# STC SE00768CH

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Champion Aerospace LLC, United States
- Description: Replace Slick 6000, 6100, 6200 and 6300 series  magnetos and TCM/Bendix S6-20, S6-200 and S6-1200 series magnetos with the Champion Limited Authority Spark Advance Regulator (LASARTM) ignition system
- Applied: February 28, 1997
- Status date: February 10, 2009
- Product: Engine
- Certification basis: Part 21
- Data sheets: [TCDS 1E4](https://openairdocs.org/tcds/1E4), [TCDS E-295](https://openairdocs.org/tcds/E-295)
- Certificate PDF: https://openairdocs.org/files/sha256/01/1f/011f20260eb9cddd79ea9f00be15cb594c9e4228c5393c421f6635d1864a3201
- Approved model list and other attachments: [SE00768CH.AML.pdf](https://openairdocs.org/files/sha256/34/87/348756a86da6b44aff807d754bc7966a472c5c246efec03f004d72b5c926e641)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6592FEF0AD4B2E6A86257599006A3205.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SE00768CH

## ADs that name it (0)

None.

## Approved models (43)

- Textron Lycoming AVCO Corporation AEIO-540-D4A5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation AEIO-540-D4B5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation AEIO-540-D4C5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation AEIO-540-L1B5 ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation HIO 540-A1A ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation IO-540 Series ([TCDS 1E4](https://openairdocs.org/tcds/1E4))
- Textron Lycoming AVCO Corporation O-540 Series ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-A Series ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-A1A ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-A1A5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-A1B5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-A1C5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-A1D ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-A1D5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-A2B ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-A3D5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-A4A5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-A4B5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-A4C5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-A4D5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-B Series ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-B1A5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-B1B5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-B1D5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-B2A5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-B2B5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-B2C5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-B4A5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-B4B5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-D1A5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-E Series ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-E4A5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-E4B5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-E4C5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-F Series ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-F1A5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-F1B5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-G Series ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-G1A5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-G2A5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-H Series ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-H1A5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))
- Textron Lycoming AVCO Corporation O-540-H2A5 ([TCDS E-295](https://openairdocs.org/tcds/E-295))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

Part * of the *r Regulations.*

Original Product--Type Certificate Number: * *See attached FAA Approved Model List Make: * (AML) No. SE00768CH for list of approved engine Model : *models and applicable airworthiness regulations

Replace Slick 6000, 6100, 6200 and 6300 series magnetos and TCM/Bendix S6-20, S6-200 and S6-1200 series magnetos with the Champion Limited Authority Spark Advance Regulator (LASARTM) ignition system in accordance with Unison Service Letter SL1-96 dated August 28, 2001, Revision G and Approved Parts Matrix included in SL1-96, or later FAA approved revisions.

1. Compatibility of this design change with previously approved modifications must be determined by the installer.

2. LASARTM can only be installed as a complete system. Existing magnetos must be removed from the engine prior to conversion.

3. Operation of LASARTM system equipped engines requires a minimum grade of 100 Octane Av-Gas.

4. A copy of this Certificate and AML No. SE00768CH dated October 21, 1997 or later FAA approved revision must be maintained as part of the permanent records for the modified aircraft.

5. 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.

Champion Aerospace LLC 1230 Old Norris Road Liberty, SC 29657

Date reissued : February 10, 2009

Date amended : September 11, 2001

( Signature) Thaddeus D. Krolicki, Jr.

Manager, Propulsion Branch Chicago Aircraft Certification Office

( Title)

Date of application : February 28, 1997

Date of issuance : October 21, 1997

### SE00768CH.AML.pdf

**FAA APPROVED MODEL LIST (AML) NO. SE00768CH**

CHAMPION AEROSPACE LLC FOR INSTALLING CHAMPION LASAR ™ IMPULSE COUPLED MAGNETO SYSTEM Date of Issuance: October 21, 1997

Page 1 of 1

**ORIGINAL TYPE**

CERTIFICATION BASIS * INSTALLATION

**INSTRUCTIONS**

* AFM

AML

**ITEM ENGINE MAKE ENGINE MODEL**

**CERTIFICATE NUMBER FOR**

**ALTERATION**

**NUMBER**

**REVISION NO. / DATE**

**SUPPLEMENT NO. / DATE**

AMENDMENT DATE 1 Textron Lycoming O-540-A1A, -A1A5, -A1B5, -A1C5, -A1D, -A1D5, -A2B, -A3D5, -A4A5, -A4B5, -A4C5, -A4D5, -B1A5, -B1B5, -B1D5, -B2A5, -B2B5, -B2C5, -B4A5, -B4B5, -D1A5, -E4A5, -E4B5, -E4C5, -F1A5, -F1B5, -G1A5, -G2A5, -H1A5, -H2A5

E-295 CAR 13 SL1-96 Rev. G Dated:

8/28/2001 N/A 9/11/01 2 Textron Lycoming IO-540-A1A5, -B1A5, -B1B5, -B1C5, -C1B5, - C1C5, -C2C, -C4B5, -C4C5, -C4D5, -D4A5, -D4B5, -D4C5, -E1A5, -E1B5, -E1C5, -G1A5, -G1B5, -G1C5, -G1D5, -G1E5, -G1F5, -J4A5, -K1A5, -K1B5, -K1C5, -K1D5, -K1E5, -K1F5, -K1G5, -K1H5, -K1J5, -K1K5, -K2A5, -L1A5, -L1C5, -M1A5, -M1C5, -N1A5, -P1A5, -R1A5, -S1A5, -T4B5, -AA1A5, -AA1B5, -AB1A5, -AC1A5 AEIO-540-D4A5, -D4B5, -D4C5, -D4D5, -L1B5 HIO-540-A1A 1E4 CAR 13 SL1-96 Rev. G Dated:

8/28/2001 N/A 9/11/01 *or later FAA approved revision.

FAA Approved:_____________________________________ T h a d d e u s D . K r o l i c k i , J r .

M a n a g e r , P r o p u l s i o n B r a n c h C h i c a g o A i r c r a f t C e r t i f i c a t i o n O f f i c e

D a t e R e i s s u e d : F e b r u a r y 1 0 , 2 0 0 9 D a t e A m e n d e d : S e p t e m b e r 1 1 , 2 0 0 1

## Every issue (1)

- February 10, 2009: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/01/1f/011f20260eb9cddd79ea9f00be15cb594c9e4228c5393c421f6635d1864a3201), [SE00768CH.AML.pdf](https://openairdocs.org/files/sha256/34/87/348756a86da6b44aff807d754bc7966a472c5c246efec03f004d72b5c926e641)

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