# STC SA5935SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Textron Aviation Inc, United States
- Description: Installation of Sperry EDZ-610/611 electronic flight instrument system with a Sperry primus 650 or800 weather radar system.
- Status date: December 12, 2016
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A3EU](https://openairdocs.org/tcds/A3EU)
- Certificate PDF: https://openairdocs.org/files/sha256/ad/55/ad5580898bc0363cf1386534cd64d1c7612b8e635fb322ea6fe0898a4e4d0b39
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1A9D19DADCF405CE86258148006AC6BF.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA5935SW

## ADs that name it (0)

None.

## Approved models (1)

- Hawker Beechcraft Corporation BAe.125 Series 800A ([TCDS A3EU](https://openairdocs.org/tcds/A3EU))

## 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

Part of the

Signature

Title Textron Aviation Inc.

One Cessna Boulevard Wichita, KS 67215 2 SA5935SW Civil Air Regulations.

4b Installation of Sperry EDZ-610 or EDZ-611 Electronic Flight Instrument System with a Sperry Primus 650 or Primus 800 Weather Radar System in accordance with Arkansas Aerospace, Inc. Drawing List No. 800-010, Revision FF, dated December 19, 1991, or later FAA approved revision.

NOTE: The installation on Airplane Serial No. 258027 was a one only STC based on Arkansas Aerospace, Inc. Drawing List No. 800-010, Revision DD, dated July 2, 1991.

British Aerospace BAe 125-800A The following FAA approved Airplane Flight Manual Supplement or later FAA approved revision is required: EDZ-610 requires AFMS dated May 15, 1985, or Revision A dated December 5, 1985. EDZ-611 requires AFMS dated March 18, 1986; or AFMS dated April 30, 1987; or AFMS dated June 2, 1989, or Revision A dated July 5, 1989, or Revision B dated May 25, 1990, or Revision C dated July 3, 1991. Compatibility of this design change with previously approved modifications must be determined by the installer. 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.

May 14, 2003; March 26, 2007;

December 12, 2016 March 14, 1984 May 15, 1985 A3EU December 5, 1985; March 18, 1986; April 30, 1987; June 2, 1989; July 5, 1989; May 25, 1990;

December 19, 1991 Mark Fuller STC ODA administrator ODA-100129-CE

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

To (Name and address of transferee)

From (Name and address of grantor)

## Every issue (2)

- December 12, 2016: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/ad/55/ad5580898bc0363cf1386534cd64d1c7612b8e635fb322ea6fe0898a4e4d0b39)
- March 26, 2007: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/12/34/1234f1359b3df3d67b2d024012eb6f4158c14c7884c2a55e576f7f076bbaa2ab)

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