What it approves
Modification of a Lycoming0-235-L2C, or 0-235-L2A engine to increase HP rating from 115-HP at 2700 rpm to a continuous125 HP at 2800 rpm.
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.
Number SE792NW
This certificate, issued to 4J’s Aviation 661 Crawford Avenue Delta, CO 81416
Part 13 of the Civil Air Regulations, dated June 15, 1956 as amended by 13-1, 13-2, and 13-3 Original ProductType Certificate Number: E-223 Make: Lycoming Model: 0-235-L2C/L2A
Description of the Type Design Change: Modification of a Lycoming 0-235-L2C or 0-235-L2A engine to increase horsepower rating from 15 HP @ 2700 rpm to a continuous 125 HP @ 2800 RPM in accordance with Kennis B. Blackman Installation Instructions KB 1250.
NOTE: The modified engine shall be designated as 0-235-L2C(M) or 0-235-L2A(M).
Limitations and Conditions: Approval of this change in type design applies to the above model engine only.
This approval should not be extended to other engines of this model unless the installer determines that the relationship between this change and any other previously incorporated approved modifications will introduce no adverse effect upon the airworthiness of that engine. A copy of this certificate, and Addendum, must be maintained as part of the permanent records of the modified engine.
If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.
Date of application: June 26, 1979 Date reissued: July 26, 2019 Date of issuance: June 28, 1979 Date amended: February 19, 1987
FAA FORM 8110-2 (5/14) PAGE 1 OF 3 PAGES By direction of the Administrator
(Signature)
Acting Manager, Seattle ACO Branch (Title)
Transfer the ownership of Supplemental Type Certificate Number
to (Name of Transferee)
(Address of Transferee)
(Number and Street)
(City, State, and ZIP Code)
from (Name of Grantor) (Print or Type)
(Address of Grantor)
(Number and Street)
(City, State, and ZIP Code)
Signature of Grantor (In Ink):
U.S. GPO: 1987-763-289
United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) SUPPLEMENTAL TYPE CERTIFICATE ADDENDUM NO. SE792NW Number SE792NW
The conditions and limitations of Type Certificate Data Sheet E-223 apply except where superseded by the following:
This Supplemental Type Certificate Data Sheet, which is part of STC SE792NW, prescribes the conditions and limitations under which the product for which the STC was issued meets the airworthiness requirements of the Civil Air Regulations:
SUPPLEENTAL TYPE CERTIFICATE HOLDER: 4J’s Aviation
Engine: Lycoming 0-235-L2C (Modified) /-L2A (Modified) Fuel: 100/130 minimum grade aviation gasoline Engine Limits: For all operations, 2800 RPM (125 HP) Compression Ratio: 9.7:1 Placards: Placards and Operating Limitations on Type Certificate Data Sheet E-223 apply Except as noted herein:
a. Original Engine Data Plate:
Add a “suffix” (M) and the STC number to the model designation as follows:
b. Supplemental Engine Data Plate:
Install a Supplemental Data Plate adjacent to the original Data Plate to read as follows:
- END -
FAA FORM 8110-2 (5/14) PAGE 3 OF 3 PAGES
MODEL: 0-235-L2C(M) STC SE792NW
AVCO LYCOMING ENGINE
SUPPLEMENTAL DATA PLATE STC SE792NW
- TAKEOFF (5 MIN) 125 HP @ 2800 RPM
- NORMAL RATED 125 HP @ 2800 RPM
SPARK ADVANCE - 25º BTC
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 2
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| July 26, 2019 | Reissued, current | Certificate |
| February 19, 1987 | Amended, earlier issue | Certificate |