HSCG38-11-R-H00002 COMPLIANCE MATRIX

59 KB Posted

Attached to
C-130H Segment II (A1U) COTS Electronic Flight Display System (EFDS)
Solicitation number
HSCG38-11-R-H00002
Issued by

About this file

HSCG38-11-R-H00002 Compliance Matrix ATTACHMENT 3

Text of this file

Compliance Matrix Description SOW System/Subsystem

Specification

(SSS)

Proposal Volume and Paragraph # (To be completed by Prospective Vendors)

Requirements Verification (To be completed by Prospective Vendors)

Inspection (I) Analysis (A) Demonstration (D) Test (T)

Subsystem Technical Review 3.4.1.4

CDR Entry Criteria 3.4.1.5.1

Installation Readiness Review 3.4.1.6

Built In Test (BIT) 3.1.1

Power up BIT 3.1.1.1

CBIT 3.1.1.2

IBIT 3.1.1.3

Flight Instrument Display and Data Management

3.2

Primary Display

3.3

Attitude Direction Indicator (ADI) Data

3.3.1

Barometric Altimeter 3.3.2

Radar Altimeter (ALT- 4000) 3.3.3

Airspeed Indicator 3.3.4

Vertical Speed Indicator (VSI) 3.3.5

Heading 3.3.6

Bearing Pointer

3.3.7

Course Deviation Indicator (CDI) 3.3.8

Receiver Autonomous Integrity Monitor (RAIM)

3.3.9

Distance To Go 3.3.10

Temperature, Speed, and Wind 3.3.11

Flight Plans & Waypoint Representation

3.3.12

Vertical Flight Representation 3.3.13

RFP HSCG38-11-R-H00002

ATTACHMENT 3

Range Scaling 3.3.14

Patterns/Procedures 3.3.15

Overlays 3.3.16

Secondary Display Management 3.4

Electronic IFR Charts and Digital Moving Maps

3.5

Instrument Flight Rules (IFR) Electronic Charts

3.5.1

Digital Maps 3.5.2

ADS-B (GDL-90) 3.6

Cursor Control Devices (CCD) 3.7

Miscompare 3.8

Data Integrity 3.9

Advisory, Caution, and Warning System (ACAWS)

3.10

Control Panel Management 3.11

Computer Resources and Hardware 3.12

Memory/Processor Reserve 3.12.1

Receiver/Transmitter Address Selection

3.12.2

Interchangeability 3.12.3

Elapsed Time Indicator 3.12.4

Thermal Requirements 3.12.5

System Safety 3.13.1

Prohibited Materials 3.13.2

Personnel Safety 3.13.3

Environmental Safety 3.13.4

Electrical Power Switches 3.13.5

Low Pressure (Altitude) 3.14.1

Non-operating temperatures 3.14.2

Operating temperatures 3.14.3

Temperature Shock 3.4.14

Humidity 3.14.5

Vibration 3.14.6

Shock 3.14.7

Salt Fog 3.14.8

Fluid Contamination 3.14.9

Rapid Decompression 3.14.10

Explosive Atmosphere 3.14.11

Sand and Dust 3.14.12

Rain/Drip Proof 3.14.13

Fungus 3.14.14

Acceleration 3.15

Electromagnetic Interference and Compatibility and Electrical Power

3.16

Electromagnetic Interference Requirements

3.16.1

Electromagnetic Compatibility Requirements

3.16.2

Specific Box Level EMI Testing Requirements

3.16.3

Power Requirements 3.16.4

Communication Security and Information Security

3.17

Red-Black Data Separation 3.17.1

TEMPEST Performance 3.17.2

Reliability 3.18

Mean Time Between Failure 3.18.1

Operational Stability 3.18.2

Operational Service Life 3.18.3

Storage Life 3.18.4

Preventive Maintenance 3.19.1

Adjustments 3.19.2

Panel Lamps 3.19.3

Peculiar Support Equipment 3.19.4

Organizational Level Maintenance 3.19.5

Packaging 3.19.6

Training and Intuitive Design 3.20.1

Design for Maintainer 3.20.2

Environment 3.20.3

Controls and Displays 3.20.4

Luminance 3.20.5.1

Night Vision Imaging System Compatibility (NVIS)

3.20.5.2

Flight Equipment Compatibility 3.20.5.3

NVIS Compatibility 3.20.6.1

Daylight Readability 3.20.6.2

Display Luminance 3.20.6.3

Advisories, Cautions, and Warnings 3.20.6.4

Other files

On GovTribe

Work with this file

  • Download the original file
  • Contacts named in this file
  • Similar government files
  • Ask GovTribe AI about this file

File details come from the government source that posted it. Updated .