STC SE4-1638

Supplemental type certificate · TALCO Aviation

Holder
TALCO Aviation · United States
Status
Current · Reissued
Status date
August 31, 2023
Applied
February 2, 1959
Product
Engine
Data sheet
TCDSE-274

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

What it approves

Installation of one Roto-Master Turbocharger Model No. 3DT5FF10J2, P/N 600572-00 (formerly Rajay 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.

SE4-1638 TALCO Aviation 3015 E. New York St, STE A2-270 Aurora, IL 60504 Part 13 the Civil Air Regulations E-274 Lycoming O-320-A and -B Series Installation of one Roto-Master Turbocharger Model No. 3DT5FF10J2, P/N 600572-00 (formerly Rajay Model No. 315F10 P/N RJ0080-100, -101, or -102) in accordance with FAA sealed Roto-Master (formerly Rajay) Drawing List RJ0199, Revision "A", dated 5/24/83 or later, FAA approved revision.

(See continuation sheet 3 of 4) February 2, 1959 1/10/64, 1/14/69, 2/10/82, 10/30/87, 9/22/95, 1/16/04, 6/26/06, 3/16/07, 3/12/18; 2/2/2021; 8/31/2023 December 5, 1961 May 1, 1962, July 15, 1983 for Paul (Vu) Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 4

SE4-1638 4

SE4-1638 Date of Issuance: December 5, 1961 Date Amended: July 15, 1983 Date of Reissuance: August 31, 2023

This approval covers engine/turbocharger compatibility only. See below for Engine Operating Limitations. 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.

ENGINE OPERATING LIMITATIONS

Where applicable, the following engine limitations supersede those specified on Engine Type Certificate Data Sheet E-274-7.

Engine Speed (Turbosupercharged)

Maximum - 2400 RPM

Minimum - 2200 RPM

Manifold Pressure (Turbosupercharged)

Maximum - 28.0 in. Hg.

Cylinder head temperature (Maximum)

Unsupercharged - 500 deg. F.

Turbosupercharged - 475 deg. F.

SE4-1638 Date of Issuance: December 5, 1961 Date Amended: July 15, 1983 Date of Reissuance: August 31, 2023

Fuel

Model O-320-A - minimum grade aviation - 91/96 octane

Model O-320-B - minimum grade aviation - 100/130 octane

Altitude

Maximum - 20,000 ft.

Minimum - 5,000 ft.

Fuel pressure

Green arc .5 psi to 5.0 psi with red lines at .5 psi and 5.0 psi. Additional green arcs from 1 psi to 13 psi with red lines at 1 psi and 13 psi with note "Turbo Range See Placard".

Engine and Turbocharger Operation

Do not operate the turbosupercharger unless the throttle is wide open.

When increasing power, fully open the throttle, and then slowly close the wastegate until desired power setting is obtained. When decreasing power, fully open wastegate, then close the throttle. The mixture control must be in full rich position for all turbosupercharged operation.

-END- 4 4

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
Textron Lycoming AVCO CorporationO-320-A SeriesE-274
Textron Lycoming AVCO CorporationO-320-B SeriesE-274

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
January 16, 2004Reissued, earlier issueCertificate