# STC SA2859WE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Charles Lischer Jr., United States
- Description: Installation of Lycoming 0-320-A3B engine & Hartzell HC-C2YL-1BF/F7663A-4 propeller.
- Applied: September 11, 1973
- Status date: April 1, 1974
- Product: Aircraft
- Certification basis: Part 21
- Data sheets: [TCDS A-766](https://openairdocs.org/tcds/A-766)
- Certificate PDF: https://openairdocs.org/files/sha256/53/43/53439a189d24b0a3b5899bec6d2039ead0c6b2a696828de80b183a5fe9e8f5b8
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/73EF8D03D3DF36A7862579800071B160.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2859WE

## ADs that name it (0)

None.

## Approved models (1)

- Swift Museum Foundation Inc. GC-1B ([TCDS A-766](https://openairdocs.org/tcds/A-766))

## What the certificate says

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

Binited Statce of Simrico Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number 512859WE Pricertificato, isicala CHAFIES IISCHER, VA Part 4a of the CIVI1 Aix Regulations:

Original Product -Type Portificate Numben: A-766 Make: UNIVERSAL: (Globe) Model: GC-1B, N80779, Serial No. 182 Description of Type Design Change:

Installation of Lucoming 0-320-AЗB engine and Hartzell HC-C2YI-1BF/F7663A-L propeller (in lieu of the Lycoming 0-320-AЗA engine and Hartzell HC-82XG-76361)-2 propeller approved per STO SA2-1007) and associated installation components in accordance with Charles Lischer, Jr. Installation instructions for Swift GC-1B dated September 13, 1973.

limitalinvandEnditiona: This installation eligible only on aircraft previously modified per STO SA2-1007.

Data not suitable for reproduction of installation in other aircraft; therefore, they are satisfactory for Universal (Globe) Go-P, N00([9, Serial Jo. 182 only. 170 additional modifications of this type are to be approved solely by reference to this Supplemental Type Certificate (STC) or to the data submitted therefor.

SIC Addendum No. SA2059WE is a part of this Certificate. A copy oi this Certiiicate and Charles Lischer, Jr. Installation Instructions for Swift GC-1B shall be maintainet I perfat the peppering antenne toods rone marred asset unlil sur sendered, suspended, revoked, or a termination date is otherwise estabbished try the Administrater of the Federal Aviation Administration .

Date of Application: September 11, 1973 Lute missued:

Tate spissuance. APR 1 1974 Date Amended:

**FEDERAL AVIATIO**

**TOHINISTRATO**

FAA FORK 8110-2 (10-68) Tires 3 At 2 OrmAn

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continvotion Sheet) Number: SA285918 820 " 1074 Make:

SUPPLENINLAL TYPE CURIIFICATE ADDENDUM NO. SA2859VE The conditions and limitations of Aircraft Specification No. A-766 and STO SA2-1007 apply except as follows:

This Addendun, which is part of Supplemental Type Certificate No. SA2859WE, prescribes 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 Addendum shall be maintained as part of the modified aircraft permanent records.

I - Model Universal (Globe) GO-1B (Lanäplane Only), as modified by STO SA2859WE.

Propeller: Hartzell Hub Model: HC-C2YL-1BF Blade Model: F76634-4 Diameter: 72 inches Maximum 71 inches Minimum Pitch Stop Settings: At 30 in. station - Low 120 High 276 Serial Number Eligible: No. 182 only.

Certification Basis: Same as specified by Aircraft Specification No.

A- 766.

Required Equipment: In addition to the equipment applicable and required by Aircraft Specification No. A-766 and Supplemental Type Certificate SA2-1007 the equipment specified by Charles Lischer, Jr. Installation Instructions for Swift GC-18 must be installed as a result of the incorporation of this SIC.

Note l. The following placard must be displayed on the instrument panel adjacent to the electric fuel pump switch and adjacent to the electric fuel pump circuit breaker:

"AUX FUEL PUMP"

47.

**PAGE 3 OF 3 PAGES C FAA AC 73-2651**

## Every issue (1)

- April 1, 1974: Issued, Current. [certificate](https://openairdocs.org/files/sha256/53/43/53439a189d24b0a3b5899bec6d2039ead0c6b2a696828de80b183a5fe9e8f5b8)

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