STC SA4328WE

Supplemental type certificate · Dynamic Aviation Group Inc.

Holder
Dynamic Aviation Group Inc. · United States
Status
Current · Reissued
Status date
October 2, 2014
Applied
November 5, 1980
Product
Aircraft · Small Airplane
Certification basis
Part 3, Part 21
Data sheet
TCDS3A20

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of a hydraulic landing gear retraction system.

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 Dynamic Aviation Group, Inc.

1402 Airport Rd., PO Box 7 Bridgewater, VA 22812 Part 3* of the Civil Air Regulations (*Certification basis is set forth in Type Certificate Data Sheet 3A20, Rev. 37.)

Original Product Type Certificate Number : 3A20 Make : Beech Model : 65 (L-23F), A65, A-65-8200, 65-80, 65-A80, 65-A80-8800, 65-B80, 65-88, 65-90, 65-A90, 65-A90-1 (JU-21A), (U-21A), (RU-21A), (RU-21D), (U-21G), (RU-21H), 65-A90-2 (RU-21B), 65-A90-3 (RU-21C), 65-A90-4 (RU-21E), (RU-21H), B90, C90, E90, H90 (T-44A) Description of Type Design Change: Installation of a hydraulic landing gear retraction system in accordance with FAA Approved Aviadesign Drawing List E.O.-B9979-1, Issue 2, dated March 10, 1981, or later FAA approved revision.

FAA Approved Aviadesign Airplane Flight Manual Supplement dated April 8, 1981, or later FAA approved revision is required as part of this installation.

Limitations and Conditions: This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this STC must be included in the permanent records of each airplane modified in accordance with this STC. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

Date of application : November 5, 1980

Date of issuance : April 8, 1981

Date reissued : October 2, 2014

Date amended : December 4, 1981, December 17, 1982, August 27, 1985

(Signature) Supervisor, Technical & Administrative Support Staff Los Angeles Aircraft Certification Office (Title)

Transfer the ownership of Supplemental Type Certificate Number

to (Name of transferee)

(Address of transferee) (Number and street)

(City, State, and ZIP Code)

from (Name of grantor) (Print or type)

(Address of grantor) (Number and street)

(City, State, and ZIP Code)

Signature of grantor (In ink):

U.S. GPO 1987-763-289

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 17

MakeModelData sheet
Beechcraft Corporation653A20
Beechcraft Corporation65-803A20
Beechcraft Corporation65-883A20
See all 17 models

Every issue · 2

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
October 2, 2014Reissued, currentCertificate
August 27, 1985Amended, earlier issueCertificate