# STC SA13BO

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Woven Electronics LLC
- Description: Installation of a Sundstrand Mark VI ground proximity warning system.
- Status date: April 10, 2023
- Data sheets: A24CE
- Certificate PDF: https://openairdocs.org/files/sha256/4c/48/4c48c3f4a1c14d03e54dd5a5ce024236c9793a9f5ee6dad5b0d9df99cb595c45
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171986846520230918140921.0001
- Page: https://openairdocs.org/stc/SA13BO

## ADs that name it

None.

## Approved models (1)

- Beechcraft Corporation 1900C (C-12J) (TCDS A24CE)

## 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.

Title: (for) Robert Capezzuto Acting Manager, East Certification Branch Compliance and Airworthiness Division Aircraft Certification Service SA13BO Woven Electronics, LLC 16000 Pines Blvd #824431 Pembroke Pines, FL 33082-9599 Part 23 Federal Aviation Regulations A24CE Beech Aircraft Corporation 1900C Installation of a Sundstrand Mark VI Ground Proximity Warning System in a Beech Aircraft Corporation Model 1900C airplane, in accordance with AVITAS Engineering Report No. 93ECSW.001R-1, Revision B, dated December 28, 1993, or later FAA-approved revisions.

(Continued on Sheet 3) November 11, 1993 September 21, 2015; April 10, 2023 January 24, 1994 3

SA13BO 3

SA13BO Limitations and Conditions (Continued):

1. AVITAS Engineering Supplement, dated January 24, 1994 but unnumbered, to the basic Beech Aircraft Model 1900C Airplane Flight Manual, or later FAA-approved revisions, is required and must be carried in the aircraft during all flights.

2. The modifications approved by this STC must be installed in conjunction with those modifications approved by STC No. SA14BO.

3. This approval should not be incorporated in any aircraft of these models 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 those aircraft..

--------------------- END --------------------- 3 3

## Every issue (2)

- April 10, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/4c/48/4c48c3f4a1c14d03e54dd5a5ce024236c9793a9f5ee6dad5b0d9df99cb595c45)
- September 21, 2015: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/70/78/70781d026461ada8b9143ab5d01b36ac994c2e96c9b08bbde459f2682ce51f55)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.