# STC SA2765CE-D

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Rockwell International Collins Commercial Avionics, United States
- Description: Installation of Alternate Autopilot Computer, APC-65H, Collins Part Number 622-9724-119
- Applied: August 6, 1992
- Status date: August 31, 1992
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A9EA](https://openairdocs.org/tcds/A9EA)
- Certificate PDF: https://openairdocs.org/files/sha256/be/7d/be7df8ba1a21a4922b1ec06a8a54f522ea3b40bedd333b15b5ab65d5f9d23575
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5A54BACB1FA3171486258130005BEA02.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2765CE-D

## ADs that name it (0)

None.

## Approved models (1)

- Viking Air Limited DHC-6-300 ([TCDS A9EA](https://openairdocs.org/tcds/A9EA))

## What the certificate says

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

United States of America Ex l Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA2765CE-D This certificate issued to: Rockwell International Collins Commercial Avionics 400 Collins Road NE Cedar Rapids, IA 52498 Purt 23 the Federal Aviation Regulations:

Original Product - Type erlificate Number: AGEA Make: DeHavilland Aircraft Model: DHC-6-300 Description of Type Design Change: Installation of Alternate Autopilot Computer, APC-65H, Collins Part Number 622-9724-119, in accordance with Collins Drawing Index 992-1983-001, no revision, dated August 31, 1992 or later FAA approved revision.

Limitations and Conditions: Installation of DeHavilland Service Bulletin 6/505, is a prerequisite to this STC. This approval should not be extended to other specific airplanes of this model on which other previously approved modification are incorporated, unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane.

Date of Application: August 6, 1992 Date Reissued:

Date of Issuance: . August 31, 1992 Date Amended:

FEDERAL AVIATION By Direction of the Administrator Vali R. Monta TO MINISTRAID Jer Terald R. Lamb Manager, DAS-3CE (Signature ) (Title)

## Every issue (1)

- August 31, 1992: Issued, Current. [certificate](https://openairdocs.org/files/sha256/be/7d/be7df8ba1a21a4922b1ec06a8a54f522ea3b40bedd333b15b5ab65d5f9d23575)

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