# STC SA6046NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Installation of Primus 2000 integrated avionics system.
- Applied: March 8, 1989
- Status date: March 18, 2020
- Product: Aircraft, Large Airplane
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A9NM](https://openairdocs.org/tcds/A9NM)
- Certificate PDF: https://openairdocs.org/files/sha256/d5/61/d561ec36b3dfc46979e7988dca2e6f9128d03b17ca49999eea184fb0573343d7
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C1B1C2F28328225F8625861E007936BE.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA6046NM

## ADs that name it (0)

None.

## Approved models (1)

- Textron Aviation Inc. 650 ([TCDS A9NM](https://openairdocs.org/tcds/A9NM))

## 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.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 1 of 3 FAA Form 8110-2 (5/14)

Number: SA6046NM This certificate issued to: Honeywell International Inc.

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

Original Product – Type Certificate Number: Make: Cessna Model:

A9NM 650, Citation III

Installation of Honeywell Primus 2000 Integrated Avionics System in accordance with FAA Approved Honeywell Inc.

Master Data List, Honeywell Document No. 1050-0727, Revision "B", dated June 28, 1993, or later FAA approved revision.

Honeywell Airplane Flight Manual Supplement, Document No. 1050-0721, Revision "NC", FAA approved on July 30, 1993, or later FAA approved revision is required aspart of this modification.

1) The approval of this change in type design appliesto the above listed model only.

2) This approval should not be extended to other aircraft of this model on which other previously approved modificationsare incorporated unlessit isdetermined by the installer that the interrelationship between this change and any of those other previously approved modificationswill not introduce any adverse affect on the airworthinessof the aircraft.

Date of Application: May 8, 1989 Date Reissued: March 2, 2009, March 18, 2020

Date of Issuance: July 30, 1993 Date Amended:

Signature

Title Richard B. Sleigh ODA Administrator, ODA-602216-NM

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 2 of 3 FAA Form 8110-2 (5/14)

To (Name and address of transferee)

From (Name and address of grantor)

## Every issue (2)

- March 18, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/d5/61/d561ec36b3dfc46979e7988dca2e6f9128d03b17ca49999eea184fb0573343d7)
- March 2, 2009: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/91/fa/91fa56bca60cd51dab60d0dd3ad5546c9c48a829525c64b91942fd5f3d0225ba)

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