STC SR03635NY

FAA Form 8110-2 (5/14) Page 1 of

Part of the

Signature

Title SR03635NY International Services Electronique Informatique 1030 Avenue JR Guillibert Gauthier de la Lauzière 13290 Aix-en-Provence France Federal Aviation Regulations.

27 Installation of flight data monitoring and transmitting system in two configurations:

1. Configuration 1 is for the Safetyplane system in accordance with ISEI Installation Document N6-AS350 B BA BB B1 B2, E- A-02, dated February 02, 2010, or later EASA-approved revision.

2. Configuration 2 is for the Helicom V2 ANA or Helicom V2+ ANA system in accordance with ISEI Master Drawing List N9-AS 350 B BA BB B1 B2, E-A-01, dated January 14, 2015, or later EASA-approved revision.

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

1. Airbus Helicopters model AS350BB is not type certificated by the FAA and therefore is outside the scope of this approval.

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

3. 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.

Raymond Reinhardt Acting Manager New York Aircraft Certification Office Airbus Helicopters AS350B, AS350BA, AS350B1, AS350B2 February 23, 2015 December 12, 2015 IMPORT H9EU 3

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee)

From (Name and address of grantor)

3 SR03635NY

FAA Form 8110-2 (5/14) Page 3 of

3 Date of Issuance: December 12, 2015

Description of Type Design Change (continued):

3. For both configurations, rotorcraft is to be maintained in accordance with ISEI Instructions for Continued Airworthiness N7-AS350 B BA BB B1 B2-ICA-E-C-05, Revision 11, dated October 15, 2015, or later EASA- accepted revision.

4. For both configurations, rotorcraft is to be operated in accordance with ISEI Rotorcraft Flight Manual Supplement N8-AS350 B BA BB B1 B2-E-C-03, Revision 05, dated January 21, 2015, or later EASA-approved revision.

Certification Basis:

Based on 14 CFR 21.115 and 21.101, and FAA Order 8110.48, the certification basis for the Airbus AS350 rotorcraft models identified herein is as follows:

a. The certification basis for the Airbus AS350 rotorcraft models identified herein is shown on Type Certificate Data Sheet H9EU for parts not changed or not affected by this change.

b. The certification basis for parts changed or affected by this change is as shown on Type Certificate Data Sheet H9EU, except as follows:

Regulations at the latest Amendment 27-1 through 27-47:

27.25, 27.27, 27.301, 27.303, 27.305, 27.307, 27.561, 27.607, 27.609, 27.610, 27.771, 27.773, 27.777, 27.1301,

27.1309, 27.1322, 27.1323, 27.1325, 27.1351, 27.1353, 27.1357, 27.1365, 27.1501, 27.1529, 27.1581

The requirements for environmental protection and the associated certified noise and/or emissions levels of the original product are unchanged and remain applicable to this certificate.

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