STC SA4378WP

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/Large Airplane
Certification basis
Part 21, Part 23
Data sheet
TCDSA24CE

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

What it approves

Installation of 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 23* of the Federal Aviation Regulations (*Certification basis is set forth in Type Certificate Data Sheet A24CE, Rev. 12.)

Original Product Type Certificate Number : A24CE Make : Beech Model : 200 (A100-1 [RU-21J]), 200C, 200CT, 200T, A200 (C-12A) or (C-12C), A200C (UC-12B), A200CT (C-12D), B200, B200C, B200CT, B200T 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 5, dated November 16, 1981, or later FAA approved revision.

FAA Approved Aviadesign Airplane Flight Manual Supplement dated November 19, 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. This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight of the fuselage. 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 : November 20, 1981

Date reissued : October 2, 2014

(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 · 13

MakeModelData sheet
Beechcraft Corporation200A24CE
Beechcraft Corporation200CA24CE
Beechcraft Corporation200CTA24CE
Beechcraft Corporation200TA24CE
Beechcraft CorporationA100-1 (U-21J)A24CE
Beechcraft CorporationA200 (C-12A)A24CE
Beechcraft CorporationA200 (C-12C)A24CE
Beechcraft CorporationA200C (UC-12B)A24CE
Beechcraft CorporationA200CT (C-12D)A24CE
Beechcraft CorporationB200A24CE
Beechcraft CorporationB200CA24CE
Beechcraft CorporationB200CTA24CE
Beechcraft CorporationB200TA24CE

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
November 20, 1981Issued, earlier issueCertificate