# STC SA1624GL

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Resource Aircraft Conversions
- Description: 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.
- Status date: February 6, 2019
- Data sheets: 3A20, 3A20
- Certificate PDF: https://openairdocs.org/files/sha256/fd/ac/fdacf2cc04f84aaccf123a0fbdd884f75904d4630ec809482c806e009c9b62f4
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8BDC86C9A475E636862585C900544958.0001
- Page: https://openairdocs.org/stc/SA1624GL

## ADs that name it

None.

## Approved models (2)

- Textron Aviation Inc. 65-A90 (TCDS 3A20)
- Textron Aviation Inc. B90 (TCDS 3A20)

## 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.

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

## Every issue (1)

- February 6, 2019: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/fd/ac/fdacf2cc04f84aaccf123a0fbdd884f75904d4630ec809482c806e009c9b62f4)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.