STC SE40WE

Supplemental type certificate · TALCO Aviation

Holder
TALCO Aviation · United States
Status
Current · Reissued
Status date
August 31, 2023
Applied
September 17, 1967
Product
Engine
Data sheet
TCDSE-295

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of two Roto-Master Turbochargers Model No. 3DT5FF10J2, P/N 600572-00 (formerly Rayjay Model No. 315F10 P/N RJ0080-100, -101, or - 102)

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.

SE40WE TALCO Aviation 3015 E. New York St, STE A2-270 Aurora, IL 60504 Part 13 the Civil Air Regulations E-295 Lycoming O-540-A1A, A1A5, A1B5, A1C5, A1D5, A3D5, B1A5, B1B5, D1A5, E4A5, E4B5, E4C5 Installation of two Roto-Master Turbochargers Model No. 3DT5FF1012, P/N 600572-00 (formerly Rayjay Model No. 315F10 P/N RJ0080-100, -101, or -102) on engine models listed above in accordance with FAA sealed Roto-Master (formerly Rajay) Drawing No. RJ0899, dated September 27, 1967, and Revision "C", dated April 15, 1983, or later FAA-approved revision. (Turbocharger/Engine compatibility only).

(See continuation sheet 3 of 3) September 17, 1967 1/14/68, 2/10/82, 11/23/87, 9/22/95, 12/19/03, 6/26/06, 3/16/07, 3/12/18, 2/2/2021; 8/31/2023 December 8, 1967 July 30, 1968, July 15, 1983 for Paul (Vu) Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 3

SE40WE 3

SE40WE Date of Issuance: December 8, 1967 Date Amended: July 15, 1983 Date of Reissuance: August 31, 2023

The installer must determine whether this design change is compatible with previously approved modifications. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

See attached Supplemental Type Certificate S40WE Addendum which is part of this certificate, for the applicable operating limitations.

OPERATING LIMITATIONS:

The limitations prescribed in FAA Engine Type Certificate Data Sheet No. E-295 are applicable except as noted below:

Altitude RPM MP

Below 3500 feet - Do Not Use Turbocharger.

2500-14,000 feet 2700 28.5

Over 14,000 feet 2500 27.0

-END- 3 3

ADs that name this STC · 1

An AD can apply because an STC is installed, or mention one in its text.

Approved models · 12

MakeModelData sheet
Textron Lycoming AVCO CorporationO-540-A1AE-295
Textron Lycoming AVCO CorporationO-540-A1A5E-295
Textron Lycoming AVCO CorporationO-540-A1B5E-295
Textron Lycoming AVCO CorporationO-540-A1C5E-295
Textron Lycoming AVCO CorporationO-540-A1D5E-295
Textron Lycoming AVCO CorporationO-540-A3D5E-295
Textron Lycoming AVCO CorporationO-540-B1A5E-295
Textron Lycoming AVCO CorporationO-540-B1B5E-295
Textron Lycoming AVCO CorporationO-540-D1A5E-295
Textron Lycoming AVCO CorporationO-540-E4A5E-295
Textron Lycoming AVCO CorporationO-540-E4B5E-295
Textron Lycoming AVCO CorporationO-540-E4C5E-295

Every issue · 4

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
August 31, 2023Reissued, currentCertificate
March 5, 2018Reissued, earlier issueCertificate
June 26, 2006Reissued, earlier issueCertificate
December 19, 2003Reissued, earlier issueCertificateSE40WE-1