STC SE00143SE

Supplemental type certificate · Dakota Aircraft Parts Inc

Holder
Dakota Aircraft Parts Inc · United States
Status
Current · Issued
Status date
April 26, 1995
Applied
January 23, 1992
Product
Engine
Certification basis
Part 21
Data sheet
TCDSE5CE

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

What it approves

Replaces the following Teledyne-Continental part numbers: 641682 (Rocker Arm, Exhaust), 539742 (Rocker Arm, Intake), 539740 (Rocker Arm, Shaft) and 538304 (Pushrod Assembly)

What the certificate saysOCR

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SE00143SE This certificate issued to: Dakota Aircraft Parts, Inc.

P.O. Box 1021 Sturgis, SD 57785 Purt 13 of the Civil Air Regulations.

Original Product - Type Certificate Number: ESCE Make: Teledyne-Continental Model: See Page 3 Description of Type Design Change:

Replaces the following Teledyne-Continental part Numbers: 641682 (Rocker Arm, Exhaust), 539742 (Rocker Arm, Intake), 539740 (Rocker Arm, Shaft) and 538304 (Pushrod Assembly) in the engine models listed in page 3 with parts manufactured in accordance with Dakota Aircraft Parts, Inc., Master Drawing List No 91-Rocker, dated June 14. 1994.

tirnitalions and benditions:

Approval of this change in type design applies specifically to the engine models listed in page 3 only.

This approval should not be extended to other engines of these models on which other previously approved modifications are incorporated unless it is determined that the inter-relationship between this change and any of these other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that engine. A copy of this certificate shall be anaid and of the ping daint reds for the peed enginel/emain inful unlid surrendered, suspended, revoked, or a lermination dale is dherwise es labdished by the Adminis traler of the Federal Aviation Administration Date of Application: January 23, 1992 Sate visard Dates issuana: APR 2 6 1995 Date Amended:

FEDERAL AVIATION "By direction of the Stel ві Скенк tanu (Signature ) VANIS RATOR Acting Manager, Seattle Aircraft Certification Office, ANM-100S (Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SE00143SE The following Teledyne-Continental parts are being replaced by parts manufactured by Dakota Aircraft Parts, Inc.:

Part Name Teledyne-Continental Dakota Aircraft Part Numbers Part Numbers Rocker Arm, Exhaust 641682 R91-E, R91-S & R91-PR Rocker Arm, Intake 539742 R91-1, R91-S & R91-PR Push Rod Assembly 538304 P91-C Rocker Arm Shaft 539740 S91-2 In the chart above: R91-E is exhaust rocker arm, R91-l is intake rocker arm, R91-S is the rocker arm seat and R91-PR represents the rocker arm roller and pin.

All Dakota Aircraft Parts, Inc. components listed ahove must be installed as a set.

Applicability of the Design Change.

The following Teledyne-Continental engine models are eligible to use the Dakota Aircraft Parts, Inc. components listed above:

Engine Model Type Cert. No. Regulation IO-520-A, -BA, -C, -D. -E. ESCE See Type Certificate -F, -J, -K, -L, and -M Data Sheet END

FAA FORM B110-2-1 (10-69) PAGE 3 OF 3 PAGES APR 2 6 1995 c FAA AC 82-03578

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 · 10

MakeModelData sheet
Continental MotorsIO-520-AE5CE
Continental MotorsIO-520-BAE5CE
Continental MotorsIO-520-CE5CE
Continental MotorsIO-520-DE5CE
Continental MotorsIO-520-EE5CE
Continental MotorsIO-520-FE5CE
Continental MotorsIO-520-JE5CE
Continental MotorsIO-520-KE5CE
Continental MotorsIO-520-LE5CE
Continental MotorsIO-520-ME5CE