# STC SA2608NM

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Soper Steve, United States
- Description: Installation of a Lycoming A10-360-A1B engine and a Hartzell HCC2YK-4CF/FC7666A-2 propeller.
- Applied: December 15, 1983
- Status date: April 22, 1986
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A21CE](https://openairdocs.org/tcds/A21CE)
- Certificate PDF: https://openairdocs.org/files/sha256/e3/bb/e3bb3c5e86afc0e4c0c752b764a3c6cf3128ac94c3ff74716e122d29ce885a50
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/073882E32EE7512785256CC20008C660.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA2608NM

## ADs that name it (0)

None.

## Approved models (1)

- American Champion Aircraft Corp. 8KCAB ([TCDS A21CE](https://openairdocs.org/tcds/A21CE))

## 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: SA2608NM This certificate issued to: Steve Soper Part. 23 of the Federal Aviation Regulations, dated February 1, 1965, as amended by 23-1 through 23-6.

Original Product -Type Certificate Number: A21CE Make: Bellanca Model: 8KCАВ Description of Type Design Change:

Installation of a Lycoming A10-360-A1B Engine and a Hartzell HCC2YK-4CF/FC7666A-2 Propeller per FAA Approved Pictures and Sketches attached to FAA Form 337, dated April 24, 1984, or later FAA Approved Revisions.

Data pertaining to this modification are considered inadequate for duplication in other aircraft. This approval is limited to the installation in Bellanca Model 8KCAB, Serial Number 150-74 only. A copy of this Certificate shall be maintained as part of the permanent records for the modified aircraft. (This Certificate is comprised of two pages)

Date of Application: December 15, 1983 Date Reissued:

Date of Issuance: . May 30, 1984 Date Amended: April 22, 1986 FEDERAL FYIATION By Direction of the Administrator TO MINISTRATION Acting Manager, Seattle Aircraft Certification Office (Title) 47 FAA FOR 8110-2 (10-68)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number Supplemental Type Certificate ADDENDUM NO. SA2608NH The conditions and limitations of Type Certificate Data Sheet Number A21CE apply except where superseded by the following:

Supplemental Type Certificate Data Sheet, which is part of STC SA2608NM prescribes the conditions and limitations under which the product for which the STC was issued meets the airworthiness requirements of the Federal Aviation Regulations.

Supplemental Type Certificate HOLDER: Steve Soper 1- BELLANCA 8KCAB (2PCLM-NORMAL/ACROBATIC CATEGORY) AS MODIFIED BY STC SA2608NM Engine: Lycoming AI0-360-A1B Engine Limits: 200 Hp @ 2700 rpm Fuel: 100/100LL aviation gasoline Propeller and Hartze11 HC-C2YK-4CF/FC7666A-2 Propeller Limits: 250 Hp @ 2700 rpm maximum Diameter: 74" maximum; 72" minimum "Avoid continuous operation between 2000 and 2350 rpm" Placard: Located in full view of the pilot

**AIRCRAFT IS EQUIPPED WITH A LYCOMING AIO-360-A1B ENGINE.**

**CONSULT LYCOMING MANUAL FOR OPERATING INSTRUCTIONS.**

Serial Number Eligible: 150-74 only -END-

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

## Every issue (1)

- April 22, 1986: Amended, Current. [certificate](https://openairdocs.org/files/sha256/e3/bb/e3bb3c5e86afc0e4c0c752b764a3c6cf3128ac94c3ff74716e122d29ce885a50)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.