# STC SA3260WE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Keasling Chester I, United States
- Description: Installation of electric driven fuel pump.
- Applied: December 2, 1975
- Status date: September 8, 1976
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A-777](https://openairdocs.org/tcds/A-777)
- Certificate PDF: https://openairdocs.org/files/sha256/dd/b9/ddb97bb99cd7d34134acfb599dedf38d40afc16f7d413b504c109b1bbb3863e7
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B4A69197F3BA10B985256CC2000A9600.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA3260WE

## ADs that name it (0)

None.

## Approved models (9)

- Raytheon Aircraft Company 35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company 35R ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company A35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company B35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company C35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company D35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company E35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company F35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company G35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))

## What the certificate says

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

Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA3260WE This certificate issued to: Chester I. Keasling Part 03 of the Civi? AiT Regulations, offective November 13, 1945.

Original Product - Type Pertificate Number: A-777 Make: Beech Model: 35, A35, B35, C35, D35, E35, F35, G35, 3ER Description of Type Design Change: Installation of electric driven fuel pump in accordance with sealed Chester I. Keasling Electric Auxiliary Fuel Pump System Installation Instructions No. C1K-100-1 dated December 2, 1975.

Chester I. Keasling FAA Approved Airplane Flight Manual Supplement dated SEP 8 1976 is required.

Limitations and Conditions: The approval of this change in type design applies to the basic aircraft of the specified models that are otherwise unmodified. This approval should not be extended to other aircraft of these models 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.

Date of Application: December 2, 1975 Date Reissued:

Date of Issuance: SEP 8 1976 Date Amended:

FEDERAL AVIATION By Direction of the Administrator (Signature )

DOMINI STRANDE Chief, Aircraft Modification Branch Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or meth This certificate may be transferred in accordance with FAR 2 47 FAA FORM 8110-2 (10-68)

## Every issue (1)

- September 8, 1976: Issued, Current. [certificate](https://openairdocs.org/files/sha256/dd/b9/ddb97bb99cd7d34134acfb599dedf38d40afc16f7d413b504c109b1bbb3863e7)

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