# STC SA02303NY

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Infinion Certification Engineering, Canada
- Description: Installation of a Single or Dual Port Fuselage Camera Hole Cutout
- Applied: September 18, 2006
- Status date: March 26, 2019
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A20SO](https://openairdocs.org/tcds/A20SO)
- Certificate PDF: https://openairdocs.org/files/sha256/d9/ce/d9ce9800393f91f833d9ea7e568ce728196f604a8136506c7edd88ef151ac2e1
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/628402CE41EFF4478625859E0050F25E.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02303NY

## ADs that name it (0)

None.

## Approved models (4)

- Piper Aircraft Inc. PA-31 ([TCDS A20SO](https://openairdocs.org/tcds/A20SO))
- Piper Aircraft Inc. PA-31-300 ([TCDS A20SO](https://openairdocs.org/tcds/A20SO))
- Piper Aircraft Inc. PA-31-325 ([TCDS A20SO](https://openairdocs.org/tcds/A20SO))
- Piper Aircraft Inc. PA-31-350 ([TCDS A20SO](https://openairdocs.org/tcds/A20SO))

## 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 SA02303NY Infinion Certification Engineering #12-6213 TWP RD 122 Cypress County, AL - Canada - T1A 8M4 Civil Air Regulations.

1. Installation of a Single or Dual Port Fuselage Camera Hole Cutout to be done in accordance with Transport Canada Civil Aviation (TCCA) approved Infinion Installation Instructions E0-1141-01 Issue 5, dated February 18, 2019 or later TCCA approved revision.

2. Maintenance of the Single or Dual Port Fuselage Camera Hole Cutout must be in accordance with TCCA accepted Infinion Maintenance Manual Supplement MMS-1141-01 Issue 5, dated February 14, 2019 or later TCCA accepted revision.

3. Operation of this modification must be in accordance with TCCA approved Infinion Flight Manual Supplement FMS-1141-01 Issue 3, dated February 18, 2019 TCCA approved February 20, 2019 or later TCCA approved revision.

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

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.

Anthony E. Gallo Manager New York ACO Branch Piper Aircraft, Inc.

PA-31 PA-31-300 PA-31-325 PA-31-350 July 8, 2015, March 26, 2019 September 18, 2006 October 17, 2006 IMPORT A20SO 2

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

To (Name and address of transferee)

From (Name and address of grantor)

2 SA02303NY

## Every issue (2)

- March 26, 2019: Amended, Current. [certificate](https://openairdocs.org/files/sha256/d9/ce/d9ce9800393f91f833d9ea7e568ce728196f604a8136506c7edd88ef151ac2e1)
- July 8, 2015: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/c4/4b/c44bf59e24bbe7b0b0b9444236069b1065b32064cab5c99fd4e73e7f8a952b94)

---
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.
