HSCG38-16-Q-200052_-_Attachment_5_-_Technical_Acceptability_Compliance_Matrix_(Amended).xls
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- HSCG38-16-Q-200052
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HSCG38-16-Q-200052 - Attachment 5 - Technical Acceptability 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 | |
| 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_7_-_SFI_Objective_Capabilities_Compliance_Matrix.xls | XLS spreadsheet | |
| 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 2
| HSCG38-16-Q-200052 Technical Acceptability 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 | ||
| Requirement: | SOW Reference: | Compliant? (Yes or No) | Technical Quote Page Reference |
| Offeror compliant with FAA Form 8130, EASA Form 1, or DOD equivalent air worthiness certification | 3.5.1 | ||
| SFI system requirement: Must be compatible with use of Type I, Class B NVIS | 3.5.2 | ||
| SFI system requirement: New wiring must conform to SAE AS50881, Rev. D; Wiring maintenance/repair shall conform to NAVAIR 01-1A-505 series; General aircraft wiring shall be IAW NEMA publication WC 27500; kapton wiring SHALL NOT be used. | 3.4.3 | ||
| SFI system requirement: SFI must meet the requirements of FAA TSO C113a | 5.1 | ||
| SFI system requirement: SFI must meet requirements of Federal Aviation Regulation 29, Appendix B | 5.1.2 | ||
| SFI description requirement: Described as single unit or product of multiple part numbers | 5.1.6 | ||
| Strapping, set up, and intallation instructions for SFI system provided | 5.1.6 | ||
| SFI description requirement: Provides dimensions of all part numbers | 5.2 | ||
| SFI display requirement: Height must not exceed 3.6" | 5.3.3.1 | ||
| SFI display requirement: Width must not exceed 4.06" | 5.3.3.1 | ||
| SFI display requirement: Depth must not exceed 10" | 5.3.3.1 | ||
| SFI display requirement: Mounting case size must be 3 ATI standard | 5.3.3.1 | ||
| SFI system requirement: Must be capable of being configured for 2 degrees right wing down display level | 5.3.3.1.1 | ||
| SFI system requirement: Ability for pitch, roll, and yaw offsets to be adjusted if SFI system is multiple part numbers | 5.3.3.1.2 | ||
| SFI system requirement: Magnetic Sensor/Magnetometer | 5.3.4 | ||
| SFI system requirement: Magnetic Sensor accomodates wire run of 420" if separate part number | 5.3.4 | ||
| SFI system requirement: Air Data Receiver | 5.3.5 | ||
| SFI system requirement: Air Data Receiver accomodates wire run of 200" if separate part number | 5.3.5 | ||
| SFI system requirement: SFI Battery | 5.3.6 | ||
| SFI system operates from 28 VDC source | 5.3.6 | ||
| SFI Battery requirement: Must be TSO C179a certified, if lithium battery | 5.3.6.1 | ||
| SFI Battery requirement: Must provide SFI system power for minimum of 30 minutes | 5.3.6.1 | ||
| SFI Battery requirement: Manufacturer identified | 5.3.6.2 | ||
| SFI system contains the following required functions: | 5.4.1 | ||
| 1) Attitude (pitch and bank) | 5.4.1 | ||
| 2) Magnetic Heading | 5.4.1 | ||
| 3) Barometric Altitude | 5.4.1 | ||
| 4) Air Speed | 5.4.1 | ||
| SFI system requirement: Must operate in temperature range of -20 to +50 degrees Celsius | 5.4.2 | ||
| SFI system requirement: Must be Electromagnetic Environment tested per TSO C113a | 5.4.3.1 | ||
| Description of how SFI system will provide corossion resistance provided | 5.4.3.2 | ||
| SFI display requirement: Display does not exceed 5lbs. | 5.4.4.1 | ||
| Weight requirement: Total system does not exceed 10lbs. | 5.4.4.1 | ||
| SFI Storage requirement: AVRACK space of 10" deep, 5.5" wide, and 6" high for separate part numbers (air data receiver, magnetic sensor, battery) | 5.4.4.2 | ||
| SFI Storage requirement: Nose compartment space of 16" deep, 11" wide, and 9" high for separate part numbers (air data receiver, magnetic sensor, battery) | 5.4.4.2 | ||
| SFI MTBF not less than 3,000 flight hours or five (5) years without failure | 5.5.2.4 | ||
| SFI system requirement: Electrical connectors must comply with MIL-DTL-38999 | 5.5.2.5 | ||
| Ability to meet first article testing schedule | 16.1 | ||
| Ability to meet production/spares schedule | 16.1 | ||
| QUOTES THAT DO NOT MEET THE REQUIREMENTS IDENTIFIED ABOVE WILL NOT BE CONSIDERED FOR AWARD. |
&L&"-,Bold"&14Attachment 5
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