Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Reissued
Status date
December 10, 2008
Applied
March 29, 2002
Product
Aircraft · Single-Engine
Certification basis
Part 3, Part 21, Part 23
Data sheet
TCDSA25SO

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

What it approves

Installation of S-TEC Digital Flight Control System (autopilot) Part No. 01298-01-01-001 or 01304-01-01-001 1500 Autopilot with Autotrim and Yaw Damper System, per Report 97-13001-003, Revision 2 dated 9/23/2003

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.

This Certificate issued to

Part 3 of the Civil Air Regulations.

1. Installation of S-TEC Digital Flight Contro l System (autopilot) Part No. 01298-01-01-001 or 01304- 01-01-001 1500 Autopilot with Autotrim and Yaw Damper System, per Report 97-13001-003, Revision 2 dated 9/23/2003 and in accordance with ST-891 Master Drawing List No. 921213, Revision D, dated 7-24-08 or later FAA Approved revisions of the above data (28 Volt System).

(See Continuation Sheet, Page 2, a part of this STC.)

1. Compatibility of this modification with other previ ously approved modifications must be determined by the installer.

S-TEC Corporation One S-TEC Way Mineral Wells Municipal Airport Mineral Wells, TX 76067-9236 A25SO Make : Piper Model : PA-46-500TP

Date of application : 3-29-02 Date of issuance : 5-21-02 Date reissued : 12-10-2008 Date amended : 10-01-2003 By direction of the Administrator

(Signature)

Randy Harper DAS 100.4 DAS assistant administrator, DAS700096SW (Title)

FAA Form 8110-2-1(10-69) Page 2 of 3

Number SA09521AC-D Date Re-Issued 12-10-2008

Transfer the ownership of Supplemental Type Certificate Number

to (Name of transferee)

(Address of transferee) (Number and street)

(City, State, and ZIP code)

from (Name of grantor) (Print or type)

(Address of grantor) (Number and street)

(City, State, and ZIP code)

Signature of grantor (In ink):

FAA Form 8110-2-1(10-69) Page 3 of 3

Number SA09521AC-D Date Re-Issued 12-10-2008 Limitations and Conditions (con’t.)

2. 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.

3. FAA/DAS Approved Pilot’s Operating Handbook and/ or Airplane Flight Manual Supplement, P/N 892112, dated 5-21-02 is required for Piper model PA-46-500TP for MAGIC 1500 Autopilot or later FAA Approved revisions of the above supplement.

4. FAA Approved Pilot’s Operating Handbook and/or Airplane Flight Manual Supplement, P/N 892112, Revision 1, dated 10-01- 03 is required for Piper m odel PA-46-500TP for S-TEC 1500 Autopilot or later FAA Approved revisions of the above supplement.

5. FAA/DAS Approved Pilot’s Operating Handbook and/ or Airplane Flight Manual Supplement, P/N 892112, Revision 2, dated 12-10-08 for S-TEC 01298/ 01304 Digital Flight Control System with WAAS is required for Piper model PA-46-500TP for S-TEC 1500 Autopilot or later FAA Approved revisions of the above supplement.

The Federal Aviation Regulations applicable to this project are shown below.

Systems and Equipment:

FAR 23.603 23.685 23.1321 23.1351

23.1541

23.607 23.689 23.1325 23.1357

23.1555

23.609 23.771 23.1329 23.1365

23.671 23.1301 23.1331 23.1367

23.677 23.1309 23.1335 23.1381

Structures:

FAR 23.301(a) 23.307 23.601 23.609

23.303 23.395(a)(1) 23.603 23.611

23.305 23.561(e) 23.605(a)

Flight Test:

FAR 23.777(a)(b) 23.1357(a)(d) 23.1541(a)(2) & (b)

23.1321 23.1367(c)(d) 23.1555(a)

23.1322 23.1381(a)(b) 23.1581(a)(1)(2)

23.1329 23.1501 23.1585(a)

Additionally, in accordance with FAR 21.50, compliance will be shown with FAR section 23.1529.

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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 · 1

MakeModelData sheet
Piper Aircraft Inc.PA-46-500TPA25SO