STC SR00154IB

IMPORT SR00154IB

SAFRAN AEROSYSTEMS 61 RUE PIERRE CURIE 78370 PLAISIR FRANCE Part 27 Title 14 Code of Federal Regulations H9EU Airbus Helicopters EC130B4, EC130T2

1. Installation of Quick Removal System for Airbus Helicopters (AH) Emergency Floatation System (EFS) must be in accordance with Safran Aerosystems Installation Procedures listed in Aircraft Maintenance Manual Supplement Doc. No. ILS-000235, Issue 5.0, dated July 20, 2023, or later EASA approved revisions.

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

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

(See Limitations and Conditions Continued on Page 3 of 3) June 26, 2023 November 15, 2023 Anthony E. Gallo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 3

IMPORT SR00154IB 3

IMPORT SR00154IB Date of Issuance: November 15, 2023

Description of Type Design Change (continued):

2. Aircraft is to be maintained in accordance with Aircraft Maintenance Manual Supplement Doc. No. ILS-000235, Issue 5.0, dated July 20, 2023, or later EASA accepted revisions.

2. If the holder agrees to permit another person to use the certificate to alter the product, the holder shall give the other person written evidence of that permission.

3. This STC can be applied to AH EFS configuration (P/N 704A42690054 for LHS and P/N 704A42690053 for RHS).

Certification Basis:

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

a) The type certification basis for the Airbus Helicopters model EC130B4 and EC130T2 rotorcraft is as shown on TCDS H9EU for parts not changed or not affected by the change.

----------END---------- 3 3