# STC SA09839AC

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Intercontinental Jet Service Corporation, United States
- Description: Replacement of analog primary cockpit indicators with the Sagem Integrated Cockpit Display System (ICDS) and installation of dual ADAHRS with standby instruments
- Applied: March 17, 2008
- Status date: March 13, 2015
- Product: Aircraft, Small Airplane
- Certification basis: Part 3, Part 21, Part 23
- Data sheets: [TCDS A10SW](https://openairdocs.org/tcds/A10SW)
- Certificate PDF: https://openairdocs.org/files/sha256/56/c3/56c323de4d524143198d540961126592f2c1972aa4adb472608772e49bc73ce7
- Approved model list and other attachments: [AML_SA09839AC.pdf](https://openairdocs.org/files/sha256/13/e7/13e7bf29166802d2dce2ce0d58615c7fd410c79e8140f889860dcfe835d880fe)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/53F51C053F0046EC86257E270064C49A.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA09839AC

## ADs that name it (0)

None.

## Approved models (1)

- Mitsubishi Heavy Industries Ltd. MU-2B-26A ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))

## 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.

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

Part of the

Signature

Title 3 SA09839AC Intercontinental Jet Services, Corporation (IJSC) 3322 N. 74th E. Avenue, Hangar 27 Tulsa, OK 74115 Federal Aviation Regulations.

23 Replacement of analog primary cockpit indicators with the Sagem Integrated Cockpit Display System (ICDS) and installation of dual ADAHRS with standby instruments in accordance with Master Data List: 001-3400-L01-00, rev: 1.0 or later FAA approved revision. FAA Approved Flight Manual Supplement , IJSC-3400-A01-00, Rev: IR or later FAA approved revision must be attached to the FAA approved flight manual when this modification is installed. Instructions for Continued Airworthiness (ICA), 001-3400-C01-00, rev: 3.0 or Later FAA approved revision are a require part of this modification.

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

2) 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.

3) This modification is only applicable to aircraft with the M4D autopilot system installed.

Acting Manager, Airplane Certification Office Mitsubishi Heavy Industries, Ltd.

See AML SA09839AC for type certificate number and model eligibility.

March 17, 2008 March 13, 2015

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

To (Name and address of transferee)

From (Name and address of grantor)

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

3 Certification Basis:

CAR 3 dated May 15, 1956, including Amendments 3-1 through 3-8 plus the Special Conditions stated in FAA letter to the JCAB dated May 14, 1965, modified by FAA letters to the JCAB dated January 25, 1968, and May 12, 1971. Exemption No. 1951, dated February 4, 1974, granted an exemption from Section 21.17.

Except where replaced by the following regulations:

14 CFR 23 regulations as amended by Amendment N/C:

14 CFR 23.1367 and 23.1381, 23.1519.

14 CFR 23 regulations as amended by Amendment 23-20:

**14 CFR 23.1301, 23.1327, 23.1335.**

14 CFR 23 regulations as amended by Amendment 23-21:

14 CFR 23.1353,(h) 23.1501, 23.1541.

14 CFR 23 regulations as amended by Amendment 23-26:

**14 CFR 23.1529.**

14 CFR 23 regulations as amended by Amendment 23-34:

**14 CFR 23.1523.**

14 CFR 23 regulations as amended by Amendment 23-43:

14 CFR 23.1322, 23.1331, and 23.1357(c),(d).

14 CFR 23 regulations as amended by Amendment 23-45:

14 CFR 23.1525, and, 23.1549.

14 CFR 23 regulations as amended by Amendment 23-49:

14 CFR 23.1303(a),(b),(c),(d),(f) , 23.1307, 23.1309(a), (b), (c), (e), 23.1311, 23.1321(a),(b),(d), 23.1323,(a),(b),(c), 23.1329(h), 23.1351

(a)(2), 23.1359, 23.1365, 23.1431, 14 CFR 23 regulations as amended by Amendment 23-50:

14 CFR 23.1325, 23.1543(b), (c), 23.1545, 23.1581.

14 CFR 23 regulations as amended by Amendment 23-51:

14 CFR 23.1337(c).

14 CFR 23 regulations as amended by Amendment 23-52:

14 CFR 23.1305 14 CFR 23 regulations as amended by Amendment 23-57:

14 CFR 23.1308 14 CFR 23 regulations as amended by Amendment 23-61:

**14 CFR 23.1306 SA09839AC**

### AML_SA09839AC.pdf

REVISION - IR DATE: March 13, 2015

FEDERAL AVIATION ADMINISTRATION – Approved Model List (AML) No. SA09839AC

For the Installation of and STC Certification of a Sagem Integrated Cockpit Display System (ICDS) for the Mitsubishi MU-2B Models

1/1 Aircraft Make and Model Designation Original Type Certificate Number Configuration ID Number

Software Version

Certification Basis

**AFMS ICA**

Mitsubishi Heavy Industries, Ltd.

MU-2B-26A A10SW MU2B26AX-001-A

V960BE

Part 23 IJSC-3400-A01-00 001-3400-C01-00 --------------------END OF LIST--------------------

____________________________________ Scott A. Horn, Acting Manager Airplane Certification Office

Aircraft Certification Service

## Every issue (1)

- March 13, 2015: Issued, Current. [certificate](https://openairdocs.org/files/sha256/56/c3/56c323de4d524143198d540961126592f2c1972aa4adb472608772e49bc73ce7), [AML_SA09839AC.pdf](https://openairdocs.org/files/sha256/13/e7/13e7bf29166802d2dce2ce0d58615c7fd410c79e8140f889860dcfe835d880fe)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
