# STC ST09849AC

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Textron Aviation Inc, United States
- Description: Upgrade of a Honeywell NZ-2000 Flight Management System to NZ-2010 with 6.1 software
- Applied: June 29, 2014
- Status date: April 19, 2017
- Product: Aircraft, Large Airplane
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A3EU](https://openairdocs.org/tcds/A3EU)
- Certificate PDF: https://openairdocs.org/files/sha256/e6/cb/e6cb4cbe2746c2231677b8a38712ee577a67bd8545bbab2462a6e7508ee6c6d1
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/227BDFAB491449D08625817C0058C8F6.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/ST09849AC

## ADs that name it (0)

None.

## Approved models (3)

- Beechcraft Corporation BAe.125 Series 800A ([TCDS A3EU](https://openairdocs.org/tcds/A3EU))
- Beechcraft Corporation Hawker 800 ([TCDS A3EU](https://openairdocs.org/tcds/A3EU))
- Beechcraft Corporation Hawker 800XP ([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 ST09849AC Textron Aviation Inc.

One Cessna Boulevard Wichita, KS 67215 4b/25 Federal Aviation Regulations.

Beechcraft Corporation Hawker 800/800XP, BAe.125 Series 800A See sheet 3 for certification basis 3 A3EU Upgrade of a Honeywell NZ-2000 Flight Management System to NZ-2010 with 6.1 software in accordance with Aerospace Systems, Inc. Master Data List MDL916034-01, Rev. 3, dated July 30, 2015, or later FAA approved revision.

The installer must determine whether this design change is compatible with previously approved modifications. 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.

(see continuation sheet 3 of 3) September 9, 2015; September 21, 2015;

April 19, 2017 June 29, 2014 August 12, 2015 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)

FAA Form 8110-2 (5/14) Page 3 of

Date of Issuance: August 12, 2015 Date Reissued: April 19, 2017

Limitations and Conditions (cont'd):

FAA Approved Flight Manual Supplement, Aerospace Systems, Inc. document AFM916-034-01, Revision 01, dated August 10, 2015, or later FAA approved revision is required onboard the modified aircraft. Instructions for Continued Airworthiness (ICA), Aerospace Systems, Inc. document ICA916-034-01, Rev. 1, Dated October 9, 2014 or later FAA accepted revision must be made available to the operator at the time of installation.

Certification Basis:

Based on 14 CFR §21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be:

Regulations per Type Certificate data sheet A3EU (4b-1 through 4b-11 and 25-1 through 25-54):

CAR 4b: 200, 201, 202, 210, 230, 260, 300, 301, 302, 303, 304, 305, 306, 307, 600, 601, 605, 606, 611, 612, 621, 624, 625, 650, 740, 741, 742

Part 25: 613, 615, 1301, 1309, 1316, 1529

-- END -- 3 ST09849AC

## Every issue (2)

- April 19, 2017: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/e6/cb/e6cb4cbe2746c2231677b8a38712ee577a67bd8545bbab2462a6e7508ee6c6d1)
- September 21, 2015: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/0a/cd/0acddf1b1af462ea9240416118b90be615f56b623f19ecab2b5d1ec682a1f590)

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