# STC SA03342NY

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Marsh Brothers Aviation Inc, Canada
- Description: Installation of the replacement to the OEM landing gear door hinge bushings
- Applied: July 19, 2013
- Status date: November 14, 2013
- Product: Aircraft, Small Airplane
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 3A16](https://openairdocs.org/tcds/3A16)
- Certificate PDF: https://openairdocs.org/files/sha256/8f/70/8f70f1710f4e5a000146604f946e120f3442277cd9ae94b1f14de5a15b1388cd
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/344222987BE9C45C86257CEE006F7EB4.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA03342NY

## ADs that name it (0)

None.

## Approved models (21)

- Beechcraft Corporation 56TC ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation 58 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation 58A ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation 95 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation 95-55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation 95-A55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation 95-B55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation 95-B55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation 95-B55B ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation 95-C55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation 95-C55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation A56TC ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation B95 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation B95A ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation D55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation D55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation D95A ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation E55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation E55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation E95 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation G58 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))

## 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

Part 3 of the Civil Aviation R egulations.

Original Product – Type Certificat e N umber:

Description of Type Design Chang e:

Installation of the replacement to the OEM landing gear door hinge bushings, in accordance with Marsh Brothers Aviation Inc.

Installation Instructions II0002, Revision Original, dated November 1, 2012 or later Transport Canada approved revision.

For Instructions for Continued Airworthiness refer to Marsh Brothers Aviation Inc. Maintenance Manual Supplement, MMS0002, Revision Original, dated November 1, 2012, or later Transport Canada accepted revision.

1. Mandatory replacement time and/or inspection intervals, defined in the “Airworthiness Limitation” section of Marsh Brothers Aviation Inc. Maintenance Manual Supplement, MMS0002, Revision Original, dated November 1, 2012, or later Transport Canada accepted revision, are to be complied with.

Marsh Brothers Aviation Inc.

3225 Mainway Burlington, Ontario Canada L7M 1A6 3A16 Beechcraft Corporation M ake:

M odel:

56TC, 58, 58A, 95, 95-55, 95-A55, 95- B55, 95-B55A, 95-B55B, 95-C55, 95- C55A, A56TC, B95, B95A, D55, D55A, D95A, E55, E55A, E95, G58

Date of application : July 19, 2013

Date of issuance : November 14, 2013 Date reissued:

B y direction of the A dministrator

(Signature) Gaetano Sciortino Manager New York Aircraft Certification Office

(Title)

FAA Form 8110-2-1(10-69) Page 3 of 3

N umber SA03342NY

Date of Issuance: November 14, 2013

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

3. 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.

..……………END………………..

## Every issue (1)

- November 14, 2013: Issued, Current. [certificate](https://openairdocs.org/files/sha256/8f/70/8f70f1710f4e5a000146604f946e120f3442277cd9ae94b1f14de5a15b1388cd)

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