STC SR00919DE

(See Continuation Sheet Page 3 of 3 Pages) SR00919DE Blackhawk Mission Equipment 4125 West Wright Street Boise, ID 83705 29 the Federal Aviation Regulations * UH-60A, S-70C, S-70A

1. The installer is responsible determine whether this design change is compatible with previously approved alterations on an aircraft.

2. If the holder agrees to permit another person to use this certificate to alter an aircraft, the holder must provide the other person written evidence of that permission.

August 29, 2019 November 27, 2019; July 25, 2023 September 18, 2019 for Manager, West Certification Branch * See attached FAA Approved Model List (AML) No. SR00919DE for List of approved rotorcraft models and applicable airworthiness regulations.

Installation of Left and Right Pulse Light is to be done in accordance with Documents:

• BME-004-001, Revision IR, or later FAA approved revision.

• BME-004-101, Revision IR, or later FAA approved revision.

• BME-004-102-1, Revision IR, or· later FAA approved revision.

SR00919DE

End Limitations and Conditions Continued:

SR00919DE

3. A copy of this certificate and Approved Model List must be maintained part of the permanent record of an altered aircraft.

4. Aircraft with this STC installed shall be maintained in accordance with the Instructions for Continued Document BHI-202-107, Revision IR, dated March 30, 2019, or later FAA accepted revision unless other methods, techniques and practices for maintaining this STC have been accepted by the FAA.

5. Aircraft with this STC installed shall be operated in accordance with the RFMS BHI-210-107, Revision IR, FAA approved on September 11, 2019, or later FAA approved revision.

6. In accordance with 21.50, the Instructions for Continued Airworthiness (ICA) are required be made available at installation.

Certification Basis:

Basis 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 STC is:

a. For parts not altered or not affected by the change, the type certification basis for aircraft(s) is shown on TCDS(s):

Refer to Approved Model List for this STC

b. The certification basis for parts altered or affected by the change since date of application is:

Refer to Approved Model List for this STC