# STC SA2667WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Textron Aviation Inc, United States
- Description: Installation of Sperry SPZ-200 autopilot and Stars Instrument System or SPI-77C flight director system.
- Status date: December 12, 2016
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A20](https://openairdocs.org/tcds/3A20)
- Certificate PDF: https://openairdocs.org/files/sha256/f8/76/f8768e8fd4af572c3cefffb0a7d573a8dae99ce55531e3ca660d4eebd52a112b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A24CE3D4010DB9798625814800685AD1.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2667WE

## ADs that name it (0)

None.

## Approved models (1)

- Hawker Beechcraft Corporation E90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))

## 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 SA2667WE Civil Air Regulations * 3 Beech Aircraft Corporation 3A20 E90 *See Type Certificate Data Sheet 3A20

1. Installation of a Sperry SPZ-200 Autopilot and Stars Instrument System or SPI-77C Flight Director Instrument System in accordance with Beech Aircraft Corp. Drawing No. 90500022 as revised by Change Order No. D33813A, D36334 and D38766. FAA approved AFM Supplement dated March 23, 1973 is required. OR

2. Installation of Sperry SPZ-200 Autopilot and single flight director STARS IVC configuration defined by Beech Drawings 90-500022 Revision A, R-210015 Revision A, R-750029 Revision A, and FAA Approved AFM Supplement dated February 6, 1974.

The approval of this change in type design applies basically to Model E90 airplanes only. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. 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.

September 17, 1973; April 15, 1996;

March 26, 2007; December 12, 2016 April 25, 1973; March 7, 1974 December 18, 1972 March 23, 1973 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/f8/76/f8768e8fd4af572c3cefffb0a7d573a8dae99ce55531e3ca660d4eebd52a112b)
- March 26, 2007: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/4a/15/4a1575ef1182034c54d9a9330c22b229154d1344ed7bb727f0f0b97dbc818586)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.