STC SA4737SW

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
August 4, 1982
Applied
May 13, 1982
Product
Aircraft · Small Airplane
Certification basis
Part 21
Data sheet
TCDS2A13

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of S-TEC System 60 Pitch Stabilization System Model ST-111 with optional Autotrim System

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.

United grata of America department of Transportation— federal atriation Administration Supplemental TCgpe CertificateAS , isKitmver' SA4737SW Project A5903SW-DS FKP-190 S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 ^ ^.^<sc^Wy£5»«<^xw<!«<^^ 3 *sleaMta&&nA>.

Civil Air 2A13 Piper PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA— 28— 235 Installation of S-TEC System 60 Pitch Stabilization System, Model ST-111 with Optional Autotrim System according to Bulletin No. 214 dated 5-06-82 and Master Drawing list No. 92121 dated 5-06-82, or later FAA approved revision.

(14 Volt System) gee Continuation Sheet, page 2, of this STC.

May 13, 1982 AugUSt 4, 1982 _ . Wat80n Manager, Aircraft Certification Division Southwest Region (Title)

FAA Fou> 8110-2 (10-68)

United States of America Bepartment of Itonsportadon— federal Stn'adon Administration Supplemental t^pt Certificate(Continuation £heet) SA4737SW Limitations and Conditions:

1. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89141 dated 8-4-82, is required for Piper Models PA-28-140, PA-28-150, PA-28-160, PA-28-180 S/N 28-1 through S/N 28-7205318 and PA-28-235, S/N 28-10003 through S/N 28-10719 with S-TEC System 60 Pitch Stabilization System; OR, FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89142 dated 8-4-82, is required for Piper Model PA-28-235 S/N 28-10720 through S/N 7210023 with S-TEC System 60 Pitch Stabilization System.

3. Compatibility of this modification with other previously approved modifications must be determined by the installer.

1 alteration of this certificate is punishable by a fine of not exceeding SI,000, or imprisonment not exceeding 3 years, or both.

FORM Blio-2-1 (10-69) '1 his certijifate may be transferred in accordance with FAR i'7 •/" PAGE 2 OF 2PAGES

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) ( City, State, and <Y/> code) from (Name of grantor) (Print or type) .

(Address of grantor) (Number and street) (City, State, and .?1P code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

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 · 5

MakeModelData sheet
Piper Aircraft Inc.PA-28-1402A13
Piper Aircraft Inc.PA-28-1502A13
Piper Aircraft Inc.PA-28-1602A13
Piper Aircraft Inc.PA-28-1802A13
Piper Aircraft Inc.PA-28-2352A13