STC SA5146SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
March 21, 1983
Applied
February 9, 1983
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS3A13

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-047 with optional automatic electric trim 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.

ttratrd gtotw of awrtca Bepartmcnt of ICransportation—federal 2Uriation administration Supplemental t:uje Certificate SA5146SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 £Tn//a/<<?T^*(vnd<c<>ncu&4>n& J 4*^2/14 L1V1 I Air

•SleiaMfa&c- CESSNA 182P AND 182Q Installation of S-TEC System 60 Pitch Stabilization System Model ST-047 with Optional Automatic Electric Trim System according to Bulletin No. 150, Revision 3, dated 2-02-83 and Master Drawing List No. 9262, Revision C, dated 2-02-83 and/or later FAA Approved revisions of the above data (14 Volt System).

1. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 8975-1, dated 3-21-83 is required for Cessna Models 182Q S/N 18266591 and up and/or later FAA Approved revisions of the above supplement.

See continuation sheet, Page 2, a part of this STC.

^ £Xdrri*n4&tr<i&>r*jifJ 2-09-83 3-21-83 ( Signature} Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW————————(TitU)————————

This ctrtificatt may bt trmuftrnd m ttetrianc* mtk FAR 21.47.

rxA row • 110-2 (i »-6<)

ttmtrd Stotu of ©cpartment of ^Transportation— Jp ederal aoiation administration Supplemental i:gpe Certificate(Continuation SA5146SW-D Continued 2 FAA Approved Supplemental Flight Manual for Cessna Model 182P and Cessna Model 182Q, S/N 18266590 and below, P/N 8960-2, dated 3-21-83 is required and/or later FAA Approved revisions of the above Supplement.

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

FAA FORM 8ito-2-i (10-69) This ctrtifcatt may bt transferred in accordant with FAR 21.17.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, Stale, and ZIP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and QP code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):.

US. GOVERNMENT PRINTING OFFICE : 1966 OF —205-579

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 · 2

MakeModelData sheet
Textron Aviation Inc.182P3A13
Textron Aviation Inc.182Q3A13