# STC SA69AL

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Cub Crafters Inc
- Description: Fabrication and installation of Stoddard Aero Service Model 15 fuel tanks per Stoddard Aero Service Drawing List No. 447, dated February 7, 1975, or later Federal Aviation Administration approved revision.  Stoddard Aero Service Airplane Flight Manual Supplement, dated June 10, 1963, is required for this installation.
- Status date: January 26, 2012
- Data sheets: A-800
- Certificate PDF: https://openairdocs.org/files/sha256/3e/5c/3e5cc831d5ac4ba39a0e3dbf207c3aa60f0462be90d620acccb67e95ba38ddb2
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DBA49C8769A68CC0862579A5005DEC47.0001
- Page: https://openairdocs.org/stc/SA69AL

## ADs that name it

None.

## Approved models (1)

- Piper Aircraft Inc. PA-15 (TCDS A-800)

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

Number SA69AL

This certificate, issued to Cub Crafters, Inc.

1918 South 16th Avenue Yakima, WA 98903-1212

Part 3 of the Civil Air Regulations.

Original ProductType Certificate Number: 800 Make: Piper Model: PA-15

Description of the Type Design Change: Fabrication and installation of Stoddard Aero Service Model 15 fuel tanks per Stoddard Aero Service Drawing List No. 447, dated February 7, 1975, or later Federal Aviation Administration approved revision. Stoddard Aero Service Airplane Flight Manual Supplement, dated June 10, 1963, is required for this installation.

Limitations and Conditions: The approval of this change in type design applies basically to Piper PA-15 only.

This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer 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. This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight in the fuselage. The approval of this modification applies to the above noted airplane model series only.

If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

Date of application: May 24, 1963 Date reissued: May 14, 1998; January 26, 2012 Date of issuance: June 10, 1963 Date amended: 12/26/63; 1/16/64; 2/6/70; 8/6/71;

2/7/75

(Signature) Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (1)

- January 26, 2012: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/3e/5c/3e5cc831d5ac4ba39a0e3dbf207c3aa60f0462be90d620acccb67e95ba38ddb2)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.