# STC SA01334CH

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Crown MN Aviation LLC, United States
- Description: Installation of a 19-gallon wing fuel tank.
- Applied: June 5, 2000
- Status date: September 10, 2024
- Product: Aircraft, Small Airplane
- Data sheets: [TCDS A-725](https://openairdocs.org/tcds/A-725)
- Certificate PDF: https://openairdocs.org/files/sha256/e5/a1/e5a1ba64614d43f37e01a9f41de8d2a880c1bc39bb4c7927beb92d9a1bd56da0
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173288538020250404142934.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01334CH

## ADs that name it (0)

None.

## Approved models (4)

- The New Piper Aircraft Inc. J5 Series ([TCDS A-725](https://openairdocs.org/tcds/A-725))
- The New Piper Aircraft Inc. J5A (Army L-4F) ([TCDS A-725](https://openairdocs.org/tcds/A-725))
- The New Piper Aircraft Inc. J5A-80 ([TCDS A-725](https://openairdocs.org/tcds/A-725))
- The New Piper Aircraft Inc. J5B (Army L-4G) ([TCDS A-725](https://openairdocs.org/tcds/A-725))

## 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.

SA01334CH Crown MN Aviation, LLC 33361 Cobalt Circle NW Cambridge, MN 55008 04a Civil Air Regulations A-725 Piper Aircraft, Inc.

J-5A (Army L-4F), J5B (Army L-4G)

1. Continued Airworthiness Instructions: repair to the installed fuel tanks and any tank installation associated hardware shall meet the requirements of 14 Code of Federal Regulations Section

43.13(b).

(Limitations and Conditions continued on page 3 of 3) 06/05/2000 11/16/2000 Christina M. Underwood Manager, East Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 3 Installation of a nineteen (19) gallon wing fuel tank in accordance with AESI drawing List 303, dated June 06, 2000, or later FAA approved revision.

09/28/2004, 02/09/2009, 06/26/2018, 09/10/2024

SA01334CH 09/10/2024 3

SA01334CH 09/10/2024 Limitations and Conditions continued:

2. A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft.

3. See Aircraft Specification No. A-725 for complete certification basis.

4. Compatibility of this design with previously approved modifications must be determined by the installer.

------------------------------------------------------END-------------------------------------------------- 3 3 Add Page

## Every issue (3)

- September 10, 2024: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/e5/a1/e5a1ba64614d43f37e01a9f41de8d2a880c1bc39bb4c7927beb92d9a1bd56da0)
- June 26, 2018: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/f6/02/f6026c6b7fa4d74c4cf8900f8a21dbe3552788bf02bb34cef6ea44ca4ea75211)
- February 9, 2009: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/01/05/01052e61aab7a2ac57556d81b7dd135d272f997f5654dc9e254628533cfcc91e)

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