# STC SA02825LA

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Satco Inc., United States
- Description: Installation of a Unit Load Device (ULD), including pallet, net, and container
- Applied: January 9, 2022
- Status date: April 17, 2024
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Data sheets: [TCDS A00016WI](https://openairdocs.org/tcds/A00016WI)
- Certificate PDF: https://openairdocs.org/files/sha256/de/54/de5414b756e28c8854a820500771362e47301ed27dd0618caa6397ad5cd889b9
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149433495820240430204223.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA02825LA

## ADs that name it (0)

None.

## Approved models (1)

- Textron Aviation Inc. 408 ([TCDS A00016WI](https://openairdocs.org/tcds/A00016WI))

## 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.

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Number SA02825LA

This Certificate issued to Satco Inc.

1601 E. El Segundo Blvd.

El Segundo, CA 90245 Part 23** of the Federal Aviation Regulations.

Original Product - Type Certificate Number: A00016WI Make :

Textron Aviation Inc.

Description of Type Design Change: Installation of a Unit Load Device (ULD), including pallet, net, and container in accordance with Satco Controlled Drawing Lists CD37670-501 Revision A, dated December 14, 2023, 37671-501 Revision A, dated December 14, 2023, and 37672-501 Revision A, dated December 15, 2023, or later approved revisions.

Limitations and Conditions: This Supplemental Type Certificate (STC) is eligible only on Textron Model 408 aircraft in the Freighter Variant with the Ancra Cargo Loading System part number 85540-10, or later approved revisions.

Installation and operation shall be in accordance with Section VI – Weight And Balance Data and Equipment List of the FAA Approved Textron Model 408 Airplane Flight Manual 408FM-00, dated March 7, 2022, or later approved revisions. This installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this change and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the 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.

** Certification Basis:

Changed or affected areas complied with 14 CFR part 23 Amd’t (23–1) through (23–64)

Date of application : January 9, 2022

Date of issuance : April 17, 2024

(Signature) for Gregory S. DiLibero Manager, West Certification Branch Compliance & Airworthiness Division Aircraft Certification Service

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION

Number SA02825LA

## Every issue (1)

- April 17, 2024: Issued, Current. [certificate](https://openairdocs.org/files/sha256/de/54/de5414b756e28c8854a820500771362e47301ed27dd0618caa6397ad5cd889b9)

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