What it approves
Installation of Turbocharged Lycoming IO-360-A1B engine
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.
SA2990WE TALCO Aviation 3015 E. New York St, STE A2-270 Aurora, IL 60504 * * 1A13 Consolidated Aeronautics, Inc.
Lake LA-4-200 Installation of Turbocharged Lycoming IO-360-A1B engine in accordance with FAA Sealed Rotomaster Drawing List No. RJ 5450, dated June 11, 1982, or later FAA-approved sealed revision.
(See continuation sheet 3 of 4) September 13, 1974 February 10, 1982; October 23, 1987; September 22, 1995; January 16, 2004; July 3, 2006;
March 16, 2007; March 30, 2018; February 2, 2021; August 31, 2023 February 14, 1975 July 19, 1982 for Paul (Vu) Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 4
SA2990WE 4
SA2990WE Date of Issuance: February 14, 1975 Date Amended: July 19, 1982 Date of Reissuance: August 31, 2023
*Part 3 of the Civil Air Regulations dated December 15, 1946 and Amendments 3-1 and 3-2 thereto.
The limitations and conditions of Aircraft Specification No. 1A13 apply except as outlined below. A copy of this Supplemental Type Certificate must be included in the permanent records of each airplane modified in accordance with this Supplemental Type Certificate. 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 Lycoming IO-360-A1B modified to incorporate Turbosupercharging in accordance with Supplemental Type Certificate No. SE32WE
Engine Limits For all unsupercharged operations, 2700 rpm, Full throttle (200 HP).
For all turbosupercharged operations from 3,500 feet to 20,000 feet, 2700 rpm
28.5 in. Hg.
Airspeed Limits Never exceed Vne and maximum structural cruising Vno;
Reduce Vne and Vno 3 MPH per 1,000 feet above 18,000 feet.
SA2990WE Date of Issuance: February 14, 1975 Date Amended: July 19, 1982 Date of Reissuance: August 31, 2023
Maximum altitude 20,000 feet
Airplane Flight Manual The FAA Approved Rajay Airplane Flight Manual Supplement dated February 14, 1975 is required with this installation.
Limitation of Applicability The approval of this change in type design applies to the basic Lake LA-4-200 aircraft that are otherwise unmodified.
-END- 4 4
ADs that name this STC · 1
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| REVO Incorporated | Lake LA-4-200 | 1A13 |
Every issue · 5
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| August 31, 2023 | Reissued, current | Certificate |
| February 2, 2021 | Reissued, earlier issue | Certificate |
| March 30, 2018 | Reissued, earlier issue | Certificate |
| July 3, 2006 | Reissued, earlier issue | Certificate |
| January 16, 2004 | Reissued, earlier issue | Certificate |