# STC SA04424AT

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Continental Motors, Inc., United States
- Description: Installation of Continental Motors, Inc. (CMI) Shower-of-Sparks  Starting Vibrator Booster Systems
- Applied: August 30, 2017
- Status date: June 4, 2018
- Product: Aircraft, Small Airplane
- Certification basis: Part 3, Part 21, Part 23
- Data sheets: [TCDS A-758](https://openairdocs.org/tcds/A-758), [TCDS A4WE](https://openairdocs.org/tcds/A4WE), [TCDS A17EU](https://openairdocs.org/tcds/A17EU), [TCDS A29EU](https://openairdocs.org/tcds/A29EU), [TCDS A12SO](https://openairdocs.org/tcds/A12SO), [TCDS A47CE](https://openairdocs.org/tcds/A47CE), [TCDS A67EU](https://openairdocs.org/tcds/A67EU), [TCDS A00011LA](https://openairdocs.org/tcds/A00011LA), [TCDS A00001LA](https://openairdocs.org/tcds/A00001LA), [TCDS A2EA](https://openairdocs.org/tcds/A2EA), [TCDS 1A8](https://openairdocs.org/tcds/1A8), [TCDS A2WI](https://openairdocs.org/tcds/A2WI), [TCDS 2A10](https://openairdocs.org/tcds/2A10), [TCDS 2A8](https://openairdocs.org/tcds/2A8), [TCDS 3A23](https://openairdocs.org/tcds/3A23), [TCDS 2A3](https://openairdocs.org/tcds/2A3), [TCDS A7EA](https://openairdocs.org/tcds/A7EA), [TCDS 2A13](https://openairdocs.org/tcds/2A13), [TCDS A3SO](https://openairdocs.org/tcds/A3SO), [TCDS A10SO](https://openairdocs.org/tcds/A10SO) and 4 more
- Certificate PDF: https://openairdocs.org/files/sha256/03/10/0310edb4a380d4378fd493446da98b37f08496d523c57cf4866a1ea5f23a67f1
- Approved model list and other attachments: [SA04424AT_AML.pdf](https://openairdocs.org/files/sha256/6e/60/6e6067e9b10cc777540887338e0a90675b30ed786fca160fc5f2cec265f78903)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/46DAA6B71134791D86258301005582B5.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA04424AT

## ADs that name it (0)

None.

## Approved models (75, first 50)

- Aircraft Parts & Development Corp. A-9 ([TCDS A-758](https://openairdocs.org/tcds/A-758))
- Aircraft Parts & Development Corp. A-9A ([TCDS A4WE](https://openairdocs.org/tcds/A4WE))
- Aircraft Parts & Development Corp. A-9B ([TCDS A-758](https://openairdocs.org/tcds/A-758))
- B-N Group Ltd. BN-2 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-2 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-20 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-21 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-26 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-27 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-6 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-8 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-9 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2B-20 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2B-21 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2B-26 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2B-27 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN2A MK. III ([TCDS A29EU](https://openairdocs.org/tcds/A29EU))
- B-N Group Ltd. BN2A MK. III-2 ([TCDS A29EU](https://openairdocs.org/tcds/A29EU))
- B-N Group Ltd. BN2A MK. III-3 ([TCDS A29EU](https://openairdocs.org/tcds/A29EU))
- Commander Aircraft Corporation 114B ([TCDS A12SO](https://openairdocs.org/tcds/A12SO))
- Commander Aircraft Corporation 114TC ([TCDS A12SO](https://openairdocs.org/tcds/A12SO))
- Diamond Aircraft Industries Inc DA 40 ([TCDS A47CE](https://openairdocs.org/tcds/A47CE))
- Extra Flugzeugproduktions- und Vertriebs- GmbH EA 300/LC ([TCDS A67EU](https://openairdocs.org/tcds/A67EU))
- Extra Flugzeugproduktions- und Vertriebs- GmbH EA-300 ([TCDS A67EU](https://openairdocs.org/tcds/A67EU))
- Extra Flugzeugproduktions- und Vertriebs- GmbH EA-300L ([TCDS A67EU](https://openairdocs.org/tcds/A67EU))
- Extra Flugzeugproduktions- und Vertriebs- GmbH EA-300S ([TCDS A67EU](https://openairdocs.org/tcds/A67EU))
- GA 8 Airvan (Pty) Ltd GA8 ([TCDS A00011LA](https://openairdocs.org/tcds/A00011LA))
- GA 8 Airvan (Pty) Ltd GA8-TC320 ([TCDS A00011LA](https://openairdocs.org/tcds/A00011LA))
- GA200 (Pty) Ltd GA200 ([TCDS A00001LA](https://openairdocs.org/tcds/A00001LA))
- GA200 (Pty) Ltd GA200C ([TCDS A00001LA](https://openairdocs.org/tcds/A00001LA))
- Helio Aircraft LLC 500 ([TCDS A2EA](https://openairdocs.org/tcds/A2EA))
- Helio Aircraft LLC H-250 ([TCDS 1A8](https://openairdocs.org/tcds/1A8))
- Lavia Argentina S.A. (Laviasa) PA-25-235 ([TCDS 2A10](https://openairdocs.org/tcds/2A10))
- Lavia Argentina S.A. (Laviasa) PA-25-235 ([TCDS 2A8](https://openairdocs.org/tcds/2A8))
- Lavia Argentina S.A. (Laviasa) PA-25-260 ([TCDS 2A10](https://openairdocs.org/tcds/2A10))
- Lavia Argentina S.A. (Laviasa) PA-25-260 ([TCDS 2A8](https://openairdocs.org/tcds/2A8))
- Maule Aerospace Technology Inc. M-5-235C ([TCDS 3A23](https://openairdocs.org/tcds/3A23))
- Maule Aerospace Technology Inc. M-6-235 ([TCDS 3A23](https://openairdocs.org/tcds/3A23))
- Maule Aerospace Technology Inc. M-7-235 ([TCDS 3A23](https://openairdocs.org/tcds/3A23))
- Maule Aerospace Technology Inc. M-7-235A ([TCDS 3A23](https://openairdocs.org/tcds/3A23))
- Maule Aerospace Technology Inc. M-7-235B ([TCDS 3A23](https://openairdocs.org/tcds/3A23))
- Maule Aerospace Technology Inc. M-7-235C ([TCDS 3A23](https://openairdocs.org/tcds/3A23))
- Maule Aerospace Technology Inc. M-7-260 ([TCDS 3A23](https://openairdocs.org/tcds/3A23))
- Maule Aerospace Technology Inc. M-7-260C ([TCDS 3A23](https://openairdocs.org/tcds/3A23))
- Maule Aerospace Technology Inc. M-8-235 ([TCDS 3A23](https://openairdocs.org/tcds/3A23))
- Maule Aerospace Technology Inc. M-9-235 ([TCDS 3A23](https://openairdocs.org/tcds/3A23))
- Maule Aerospace Technology Inc. MT-7-235 ([TCDS 3A23](https://openairdocs.org/tcds/3A23))
- Maule Aerospace Technology Inc. MT-7-260 ([TCDS 3A23](https://openairdocs.org/tcds/3A23))
- Maule Aerospace Technology Inc. MX-7-235 ([TCDS 3A23](https://openairdocs.org/tcds/3A23))

All 75: https://openairdocs.org/stc/SA04424AT/models.md

## 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.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate FAA Form 8110-2 (5/14) Page 1 of 1

Number: SA04424AT This certificate issued to: Continental Motors, Inc.

2039 South Broad Street Mobile, AL 36615

Part *of the *Regulations.

Original Product Type Certificate Number: *See attached FAA Approved Model List (AML) No. SA04424AT for a list of approved aircraft models and applicable airworthiness regulations.

Installation of Continental Motors, Inc. (CMI) “Shower-of-Sparks” Starting Vibrator Booster Systems in accordance with FAA Approved Model List (AML) SA04424AT and Service Information Letter (SIL) 671 that provides Installation Instructions for Shower-of-Sparks Starting Vibrator Booster Systems, dated May 31, 2018, or latest FAA approved revision.

See limitation notes on AML SA04424AT. This modification is to be maintained in accordance with the CMI Service Support Manual, Publication X43003, Revision 3, dated May 31, 2018, or later FAA approved revisions. Approval of this change in type design applies only to the models of aircraft listed in AML SA04424AT. This approval should not be extended to aircraft of these models on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effects upon the airworthiness of the aircraft. A copy of this Certificate, AML SA04424AT, and the FAA Form 337, must be maintained as part of the permanent records for the modified aircraft. The installer must determine whether this design is compatible with previously approved modifications. 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: August 30, 2017 Date Reissued:

Date of Issuance: June 04, 2018 Date Amended:

By Direction of the Administrator Signature

Title Christina Underwood, Manager Atlanta Aircraft Certification Office

### SA04424AT_AML.pdf

FAA - Approved Model List (AML) SA04424AT Installation of CMI Shower-of-Sparks Starting Vibrator Booster Systems ISSUE DATE: 6/04/2018

Item

Make

Model/ Series Cert Basis/ Amendment/ Category

TCDS No

MDL/ Inst DWG

FMS

ICA

MFG P/N Model Specific Notes Initial Approve Date

Amended Date

Aircraft Parts & Development Corp.

A-9 A-9B

CAR 8/ None/ Restricted

A-758 Rev 23 10-400395, Rev A, dated 9/26/2017 or latest FAA approved revision

N/A X43003, Rev 3, dated 5/31/2018 or the latest FAA approved revision A-9 12V:

10-176487-121 A-9 24V:

10-357487-241 A-9B 12V:

10-176487-122 A-9B 24V:

10-357487-242

N/A

6/04/2018

N/A

Aircraft Parts & Development Corp.

A-9A CAR 3 effective 5/15/ 56, with amendments 3-1 through 3-

7./ Normal

A4WE Rev 6 10-400395, Rev A, dated 9/26/2017 or latest FAA approved revision

N/A X43003, Rev 3, dated 5/31/2018 or the latest FAA approved revision

A-9A 12V:

10-176487-121 A-9A 24V:

10-357487-241

N/A

6/04/2018

N/A

B-N Group LTD BN-2 BN-2A BN-2A-6 BN-2A-8 BN-2A-2 BN-2A-9 BN-2A-3 BN-2A-20 BN-2A-21 BN-2A-26 BN-2A-27 BN-2B-20 BN-2B-21 BN-2B-26 BN-2B-27

14 CFR Part 23, effective February 1, 1965 including amendment 23-1 …/ Normal

A17EU Rev 18 10-400395, Rev A, dated 9/26/2017 or latest FAA approved revision

N/A X43003, Rev 3, dated 5/31/2018 or the latest FAA approved revision

12V:

10-176487-122 24V:

10-357487-242

N/A

6/04/2018

N/A

B-N Group LTD

BN-2A MK.

**III BN-2A MK.**

**III-2 BN-2A MK.**

III-3 14 CFR Part 23 effective February 1, 1965 as amended by amendments 23-1 through 23-9 inclusive / Normal

A29EU Rev 5 10-400395, Rev A, dated 9/26/2017 or latest FAA approved revision

N/A X43003, Rev 3, dated 5/31/2018 or the latest FAA approved revision

12V:

10-176487-122 24V:

10-357487-242

N/A

6/04/2018

N/A

Item

Make

Model/ Series Cert Basis/ Amendment/ Category

TCDS No

MDL/ Inst DWG

FMS

ICA

MFG P/N Model Specific Notes Initial Approve Date

Amended Date

Textron Aviation Inc.

(Cessna)

182S, 182T, T182T 14 CFR Part 23 … as amended … through 23-6, except as follows:

FAR23.611 as amended by Amendment

**23-7. FAR**

23.1301 as amended by Amendment

23-20.

23.1357 as amended by Amendment

23-43. /Normal

3A13 Rev 72 10-400395, Rev A, dated 9/26/2017 or latest FAA approved revision

N/A X43003, Rev 3, dated 5/31/2018 or the latest FAA approved revision

182S, 182T:

10-357487-241 T182T:

10-357487-242

N/A

6/04/2018

N/A

Item

Make

Model/ Series Cert Basis/ Amendment/ Category

TCDS No

MDL/ Inst DWG

FMS

ICA

MFG P/N Model Specific Notes Initial Approve Date

Amended Date

Textron Aviation Inc.

(Cessna)

206H, T206H 14 CFR Part 23 … as amended … through 23-6, except as follows:

FAR 23.611 as amended by Amendment

**23-7. FAR**

23.607… as amended by Amendment

**23-17. FAR**

23.1301 as amended by Amendment

23-20.

FAR 23.1357 as amended by Amendment

23-43. /Normal

A4CE Rev 49 10-400395, Rev A, dated 9/26/2017 or latest FAA approved revision

N/A X43003, Rev 3, dated 5/31/2018 or the latest FAA approved revision

206H:

10-357487- 241 T206H:

10-357487- 242

N/A

6/04/2018

N/A

Commander Aircraft Corporation

114B, 114TC

14 CFR Part 23/ through amendment 23-7 /Normal

A12SO Rev 23 10-400395, Rev A, dated 9/26/2017 or latest FAA approved revision

N/A X43003, Rev 3, dated 5/31/2018 or the latest FAA approved revision 114B 12V:

10-176487- 121 114B 24V:

10-357487- 241 114TC 24V:

10-357487- 242

N/A

6/04/2018

N/A

8 Extra Flugzeugpro duktions und Vertreibs GmbH

EA 300, EA 300/S, EA 300/L, EA 300/L C 14 CFR Part 23/ through amendment 23-34 / Acrobatic, Normal

A67EU Rev 12 10-400395, Rev A, dated 9/26/2017 or latest FAA approved revision

N/A X43003, Rev 3, dated 5/31/2018 or the latest FAA approved revision

12V:

10-176487- 121 24V:

10-357487- 241

N/A

6/04/2018

N/A

Diamond Aircraft Industries GmbH

DA 40 14 CFR Part 23 effective February 1, 1965, including Amendments 23-1 through Amendment 23-51/ Normal and Utility

A47CE Rev 15 10-400395, Rev A, dated 9/26/2017 or latest FAA approved revision

N/A X43003, Rev 3, dated 5/31/2018 or the latest FAA approved revision

10-357487- 241

N/A

6/04/2018

N/A

Item

Make

Model/ Series Cert Basis/ Amendment/ Category

TCDS No

MDL/ Inst DWG

FMS

ICA

MFG P/N Model Specific Notes Initial Approve Date

Amended Date

Found Aircraft, Canada, Inc

FBA-2C, FBA-2C1, FBA-2C2, FBA-2C3, FBA-2C4, FBA-2C3T, FBA-2C4T FBA-2C:

14 CFR Part 23 … as amended … through 23-6 except:

FAR 23.611;

amended by amendment 23-7.

FAR 23.1529 amended by amendment 23-26.

FAR 23.1351;

23.1357; amended by amendment 23-

43.

FBA-2C1:

14 CFR Part 23 … through 23-6 except:

FAR 23.611;

amended by amendment 23-7.

FAR 23.607;

amended by amendment 23-17.

FAR 23.1301 amended by amendment 23-20.

FAR 23.1529 amended by amendment 23-26.

FAR 23.1351;

amended by amendment 23-43.

FBA-2C2 The Certification Basis for the model FBA-2C1, except:

FAR 23.1365;

amended by amendment 23-43.

FBA-2C3, FBA 2C4, FBA-2C3T, FBA-2C4T 14 CFR Part 23 … through 23-6 except:

23.1301, As amended by Amendment 23-20

23.605 As amended by Amendment 23-23

23.1529 As amended by Amendment 23-26

23.1357, As amended by Amendment 23-43

23.607, 23.611, As amended by Amendment 23-48

23.1351 As amended by Amendment 23- 49/Normal

A7EA Rev 8 10-400395, Rev A, dated 9/26/2017 or latest FAA approved revision

N/A X43003, Rev 3, dated 5/31/2018 or the latest FAA approved revision

12V, S- 200:

10-176487- 121 12V, S- 1200:

10-176487- 122 24V, S- 200:

10-357487- 241 24V, S- 1200:

10-357487- 242

N/A

6/04/2018

N/A

GA8 Airvan

GA8, GA8-TC 320 GA8:

14 CFR Part 23 … through 23-54 GA8TC320 FAR 23, dated December 18, 1964…through 23-55 /Normal

A00011 LA Rev 10 10-400395, Rev A, dated 9/26/2017 or latest FAA approved revision

N/A X43003, Rev 3, dated 5/31/2018 or the latest FAA approved revision

12V:

10-176487- 122 24V:

10-357487- 242

N/A

6/04/2018

N/A

Item

Make

Model/ Series Cert Basis/ Amendment/ Category

TCDS No

MDL/ Inst DWG

FMS

ICA

MFG P/N Model Specific Notes Initial Approve Date

Amended Date

GA200

GA200 GA200C 14 CFR Part 23 … through 23-36 Except: 23.562 (see letter dated April 5, 1995, from Manager, LAACO) for the special purpose of:

(1) Agricultural operations under FAR

21.25 (b)(1)./ Restricted

A00001 LA Rev 3 10-400395, Rev A, dated 9/26/2017 or latest FAA approved revision

N/A X43003, Rev 3, dated 5/31/2018 or the latest FAA approved revision

12V, S-200:

10-176487- 121 12V, S-1200:

10-176487- 122 24V, S-200:

10-357487- 241 24V, S-1200:

10-357487- 242

N/A

6/04/2018

N/A

Helio

H-250

CAR 3/ as amended to May 16, 1953 / Normal

1A8 Rev 37 10-400395, Rev A, dated 9/26/2017 or latest FAA approved revision

N/A X43003, Rev 3, dated 5/31/2018 or the latest FAA approved revision

12V:

10-176487- 121 24V:

10-357487- 241

N/A

6/04/2018

N/A

Helio

500 CAR 3, dated May 15, 1956, plus Amendments 3-1 through 3- 5/ Normal

A2EA Rev 10 10-400395, Rev A, dated 9/26/2017 or latest FAA approved revision

N/A X43003, Rev 3, dated 5/31/2018 or the latest FAA approved revision

12V:

10-176487- 121 24V:

10-357487- 241

N/A

6/04/2018

N/A

Lavia Argentina S. A.

PA-25-235 PA-25-260

CAR 8.10(b), effective October 11, 1950.

/Restricted

2A10 Rev 28 10-400395, Rev A, dated 9/26/2017 or latest FAA approved revision

N/A X43003, Rev 3, dated 5/31/2018 or the latest FAA approved revision

12V, S-200:

10-176487- 121 12V, S-1200:

10-176487- 122 24V, S-200:

10-357487- 241 24V, S-1200:

10-357487- 242

N/A

6/04/2018

N/A

Item

Make

Model/ Series Cert Basis/ Amendment/ Category

TCDS No

MDL/ Inst DWG

FMS

ICA

MFG P/N Model Specific Notes Initial Approve Date

Amended Date

Lavia Argentina S. A.

PA-25-235 PA-25-260 CAR 3 effective May 15, 1956, Amendment 3- 1, April 1, 1957.

/Normal

2A8 Rev 22 10-400395, Rev A, dated 9/26/2017 or latest FAA approved revision

N/A X43003, Rev 3, dated 5/31/2018 or the latest FAA approved revision 12V, S-200:

10-176487- 121 12V, S-1200:

10-176487- 122 24V, S-200:

10-357487- 241 24V, S-1200:

10-357487- 242

N/A

6/04/2018

N/A

Maule Aerospace Technology, Inc.

M-5-235C M-6-235 M-7-235 M-7-235A M-7-235B M-7-235C M-7-260 M-7-260C MT-7-235 MT-7-260 MX-7-235 M-8-235 M-9-235

Part 3, Civil Air Regulations, effective May 15, 1956 as amended by 3- 1 thru 3-5 and

3.705 as amended by 3- 7 /Normal

3A23 Rev 32 10-400395, Rev A, dated 9/26/2017 or latest FAA approved revision

N/A X43003, Rev 3, dated 5/31/2018 or the latest FAA approved revision

12V:

10-176487- 121 24V:

10-357487- 241

N/A

6/04/2018

N/A

Item

Make

Model/ Series Cert Basis/ Amendment/ Category

TCDS No

MDL/ Inst DWG

FMS

ICA

MFG P/N Model Specific Notes Initial Approve Date

Amended Date

Mooney International Corporation

M20M CAR 3 effective November 1, 1949, as amended to May 18, 1954, … 3.74 as amended to August 25, 1955; …3.109,

3.112, 3.115,

3.118, 3.120, and 3.441 of CAR 3 effective May 15, 1956, as amended to October 1, 1959. In lieu of corresponding CAR 3 paragraphs, where applicable - FAR 23, effective February 1, 1965; 23.1351 as amended to September 14, 1969 / Normal

2A3 Rev 57 10-400395, Rev A, dated 9/26/2017 or latest FAA approved revision

N/A X43003, Rev 3, dated 5/31/2018 or the latest FAA approved revision

10-357487-242

N/A

6/04/2018

N/A

Piper

PA-28-235 CAR 3 effective May 15, 1956, … 3- 2; … 3.304 and 3.705 of Amendment 3- 7 effective May 3, 1962./ Normal

2A13 Rev 57 10-400395, Rev A, dated 9/26/2017 or latest FAA approved revision

N/A X43003, Rev 3, dated 5/31/2018 or the latest FAA approved revision

12V:

10-176487-121 24V:

10-357487-241

N/A

6/04/2018

N/A

Item

Make

Model/ Series Cert Basis/ Amendment/ Category

TCDS No

MDL/ Inst DWG

FMS

ICA

MFG P/N Model Specific Notes Initial Approve Date

Amended Date

Piper

PA-32-260 PA-32-300 PA-32S- 300 PA-32R- 301 PA-32-301 PA-32R- 301T PA-32- 301FT PA-32R- 301FT PA-32- 301XTC PA-32-260, PA-32S-300, PA-32-300, PA-32R-301 PA-32-301 PA-32R-301T CAR 3, effective May 15, 1956, through Amendment 3- 8, effective December 18, 1962.

PA-32-301FT, PA-32- 301XTC CAR 3, effective May 15, 1956, through Amendment 3- 8, effective December 18, 1962. FAR

23.1529 as amended by Amendment 23-26, effective October 14, 1980/ Normal

A3SO Rev 33 10-400395, Rev A, dated 9/26/2017 or latest FAA approved revision

N/A X43003, Rev 3, dated 5/31/2018 or the latest FAA approved revision

12V, S-200:

10-176487- 121 12V, S- 1200:

10-176487- 122 24V, S-200:

10-357487- 241 24V, S- 1200:

10-357487- 242

N/A

6/04/2018

N/A

Piper

PA-36-300 14 CFR Part 23 including Amendments 23-1 through 23-6 dated August 1, 1967/ Normal

A9SO Rev 10 10-400395, Rev A, dated 9/26/2017 or latest FAA approved revision

N/A X43003, Rev 3, dated 5/31/2018 or the latest FAA approved revision

12V:

10-176487- 122 24V:

10-357487- 242

N/A

6/04/2018

N/A

Piper

PA-36-300 14 CFR Part 23 including Amendments 23-1 through 23-6 dated August 1, 1967, with exception to FAR 23 per FAR

21.25(a)(1)./ Restricted

A10SO Rev 13 10-400395, Rev A, dated 9/26/2017 or latest FAA approved revision

N/A X43003, Rev 3, dated 5/31/2018 or the latest FAA approved revision

12V:

10-176487- 122 24V:

10-357487- 242

N/A

6/04/2018

N/A

Item

Make

Model/ Series Cert Basis/ Amendment/ Category

TCDS No

MDL/ Inst DWG

FMS

ICA

MFG P/N Model Specific Notes Initial Approve Date

Amended Date

The King’s Engineering Fellowship

14 CFR Part 23/ through amendment 23-36/Normal

A2WI Rev 3 10-400395, Rev A, dated 9/26/2017 or latest FAA approved revision

N/A X43003, Rev 3, dated 5/31/2018 or the latest FAA approved revision

12V:

10-176487- 122 24V:

10-357487- 242

N/A

6/04/2018

N/A

Twin Commander

CAR 3 as amended May 15, 1956/ Normal

6A1 Rev 48 10-400395, Rev A, dated 9/26/2017 or latest FAA approved revision

N/A X43003, Rev 3, dated 5/31/2018 or the latest FAA approved revision

12V:

10-176487- 121 24V:

10-357487- 241

N/A

6/04/2018

N/A

FAA - Approved Model List (AML) SA04424AT Installation of CMI Shower-of-Sparks Starting Vibrator Booster Systems ISSUE DATE: 6/04/2018

NOTES AND LIMITATIONS:

1. Installation is to be accomplished in accordance with Service Information Letter (SIL) 671, dated May 31, 2018, or later FAA approved revisions. Instructions are written to install Shower-of-Sparks in aircraft equipped with rotary action combined ignition/starter switches, or pushbutton 4PST start switches and separate magneto switch(es) along with a dedicated starter solenoid.

2. In conjunction with installation of CMI Shower-of-Sparks starting vibrator kit in the aircraft, the engine(s) must also be retrofitted to the CMI Shower-of-Sparks magneto configuration, consisting of PMA eligible CMI S-200 and S-1200 series magnetos and matching harnesses.

3. CMI Ignition Application Data, Publication X44001, Revision 5, dated May 15, 2017, or later FAA approved revisions, provide a list of engine models and applicable PMA eligible CMI S-200 and S-1200 series magnetos and matching harnesses.

F A A A p p r o v e d :________________________________________ Christina Underwood, Manager Atlanta Aircraft Certification Office

## Every issue (1)

- June 4, 2018: Issued, Current. [certificate](https://openairdocs.org/files/sha256/03/10/0310edb4a380d4378fd493446da98b37f08496d523c57cf4866a1ea5f23a67f1), [SA04424AT_AML.pdf](https://openairdocs.org/files/sha256/6e/60/6e6067e9b10cc777540887338e0a90675b30ed786fca160fc5f2cec265f78903)

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