# STC SA1233WE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Robert A. Archer, United States
- Description: Installation of Lycoming 0-360-AID Engine & Hartzell HC92ZK-8D/8447A-12A Propeller
- Applied: September 20, 1965
- Status date: June 23, 1966
- Product: Aircraft, Large Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A21EA](https://openairdocs.org/tcds/A21EA)
- Certificate PDF: https://openairdocs.org/files/sha256/63/5c/635c075930f7c78f8d4c2cfaf0e9127476f6e52318f7e96971861f0251a9233e
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/97744F8A8B46BBF1862585C30051C585.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1233WE

## ADs that name it (0)

None.

## Approved models (3)

- Bombardier Inc. CL-600-2B16 (CL-601-3A) ([TCDS A21EA](https://openairdocs.org/tcds/A21EA))
- Bombardier Inc. CL-600-2B16 (CL-601-3R) ([TCDS A21EA](https://openairdocs.org/tcds/A21EA))
- Bombardier Inc. CL-600-2B16 (CL-604) ([TCDS A21EA](https://openairdocs.org/tcds/A21EA))

## What the certificate says

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

Federal Aviation Agency Supplemental Type Certificate Number 8A1233473 This certificate issued to: Mr. Robert A. Archer 21818 Ocean Avenue Torrance, California Part Aa of the BEER Regulations.

Original Product - Typebortificate Number: A-773 Make: BELLANCA Model: 14-13-2 Description of Type Design Change: Installation of Lycoming 0-360-AID Engine and Hartzell HC92ZK-8D/8447A-12A Propeller in accordance with Robert A. Archer Report No. RAA-92065.

Limitations and Conditions: Data not suitable for reproduction of installation in other aircraft; therefore, it is satisfactory for Bellanca 14-13-2, N86806, Serial 1167 only. No additional modifications of this type are to be approved solely by reference to this Supplemental Type Certificate or to the data submitted therefor.

NOTE: See Attached Sheet for Operating Limitations.

Date of Application: September 20, 1965 Date Reissued:

Date of Issuance: June 23, 1966 Date Amended:

By Direction of the Administrator na2 S15201 B7.

- D, DOOME Charles R. Hawks, (Signature) Chief, Aircraft Engineering Division

47.

**FAA FORM 8110-2 (1-66) 0052-657-6000**

OPERATING LIMITATIONS FOR BELLANCA 14-13-2, N86806, Serial No. 1167 Same as the Operating Limitations and placards prescribed by CAA Aircraft Specification No. A-773 except as follows:

ENGINE: Lycoming 0-360-A1D FUEL: 91/96 Minimum Octane Aviation Gasoline ENGINE LIMITS: 2700 RPM (180 H.P.) for all operations PROPELLER: HARTZELL HC92ZK-8D/8447A-12A Diameter: Maximum - 72 in.

Minimum - 70 in.

Pitch Settings: At 30" Station - High: 27°

- LoW: 13° POWERPLANT INSTRUMENTS: To be provided by permanent markings Tachometer: 2700 RPM (Red Line) Cylinder Head Temperature Gage: 500°F (Red Line) Oil Temperature: 245°F (Red Line) Oil Pressure: Maximum - 100 psi (Red Line) Minimum - 25 psi (Red Line) Normal - 60 to 90 psi (Green Are) .

OIL CAPACITY: Two Gallons (-35).

**A COPY OF THESE LIMITATIONS SHALL BE CARRIED IN THE AIRCRAFT AT ALL TIMES.**

## Every issue (1)

- June 23, 1966: Issued, Current. [certificate](https://openairdocs.org/files/sha256/63/5c/635c075930f7c78f8d4c2cfaf0e9127476f6e52318f7e96971861f0251a9233e)

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