Appendix 1 SRD Cross Reference 13Oct22.xlsx
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- AN/TRN-41 MP TACAN Replacement Federal contract opportunity
- Solicitation number
- FA8102-23-R-2000
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Sheet1
| Section L, Appendix 1- SRD as of 10/13/22 | ||||
| (Subfactor One SRD minimum threshold requirements) | ||||
| No. | Description | Requirement | Threshold | |
| (T) | Compliant | |||
| (Y) | Non- |
Compliant (N)
| SYSTEM FUNCTIONAL REQUIREMENTS | |||
| EINT-1 | External Power | a. | The system shall operate utilizing 100-250 VAC, 48-62Hz, single phase power. |
| b. | The system shall be compatible (mating connector is readily available commercially) with multiple types of power sources to include (but not limited to): Commercial power, solar power, generator power, and battery power. | |||
| T | ||||
| EINT-2 | Very High Frequency Omni-Directional Range (VOR) Compatibility | The system shall be compatible with VOR systems to include ID synchronization. | T | |
| EINT-3 | Worldwide Deployability | a. | The system shall be capable of setup and operations in worldwide austere locations in all course-grained and fine-grained soil conditions as defined in TM 3-34.43, Materials Testing, App B, Unified Soil Classification System without requiring permanent foundations (e.g., concrete, cement, etc.). |
| b. | The system shall be capable of setup and operation on permanent foundations (e.g., concrete, cement, etc.) in which no anchors or tie-downs are available. | ||
| T | |||
| EINT-4 | Airborne TACAN | ||
| Equipment | System shall be compatible with all airborne TACAN interrogators/transponders currently in use. | T | |
| SYSTEM INTERNAL INTERFACE REQUIREMENTS | |||
| IINT-1 | Battery Power | a. Interchangeable and rechargeable battery packs shall be included as part of each system. |
b. Each system shall include 1 battery pack that will be included into size, weight and carry considerations for the system and 2 spare battery packs that will be excluded from these considerations.
c. While the system is powered by an external power source and operational, the batteries shall be recharged.
d. System shall operate using VDC power for a minimum of 5 hours on the included battery pack at 0°C.
e. Batteries shall be capable of being recharged external to the system from any of the external power sources listed in EINT-1.
| T | |||
| IINT-2 | Communication with RCSU | a. | Remote Control Status Unit (RCSU) shall be capable of wireless and wired connectivity (connections/interface only). |
b. RCSU shall connect and properly communicate locally at the TACAN as well as from a distance of at least 10,000 feet from the TACAN location using twisted pair copper wire.
c. All wire needed to make the connection with the RCSU shall be provided by the contractor along with system delivery.
| T | |||
| ENVIRONMENTAL, SAFETY, AND OPERATIONAL HEALTH (ESOH) REQUIREMENTS. | |||
| ESOH-1 | HAZMAT | The use of toxic chemicals, hazardous substances, or ozone depleting chemicals (ODCs) shall be avoided, whenever feasible. EPA Title III, List of Lists, EPA 550-B-21-001, provides a listing of toxic chemicals to be avoided. | T |
| ESOH-2 | MSDS | The supplier shall provide copies of Material Safety Data Sheets (MSDS) for all hazardous or toxic materials being supplied at least 120 days prior to the first delivery. | T |
| ESOH-3 | Preferred Materials | Recycled, recovered, or environmentally preferable materials shall be used to the maximum extent possible provided that the material meets or exceeds the operational and maintenance requirements, and promotes economically advantageous life cycle costs. | T |
| ESOH-4 | OSHA | System shall comply with all OSHA requirements per AFMAN 91-203. | T |
| ESOH-5 | NFPA-70 (NEC) | All electrical systems shall comply with the National Electrical Code (NEC). | T |
| ESOH-6 | Grounding Protection | a. | System shall meet the requirements of MIL-STD- 188-124B for grounding, bonding, and shielding though the government will be responsible for providing the appropriate ground rod for the delivered systems. |
b. System shall meet the requirements of NFPA-77 for static electricity.
Note: The contractor shall appropriately ground the system for all testing performed at contractor facilities.
| T | |||
| ESOH-7 | System Safety | The TACAN system shall meet the requirements of MIL-STD-882E, Section 4. | |
| T | |||
| ESOH-8 | Internal Chassis Ground | A ground terminal or equivalent function shall be provided on all TACAN system Line Replaceable Units (LRUs) within the equipment. The ground terminal shall be located on the input power connector or on the equipment terminal board and shall connect to the internal chassis by means of conductors at least equal in size to one of the power input conductors. Safety grounding within the equipment shall terminate on the ground terminal. Grounds and AC return lines shall be separated. | T |
| ESOH-9 | External Chassis Ground | A ground conductor shall be included with the TACAN system power conductors and shall connect to the ground terminal of individual units when power is routed externally between individual units of the equipment. | T |
| ESOH-10 | Safety Shielding | System protective shields shall be provided to protect personnel from accidental contact with parts in excess of 30V RMS or 30V DC during operation or maintenance actions. | T |
| ESOH-11 | Electromagnetic Radiation Hazards | a. Hazard of Electromagnetic Radiation to Ordinance (HERO) safe separation distances shall be determined and documented for the TACAN in accordance with MIL-STD-464D Appendix A, paragraph A.5.9.3. |
b. Hazard of Electromagnetic Radiation to People (HERP) safe separation distances shall be determined and documented for the TACAN in accordance with MIL-STD-464D, Appendix A, paragraph A.5.9.1.
c. Hazard of Electromagnetic Radiation to Fuel (HERF) safe separation distances shall be determined and documented for the TACAN in accordance with MIL-STD-464D, Appendix A, paragraph A.5.9.2.
| T | |||
| SECURITY AND PRIVACY REQUIREMENTS | |||
| SEC-1 | Operating System | The operating system for all computers shall be fully compatible and required to run on the current Security Technical Implementation Guide (STIG) version from Defense Information Systems Agency’s (DISA). | |
| T | |||
| SEC-2 | Highly Secure | a. | For Windows based devices, computers and software shall meet the standards for a highly secure environment published by Microsoft which lists the minimum hardware and software requirements at: https://docs.microsoft.com/en- us/windows-hardware/design/device- experiences/oem-highly-secure. |
| b. | For Linux devices, computers and software shall meet the following standards: | |||
| • | Confirm SeLinux is enabled. | |||
| • | Operating in enforcing mode. | |||
| • | A targeted policy is being used. | |||
| • | Reference: https://access.redhat.com/documentation/en- us/red_hat_enterprise_linux/7/html/selinux_ users_and_administrators_guide/index | |||
| T | ||||
| SEC-3 | BitLocker | All computers and software shall function with BitLocker (or equivalent) encryption enabled. | T | |
| SEC-4 | Encryption Level | All remote connections between the TACAN and the RCSU shall meet AES 256-bit or higher-level encryption. | T | |
| SEC-5 | Network | The RCSU connection to the TACAN shall function as a stand-alone network only. No external network connections shall be required for system operation. Bluetooth and Wireless Fidelity (Wi-Fi) enabled mobile device connections are prohibited. | T | |
| SEC-6 | User Level Control | a. | Any maintenance software shall include user Identification (ID) and password controls to prevent unauthorized access. |
| b. | System/User accounts shall have a minimum of three tiers of access (one allowing viewing status only, one allowing full maintenance functionality and one with administrative access that allows all functionality and assigning of usernames and passwords). | ||
| T | |||
| SEC-7 | Password Complexity | All passwords shall meet the below minimum requirements: |
a. Be at least 14 characters in length.
b. Must contain at least 1 uppercase, 1 lowercase, 1 number, and 1 special character (~!@#$%^&*_-
c. May not contain the account name associated with the password.
d. May not contain more than 2 consecutive characters.
| e. | Password complexity filter must be enabled to disallow use of passwords not meeting these requirements. | |
| T | ||
| SYSTEM ENVIRONMENT REQUIREMENTS | ||
| ENV-1 | CBRNE | |
| Survivability, Decontamination | a. | Decontamination of the system shall not cause the system to become inoperable (system is assumed to be off air during decontamination) and shall not induce any safety hazards. |
| b. | The system shall continue to operate when exposed to an environment of chemical and biological contamination. | |||
| T | ||||
| ENV-2 | Temperature | a. | Operating: -40°C to +71°C. |
b. Non-operating (outdoor): -40°C to +71°C.
| c. | Non-operating (indoor)/Storage/Transport: -40°C to +71°C. | |||
| T | ||||
| ENV-3 | Temperature Shock | a. | Non-Operating: -40°C to +24°C and +18°C to +71°C. |
| b. | Storage/Transport: -40°C to +71°C. | |||
| T | ||||
| ENV-4 | Relative Humidity | Operating/Non-Operating: 5 to 100% with ambient temperatures above 27°C, maximum dew point of 27°C, including condensation due to temperature change. | T | |
| ENV-5 | Altitude | a. | Operating/Non-Operating: Sea level to 13,100 feet (3.1 km). |
| b. | Storage/Transport: Sea level to 45,900 feet (12.2 km), | |||
| T | ||||
| ENV-6 | Rapid | |||
| Decompression | No safety hazard resulting from rapid decompression from 8,000 ft to 40,000 ft in less than 15 s. | T | ||
| ENV-7 | Wind and Ice | Operating/Non-Operating: 50 mph (43 knots) steady state and 71 mph (62 knots) gusts with no ice and with ½-in glaze ice mix (in accordance with MIL-HDBK-310 for 1% location at 3m (10 ft) off the ground). | T | |
| ENV-8 | Snow | Up to 50 pounds per square foot on all horizontal surfaces (in accordance with MIL-HDBK-310 for “semi-permanent equipment”). | T | |
| ENV-9 | Solar Radiation and UV | |||
| Resistance | External surfaces and materials, including cables, shall be resistant to the effects of solar radiation at a rate of 1120 W/m2. | T | ||
| ENV-10 | Sand and Dust | a. Blowing Sand: |
- Concentration: 0.18 g/m3, -0.0/+0.2 g/m3.
| - | Particle Size: 150 to 850 μm. |
| - | Air Velocity: 18 m/s. |
b. Blowing Dust:
| - | Concentration: 10.6 ±7 g/m3. | |||
| - | Particle Size: <149 μm. | |||
| - | Air Velocity: 8.9 ± 1.3 m/s. | |||
| T | ||||
| ENV-11 | Salt Atmosphere | Withstand exposure to a salt fog atmosphere with a salt concentration of at least 5%. | T | |
| ENV-12 | Fungus | Show no signs of fungal growth after prolonged exposure to fungus growth as encountered in tropical climates. | T | |
| ENV-13 | Rain | 1.2 inches/hour (in accordance with MIL-HDBK-310 for the 0.5% frequency of occurrence for rainfall). | T | |
| ENV-14 | Shock | a. | When packaged for transport, withstand the loading and unloading from vehicles, aircraft, rail, and ship without suffering damage. |
| b. | Operate without malfunction or performance degradation following exposure to the shock environment encountered during transit drops to the extent of the package size and weight. | |||
| T | ||||
| ENV-15 | Vibration | When transported via fixed-wing and rotary wing aircraft, ocean-going ship, rail, and ground vehicles operating in Type IV and Type V as defined in SAE 8090A mobility conditions, or a combination of these conditions, the system shall withstand the vibration encountered with no damage. | T | |
| COMPUTER RESOURCE REQUIREMENTS | ||||
| COMP-1 | Computer Hardware | The Contractor shall determine and configure specific computer hardware in order to meet the performance requirements below for a STIG compliant operating system and installed contractor software. |
a. Average computer boot/re-boot times less than 2 minutes.
| b. | Response times average less than 2 seconds. | |||
| T | ||||
| REMOTE MAINTENANCE MONITORING REQUIREMENTS | ||||
| RMM-1 | Maintenance Status | a. | All system parameters required for maintenance and monitoring actions shall be available at the TACAN site. |
b. The communicated data shall be displayed in the correct engineering units requiring no conversion by the technician.
c. Units of monitored electronic parameters shall follow the International Standard (SI) convention.
| d. | Units for monitored non-electronic parameters shall be available in the English Standard. | |||
| T | ||||
| RMM-2 | Remote Monitoring & Maintenance (RMM) | a. | System shall include a Remote Control and Status Unit (RCSU). |
| b. | RCSU shall remotely monitor status of the system and provide reset capability as a minimum. | |||
| T | ||||
| RMM-3 | Fault Isolation | a. | The equipment shall be provided with enough self- diagnostics tools to troubleshoot the equipment down to each specific LRU. |
| b. | At least 95% of all detected faults shall be isolated to one LRU. | |||
| T | ||||
| RMM-4 | Frequency of Diagnostics | a. | System shall perform diagnostics that identifies issues and potential problems and shall store this information per RMM-9. |
b. Diagnostics shall be performed at start-up and then periodically (≤ every 90 seconds).
| c. | The Remote Monitoring and Maintenance (RMM) equipment shall have self-diagnosis ability to identify faults within the software subsystem. | |||
| T | ||||
| RMM-5 | System Information Availability | System shall provide all information “Real Time” as it pertains to site ID, system status, system configuration, equipment settings, equipment status (ON/OFF), equipment performance and parameters, and test results. | T | |
| RMM-6 | Alarm Information | System shall provide information “Real Time” as it pertains to alarm conditions (ON/OFF), alarm status (Enabled/Disabled) and alarm thresholds. | T | |
| RMM-7 | Alarm & Fault Control | System shall provide “Real Time” control and feedback as it pertains to all alarm activation and threshold adjustment, alarm bypass, alarm response, alarm reset, fault limit settings, fault conditions, fault checks, and fault reset. | T | |
| RMM-8 | Fault Information | a. | System shall provide all information “Real Time” as it pertains to fault conditions and fault limits. |
| b. | Fault limits shall be differentiated by Green (operational/online), Yellow (degraded), and Red (failure/offline). | |||
| T | ||||
| RMM-9 | Archived Information | a. | System shall provide historical data on fault conditions, alarms, and maintenance actions. |
b. A minimum of 96 hours of historical shall be available (e.g. Error on Friday available for viewing on Monday).
c. This data shall be stored with the system.
| d. The contractor shall provide the equipment to access this data. | T | |||
| RMM-10 | Real Time Clock | The clock/calendar shall be adjustable for initial setup as well as to ensure accuracy later. | T | |
| RMM-11 | Master Reset/Startup | System software shall have a master reset/startup and a master shutdown function to start or stop TACAN operation locally and remotely. | T | |
| RMM-12 | Default Parameters | The system and its software shall maximize the use of default parameters in an effort to minimize user required input for initial setup. | T | |
| RMM-13 | Messages | a. | A priority alarm message shall be generated when a failure occurs within a TACAN subsystem which causes a loss of service to the user (i.e. shutdown). |
b. Non-priority messages shall be generated to alert for either fault or alert conditions.
| c. | All alarm notifications shall also be transmitted to a RCSU. | |||
| T | ||||
| RMM-14 | Non-Volatility | All control settings, operational parameters and limits, initialization data, data files and fault history shall be stored locally with enough power backup capacity to ensure non-volatility. | T | |
| RMM-15 | Software/RCSU Failure | a. | Failures within the software subsystem shall not degrade the capability of the TACAN to provide signal in space (azimuth/bearing) information. |
| b. | Failures of the RCSU or its connections shall not degrade the capability of the TACAN to provide signal in space (azimuth/bearing) information. | ||
| T | |||
| RMM-16 | Continuous Monitoring | System shall provide continuous monitoring of critical parameters and cause shutdown of the system in the event any one of the parameters fall outside of its specified tolerance. This requirement shall be met for both internally caused failures (e.g. LRU fault) and externally caused failures (e.g. shift of tripod). |
Note: Critical parameters shall be any parameter that contributes to the radiated signal including the azimuth/bearing, Distance Measuring Equipment (DME) signal and Identification (ID) information.
| T | ||
| SYSTEM QUALITY FACTORS | ||
| QLT-1 | Signal-in- Space | Provided equipment shall emit, as a minimum, the appropriate TACAN signal per MIL-STD-291C and ICAO Annex 10, Volume 1, Attachment C, Figure C-20 with the following exceptions due to a system operating with a short aperture antenna: |
| a. | Harmonic content of 15 Hz modulation component (0° to +6° elevation) |
| 1. | Root Mean Square (RMS) sum of 2nd through 6th harmonics: ≤ 30%. |
| 2. | RMS sum of 7th through 11th harmonics (except 9th harmonic): ≤ 25%. |
| 3. | Individual amplitude of 7th through 11th harmonics (except 9th harmonic): < 30%. |
| b. | Harmonic content of 135 Hz modulation component (0° to +6° elevation) |
| 1. | RMS sum of 2nd through 6th harmonics: < 15%. |
| c. | 15 Hz modulation |
| 1. | 21% ±9% modulation from -2° to +10° elevation. |
| 2. | ≥ 5% modulation from +10° to +30° elevation. |
| d. | 135 Hz modulation | |||
| 1. | 12% to 36% modulation from -2° to +10° elevation | |||
| 2. | ≥ 5% modulation from +10° to + 25° elevation. | |||
| T | ||||
| QLT-2 (KPP) | Flight Check | System shall pass a FAA flight check per FAA Order 8200.1D or ICAO with a satisfactory rating. | T | |
| QLT-3 | Reply Efficiency | The system shall provide identification, distance measurement and azimuth information to at least 100 aircraft simultaneously with 80% reply rate in X-mode and 75% reply rate in Y-mode to interrogating aircraft transponders with a receive signal level of -90dBm. The TACAN system shall be capable of “On Request Mode” of operation. | T | |
| QLT-4 | Capacity | System shall be capable of fully supporting at least 100 aircraft simultaneously and providing azimuth and identity information to an unlimited number of aircraft. | T | |
| QLT-5 | Transmitter Power Out | a. | The system shall be capable of transmitting enough watts RF peak power to reach a distance of 75 nm at 0.5 degree while adhering to MIL-STD-291C and ICAO Annex 10. |
| b. | The TACAN transmitter shall be adjustable to lower power settings to include as a minimum a 50% power setting. | |||
| T | ||||
| QLT-6 | Lock-on | Continuous lock-on (azimuth and distance measurement) for 15 nautical miles within plus or minus 5 degrees or less of the approach course. | T | |
| QLT-7 | Standby Mode of Operation | a. | Standby condition until interrogated by the using aircraft. |
| b. | When interrogation occurs, full power should automatically be transmitted within 60 seconds. | |||
| T | ||||
| QLT-8 | Course Alignment | Within plus or minus 3.5 degrees of the correct magnetic bearing with the exception of the approach courses which will be within plus or minus 2.5 degrees. | T | |
| QLT-9 | Radial | |||
| Roughness and Scalloping | The radial roughness and scalloping will be within plus or minus 4.0 degrees of the radial. | T | ||
| QLT-10 | Radial Course Bends | The radial course bends will be within plus or minus 4.0 degrees of the correct magnetic bearing. | T | |
| QLT-11 | Polarization Effect | The polarization effect will be within plus or minus 4.0 degrees. | T | |
| QLT-12 | Unlock | No more than one condition of azimuth and/or distance measurement unlock of not more than two search cycles will be permissible in any five nautical miles of radial flight with a ground speed of 150 knots. | T | |
| QLT-13 | Power Spectrum | Output power spectrum shall meet FAA, ICAO and MIL-STD-291C requirements at maximum output per FAA Advisory Circular 00-31A. | T | |
| QLT-14 | TACAN | |||
| Antenna Performance | The MP TACAN antenna shall provide performance equal to or better than the following: |
a. Frequency Range: 962 to 1213 MHz (transmit); 1025 to 1150 MHz (receive).
b. Channels: 1X through 126X; 1Y through 126Y.
c. VSWR: 962 MHz to 1213 MHz less than 2.0 to 1.
d. Gain (peak): +3.0 dBi (main lobe); -1.0 dBi (horizon).
e. Energy radiated below horizon: < 25% of total radiated energy.
| f. | The peak signal occurs between +15° and +35° above the horizon (main lobe). | |||
| T | ||||
| QLT-15 | Mean-Time- To-Repair | |||
| (MTTR) | The MTTR for the system and all major subsystems shall be 30 minutes or less at field level. | T | ||
| QLT-16 | Maximum | |||
| Time to Repair (MaxTTR) | The MaxTTR for the system and all major subsystems shall be ≤ 1.5 hours to the 95th percentile at field level. | T | ||
| QLT-17 | Mean-Time- | |||
| Between Failure (MTBF) | The MTBF for the system and all major subsystems shall be greater than or equal to 10,000 hrs. | T | ||
| QLT-18 | Service Life | All requirements stated within this specification shall be maintainable over the minimum expected service life of 20 years. | T | |
| DESIGN AND CONSTRUCTION CONSTRAINTS | ||||
| DES-1 | Anchoring | System shall be equipped (or come with) an anchoring system that will anchor the system in the environmental conditions presented in Para 3.9 and in locations as presented in Para EINT-3 (worldwide deployability). | T | |
| DES-2 | Transport-ability to Include: Low Velocity Airdrop (LVAD) and 463L pallet requirement | a. | When packaged for transport, withstand Low Velocity Airdrop from an altitude not to exceed 1000 feet and operate without malfunction or performance degradation in accordance with AFMAN 11-231. |
| b. | When packaged for transport, the combined envelope of the complete system (Antenna Kit, Beacon Transponder Kit, RCSU Kit, and Assembly System Kit) shall not exceed the usable dimensions of one 463L pallet. | |||
| T | ||||
| DES-3 | Adjustments | System shall require no adjustments subsequent to being placed in operation and all tuning controls utilized prior to deployment will include locking devices to hold the control firmly in place once it is set. | T | |
| DES-4 | TACAN |
Antenna Type
a. System shall include a mechanically or electronically scanned antenna with a scanning speed of 900 RPM ±0.015%.
| b. | The Antenna shall include a support stand capable of adjustment from 3 feet to 5 feet. | |||
| T | ||||
| DES-5 | Electrostatic Discharge (ESD) | Identification markings including ESD warning labels shall be affixed on all ESD-sensitive subassemblies to be visible to maintenance personnel prior to maintenance handling of the equipment. Enclosures, assemblies, and subassemblies containing class 1 or class 2 ESD sensitive components (as defined by ANSI/ESD S20.20-2021), shall be appropriately marked using the documentation in ANSI/ESD S20.20-2021 as an example. | T | |
| DES-6 | Internal Wiring | To the maximum extent possible, all multi-conductor wiring and cable design shall follow the guidelines of MIL-HDBK-454C, Guideline 66. | T | |
| DES-7 | Workmanship | General workmanship acceptance criteria shall be based on best commercial practice. The contractor’s workmanship practices will be evaluated based on MIL-HDBK-454C, Guidelines 1, 5, 9 and 15 and USAF Technical Manual T.O. 00-25-234. | T | |
| DES-8 | Commercial Standards | A listing of the contractor’s “best commercial standards” shall be provided to the Government that includes all the standards to which the equipment was designed to (or referenced during the design). These standards shall be physically or electronically be available for review by the Government minimally at the supplier’s facility. | T | |
| DES-9 | Controls and | |||
| Indicators | System equipment controls and indicators shall be designed in accordance with MIL-STD-1472H. | T | ||
| DES-10 | Electromagnetic Environment | System shall meet its operational performance requirements in its intended operational Electromagnetic Environment (EME) without causing or suffering any unacceptable performance degradation due to unintentional Electromagnetic Interference (EMI) to or from other equipment in the same environment. | T | |
| DES-11 | Corrosion Protection | System shall have a corrosion protection finish preferably in a desert tan color (other subdued colors acceptable). | T | |
| PERSONNEL-RELATED REQUIREMENTS. | ||||
| PER-1 (KPP) | Portability | a. | The system components shall comply with the lift and carry criteria defined in Section 5.20.2 of MIL-STD-1472H. |
b. The weight of the components shall accommodate the Low Body Weight criteria stated in Paragraph 5.20.2.3.5.2.3 of MIL-STD-1472H both in and outside of the transport cases with 2 person lifts allowed.
c. The system (with the transport cases) shall be transportable across all terrain types for a distance of up to 1.25 miles by no more than 2 persons in 2 trips. Shall include soft carrying case with carrying handles and/or with adjustable straps
| d. For system components which do not meet the portability requirements (shown above in bullets a-c), transport aids (e.g. carts with run-flat all-terrain tires) are an acceptable means to support them and shall be provided with each system. Any transportation aid will be included total system envelope of one 463L pallet | T | ||
| PER-2 | Set Up | The TACAN system design and construction shall permit setup, leveling, aligning, and operational ready to transmit ready for flight inspection in no more than 75 minutes by two trained and qualified Radar, Airfield, and Weather Systems (1C853, 5-skill level, Journeyman) personnel. |
Note: Set up time does not include personnel wearing Mission Oriented Protective Posture (MOPP) Level 4 attire.
| T | |||
| PER-3 | Mission Oriented Protective Posture (MOPP) | The system shall be able to be set up, maintained in the field, and operated by personnel wearing MOPP Level 4 attire. | T |
| LOGISTICS-RELATED REQUIREMENTS | |||
| LOG-1 | Support/Test Equipment | a. | Unique support and test equipment shall not be required unless analysis determines that no common equipment exists that can perform the function. |
b. Any unique equipment as well as basic COTS/NDI equipment that is to be used for field level maintenance shall be identified and provided with each system.
Note: Unique equipment would include any equipment that is unique to the system being provided and is not readily available for purchase in the commercial marketplace from multiple vendors.
| T | |||
| PACKAGING REQUIREMENTS | |||
| PAK-1 | Identification Plates//Labels/ Markings | a. | Identification plates, labels or markings shall be located in conspicuous spaces on all assemblies, LRUs, external cables and all other components, exceptions shall be noted. |
b. Plates/labels/markings shall provide the necessary information to uniquely identify the unit or subassembly and IAW MIL-STD-130N.
| c. | I.D. marking plates/labels/markings shall be durable and legible over the intended service life of the equipment. | |||
| T | ||||
| PAK-2 | Packaging | Packaging of systems, subsystems and LRUs for delivery to the government shall be per MIL-STD- 2073-1E Change 4. | T | |
| PAK-3 | Marking of Packaging | Marking of packaging shall be in accordance with MIL-STD-129R Change 2. | T | |
| CERTIFICATION REQUIREMENTS | ||||
| CERT-1 | Spectrum Management | System spectrum management and use shall be in accordance with DoDI 4650.01, Policy and Procedures for Management and Use of the Electromagnetic Spectrum. | T | |
| CERT-2 | Spectral Emissions | System emission spectra shall conform to the applicable sections of the National Telecommunication and Information Administration (NTIA) Manual of Regulations and Procedures for Federal Radio Frequency Management (Redbook). | T | |
| CERT-3 | Certification | Spectrum dependent system equipment shall be capable of: | ||
| a. | Receiving an approved stage 3 Defense Department (DD) Form 1494 thru the NTIA spectrum supportability certification process in support of system testing. |
b. Receiving a frequency assignment, in support of system testing, thru the NTIA spectrum supportability
c. Receiving an approved stage 3 Defense Department (DD) Form 1494 thru the NTIA spectrum supportability certification process in support of system testing.
d. Receiving a frequency assignment, in support of system testing, thru the NTIA spectrum supportability certification process.
e. Receiving an approved stage 4 DD Form 1494 thru the NTIA spectrum supportability certification process in support of operational activities.
| f. | Receiving a frequency assignment, in support of operational activities, thru the NTIA spectrum supportability certification process. | |
| T | ||
| CERT-4 | EMI/EMC | |
| Compliance | System shall be certified to applicable EMI/Electromagnetic Compatibility (EMC) requirements of either MIL-STD-461G, EN55032/EN55024, or equivalent commercial EMI/EMC standard. | T |
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