STC ST00111LA-D

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number STO0111LA-D Certificate

SURRENDERED This certificate issued to: Hollingsead International 2226 Goodyear Avenue on 6-23-09 Ventura, California 93003 Part 25 of the Federal Aviation Regulations.

Original Product Type Certificate Number A20WE Make: BOEING Model: 747-200B Description of Type Design Change:

Installation of a cargo handling system in accordance with AAR Advanced Structures Drawing List B.P. Report No.: 733 Rev. H, dated Dec. 3, 1995, or later FAA approved revisions, or later FAA approved revisions.

1. Installation of this STC is limited to those aircraft modified in accordance with STC ST00105LA-D. When installed, this installation, with cargo loaded, must maintain a minimum aisle width of 16 inches between the cargo containers and the fuselage to ensure access to the cargo door for the purpose of visual inspection of the cargo door latching/locking mechanism.

If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

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Date of Application: June 6, 1996 Date Reissued: April 1, 1998; June 13, 2005;

May 14, 2007 Date of Issuance: June 28, 1996 Date Amended:

By Direction of the Administrator FEDERAL AVIATION Callin K. Woo (Signature) Manager, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office TOMINISTRATON (Title)

TRANSFER ENDORSEMENT Transfer the ownership of the Supplemental Type Certificate Number_ to (Name of transferee) (Address of transfer) (Number and street) (City, State, and Zip code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and Zip code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: ST00111LA-D Limitations and Conditions: (Continued from page 1)

2. This modification is permitted to be operated with specific missing, broken, inoperable or malfunctioning restraint hardware only in strict compliance to Report Number BPS 584, Revision A, dated April 9, 1990, or later FAA approved revisions.

This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those previously approved modifications will introduce no adverse effect upon the airworthiness of the certified product. A copy of this STC must be included in the permanent record of the modified aircraft.

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