DAR 400 Follow On SOW With Appendices_Sep 2026.pdf

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CUI

Controlled by: Air Force Material Command Controlled by: AFLCMC/HBSD CUI Category: Controlled Technical Information/Export Controlled Distribution/Dissemination: D POC: Andrew Mathias, Comm: (405) 739‐8417 Exported: 3 April 2024

ID : AF SS_19439

Object Number : 0-1

UNCLASSIFIED

Government E‐3G Requirements Baseline

E‐3G System Set

Number: 888‐16001

Revision: H

Release Date: 1 Apr 24

CAGE CODE: 98752

AFLCMC/HBSD

3001 Staff Drive

2AG1 98C

Tinker AFB, OK 73165

Distribution Statement D: Distribution authorized to the Department of Defense and U.S. DoD contractors only: ( Critical Technology) (17 April 2013). Other requests shall be referred to

AFLCMC/HBSB.

WARNING

This document contains technical data whose export is restricted by the Arms Export Control Act (Title

22, U.S.C. SEC 2751, et seq.), or the Export Administration Act of 1979 (Title 50, U.S.C., App. 2401 et seq.), as amended. Violations of these export laws are subject to severe criminal penalties.

Disseminate in accordance with provisions of DoD Directive 5230.25.

DESTRUCTION NOTICE: For classified and unclassified documents, follow the procedures in the most recently published National Industrial Security Program Operating Manual (NISPOM), DoD 5220.22‐M and the appropriate Program Security Guidance.

ID : AF SS_1

Object Number : 1

1 (U) SCOPE

ID : AF SS_6

Object Number : 2

2 (U) APPLICABLE DOCUMENTS

ID : AF SS_12755

Object Number : 2.0-10

(U) MIL‐STD‐130K, Identification Marking of U.S. Military Property, 15 January 2000

In‐links (All modules) : Module Name:/DMS 4 Data at Rest ‐DaR 40‐45 Enterprise /Block 40 45 Enterprise

DMS 4 Data at Rest ‐DaR

Object Identifier:DaR_121

Object Heading:

Object Text:(U) The 4045 DaR Type 1 Encryptor shall conform to MIL‐STD‐130K, Identification Marking of

U.S. Military Property, 15 January 2000

ID : AF SS_12731

Object Number : 2.0-12

(U) MIL‐HDBK‐217F, Notice 2, Reliability Prediction of Electronic Equipment, 28 February 1995

(TRDp_2829)

In‐links (All modules) : Module Name:/DMS 4 Data at Rest ‐DaR 40‐45 Enterprise /Block 40 45 Enterprise

Object Identifier:DaR_122

Object Text:(U) The 4045 DaR Type 1 Encryptor shall conform to MIL‐HDBK‐217F, Notice 2, Reliability

Prediction of Electronic Equipment, 28 February 1995 (TRDp_2829)

Module Name:/Prd_SIC_final_A010_8‐29‐14/TRD/SIC TRD_PR

Object Identifier:TRDp_2829

Object Text:(U) MIL‐HDBK‐217F, Notice 2, Reliability Prediction of Electronic Equipment, 28 February

ID : AF SS_12732

Object Number : 2.0-14

(U) MIL‐HDBK‐472, Notice 1, Maintainability Prediction, 12 January 1984 (TRDp_2827)

In‐links (All modules) : Module Name:/DMS 4 Data at Rest ‐DaR 40‐45 Enterprise /Block 40 45 Enterprise

Object Identifier:DaR_123

Object Text:(U) The 4045 DaR Type 1 Encryptor shall conform to MIL‐HDBK‐472, Notice 1, Maintainability Prediction, 12 January 1984 (TRDp_2827)

Object Identifier:TRDp_2827

Object Text:(U) MIL‐HDBK‐472, Notice 1, Maintainability Prediction, 12 January 1984

ID : AF SS_12743

Object Number : 2.0-15

(U) MIL‐HDBK‐454A, General Guidelines for Electronic Equipment, 03 November 2000

In‐links (All modules) : Module Name:/DMS 4 Data at Rest ‐DaR 40‐45 Enterprise /Block 40 45 Enterprise

Object Identifier:DaR_124

Object Text:(U) The 4045 DaR Type 1 Encryptor shall conform to MIL‐HDBK‐454A, General Guidelines for

Electronic Equipment, 03 November 2000

ID : AF SS_12742

Object Number : 2.0-16

(U) MIL‐STD‐461E, Requirements for the Control of Electromagnetic Interference Characteristics of

Subsystems and Equipment, 20 August 1999 (TRDp_2836)

In‐links (All modules) : Module Name:/DMS 4 Data at Rest ‐DaR 40‐45 Enterprise /Block 40 45 Enterprise

Object Identifier:DaR_125

Object Text:(U) The 4045 DaR Type 1 Encryptor shall conform to MIL‐STD‐461E, Requirements for the

Control of Electromagnetic Interference Characteristics of Subsystems and Equipment, 20 August 1999

(TRDp_2836)

Module Name:/Mode 5 AWACS Non‐Dragon 2020‐05‐27/0 ‐ Program/SRD_Mode 5_SIGNED

Final_07Mar2019

Object Identifier:SRD‐367

Object Text:The M5Ll IFF system shall(l) comply with AFI 17‐220 to be supportable in the electromagnetic spectrum and to be interoperable with civil CNS/ATM systems in order to accomplish the aircraft mission and comply with the intent of applicable civil standards.

Module Name:/Mode 5_Archived off 24 Feb 22/0 ‐ Program/SRD_Mode 5_SIGNED Final_07Mar2019

Object Identifier:SRD‐367

Object Text:The M5Ll IFF system shall(l) comply with AFI 17‐220 to be supportable in the electromagnetic spectrum and to be interoperable with civil CNS/ATM systems in order to accomplish the aircraft mission and comply with the intent of applicable civil standards.

Object Identifier:TRDp_2836

Object Text:(U) MIL‐STD‐461E, Requirements for the Control of Electromagnetic Interference

Characteristics of Subsystems and Equipment, 20 August 1999

ID : AF SS_12749

Object Number : 2.0-17

(U) MIL‐STD‐464A, Electromagnetic Environmental Effects, 19 December 2002 (TRDp_3865)

In‐links (All modules) : Module Name:/DMS 4 Data at Rest ‐DaR 40‐45 Enterprise /Block 40 45 Enterprise

Object Identifier:DaR_126

Object Text:(U) The 4045 DaR Type 1 Encryptor shall conform to MIL‐STD‐464A, Electromagnetic

Environmental Effects, 19 December 2002 (TRDp_3865)

Object Identifier:TRDp_3865

Object Text:(U) MIL‐STD‐464A, Electromagnetic Environmental Effects Requirements for Systems, 19

December 2002

ID : AF SS_22521

Object Number : 2.0-18

(U) MIL‐STD‐681D, Identification Coding and Application of Hookup and Lead Wire, Notice 1, 19 June

In‐links (All modules) : Module Name:/DMS 4 Data at Rest ‐DaR 40‐45 Enterprise /Block 40 45 Enterprise

Object Identifier:DaR_127

Object Text:(U) The 4045 DaR Type 1 Encryptor shall conform to MIL‐STD‐681D, Identification Coding and Application of Hookup and Lead Wire, Notice 1, 19 June 2000

ID : AF SS_12734

Object Number : 2.0-21

(U) MIL‐STD‐810F, Environmental Test Methods and Engineering Guidelines, 30 August 2002

(TRDp_2830)

In‐links (All modules) : Module Name:/DMS 4 Data at Rest ‐DaR 40‐45 Enterprise /Block 40 45 Enterprise

Object Identifier:DaR_128

Object Text:(U) The 4045 DaR Type 1 Encryptor shall conform to MIL‐STD‐810F, Environmental Test

Methods and Engineering Guidelines, 30 August 2002 (TRDp_2830)

Object Identifier:TRDp_2830

Object Text:(U) MIL‐STD‐810F, Environmental Test Methods and Engineering Guidelines, 30 August 2002

ID : AF SS_13673

Object Number : 2.0-32

(U) MIL‐STD‐2036, General Requirements for Electronic Equipment Specifications, June 1991

In‐links (All modules) : Module Name:/DMS 4 Data at Rest ‐DaR 40‐45 Enterprise /Block 40 45 Enterprise

Object Identifier:DaR_130

Object Text:(U) The 4045 DaR Type 1 Encryptor shall conform to MIL‐STD‐2036, General Requirements for Electronic Equipment Specifications, June 1991

3 (U) REQUIREMENTS

ID : AF SS_12

Object Number : 3.1

3.1 (U) System Definition

ID : AF SS_9247

Object Number : 3.1.1

3.1.1 (U) System Constraints

ID : AF SS_9257

Object Number : 3.1.1.3

3.1.1.3 (U) Natural Environments

ID : AF SS_9258

Object Number : 3.1.1.3.0-1

(U) New and modified equipment of the AWACS shall be designed for operation and maintenance under the conditions defined in the Section 9, AWACS Natural Environment Appendix. (U) Note: Appendix

Section 9.6 lists the requirements for the Ground System.

In‐links (All modules) : Module Name:/40‐45 Prd_U_CDRL_A024_2022‐06‐21 /Tier 1/R‐System Set_PR

Object Identifier:REQ‐SSp_9258

Object Text:(U) New and modified equipment of the AWACS shall be designed for operation and maintenance under the conditions defined in the Section 9, AWACS Natural Environment Appendix. (U)

Note: Appendix Section 9.6 lists the requirements for the Ground System.

Module Name:/40‐45 Prd_U_CDRL_A024_2022‐06‐21 /Tier 2/AVFG/R‐AVFG_PR

Object Identifier:REQ‐AVp_3140

Object Text:(U) Air vehicle equipment shall be designed and constructed that no fixed part or assembly shall become loose, no movable part or control be shifted in setting, position, or adjustment, and no degradation be caused in the specified equipment performance during operation, or after storage, in the specified natural and induced environments specified in the Environments section.

Object Identifier:REQ‐AVp_3143

Object Text:(U) Air vehicle equipment mounted externally to the pressurized fuselage shall be designed to enable the assembly, checkout, operation and organizational maintenance during exposure to the environmental extremes specified in the External Environmental Requirements section of System Set

Requirements of 775‐16001.

Object Identifier:REQ‐AVp_10985

Object Text:(U) Air vehicle equipment mounted internally to the pressurized fuselage shall be designed internal environments specified in the Internal Environmental Requirements section of the System Set

Object Identifier:REQ‐AVp_10986

Object Text:(U) Air vehicle equipment mounted externally, but protected in part from the full regime of external environments by fairings, radomes or other devices shall be designed to enable the assembly, checkout, operation and organizational maintenance during exposure to the environmental extremes specified in the External Environmental Requirements (Protected) section of 775‐16001.

Module Name:/40‐45 Prd_U_CDRL_A024_2022‐06‐21 /Tier 2/CFG/R‐CFG_PR

Object Identifier:REQ‐CFGp_532

Object Text:(U) New/modified CFG equipment mounted external to the pressurized fuselage and not protected by fairings, radomes or other devices shall be designed to enable assembly, checkout, operation and organizational maintenance during exposure to the external environments identified in

Table 9.1‐1, 775‐16001, AWACS Natural Environment Appendix.

Object Identifier:REQ‐CFGp_537

Object Text:(U) New/modified CFG equipment mounted internally to the pressurized fuselage shall be designed to enable assembly, checkout, and organizational maintenance during exposure to the internal environments identified in 775‐16001, AWACS Natural Environment Appendix, Table 9.2‐1.

Object Identifier:REQ‐CFGp_538

Object Text:(U) New/modified CFG equipment shall be capable of operation with exposure to a neutron radiation flux of 9000 n/cm^2*hr with E>10 MEV. Satisfactory operation can be accomplished by use of a combination of upset resistant hardware, system redundancy or system restart performance.

Object Identifier:REQ‐CFGp_539

Object Text:(U) New/modified CFG equipment mounted internally to an enclosure shall be designed to enable assembly, checkout, operation, and organizational maintenance during exposure to the enclosure environments specified in the AWACS Natural Environments Appendix of 775‐16001, Table

9.2‐1.

(U) COTS hardware is exempt from the requirements in this section that pertain to the ability of equipment to withstand fungus growth.

Object Identifier:REQ‐CFGp_540

Object Text:(U) New/modified externally mounted CFG equipment shall be designed to meet the birdstrike requirements defined in section 9.4 "Birdstrike", 775‐16001, AWACS Natural Environment

Appendix.

Object Identifier:REQ‐CFGp_791

Object Text:(U) New/modified CFG equipment that are mounted externally, but protected in part from the full regime of external environments by fairings, radomes, or other devices, shall be designed to enable assembly, checkout, operation and organizational maintenance during exposure to the protected external environments listed in Table 9.3‐1, 775‐16001, AWACS Natural Environment Appendix.

Object Identifier:REQ‐CFGp_802

Object Text:(U) New/modified CFG equipment design shall comply with the random vibration requirements specified in Tables 10.5‐3 through 10.5‐23, section 10.5, 775‐16001 depending on where the equipment is installed (zone) on the AWACS.

Module Name:/40‐45 Prd_U_CDRL_A024_2022‐06‐21 /Tier 2/ESMG/R‐ESMG_PR

Object Identifier:REQ‐ESMp_284

Object Text:(U) New or modified ESM System components mounted externally to the pressurized fuselage and protected by fairings, radomes or other devices, shall be designed to enable removal/installation, checkout, operation and organizational maintenance during exposure to the environmental extremes listed in Table 9.3‐1 of 775‐16001.

Object Identifier:REQ‐ESMp_285

Object Text:(U) New or modified ESM System components mounted internally to the pressurized fuselage shall be designed to enable removal/installation, checkout, operation (except for equipment within a COTS enclosure) and organizational maintenance during exposure to the environmental extremes listed in Table 9.2‐1 of 775‐16001.

Module Name:/40‐45 Prd_U_CDRL_A024_2022‐06‐21 /Tier 2/GSFG/R‐GSFG_PR

Object Identifier:REQ‐GSp_182

Object Text:(U) MCTS equipment which is operated and maintained within a conditioned environment shall be designed to enable operation and maintenance during exposure to the environments specified in System Set 775‐16001, Table 9.6‐2. COTS hardware installed in conditioned environments is exempt from this requirement.

Object Identifier:REQ‐GSp_931

Object Text:(U) GSS equipment which is operated and maintained within a conditioned environment

Object Identifier:REQ‐GSp_2248

Object Text:(U) DGS equipment which is operated and maintained within a conditioned environment

Object Identifier:REQ‐GSp_2281

Object Text:(U) GSFG equipment which is operated and maintained as part of a Mission Computing Test

Rack (MCTR) shall be designed to enable operation and maintenance during exposure to the environments specified in 775‐16001, Table 9.6‐2. COTS hardware installed in conditioned environments at the MOB is exempt from this requirement.

Module Name:/40‐45 Prd_U_CDRL_A024_2022‐06‐21 /Tier 2/IFG/R‐IFG_PR_NG

Object Identifier:REQ‐IFGpn_1523

Object Text:(U) The IFG shall be designed for operation and maintenance under the conditions defined in the IFG Natural Environments Appendix.

Module Name:/40‐45 Prd_U_CDRL_A024_2022‐06‐21 /Tier 2/MCFG/R‐MCFG_PR

Object Identifier:REQ‐MCp_863

Object Text:(U) The MCFG components mounted internal to the pressurized fuselage, including mounting internal to an enclosure, shall be designed and/or selected to enable assembly, checkout, operation, and organizational maintenance during exposure to the internal environments listed in 775‐

16001, Table 9.2‐1. COTS hardware is exempt from the requirements in this section that pertain to the ability of equipment to withstand fungus growth.

Module Name:/40‐45 Prd_U_CDRL_A024_2022‐06‐21 /Tier 2/NFG/R‐NFG_PR

Object Identifier:REQ‐NFGp_10615

Object Text:(U) The NFG equipment shall be designed for operation and maintenance under the conditions defined in the AWACS Natural Environments Appendix of 775‐16001.

Module Name:/40‐45 Prd_U_CDRL_A024_2022‐09‐20 /Tier 1/R‐System Set_PR

Module Name:/40‐45 Prd_U_CDRL_A024_2022‐09‐20 /Tier 2/AVFG/R‐AVFG_PR

Object Identifier:REQ‐AVp_3140

Object Text:(U) Air vehicle equipment shall be designed and constructed that no fixed part or assembly shall become loose, no movable part or control be shifted in setting, position, or adjustment, and no

Object Identifier:REQ‐AVp_3143

Object Text:(U) Air vehicle equipment mounted externally to the pressurized fuselage shall be designed

Object Identifier:REQ‐AVp_10985

Object Text:(U) Air vehicle equipment mounted internally to the pressurized fuselage shall be designed

Object Identifier:REQ‐AVp_10986

Object Text:(U) Air vehicle equipment mounted externally, but protected in part from the full regime of external environments by fairings, radomes or other devices shall be designed to enable the assembly, specified in the External Environmental Requirements (Protected) section of 775‐16001.

Module Name:/40‐45 Prd_U_CDRL_A024_2022‐09‐20 /Tier 2/CFG/R‐CFG_PR

Object Identifier:REQ‐CFGp_537 designed to enable assembly, checkout, and organizational maintenance during exposure to the internal environments identified in 775‐16001, AWACS Natural Environment Appendix, Table 9.2‐1.

Object Identifier:REQ‐CFGp_538 radiation flux of 9000 n/cm^2*hr with E>10 MEV. Satisfactory operation can be accomplished by use of

Object Identifier:REQ‐CFGp_539 enclosure environments specified in the AWACS Natural Environments Appendix of 775‐16001, Table

Object Identifier:REQ‐CFGp_540 birdstrike requirements defined in section 9.4 "Birdstrike", 775‐16001, AWACS Natural Environment the full regime of external environments by fairings, radomes, or other devices, shall be designed to

Object Identifier:REQ‐CFGp_802 requirements specified in Tables 10.5‐3 through 10.5‐23, section 10.5, 775‐16001 depending on where

Module Name:/40‐45 Prd_U_CDRL_A024_2022‐09‐20 /Tier 2/ESMG/R‐ESMG_PR

Object Identifier:REQ‐ESMp_284 environmental extremes listed in Table 9.3‐1 of 775‐16001.

Object Identifier:REQ‐ESMp_285 extremes listed in Table 9.2‐1 of 775‐16001.

Module Name:/40‐45 Prd_U_CDRL_A024_2022‐09‐20 /Tier 2/GSFG/R‐GSFG_PR environments specified in 775‐16001, Table 9.6‐2. COTS hardware installed in conditioned environments

Module Name:/40‐45 Prd_U_CDRL_A024_2022‐09‐20 /Tier 2/IFG/R‐IFG_PR_NG

Object Identifier:REQ‐IFGpn_1523

Module Name:/40‐45 Prd_U_CDRL_A024_2022‐09‐20 /Tier 2/MCFG/R‐MCFG_PR

Object Identifier:REQ‐MCp_863 operation, and organizational maintenance during exposure to the internal environments listed in 775‐

16001, Table 9.2‐1. COTS hardware is exempt from the requirements in this section that pertain to the

Module Name:/40‐45 Prd_U_CDRL_A024_2022‐09‐20 /Tier 2/NFG/R‐NFG_PR

Module Name:/40‐45 Prd_U_CDRL_A024_2023‐09‐07 /Tier 1/R‐System Set_PR

Module Name:/40‐45 Prd_U_CDRL_A024_2023‐09‐07 /Tier 2/GSFG/R‐GSFG_PR environments specified in 775‐16001, Table 9.6‐2. COTS hardware installed in conditioned environments

Module Name:/DMS 4 Data at Rest ‐DaR 40‐45 Enterprise /Block 40 45 Enterprise DMS 4 Data at Rest ‐

DaR

Object Identifier:DaR_131 maintenance under the conditions defined in the Section 9, AWACS Natural Environment Appendix.

(U) Note: Appendix Section 9.6 lists the requirements for the Ground System.

Object Identifier:TRDp_20

Object Text:(U) The 40/45 AWACS shall be operable, maintainable, and supportable in naturally occurring and AWACS induced environmental conditions on both the ground and in the air.

Module Name:/Program Archives /Program Archives/IPEC Archive /Archived version_SRD/V‐System

Set_PR

Object Identifier:VR‐SSp_3

Object Text:(U) Verification that new and/or modified (not previously verified or qualified) AWACS

40/45 aircraft mission systems equipment is operable, maintainable and supportable in naturally occurring environmental conditions defined in Section 9.0 shall be verified in Functional Group and lower level specifications. Lower level verification shall result from component level test, analysis, demonstration and/or inspection. MIL‐STD‐810 shall be used as a guide for testing where applicable.

Provision of active (e.g., EAGE air conditioning) and/or inactive protection to mitigate the effects of the natural environment upon COTS is acceptable. Individual equipment performance to its requirements before, during (where applicable) and after exposure to the environment shall constitute satisfaction of these requirements. Successful completion of all lower level requirement verification will provide evidence of successful verification of this System Set requirement.

(U) For new and modified mission equipment only (including COTS), it is acceptable to perform the verification for the Table 9.2‐1 humidity requirement in accordance with the temperature and humidity cycling as follows:

(U) Radar and NGIFF are both previously verified. For Radar, the verification was conducted under the

RSIP contract and for NGIFF, it was conducted under DO 0058 to the AMASS shell contract. No changes have been made to the radar system for 40/45.

Module Name:/a. Aircraft_Flight Deck/a. Air Vehicle/AVFG_PR

Object Identifier:AVp_3140

Object Text:(U) Air vehicle equipment shall be designed and constructed that no fixed part or assembly shall become loose, no movable part or control be shifted in setting, position, or adjustment, and no

Object Identifier:AVp_3143

Object Text:(U) Air vehicle equipment mounted externally to the pressurized fuselage shall be designed

Requirements of 888‐16001.

Object Identifier:AVp_10985

Object Text:(U) Air vehicle equipment mounted internally to the pressurized fuselage shall be designed

Requirements of 888‐16001.

Object Identifier:AVp_10986

Object Text:(U) Air vehicle equipment mounted externally, but protected in part from the full regime of external environments by fairings, radomes or other devices shall be designed to enable the assembly, specified in the External Environmental Requirements (Protected) section of 888‐16001.

Module Name:/a. Aircraft_Flight Deck/o. Nav FG/NFG_PR

Object Identifier:NFGp_10615 conditions defined in the AWACS Natural Environments Appendix of 888‐16001.

Module Name:/b. Mission Subsystems/a. IFF Functional Group/IFG

Object Identifier:IFGpn_1523

Module Name:/b. Mission Subsystems/d. Mission Communication Functional Group/CFG_PR

Object Identifier:CFGp_532

Table 9.1‐1, 888‐16001, AWACS Natural Environment Appendix.

Object Identifier:CFGp_537 designed to enable assembly, checkout, and organizational maintenance during exposure to the internal environments identified in 888‐16001, AWACS Natural Environment Appendix, Table 9.2‐1.

Object Identifier:CFGp_538 radiation flux of 9000 n/cm^2*hr with E>10 MEV. Satisfactory operation can be accomplished by use of

Object Identifier:CFGp_539 enclosure environments specified in the AWACS Natural Environments Appendix of 888‐16001, Table

Object Identifier:CFGp_540 birdstrike requirements defined in section 9.4 "Birdstrike", 888‐16001, AWACS Natural Environment

Object Identifier:CFGp_791 the full regime of external environments by fairings, radomes, or other devices, shall be designed to external environments listed in Table 9.3‐1, 888‐16001, AWACS Natural Environment Appendix.

Object Identifier:CFGp_802 requirements specified in Tables 10.5‐3 through 10.5‐23, section 10.5, 888‐16001 depending on where

Module Name:/b. Mission Subsystems/m. Mission Computing/MCFG_PR

Object Identifier:MCp_863 operation, and organizational maintenance during exposure to the internal environments listed in 888‐

16001, Table 9.2‐1. COTS hardware is exempt from the requirements in this section that pertain to the

Module Name:/b. Mission Subsystems/t. Radar Set /Radar Specification

Object Identifier:RAD_32

Object Text:The Radar shall be capable of operation as specified herein when exposed to the environments and operational conditions specified in all paragraphs of 3.1.2.4 with the antenna installed in the Rotodome as specified in 3.2.1.

Module Name:/b. Mission Subsystems/w. ESM/ESMG_PR

Object Identifier:ESMp_284 environmental extremes listed in Table 9.3‐1 of 888‐16001.

Object Identifier:ESMp_285 extremes listed in Table 9.2‐1 of 888‐16001.

Module Name:/c. Ground Systems/GSFG_PR

Object Identifier:GSp_182 in System Set 888‐16001, Table 9.6‐2. COTS hardware installed in conditioned environments is exempt

Object Identifier:GSp_931

Object Identifier:GSp_2248

Object Identifier:GSp_2281 environments specified in 888‐16001, Table 9.6‐2. COTS hardware installed in conditioned environments

ID : AF SS_12157

Object Number : 3.1.1.3.0-2

(U) The AWACS shall be capable of performing normal flight operations in adverse weather conditions

(defined in Section 6.3). (TRDp_21)

Object Identifier:REQ‐SSp_12157

Object Text:(U) The AWACS shall be capable of performing normal flight operations in adverse weather conditions (defined in Section 6.3). (TRDp_21)

Object Identifier:REQ‐AVp_870

Object Text:(U) The basic mission of the air vehicle shall be to (1) transport the mission avionics, flight subsystems equipment and crews, and (2) provide a long‐range, high altitude airborne platform with sufficient loitering and support capabilities to enable the USAF AWACS system surveillance, communications and command systems and crews to function at required performance levels and to survive and operate through all operational modes specified in the System Set Requirements of 775‐

16001.

the full regime of external environments by fairings, radomes, or other devices, shall be designed to

Object Identifier:REQ‐ESMp_287

Object Text:(U) The ESM System shall be capable of performing normal flight operations in adverse weather conditions. Adverse weather is defined in Section 6.3.

Object Identifier:REQ‐AVp_870

Object Text:(U) The basic mission of the air vehicle shall be to (1) transport the mission avionics, flight sufficient loitering and support capabilities to enable the USAF AWACS system surveillance, communications and command systems and crews to function at required performance levels and to survive and operate through all operational modes specified in the System Set Requirements of 775‐

16001.

the full regime of external environments by fairings, radomes, or other devices, shall be designed to

Object Identifier:REQ‐ESMp_287

Object Text:(U) The ESM System shall be capable of performing normal flight operations in adverse weather conditions. Adverse weather is defined in Section 6.3.

Object Identifier:TRDp_21

Object Text:(U) The 40/45 AWACS shall be capable of performing normal flight operations in adverse weather conditions.

Object Identifier:VR‐SSp_4

Object Text:(U) Verification that the new or modified equipment for FRP (DMS 4.0) AWACS performs normal flight operations in adverse weather conditions shall be accomplished by analysis of the lower level verifications.

Object Identifier:AVp_870

Object Text:(U) The basic mission of the air vehicle shall be to (1) transport the mission avionics, flight sufficient loitering and support capabilities to enable the USAF AWACS system

ID : AF SS_12061

Object Number : 3.1.1.8

3.1.1.8 (U) Human Performance/Engineering

In‐links (All modules) : Module Name:/CNU_06302020/SRD CNU

Object Identifier:SRD_269

Object Text:Hazards to personnel or equipment resulting from subsystem or component failures, defects or malfunctions shall be minimized or eliminated in accordance with MIL‐STD‐1472G.

Module Name:/PED ‐ Portable Electronic Devices/PED SRD

Object Identifier:PED_47

Object Text:(U) Human Interface: The interface with users of PED shall be consistent with MIL‐STD‐

1472G or industry equivalent.

Module Name:/PED ‐ Portable Electronic Devices/PED SRD

Object Identifier:PED_77

Object Text:(U) Human Interface: Aircrew shall make portable EFBs secure and viewable during critical phases of flight and the location must not interfere with flight control movement, emergency egress, or oxygen deployment. Exception: Aircrew may remove EFB from its securing device and hold by hand during critical phases of flight when operationally necessary (e.g. briefing an approach).

ID : AF SS_5773

Object Number : 3.1.1.8.0-1

(U) The requirements of human engineering shall be applied to the design, development, and acquisition of the AWACS.

(U) Human engineering requirements are based on applicable MIL‐STD‐1472 design criteria and the implementation of these requirements for AWACS is detailed in the Boeing Human Engineering Plan

(HEP), D775‐00071‐1.

(U) The selection of COTS equipment through the use of the Off‐The‐Shelf Hardware Selection Process, D204‐30707‐1 (reference SSp_5136) considers and documents human engineering requirements.

Object Identifier:REQ‐SSp_5773

Object Text:(U) The requirements of human engineering shall be applied to the design, development, and acquisition of the AWACS.

Object Identifier:REQ‐AVp_9721

Object Text:(U) The air vehicle shall be in compliance with the human performance and engineering requirements specified in the Human Performance/Engineering section of 775‐16001.

Module Name:/CNU_06302020/SRD CNU

Object Identifier:DaR_132

Object Identifier:VR‐SSp_13

Object Text:(U) This requirement was verified under the PreProduction contract. For new and modified equipment, requirements shall be verified by analysis of documented compliance in a MIL‐STD‐1472 hardware integration report produced by Human Factors Engineering (HFE). For new and modified

COTS equipment, human engineering considerations will be applied by HFE participation in the COTS selection process.

Object Identifier:AVp_9721 requirements specified in the Human Performance/Engineering section of 888‐16001.

ID : AF SS_5776

Object Number : 3.1.1.8.0-3

(U) Installation of new and modified AWACS equipment shall be designed to provide accessibility for troubleshooting, alignment/adjustment, removal, replacement, and maintenance IAW MIL‐STD‐1472, Human Engineering.

Object Identifier:REQ‐SSp_5776

Object Text:(U) Installation of new and modified AWACS equipment shall be designed to provide accessibility for troubleshooting, alignment/adjustment, removal, replacement, and maintenance IAW

MIL‐STD‐1472, Human Engineering.

Object Identifier:REQ‐AVp_3111

Object Text:(U) All areas requiring frequent maintenance or inspection shall incorporate access panels with quick disconnect fasteners.

Object Identifier:REQ‐AVp_5558

Object Text:(U) Equipment which requires periodic maintenance shall be easily accessible.

Object Identifier:REQ‐AVp_8540

Object Text:(U) Equipment requiring periodic observation or maintenance shall be located where it is accessible.

Object Identifier:REQ‐AVp_12067

Object Text:(U) AVFG LRUs requiring handling equipment for installation/removal in the aircraft main cabin shall not exceed 21 inches wide by 34 inches high by 36 inches long.

Object Identifier:REQ‐AVp_12068

Object Text:(U) The AV main aisle shall accommodate an LRU and its handling equipment whose maximum dimensions shall not exceed 22 inches wide by 40 inches high by 42 inches long.

Object Identifier:REQ‐CFGp_615

Object Text:(U) New/modified CFG equipment and its handling equipment shall be designed/selected to fit within the existing doorways and aisleways of the air vehicle.

Object Identifier:REQ‐CFGp_862

Object Text:(U) New/modified CFG equipment, when installed, shall be designed and constructed to provide ease of access for maintenance activities to comply with Human Engineering criteria specified in

MIL‐STD‐1472, as tailored in the Boeing Human Engineering Plan, D775‐00071‐1.

(U) Maintenance activities include troubleshooting, alignment/adjustment, removal and replacement actions.

Object Identifier:REQ‐ESMp_152

Object Text:(U) The new or modified LRUs/LRMs for the ESM System shall be constructed to provide accessibility for maintenance to include troubleshooting, alignment/adjustment, removal and replacement actions

Object Identifier:REQ‐ESMp_600

Object Text:(U) Design of new components, and modifications to existing components, shall comply with

Human Engineering criteria specified in MIL‐STD‐1472 as tailored in the Boeing Human Engineering Plan, D775‐00071‐1. Legacy components do not need to be re‐evaluated for compliance with MIL‐STD‐1472 design criteria.

Object Identifier:REQ‐GSp_962

Object Text:(U) Design and construction of new GS components/equipment, modifications to existing components/equipment, and GS component installations, for the GSS, shall be designed for ease of access for maintenance activities to comply with Human Engineering requirements which are based on

MIL‐STD‐1472 Revision F design criteria. Maintenance activities include troubleshooting, alignment/adjustment, removal and replacement actions. COTS equipment selection criteria is specified in GSp_48.

Object Identifier:REQ‐GSp_4388 components/equipment, and GS component installations, for the DGS, shall be designed for ease of alignment/adjustment, removal and replacement actions. COTS equipment selection criteria is specified in REQ‐GSp_2106.

Object Identifier:REQ‐GSp_4389 components/equipment, and GS component installations, for the MCMT, shall be designed for ease of alignment/adjustment, removal and replacement actions. COTS equipment selection criteria is specified in REQ‐GSp_2335.

Object Identifier:REQ‐GSp_4390 components/equipment, and GS component installations, for the MCTS, shall be designed for ease of alignment/adjustment, removal and replacement actions. COTS equipment selection criteria is specified in REQ‐GSp_2030.

Object Identifier:REQ‐IFGpn_1191

Object Text:(U) New and modified IFG equipment, when installed, shall be designed and constructed to provide ease of access for maintenance activities to comply with Human Engineering criteria specified in

MIL‐STD‐1472, as tailored in the Boeing Human Engineering Plan, D775‐00071‐1. Maintenance activities include troubleshooting, alignment/adjustment, removal and replacement actions.

Object Identifier:REQ‐IFGpn_1661

Object Text:(U) The IFG shall be designed to provide accessibility for maintenance to include troubleshooting, alignment/adjustment, removal, and replacement actions.

Object Identifier:REQ‐MCp_1324

Object Text:(U) The MCFG shall be designed to provide accessibility for maintenance to include

Object Identifier:REQ‐MCp_1782

Object Text:(U) MCS equipment and its handling equipment shall be designed/selected to fit within the existing doorways and aisleways of the air vehicle.

Object Identifier:REQ‐MCp_2082

Object Text:(U) Design and construction of new MCS components/equipment, and modifications to existing components/equipment shall provide accessibility for maintenance to include troubleshooting, alignment/adjustment, removal, and replacement actions to comply with human engineering criteria specified in MIL‐STD‐1472, as tailored in the Boeing Human Engineering Plan, D775‐00071‐1.

Consideration of accessibility within COTS components is a selection criteria as specified in MCp_1294.

Access to installed MCS components in racks is dependent on rack design, which is not within the scope of the MCFG specification.

Object Identifier:REQ‐NFGp_10248

Object Text:(U) The physical characteristics of the new and modified NFG equipment on‐board the aircraft shall be as defined in the TANS to AV ICD 775‐13213.

Object Identifier:REQ‐NFGp_10264

Object Text:(U) The NFG equipment shall be designed and installed in a manner that requires no more than two people to remove and replace an LRU/LRM.

Object Identifier:REQ‐NFGp_10274

Object Text:(U) New and modified NFG equipment shall be designed to provide access to frequently accessed areas within 1 minute.

Object Identifier:REQ‐NFGp_10283

Object Text:(U) New and modified NFG equipment shall provide in‐flight access for operators to reset devices and view any indicator lights during mission operations.

Object Identifier:REQ‐NFGp_10542

Object Text:(U) MIL‐STD‐1472 shall be applied to the design, development, and acquisition of new and modified NFG equipment. Legacy components are not required to be re‐evaluated for compliance with

MIL‐STD‐1472 design criteria.

Object Identifier:REQ‐NFGp_10555

Object Text:(U) Installation of new and modified NFG equipment shall not impair normal workspace thoroughfare and in‐flight maintenance actions.

Object Identifier:REQ‐NFGp_10661

Object Text:(U) LRUs requiring handling equipment for installation/removal in the aircraft main cabin shall not exceed 21 inches wide by 34 inches high by 36 inches long.

Object Identifier:REQ‐AVp_3111

Object Text:(U) All areas requiring frequent maintenance or inspection shall incorporate access panels

Object Identifier:REQ‐AVp_5558

Object Identifier:REQ‐AVp_8540

Object Identifier:REQ‐AVp_12067

Object Identifier:REQ‐AVp_12068

Object Identifier:REQ‐CFGp_615

Object Identifier:REQ‐CFGp_862 provide ease of access for maintenance activities to comply with Human Engineering criteria specified in

Object Identifier:REQ‐ESMp_152

Object Identifier:REQ‐ESMp_600

Object Text:(U) Design of new components, and modifications to existing components, shall comply with

Human Engineering criteria specified in MIL‐STD‐1472 as tailored in the Boeing Human Engineering Plan, alignment/adjustment, removal and replacement actions. COTS equipment selection criteria is specified alignment/adjustment, removal and replacement actions. COTS equipment selection criteria is specified alignment/adjustment, removal and replacement actions. COTS equipment selection criteria is specified alignment/adjustment, removal and replacement actions. COTS equipment selection criteria is specified

Object Identifier:REQ‐IFGpn_1191 provide ease of access for maintenance activities to comply with Human Engineering criteria specified in

MIL‐STD‐1472, as tailored in the Boeing Human Engineering Plan, D775‐00071‐1. Maintenance activities

Object Identifier:REQ‐IFGpn_1661

Object Identifier:REQ‐MCp_1324

Object Identifier:REQ‐MCp_1782

Object Text:(U) MCS equipment and its handling equipment shall be designed/selected to fit within the

Object Identifier:REQ‐MCp_2082 existing components/equipment shall provide accessibility for maintenance to include troubleshooting, Consideration of accessibility within COTS components is a selection criteria as specified in MCp_1294.

Access to installed MCS components in racks is dependent on rack design, which is not within the scope

Object Identifier:REQ‐NFGp_10248

Object Identifier:REQ‐NFGp_10264

Object Identifier:REQ‐NFGp_10274

Object Identifier:REQ‐NFGp_10283

Object Identifier:REQ‐NFGp_10542

Object Identifier:REQ‐NFGp_10555

Object Identifier:REQ‐NFGp_10661

Object Text:(U) LRUs requiring handling equipment for installation/removal in the aircraft main cabin alignment/adjustment, removal and replacement actions. COTS equipment selection criteria is specified alignment/adjustment, removal and replacement actions. COTS equipment selection criteria is specified alignment/adjustment, removal and replacement actions. COTS equipment selection criteria is specified alignment/adjustment, removal and replacement actions. COTS equipment selection criteria is specified

Object Identifier:SRD_267

Object Text:CNU Equipment shall be designed and constructed to comply with the Maintenance

Accessibility requirements in section 5.9 of MIL‐STD‐1472G. Note: Maintenance activities include troubleshooting, alignment/adjustment, removal and replacement actions.

Object Identifier:DaR_135

Object Identifier:TRDp_1758

Object Text:(U) New and modified equipment shall be constructed to provide accessibility for maintenance to include troubleshooting, alignment/adjustment, removal and replacement actions.

Object Identifier:VR‐SSp_15

Object Text:(U) This requirement was verified under the PreProduction contract. For new and modified equipment, requirement verification will consist of documentation of compliance in a MIL‐STD‐1472 hardware integration report produced by HFE. For new and modified COTS equipment, human engineering considerations will be applied by HFE participation in the COTS selection process. No further system‐level verification will be performed.

(U) Radar and NGIFF are both previously verified. For Radar, the verification was conducted under the

RSIP contract and for NGIFF, it was conducted under DO 0058 to the AMASS shell contract. No changes have been made to the radar system for 40/45.

Note:

(U) Verification that new and modified Block 40/45 Production components/equipment items are designed and constructed to provide ease of access for maintenance, removal and replacement is accomplished by analysis. Installation and layout drawings are assessed with respect to the guidance of

MIL‐STD‐1472. Digital models may be examined to assess equipment accessibility and maintenance features. Physical mockups and virtual simulations may be used to assess equipment installation and ease of maintenance and replacement. Selected maintainability demonstrations can be conducted to validate analysis assessments.

Object Identifier:AVp_3111

Object Text:(U) All areas requiring frequent maintenance or inspection shall incorporate access panels

Object Identifier:AVp_5558

Object Identifier:AVp_8540

Object Identifier:AVp_9721 requirements specified in the Human Performance/Engineering section of 888‐16001.

Object Identifier:AVp_12067

Object Identifier:AVp_12068

Object Identifier:NFGp_10248

Object Identifier:NFGp_10264

Object Identifier:NFGp_10274

Object Identifier:NFGp_10283

Object Identifier:NFGp_10542

Object Identifier:NFGp_10555

Object Identifier:NFGp_10661

Object Text:(U) LRUs requiring handling equipment for installation/removal in the aircraft main cabin

Object Identifier:IFGpn_1191 provide ease of access for maintenance activities to comply with Human Engineering criteria specified in

MIL‐STD‐1472, as tailored in the Boeing Human Engineering Plan, D775‐00071‐1. Maintenance activities

Object Identifier:IFGpn_1661

Object Identifier:CFGp_615

Object Identifier:CFGp_862 provide ease of access for maintenance activities to comply with Human Engineering criteria specified in

Object Identifier:MCp_1324

Object Identifier:MCp_1782

Object Text:(U) MCS equipment and its handling equipment shall be designed/selected to fit within the

Object Identifier:MCp_2082 existing components/equipment shall provide accessibility for maintenance to include troubleshooting, Consideration of accessibility within COTS components is a selection criteria as specified in MCp_1294.

Access to installed MCS components in racks is dependent on rack design, which is not within the scope

Object Identifier:RAD_764

Object Text:Aerospace Ground Equipment required for organizational maintenance shall be held to a minimum,...

Object Identifier:RAD_4826

Object Text: ... and shall be designed to comply with MIL‐STD‐1472 in accordance with 3.1.2.6.f.

Object Identifier:RAD_4847

Object Text: (8) Shall have easily removable items. Separate card pullers shall not be required for card removal except for the RCMP display units' cards, which may use a single standard card puller from the Standard Government tool list.

Object Identifier:ESMp_152

Object Identifier:ESMp_600

Object Text:(U) Design of new components, and modifications to existing components, shall comply with

Human Engineering criteria specified in MIL‐STD‐1472 as tailored in the Boeing Human Engineering Plan, Object Identifier:GSp_962 alignment/adjustment, removal and replacement actions. COTS equipment selection criteria is specified

Object Identifier:GSp_4388 alignment/adjustment, removal and replacement actions. COTS equipment selection criteria is specified in Req‐GSp_2106.

Object Identifier:GSp_4389 alignment/adjustment, removal and replacement actions. COTS equipment selection criteria is specified

Object Identifier:GSp_4390 alignment/adjustment, removal and replacement actions. COTS equipment selection criteria is specified

ID : AF SS_27

Object Number : 3.2

3.2 (U) Performance

ID : AF SS_1761

Object Number : 3.2.3

3.2.3 (U) Command and Control

ID : AF SS_1762

Object Number : 3.2.3.2

3.2.3.2 (U) Command and Control Functions

ID : AF SS_12232

Object Number : 3.2.3.2.7

3.2.3.2.7 (U) Security

ID : AF SS_22394

Object Number : 3.2.3.2.7.1

3.2.3.2.7.1 (U) Information Assurance (IA)

ID : AF SS_25572

Object Number : 3.2.3.2.7.1.0-1

(U) The AWACS, for the MCTS, shall lock user accounts after fifteen (15) minutes of inactivity or upon receiving a request from a user while in an Operational state per section 6.4.1.4.

Object Identifier:REQ‐SSp_25572

Object Text:(U) The AWACS, for the MCTS, shall lock user accounts after fifteen (15) minutes of inactivity or upon receiving a request from a user while in an Operational state per section 6.4.1.4.

Object Identifier:REQ‐GSp_16050

Object Text:(U) The MCTS shall lock machines user accounts after fifteen (15) minutes of inactivity or upon receiving a request from a user input while in an Operational state per section 6.3.4.

Object Text:(U) The AWACS, for the MCTS, shall lock user accounts after fifteen (15) minutes of inactivity

Object Text:(U) The MCTS shall lock machines user accounts after fifteen (15) minutes of inactivity or

Object Text:(U) The AWACS, for the MCTS, shall lock user accounts after fifteen (15) minutes of inactivity

Object Text:(U) The MCTS shall lock machines user accounts after fifteen (15) minutes of inactivity or

Object Identifier:VR‐SSp_207985

Object Text:(U) An analysis of software demonstration shall be conducted to determine that the MCTS locks machines after fifteen (15) minutes of inactivity or upon receiving a request from a user.

Object Identifier:GSp_16050

Object Text:(U) The MCTS shall lock machines user accounts after fifteen (15) minutes of inactivity or

ID : AF SS_25573

Object Number : 3.2.3.2.7.1.0-2

(U) The AWACS, for the MCTS, shall lock user accounts after five (5) hours of inactivity or upon receiving a request from a user while in an Operational state per section 6.4.1.4.

Object Identifier:REQ‐SSp_25573

Object Text:(U) The AWACS, for the MCTS, shall lock user accounts after five (5) hours of inactivity or upon receiving a request from a user while in an Operational state per section 6.4.1.4.

Object Identifier:REQ‐GSp_16051

Object Text:(U) The MCTS shall lock machines user accounts after five (5) hours of inactivity or upon receiving a request from a user input while in an Operational state per section 6.3.4.

Object Text:(U) The AWACS, for the MCTS, shall lock user accounts after five (5) hours of inactivity or

Object Text:(U) The MCTS shall lock machines user accounts after five (5) hours of inactivity or upon

Object Text:(U) The AWACS, for the MCTS, shall lock user accounts after five (5) hours of inactivity or

Object Text:(U) The MCTS shall lock machines user accounts after five (5) hours of inactivity or upon

Object Identifier:VR‐SSp_207986

Object Text:(U) An analysis of software demonstration shall be conducted to determine that the MCTS locks machines after five (5) hours of inactivity or upon receiving a request from a user.

Object Identifier:GSp_16051

Object Text:(U) The MCTS shall lock machines user accounts after five (5) hours of inactivity or upon

ID : AF SS_25574

Object Number : 3.2.3.2.7.1.0-3

(U) The AWACS, for the MCTS, shall retain a session lock on an inactive user account until the user reestablishes access using established identification and authentication procedures while in an

Operational state per section 6.4.1.4.

(U) Note: Authentication is defined in section 6.3.1.

Object Identifier:REQ‐SSp_25574

Object Text:(U) The AWACS, for the MCTS, shall retain a session lock on an inactive user account until the user reestablishes access using established identification and authentication procedures while in an

Operational state per section 6.4.1.4.

(U) Note: Authentication is defined in section 6.3.1.

Object Identifier:REQ‐GSp_16052

Obje