STC SE03495NY

FAA Form 8110-2 (8/13) Page 1

Car of the Civil Air Regulations.

Original Product – Type Certificate Number: MDNH:

MRGHO:

Signature

Title

IMPORT SE03495NY Helicopteres Guimbal S.A.

Aerodrome d’Aix-en-Provence 13290 Les Milles, France 13 E-286 Lycoming Engines O-360-J2A Installation of an electronic ignition system, an air conditioning compressor, and an oil filter adapter in accordance with Helicopteres Guimbal document “Installation, Operator’s and Maintenance Manual,” Doc. No. P/N J45-001, Issue 04, dated October 2, 2014 or later EASA approved revisions, and Type Design Definition “O360-J2A Plasma STC Parts List” Doc. No.

J45-002, Revision F, dated December 31, 2012 or later EASA approved revisions.

(See Description of Type Design Change continued on Page 3 of 3)

1. The ignition system control unit must not be installed in a dedicated engine fire zone. The installation conditions and assumptions are defined in the Installation Manual that is specified above.

2. This STC is exclusive of any rotorcraft or aircraft installation. A separate FAA certification is required for installation of the engine with this modification into any rotorcraft or aircraft.

(See Limitations and Conditions continued on Page 3 of 3) January 21, 2013

January 14, 2015

Gaetano Sciortino Manager New York Aircraft Certification Office

FAA Form 8110-2 (8/13) Page 2

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

SE03495NY

FAA Form 8110-2 (8/13) Page 3

SE03495NY Date Issued: January 14, 2014

Description of Type Design Change (continued):

The following Helicopteres Guimbal instructions for operation, maintenance, and inspection document is required with this installation: Helicopteres Guimbal document “Installation, Operator’s and Maintenance Manual,” Doc. No. P/N J45-001, Issue 04, dated October 2, 2014 or later EASA approved revisions.

3. The data in the TCDS E-286 remains valid except for the following:

Dimensions:

Overall height: 602 mm (23.7 in.)

Fuels:

- Aviation gasoline, 100 or 100LL per ASTM D910, B95/130 CIS or RH95/130.

- Unleaded fuel with a minimum octane rating of 98 as outlined in Doc. No. P/N J45-001, Issue 04, dated October 2, 2014, Section 2, or later EASA approved revisions.

Environmental Conditions:

Refer to Helicopteres Guimbal document “Installation, Operator’s and Maintenance Manual,” Doc. No. P/N J45-001, Issue 04, dated October 2, 2014, Section 7, or later EASA approved revisions.

4. Mandatory replacement time and/or inspection intervals are defined in the FAA Approved “Airworthiness Limitation” section of the Helicopteres Guimbal document “Installation, Operator’s and Maintenance Manual,” Doc. No. P/N J45-001, Issue 04, dated October 2, 2014.

5. The Installer must determine whether this design change is compatible with previously approved modifications.

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

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for changes that are not significant in FAA Order 8110.48, the certification basis for this modification are as follows:

• The type certification basis for the Lycoming Engines O-360-J2A engine is shown on TCDS No. E-286 for parts not changed or not affected by the change.

• The type certification basis for the Lycoming Engines O-360-J2A engine is shown on TCDS No. E-286 for parts changed or affected by the change with the following CFR 14 exceptions:

Regulations at the amendment 33-0 through 33-22:

33.1 33.3 33.4 33.5 33.7 33.8

33.11 33.15 33.17 33.19 33.21 33.23

33.25 33.27 33.28 33.29 33.31 33.33

33.34 33.35 33.37 33.39 33.42 33.43

33.45 33.47 33.49 33.51 33.53 33.55

33.57

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