# STC SA2043NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Boeing Company, United States
- Description: Installation of Delco Performance Management System
- Applied: March 12, 1984
- Status date: September 7, 2010
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE)
- Certificate PDF: https://openairdocs.org/files/sha256/76/95/76953d68babd39c68a612083e57d22ec41b6bea7d19a1fb8183e8f386aeef912
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1F67E570B3A81B4986257877007031A8.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2043NM

## ADs that name it (0)

None.

## Approved models (3)

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

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA2043NM This certificate issued to: The Boeing Company 4000 Lakewood Boulevard Long Beach, California 90808 Part 25* of the Federal Poviation Pegulations.

*see Type Certificate Data Sheet No. A22WE Original Product Type Certificate Number A22WE Make: Boeing Model: DC-10-30, -30F, -40 Description of Type Design Change: Installation of Delco Performance Management System in accordance with FAA approved McDonnell Douglas Report Number J2952, No Revision, dated March 9, 1984, or later FAA approved revision. Flight Manual Supplement Number MDC-J1030/J1040/J5830, No Revision, FAA approved on April 3, 1984, or later FAA approved revision, is required as part of this installation.

Limitations and Conditions: . This approval should not be incorporated on 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.

FAR Form 8110-2(10-68) I FAR. 21.47

## Every issue (1)

- September 7, 2010: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/76/95/76953d68babd39c68a612083e57d22ec41b6bea7d19a1fb8183e8f386aeef912)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.