# STC SR00821SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Heli-Jet Corporation, United States
- Description: Installation in accordance with Heli-Jet Drawing List HJ-1001, Revision New, dated July 14, 2000, or later FAA approved revisions.
- Applied: June 3, 1999
- Status date: July 18, 2000
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS H1SW](https://openairdocs.org/tcds/H1SW)
- Certificate PDF: https://openairdocs.org/files/sha256/f7/b5/f7b52b3b535e90149c8ebe74055f56cfb0b0db310994df458660d7cf5dd9fe94
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C52E1B8D79A4B517862579980070F6C5.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SR00821SE

## ADs that name it (0)

None.

## Approved models (1)

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

## 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.

Number SR00821SE This certificate, issued to Heli-Jet Corporation 90711 Greenhill Road Eugene, OR 97402 Part 25 of the Federal Aviation Regulations.

Original ProductType Certificate Number: H1SW Make: Bell Helicopter Textron, Inc.

Model: 205A-1

Description of the Type Design Change: Installation in accordance with Heli-Jet Drawing List HJ-1001, Revision New, dated July 14, 2000, or later FAA approved revisions.

Note: The Rotocraft modified must have Bell Kit 204-706-034-007, Co-Pilot Dual Controls installed per Service Instruction 205-1 and Bell Kit 204-706-040-3, Co-Pilot Instrument Kit, installed per Bell Service Instruction 205-3 less torque pressure indicator (one indicator is adjacent on pilot panel, second is in door panel).

Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to other aircraft 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 aircraft. A copy of this certificate and Rotocraft Flight Manual Supplement HJ1-FMS Revision N/C, FAA approved July 18, 2000, or later FAA approved revison, must be maintained as part of the permanent records for the modified aircraft.

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.

Date of application: June 3, 1999 Date reissued:

Date of issuance: July 18, 2000 Date amended:

(Signature) Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (1)

- July 18, 2000: Issued, Current. [certificate](https://openairdocs.org/files/sha256/f7/b5/f7b52b3b535e90149c8ebe74055f56cfb0b0db310994df458660d7cf5dd9fe94)

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