HSCG38-16-Q-200052_-_Attachment_7_-_SFI_Objective_Capabilities_Compliance_Matrix.xls
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- HSCG38-16-Q-200052
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Attachment 7 - SFI Objective Capabilities Compliance Matrix
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| File | Type | Posted |
|---|---|---|
| HSCG38-16-Q-200052_-_Attachment_1_-_Schedule_(Amended).xlsx | XLSX spreadsheet | |
| Solicitation_-_HSCG38-16-Q-200052_-_Q A_(Amended).doc | DOC document | |
| HSCG38-16-Q-200052_-_Attachment_2_-_Statement_of_Work_(Amended).docx | DOCX document | |
| HSCG38-16-Q-200052_-_Attachment_5_-_Technical_Acceptability_Compliance_Matrix_(Amended).xls | XLS spreadsheet | |
| Solicitation_-_HSCG38-16-Q-200052_-_Q A.doc | DOC document | |
| HSCG38-16-Q-200052_-_Attachment_1_-_Schedule.xlsx | XLSX spreadsheet | |
| HSCG38-16-Q-200052_-_Attachment_2_-_Statement_of_Work.docx | DOCX document | |
| HSCG38-16-Q-200052_-_Attachment_5_-_Technical_Acceptability_Compliance_Matrix.xls | XLS spreadsheet | |
| HSCG38-16-Q-200052_-_Attachment_4_-_Offeror_Checklist_.doc | DOC document | |
| HSCG38-16-Q-200052_-_Attachment_3_-_Terms_ _Conditions.docx | DOCX document | |
| HSCG38-16-Q-200052_-_Attachment_6_-_Sustainment_and_Repair_Capability_Compliance_Matrix.xls | XLS spreadsheet |
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Attachment 4
| HSCG38-16-Q-200052 SFI Objective Capabilities Compliance Matrix | |||
| Offeror | Name of company | ||
| CAGE Code | As listed in SAM | ||
| Company Size | According to NAICS 334511 | ||
| Type of Small Business | If applicable | ||
| Device(s) Identified | Name of SFI system | ||
| Subfactor 1: Ability of SFI to Exceed Physical and Functional Minimum Requirements | |||
| Requirement: | SOW Reference: | Included in Quote? (Yes or No) | Quote Page Reference |
| SFI objective: Display depth of 10" or less (Ultimate objective is 6") | 5.3.3.1 | ||
| SFI objective: Compact, low weight unit | 5.4.4 | ||
| SFI objective: Temperature range of -55 to +70 degrees Celsius | 5.3.6.1 | ||
| SFI objective: SFI Battery operates for greater than 30min - 1hr | 5.4.2 | ||
| SFI MTBF exceeds 3,000 flight hours or five (5) years without failure | 5.5.2.4 | ||
| SFI objective: Current draw is less than 3 Amps | 5.3.6 | ||
| Subfactor 2: Additional Desired Objectives | |||
| Requirement: | SOW Reference: | Included in Quote? (Yes or No) | Quote Page Reference |
| Environmental compliance objective per RTCA DO-160G: | 5.4.3 | ||
| 1) Shock | 5.4.3 | ||
| 2) Waterproofness | 5.4.3 | ||
| 3) Sand and Dust | 5.4.3 | ||
| 4) Fungus | 5.4.3 | ||
| Electro-Magnetic Engivonement Objective: Incorporate protection that will increase the system capability to operate normally in proximity to vessel radar | 5.4.3.1 | ||
| Additional Objective Features: | 5.5.1 | ||
| 1) Slip & Skid | 5.5.1 | ||
| 2) Remote Air Data Receiver | 5.5.1 | ||
| 3) Display Dimmer Control | 5.5.1 | ||
| 4) Vertical Speed | 5.5.1 | ||
| SFI Supportability Objectives: | 5.5.2 | ||
| 1) SFI processor easily removable and replaced | 5.5.2.1 | ||
| 2) Test mode | 5.5.2.2 | ||
| 3) Built-in-Test capability | 5.5.2.3 | ||
| SFI objective: Solid state, self-contained electronic display system | 5.1.1 | ||
| SFI objective: Additional protection from: | 5.1.5 | ||
| 1) Marine environment | 5.1.5 | ||
| 2) Aircraft vibrations | 5.1.5 | ||
| 3) Electromagnetic Interference (EMI) | 5.1.5 | ||
| SFI objective: Capability of unit to interface with and display attitude and heading info in flight training simulator | 5.5.3 | ||
| SFI objective: Solid models of 3D computer-aided design STEP files of each LRU | 5.3.2 | ||
| Any quote that does not contain the objectives above will not be negatively impacted. These objectives are evaluated for above and beyond requirements and additionally desired objectives. |
&L&"-,Bold"&14ATTACHMENT 7
Sheet1
| Evaluator (Print Name) : ______________________________________________ | Date: ________________ |
| Offeror: ________________________________________________ | |
| FACTOR 1: TECHNICAL ACCEPTABILITY | Evaluation (Acceptable/Unacceptable) |
| Ability to meet first article testing schedule | |
| Ability to meet production/spares schedule | |
| Ability to meet repair schedule | |
| SFI display requirement: Height must not exceed 3.6" | |
| SFI display requirement: Width must not exceed 4.06" | |
| SFI display requirement: Depth must not exceed 10" | |
| SFI display requirement: Mounting case size must be 3 ATI standard | |
| SFI display requirement: Display does not exceed 5lbs. | |
| Weight requirement: Total system does not exceed 10lbs. | |
| Interface Control Document provided with quote | |
| SFI system requirement: Magnetic Sensor/Magnetometer | |
| SFI system requirement: Magnetic Sensor accomodates wire run of 420" if separate part number | |
| SFI system requirement: Air Data Receiver | |
| SFI system requirement: Air Data Receiver accomodates wire run of 200" if separate part number | |
| SFI system requirement: SFI Battery | |
| SFI Battery requirement: Must be TSO C179a certified, if lithium battery | |
| SFI Battery requirement: Manufacturer identified | |
| SFI Battery requirement: Must provide SFI system power for minimum of 30 minutes | |
| SFI system operates from 28 VDC source | |
| SFI system requirement: Must operate in temperature range of -20 to +55 degrees Celsius | |
| SFI MTBF not less than 3,000 flight hours of five (5) years without failure | |
| SFI Storage requirement: AVRACK space of 10" deep, 5.5" wide, and 6" high for separate part numbers (air data receiver, magnetic sensor, battery) | |
| SFI Storage requirement: Nose compartment space of 16" deep, 11" wide, and 9" high for separate part numbers (air data receiver, magnetic sensor, battery) | |
| SFI required functions: 1) Attitude (pitch and bank), 2) Magnetic Heading, 3) Barometric Altitude, 4) Air Speed | |
| SFI description requirement: Described as single unit or product of multiple part numbers | |
| SFI description requirement: Provides dimensions of all part numbers | |
| Offeror provided FAA Form 8130, EASA Form 1, or DOD equivalent air worthiness certification | |
| SFI system requirement: Must be compatible with use of Type I, Class B NVIS | |
| SFI system requirement: Must be Electromagnetic Environment tested per TSO C113a | |
| SFI system requirement: Must be capable of being configured for 2 degrees right wing down display level | |
| SFI system requirement: Ability for pitch, roll, and yaw offsets to be adjusted if SFI system is multiple part numbers | |
| SFI system requirement: Electrical connectors must comply with MIL-DTL-38999 | |
| Evaluation Rating (See attached criteria): | |
| QUOTES THAT DO NOT MEET THE REQUIREMENTS IDENTIFIED IN FACTOR 1 WILL NOT BE FURTHER CONSIDERED FOR AWARD. ONLY CONTINUE FORWARD WITH EVALUATION IF THE OFFERORS QUOTE HAS MEET ALL OF THE ABOVE REQUIREMENTS. | |
| FACTOR 2: SUSTAINMENT AND REPAIR CAPABILITY | Evaluation (Acceptable/Unacceptable) |
| Sustainment requirement: Strapping, set up, and intallation instructions for SFI system provided | |
| Sustainment requirement: Description of how SFI system will provide corossion resistance provided | |
| Repair capability requirement: Offeror must provide the repair facility location | |
| Repair capability requirement: Offeror must identify subcontractor (if applicable), location of subcontractor facility, and all subcontracted out repair capabilities | |
| Repair capability requirement: Offeror must provide FAA or DOD certification for the manufacture and repair of SFI systems | |
| Repair capability requirement: If not the OEM, must provide OEM certification for repairs in additiona to FAA/DOD certification | |
| Evaluation Rating (See attached criteria): | |
| QUOTES THAT DO NOT MEET THE REQUIREMENTS IDENTIFIED IN FACTOR 2 WILL NOT BE FURTHER CONSIDERED FOR AWARD. ONLY CONTINUE FORWARD WITH EVALUATION IF THE OFFERORS QUOTE HAS MEET ALL OF THE ABOVE REQUIREMENTS. | |
| FACTOR 3: ABILITY OF SFI TO EXCEED PHYSICAL AND FUNCTIONAL MINIMUM REQUIREMENTS | Place check mark for each objective met: |
| SFI objective: Display depth of 6" or less | |
| SFI objective: Compact, low weight unit | |
| SFI objective: SFI Battery operates for up to one (1) hour | |
| SFI objective: Temperature range of -55 to +70 degrees Celsius | |
| SFI objective: Solid state, self-contained electronic display system | |
| SFI objective: Additional protection from marine environment, aircraft vibrations, and EMI | |
| Environmental compliance objective: 1) Shock | |
| Environmental compliance objective: 2) Waterproofness | |
| Environmental compliance objective: 3) Sand and Dust | |
| Environmental compliance objective: 4) Fungus | |
| Additional Objective Features: 1) Slip & Skid | |
| Additional Objective Features: 2) Remote Air Data Receiver | |
| Additional Objective Features: 3) Display Dimmer Control | |
| Additional Objective Features: 4) Vertical Speed | |
| SFI Supportability Objectives: 1) SFI processor easily removable and replaced | |
| SFI Supportability Objectives: 2) Test mode | |
| SFI Supportability Objectives: 3) Built-in-Test capability | |
| SFI objective: Capability of unit to interface with and display attitude and heading info in flight training simulator | |
| SFI objective: Solid models of 3D computer-aided design STEP files of each LRU | |
| Number of objectives met: | |
| Evaluation Rating (See attached criteria): | |
| I certify that the evaluations provided above are compared to the factors listed and not to other submitted quotes. I have followed the established procedures identified in the Evaluation Factors and Procedures document reviewed prior to evaluating any quotes. | |
| Evaluator Signature : ______________________________________________ |
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