# STC SA01062SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Deluca of California Inc., United States
- Description: Install structural reinforcement for increased engine weight and provisions for increased gross weight
- Applied: December 13, 2000
- Status date: March 11, 2002
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A-782](https://openairdocs.org/tcds/A-782)
- Certificate PDF: https://openairdocs.org/files/sha256/ce/7f/ce7fe25a9ba6e14569bca56096a82d14127f26af3255b9ac5332b10c0f0cdf2e
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/81BA243E674A02B7862576E00058C51B.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA01062SE

## ADs that name it (0)

None.

## Approved models (1)

- Sierra Hotel Aero Inc. Navion A (Army L-17B and L-17C) ([TCDS A-782](https://openairdocs.org/tcds/A-782))

## 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 Number SA01062SE

This certificate, issued to DeLuca of California, Inc.

50010 Main St., P.O. Box 727 Cabazon, CA 92230

Parnt 3 of theCivil Air Regulations.

Original Product⎯Type Certificate Number: A-782 Make: Navion Model: Navion(L-17A), Navion A(L-17B), and (L-17C)

Description of the Type Design Change: Install structural reinforcement for increased engine weight and provisions for increased gross weight in accordance with DeLuca of California, Inc., Drawing List 143-31001-700DOC Revision New, dated September 26, 2000, and Installation instructions, EO 143-31001-7DOC Revision New, dated December 13, 2000, or later FAA approved revision.

Note: TCDS A-782, Note 6 requires that the structural improvements identified as 143-3100-700 be installed for engines of greater than 250 HP. This kit provides an equivalent capability.

Limitations and Conditions: Additional modification must be made to the aircraft before an increased gross weight can be FAA approved. Approval of this change in type design applies to the above model aircraft only. 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 relationship 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 must be maintained as part of the permanent records for the modified aircraft.

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: December 13, 2000 Date reissued:

Date of issuance: March 11, 2002 Date amended:

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

## Every issue (1)

- March 11, 2002: Issued, Current. [certificate](https://openairdocs.org/files/sha256/ce/7f/ce7fe25a9ba6e14569bca56096a82d14127f26af3255b9ac5332b10c0f0cdf2e)

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