# STC SH5206NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Dart Aerospace USA Inc., United States
- Description: Installation of two underfuselage jacking hard points.
- Applied: October 31, 1990
- Status date: July 5, 2023
- Product: Aircraft, Rotorcraft
- Data sheets: [TCDS H3WE](https://openairdocs.org/tcds/H3WE)
- Certificate PDF: https://openairdocs.org/files/sha256/b6/fc/b6fc1fc17fda3c3720e4c80f6f84fdc4c24e458aa02ff4395ccc290c43916035
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123246905820230812023452.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SH5206NM

## ADs that name it (0)

None.

## Approved models (7)

- MD Helicopter Inc. 369D ([TCDS H3WE](https://openairdocs.org/tcds/H3WE))
- MD Helicopter Inc. 369E ([TCDS H3WE](https://openairdocs.org/tcds/H3WE))
- MD Helicopter Inc. 369F ([TCDS H3WE](https://openairdocs.org/tcds/H3WE))
- MD Helicopter Inc. 369FF ([TCDS H3WE](https://openairdocs.org/tcds/H3WE))
- MD Helicopter Inc. 369HS ([TCDS H3WE](https://openairdocs.org/tcds/H3WE))
- MD Helicopter Inc. 500N ([TCDS H3WE](https://openairdocs.org/tcds/H3WE))
- MD Helicopter Inc. 600N ([TCDS H3WE](https://openairdocs.org/tcds/H3WE))

## 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 (11/20) SUPERSEDES PREVIOUS EDITION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

Page 1 of 2 SH5206NM Dart Aerospace USA, Inc 3845 NE 30th Avenue Hillsboro, OR 97124 Part 6 the Civil Air Regulations H3WE MD Helicopters, LLC 369HS, (S/N 0101 and subs), 369D,369E, 369F, 369FF, 500N, & 600N Installation of two underfuselage jacking hard points in accordance with FAA approved Drawing Lsit DL-369HP, no revision, FAA approved March 14, 1991, or subsequent FAA approved revision.

October 31, 1990 July 5, 2023 March 15, 1991 December 5, 1991; November 16, 1995; August 6, 1998 for Manager, West Certification Branch

1. The following placard must be displayed on each hard point: - "Suspending - maximum 230 lbs each point. - Suspended loads must be FAA approved."

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. 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.

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

Page 2 of 2 SH5206NM

## Every issue (2)

- July 5, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/b6/fc/b6fc1fc17fda3c3720e4c80f6f84fdc4c24e458aa02ff4395ccc290c43916035)
- August 6, 1998: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/08/70/0870f32d9e5927a8d46d7f82278dcb73cd777c79e2fddb5275b7a16d1d62996e)

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