# STC SE10WE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Aviation Power Supply Inc, United States
- Description: Bendix fuel injection system, RS-10B2.
- Applied: December 20, 1963
- Status date: March 2, 1964
- Product: Engine
- Certification basis: Part 21
- Data sheets: TCDS 5E-1, [TCDS E-123](https://openairdocs.org/tcds/E-123)
- Certificate PDF: https://openairdocs.org/files/sha256/31/76/3176e2eab71b082322d51fdef8c9899787c470f1e5b68f3cad6bcf7b8b117572
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B8ACD8FEC58BB9698625735C006CCC60.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SE10WE

## ADs that name it (0)

None.

## Approved models (2)

- Pratt & Whitney Division R-985 Series (TCDS 5E-1)
- Pratt & Whitney Division Wasp Jr. Series ([TCDS E-123](https://openairdocs.org/tcds/E-123))

## What the certificate says

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

E40Z

FEDERAL AVIATION AGENCY Supplemental Type Certificate

**1. NAME AND ADDRESS OF APPLICANT FORM APPROVED, BUDGET BUREAU NO. 04-R015**

**INSTRUCTIONS - SUBMIT IN TRI PLICATE TO LOCAL**

**FAA FLIGHT STANDARDS INSPECTOR**

**COPY WILL BE RETURNED TO APPLICANT UPON**

ISSUANCE Supplemental Type Certificate APPLIED FOR:

Aviation Power Supply, Inc. AIRCRAFT ENGINE PROPELLER 3111 Kenwood Street ORIGINAL MODEL DESIGNATION Pratt & Whitney Burbank, California R-985-AN-1, -3, -3, -6, -6, -63, -3, -10, NEW -12B, -14B, -14BML and Wasp Jr. SB-3 & B-5

3. DESCRIPTION OF CHANGE Installation of Bendix Fuel Injection System, RS-10B2, in accordance with APS Installation Instructions dated December 20, 1963, and APS Drawings B-4 and B-6.

LIMITATION OF APPLICABILITY: This approval should not be extended to other specific engines 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 engine.

OPERATIONAL LIMITATIONS: All ratings and limitations of the original engine are applicable except: Fuel Pressure - Maximum 21 psi; Minimum 17 psi.

CERTIFICATION BASIS: CAR 13.

• WILL DATA BE AVAILABLE FOR SALE OR RELEASE TO OTHER PERSONS? YES NO

b. WILL PARTS BE MANUFACTURED FOR SALE (Ref. CAR 1.55)? YES • NO

5. SIGNATURE AND TITLE OF APPLICANT December 20, 1963 Manage, Bunner dune Sis. Mauin a Si: Natt SIGNATURE Date of Application:

6. To be Completed by FAA

NATURE AND LOCATION OF DATA Aviation Power Supply Installation Instructions and Drawings B-4 and B-6 are on file at FAA Engineering and Manufacturing Branch, Western Region, 5651 W. Manchester Ave., Los Angeles, California.

ORIGINAL TYPE CERTIFICATE NO. FAA APPROVAL 5E-1, E-123 Original signed by Supplemental Type Certificate NO. Rocco L. Lippis

SELOWE SIGNATURE DATE OF APPROVAL Charles R. Hawks, Chief Engineering & Manufacturing Branch March 2, 1964 Flight Standards Division TITLE * U.S. GOVERNMENT PRINTING OFFICE: 1959 0-509657 FORM FAA -2417 (5-59)

## Every issue (1)

- March 2, 1964: Issued, Current. [certificate](https://openairdocs.org/files/sha256/31/76/3176e2eab71b082322d51fdef8c9899787c470f1e5b68f3cad6bcf7b8b117572)

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