STC SR09559RC

United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate Number: SR09559RC REB Technologies, Inc. This certificate issued to:

1500 Brown Trail Bedford, TX 76022 Part 27 of the Federal Aviation Regulations.

Original Product Type Certificate Number: H88EU Make: Airbus Helicopters Deutschland GmbH (AHD)

Model: EC135P1, EC135T1, EC135P2+, Description of Type Design Change: EC135T2+, EC135P3, EC135T3 Installation of Night Vision Imaging System (NVIS) / Night Vision Goggle (NVG) Compatible Lighting System in accordance with REB Technologies, Inc., Master Drawing List (MDL) Document No.

98020135MDL, Rev. AD, dated March 29, 2022, or later Federal Aviation Administration (FAA) approved revision.

Installation of NVIS/NVG Compatible Lighting System does not include or imply approval for flight operations with NVGs.

Date of Application: August 15, 2008 Date Reissued: December 30, 2009; February 17, 2016 Date of Issuance: November 17, 2009 Date Amended: March 21, 2011; April 3, 2012; April 7, 2022

S. Frances Cox Acting Manager, Fort Worth ACO Branch, Compliance & Airworthiness Division Aircraft Certification Service

United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate Page 2 of 4 FAA Form 8110-2 (03/21)

Number: SR09559RC

United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate Page 3 of 4 FAA Form 8110-2 (03/21)

(Continuation Sheet) Number: SR09559RC Date of Issuance: November 17, 2009 Date Amended: April 7, 2022 Date of Reissuance: February 17, 2016

Description of Type Design Change (continued):

Rotorcraft Flight Manual Supplement (RFMS), REB Technologies, Inc. Document No.

98020135-RFMS, Rev. F, dated April 7, 2022 or later FAA approved revision is required. Instructions for Continued Airworthiness (ICA), REB Technologies, Inc.

Document No. 98020135-ICA, Rev. G, dated September 15, 2021 or later FAA accepted revision is required for this installation.

The operator must receive a determination from their civil aviation authority if an approval to operate with NVGs is required. Any subsequent deviation to the cockpit/cabin configuration specified in the type design of this STC may affect the compatibility of the NVIS and will require a re-evaluation for NVIS cockpit and NVG compatibility.

The aircraft is not certificated for NVG operations until the evaluation is completed.

Once the aircraft is modified with this STC, any future modification to the aircraft may also affect the compatibility with NVG and may require a re-evaluation by the FAA Flight Test Branch. The installer must determine whether this design change is compatible with previously approved modifications. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate Page 4 of 4 FAA Form 8110-2 (03/21)

(Continuation Sheet) Number: SR09559RC Date of Issuance: November 17, 2009 Date Amended: April 7, 2022 Date of Reissuance: February 17, 2016

Certification Basis:

Based on 14 CFR §§ 21.101 and 21.115, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Airbus Helicopters Deutschland GmbH (AHD) models EC135P1, EC135T1, EC135P2+, EC135T2+, EC135P3 and EC135T3 modified in accordance with REB Technologies, Inc., Master Drawing List (MDL) Document No. 98020135MDL, Rev. AD, dated March 29, 2022, or later Federal Aviation Administration (FAA) approved revision is as follows:

27.1(a)(b), amdt. 27-0; 27.301(a), amdt. 27-0; 27.303, amdt. 27-0; 27.305(a), amdt.

27-0; 27.307(a), amdt. 27-26; 27.561(a)(b), amdt. 27-32; 27.601(a), amdt. 27-0; 27.603

(a)(b)(c), amdt. 27-16; 27.605(a), amdt. 27-16; 27.609(a), amdt. 27-0; 27.613(a)(b)(c)

(d), amdt. 27-26; 27.771(a)(b), amdt. 27-0; 27.773(a)(b), amdt. 27-0; 27.777 (a)(b), amdt. 27-0; 27.853(a), amdt. 27-37; 27.1301(a)(b)(c)(d), amdt. 27-0; 27.1303(a)(b)(c), amdt. 27-0; 27.1309(a)(b), amdt. 27-46; 27.1321(a)(b)(c)(d), amdt. 27-13; 27.1322(a)

(b)(c)(d), amdt. 27-11; 27.1351(a)(b)(1)(i), amdt. 27-13; 27.1381(a)(b), amdt. 27-0;

27.1383(a)(b)(c), amdt. 27-0; 27.1385(a)(b)(c)(d), amdt. 27-0; 27.1387(a)(b)(c)(d)(e), amdt. 27-7; 27.1389(a)(b), amdt. 27-0; 27.1391, amdt. 27-0; 27.1393, amdt. 27-0;

27.1395, amdt. 27-0; 27.1397(a)(b)(c), amdt. 27-6; 27.1401(a)(b)(c)(d)(f), amdt. 27-10;

27.1501(a)(b), amdt. 27-14; 27.1523(a)(b)(c), amdt. 27-0; 27.1525, amdt. 27-21;

27.1529, amdt. 27-18; 27.1541(a)(b), amdt. 27-0; 27.1555(a)(d), amdt. 27-21; 27.1581

(a)(b)(c)(d), amdt. 27-14; 27.1583(d)(e), amdt. 27-16; A27.1(a)(b)(c), amdt. 27-18;

A27.2(a)(b), amdt. 27-18; A27.3(a)(b)(c)(d)(e)(f)(g), amdt. 27-18; A27.4, amdt. 27-47

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