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AC 43.13-2B

Historical
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Advisory circular · Acceptable Methods, Techniques, and Practices – Aircraft Alterations

A newer version is currentThis is a historical version. AC 43.13-2C is the version in force, approved August 10, 2026.
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Approved
March 3, 2008
Last reviewed
June 12, 2024
Cancels
AC43.13-2A
Family
AC 43.13-2 · 3 versions
Revision
B
14 CFR parts
43, 23, 27, 65, 91, 133, 45, 21, 29, 25
Cited by
11 ADs
14 CFR sections
§ 43.13§ 43.16§ 43.3§ 43.9§ 43.5§ 23.303§ 23.562§ 23.561§ 23.341§ 23.473§ 23.301§ 23.337§ 23.321§ 23.471§ 23.307§ 23.621§ 23.625§ 23.785§ 23.787§ 23.613§ 23.611§ 23.1401§ 23.1397§ 23.1321§ 23.1311§ 27.1401§ 27.1397§ 91.205§ 91.407§ 91.409§ 133.43§ 133.47§ 45.15§ 21.607§ 21.303§ 21.305§ 27.321§ 27.471§ 27.561§ 27.307§ 27.785§ 27.787§ 27.613§ 29.785§ 29.787§ 29.613§ 25.307§ 25.561§ 25.613§ 29.307§ 29.561

Guidance, not mandatory unless a rule or AD requires it. DRS record last changed August 10, 2026.

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Show pages 125–136
Page 137OCROpen in PDF

FIGURE. 12-6. TYPICAL ALLOWABLE CARGO LOADING DIAGRAM AirDesign report 490-1 sheet E3 1906 Conard Circle prepared by H.Wells Austin, Texas 78734 checked by H. Wells Howard

(512) 266-5250 fax (512) 266-5052 revision G 183 Ibs.

100 Ibs. (45 kg.) 50 Ibs. each- (23 kg.) 28.737 NO LOAD heat duct) ST.A 106,628 TA 73.040 183 IDS STA 53 986 Seat belt fittings- 170 Ibs. each (77 kg.) 5441bs.- (247kg) Page 144 Par 1205