STC SA7812SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Amended
Status date
January 12, 1999
Applied
February 19, 1992
Product
Aircraft · Small Multi-Engine
Certification basis
Part 21
Data sheet
TCDSA20SO

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

What it approves

Installation of S-TEC Yaw Damper System, Model ST-468.

What the certificate saysOCR

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA7812SW-D This certificate issued to: S-TEC Corporation One S-TEC Way Mineral Wells Municipal Airport Mineral Wells, TX 76067-9236 Certifies that the change in the type design for the following freduct with the limitations and conditions therefor as specified hercen meets the ninothiness requiements of Part 3 of the kirit din Regulutions.

Original Product Type Certificate A unter: A20SO Make: Piper Model: PA-31, PA-31-300, PA-31-325, and PA-31-350 Description of Type Design Change:

Installation of S-TEC Yaw Damper System, Model ST-468, according to Bulletin No. 568, Revision 3, dated 1-07-99 and Master Drawing List No. 92558, Revision C, dated 1-07-99 or later FAA Approved revisions of the above data (28 Volt System).

Also eligible on models PA-31 and PA-31-300 when modified per STC SA970SO (350 H.P.

Colemill conversion).

Also eligible on model PA-31-325 when modified per STC SA00048SE (vortex generator system).

Also eligible on model PA-31-350 when modified per STC SA1151SO (Colemill Panther II conversion) and/or any of the following SICS: STC SA5796NW, STC SA00192SE, STC SA00039SE, STC SA00126SE (vortex generators and gross weight increase).

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

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: 2-19-92 Date Reissued:

Date of Issuance: 3-09-92 Date Amended: 5-09-97, 11-09-98, 1-12-99 Revision 3 By Direction of the Administrator EDERAL AVIATION Milal le (Signature) TOMINSTRATO Michael Keirnan DAS Staff Coordinator, DAS 5 SW (Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA7812SW-D, Revision 3 Limitations and Conditions: (con't.)

4. FAA/DAS Approved Airplane Flight Manual Supplement, P/N 89963, dated 3-09-92 is required for Piper Models PA-31 and PA-31-300 And The Above Models When Modified Per STC SA970SO (350 H.P. Colemill Conversion) or later FAA Approved revisions of the above supplement.

FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 89963, Revision 1, dated 5-09-97 is required for Piper Models PA-31 and PA-31-300 And The Above Models When Modified Per STC SA970SO (350 H.P. Colemill Conversion) and Model PA-31-325 And The Above Model When Modified Per STC SA00048SE (Vortex Generator System) or later FAA Approved revisions of the above supplement.

FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 89963, Revision 2, dated 11-09-98 is required for Piper models PA-31 and PA-31-300 and the above models when modified per STC SA970SO (350 H.P. Colemill conversion) and model PA-31-325 and the above model when modified per STC SA00048SE (vortex generator system) and model PA-31-350 and the above model when modified per STC SA1151SO (Colemill Panther I| conversion) or later FAA Approved revisions of the above supplement.

FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 89963, Revision 3, dated 1-12-99 is required for Piper models PA-31 and PA-31-300 and the above models when modified per STC SA970SO (350 H.P. Colemill conversion) and Piper model PA-31-325 and the above model when modified per STC SA00048SE (vortex generator system) and Piper model PA-31-350 and the above model when modified per STC SA1151SO (Colemill Panther II conversion) and/or any of the following STCS: SIC SA5796NW, STC SA00192SE, STC SA00039SE, STC SA00126SE (vortex generators and gross weight increase) or later FAA Approved revisions of the above supplement.

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

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

TRANSFER ENDORSEMENT 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) (Numher and streel) (Calr. Stale, and All code ) Extent of Authority (if licensing agreement):

Date of Transfer: - 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 · 4

MakeModelData sheet
The New Piper Aircraft Inc.PA-31A20SO
The New Piper Aircraft Inc.PA-31-300A20SO
The New Piper Aircraft Inc.PA-31-325A20SO
The New Piper Aircraft Inc.PA-31-350A20SO