Synopsis 22-00010.pdf

Depot repair of the Improved Altitude Hold and Hover Stabilization (IAHHS) System Applicable to the HH-60G Aircraft

This acquisition will be to establish a firm-fixed price requirements contract for the purpose of repairing assets in the table below associated with the HH- 60G Helicopter Improved Altitude Hold and Hover Stabilization (IAHHS) System.

NOUN NSN Part Number

Systems Electronics Unit (SEU) 5998-01-623-0775GC 201124536-01

Torque and Turbine Gas Temperature Converter (TGT) 5998-01-623-1129GC 3201-0107-103-1

System Interface Unit (SIU) 5998-01-623-1130GC 3201-0103-103-1

Altitude Hover Hold Stabilization (AHHS) Control Panel (ACP) 5998-01-623-1136GC 3201-0002-03-1

System Electronics Unit (SEU) 5998-01-660-1710GC 3201-0101-03-2

The requirements contract will have a basic performance period of one year plus four annual one-year options.

The BEQ for each of the assets is listed below:

Ordering Period - Best Estimated Quantities (BEQs)

NOUN Basic 1 2 3 4

Systems Electronics Unit (SEU) 25 20 20 15 15

Torque and Turbine Gas Temperature Converter (TGT) 2 2 2 2 2

System Interface Unit (SIU) 2 2 2 2 2

Altitude Hover Hold Stabilization (AHHS) Control Panel (ACP) 15 15 12 12 12

System Electronics Unit (SEU) 25 25 30 30 30

The SEU and TGT have a Repair Method Code (RMC/RMSC) of RMC “R3/R”. R3 – Repair, for the second or subsequent time, directly from the actual manufacturer. Repair Method Suffix Code RMSC R; The Government does not own the data or the rights to the data needed to contract repair of this part from additional sources. It has been determined to be uneconomical to buy the data or rights to the data. It is uneconomical to reverse engineer the part. This code is used when the Government did not initially purchase the data and/or rights.

The SIU, ACP, and the SEU -2 have a Repair Method Code (RMC/RMSC) of RMC “R4/R”. R4 – Repair, for the first time, directly from the actual manufacturer. Repair Method Suffix Code RMSC R; The Government does not own the data or the rights to the data needed to contract repair of this part from additional sources. It has been determined to be uneconomical to buy the data or rights to the data. It is uneconomical to reverse engineer the part. This code is used when the Government did not initially purchase the data and/or rights.

The Original Equipment Manufacturer (OEM) for the System Electronics Unit (SEU), Torque and Turbine Gas Temperature Converter (TGT), System Interface Unit (SIU) System Electronics Unit (SEU) Symbol Generator Unit (SGU) and the Altitude Hover Hold Stabilization (AHHS) Control Panel (ACP) for the HH- 60G Helicopter is DRS Advanced ISR, LLC.

Inspection and Acceptance will be at F.O.B. Origin. Destination: Robins AFB, GA 31098-1887. Routine Delivery: 120 calendar days after receipt of order or reparable, whichever is later. SURGE and MICAP is 60 work days after receipt of order or reparable, whichever is later. SURGE and MICAP delivery orders shall take precedence over routine repair, and the delivery schedule shall be adjusted accordingly based on concurrence between the Procuring Contracting Officer (PCO), Administrative Contracting Officer (ACO), and the contractor.

This is a sole source requirement to DRS Advanced ISR, LLC, 2601 Mission Point Blvd, Ste 250, Beavercreek, OH, 45431-6600. Authority: 10 U.S.C. 2304(c)(1) as implemented by FAR 6.302-1, Only One Responsible Source, and no other supplies or services will satisfy agency requirements. Data or rights are not owned by the Government for this solicitation. To request a copy of this solicitation, go to http://www.BetaSAM.gov. Approximate issue date of solicitation is 4 June 2021.