STC SA1624GL

Supplemental type certificate · Resource Aircraft Conversions

Holder
Resource Aircraft Conversions · United States
Status
Current · Reissued
Status date
February 6, 2019
Applied
February 4, 1991
Product
Aircraft · Small Airplane
Certification basis
Part 21, Part 23
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 cargo door, 9G cargo restraint system and crew comfort bulkhead; removal of pressurization system and a/c system; relocation of oxygen supply 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.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder.

FAA Form 8110-2 (5/14) Page 1 of 3

Number: SA1624GL

This certificate issued to: Resource Aircraft Conversions 691 Fitzhugh Blvd Smyrna Tennessee 37167

Part 23 of the Federal Aviation Regulations.

Original Product – Type Certificate Number: 3A20 Make: Beech Aircraft Corporation Model: 65-A90, B90

Installation of cargo door, 9G cargo restraint system and crew comfort bulkhead; removal of pressurization system and air conditioning system; relocation of oxygen supply system per King Cargo Systems Master Document List 87-001, Rev. B, dated June 20, 1991, or later FAA approved revisions.

1. FAA-approved Airplane Flight Manual Supplement (King Cargo Systems Document FM-2), No Rev., dated 6/3/91 or later FAA-approved revision is required.

2. An FAA-approved cockpit Crew Door is required.

3. Compatibility of this design change with previously approved modifications must be determined by the installer.

4. 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: February 4, 1991 Date Reissued: October 1, 1997, February 6, 2019 Date of Issuance: July 2, 1991 Date Amended:

Signature Title Manager, Atlanta Aircraft Certification Branch

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to t he design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder.

FAA Form 8110-2 (5/14) Page 2 of 3

To (Name and address of transferee)

From (Name and address of grantor)

Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to t he design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder.

FAA Form 8110-2 (5/14) Page 3 of 3

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 · 2

MakeModelData sheet
Textron Aviation Inc.65-A903A20
Textron Aviation Inc.B903A20