STC SA01158SE

Supplemental type certificate · Cub Crafters Inc

Holder
Cub Crafters Inc · United States
Status
Current · Reissued
Status date
January 26, 2012
Applied
August 12, 2002
Product
Aircraft · Single-Engine
Certification basis
Part 21, Part 23
Data sheet
TCDS1A2

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Install heavy duty tail wheel assembly in accordance with Cub Crafters, Inc. Master Document List Report CR123300-3, Revision D, dated July 15, 2003, or later Federal Aviation Administration approved revision. This modification does not require specific continued airworthiness instructions. Federal Aviation Regulation 43 is adequate to insure Continued Airworthiness of this modification.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

Number SA01158SE

This certificate, issued to Cub Crafters, Inc.

1918 South 16th Avenue Yakima, WA 98903-1212 Part 23 of the Federal Aviation Regulations.

Original ProductType Certificate Number: 1A2 Make: Piper Model: PA-18, PA-18A, PA-18S, PA-18 “105” Special, PA-18S “105” Special, PA-18 “125” (Army L-21A), PA-18S “125,” PA-18AS “125,” PA-18 “135” (Army L-21B), PA-18A “135,” PA-18S “135,” PA-18AS “135,” PA-18 “150,” PA-18A “150,” PA-18S “150,” PA-18AS “150,” PA-19 (Army L-18C), PA-19S

Description of the Type Design Change: Install heavy duty tail wheel assembly in accordance with Cub Crafters, Inc. Master Document List Report CR123300-3, Revision D, dated July 15, 2003, or later Federal Aviation Administration approved revision. This modification does not require specific continued airworthiness instructions. Federal Aviation Regulation 43 is adequate to insure Continued Airworthiness of this modification.

Limitations and Conditions: Approval of this change in type design applies to the airplane models listed above, only. This approval should not be extended to other aircraft 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: August 12, 2002 Date reissued: January 26, 2012 Date of issuance: January 3, 2003 Date amended: June 13, 2003; August 8, 2003

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

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 18

MakeModelData sheet
Piper Aircraft Inc.PA-181A2
Piper Aircraft Inc.PA-18-105 (Special)1A2
Piper Aircraft Inc.PA-18-125 (Army L-21A)1A2
See all 18 models

Every issue · 2

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
January 26, 2012Reissued, currentCertificate
August 8, 2003Amended, earlier issueCertificate