# STC ST00146WI-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Installation of Bendix/King CAS 66A TCAS I System.
- Status date: April 24, 2020
- Product: Aircraft, Large Airplane
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A52EU](https://openairdocs.org/tcds/A52EU)
- Certificate PDF: https://openairdocs.org/files/sha256/1a/45/1a454c36f4eba7d19028b258a88304d1007a4d4c26df99cca292cf9c49a1d90e
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E1927F0E54D1DB5B862585D100669DA8.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/ST00146WI-D

## ADs that name it (1)

- [AD 2011-09-02](https://openairdocs.org/ad/2011-09-02): Fuselage · Saab AB, Saab Aerosystems 340A (SAAB SF340A) and SAAB 340B with STC SA984GL-D or 2 others. Effective May 25, 2011. Named in the applicability

## Approved models (2)

- Saab Aircraft AB 340A (SAAB-SF340A) ([TCDS A52EU](https://openairdocs.org/tcds/A52EU))
- Saab Aircraft AB SAAB 340B ([TCDS A52EU](https://openairdocs.org/tcds/A52EU))

## 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 (5/14) Page 1 of 2 Number: ST00146WI-D This certificate issued to: Honeywell International Inc.

21111 N 19th Ave Phoenix, Arizona 85027 Part 25 of the Federal Aviation Regulations.

Original Product – Type Certificate Number: Make: Saab-Fairchild (SAAB) A52EU Model: SF340A, 340B Description of Type Design Change:

Installation of the Bendix/King CAS 66A TCAS I System.

REQUIRED DATA: 1. Master Drawing List 155-09666-0000, Rev. 1, dated 3-21-94 and 2. Airplane Flight Manual Supplement 006-00829-0000, dated 3-29-94. Later FAA approved revisions to the above listed data are incorporated without further revision to this Supplemental Type Certificate.

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 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: 3-8-94 Date Reissued: 2-28-00; 4-24-20 Date of Issuance: 3-29-94 Date Amended:

By Direction of the Administrator Signature Richard B. Sleigh Title ODA Administrator, ODA-602216-NM

FAA Form 8110-2 (5/14) Page 2 of 2

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

## Every issue (1)

- April 24, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/1a/45/1a454c36f4eba7d19028b258a88304d1007a4d4c26df99cca292cf9c49a1d90e)

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