# STC SA5466NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Telair International LLC, United States
- Description: Installation of Telair International cargo loading systems
- Applied: July 31, 1990
- Status date: July 27, 2015
- Product: Aircraft, Large Airplane
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE)
- Certificate PDF: https://openairdocs.org/files/sha256/ae/72/ae72325f4525d4da4cab9862165af7c107128c0aabfa985dbe69df626e8ef913
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/79EE98B3D10DAD0E86257E9D00666F3F.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA5466NM

## ADs that name it (0)

None.

## Approved models (8)

- The Boeing Company DC-10-10 ([TCDS A22WE](https://openairdocs.org/tcds/A22WE))
- The Boeing Company DC-10-10F ([TCDS A22WE](https://openairdocs.org/tcds/A22WE))
- The Boeing Company DC-10-15 ([TCDS A22WE](https://openairdocs.org/tcds/A22WE))
- The Boeing Company DC-10-30 ([TCDS A22WE](https://openairdocs.org/tcds/A22WE))
- The Boeing Company DC-10-30F (KC-10A KDC-10) ([TCDS A22WE](https://openairdocs.org/tcds/A22WE))
- The Boeing Company DC-10-40 ([TCDS A22WE](https://openairdocs.org/tcds/A22WE))
- The Boeing Company MD-10-10F ([TCDS A22WE](https://openairdocs.org/tcds/A22WE))
- The Boeing Company MD-10-30F ([TCDS A22WE](https://openairdocs.org/tcds/A22WE))

## 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 25* of the Federal Aviation Regulations * Certification Basis is set forth in T. C. Data Sheet A22WE.

A22WE Boeing DC-10-10, -10F, -15, -30, -30F, -40, MD-10-30F, MD-10-10F Description of Type Design Change: Installation of Telair International cargo loading systems in accordance with FAA Approved Telair International Index List, ER 84850, Revision “D”, dated June 27, 2000, or later FAA approved revisions.

Limitations and Conditions: This installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. The approval of this modification applies to the above noted airplane model series only. 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.

Date of application : July 31, 1990

Date of issuance : August 28, 1991

Date reissued : December 14, 1993; October 20, 1997; March 8, 2002; March 9, 2005; January 10, 2012; May 12, 2015; July 27, 2015

Date amended : June 9, 1994; March 16, 1995;

October 4, 1996; June 29, 2000

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

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/ae/72/ae72325f4525d4da4cab9862165af7c107128c0aabfa985dbe69df626e8ef913)
- May 12, 2015: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/91/aa/91aac966aa73c05959b82e9e1805539e50ffface13ada04e20fb20e88285d370)
- January 10, 2012: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/c2/2e/c22e2593536b33d29729b99eb3d6d921a2891ccbbf783a21fc854e19dae54671)
- March 9, 2005: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/2f/f4/2ff4bc4b57c56a07e2b922f74ed7d2f58770a8e0982c5bb17e6930b9ec9160a7)

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