Attachment_2_Statement_of_Work_final.pdf

A/MH-6M Block 3.0 MFD 1

A/MH-6M Block 3.0 MFD Statement of Work

1.0 SCOPE

This Statement of Work (SOW) describes the effort to procure a Multi-Function Display (MFD) for the A/MH-6M special operations aircraft. The new line replaceable unit (LRU) shall interface with the Avionics Management System (AMS) on the A/MH-6M. A total of 72 units will be procured, 10 prototype units that will be used for qualification testing and systems integration, and 62 production units. The contractor/supplier shall be responsible for providing the MFD, conducting and documenting the airworthiness qualification testing of the LRU, and providing the documentation necessary to integrate and operate the system.

2.0 APPLICABLE DOCUMENTS

The current issues of following documents form a part of this SOW to the extent they are specifically addressed in the SOW and CDRLs. In case of a conflict between this SOW and any referenced document, this statement of work shall take precedence. The Contractor, if it detects a conflict, will notify the Government Procuring Contracting Officer and Program Office technical point of contact of such conflicts for resolution.

2.1 DEPARTMENT OF DEFENSE GUIDELINES

MIL-STD-882E Standard Practice for System Safety

MIL-STD-810G Environmental Engineering Considerations And Laboratory

Tests

MIL-STD-461F Requirements for the Control of Electromagnetic

Interference Characteristics of Subsystems and Equipment

MIL-STD-704F Aircraft Electrical Power Characteristics

2.2 OTHER GOVERNMENT DOCUMENTS

ADS-37A-PRF Aeronautical Design Standard Electromagnetic Environmental Effects (E3) Performance and Verification Requirements

A/MH-6M Block 3.0 MFD 2

AR 71-SP Aeronautical Design Standard Practice Environmental Airworthiness and Qualification Requirements For Electronics, Avionics, and Mission Equipment Installed on Army Aircraft

2.3 AVAILABILITY OF DOD DOCUMENTS

Copies of Government Specifications and Standards may be obtained on-line from https://assist.dla.mil/online/start/index.cfm. Other government documents can be obtained from the defense technical information center (http://www.dtic.mil/). The documents pertaining to the A/MH-6M will be provided as Government Furnished Information (GFI) at contract award.

3.0 REQUIREMENTS

3.1 SYSTEM REQUIREMENTS

The system requirements are documented in the Multi-Function Display Performance Specification. The contractor shall provide an interface control document (CDRL A001) that defines the mechanical and electrical interfaces of the MFD. The Contractor shall provide a MFD that adheres and does not deviate from the attached MFD Performance Specification.

3.2 AIRWORTHINESS SUBSTANTIATION

The contractor shall provide a product that is fully qualified to U.S. Army airworthiness standards.

3.2.1 Documentation

The documentation required to substantiate airworthiness is listed in Table 1.

Table 1. Airworthiness Documentation

CDRL Description DIDs A001 Interface Control Document DI-CMAN-81248A A002 Qualification Test Plans DI-NDTI-80566 A003 Qualification Test Reports DI-NDTI-80809B A004 Failure Mode Effects and Criticality DI-ILSS-81495 A005 Acceptance Test Procedures DI-QCIC-80553A A006 Operation and Maintenance Manual MIL-STD-40051-2

A/MH-6M Block 3.0 MFD 3

3.2.2 Environmental Testing

The contractor shall develop a test plan (CDRL A002), conduct the MIL-STD- 810G tests necessary to qualify the MFD, and provide a test report documenting the test results (CDRL A003). The required tests are listed below.

3.2.2.1 Temperature, Humidity, Altitude

The MFD shall meet the requirements of MIL-STD-810, Method 520.4 (Procedure III). The maximum operating altitude shall be 15,000 feet pressure altitude. The minimum operating temperature is -40°C and the maximum operating temperature is 71°C.

3.2.2.2 High Temperature Storage

The MFD shall meet the requirements of MIL-STD-810, Method 501.6 (Procedures I and II).

3.2.2.3 Low Temperature Storage

The MFD shall meet the requirements of MIL-STD-810, Method 502.6 (Procedures I and II).

3.2.2.4 Low Pressure (Altitude)

The MFD shall meet the requirements of MIL-STD-810, Method 500.6 (Procedure I).

3.2.2.5 Temperature Shock

The MFD shall meet the performance characteristics specified here in during exposure to variable temperature conditions ( 5C/min, within the range of operating temperatures specified in paragraph above as specified in MIL-STD- 810, Method 503.6 Proc I-C, 3 cycles minimum). The MFD design is intended to withstand changes in temperature without damage due to extreme temperature military operations.

3.2.2.6 Humidity

The MFD shall meet the performance characteristics specified here in without damage or loss of function after exposure to 95% relative humidity conditions for MIL-STD-810, Method 507.6 Procedure II.

3.2.2.7 Salt Fog

The MFD shall meet the performance characteristics specified here in without damage or loss of function after exposure to salt atmosphere or salt spray for MIL-STD-810, Method 509.6.

A/MH-6M Block 3.0 MFD 4

3.2.2.8 Sand and Dust

The MFD shall meet the performance characteristics specified here in after exposure to blowing sand and dust for MIL-STD-810, Method 510.6, Proc I & II.

Marking, paint, and surface deterioration on control panels is permissible.

3.2.2.9 Rain

The MFD shall meet the performance characteristics specified here in without damage or loss of function during exposure to falling water for MIL-STD-810, Method 506.6, Proc III. As an internally mounted piece of equipment the MFD design is intended to withstand leaks and aircraft washes.

3.2.2.10 Vibration

The MFD shall provide the required performance specified here in when exposed to vibration levels and duration’s experienced in the aircraft operating environment (background vibration and rotor modulation sine tones) for MIL- STD-810, Method 514.7, Proc I, Cat 14-Rotary Wing Aircraft – Helicopter: 1P =

7.92 Hz, 1T = 44.38 Hz, n=6, m=4, Method 516.7, Proc I, V & VI, and Method

519.7 Proc III.

3.2.2.10.1 Shock

The MFD product shall meet the requirements of MIL-STD-810, Method 516.7 for functional shock (Procedure I), crash hazard shock (Procedure V), and bench handling test (Procedure VI).

3.2.2.10.2 Gunfire Shock

The MFD shall meet meet the requirements of MIL-STD-810, Method 519.7 Procedure III, functional performance characteristics specified in Figure 3-4 of the MFD Performance Specification.

3.2.2.10.3 Explosive Atmosphere

When operating in an explosive gas and air ambient mixture the MFD shall not cause ignition of the mixture for MIL-STD-810, Method 511.6, Proc I.

A/MH-6M Block 3.0 MFD 5

3.2.3 Electromagnetic Interference Testing

The contractor shall develop a test plan (CDRL A002), conduct the MIL-STD- 461E testing required to qualify the MFD, and provide a test report (CDRL A003) documenting the test results. The required tests are listed below.

Test Requirement Description

CE101 Power Leads 30Hz to 10kHz

CE102 Power Leads 10kHz to 10MHz

RE102 Electric Field 10kHz to 18GHz

CS101 Power Leads 30Hz to 150kHz

CS114 Bulk cable injection 10kHz to 200MHz

CS115 Bulk cable/impulse 5A, 30 ns

RS103, per

ADS‐37A‐PRF

Table I, Parts A/B

Electric Field

CS116 Damped sinusoidal transients 10kHz to 100MHz

RE101 Magnetic field 30Hz to 100kHz

3.2.4 System Safety

The contractor shall conduct a failure mode effects and criticality analysis of the MFD system in accordance with MIL-STD-882 and provide a Failure Mode Effects and Criticality Analysis Report (CDRL A004)

4.0 DELIVERIES

The contractor is responsible for delivering 10 prototype units and 62 production units. Six of the prototypes are units that have not been through qualification testing. The contractor shall provide a schedule for delivery of the prototype units, data deliverables, testing, and production units.

A/MH-6M Block 3.0 MFD 6

4.1 Prototypes

The 10 prototype units are for system integration and testing. The first 6 prototype units shall be delivered within 6 months after contract award.

Two of the prototype units will be utilized to complete environmental and electromagnetic interference testing per paragraphs 3.2.2 and 3.2.3, but will be sent to the Program Office at the completion of testing. The Government reserves the right to review test preparation, set-up and/or witness the execution of these tests.

The remaining 4 prototypes are Low-Rate Initial Production units and shall be delivered after successful completion of all environmental and electromagnetic interference testing per paragraphs 3.2.2 and 3.2.3.

4.2 Production

Production shall not begin until all qualification testing has been completed and the unit meets the qualification standard. The 62 production units shall be delivered according to the schedule negotiated in the IDIQ contract orders.

Acceptance procedures shall be submitted to support delivery of the first production unit (CDRL A005).

The anticipated production quantities are shown below.

FY 2018 2019 2020 2021 Total

MFD procurements 17 17 14 14 62

4.3 Documentation

The Draft ICD (CDRL A001) shall be submitted within 45 days of contract award.

The remainder of the documentation shall be submitted in-accordance-with (IAW) the CDRLs.

5.0 LIFE CYCLE SUPPORT

5.1 Supportability

The contractor shall describe the maintenance processes and procedures required for unit and intermediate level maintenance (CDRL A006).

5.2 Obsolescence

The contractor shall provide an overview of their obsolescence management approach and address Diminishing Manufacturing Sources and Material Shortages (DMSMS).

A/MH-6M Block 3.0 MFD 7

5.3 Technical Manuals

The contractor shall create operation and maintenance manuals (CDRL A006) for the MFD.

6.0 PROGRAM MANAGEMENT

The contractor shall provide the management necessary to oversee the program.

Close cooperation with the Army management and technical team shall be maintained.