STC SR02592NY-D

This certificate issued to

Part 27 of the Federal Aviation R egulations.

Original Product -- Type Certificate N umber :

Installation of Aspen Avionics EFD1000H Pro PFD in accordance with Keystone Helicopter Installation drawing List IDL02209 Rev. B dated 02/08/2010 or later FAA approved revision.

1. Keystone Helicopter Instructions for Continued Airworthiness, Aspen Avionics EFD1000H PRO PFD with GPS Enabled Remote Sensor Module Installation, Report No. IC02209 Rev. - dated December 1, 2009 or later FAA accepted revision is required for this modification.

2. FAA Approved Rotorcraft Flight Manual Supplement, Supplement No. FM02209 Rev. - dated 02/12/2010 or later FAA approved revision is required for this modification.

This certificate and the supporting data whic h is the basis for approval shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the A dministrator of the F ederal A viation A dministration.

Aspen Avionics, Inc.

5001 Indian School Road N.E.

Albuquerque, NM 87110

H2SW M ake: Bell

M odel : 206 Series Date of application : October 22, 2009

Date of issuance: February 12, 2010 Date reissued : October 1, 2011, January 29, 2013, February 5, 2013 Date amended :

B y direction of the A dministrator

(Signature) Gaetano Sciortino Manager New York Aircraft Certification Office

(Title)

FAA Form 8110-2-1(10-69) Page 2 of 2

N umber SR02592NY-D Date reissued: February 5, 2013

Limitations and C onditions (Con’t.):

3. This approval should not be incorporated in any aircraft of this specific model on which other approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those previously incorporated approved modification will not introduce any adverse effect upon the airworthiness of the aircraft.

4. 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.

Certification B asis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certific ation basis for the Bell 206 Series is as follows:

1. The type certification basis for Bell 206 Series is shown on TCDS H2SW for parts not changed or not affected by the change.

2. The certification basis for parts changed or affected by the change since the reference date of application is based upon Part 27 as amended by Amendment 27-44. 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 was determined to be:

Regulations at the latest amendment 27-0 through 27-44

27.301, 27.303, 27.305(a), 27.307(a), 27.337, 27.341, 27.601, 27.603, 27.607, 27.609, 27.613(a)(b)(d), 27.771(a)(c), 27.773(a )(1)(b),

27.777, 27.853(a), 27.1301, 27.1303, 27.1307(d)(e), 27.1309(a)(b), 27.1321(a)(c)(d), 27.1322(b), 27.1323, 27.1327(a),

27.1351(a)(b)(1)(i), 27.1357(a)(b)(c)(d), 27.1365, 27.1367(a)(b)(c), 27.1381, 27.1501, 27.1525, 27.1529, 27.1541, 27.1543(b),

27.1545, 27.1559, 27.1581(a)(b)(d), 27.1583(e), 27.1585(a)

Regulations at an intermediate amendment N/A

Regulations at the amendment level in TCDS H2SW

27.561(a)(b)(3)(c), 27.1309, 27.1545

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