STC SR03531NY

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

Part of the

Signature

Title SR03531NY Aerospace Design Facilities Ltd.

Taymount, 4A Wood End Close SL2 3RF Farnham Common United Kingdom Federal Aviation Regulations.

1. Installation of Spectrolab SX7 Searchlight in accordance with Aerospace Design Facilities Ltd. Master Document List ADF- MDL2013-100 Issue 1A dated March 11, 2014, or later EASA-approved revision.

2. Aircraft is to be maintained in accordance with Aerospace Design Facilities Ltd. Instructions for Continued Airworthiness ADF- ICA2013-100 Issue 2 dated February 26, 2015, or later EASA-accepted revision.

3. The rotorcraft must be operated in accordance with Aerospace Design Facilities Ltd. AS355 Flight Manual Supplement No. 12, Issue 1, Revision 0, dated March 14, 2014, or later EASA-approved revision.

1. The "Limitation" section of Aerospace Design Facilities Ltd. AS355 Flight Manual Supplement No. 12, Issue 1, Revision 0, EASA approved on March 14, 2014 is applicable as part of this installation.

2. Operation of the searchlight is prohibited with emergency flotation system installed.

3. Operation of the searchlight is prohibited with landing gear "Bear Foot" settling protectors.

4. Operation of the searchlight is prohibited with the cargo swing attached.

(See Limitations and Conditions continued on sheet 3) Gaetano Sciortino Manager New York Aircraft Certification Office Airbus Helicopters AS355F, AS355F1, AS355F2, AS355N, AS355NP August 25, 2014 May 15, 2015 IMPORT H11EU 3

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

To (Name and address of transferee)

From (Name and address of grantor)

3 SR03531NY

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

3 Date of Issuance: May 15, 2015

Limitations and Conditions, continued:

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 the certificate to alter the 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 FAA Order 8110.48, the certification basis for the Airbus AS355 rotorcraft models identified herein is as follows:

a. The certification basis for the Airbus AS355 rotorcraft models identified herein is shown on Type Certificate Data Sheet H11EU 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 H11EU, except as follows:

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

27.1(a)(b)(c), 27.601(a)(b), 27.603(a)(b)(c), 27.605(a)(b), 27.607(a)(b), 27.609(a)(b), 27.610(a)(b)(c)(d), 27.611(a)

(b)(c), 27.613(a)(b)(c)(d)(e), 27.625(a)(b)(c)(d), 27.629, 27.771(a)(b)(c), 27.777(a)(b), 27.1301(a)(b)(c)(d),

27.1309(a)(b)(c)(d), 27.1321(a)(b)(c)(d), 27.1322(a)(b)(c)(d), 27.1327(a)(b), 27.1351(a)(b)(c)(d)(e), 27.1365(a)(b)

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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SR03531NY