STC SA5354SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
November 29, 1984
Applied
October 18, 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 5, 2025.

What it approves

Installation of S-TEC System 60 pitch stabilization system, Model ST-250, with optional automatic electric trim system.

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: SA5354SW-D This certificate issued to: 1e. S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 Part 3 of the CiVil Air Hegulations.

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

installation of S-TEC System 60 Pitch Stabilization System, Model ST-250, with Optional Automatic Electric Trim System, according to Bulletin No. 350, dated 10-05-84 and Master Drawing List No. 92291, dated 10-05-84 and/or later FAA Approved revisions of the above data (14 Volt System).

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

2. Also eligible on the above listed Models when equipped with Approved Turbo- . charged Engines (250 H.P.) and/or Wing Tip Tanks per STC SA1480WE, This creati and the supering Pade which paht basis orS STeal shal remain in effect until sun vendered, suspended, versked, on a termination date is sherise estallished by the Administrator of the Federal Aviation Administration .

Date of Application: 10-18-84 Date Reissued:

Date of Issuance: 11-29-84 Date Amended:

FEDERAL AVIATION By Direction of the Administrator (Signature ) TOMINISTA ATIO DAS Staff Coordinator, DAS 5 Sw Harold W. Holdeman (Title) 47 FAr FoRM 8110-2 (10-68)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Shcet) Number: SA53545W-D Limitations and Conditions: (con't)

3. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89538, dated 11-29-84 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.

t abestan of thus ertıficate is punshable by a fıne of not exteeding SLO00, or imprisonment not excedrs 3 vears, a har 1 2^ [i211 81102-1 (10-60) This certificate may be transferred in accrdance with fAk 1 I PAGE 20F 2 PAGES

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):

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