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| Commercial Airplanes 737
 Service Bulletin
 ALERT
 Number: 737-53A1319
 Original Issue: April 04, 2011
 ATA System: 5331
 SUBJECT: FUSELAGE - Skin - Crown Skin Lap Joint - Inspection for Lower Row Cracking at
 Stringer S-4, Between BS 360 and BS 908
 Export of this technology is controlled under the United States Export Administration Regulations (EAR) (15
 CFR 730-774). An export license may be required before it is used for development, production or use by foreign
 persons from specific countries. The controller of this data has the individual responsibility to abide by all export
 laws.
 ECCN: 9E991
 BOEING PROPRIETARY, CONFIDENTIAL, AND/OR TRADE SECRET
 Copyright . 2011 The Boeing Company
 Unpublished Work - All Rights Reserved
 Boeing claims copyright in each page of this document only to the extent that the page contains copyrightable
 subject matter. Boeing also claims copyright in this document as a compilation and/or collective work.
 This document includes proprietary information owned by The Boeing Company and/or one or more third parties.
 Treatment of the document and the information it contains is governed by contract with Boeing. For more
 information, contact The Boeing Company, P.O. Box 3707, Seattle, Washington 98124.
 Boeing, the Boeing signature, the Boeing symbol, 707, 717, 727, 737, 747, 757, 767, 777, 787, Dreamliner,
 BBJ, DC-8, DC-9, DC-10, KC-10, KDC-10, MD-10, MD-11, MD-80, MD-88, MD-90, P-8A, Poseidon and the
 Boeing livery are all trademarks owned by The Boeing Company; and no trademark license is granted in
 connection with this document unless provided in writing by Boeing.
 BOEING PROPRIETARY -
 Copyright . Unpublished Work - See page 1 for details.
 Original Issue: April 04, 2011
 737-53A1319
 1 of 33
 2.0
 BOEING PROPRIETARY -
 Copyright . Unpublished Work - See page 1 for details.
 Original Issue: April 04, 2011
 737-53A1319
 2 of 33
 BOEING SERVICE BULLETIN 737-53A1319
 ALERT ALERT
 BLANK PAGE
 Table of Contents
 Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5
 1. PLANNING INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9
 A. Effectivity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9
 1. Airplanes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9
 2. Spares Affected . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12
 B. Concurrent Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12
 C. Reason . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13
 D. Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13
 E. Compliance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13
 F. Approval . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14
 G. Manpower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14
 H. Weight and Balance Changes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14
 I. Electrical Load Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14
 J. References . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14
 1. Existing Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14
 2. Data supplied with this Service Bulletin . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14
 3. Installation Drawings Used in the Preparation of this Service Bulletin . . . . . . . . . . . . 14
 K. Publications Affected . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14
 L. Interchangeability and Intermixability of Parts . . . . . . . . . . . . . . . . . . . . . . . . . . . 15
 2. MATERIAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17
 A. Material - Price and Availability . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17
 B. Industry Support Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17
 C. Parts Necessary For Each Airplane . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17
 1. Kits/Parts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17
 2. Parts and Materials Supplied by the Operator . . . . . . . . . . . . . . . . . . . . . . . . 17
 3. Parts Modified and Reidentified . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17
 4. Parts Removed and Not Replaced . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17
 D. Parts Necessary to Change Spares . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17
 E. Special Tooling - Price and Availability . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17
 F. Special Tooling Necessary to do this Service Bulletin . . . . . . . . . . . . . . . . . . . . . . . 17
 3. ACCOMPLISHMENT INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19
 A. GENERAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19
 B. WORK INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20
 FIGURE 1: EXTERNAL INSPECTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21
 FIGURE 2: ALTERNATIVE INTERNAL INSPECTION . . . . . . . . . . . . . . . . . . . . . . . . . . 23
 FIGURE 3: CONFIRMING A CRACK INDICATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26
 FIGURE 4: SECOND EXTERNAL INSPECTION - INSPECTION LOCATION . . . . . . . . . . . . . . 29
 FIGURE 5: INSPECTION ZONES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31
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