STC SR03694AT

This certificate issued to

Part 29 of the Federal Aviation Regulations.

Description of Type Design Change: Installation of an Avalex Technologies Digital Moving Map in accordance with Avalex Technologies Master Drawing List (MDL) No. AMS7102-145-MDL, Rev. B, Dated November 25, 2008, or later FAA approved revision.

Limitations and Conditions: This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. 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. FAA Approved Rotorcraft Flight Manual Supplement for Eurocopter Deautschland BK117 C-2 Rotorcraft, Rev. IR, dated May 1, 2009, or later FAA approved revision is a required part of this STC

Avalex Technologies Corporation 115-A Gregory Square Pensacola, FL 32502 H13EU Make : EUROCOPTER DEUTSCHLAND GMBH (ECD) Model: MBB-BK 117 C-2 Date reissued :

( Signature)

Melvin D. Taylor Manager Atlanta Aircraft Certification Office

( Title) Date of application : October 4, 2007

Date of issuance : May 1, 2009

FAA FORM 8110-2-1(10-69) PAGE 2 of 2 PAGES

Number SR03694AT

Instructions for Continued Airworthiness (ICA), Avalex Technologies, Corporation Document No. # BR- 08004, Rev IR, dated May 20, 2008, or later FAA accepted revision must be made available to the operator at the time of installation.

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Eurocopter Deutschland GMBH (ECD) MBB-BK 117 C-2 rotorcraft is as follows:

a. The type certification basis for Eurocopter Deutschland GMBH (ECD) MBB-BK 117 C-2 rotorcraft is shown on TCDS H13EU for parts not changed or not affected by the change.

b. The certification basis for parts changed or aff ected by the change since the reference date of application, October 4, 2007, is based upon part 29 as amended by Amendment 29-47. Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification were determined to be:

Regulations at the latest amendment 29-0 through 29-47 §§ 29.301 §§ 29.601 §§ 29.613 §§ 29.1353 §§ 29.303 §§ 29.603 §§ 29.773 §§ 29.1357 §§ 29.305 §§ 29.605 §§ 29.803 §§ 29.1381 §§ 29.307 §§ 29.607 §§ 29.1301 §§ 29.1431 §§ 29.337 §§ 29.609 §§ 29.1309 §§ 29.1529 §§ 29.561 §§ 29.610 §§ 29.1351 §§ 29.1581

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