# STC SA1027NW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Milo DeAngelis, Canada
- Description: Auxiliary fuel tanks.
- Applied: September 18, 1980
- Status date: February 6, 2006
- Product: Aircraft, Single-Engine
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 1A6](https://openairdocs.org/tcds/1A6)
- Certificate PDF: https://openairdocs.org/files/sha256/03/cb/03cb69cbfe7f29672b6debbd1c88ba2749900faf1d65f54b75101b7448d3b894
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E45FB8D448880454862571160072D9D7.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1027NW

## ADs that name it (0)

None.

## Approved models (3)

- The New Piper Aircraft Inc. PA-22-150 ([TCDS 1A6](https://openairdocs.org/tcds/1A6))
- The New Piper Aircraft Inc. PA-22-160 ([TCDS 1A6](https://openairdocs.org/tcds/1A6))
- The New Piper Aircraft Inc. PA-22S-160 ([TCDS 1A6](https://openairdocs.org/tcds/1A6))

## 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.

United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate (This STC is a duplicate original to replace the original which was lost. Issued 2/06/06) Number SA1027NW This certificate, issued to: Milo DeAngelis 6665 Old Kamloops Rd Vernon, B.C. V1H 1P8 Part 3 of the Civil Air Regulations, dated November 1, 1949.

Original Product⎯Type Certificate Number: 1A6 Make: Piper Model: PA-22-150, PA-22-160, and PA-22S-160

Description of the Type Design Change: Installation of 9.5 gallon auxiliary fuel tanks and associated systems in accordance with Simpson Aviation Company Drawing SAC 2300.

NOTE: These tanks are used as transfer tanks to each adjacent main (wing) fuel tank.

PLACARD: The following placard is required at the wing tank control valve:

ONLY TURN ON IN LEVEL FLIGHT AND WHEN MAIN TANK IS LESS THAN ½ FULL

Limitations and Conditions: Approval of this change in type design applies basically to the above model aircraft only. It may be used with the above models with extended wing and fuselage modified in accordance with STC SA819SW. This approval should not be extended to other aircraft of this model on which any other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate shall be maintained with the aircrafts permanent records.

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: September 18, 1980 Date reissued: November 10, 1980, February 6, 2006 Date of issuance: September 22, 1980 Date amended:

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

**FAA FORM 8110-2(10-68**

## Every issue (1)

- February 6, 2006: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/03/cb/03cb69cbfe7f29672b6debbd1c88ba2749900faf1d65f54b75101b7448d3b894)

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