STC SE00754DE

Supplemental type certificate · Oilamatic, Inc

Holder
Oilamatic, Inc · United States
Status
Current · Reissued
Status date
January 11, 2013
Applied
October 31, 2011
Product
Engine
Certification basis
Part 21, Part 33
Data sheet
TCDSE7CE

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of an auxiliary oil sump port on the oil sump pan

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.

N umber SE00754DE This certificate, issued to : Oilamatic, Inc 5816 S. Jamaica Way Englewood, Colorado 80111 P art 33 of the Federal Aviation R egulations.

Original Product T ype Certificate N umber: E7CE M ake: Continental Motors M odel: GTSIO-520-D, -H, -L, -M and -N Description of the Type Design Change :

Installation of an auxiliary oil sump port on the oil sump pan in accordance with DRAWING LIST -520 Sump Drain Installation, Drawning No. 520400, dated April 11, 2012, FAA approved October 27, 2012, or later FAA approved revision.

1. Instructions for Continued Airworthiness, Oil Sump Port Installation Continental GTSIO-520 Engines, Document No. CW0720-1095, Revision IR, dated October 5, 2012, or later FAA accepted revision is required.

(Continued on Page 2)

Date of application: October 31, 2011 Date reissued: January 11, 2013

Date of issuance: November 28, 2012 Date amended: December 3, 2012

B y direction of the A dministrator

(Signature) Todd G. Dixon Northwest Mountain Region Manager Denver Aircraft Certification Office (Title)

N umber SE00754DE

2. Instructions for Continued Airworthiness, Oil Sump Port Installation Continental GTSIO-520 Engines, Document No. CW0720-1095, Revision IR, dated October 5, 2012, or later FAA accepted revision is required.

3. A copy of this STC must be included in the permanent records of the modified aircraft.

4. The installer must determine whether this design change is compatible with previously approved modifications.

5. If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission.

6. The FAA has not certified the equipment for which these provisions are intended. You must get additional FAA approval to install this equipment. The FAA must evaluate the installation to ensure it complies with the applicable airworthiness standards.

Certification B asis:

The type certification basis for the Continental Motors Model GTSIO-520 series engine is shown on TCDS E7CE for parts not changed or affected by this Supplemental Type Certificate. For parts changed or affected by this Supplemental Type Certificate, the certification basis is as follows:

33.1 Amendment 33-14

33.4 Amendment 33-9

33.15 Amendment 33-10

33.17(a)(b) Amendment 33-29

33.19(a) Amendment 33-28 A33.1 Amendment 33-9 A33.2 Amendment 33-9 A33.3 Amendment 33-21

-END-

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 · 5

MakeModelData sheet
Continental MotorsGTSIO-520-DE7CE
Continental MotorsGTSIO-520-HE7CE
Continental MotorsGTSIO-520-LE7CE
Continental MotorsGTSIO-520-ME7CE
Continental MotorsGTSIO-520-NE7CE

Every issue · 3

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

DateStatusFiles
January 11, 2013Reissued, currentCertificate
December 3, 2012Amended, earlier issueCertificate
November 28, 2012Issued, earlier issueCertificate