STC SA5365SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
December 20, 1984
Applied
October 31, 1984
Product
Aircraft · Small Multi-Engine
Certification basis
Part 21
Data sheet
TCDS1A10

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

What it approves

Installation of S-TEC System 60 single axis automatic flight guidance system, Model ST-264.

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: SA53655W-0 This certificate issued to: S-TEC Corporation Rt. 4, Blag. 940 Wolters Industrial Complex Mineral Wells, TX 76067 Part 3 of the CiVIl Air Regulations.

Original Product - Type tientifical Number: 1A10 Make: PIPER Model: PA-23-250 AND PA-E23-250 Description of Type Design Change:

Installation of S-TEC System 60 Single Axis Automatic Flight Guidance System, Model ST-264, according to Bulletin No. 364, dated 10-19-84 and Master Drawing List No. 9769t System 10-19-84 and/or fater FAA Approved revisfons of the above data (28 Volt Limitations and Conditions:

1. Eligible only on Piper Models PA-23-250 and PA-E23-250, S/N 27-2000 througn S/N 27-7554172.

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

Date of Application: 10-31-84 Date Reissued:

Date of Issuance: 12-20-84 Date Amended:

FEDERAL AVIATION By Direction of the Administrator (Signalure) TAMIN STRATIO Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW (Title)

Fra Food 8110-2 (10-68)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA53655W-D Limitations and Conditions: (con't)

2. Also eligible on the above listed Models when equipped with Approved Turbocharged Engines (250 H.P.) and/or Wing Tip Tanks per STC SA1480WE.

3. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89543, dated 12-20-84 is required and/or later FAA Approved revisions of the above supplement.

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

taran of this certificate is punishable by a fine of not exceeding SLODO, or imprisonment not exceeding 3 vars, uper IA: FÖRM1 81102-1 (10-69) This certificate may be transferred in accordance with 1.1k at 1:

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 ) trom (Name of grantor) (Print or type) - (Address of grantor) (Number and street) (City, State, and ZIP code ) Extent of Authority (if licensing agreement):

Date of Transfer: _ Signature of grantor (In ink): _ U.S. 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
Piper Aircraft Inc.PA-23-2501A10
Piper Aircraft Inc.PA-E23-2501A10