Appendix_A_-_SOW.pdf
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APPENDIX A
STATEMENT OF WORK (SOW)
For
B-1B Self-Contained Attitude Indicator (SCAI)
AFLCMC/WWNMA 13-04
DATE: February 4, 2014
Prepared by:
AFLCMC/WWNMA 13-04
3001 Staff Drive, Ste 2AB78A Tinker AFB, OK, 73145-3019
B-1B Self-Contained Attitude Indicator (SCAI) SOW
Table of Contents
1 SCOPE 1
1.1 General 1
1.2 Blank 1
1.3 Associate Contractor Agreements 1
1.4 Government Furnished Property (GFP) 1
1.5 Inspection and Acceptance 2
1.6 Security 2
1.7 Data Rights 2
1.8 Air Worthiness Certification 3
1.9 Safety 3
2 APPLICABLE DOCUMENTS 3
2.1 Referenced Documentation 3
2.2 Attachments to Statement of Work (SOW) 3
3 REQUIREMENTS 4
3.1 Engineering Requirements 4
3.2 Technical Reviews 6
3.3 Item Unique identification (IUID) 7
3.4 Packaging, Handling, Shipping, and Transportation 7
3.5 Warranty 7
3.6 Hazardous Waste Disposal 7
3.7 Mission Essential Services 7
3.8 Change Request 7
3.9 Change Evaluation 8
3.10 Program Management 8
3.11 Program Cost 8
3.12 Quality 8
4 Travel 8
Appendix A: Acronyms 9 ii
1 SCOPE
1.1 General
The Oklahoma City Air Logistics Center, B-1 System Program Office (SPO) requires replacement of the current B-1B standby flight instruments. The current Standby Altimeter, Standby Airspeed/Mach Indicator, and the Standby Attitude Indicator shall be replaced with a Self-Contained Attitude Indicator (SCAI). The SCAI shall be a single Line Replaceable Unit (LRU) that provides the same functionality and meets the same environmental specifications of the current B-1 standby instrumentation identified above. The Group B kit shall be defined as the SCAI single LRU. The Group A kit also referred to as SCAI aircraft installation kit shall be defined as parts or components permanently installed to support, secure, interconnect or accommodate the equipment in a Group B kit.
The following tasks apply to this Statement of Work (SOW): Technology Insertion, Systems Integration and Systems Engineering, Installation, Hardware, Test and Evaluation, and Technical Data Management.
This contract shall include qualification testing, SCAI installation design, design of a SCAI installation kit, aircraft kit proof, and development of technical data supplements and updates.
1.2 This Paragraph is intentionally left blank
1.3 Associate Contractor Agreements
The Contractor shall enter into an Associate Contractor Agreements (ACA) with the Boeing Company for any portion of the contract requiring joint participation in the accomplishment of the Government's requirement. Liability for the improper disclosure of any proprietary data contained in or referenced by any ACA shall rest with the parties to the agreement, and not the Government.
The contractor shall provide a copy of the ACA to the Government Contracting Officer.
At no time will the Government review or make comments on the ACA’s, as this is a contractor to contractor agreement. The Contractor is not relieved of any contract requirements or entitled to any adjustments to the contract terms because of a failure to resolve a disagreement with an associate contractor.
1.4 Government Furnished Property (GFP)
No Government Furnished Property (GFP) shall be furnished by the Government to accomplish the tasks identified in this SOW.
1.5 Inspection and Acceptance
Inspection and acceptance for both Group A and Group B kits shall be at source by DCMA. After DCMA acceptance, kits shall be delivered 6 months ARO to locations directed by the B-1B SPO SCAI Program Manager or by the Contracting Officer. A signed Material Inspection and Receiving Report, DD form 250, will constitute the acceptance document for kit/spare delivery. Supplies that do not conform to the contract requirements will be handled in accordance with FAR 52.246-2.
1.6 Security
The Contractor shall possess a facility clearance at the classification level indicated on the associated DD Form 254, Department of Defense (DoD) Contract Security Classification Specification.
1.7 Data Rights
All data (to include associated drawings, modification procedures, new and altered parts lists), shall be submitted to the government prior to implementation.
The government will own unlimited data rights to all data generated by this requirement. If not, contractor must state that in the proposal. All data shall be delivered with "Unlimited Rights" as defined by FAR Part 27 and Title 10 U.S.C. §2320. The contractor shall retain no intellectual property rights to the documentation delivered to the Government. The Contractor shall waive any/all rights of intellectual property with regard to concepts, principles, and/or theory used in the design(s) submitted to the Government. Data elements delivered to the Government shall include, but are not limited to:
Conceptual design drawings/models Developmental design drawings/models and associated lists Production drawings/models and associated lists Commercial drawings/models and associated lists Special Inspection equipment (SIE) drawings/models and associated lists Special Tooling (ST) drawings/models and associated lists Specifications Software documentation Special Packaging Instruction (SPI) documents, drawings/models and associated lists
Quality assurance provisions
1.8 Air Worthiness Certification
The Contractor shall provide the Airworthiness Plan, Airworthiness Risk Assessment for reportability determination (Configuration Control Board (CCB)), and the Modification Airworthiness Certification Criteria (MACC). The Contractor shall verify the certification criteria using the standards, method(s) of compliance and evidence of compliance as outlined in the MACC. The Contractor shall provide system engineering data and artifacts required for the MACC compliance. The data provided shall be updated and completed to include the results of flight test and any aircraft system impacts. This data shall be included as a Service Engineering Report. (CDRL B009 DI-MISC- 81384/T)
1.9 Safety
The Contractor shall prepare and submit a Safety Assessment Report (SAR) to ensure all system and operational hazards are identified, eliminated, or controlled and verified.
The Contractor shall use the most current version of MIL-STD-882 (Standard Practice for System Safety) to determine hazard probability and severity reporting thresholds.
(CDRL A008 DI-SAFT-80102B/T)
2 APPLICABLE DOCUMENTS
2.1 Referenced Documentation
The following documents are referenced for the performance of this effort. All referenced documents can be found at publically available websites.
• FAR 52.246-4, 52.246-5, 52-246-6, Inspection of Services Clauses
• MIL-STD-882, Standard Practice for System Safety
• DFARS clause 252.211-7003
• Mil STD 1787C, Aircraft Display Symbology
• Mil STD 210A, Atmosphere Models
• Mil STD 1472, Design Criteria Human Engineering
• ARINC 408, Casing and Mounting
• Mil-C-5541, Coating
• Mil-DTL-38999, Connectors
• MIL-STD-810B, Environmental Test Methods
• MIL-STD-461E, Electromagnetic Compatibility
• MIL-STD-464C, Electromagnetic Environmental Effects
• MIL-HDBK-516B Expanded, Airworthiness Certification Criteria
2.2 Attachments to SOW
• LP032-0024-0001, Design Standard Cutout
• System Requirements Document (SRD)
3 REQUIREMENTS
3.1 Engineering Requirements
3.1.1 The Contractor shall provide to the Government a SCAI that is a single LRU that is to be installed into the instrument panel. All parts and hardware necessary to provide for physical and functional incorporation of this LRU into the B-1B Aircraft shall also be provided. The LRU shall be capable of replacing the following standby instruments on the B-1B Aircraft into a single standby indicator:
• Standby Altimeter, NSN 6610-00-468-1958
• Standby Airspeed/Mach Indicator, NSN 6610-01-119-2298
• Standby Attitude Indicator, NSN 6610-01-182-9481
3.1.2 The SCAI design shall meet all requirements listed in the attached B-1 SCAI SRD.
3.1.3 The proposed LRU shall have a unit technology readiness level defined as a system that has completed development and has been “flight qualified” through test and demo in a flight environment similar to that of a B-1B.
3.1.4 The contractor shall design and develop a SCAI Group A kit that will interface into the existing B-1 Standby Instrumentation architecture. The proposed design shall incorporate a single LRU that can be installed in one of the three legacy instrument locations and does not require any alteration of the B-1 instrument panel structure (e.g. enlargement of existing instrument panel openings). The design shall provide for covering of the two holes left in the aircraft instrument panel by the vacated legacy instruments. The architecture shall not contain any known Diminishing Manufacturing Sources (DMS).
Mounting or adapter plates may be used for the installation; however they shall not project further than one-half inch from the instrument panel surface and cannot occlude the visibility or reach of any legacy instruments, indicators, or controls.
3.1.5 Engineering Installation data:
The contractor shall develop and deliver a Top Kit drawing that lists all components, component fabrication drawings, installation drawings, installation specifications, installation processes and installation instructions necessary to install and operationally checkout the SCAI. All sub-kit and associate lower tier data (component drawings, specifications, etc.) shall be delivered with the Top Kit drawing. (CDRL B001 DI-SESS-8000D/T)
3.1.6 Test data:
The contractor shall develop and deliver an Installation and Checkout Procedure, Flight Test Plan, Flight Test Procedure, and Flight Test Report. (CDRL A002 DI-
NDTI-80809B/T) (CDRL A00D DI-NDTI-80566A/T), (CDRL B004 DI-NDTI-
80603A/T)
3.1.7 Environmental Qualification Data:
The contractor shall develop and deliver a Qualification Report that identifies where, when, and how all SCAI dynamic and environmental qualification requirements identified in the SRD are met. (CDRL J038 DI-QCIC-81890/T)
3.1.8 Temporary Modification Package
The contractor shall develop and deliver a Temporary Modification package and support a temporary installation using both the Group B and the Group A kits for the purposes of flight test. Any design changes that result from the temporary kits testing shall be documented. The drawings, technical data, and kit build instructions shall reflect design changes required as a result of the temporary kits testing. (CDRL J019 DI-NDTI-81562/T)
3.1.9 Validation and Verification of Manuals
The contractor shall conduct and support a validation and verification of all flight and technical manuals updated during this effort.
3.1.10 Installation Kit Design
The contractor shall provide a proof of concept design that demonstrates that the Group A and Group B kits installation can be accomplished within 24 man-hours.
(CDRL B00K, DI-TMSS-80065/T)
3.1.11 Time Compliant Technical Order (TCTO) and Technical Order (TO) Source Data
The contractor shall provide source data sufficient to allow the government to generate a Routine TCTO for permanent installation of the SCAI. The contractor shall provide all source data required to update all B-1B flight and technical manuals affected by this modification. (CDRL B002, TM-86-01N/T)
3.1.12 Production
During the Production period of the contract, the contractor shall provide kit delivery and support as follows:
3.1.12.1 The contractor shall deliver production Group A and B kits and Group B kit spares needed for the B-1B fleet.
3.1.12.2 The contractor shall provide repair support for Group B equipment during the installation period.
3.1.12.3 The contractor shall provide technical support via telephone during the first two years of the installation period.
3.1.13 Training
The Contractor shall provide Knowledge Training (Type 1) that is adequate to give maintenance personnel a basic understanding of the theory of operation of SCAI. This Knowledge Training shall be adequate to provide for the development of sound SCAI troubleshooting skills by maintenance personnel.
This Knowledge Training shall be adequate to provide for the preparation of maintenance personnel for On the Job Training (OJT) for SCAI.
3.2 Technical Reviews
The contractor shall provide an EMD schedule that meets the following meetings/reviews:
• Post Award Conference, within 30 days ARO
• System Requirements Review (SRR), within 60 days ARO
• Preliminary Design Review (PDR), within120 days ARO
• Critical Design Review (CDR), within 60 days after PDR
• Flight Test Readiness Review (FTRR), within 60 days after approved CDR
• Functional Configuration Audit/Physical Configuration Audit (FCA/PCA), within 60 days after successful completion of FTRR
• 2 Technical Interchange Meetings (TIMs) as required
• Technical Order Guidance Conference
• Drawing Guidance Conference
The Contractor shall specify agenda items and provide briefing material with specific dates and locations. The contractor shall schedule an in-process review and a pre-publication review which will present all data identified and updated by this modification.
The contractor shall provide meeting Agenda/Minutes for each review. (CDRL A009, DI-
ADMIN-81249A/T), (CDRL A006, DI-ADMIN-81250A/T), (CDRL A007, DI-ADMN-
81373/T)
3.3 Item Unique identification (IUID)
The contractor shall comply with all requirements for Item IUID marking for all delivered items for which the Government unit acquisition cost is $5,000.00 or more. All efforts required by this SOW and contract, including the preparation of Engineering Change Proposals (ECP) or notification of marking deficiencies, serial number data reporting at end of contract and the actual marking of hardware, shall be included in the base contract price. The contractor shall submit an IUID Marking Activity and Verification Report documenting items which meet or exceed the acquisition cost minimum of
$5,000.00 (CDRL B00X, DI-MGMT-81804A/T).
3.4 Packaging, Handling, Shipping, and Transportation
The contractor shall be responsible for kits packaging, handling, shipping and transportation using industry standards. To facilitate installation, the kits shall be packaged with the appropriate parts, hardware, and a packing list of comprised material in each kit. The contractor shall be responsible for shipping kits to locations directed by the B-1B SPO SCAI Program Manager or by the Contracting Officer.
3.5 Warranty
If applicable, the contractor shall provide the terms and conditions of any warranty including but not limited to covering workmanship, parts, and labor. This information shall be submitted with the contractor’s proposal.
3.6 Hazardous Waste Disposal
During any contractor associated installation activities the contractor shall be responsible for hazardous waste disposal generated as a result of the contractor’s action and will be required to follow local state/base laws and regulations.
3.7 Mission Essential Services
Not Applicable.
3.8 Change Request
The contractor shall submit to the Government a Request for Change (RFC) for engineering changes and supporting documentation by which the change is described and suggested. RFC shall describe the changes and associated Contractor documents and data (if applicable) that are affected by the proposed engineering change. The RFC shall also describe a full impact analysis of the effect of the change on the logistics, interface, design, cost and schedule requirements. (CDRL C004, DI-CMAN-80639C/T)
3.9 Change Evaluation
Contractor-approved changes that adversely impact any of the conditions listed in paragraph 3.1 may require re-evaluation by the Government. Re-evaluation may include operational testing re-assessment or re-assessment of the logistics impact of the proposed change. The Procuring Contracting Officer (PCO) must approve changes and the design shall be verified to ascertain that the functional attributes and requirements specified in the baselined product definition information and is adequate for its intended purposes. The Government is not obligated to accept any changes that no longer meet the Government’s requirements as established by the change.
3.10 Program Management
The contractor shall provide monthly program status reports electronically. The reports shall include progress of each assigned task, discussion of key accomplishments, issues impacting delivery, areas for improvement, and anticipated schedule impacts.
(CDRL A00A, DI-MGMT-80368A/T)
3.11 Program Cost
The contractor shall report program cost during Engineering and Manufacturing Development (EMD) phase. The contractor shall use the Wide Area Work Flow (WAWF), a web-based application that utilizes email notifications and secure, digital signature to generate, capture, and process receipt and payment related information.
(CDRL A00A, DI-MGMT-80368A/T)
3.12 Quality
The contractor shall develop and maintain an effective quality assurance program to ensure a quality product is delivered IAW this SOW. The contractor shall develop and implement procedures to identify, prevent, and ensure non-recurrence of defective services. The contractor’s Quality Program Plan (QPP) shall ensure that all requirements of the contract are being complied with. (CDRL J040, DI-QCIC-81722)
4 TRAVEL
Contractor will be authorized travel expenses consistent with the substantive provisions of the Joint Travel Regulation (JTR), FAR part 31 and Not-to-Exceed (NTE) the amounts specified in this contract. All necessary travel meeting the above criteria shall be submitted to PCO for approval no later than 5 business days prior to travelling.
Appendix A
Acronyms
ACA Associate Contractor Agreements CCB Configuration Control Board CDR Critical Design Review COC Certificate of Compliance COR Contract Officer Representative DMS Diminishing Manufacturing Sources DoD Department of Defense ECP Engineering Change Proposals EMD Engineering and Manufacturing Development FAR Federal Acquisition Regulation FCA Functional Configuration Audit FTRR Flight Test Readiness Review GFP Government Furnished Property IAW In Accordance With IUID Item Unique identification JTR Joint Travel Regulation LRU Line Replaceable Unit MACC Modification Airworthiness Certification Criteria NTE Not-to-Exceed OJT On the Job Training PCA Preliminary Configuration Audit PCO Procuring Contracting Officer PDR Preliminary Design Review QPP Quality Program Plan RFC Request for Change SAR Safety Assessment Report
SCAI
SOW
Self-Contained Attitude Indicator Statement of Work
SPO System Program Office SRD System Requirements Document SRR System Requirements Review TCTO Time Compliant Technical Orders TIM Technical Interface Meeting TRL Technology Readiness Level WAWF Wide Area Work Flow
| 1 SCOPE |
| 2 APPLICABLE DOCUMENTS |
| 3 REQUIREMENTS |
| 3.1.1 The Contractor shall provide to the Government a SCAI that is a single LRU that is to be installed into the instrument panel. All parts and hardware necessary to provide for physical and functional incorporation of this LRU into the B-1B Aircra... |
| 3.1.2 The SCAI design shall meet all requirements listed in the attached B-1 SCAI SRD. |
| 3.1.3 The proposed LRU shall have a unit technology readiness level defined as a system that has completed development and has been “flight qualified” through test and demo in a flight environment similar to that of a B-1B. |
| 3.1.4 The contractor shall design and develop a SCAI Group A kit that will interface into the existing B-1 Standby Instrumentation architecture. The proposed design shall incorporate a single LRU that can be installed in one of the three legacy instr... |
| Mounting or adapter plates may be used for the installation; however they shall not project further than one-half inch from the instrument panel surface and cannot occlude the visibility or reach of any legacy instruments, indicators, or controls. |
| 3.1.5 Engineering Installation data: |
| 3.1.6 Test data: |
| 3.1.7 Environmental Qualification Data: |
| 3.1.8 Temporary Modification Package |
| The contractor shall develop and deliver a Temporary Modification package and support a temporary installation using both the Group B and the Group A kits for the purposes of flight test. Any design changes that result from the temporary kits testing... |
| 3.1.9 Validation and Verification of Manuals |
| The contractor shall conduct and support a validation and verification of all flight and technical manuals updated during this effort. |
| 3.1.10 Installation Kit Design |
| The contractor shall provide a proof of concept design that demonstrates that the Group A and Group B kits installation can be accomplished within 24 man-hours. (CDRL B00K, DI-TMSS-80065/T) |
| 3.1.11 Time Compliant Technical Order (TCTO) and Technical Order (TO) Source Data |
| The contractor shall provide source data sufficient to allow the government to generate a Routine TCTO for permanent installation of the SCAI. The contractor shall provide all source data required to update all B-1B flight and technical manuals affec... |
| 3.1.12 Production |
| 3.1.13 Training |
4 TRAVEL
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