# STC SA1106CE-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Rockwell Collins Inc, United States
- Description: Installation of Collins Radio Group AP-106 3-axis autopilot system and interface with Collins FD-112V flight director.
- Applied: May 12, 1975
- Status date: September 12, 1997
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A16](https://openairdocs.org/tcds/3A16)
- Certificate PDF: https://openairdocs.org/files/sha256/e1/fa/e1faa77584b74bedb47d97e9a8acbb28ecf99d77d964a846343e7be3717ae500
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3511B9852ECE512286257A21005BAA5D.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA1106CE-D

## ADs that name it (0)

None.

## Approved models (2)

- Hawker Beechcraft Corporation 58 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Hawker Beechcraft Corporation 58A ([TCDS 3A16](https://openairdocs.org/tcds/3A16))

## 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 SAI106CE-D This certificate issued to: Rockwell Collins, Inc.

Avionics & Communications 400 Collins Road NE, MS 164-100 Cedar Rapids, LA 52498 Part 3 of the Civil Air Poegulations.

Original Product Typo Certificale Number: 3A16 Make: Beech Model: 58,58A Description of Type Design Change: Installation of the Collins Radio Group AP-106 3 Axis Autopilot System and interface with the Collins FD-112V Flight Director. DATA REQUIRED: (1) Collins Drawing No. 992-1139-001, Revision A, dated November 18, 1975, or "FAA Approved" revisions. (2) FAA Approved Airplane Flight Manual Supplement for Beech Models 58, 58A, dated June 25, 1975.

Limitations and Conditions: This approval should not be extended to other specific airplanes of this model on which other previously approved modifications 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. 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: May 12, 1975 Date Reissued: September 12, 1997 Date of Issuance: June 25, 1975 Date Amended: March 15, 1976 FEDERAL AVIATION By Direction of the Administrator Val R. Koonto (Signature) TOMINSTRATO Dale R. Koonts Manager, DAS-3CE (Title)

**PRA PORM 9110-2 (10-68) PAGE 1**

## Every issue (2)

- September 12, 1997: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/e1/fa/e1faa77584b74bedb47d97e9a8acbb28ecf99d77d964a846343e7be3717ae500)
- March 15, 1976: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/e1/fa/e1faa77584b74bedb47d97e9a8acbb28ecf99d77d964a846343e7be3717ae500)

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