# STC SA00132WI-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Rockwell Collins Inc, United States
- Description: Installation of alternate Air Data Computer, ADC-85, Collins Part Number 622-8051-003 and Air Data Module, ADM-85, Collins Part Number 622-8692-015, in accordance wiht Collins Drawing Index 992-2982-001, no revision, dated June 16, 1993 or later approved revision.
- Applied: December 10, 1992
- Status date: August 22, 1997
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/71/c2/71c2be6cf9c9412f7406b6a7e623d964b93b4aa388acdd070b4b3682699ec0da
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/CF5C13C39A42B0CC8625788C0057984B.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00132WI-D

## ADs that name it (0)

None.

## Approved models (2)

- Hawker Beechcraft Corporation B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B300C (C-12W) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))

## 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: SA00132WI-D This certificate issued to: Rockwell Collins, Inc.

400 Collins Road NE, MS 164-100 Cedar Rapids, IA 52498 Part 23 of the Federal Aviation

•Regulations.

Original Product Type Certificate Number : A24CE Make: Beech Aircraft Corporation Model: B300/B300С Description of Type Design Change: Installation of alternate Air Data Computer, ADC-85, Collins Part Number 622-8051-003 and Air Data Module, ADM-85, Collins Part Number 622-8692-015, in accordance with Collins Drawing Index 992-2982-001, no revision, dated June 16, 1993 or later FAA approved revision.

Limitations and Conditions: (1) 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. (2) 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: December 10, 1992 Date Reissued: August 22, 1997 Date of Issuance: February 2, 1994 Date Amended:

FEDERAL AVIATION By Direction of the Administrator ValeR Rents (Signature) Dale R. Koonts TOMINSTRATO Manager, DAS-3CE (Title) 47

## Every issue (1)

- August 22, 1997: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/71/c2/71c2be6cf9c9412f7406b6a7e623d964b93b4aa388acdd070b4b3682699ec0da)

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