# STC SA2773WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Telair International LLC, United States
- Description: Installation of Tridair Industries 3G Net Assy. Part No. 43568-1201 used in conjunction with unit load devices NAS3610-2A4P or Satco Pallet Assy. Part No. 31095-505
- Applied: August 30, 1973
- Status date: July 27, 2015
- Product: Aircraft, Large Airplane
- Certification basis: Part 21
- Data sheets: [TCDS 4A26](https://openairdocs.org/tcds/4A26)
- Certificate PDF: https://openairdocs.org/files/sha256/66/09/6609a4048a4fdb574335e7aeaedf025f8c42f8b66ebbb459924dd8e063f5ed1c
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DF4D99B2FAB287A886257E9D00604469.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2773WE

## ADs that name it (0)

None.

## Approved models (1)

- The Boeing Company 707-300C Series ([TCDS 4A26](https://openairdocs.org/tcds/4A26))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

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

Part 4b* of the Civil Air Regulations * See T. C. Data Sheet 4A26.

4A26 Boeing 707-351C

Description of Type Design Change: Installation of Tridair Industries 3G Net Assy. Part No. 43568-1201 used in conjunction with unit load devices NAS3610-2A4P or Satco Pallet Assy. Part No. 31095-505 per FAA Approved Loading Instructions No. 43597. See weight and balance manual referenced to in T.C.

Data Sheet 4A26. The maximum allowable gross cargo load of this pallet-net combination is 13,300 lbs.

Limitations and Conditions: The approval of this change in type design applies basically to model Boeing 707-351C aircraft 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 of the fuselage. 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.

Date of application : August 30, 1973

Date of issuance : October 18, 1973

Date reissued : November 25, 1974; December 7, 1981; February 6, 1987; June 28, 2000;

March 9, 2005; January 10, 2012; May 12, 2015;

July 27, 2015

Date amended : May 16, 1975

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

NOTE:

**DO NOT DELETE THIS PAGE.**

**DO NOT ADD ANY DATA TO THIS PAGE.**

**THIS PAGE IS FOR PAGE NUMBERING PURPOSES, PLEASE DISCARD PRINTED COPY.**

Number (STC No.)

## Every issue (4)

- July 27, 2015: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/66/09/6609a4048a4fdb574335e7aeaedf025f8c42f8b66ebbb459924dd8e063f5ed1c)
- May 12, 2015: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/43/49/4349ec1c1753460a050b0f67cb33bf4bdf12158193f0b229fc9e09fcf6d8aa5a)
- January 10, 2012: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/2f/e5/2fe531469da7943240c97aa0b378a9b5423a50bcc5ba0dac0c8d5f4be6bf85b4)
- March 9, 2005: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/95/84/95843d7b1bffc795b1e0eb5358c377b8ea0783b8cdf74e2791c97e847e1ec883)

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