STC SE32WE

Supplemental type certificate · TALCO Aviation

Holder
TALCO Aviation · United States
Status
Current · Reissued
Status date
August 31, 2023
Applied
December 6, 1966
Product
Engine
Data sheet
TCDS1E10

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

What it approves

Installation of Turbocharger P/N 600573-00 (formerly RJ 0326, RJ 0326-1), 600576-00(formerly RJ 0326-2) and600577000 (formerly RJ 0329).

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.

SE32WE TALCO Aviation 3015 E. New York St, STE A2-270 Aurora, IL 60504 Part 13 the Civil Air Regulations 1E10 Lycoming IO-360-A1A, A1B, A1C, A2A, A2B, A2C, B1A, B1B, B1C, B1D, B1E, B1F, B2E, B2F, B4A, C1A, C1B, C1C, D1A, E1A, C1E6, & LIO-360-C1E6, AEIO-360-A1A, A1B, A2A, A2B, B1B Installation of Turbochargers P/N's 600573-00 (formerly RJ 0326, RJ 0326-1), 600576-00 (formerly RJ 0326-2), and 600577-00 (formerly RJ 0329) in accordance with FAA sealed Roto-Master (formerly Rajay) Drawing No. RJ 4999, dated December 5, 1966, revised on September 23, 1982, or later FAA approved sealed revision.

(See continuation sheet 3 of 4) December 6, 1966 1/14/69, 2/10/82, 9/24/82, 10/30/87, 9/22/95, 12/12/03, 6/26/06, 3/16/07, 3/12/18, 2/2/2021; 8/31/2023 January 12, 1967 September 17, 1970; October 22, 1974; November 13, 1974;

March 31, 1978 for Paul (Vu) Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 4

SE32WE 4

SE32WE Date of Issuance: January 12, 1967 Date Amended: March 31, 1978 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 SE32WE 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. 1E10 are applicable except as noted below:

Altitude MAP RPM

Normal Operation

Takeoff S.L. F.T. 2700

Max. Cont. S.L. F.T. 2700

Turbocharged Operation

For all operation 3500 to 20,000 28.5 2700

20,000 to 25,000 25.0 2700

Air Throttle Valve Inlet Air Temp. 238˚F Max.

SE32WE Date of Issuance: January 12, 1967 Date Amended: March 31, 1978 Date of Reissuance: August 31, 2023

Throttle must be wide open prior to and during turbocharger operation. Wastegate must be fully open prior to moving throttle from wide-open position.

-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 · 26

MakeModelData sheet
Textron Lycoming AVCO CorporationAIO-360-A1A1E10
Textron Lycoming AVCO CorporationAIO-360-A1B1E10
Textron Lycoming AVCO CorporationAIO-360-A2A1E10
See all 26 models

Every issue · 3

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