# STC SA282NW

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: STC Bee, Inc, United States
- Description: Installation of Lycoming GO-435 and GO-480 series engines, Hartzell HC-A3X and  HC83X series propeller, new nacelle, engine mount, modified rear spar, and associated systems.
- Applied: December 29, 1975
- Status date: November 7, 1978
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A-769](https://openairdocs.org/tcds/A-769)
- Certificate PDF: https://openairdocs.org/files/sha256/fc/25/fc251fb7c7187b8228bbae7b066208b4b215a87051ab54bfd10b1a6090dd9a16
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6E109057A9819EC586257AD90061B9E6.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA282NW

## ADs that name it (0)

None.

## Approved models (1)

- Sky Enterprises Inc. RC-3 ([TCDS A-769](https://openairdocs.org/tcds/A-769))

## What the certificate says

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

STL Department of Transportation Federal Aviation Administration BooK Supplemental Type Certificate Number: SA282NN This certificate issued to: S.T.C. BEE, INC.

Purt 03 of the CIViT Air Regulalions: effective November 13, 1945 Original Product -Typebertificate Number: A-769 Make: Republic Model: RC- 3 Description of Type Design Change: Installation of Lycoming G0-435 and G0-480 series engines, Hartzell HC-A3X and HC-83X series propellers, new nacelle, engine mount, modified rear spar, and associated systems in accordance with S.T.C. Bee, Inc., Installation Instructions Model 1-LE and Drawing List Report No. 1.

documents shall be maintained as part of the permanent records for the modified aircraft.

Limitations and Conditions: Approval of this change in type design applies basically 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 interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate, Addendum SA282NW, and S.T.C. Bee, Inc., approved Airplane Flight Marcel capent spaling maintained as part of the perment records until sur- part of the permanent records.

rendered, suspended, revked, or a termination date is otherwise established by the SIdministrator of the Federal Aviation Administration .

Date of Application: December 29, 1975 Date Reissued:

Date of Issuance: April 13, 1976 Date Amended: December 6, 1976, November 7, 197E FEDERAL AVIATION By Direction of the Administrator пано Shareser Signature ) TO HINISTRAIO Chief, Engineering and Manufacturing Branch (Title )

47.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Nov 0x 1978 Number: SA282NW Supplemental Type Certificate ADDENDUM NO. SA282NW The conditions and limitations of Type Certificate Data Sheet No. A769 apply except as follows:

Supplemental Type Certificate Addendum, which is part of SIC SA282NW, prescribes the conditions and limitations under which the product for which the STC was issued meets the airworthiness requirements of the Civil Air Regulations. A copy of this STC Addendum is required to be maintained as part of the permanent records for the modified aircraft.

Supplemental Type Certificate HOLDER: S.T.C. Bee, Inc.

1. MODELS RC-3, 4PCLM (NORMAL CATEGORY) AS MODIFIED BY STC SA282NW Engine: Lycoming GO-435 and G0-480 Fuel: See Engine Data Sheet as follows:

ENGINE TC DATA SHEET GO-435 Series E-299-16 GO-480 Series E-275-10 Propeller: Hartzell HC-AX (Data Sheet No. P-913-11) Hartzell HC-83X (Data Sheet No. P-884-12) Hartzell HC-A3Y (Data Sheet No. P-6EA-5) Propeller-Engine Combinations:

The maximum and minimum propeller diameters that can be used from a vibration standpoint are shown below. No reduction below the minimum diameter listed is permissible, since this figure includes the diameter reduction allowable for repair purposes.

**FAA FORM 8110-2-1 (10-69) PAGE 3 OF 3 PAGES FAA AC 73-2651**

## Every issue (1)

- November 7, 1978: Amended, Current. [certificate](https://openairdocs.org/files/sha256/fc/25/fc251fb7c7187b8228bbae7b066208b4b215a87051ab54bfd10b1a6090dd9a16)

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