c) Design Changes. For fuel tanks
(i) Fuel tanks that are designed to be
(d) Service Instructions. No later than
2008.
(e) Instructions for Continued Airworthiness (ICA). No later...
(f) Airworthiness Limitations. Unless
(b)(1) of this section and submit it to
(g) Compliance Plan for Flammability
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Section 26.35
14 CFR Ch. I (1-1-18 Edition)
(h) Compliance Plan for Design
210 days after December 26, 2008, each
(i) Each affected type certificate
21, 2008, as amended by Amdt. 26-3, 74 FR
31619, July 2, 2009]
Section 26.35 Changes to type certificates affecting fuel ta...
(a) Applicability. This section applies
(i) Installation of a fuel tank designed to be Normally Empt...
(b) Flammability Exposure Analysis - (1)
(i) Holders of supplemental type certificates and field appr...
(i) Fuel tanks for which the type certificate holder, supple...
(f) of this section that it will provide
(c) Impact Assessment. By the times
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Section 26.35
(a)(3)(iii) of this section, must submit
(d) Design Changes and Service Instructions. By the times sp...
(d)(2) of this section, as applicable.
(a)(2), or (a)(3)(i) of this section must
2008.
(a)(3)(ii) of this section must comply
(e) Compliance Times for Design
2012, or before the certificate is issued,
(f) Compliance Planning. By the applicable date specified in...
(c) of this section, and the design
(d) of this section, a proposal for submitting a draft of al...
(d) of this section, a proposal for how
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Section 26.37
14 CFR Ch. I (1-1-18 Edition)
(g) Each person subject to this section must implement the c...
21, 2008, as amended by Amdt. 26-3, 74 FR
31619, July 2, 2009]
Section 26.37 Pending
(a) Applicability. This section applies
2008, and if the certificate was not
7,500 pounds or more.
(b) If the application was made on or
14 CFR 25.981 in effect on December 26,
2008, apply.
21, 2008, as amended by Amdt. 26-3, 74 FR
31619, July 2, 2009]
Section 26.39 Newly produced airplanes: Fuel
(a) Applicability: This section applies
(b) Any fuel tank meeting all of the
...
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Section 26.43
Section 26.43 Holders of and applicants for
(a) Applicability. Except as specified
1958, that as a result of original type
7,500 pounds or more.
(b) List of fatigue critical baseline structure. For airplan...
(c) Existing and future published repair
(b)(1) of this section;
(d) Future repair data not published.
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Section 26.43
14 CFR Ch. I (1-1-18 Edition)
(e) Repair evaluation guidelines. Except for airplane models...
2008, holders of a type certificate for
(i) A process for conducting surveys
(f) Compliance times. Holders of type
30, 2009.
12 months of the airplane-s return to
30, 2009.
(g) Exceptions. The requirements of
1A20.
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Section 26.45
4A21.
4A26.
12, 2007, as amended by Amdt. 26-4, 75 FR
11734, Mar. 12, 2010]
Section 26.45 Holders of type certificates - Alterations and...
(a) Applicability. This section applies
(b) Fatigue critical alteration structure.
(c) DT Data. For existing and future
(d) DT Data for Repairs Made to Alterations. For existing an...
(e) Compliance times. Holders of type
(i) No later than 360 days after January 11, 2008, for alter...
12, 2010 or before initial approval of the
30, 2009.
11:00 Mar 08, 2018
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Section 26.47
14 CFR Ch. I (1-1-18 Edition)
30, 2009.
12 months after initial approval of the
12, 2007, as amended by Amdt. 26-4, 75 FR
11734, Mar. 12, 2010]
Section 26.47 Holders of and applicants for a
(a) Applicability. This section applies
(b) Fatigue critical alteration structure.
(c) DT Data. For existing and future
(d) DT Data for Repairs Made to Alterations. For existing an...
(e) Compliance times. Holders of supplemental type certifica...
(b)(3) of this section must be submitted
2008.
30, 2009.
30, 2009.
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12 months after initial approval of the
Section 26.49
Subpart A - General
27.1 Applicability.
27.2 Special retroactive requirements.
Subpart B - Flight
(a) Compliance plan. Except for applicants for type certific...
2008, each person identified in SectionSection 26.43,
26.45, and 26.47, must submit a compliance plan consisting o...
26.45(e), and 26.47(e), as applicable.
(b) Compliance dates for compliance
2008.
(c) Compliance Plan Implementation.
PART 27 - AIRWORTHINESS STANDARDS:
27.21 Proof of compliance.
27.25 Weight limits.
27.27 Center of gravity limits.
27.29 Empty weight and corresponding center of gravity.
27.31 Removable ballast.
27.33 Main rotor speed and pitch limits.
27.45 General.
...