# STC SH3827NM

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Heli-Jet Corporation, United States
- Description: Installation of a one to nine passenger configuration.
- Applied: March 20, 1987
- Status date: September 11, 1991
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H1SW](https://openairdocs.org/tcds/H1SW), [TCDS H4SW](https://openairdocs.org/tcds/H4SW)
- Certificate PDF: https://openairdocs.org/files/sha256/a1/76/a17636ce83e0b2147c613ff295ba6031a8404e9010adbd56dfaf4d680ce2dc30
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/261341D0F0A9158F85256CC2005C3184.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SH3827NM

## ADs that name it (0)

None.

## Approved models (2)

- Bell Helicopter Textron Inc. 205A-1 ([TCDS H1SW](https://openairdocs.org/tcds/H1SW))
- Bell Helicopter Textron Inc. 212 ([TCDS H4SW](https://openairdocs.org/tcds/H4SW))

## What the certificate says

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

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SH3827 NM This certificate issued to: Hel i-Jet Corporation Part * of the * Regulations:

Original Product -Typebertificate Number See attached FAA Approved Model List (AML) No.

Muled and applicable airworthiness regulations. Make SH3827NM for list of approved rotorcraft models

•onfiguration in accordance With Heli-Jet Corporation Seat Installation Instructions Description of Supe Design Installation of a one to nine passenger Numbered HJ8701 or HJ8702 dated March 12, 1987, or later FAA approved revision.

Limitations and Conditions: Approval of this change in type design applies to the above model helicopter only. This approval should not be extended to other helicopters of this model on which other previously approved modifications are incorporated unless it is determined that the relationship 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 helicopter. A copy of this Certificate and FAA Approved Rotorcraft Flight Manual Supplement dated September 11, 1991, must be maintained as part of the permanent records for the modified helicopter.

Dales applicatinMarch 20, 1987 Sate wissued:

Fates/ issuance: April 23, 1987 Jake amendedeptember 11, 1991 FEDERAL AVIATION Stewart 12 miller By Direction of the Administrator (Signature ) TRAINIST RATO Assistant Manager, Seattle Aircraft Certification Office (Tille) 47 FAA FOR 8170-2 (10-68)

**FAA APPROVED MODEL LIST (AML) NO. SH3827NM**

HELI-JET CORPORATION ONE TO NINE PASSENGER CONFIGURATION Issue Date: December 10, 1990

**FAA APPROVED**

**DRAWING/**

**ORIGINAL CERTIFICATION DRAWING LIST**

TYPE BASIS AFM AML ITEM | ROTORCRAFT MAKE ROTORCRAFT MODEL CERTIFICATE NUMBER ALTERATION FOR NUMBER REVISION DATE SUPPLEMENT DATE AMENDMENT DATE BELL 205A-1 HISW CAR 7 HJ8701 ANDI 4/30/91 9/11/91 9/11/91 HJ8702 2 BELL 212 H4SW FAR 29 HJ8701 AND 4/30/91 9/11/91 9/11/91 HJ8702 FAA Approved: Stewas Kmiller Assistant Manager, Séattle SEP I Aircraft Certification Office Make:

Heli-Jet Corporation 3830 Cross Street Eugene, OR 97402 STC SH3827NM

**HELI-JET CORPORATION**

**FAA APPROVED ROTORCRAFT FLIGHT MANUAL SUPPLEMENT TO BELL 205A-1, 212**

FAA APPROVED ROTORCRAFT FLIGHT MANUAL The information in this document is FAA approved material which, together with the basic Bell 205A-1, 212 flight manual, is applicable and must be carried in the basic manual when the aircraft is equipped with the one to nine passenger seating configuration in accordance Supplemental Type Certificate SH3827NM.

The information in this document supersedes the basic manual only in the areas covered.

For further Limitation, Procedures or Performance consult the basic manual.

LIMITATIONS Maximum passenger seating is nine (9). (Refer to Heli-Jet Installation Instructions numbered HJ8701 or HJ8702 for seating configuration.)

FAR 135 aircraft will maintained in accordance with FAR 135.411 (a) (2).

Note: Weight and balance should be adjusted for passenger seating configurations.

PROCEDURES No change.

II. PERFORMANCE No change.

IV. EMERGENCY PROCEDURES No Change.

FAA Approved: Stewas HeRmilles Assistant Manger, Seattle Aircraft Certification Office SEP 1 1 1991 Make:

## Every issue (1)

- September 11, 1991: Amended, Current. [certificate](https://openairdocs.org/files/sha256/a1/76/a17636ce83e0b2147c613ff295ba6031a8404e9010adbd56dfaf4d680ce2dc30)

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