SOW.docx

C-130H2/2.5/3 AN/ALR-69A(V) Radar Warning Receiver (RWR) MODIFICATION

STATEMENT OF WORK (SOW)

for the

C-130H2/2.5/3 AN/ALR-69A(V) Radar Warning Receiver (RWR) MODIFICATION

PR: FD2060-17-31492

1322 Feb 2017

Prepared by:

AFLCMC/WLNCC

235 Byron Street, Suite 19A Robins AFB GA 31098-1670

Program Manager:

Amy Coulter C-130 Defensive Systems

1322 Feb 2017

DRAFT

Distribution Statement C: Distribution authorized to Department of Defense and U.S. Government Agencies and their Contractors (administrative and/or operational use) (20 December 2011). Other requests for this document shall be referred to AFLCMC/WLNCC, Robins AFB, GA, 31098-1622.

OFFICIAL USE ONLY

This document may contain competitive, sensitive or other non-public information Not intended for disclosure outside official government channels.

Change History

TABLE OF CONTENTS

1.0

GENERAL

1.1 SCOPE

The purpose of this SOW is to describe the scope of effort required by the Contractor to integrate the AN/ALR-69A(V) RWR System onto a selected quantity of C-130H2/2.5/3 model aircraft. The Contractor shall design, engineer, develop, manufacture, and modify a selected quantity of C-130H2/2.5/3 model aircraft (referred to as “C-130H” throughout the remaining document) by installing the AN/ALR-69A(V) RWR System. The Contractor shall provide non-recurring engineering (NRE), C130H Group A Trial Kits and Installs (TKIs), and C-130H Group A Verification Kits and installations for this contract. There will be three Ordering Options, each to order a specific number of production kits.

The Contractor shall be responsible for the conversion, maintenance and return of the aircraft to an airworthy condition at final delivery. The conversion and modification shall occur at the Contractor’s facility.

The required effort includes, but is not limited to; AN/ALR-69A(V) A-kit development, manufacture and installation of Trial Kits and Verification Kits, structural modifications to the tail cone, ground testing and supporting flight testing, updating appropriate Technical Engineering Drawings, and providing source data to update Technical Manuals. Within 18 months of contract award, the effort shall result in a fully tested modification with updated Technical Data and Engineering Data sufficient to produce the A-kits.

The Contractor shall provide non-recurring engineering (NRE), C130H2/2.5/3 Group A Trial Kit Installs (TKIs), and C-130H2/2.5/3 Verification Installs for this contract. These aircraft will be provided by the Government as Government Furnished Equipment (GFE).

The C-130H Mission Design Series (MDS) currently consist of aircraft with and without the legacy AN/ALR-69 RWR Systems installed. Aircraft with the legacy AN/ALR-69 RWR system installed are called “non-barren”. The legacy AN/ALR-69 RWR hardware, cables, wiring, and associated parts will be removed from these aircraft as part of the installation of the AN/ALR-69A(V). The Group A kits shall be based on Time Compliance Technical Order (TCTO) 1C-130-2016 INSTALLATION OF AN/ALR-69A(V) RADAR WARNING RECEIVER (RWR) ON SELECTED C-130 AIRCRAFT date 27 July 2011, which installs the AN/ALR-69A(V) on C-130H1 aircraft. Each kit shall consist of parts that shall be permanently installed on the aircraft and include all necessary components, hardware, cables, wiring, and installation drawings to successfully install AN/ALR-69A(V) on select C-130H aircraft.

The AN/ALR-69A(V) RWR is comprised of the following Group A components; four (4) C/J band antennas, two (2) Azimuth Indicators, an Indicator Control Unit (ICU) as well as all cables, brackets, connectors, and clamps permanently installed on the aircraft. Group B components consist of one (1) Countermeasures Signal Processor (CSP), and four (4) Radar Receivers (RRs). See Attachment 1: GFE.

1.2 BACKGROUND

The Government has established the requirement for selected C-130H aircraft to be modified with the installation of the AN/ALR-69A(V) RWR system to be installed on selected C-130H aircraft. The C-130H Mission Design Series (MDS) platforms rely on Electronic Countermeasures (ECM) systems to protect themselves against Radio Frequency (RF) threat weapons systems i.e. Surface to Air Missiles (SAM), Anti-Aircraft Artillery (AAA), and Air-to-Air Missiles. The AN/ALR-69A(V) RWR system provides enhanced and improved notification to the crew of threat radar signals being used to track and target the aircraft in a hostile RF environment.

The C-130H Fleet currently consist of aircraft with and without the legacy AN/ALR-69 RWR Systems installed. Aircraft with the legacy AN/ALR-69 RWR system installed are called “non-barren”. The legacy AN/ALR-69 RWR hardware, cables, wiring, and associated parts will be removed from these aircraft as part of the installation of the AN/ALR-69A(V). The contractor shall design a “single kit” to modify all three (3) versions of the aircraft (H2, H2.5, & H3) as well as aircraft with and without the legacy AN/ALR-69 installed.

The Group A kits shall be based on Time Compliance Technical Order (TCTO) 1C-130-2016 Installation Of AN/ALR-69A(V) Radar Warning Receiver (RWR) On Selected C-130 Aircraft, Dated: 27 July 2011, which installed the AN/ALR-69A(V) on C-130H1 aircraft.

The AN/ALR-69A(V) RWR is comprised of the following Group A components; four (4) C/J band antennas, two (2) Azimuth Indicators, an Indicator Control Unit (ICU) as well as all cables, brackets, connectors, and clamps permanently installed on the aircraft. Group B components consist of one (1) Countermeasures Signal Processor (CSP), and four (4) Radar Receivers (RRs). See Attachment 1: GFE.

2.0 ENGINEERING ANALYSIS

The Contractor shall perform the following engineering analysis and update as appropriate, the following studies delivered by Boeing under the C-130 AN/ALR-69A(V) System Development and Demonstration contract.

Receive Antenna – Calculate free space RF isolation, using MIL-STD-461, and MIL-STD-464 as a guide, between the RWR antennas and the other antennas of C-130H2/H2.5/H3 systems including, but not limited to, Real Time Information in the Cockpit (RTIC), APN-241 weather radar, Tactical Control and Navigation (TACAN), Identification Friend and Foe (IFF) both Mode 5 & S, Satellite Communications (SATCOM), and Enhanced Traffic Collision and Avoidance System (E-TCAS). Emphasis should be placed on the aft C/J antennas, since they will be slightly relocated. This applies to all frequencies within the C/J band.

CDRL A012, Technical Report – Study/Services, (DI-MISC-80508B/T)

Receive Antenna Footprint – Calculate radome footprint effect on viewing angle of AAR-47 sensors at the new locations for the aft C/J band antenna. The Contractor shall ensure full viewing angles of the forward and aft C/J antennas will not physically obstruct or be obstructed by other systems during installation, such as the sensors for the AAR-47 Missile Warning System (MWS).

CDRL A012, Technical Report – Study/Services, (DI-MISC-80508B/T)

Radar Receivers & Antenna Engineering Analysis -- The Contractor shall develop test plans, test reports, and/or technical reports, program deficiency reports, and all operational safety, suitability, and effectiveness (OSS&E) requirements for electromagnetic interference (EMI) test, electromagnetic compatibility (EMC) test, structural analysis, cable routing, and dummy plug locations for the new Aft C/J antenna locations, and new aft RR locations. The Contractor shall update the thermal analysis report for RR aft placement and forward RR locations with the new armor installed (TCTO 1C-130-2094). The installed RR’s with fan, ducting, and personnel safety guards must allow ground operation of the forward and aft RR’s with ambient temperatures of 51 degrees C, as measured outside the aircraft, with and without solar loading. The mounting hardware and the ambient environment around the installation shall maintain the RR thermal interface at or below 71 degrees C in flight and during ground maintenance operations.

CDRL A012, Technical Report – Study/Services, (DI-MISC-80508B/T)

32.0 AIRCRAFT SURVEY

The Contractor shall perform aircraft surveys no later than one month after contract award. The Contractor shall documentand document all key technical details pertaining to the AN/ALR-69A(V) modification installation with an Aircraft Survey Report (CDRL A001). For bidding purposes only, the locations to be surveyed are Davis Monthan AFB, AZ, Wilmington ANGB, DE, and Great Falls, MT, with the exact locations to be determined after contract award. Three aircraft will be surveyed, with an example of each version of aircraft, H2, H2.5, and H3 with at least one example of a barren aircraft and at least one example of a non-barren aircraft. The Contractor shall neither release nor share information with any entity, other than their “need-to-know” subcontractors or the Government, without written approval from the Procuring Contracting Officer (PCO).

CDRL A012A001, Technical Report -– Study/ServicesAircraft Survey, (DI-MISC-80508B/T)

34.0 ENGINEERING DESIGN REQUIREMENTS

The Contractor shall design the Group A hardware for the modification onto the C-130H models with the AN/ALR-69A(V) RWR integration onto the C-130H2/H2.5/H3 models. This design will be based on the previous AN/ALR-69A(V) C-130H1 integrationmodification effort. The integrationmodification of this system requires specialized knowledge of aircraft single mode fiber optics installation/maintenance and detailed knowledge of the operation of the aircraft defensive systems used on DOD aircraft. The Contractor shall use, where possible, existing AN/ALR-69A(V) Group A equipment design from the C-130H1 effort, to include the existing fiber optic (FO) cable design. Where that is not possible, the Contractor shall design the new equipment and provide updated drawings. Updates to the existing drawing will not consist of new drawings, but will be annotated on the existing drawings per ASME Y14.35. Any drawings and Engineering Change Order (ECOs) required will be reviewed and approved by the assigned Government Engineer prior to inclusion in the Technical Data Package (TDP). The AN/ALR-69A(V) uses ruggedized Single Mode Fiber Optic (FO) cables to transmit signals between the Countermeasure Signal Processor (CSP) and the Radar Receivers (RRs). New installations shall use the existing cable design. Any deviations from the current FO designs will require prior Government approval. The Contractor shall procure the fiber opticFO cables as assemblies IAW the Technical Data Package (TDP). On aircraft with a previously installed AN/ALR-69 RWR, the Contractor shall remove the legacy AN/ALR-69 RWR and associated equipment, both Group A wiring and Group B equipment, to include the Frequency Selective Receiver System (FSRS) antenna array and AN/ALR-69 C/D band antennas on the lower fuselage, and to provide closeout panels, as necessary. Drawing number 3343315 (see Attachment 3) and 392525 (see Attachment 4) should be used as a guide.

The Contractor shall provide one (1) new tail cone assembly with each Group A TCTO kit. The tail cone tip assembly shall maintain the current form with a top access cover and drain holes. The assembly shall maintain the formation light assemblies and AAR-47A(V) 2 sensors, while installing the new AN/ALR-69A(V) antennas with adequate separation to provide a maximum field of view in relation to the AAR-47A(V) 2 sensors and AN/ALR-69A(V) antennas. Drawing number 3337728 (see attachment 5) shall be used as a guide to standardize the tail cone assembly configuration for this program. The Contractor shall ensure structural support is adequate to accommodate the additional weight added by the C/J antennas, and ensure grounding/bonding capability to meet the antenna requirements.

The Contractor shall be responsible for the integrity of all physical, electrical, and any other interfaces between the GFE supplied Group B equipment and the aircraft being modified. The Contractor shall avoid any interoperability problems between all currently installed C-130H avionics equipment and the AN/ALR-69A(V) RWR system in light of the installation of the new RTIC system. The Contractor shall incorporate studies and test findings to generate a modification to the aircraft that shall integrate common suppression line (CSL)s such that the connected systems operate simultaneously and operate at their expected performance level. Special consideration should be placed on Real Time Intelligence in the Cockpit (RTIC), TACAN, IFF, E-TCAS, and APN-241 weather radar system.

The Contractor shall provide a Systems Engineering Management Plan (SEMP) to describe the key engineering management practices essential to the successful completion of the ALR-69A(V) RWR integrationmodification.

CDRL A02020, System Engineering Management Plan (SEMP), DI-SESS-81785A

ANY OTHER DELIVERABLES?

43.1 GENERAL DESIGN

The Contractor shall be responsible for producing and documenting a design that will satisfy all of the Government requirements and is based on the C-130H1 effort.

In the event the Contractor’s equipment fails to meet these requirements, the Contractor shall be responsible for corrective action in accordance with the contract and at no additional cost to the Government.

43.2 TRIAL KIT INSTALLATION (TKI) AND VERIFICATION

The Contractor shall start TKI no later than eight (8) months after contract award and start begin Verification no later than fifteen (15) months after contract award. The TKIs shall be accomplished on three C-130H2/2.5/3 aircraft, to include at least one of each model (i.e. C-130H2, C-130H2.5, and C-130H3) simultaneously and shall include at least one example of a barren and at least one example of a non-barren C-130H aircraft. The C-130H2/2.5/3 aircraft Verifications shall also be accomplished simultaneously using the same aircraft selection criteria as the TKI. The Contractor shall provide the necessary personnel together with any materials, tools, equipment and facilities required to support this effort.

43.3 TKI/VERIFICATION INSTALLATION FACILITY

The Contractor’s facility shall meet the following minimum requirements:

· DCMA approved facilities and approved Contractor’s procedures according to DCMA Instruction 8210.1C, Contractor’s Flight and Ground Operations

· SAE-AS9100, Quality Management Systems – Aerospace Requirements certification

· Defense Security Service (DSS) approved secured and bonded storage space for AN/ALR69A(V) classified modification kits and test equipment

· Sufficient hangar space to meet program requirements

· Sufficient ramp space to meet the requirements

43.4 TRIAL INSTALLATION RETROFIT

Following successful completion of the Verification on each aircraft, and the establishment of a production baseline, the Contractor shall retrofit TKI and Verification aircraft, at no additional cost to the Government, to bring them up to production configuration.

43.5 ENGINEERING DATA

The Contractor shall modify the existing C-130H1 TDP so that it accurately depicts the final product and addresses the installation on the C-130H1/2/2.5/3 aircraft. The TDP shall represent the approved, tested, and accepted configuration of the defined, delivered item(s). TDP data includes, but is not limited to, Computer Aided Design (CAD) data, CAD models, model based definition data sets, Gerber data, and Master Bill of Materials (BOM). The TDP shall provide the necessary design, engineering, manufacturing, testing and quality assurance requirements information necessary to enable the procurement or manufacture of an interchangeable item that duplicates the physical and performance characteristics of the original product without additional design engineering effort or recourse to the original design activity or any third party. Vendor Item Control Drawings shall be used to specify the requirements for purchased items when such items have been approved for use in the design and are used without alteration, selection or source qualification (testing of an item prior to procurement action to ensure that it satisfies the specified requirements). All engineering product definition data created using Government funding as a result of this contract shall be considered a part of the TDP and shall be delivered to the Government with unlimited rights. The Contractor shall deliver the TDP IAW with the Technical Manual Contract Requirement (TMCR). Also, The Contractor shallthe deliver the TDP shall be delivered in accordance with Air Force Product Data Specification drawing 9579776 Revision M (CAGE 98752), reference attached DD Form 1423 Block 16.

CDRL A018, Technical Manuals, TM-86-01N CDRL A01903, Product Drawings/Models & Associated Lists, DI-SESS-81000E/T

43.5.1 ENGINEERING DATA UPDATES AND REVISIONS

The Contractor shall (and shall cause subcontractors and vendors to) update and maintain engineering data for the item(s) designed/ developed/modified/produced and funded by this contract for the life of this contract and shall incorporate all changes in accordance with the following:

a. Engineering changes shall be incorporated into the applicable engineering data within 3 three months after engineering release/Air Force concurrence or at intervals of five changes. A safety change will be incorporated immediately.

b. All engineering changes shall be incorporated into the applicable engineering data prior to delivery of data for review

c. All engineering changes shall be incorporated into the applicable engineering data prior to delivery of final media Revisions to existing engineering drawings/models and associated lists and other documentation to be included in the TDP, for which the Contractor is the current design activity, shall result in the delivery of the entire revised document and associated data file. For example, when a portion of a document is revised the entire document shall be delivered. No changes can be made without prior Government aApproval is required for all changes.

CDRL A004, Engineering Change Proposal, (ECP), DI-SESS-80639D/T CDRL A005, Request For Variance (RFV), DI-SESS-80640D/T CDRL A018, Technical Manuals, TM-86-01N CDRL A019A003, Product Drawings/Models & Associated Lists, DI-SESS-81000E/T

43.6 CREW STATION WORKING GROUP (CSWG)

The Contractor shall establish a Crew Station Working Group (CSWG) to ensure the end user’s considerations and inputs are incorporated into the design of the installation of the AN/ALR-69A RWR systems onto the C-130H aircraft. The Contractor shall prepare an agenda prior to each CSWG and prepare minutes for each instancemeeting. These meetings shall be held at the Contractor’s facility, or other agreed upon location, and in conjunction with PDRother planned meetings, as much as possible, . The CSWG shall be chaired by the Contractor Program Manager and include the ANG, AATC, AFRC, AFLCMC/WLN, and Contractor representatives.

CDRL A001, Conference AgendaA006, Conference Agenda, DI-ADMN-81249A 81249B CDRL A002, Conference MinutesA007, Conference Minutes, DI-ADMN-81250A 81250B

4.0 ENGINEERING ANALYSIS

The Contractor shall perform the following engineering analysis and update as appropriate, the following studies delivered by Boeing under the C-130 AN/ALR-69A(V) System Development and Demonstration contract.

4.1 Receive Antenna

Calculate free space RF isolation, using MIL-STD-461, and MIL-STD-464 as a guide, between the RWR antennas and the other antennas of C-130H2/H2.5/H3 systems including, but not limited to, Real Time Information in the Cockpit (RTIC), APN-241 weather radar, Tactical Control and Navigation (TACAN), Identification Friend and Foe (IFF) both Mode 5 & S, Satellite Communications (SATCOM), and Enhanced Traffic Collision and Avoidance System (E-TCAS). Emphasis should be placed on the aft C/J antennas, since they will be slightly relocated. This applies to all frequencies within the C/J band.

CDRL A008, Technical Report – Study/Services, (DI-MISC-80508B/T)

4.2 Receive Antenna Footprint

Calculate radome footprint effect on viewing angle of AAR-47 sensors at the new locations for the aft C/J band antenna. The Contractor shall ensure full viewing angles of the forward and aft C/J antennas will not physically obstruct or be obstructed by other systems during installation, such as the sensors for the AAR-47 Missile Warning System (MWS).

CDRL A009, Technical Report – Study/Services, (DI-MISC-80508B/T)

4.3 Radar Receivers & Antenna Engineering Analysis

The Contractor shall develop test plans, test reports, and/or technical reports, program deficiency reports, and all operational safety, suitability, and effectiveness (OSS&E) requirements for electromagnetic interference (EMI) test, electromagnetic compatibility (EMC) test, structural analysis, cable routing, and dummy plug locations for the new Aft C/J antenna locations, and new aft RR locations. The Contractor shall update the thermal analysis report for RR aft placement and forward RR locations with the new armor installed (TCTO 1C-130-2094). The installed RR’s with fan, ducting, and personnel safety guards must allow ground operation of the forward and aft RR’s with ambient temperatures of 51 degrees C, as measured outside the aircraft, with and without solar loading. The mounting hardware and the ambient environment around the installation shall maintain the RR thermal interface at or below 71 degrees C in flight and during ground maintenance operations.

CDRL A010, Technical Report – Study/Services, (DI-MISC-80508B/T)

55.0 TESTING

The Contractor shall manufacture and test the Group A Kit items and test equipment in accordance with the TDP and related military specifications. The Contractor shall conduct aAircraft ground tests to shall be conducted by the Contractor to verify that the new and upgraded systems are appropriately integrated in accordance with the system interface documentation. All aircraft ground testing shall be conducted in accordance with Government approved Acceptance Test Plantest plans. Upon successful completion of all required ground tests, the Contractor shall prepare an Acceptance Test Report.

The Contractor shall be responsible for providing Engineering and ground support during the ground testing and the Air Force conducted flight test, which will be conducted at a date to be determined during the testing phase. The Contractor will not be required to fly on the aircraft at any time during this program.CDRL A011, Acceptance Test Plan – ATP, (DI-QCIC-80553A) CDRL A012, Acceptance Test Report (ATR), (DI-ATTA-80283B/T)

55.1 Test Responsibilities

The Contractor shall plan, develop, and conduct aircraft ground tests on the C-130H TKI aircraft and Verification aircraft after completion of aircraft kit installations and will include disturbed system checks and modification functional checkoutson the C-130 H2/2.5/3 TKI aircraft and Verification aircraft. All ground tests shall be accomplished at the aircraft modification sitelocation. Ground tests shall be conducted on the designated aircraft after completion of aircraft kit installations and will include disturbed system checks and modification functional checkouts. The Contractor shall provide tools, test equipment, technical data, drawings, and personnel, available in sufficient quantities to preclude test cancellation or degradation. The Contractor shall test and verify the proper installation of single mode fiber optics assemblies in accordance with the ARINC report 805-4, 11A-14-4, and drawing number 5009374011. The test and support equipment used for quantitative measurements shall be managed in accordance with ANSI/NCSL Z540.3 (R2013). The Contractor shall identify and document any deficiencies noted during Contractor system installation and testing and provide recommendations for correcting deficiencies related to the Group A integrationmodification effort as early as possible.

CDRL A015 Test Procedure, DI-NDTI-80603B/T CDRL A01136 Test/Inspection Report, DI-NDTI-80809B/T

55.2 Integrated Master Test Plan (ImtpIMTP)

The Contractor shall develop and follow an Integrated Master Test Plan (IMTP) for Ground Testing and t. The Government will use the IMTP during all flight testing. The Contractor shall include compliance method and criteria for Ground and Flight tests. The Contractor shall support and provide the Government in acquiring any required test/support equipment.

CDRL A01254, Integrated Master Test Plan, (DI-NDTI-80566A/T)

55.3 Test Procedures

The Contractor shall provide and update the test procedures for all ground and flight testing. The test procedures shall include detailed test procedures and cards fully demonstrating the performance of the systems installed by this SOW.

CDRL A01515, Test Procedure, (DI-NDTI-80603B80603A/T)

55.44 Aircraft Leak Down Checks

The Contractor shall perform aircraft leak-down checks on the aircraft in accordance with TO 1C-130H-2-21JG-30-1 and applicable technical orders, prior to modification for baseline leak rate and after the completion of the modification to ensure no degradation.

55.55 Electrical Load Analysis (ELA)

The Contractor shall perform and provide results of an electrical loads analysis to ensure the existing electrical systems or power distribution of each aircraft can support the AN/ALR-69A power requirements. Using MIL-E-7016, the Contractor shall provide the status consistent with the existing electrical load data per each aircraft.

CDRL A0136, Scientific and Technical Reports, DI-MISC-80711A/T

55.6 Electromagnetic Interference (EMIMI) Testing

The Contractor shall conduct EMI testing at the aircraft level in accordance with MIL-STD-461 and MIL-STD-464. Any problems associated with Group A shall be documented and corrected by the Contractor. The Contractor shall also report any Group B discrepancies for Government action.

CDRL A012A017, Technical Report–Study/Services, DI-MISC-80508B/T

55.7 Electromagnetic Compatibility (EmcMC) Testing

The Contractor shall conduct EMC ground test at the aircraft level to ensure that no detrimental safety-of-flight conditions or performance degradation of existing systems result from EMC between aircraft subsystems and to verify overall system-level compatibility.

CDRL A00818, E3 Verification, DI-EMCS-81541B/T CDRL A009A019, E3 Verification Report, DI-EMCS-81542B/T

55.8 Flight Test

The Contractor shall support AF conducted flight test, to include any trouble shooting, and repair problems or correct any AN/ALR-69A(V) discrepancies after flight testing.The Contractor shall be responsible for providing engineering and ground support during the Air Force conducted flight test, which will be conducted at a date to be determined during the testing phase. The Contractor shall include trouble shooting, correction of any AN/ALR-69A(V) discrepancies discovered during flight testing. The Contractor will not be required to fly on the aircraft at any time during this program.

55.9 Fiber Optic Cable Testing

The Contractor shall assign each fiber optic cable delivered under this contract a serial number. The Contractor shall perform a Visual End Face Inspection of all fiber optic cables, either manufactured or purchased, using a Desktop Videoscope or a hand held Fiber Optic Microscope in accordance with ARINC 805-4. The contractor shall maintain digital photographs in Tiff, LZW lossless compression format, of all fiber Visual End Face inspections. All fiber optic cables shall be tested by mating to the appropriate Aerospace-Certified Measurement Quality Jumper (MQJ). Test results shall be documented using Microsoft Excel. Multi-terminus cables shall be tested using Multi-Terminus MQJ in accordance with ARINC 805-4. All MQJ shall be verified prior to testing using ARINC 805-4, Appendix C and readings shall be documented in Microsoft Excel.

CDRL A013A020, Scientific and Technical Reports, DI-MISC-80711A/T

66.0 CONFIGURATION AND DATA MANAGEMENT

The Contractor shall perform configuration and data management in accordance with the Contractor’s established configuration and data management processes assuring systematic evaluation, coordination, authorization, change control, and implementation for configuration control for the AN/ALR-69A(V) Modification.

a. Update as necessary the functional and physical characteristics of all Group A hardware.

b. Establish and maintain a Configuration/Data Management Plan that employs company standard configuration and data management control processes that are AS 9100 compliant.

c. Monitor the Sub-Contractors by conducting audits.

d. Maintain an effective configuration change control system.

e. Report and maintain configuration status accounting and change processing information.

f. Maintain an engineering release system and document release records in accordance with the approved Configuration/Data Management Plan.

The Contractor shall document modifications, upgrades and other changes in configuration baseline documents (e.g. specifications, drawings) verified by test, similarity, demonstration, analysis, or inspection.

CDRL A021, Contractor’s Configuration Management Plan, (DI-CMAN-80858B/T)??

6.1 CONFIGURATION CONTROL

The Contractor shall provide configuration control of the evolving project baseline and the Government will have approval authority over any unexpected Group A changes resulting from the current version of the Boeing Interface Control Specification, document (see attachment 2). The Contractor’s shall provide for systematic evaluation, coordination, authorization, and implementation of configuration control for modifications to the contract, the configuration of project end items, and all related controlled documentation.

CDRL A005, Engineering Change Proposal, (ECP), DI-SESS-80639D/T CDRL A006, Request For Variance (RFV), DI-SESS-80640D/T

66.12 CONFIGURATION AUDITS

The Contractor shall conduct a Physical Configuration Audit (PCA) 30 days prior to Group A TKI and VerificationIAW CDRL A022. All Group A items developed and delivered under this program will be audited in accordance with SAE EIA-649 Rev B. The Contractor shall prepare and deliver an agenda and a configuration audit summary report and certification in support of this audit.

CDRL A001, Conference AgendaA006, Conference Agenda, (DI-ADMN-81249A81249B) CDRL A02207, Configuration Audit Summary Report & Cert, DI-SESS-81022D/T

77.0 DATA MANAGEMENT

The Contractor shall ensure that the documentation necessary for execution of the program is available IAW this SOW and the CDRL. Unclassified CDRL and Data Accession List (DAL) items shall be delivered to the Government via E-Mail and IAW the delivery instructions on the applicable CDRL. Classified material shall be handled IAW the DD-254 DOD Contract Security Classification Specification. Classified hardware, test equipment and data associated with the AN/ALR-69A(V) will be handled and stored at the Contractor’s facility according to DSS/DCMA guidance.

CDRL A023A023, Data Accession List, DI-MGMT-81453A

88.0 STANDARDIZATION AND PARTS CONTROL

The Contractor shall establish and maintain an integrated Parts Management Program and Diminishing Manufacturing Sources and Material Shortages (DMSMS) program in accordance with MIL-STD-3018 and SD-22 Guidebook for all new designs or modified equipment. These programs will ensure that the use of parts meet the contractual requirements, reduce proliferation of parts within and across DoD weapons systems and equipment through standardization, enhance reliability and supportability to meet material readiness objectives, and reduce total life-cycle costs. The Contractor shall also participate in the Government/Industry Data Exchange Program (GIDEP) for parts control and quality, track and control the use and manufacture of critical parts, and manage the selection and specification of parts used in product design to mitigate the impact of any obsolete, and/or unavailable parts.

CDRL A02244, Government Industry Data Exchange Program, DI-QCIC-80125B/T CDRL A026A025, Diminishing Manufacturing Sources & Material Shortages Plan, DI-MGMT-81948

99.0 OPERATIONAL SAFETY, SUITABILITY, AND EFFECTIVENESS (OSS&E)

The Contractor shall ensure the Group A equipment design, development, qualification, and testing, complies with the OSS&E requirements in accordance with AFI 63-201. The Contractor shall submit a Requirement Traceability Matrix (RTM) to demonstrate and meet the program installation requirements.

CDRL A02614, Specification Requirements Verification Matrix, DI-MISC-81283/T

99.1 DRAG ANALYSIS

The Contractor shall conduct a drag analysis utilizing existing applicable test data as a reference; however, this data shall not be used as a substitute for an independent analysis of the modification configurations. The drag analysis is required to determine the impacts of the modifications aerodynamic impact on the C-130H MDS performance.

CDRL A013A027, Scientific and Technical Reports, DI-MISC-80711A/T

99.2 STATIC & DYNAMIC LOADS ANALYSIS

The Contractor shall perform loads analyses for the Group A and Group B equipment installations to determine the magnitude and distribution of the static and dynamic loads that the upgrade and affected aircraft structure will encounter within the normal operating envelope of the aircraft.

CDRL A013A028, Scientific and Technical Reports, DI-MISC-80711A/T

99.3 STRESS ANALYSIS

The Contractor shall perform stress analyses for the Group A and Group B equipment installations to determine the stresses, deformation, and margins of safety resulting from the external loads imposed on the structure. When strength proof tests of each modified area are not performed, the analytical margins of safety shall not be less than 0.25. Only the aircraft structure that is affected by the modification shall be analyzed.

CDRL A02921 Stress, Fatigue & Fracture Analysis Report, DI-SESS-81939

99.4 BUFFETING, ACOUSTIC AND VIBRATION ANALYSIS

The Contractor shall perform buffeting acoustic and vibration analyses for the Group A and B equipment. Only the aircraft structure that is affected by the modification shall be analyzed.

CDRL A013A030, Scientific and Technical Reports, DI-MISC-80711A/T

99.5 CREW MEMBER CRASH SAFETY ACCELERATION

The Contractor shall design the equipment mounting to ensure the AN/ALR-69A(V) system and associated structure items shall not break free and cause a crash hazard to crew members when exposed to C-130H crash individual acceleration loads shown in the table below.

Airplane AAAccelerAcceleration

99.6 NON-CREW MEMBER CRASH SAFETY ACCELERATION

The Contractor shall design the equipment mounting to ensure the AN/ALR-69A(V) system and associated structure shall not break free and cause a crash hazard when exposed to C-130H crash individual acceleration loads shown in the table below.

Airplane Acceleration

99.7 THERMAL MASS ANALYSIS

The Contractor shall conduct a Thermal Mass Analysis for Group B (GFE) hardware to determine localized temperatures of both environment, Group B (GFE) hardware and connecting devices such as brackets, mounts or harnesses. Environmental Conditions – The environment in which the AN/ALR-69A(V) must perform satisfactorily is that for operations and maintenance of the C-130H aircraft. The Contractor shall not be responsible for the performance of the Group B (GFE) LRUs, but shall be responsible for not degradingensuring the performance of the Group B (GFE)is not degraded with this design. The Contractor shall be responsible for the performance of the contractor supplied Group A.

CDRL A03113, Scientific and Technical Reports, DI-MISC-80711A/T

1010.0 WEIGHT AND BALANCE

The Contractor shall provide and update aircraft weight and balance values using the established aircraft weight and balance system in accordance with T.O. 1C-130E-5 and T.O. 1-1B-50. The Contractor shall ensure Aircraft weight and balance shall be within the acceptable limits after modification of the aircraft. The weight and center of gravity shall support safe vehicle operations for all defined mission requirements. A calculated weight check of the aircraft shall be performed after all installations are completed and before any flight tests are accomplished. Final weight and balance data for a production product shall be provided No Later Than (NLT) 1 month prior to Verification. The Contractor shall provide updates to the basic weight data as applicable in the TCTO.

CDRL A02232, Weight and Balance Report, DI-MGMT-81501A/T

111.0 SUBSYSTEM SPECIFICATION

The Contractor shall develop and deliver a Group A subsystem-specification that captures all requirements of this modification.

CDRL A03313, Scientific and Technical Reports, DI-MISC-80711A/T

122.0 MODIFIED & INTEGRATED SYSTEM PERFORMANCE RESPONSIBILITY (MSPR & ISPR)

The Contractor shall be responsible for Group A performing to the Boeing ICD BO-SPC-04291 (see attachment 2).

133.0 ENVIRONMENT, SAFETY AND HEALTH (ES&H)

The Contractor shall provide a Safety Assessment Report (SAR) for the modification prior to Test and Evaluation (T&E), in accordance with task 301 of MIL-STD-882. The Contractor shall comply with Hazardous Material Management Program (HMMP) in accordance with AIA NAS NAS411. The Contractor shall document and review all chemicals utilized for manufacture, operation and/or servicing to prevent inclusion of Class I or II Ozone Depleting Substances (ODS) into the design. All hazardous material must be approved by the Government for use before being utilized on this modification. Also, the system shall operate and not deteriorate within environments containing the fungus groups listed in the table below.

CDRL A03417, Safety Assessment Report, DI-SAFT-80102B80102C/T

Fungus Fungus Sources Identification No

144.0 QUALITY ASSURANCE

The Contractor shall have a Quality Assurance (QA) program compliant with AS 9100 and DCMA 8210. The Contractor shall be certified on these standards prior to proposal submission. The Contractor shall ensure that design, development, production, and test for each project is supported, and shall comply with current defense industry best practices and processes suitable for the nature of the product.

155.0 LOGISTICS

155.1 INTEGRATED LOGISTICS SUPPORT (ILS)

The Contractor shall be responsible for ILS of the Group A integration of the AN/ALR-69A(V) RWR system for the TKI and Verification.

155.1.1 PACKAGING, HANDLING, STORAGE, & TRANSPORTATION (PHS&T)

The Contractor shall be responsible for preservation, packaging packing and transportation of all deliverable Group A kit items. This task shall meet the requirement of MIL-STD-2073-1 (Class B), MIL-STD-130, and MIL-STD-129. The TCTO production kits shall be packed per the guidelines as specified on Air Force Material Command (AFMC) Form 158 Packaging Requirements, as incorporated in section J of the contract. The production kits will be shipped to FY2260 DDWG SBE, 620 Peacekeeper Way, Bldg. 368A, TCTO Kitting Unit, Robins AFB, GA 31098.

155.1.2 LOGISTICS MANAGEMENT INFORMATION SUMMARIES (LMI)

The Contractor shall generate LMI Summaries in accordance with SAE GIEA-STD-0007, and using SAE GIEA-HB-0007 as a guide.

CDRL A003 Log Management Information Summaries (LMI), DI-SESS-81758A/T

155.1.2.1 TEST AND SUPPORT EQUIPMENT (SE)

The Contractor shall provide to the Government all Support Equipment (SE) necessary to operationally check-out and maintain the AN/ALR-69A(V) RWR. The Contractor shall provide a number of sets of this equipment as defined in Appendix C. The Contractor shall ensure that the test set fiber opticFO cables meet the thermal cycling testing requirement in accordance with TIA-455-3B and TIA-455-C. The production kits will be shipped to FY2260 DDWG SBE, 620 Peacekeeper Way, Bldg. 368A, TCTO Kitting Unit, Robins AFB, GA 31098.

CDRL A003A035, Log Management Information Summaries, (LMI), DI-SESS-81758A/T

155.1.2.2 PROVISIONING

An initial provisioning guidance conference shall be held in conjunction with the Kick-Off meeting at a site and on a date agreed upon by the Government contracting officer and the Contractor. The Contractor shall identify and recommend logical spare/repair parts sufficient to meet system/equipment operation and supportability. Initial provisioning for Group A was accomplished during the C-130H1 effort, therefore, the provisioning effort for this contract will only address any changes to the initial provisioning caused by this contract and the resultant TCTO 1C-130-2016 supplement. SAE GIEA-STD-0007A shall be used as a guide. Format must be consistent with existing Government Provisioning data system (D220).

CDRL A003A036, Log Management Information Summaries, (LMI), DI-SESS-81758A/T CDRL A03704, Engineering Data for Provisioning, DI-SESS-81874/T

155.1.3 TECHNICAL DATA

The Contractor shall develop and deliver a supplement to TCTO 1C-130-2016 and changes to applicable Technical Manuals in accordance with applicable TMCR, TM-86-01N.

CDRL A0A03818, Technical Manuals, TM-86-01N

166.0 GFE/GFP MANAGEMENT

The Contractor shall be responsible for safeguarding all Government property provided for Contractor use.