STC SA1581NM

Supplemental type certificate · Turbo West Inc

Holder
Turbo West Inc · United States
Status
Current · Amended
Status date
May 17, 1984
Applied
June 15, 1982
Product
Aircraft · Small Multi-Engine
Certification basis
Part 21
Data sheet
TCDSA8EA

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

What it approves

Installation of a bleed air heat system.

What the certificate saysOCR

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

Profe No. T805 NMD-DS United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA1581NM This certificate issued to: Turbo West, Inc.

Jefferson County Airport Broomfield, Colorado 80020 Part 3 of the CIVIl Air Regulations.

Original Product - Type Berlificate Number: ASEA Make: Piper Aircraft Corporation Model: PA-31T and PA-31T1 Description of Type Design Change:

Installation of a bleed air heat system in accordance with FAA sealed Drawing Lists TW1049-01 or TW-1049-02 approved May 11, 1984 or later FAA approved revisions.

1. FAA approved Airplane Flight Manual Supplement (AFMS) for Model PA-31T, and

2. Instructions for continued Airwithin Fs, supplement is continuous inspection Manual P/N 761644, FAA approved May 15, 1984, or later FAA approved revision is required.

3. See (Continuation Sheet) page 3 of 3 pages.

Date of Application: June 15, 1982 Date Reissued:

Date of Issuance: May 15, 1984 I ale unended: May 17, 1984 FEDERAL AVIATION By Direction of the Administrator Nored Rearr Woodtord K. Boyce (Signalure) Manager CMINISTRAIO Denver Aircraft Certification Office Northwest Mountain Region, Aurora, Colorado 47 FAA FoRM 8110-2(10-68)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1581 M Limitations and Conditions:

3. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any other previously approved modifications will introduce no adverse effect upon the airworthiness of the aircraft.

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ADs that name this STC · 0

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No AD in this release names this STC

Approved models · 2

MakeModelData sheet
Piper Aircraft Inc.PA-31TA8EA
Piper Aircraft Inc.PA-31T1A8EA