What it approves
Installation of the replacement to the OEM landing gear door hinge bushings
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may 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 II0001, 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, MMS0001, 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, MMS0001, Revision Original, dated November 1, 2012, or later Transport Canada accepted revision, are to be complied with.
This certificate and the supporting data which is the basis for appro val shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the A dministrator of the F ederal A viation A dministration .
Marsh Brothers Aviation Inc.
3225 Mainway Burlington, Ontario Canada L7M 1A6 3A15 Beechcraft Corporation M ake:
M odel: 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, 36, A36, A36TC, B36TC, E33, E33A, E33C, F33, F33A, F33C, G33, G36, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B Date reissued:
B y direction of the A dministrator
(Signature) Gaetano Sciortino Manager New York Aircraft Certification Office
(Title)
Date of application : July 9, 2013
Date of issuance: November 14, 2013
FAA Form 8110-2-1(10-69) Page 3 of 3
N umber SA03343NY
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………………..
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 27
| Make | Model | Data sheet |
|---|---|---|
| Beechcraft Corporation | 35-33 | 3A15 |
| Beechcraft Corporation | 35-A33 | 3A15 |
| Beechcraft Corporation | 35-B33 | 3A15 |