# STC SA00572SE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Cub Crafters Inc, United States - Description: Installation of modified instrument panel in accordance with Cub Crafters, Inc., Master Drawing List MDL 102700, Revision E, dated August 24, 1998, or later Federal Aviation Administration (FAA) approved revision. NOTE: This installation includes provisions for mounting radios and instruments in a new instrument panel. Any additions or changes to the original equipment radios or instruments will require separate FAA approval. The maximum weight of the equipment installed in the panel should not exceed that specified by Cub Crafters Installation Instructions 102700-11, Revision C, dated August 24, 1998, or later FAA-approved revision. - Applied: September 24, 1997 - Status date: January 12, 2012 - Product: Aircraft, Single-Engine - Certification basis: Part 3, Part 21 - Data sheets: [TCDS 1A2](https://openairdocs.org/tcds/1A2) - Certificate PDF: https://openairdocs.org/files/sha256/e9/de/e9de8280f7dc4de23a68441857613c02c2f985bca523047974e9ddd881fc61a4 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F989FA531A68F526862579A6005267AE.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA00572SE ## ADs that name it (0) None. ## Approved models (18) - Piper Aircraft Inc. PA-18 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18-105 (Special) ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18-125 (Army L-21A) ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18-135 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18-150 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18A ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18A-135 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18A-150 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18AS-125 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18AS-135 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18AS-150 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18S ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18S-105 (Special) ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18S-125 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18S-135 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18S-150 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-19 (Army L-18C) ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-19S ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) ## 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 SA00572SE 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: 1A2 Make: Piper Model: PA-18, -18A, -18S, -18 "105" Special, -18S "105" Special, -18 "125" (Army L-21A), -18S "125,” -18AS "125,” -18 "135" (Army L-21B), -18A “135,” -18S "135,” -18AS "135,” -18 "150,” -18A "150,” -18S "150,” -18AS "150,” -19, (Army L-18C), -19S Description of the Type Design Change: Installation of modified instrument panel in accordance with Cub Crafters, Inc., Master Drawing List MDL 102700, Revision E, dated August 24, 1998, or later Federal Aviation Administration (FAA) approved revision. NOTE: This installation includes provisions for mounting radios and instruments in a new instrument panel. Any additions or changes to the original equipment radios or instruments will require separate FAA approval. The maximum weight of the equipment installed in the panel should not exceed that specified by Cub Crafters Installation Instructions 102700-11, Revision C, dated August 24, 1998, or later FAA-approved revision. Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to other aircraft on which other previously approved modification 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: September 24, 1997 Date reissued: January 26, 2012 Date of issuance: August 31, 1998 Date amended: (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) ## Every issue (2) - January 12, 2012: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/e9/de/e9de8280f7dc4de23a68441857613c02c2f985bca523047974e9ddd881fc61a4) - August 31, 1998: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/3b/54/3b547d747cdfdf4b7331cb5424433ea3ee27e3444d30e14dab06f22a4126cfef) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.