# STC ST00144IB

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: TABY AIR MAINTENANCE AB, Sweden
- Description: Installation of LPV Approach and ADS-B Out capability
- Applied: August 21, 2023
- Status date: October 27, 2023
- Product: Aircraft, Large Airplane
- Certification basis: Part 25
- Data sheets: [TCDS A47NM](https://openairdocs.org/tcds/A47NM)
- Certificate PDF: https://openairdocs.org/files/sha256/c3/db/c3dbf50dfae520932ebf46cfb5ee5280120cbc31f6cf94bf800d680906d3af21
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184149826320231031141457.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/ST00144IB

## ADs that name it (0)

None.

## Approved models (1)

- Saab Aircraft AB SAAB 2000 ([TCDS A47NM](https://openairdocs.org/tcds/A47NM))

## 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.

**IMPORT ST00144IB**

**TABY AIR MAINTENANCE AB**

OREBRO AIRPORT S-70594 OREBRO SWEDEN Part 25 Title 14 Code of Federal Regulations A47NM Saab AB SAAB 2000

1. Installation of LPV Approach and ADS-B Out capability on SAAB 2000 must be in accordance with Taby Air Maintenance AB Master Data List 321006-C-DL-3461-001-02, dated 08th August 2023, or later EASA approved revisions.

2. Aircraft must be operated in accordance with Taby Air Maintenance AB Airplane Flight Manual Supplement 321006-C-AM-3461-002-07, Issue 07, dated 31st May 2023, or later EASA approved revisions.

(See Description of Type Design Change Continued on Page 3 of 3)

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

(See Limitations and Conditions Continued on Page 3 of 3) August 21, 2023 October 27, 2023 Anthony E. Gallo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 3

**IMPORT ST00144IB 3**

IMPORT ST00144IB Date of Issuance: October 27, 2023

Description of Type Design Change (continued):

3. Aircraft must be maintained in accordance with Taby Air Maintenance AB Instructions for Continued Airworthiness 321006-C-CA-3461-001-01, Issue 01, dated 22nd April 2022, or later EASA approved revisions.

4. Aircraft must be configured in accordance with Taby Air Maintenance AB MMEL supplement 321006-C-ME-3461-001-01, Issue 01, dated 22nd February 2023, or later EASA approved revisions.

2. If the holder agrees to permit another person to use the certificate to alter the product, the holder shall give the other person written evidence of that permission.

3. This STC is applicable to all serial numbers for this Make-Model.

4. Maintenance must be in accordance with the "Airworthiness Limitations" section of Taby Air Maintenance AB Instructions for Continued Airworthiness referenced in item 3 under description of type design change section of this STC or later EASA approved revisions.

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48A, the certification basis for the SAAB 2000 Series aircraft is as follows:

a. The type certification basis for SAAB 2000 Series is shown on TCDS A47NM for parts not changed or not affected by the change.

b. The modification certification basis for parts changed or affected by the change since the reference application date is shown on TCDS A47NM as 14 CFR Part 25 at Amendment 25-71.

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## Every issue (1)

- October 27, 2023: Issued, Current. [certificate](https://openairdocs.org/files/sha256/c3/db/c3dbf50dfae520932ebf46cfb5ee5280120cbc31f6cf94bf800d680906d3af21)

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