STC SA2801WE

This Certificate issued to Telair International, LLC 2220 E. Cerritos Avenue Anaheim, California 92806

Part 25* of the Federal Aviation Regulations * See T. C. Data Sheet A20WE Original Product Type Certificate Number :

A20WE Boeing B747-100, -200B

Description of Type Design Change: Installation of main deck cargo restraint system in accordance with FAA Approved Transequip Drawing List No. 275616, or later FAA approved revision.

Limitations and Conditions: The approval of this change in type design applies basically to the Boeing 747-100, -200B airplanes only. 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 other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight in the fuselage. This approval does not apply to the structural containers. The containers must meet the requirements of 14 CFR 25.333, 25.561, 25.855 and 25.857(d).

Date of application : March 6, 1973

Date of issuance : January 16, 1974

Date reissued : September 12, 1991; June 28, 2000; March 9, 2005; January 10, 2012;

May 12, 2015; July 27, 2015

(Signature) Supervisor, Technical & Administrative Support Staff Los Angeles Aircraft Certification Office (Title)

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Number SA2801WE

Date of Application: March 6, 1973 Date of Issuance: January 16, 1974 Date Reissued: September 12, 1991; June 28, 2000; March 9, 2005; January 10, 2012

Limitations and Conditions (Continued)

The dimension of the container base is 56.5” long by 29.0” wide and the overall dimensions are

61.5” long by 30.2” wide by 64.0” high. The C.G. of the unit must be within 3.0” fore and aft of the centerline, 1.5” laterally of the centerline and a maximum height of 30.0” from the base.

The gross weight of the container is limited to 875 pounds. No approval has been made of the partitions installed between the container system and the passenger compartment or the containers installed in the aircraft. Therefore, when the partitions and/or containers are installed, the aircraft must comply with the special passenger evacuation and crashworthiness requirements for type certification contained in Boeing Document D6-30800. A copy of this STC must be included in the permanent records of the modified aircraft.

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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