STC SR00922DE

SR00922DE Blackhawk Mission Equipment 4125 West Wright Street Boise, ID 83705 29 the Federal Aviation Regulations * * * See attached FAA Approved Model List (AML) No. SR00922DE for list of approved rotorcraft models and applicable airworthiness regulations.

September 10, 2019 July 25, 2023 September 18, 2019 October 24, 2019 for Manager, West Certification Branch Relocation and installation of Lead-Acid batteries, P/N RG24-15, in replacement of aircraft main batteries is to be done in accordance with Document BME-008-MDL, Revision IR, dated January 21, 2019, Master Drawing List (MDL), UH-60A helicopters, BATTERY REPLACEMENT AND RELOCATION MOD, FOR THE, UH-60A MODEL HELICOPTERS, or later FAA approved revision. An FAA Approved Airplane Flight Manual Supplement is not required for this Modification.

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

2. 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.

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

SR00922DE

End Limitations and Conditions Continued:

SR00922DE

4. Aircraft with this STC installed shall be maintained in accordance with the Instructions for Continued Airworthiness Document BHI-202-103, Revision IR, dated April 6, 2019, or later FAA accepted revision unless other methods, techniques and practices for maintaining this STC have been accepted by the FAA.

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

6. Aircraft with a NICAD battery installation and charging system is not compatible nor eligible for this STC 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 this Project is:

a. For parts not altered or not affected by the change, refer to the original Type Certificate Data Sheet (TCDS) for the aircraft.

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

Refer to Approved Models List for this STC.