STC SA0039BO

Number SA00339BO

FAA Form 8110-2 (8/13) Page 1 of 3 This certificate issued to:

Metro Aviation, Inc.

1214 Hawn Avenue Shreveport, LA 71107 Part 27 of the Federal Aviation Regulations.

Original Product - Type Certificate Number: H88EU Make: Eurocopter Deutschland GmbH Model: EC135P2+

Installation of Single pilot IFR KIT135M-GTN-150 with Garmin GTN 650-750 WAAS Navigators in accordance with Metro Aviation, Inc. Master Document List (MDL), MDL135M-GTN-150, Rev D, dated January 17, 2014, or later FAA approved revision.

1. Operation must be in accordance with Metro Aviation Rotorcraft Flight Manual Supplement (RFMS) FMS135M-GTN-001, Rev -, FAA approved on February 21, 2014, or later FAA approved revision.

The RFMS must be carried in the aircraft during all flights.

(continued on Page 3 of 3)

Date of Application: April 5, 2013 Date reissued:

Date of Issuance: February 21, 2014 Date amended:

Signature Robert G. Mann

Manager, Boston Aircraft Certification Office Title

SUPPLEMENTAL TYPE CERTIFICATE, FAA FORM 8110-2 (CONTINUED)

FAA Form 8110-2 (8/13) Page 2 of 3

TRANSFER

ENDORSEMENT

To (Name of transferee)

(Address of transferee)

(Number and street)

(City, State, and ZIP Code)

From (Name of grantor)

(Address of grantor)

(Number and street)

(City, State, and ZIP Code)

Number SA00339BO February 21, 2014

FAA Form 8110-2 (8/13) Page 3 of 3 Limitations and Conditions: (continued from Page 1 of 3)

2. Maintenance must be in accordance with Metro Aviation, Inc. Instructions for Continued Airworthiness (ICA), EMM135M-GTN-001, Rev -, dated September 17, 2013, or later FAA accepted revision. The ICA must be made available to the operator at the time of installation.

3. Compatibility of this design with previously approved modifications must be determined by the installer.

Certification Basis:

Based on 14 CFR § 21.115 and § 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48, the certification basis for the Eurocopter Deutschland GmbH Model EC135P2+ aircraft is as follows:

a. The type certification basis for parts not changed or not affected by the change is shown on TCDS H88EU.

b. The modification certification basis for parts changed or affected by the change since the reference application date, April 5, 2013, is based upon part 27 as amended by Amendment 27-47 as follows:

Regulations at the latest amendment 27-0 through 27-47

27.21, 27.29, 27.251, 27.301, 27.303, 27.305(a), 27.307(a), 27.601(a), 27.603, 27.605(a),

27.607, 27.609(a), 27.611, 27.613(a)(b)(c)(d), 27.619, 27.771(a), 27.773(a)(1)(b), 27.775,

27.777(a), 27.787(b)(c), 27.1301, 27.1303, 27.1307(d)(e), 27.1321(a)(c)(d), 27.1322,

27.1323, 27.1325, 27.1327, 27.1351(a)(b)(1)(c)(d)(e), 27.1353(a)(b), 27.1357(a)(b)(c)(d),

27.1367, 27.1381, 27.1501, 27.1523, 27.1525, 27.1527, 27.1529, 27.1541, 27.1543, 27.1545,

27.1547, 27.1555(a), 27.1559, 27.1581, 27.1583(c)(e), 27.1585(a), 27.1589, 27A.1, 27A.2, 27A.3, 27A.4, 27B.8, 27B.9 Regulations at an intermediate amendment None Regulations at the amendment level in TCDS H88EU

27.1, 27.2, 27.561(a)(b)(3)(c), 27.610, 27.625(a)(c), 27.853(a), 27.1309, 27.1329(e), 27.1365 ------------------------------------------------------------END-------------------------------------------------------