# STC SA02449NY

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Marinvent Corporation, Canada
- Description: Installation of Honeywell Epic Control Display System
- Applied: March 14, 2006
- Status date: August 23, 2007
- Product: Aircraft, Single-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A59EU](https://openairdocs.org/tcds/A59EU)
- Certificate PDF: https://openairdocs.org/files/sha256/39/26/39261d0c33fd2994b64fee8b7501ac2f09b5c7305d098a432b817314910b4f33
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D8E9BF84F6A6613F86257369004DA296.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02449NY

## ADs that name it (0)

None.

## Approved models (1)

- Piaggio Aero Industries S.p.A. P-180 ([TCDS A59EU](https://openairdocs.org/tcds/A59EU))

## 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.

This certificate issued to Marinvent Corporation 50, chemin de la Rabastalière Est, Suite 23 St-Bruno, QC Canada J3V 2A5

Part 23 of the Federal Aviation Regulations.

Original Product -- Type Certificate Number: A59EU

Make: PIAGGIO AERO INDUSTRIES S.p.A

Model: P-180

The installation of Honeywell Epic Control Display System to be done in accordance with Avionics Design Services Ltd. Master Drawing List MDL05123, Revision B, dated April 5, 2007, or later Transport Canada approved revision.

1. Operation must be in accordance with Marinvent Corporation Flight Manual Supplement FMS05123-1, Revision A, Transport Canada approved April 5, 2007, or later Transport Canada approved revision.

2. Maintenance must be in accordance with Avionics Design Services Ltd. Instructions for Continued Airworthiness ICA05123-1, Revision A, Transport Canada accepted April 5, 2007, or later Transport Canada accepted revision.

3. Basis of certification as defined in TCDS A59EU, Revision 15, plus FAR 23.1322, 23.1331 at amendment 23-43 and FAR

23.867, 23.1321, 1353(h) at amendment 23-49.

4. Equivalent safety findings exists with respect to the following regulation: 23.1545 (b)(4) Airspeed Indicator. RVSM operation not affected by this design change.

Date of application: March 14, 2006

Date of issuance: August 23, 2007 Date amended:

( Signature) Anthony Socias Manager New York Aircraft Certification Office

( Title)

FAA Form 8110-2-1(10-69) Page 2 of 2

Number SA02449NY Date of Issuance: August 23, 2007

5. A placard reading “MAXIMUM FLAP DN OPERATING SPEED: 150 KIAS” must be installed on the right side of the center console adjacent to the flap lever.

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

7. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

…………………………..END…………………………..

## Every issue (1)

- August 23, 2007: Issued, Current. [certificate](https://openairdocs.org/files/sha256/39/26/39261d0c33fd2994b64fee8b7501ac2f09b5c7305d098a432b817314910b4f33)

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