7.  
D6-38278, MODEL 737-300/400/500 MAINTENANCE PLANNING DATA (MPD) DOCUMENT.

8.  
D6-38441, MODEL 737-500 STRUCTURAL REPAIR MANUAL (SRM).

9.  
D6-51702, MODEL 737 BOEING STANDARD OVERHAUL PRACTICES, CHAPTER 20.

10.
SERVICE LETTER 737-SL-51-25 SUPPLEMENTAL STRUCTURAL INSPECTION DOCUMENT (SSID) REPORTING PROCEDURES.

11.  
SERVICE LETTER 737-SL-51-29B DAMAGE TOLERANCE REQUIREMENTS FOR STRUCTURAL REPAIRS AND MODIFICATIONS.

Titles and prices of the documents and data referenced in this Supplemental Structural Inspection Document can be found in the Data & Services Catalog which is available on request from the address listed below.  The Data & Services Catalog is also available on the worldwide web at MyBoeingFleet.com.  MyBoeingFleet.com customers can browse, search and order products online.  To obtain desired documents follow the ordering instructions in the catalog.  Include purchase order with the appropriate document number and title, and send to:
Boeing Commercial Airplanes Group Attention:  Data and Services Management
P.O. Box 3707, Mail Stop 2H-65 Seattle, Washington  98124-2207  USA Tel. (206) 544-5000 Fax. (206) 865-5725
1.  
Can be obtained from the applicable airworthiness authority.

2.  
AD applies to 737-100/200 aircraft. An AD for 737-300/400/500 aircraft is expected as a result of this SSID release.

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1.0  PURPOSE

The purpose of the Supplemental Structural Inspection Program is to ensure continuing structural airworthiness of 737-300/-400/-500 airplanes that have a high number of flight cycles in accordance with the requirements of FAA AC 91-56A and UK CAA Airworthiness Notice No. 89.  This FAA approved document provides operators with data to be used in evaluating and supplementing their existing structural inspection program.
It is important to realize that:
1.  The FAA has issued an Airworthiness Directive (AD), 98-11-04 R1, requiring implementation of a Supplemental Structural Inspection Program for Model 737-100/-200 airplanes, document D6-37089. It is expected that the FAA will issue an AD requiring implementation of a Supplemental Structural Inspection Program for Model 737-300/-400/-500 airplanes subsequent to the release of this document.
SSID Revision  AD  Effective Date 
Not Applicable  Nonea  Not Applicable 

a.  AD not released at printing of SSID revision
2.  This document identifies Significant Structural Items (SSIs) having fatigue crack growth characteristics warranting special attention and requiring inspection to assure timely detection of damage;
.  The inspection requirements defined by this document are based on the premise that operators are applying and will continue to apply an approved structural inspection program for identification of cracks, corrosion and other forms of damage on their 737-300/-400/-500 airplanes;
　
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