# STC SA02592CH

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Murray Aircraft Modifications, United States
- Description: Installation of a pressure bulkhead
- Applied: January 8, 2007
- Status date: June 26, 2008
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A21EU](https://openairdocs.org/tcds/A21EU), [TCDS A56EU](https://openairdocs.org/tcds/A56EU)
- Certificate PDF: https://openairdocs.org/files/sha256/40/60/40604a1b407d012eee31e51fb66ab578fcfbd717c1b3ca15791e536aedaf42bf
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F7F9B4A9E35D354C8625749D00684A6F.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA02592CH

## ADs that name it (0)

None.

## Approved models (2)

- British Aerospace (Scotland) H.P. 137 Jetstream Mk. 1 ([TCDS A21EU](https://openairdocs.org/tcds/A21EU))
- British Aerospace (Scotland) Jetstream 3201 ([TCDS A56EU](https://openairdocs.org/tcds/A56EU))

## 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.

Part 23 of the Federal Aviation Regulations. (See continuation sheet 3 of 3)

Installation of a pressure bulkhead in accordance with Murray Aircraft Modifications, LLC Master Data List, Document Number DC309-1720-00, Rev. B, dated June 19, 2008, and Murray Aircraft Modifications, LLC, Engineering Order, Document Number DC309-1720-04, Rev. B, dated June 17, 2008; or later FAA approved revisions.

1. This STC shall be accomplished only in concert with, or subsequent to STC Number SA02463CH, that modifies the aircraft from a passenger configuration aircraft to an all cargo configuration aircraft and STC Number SA02464CH, that relocates the over wing emergency exit door. 2. FAA Approved Murray Aircraft Modifications, LLC Aircraft Flight Manual Supplement, Document No.

DC309-1720-02, Revision B, dated April 7, 2008, or later FAA approved revision is required. 3. Modified aircraft must be maintained in accordance with Murray Aircraft Modifications, LLC Instructions for Continued Airworthiness, Document No.

DC309-1720-03, Revision B, dated April 8, 2008, or later FAA accepted revision. 4. The installer must determine whether this design change is compatible with previously approved modifications. 5. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

Murray Aircraft Modifications 816 Willow Run Ypsilanti, MI 48198 A21EU & A56EU Make : British Aerospace Model : Jetstream 3101, Jetstream 3201 Date of application : January 08, 2007

Date of issuance : June 26, 2008

( Signature) Gregory J. Michalik, Senior Aerospace Engineer Airframe & Administrative Branch Chicago Aircraft Certification Office

( Title)

Original signed by:

Gregory J. Michalik

FAA FORM 8110-2-1(10-69) PAGE 2 of 3 PAGES

Number

FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES

Number SA02592CH Date of Issuance: June 26, 2008

Certification Basis:

Based on 14 CFR Sections 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the British Aerospace Models Jetstream 3101 and Jetstream 3201 cargo conversion is as follows:

a. The type certification basis for the British Aerospace Models Jetstream 3101 and Jetstream 3201 is as shown on TCDS A21EU and A56EU, respectively, for parts not changed or not affected by the change.

b. The certification basis for parts changed or affected by the change since the reference date of application, January 08, 2007, is based upon part 23 as amended by Amendment 23-34 and select later amendments. Based on 14 CFR Sections

21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be:

Regulations at the latest amendment 23-0 through 23-34:

23.301, 23.303, 23.305, 23.307, 23.365, 23.561, 23.603, 23.605, 23.607, 23.609, 23.611, 23.613, 23.619, 23.621, 23.623,

23.625, 23.627, 23.689(e), 23.775, 23.783, 23.785, 23.787, 23.807, 23.831, 23.843, 23.853, 23.867, 23.1301, 23.1309,

23.1322, 23.1351, 23.1353, 23.1365, 23.1419, 23.1435, 23.1438, 23.1529, 23.1541, 23.1557 Regulations at later amendments:

23.571 Amendment 23-45

23.573(b) Amendment 23-45

23.629 Amendment 23-48

--End--

## Every issue (1)

- June 26, 2008: Issued, Current. [certificate](https://openairdocs.org/files/sha256/40/60/40604a1b407d012eee31e51fb66ab578fcfbd717c1b3ca15791e536aedaf42bf)

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