# STC SA4071NM

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Milam International Inc, United States
- Description: Installation of emergency medical system.
- Applied: August 14, 1989
- Status date: June 18, 1997
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A2PC](https://openairdocs.org/tcds/A2PC)
- Certificate PDF: https://openairdocs.org/files/sha256/79/ee/79ee68d99d778e92a2f4f98308fd4a046fd03d73be750a3aefdf7c2eec1f331a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7796503E0C9A05A385256CC2000C6095.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA4071NM

## ADs that name it (0)

None.

## Approved models (3)

- Mitsubishi Heavy Industries Ltd. MU-2B-30 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-35 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-36 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

Trico sAuce of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA4071NM This certificate issued to: Milam International, Inc. d/b/a International Jet Aviation Services Part 3 of the Civil Air Regulations.

Original Product -Type Certificate Number: A2PC Make: Mitsubishi Model: MU-2B-30, MU-2B-35, MU-2B-36 Description of Type Design Change:

Installation of emergency medical system in accordance with Drawing List RDL-03, Rev. B, dated August 4, 1995 or later FAA approved revision.

1. FAA Approved Flight Manual Supplement, Rev. C, dated October 6, 1995, or later FAA approved revision is required.

2. Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft.

3. A copy of this Certificate and FAA Approved Flight Manual Supplement dated October 6, 1995, or later FAA approved revision, shall be maintained as part of the permanent records for the modified aircraft.

4. For incubator configuration, approval is for Provisions only, Revision B of MDL.

5. Function and Safety of vital sign monitor electronics components has not been verified, FAA approval applies to aircraft installation/integration only.

Date of Application: August 14, 1989 Date Reissued:

Date of Issuance: February 8, 1990 Date Amended: 10/6/95; June 18, 1997 FEDERAL AVIATION By indian eh string abes RONALD F. MAY (Signature) Manager AOMINISTRATIOR Denver Aircraft Certification Office Northwest Mountain Region, Denver, Colorado (Title)

## Every issue (1)

- June 18, 1997: Amended, Current. [certificate](https://openairdocs.org/files/sha256/79/ee/79ee68d99d778e92a2f4f98308fd4a046fd03d73be750a3aefdf7c2eec1f331a)

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