JBADS_Draft_PSPEC_Ver_4_-_29_Aug_16.docx

DRAFT

PERFORMANCE SPECIFICATION

FOR

JOINT BIOLOGICAL AGENT DECONTAMINATION SYSTEM

(JBADS)

29 August 2016

VERSION 4

1.0 Scope.

This specification documents the performance, design and verification parameters for the Joint Biological Agent Decontamination System (JBADS). The Joint Biological Agent Decontamination System provides decontamination capabilities for sensitive and non-sensitive equipment in non-hostile environments.

1.1 Document Overview.

This specification documents the performance requirements for the JBADS. Threshold (mandatory) requirements are defined and, where applicable, objective (desired) requirements are provided as text within braces { }. The JBADS ability to meet an objective requirement may be tested but the inability to meet an objective requirement shall not be used as criteria for failure. Some threshold requirements are further defined as Key Performance Parameters (KPPs), which are capabilities or characteristics so significant that failure to meet the performance value can be cause for the concept or system selection to be reevaluated or the program to be reassessed or terminated. KPPs are identified with an asterisk “*”. This document shall be updated at each acquisition phase of the JBADS Program. The first update shall be based on the approved Capability Development Document (CDD), and the approved Test and Evaluation Master Plan (TEMP). The second major update shall be based on the results of the Engineering and Manufacturing Development (EMD) phase and the approved Capability Production Document (CPD). Other updates shall be made as deemed necessary by the Government throughout the acquisition cycle. JBADS shall be fielded to the United States Air Force.

2.0 Applicable Documents.

2.1 General.

The documents listed in this section are specified in sections 3 and 4 of this specification. This section does not include documents cited in other sections of this specification or recommended for additional information or as examples. While every effort has been made to ensure the completeness of this list, document users are cautioned that they shall meet all specified requirements documents cited in sections 3 and 4 of this specification, whether or not they are listed.

ANSI Z535.4 Safety Labels.

The following specifications, standards, and handbooks form a part of this document to the extent specified herein.

Department of Defense Standards

Department of Defense Directive (DODD) 5000.1 (paraE1.23)

Defense Instruction (DODI) 5000.2 (para 3.7.1.1, 3.7.4, and E7.1.6)

MIL-STD-464C Interface Electromagnetic Environmental Effects, 1 December 2010

MIL-STD-1474, Design Criteria for Noise Limits

MIL-STD-810G with Change 1, Department of Defense Test Method Standard, 15 April 2014

(Copies of these documents are available online at https://assist.daps.dla.mil/quicksearch/ or from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 19111-5094.)

2.2.2 Other Government Documents, Drawings, and Publications

Doctrine

AFI 63-101/20-101 Integrated Life Cycle Management

AFMAN 48-146, Occupational & Environmental Health Program Management

(Copies of these documents are available electronically from the website at http://www.dtic.mil/doctrine/)

Code of Federal Regulation (CFR)

Defense Transportation Regulations Part VI, Chapter 604 for Safe Containers Certification

(Copies of these documents are available from the U.S. Government Printing Office, Washington, DC 20402 or electronically from the website at http://www.gpoaccess.gov/cfr/index.html).

International Organization for Standardization

ISO 1496-1 Freight Containers

ISO 9001 Quality Management

2.3 Order of Precedence.

Unless otherwise noted herein or in the contract, in the event of a conflict between the text of this document and the references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained.

3.0 Requirements.

3.1 Decontamination Efficacy.

3.1.1 Decontamination Parameters. The JBADS shall maintain a temperature of 170oF +/- 5oF with a relative humidity of 90% +/- 5% throughout the Aircraft Enclosure (AE) and aircraft being decontaminated for a period of no less than 96 continuous hours.

3.1.2 Decontamination Cycle Time. The JBADS shall require no more than 240 hours (T), 144 hours (O), to perform a full decontamination cycle. This time includes system temperature ramp up to the required conditions, 96 hours at the required conditions, and cool down to ambient temperature without the formation of condensation within the AE or on any surface of the aircraft being decontaminated.

3.1.3 Aircraft Decontamination Materiel Damage. The aircraft being decontaminated shall incur no more materiel degradation by the decontamination process than is allowable in C-130 certification/guidelines to exclude Line Replaceable Units (LRUs)(T), no materiel degradation (O).

3.1.4 AE Size. The AE shall be sized to completely enclose a C-130J-30 aircraft.

3.1.5 Aircraft AE Ingress and Egress. The AE shall include provisions such that the aircraft can ingress and egress when the AE is in place.

3.1.5.1 Aircraft Placement In AE. The aircraft to be decontaminated may be pushed or pulled into the AE by an aircraft tug attached at the nose gear.

3.1.5.2 AE Equipment and Personnel Entrance and Exit. The aircraft tug and all personnel must be able to exit the AE after the aircraft is in place and to re-enter the AE at the completion of decontamination.

3.2 Operational Availability, Reliability, Maintainability.

3.2.1 Materiel Availability (Am). The JBADS shall achieve a Materiel Availability of at least 0.80 (T=O).

3.2.2 Reliability. The JBADS shall have at least a Probability (P) = 0.87 {0.95} with a confidence of {80%} )(for both the reliability threshold and objective values)of completing a 240 hour mission without an Operational Mission Failure.

3.2.3 Maintainability. The JBADS Mean Time Between Operational Mission Failures shall be no less than 1,200 hours {2,400 hours}.

3.2.4 Corrective Maintenance. The JBADS Mean Time to Repair (corrective maintenance) shall be less than or equal to 120 minutes {30} minutes (T).

3.2.5 Scheduled Maintenance. JBADS scheduled maintenance shall not be required or performed during decontamination procedures.

3.2.6 Down-Time. JBADS maximum down-time shall not exceed 24 hours (T=O).

3.2.7 Service Life. JBADS shall have a ten (10) {twenty (20)} year service life.

3.3 System Implementation.

3.3.1 Subsystems. The JBADS shall consist of three (3) subsystems: an Aircraft Enclosure (AE), Aircraft Decontamination Unit(s) (ADU), and a Control Module (CM).

3.3.1.1 Operational Configuration. The AE, ADU, and CM shall integrate to form an operational configuration.

3.3.1.2 Storage and Transport Configuration. The JBADS storage and transport configurations shall be the same.

3.3.2 Assembly and Disassembly Equipment. The JBADS shall be capable of being assembled and disassembled by personnel using standard military and industrial material handling equipment (MHE) (e.g. 25,000-lb all terrain fork-lift, 50-ton all-terrain crane, wrecker).

3.3.4.1 Unpack and Assembly Time. After arrival of all system components at the decontamination site, the JBADS shall require no more than 30 days to be unpacked and assembled for operation.

3.3.4.2 Disassembly and Pack for Transport Time. After completion of decontamination operations the JBADS shall require no more than 30 days to be disassembled and packed for transport.

3.3.5 Unpack, Setup, Teardown and Re-pack Personnel. The JBADS shall require no more than 16 personnel to unpack, setup for operation, teardown, and re-pack for transport of one JBADS.

3.3.6 Air Transport Certification. The JBADS shall receive internal air transport certification for C-5 and C-17 in the storage/transport configuration.

3.3.7 Commercial Ground Transport. The JBADS shall be transportable by commercial ground transport over paved roads in the storage/transport configuration without any special USDOT or State permits.

3.3.8 Sea Lift. The JBADS shall be transportable by sea lift in the storage/transport configuration.

3.3.9 Storage and Transport Configuration. All JBADS components shall be stored and transported within 20 or 40 foot ISO containers or in system unique configurations that shall be ISO container certified. Certified ISO Containers that are modified to accommodate JBADS equipment shall be re-certified by the USAF Air Transportability Test Loading Activity (ATTLA) as being structurally sound and “safe to fly”. ISO containers shall be the primary means used for JBADS transportation. By exception, items too large for 40’ ISO containers may be protected by some other means and be capable of being loaded on standard 463L pallet trains to be loaded on C-17 and larger aircraft. Use of 20 foot ISO containers is operationally preferred.

3.3.10 Power Sources. The JBADS shall be compatible with standard fielded and commercial power sources, local voltage & frequency, variable cycle compatible (50 and 60 cycle) and existing military generators which are defined as Class 2B per MIL-STD-1332.

3.3.11 Power Distribution. The JBADS shall include all items necessary to distribute power to its components to include any cables or connectors.

3.4 Operator Requirements.

3.4.1 Operator Personnel. The JBADS shall require no more than two personnel at a time to operate during decontamination procedures.

3.4.2 Personnel Protective Equipment (PPE). Personnel wearing PPE (full face protection, gloves, and over garment) must be capable of completing all required activities while they are in proximity of a contaminated aircraft. These activities would include: assisting in the contaminated aircraft being placed within the enclosure, any construction needed to enclose the aircraft, and working near or in the contaminated aircraft or within 6 feet of the enclosure while the contaminated aircraft is undergoing decontamination.

3.4.3 Operator Functions. Operators shall be able to monitor, control and record systems parameters to effectively employ the system.

3.4.4 Systems Controls. Systems controls shall comply with MIL-STD-1472F requirements. This shall include, but is not limited to, the sound level of any audible alarms, size of buttons and switches, as well as the color choices thereof.

3.5 Operational Environments.

3.5.1 External Operating Temperature. The JBADS shall be capable of operation under external temperature conditions from 0o C to 48.9o C (32o F to 120o F).

3.5.1.1 Low Temperature Operation. The JBADS shall be able to maintain the required temperature and humidity throughout the AE and aircraft being decontaminated while being operated at 0o C.

3.5.1.2 High Temperature Operation. The JBADS shall be able to maintain the required temperature and humidity throughout the AE and aircraft being decontaminated while being operated at 48.9o C.

3.5.2 Storage/Transport Temperature. The JBADS shall be capable of operation after storage/transport in the temperature range of: (-10o C to 48.9o C) (T); (-23o C to 71o C) (O).

3.5.2.1 Low Temperature Storage/Transport. The JBADS shall be capable of setup and operation after storage/transport at temperatures down to -10o C (14o F) {-23o C (-9o F)}.

3.5.2.2 High Temperature Storage/Transport. The JBADS shall be capable of setup and operation after storage/transport at temperatures up to 48.9o C (120o F) {71o C (160o F)}.

3.5.3 Rain. The JBADS shall be capable of withstanding exposure to rain.

3.5.3.1 Rain During Storage and Transport. The JBADS shall withstand exposure to rain in the storage/transport configuration.

3.5.3.2 Rain During Operations. The JBADS shall be capable of performing its intended mission in the operational configuration while withstanding exposure to rain at a rate of two inches per hour for thirty minutes without evidence of major leakage. Major leakage is defined as water continually leaking and dropping off or running down the system’s inner surface such that it impairs the system’s intended military use.

3.5.4 Humidity. The JBADS shall be capable of withstanding exposure to humidity.

3.5.4.1 Humidity During Storage/Transport. The JBADS shall be capable of setup and operation during after exposure to humidity from 5% to 100% in the storage/transport configuration.

3.5.4.2 Humidity During Operation. The JBADS shall be capable of operation during and/or after exposure to humidity from 5% to 100% in the operational configuration.

3.5.5 Blowing Sand and Dust. The JBADS shall be capable of setup and operation after exposure to blowing sand and dust.

3.5.5.1 Blowing Sand and Dust During Storage/Transport. The JBADS shall be capable of setup and operation after exposure to blowing sand and dust in the storage/transport configuration.

3.5.5.2 Blowing Sand and Dust During Operation. The JBADS shall be capable of operation during and after exposure to blowing sand and dust in the operational configuration.

3.5.6 Vibration from Transportation. The JBADs shall be capable of setup and operation after exposure to paved road vibration in the storage/transport configuration.

3.5.7 Transit Shock. The JBADS shall be capable of setup and operation after exposure to transit shock in the storage/transport configuration.

3.5.8 Wind. The JBADS shall show no evidence of structural damage, degradation, or permanent deformation as a result of exposure to sustained winds of 55 mph and three instances of 10 second gusts up to 65 mph within the same 30-minute period in the operational configuration.

3.5.9 Snow Load. The JBADS shall be capable of performing its intended mission while withstanding a snow load of 10 lb/ft² for 12 hours without structural damage, degradation, or permanent deformation in the operational configuration.

3.6 Electromagnetic Environmental Effects.

3.6.2 Grounding. Equipment grounding (e.g. ADU or AE) shall comply with the requirements of NFPA 70-2005, article 250, and the requirements of UL 60950, paragraph 1.6.4 and section 2.6 for Class I equipment.

3.7 Human System Integration.

3.7.0 Life Cycle Safety and Health Hazards. The JBADS shall not present uncontrolled safety or health hazards to personnel throughout its life cycle.

3.7.1 Alarms. Audible/visual alarms shall be provided to indicate malfunctions that could cause severe injury/equipment damage. Audible alarms shall be distinguishable from other sounds under normal operating conditions. Visual alarms shall be readily visible and easily recognized.

3.7.2 Colors of Safety Critical Controls. Colors of safety critical controls and indicators shall be yellow for caution, and red for danger. Any color is permitted for other functional controls or indicators provided it is clear that no safety issue is involved.

3.7.3 Safety Markings. Safety markings and labels shall be provided identifying any potential hazards to personnel. Safety markings and labels shall comply with the requirements of ANSI Z535.4. RF radiation hazards and voltages in excess of 70V shall use the signal word WARNING. Voltages in excess of 500V shall use the signal word DANGER. Safety labels complying with the requirements of UL 60950, paragraph 1.7.13 and/or UL 969 are acceptable. Markings shall be readily visible to the user/maintainer, even when a barrier or access door is opened/removed.

3.7.4 Safety Hazards. All safety hazards shall be addressed in the appropriate operator and technical manuals. Information regarding hazard-avoiding procedures and safety warning labels on equipment shall be included in all manuals. Maintenance technical manuals shall address replacement procedures for damaged or missing safety labels.

3.7.5 Noise Protection. The JBADS shall minimize external noise hazards so that noise levels shall not exceed 85 db(A) beyond 5 feet from the noise source. In areas where steady state noise levels are 85 db(A) or greater, noise hazard caution signs shall be permanently posted on the equipment in accordance with MIL-STD-1472F.

3.7.6 Lifting. All man portable items shall be labeled with the weight and number of people required to perform the lift.

3.7.7 Emergency Shutdown. The JBADS system shall include the ability for the operators to shut down the system in the event of an emergency.

3.7.8 Lights and Video Cameras. Lights and video cameras shall be used to monitor personnel and aircraft inside the AE from the control module.

3.7.8.1 Lights and Video Camera Wiring. Lights and video cameras shall be hardwired to the control module.

3.7.9 Health Hazards. The JBADS shall be designed to eliminate or minimize to the greatest extent possible any health impacts, so that system-generated illness and injury is minimized and mission readiness is not compromised. The user shall have the ability to train, operate, maintain, and dispose of the JBADS in full compliance with existing and soon to be published health requirements contained in all applicable local, state, and federal statutes, standards, regulations, and executive.

3.7.9.1 Control Module (CM). An environmentally conditioned shelter shall be provided for the control module.

3.7.9.1.1 CM Personnel Capacity. The control module shelter shall provide space for at least two operators to be present.

3.7.9.1.2 CM Inside Temperature. The control module shelter shall be environmentally conditioned to a minimum internal temperature of 60 degrees F. and a maximum internal temperature of 80 degrees F.

3.7.9.1.3 CM Temperature Excursions. All temperature excursions outside of the temperature range specified by 3.7.9.1.2 shall return to the specified range within a maximum time of 5 minutes from the time the cause of the temperature excursion is resolved (e.g. door is shut).

3.7.10 Operator Access. Operators shall not have access to components with voltages exceeding 30V. All exposed energized parts shall be guarded or covered regardless of voltage. The operator shall not be exposed to stored energy shock at the disconnecting means in accordance with UL 60950, paragraph 2.1.1.7.

3.7.11 Maintenance Protection. The JBADS shall provide protection to personnel during maintenance and repair to prevent unintentional contact with voltages exceeding 70V. Current sources exceeding 25A shall be protected from accidental short-circuiting. Voltage measurements required by maintainers shall not exceed 300V. Circuits and components exceeding 500V shall be completely enclosed and interlocked (non-by-passable). Where interlocks are used, they shall comply with UL 60950, paragraphs 2.8.3 - 2.8.5.

3.7.12 Power Interfaces. Interface with power sources, and disconnecting means shall be in accordance with NFPA 70-2002, and UL 60950, sec 3.4. Equipment designed to have multiple-input power capabilities, or powered by a generator with multiple-voltage output capabilities, shall be protected from damage when connected to incorrect input power/voltage levels.

3.7.13 Personnel Lighting. The JBADS shall include lighting so personnel can maneuver around inside the aircraft enclosure.

4.0 Verification.

Each requirement, as denoted by a “shall” statement in Section 3 above, shall be subjected to a verification process to evaluate the ability of the equipment to meet the specified requirements. Verification shall involve one or more of four methods described in Table I.

4.0.1 Verification Methods and Matrix.

Table I, Verification Methods, lists and describes the verification methods that will be used.

Table II, Requirements Verification Matrix, lists the requirements from paragraph 3 and the related verification method from paragraph 4 that will be used to verify the requirement has been met.

4.0.2 Certifications.

DRAFT

Where certificates of compliance are required, they shall list the requirement being certified, be signed by an authorized representative of the contractor, and include supporting documentation for the certification. The Government reserves the right to require additional demonstration/verification of the requirement covered by the certification, if needed.

Table I. Verification Methods

Table II. Requirements Verification Matrix

3.0 Requirements

3.1 Decontamination Efficacy

3.1.1 Decontamination Parameters

X

4.1.1

3.1.2 Decontamination Cycle Time

X

4.1.2

3.1.3 Aircraft Decontamination Materiel Damage

X

4.1.3

3.1.4 Aircraft Enclosure (AE) Size

X

4.1.4

3.1.5 Aircraft AE Ingress and Egress

X

4.1.5

3.1.5.1 Aircraft Placement In the AE

X

4.1.5.1

3.1.5.2 Equipment and Personnel Exit and Entrance

X

4.1.5.2

3.2 Operational Availability, Reliability, Maintainability

3.2.1 Materiel Availability (Am)

X

3.2.2 Reliability

X

3.2.3 Maintainability

X

3.2.4 Corrective Maintenance

X

4.2.4

3.2.5 Scheduled Maintenance

X

4.2.5

3.2.6 Down-Time

X

3.2.7 Service Life

X

4.2.7

3.3 JBADS System Implementation

3.3.1 Subsystems

X

4.3.1

3.3.1.1 Operational Configuration

X

4.3.1.1

3.3.1.2 Storage and Transport Configuration

X

4.3.1.2

3.3.2 Assembly and Disassembly Equipment

X

4.3.2

3.3.3 Material Handling Equipment

X

4.3.3

3.3.3.1 Storage /Transport Lifting and Tie Down

X

4.3.3.1

3.3.4 Assembly/Disassembly

3.3.4.1 Unpack and Assembly Time

X

4.3.4.1

3.3.4.2 Disassembly and Pack for Transport Time

X

4.3.4.2

3.3.5 Unpack, Setup, Teardown and Re-pack Personnel

X

4.3.5

3.3.6 Air Transport Certification

4.3.6*

3.3.7 Commercial Ground Transport

4.3.7

3.3.8 Sea Lift

X

4.3.8

3.3.9 Storage and Transport Configuration

4.3.9

3.3.10 Power Sources

X

X

4.3.11

3.4 Operator Requirements

3.4.1 Operator Personnel

X

4.4.1

3.4.2 Personnel Protective Equipment (PPE).

X

4.4.2

3.4.3 Operator Functions

X

4.4.3

3.4.4 Systems Controls

4.4.4

3.5 Operational Environments

3.5.1 External Operating Temperature

3.5.1.1 Low Temperature Operation

3.5.1.2 High Temperature Operation

3.5.2 Storage/Transport Temperature

3.5.2.1 Low Temperature Storage/Transport

3.5.2.2 High Temperature Storage/Transport

3.5.3 Rain

3.5.3.1 Rain During Storage and Transport

3.5.3.2 Rain During Operations

3.5.4 Humidity

3.5.4.1 Humidity During Storage/Transport

3.5.4.2 Humidity During Operation.

3.5.5 Blowing Sand and Dust

3.5.5.1 Blowing Sand and Dust During Storage/Transport

3.5.5.2 Blowing Sand and Dust During Operation

3.5.6 Vibration from Transportation

3.5.7 Transit Shock

3.5.8 Wind

4.5.8*

3.5.9 Snow Load

4.5.9*

3.6 Electromagnetic Environmental Effects

3.6.1 Near Strike Lightning (NSL)

3.6.1.1 NSL During Storage/Transport

X

3.6.1.2 NSL During Storage/Transport

X

3.6.2 Grounding

4.6.2*

3.7 Human System Integration

3.7.0 Life Cycle Safety and Health Hazards

X

4.7.0

X

4.7.1

4.7.2

4.7.3

4.7.4

3.7.5 Noise Protection

4.7.6

3.7.7 Emergency Shutdown

X

4.7.7

3.7.8 Lights and Video Cameras

X

4.7.8

4.7.8.1

3.7.9 Health Hazards

X

4.7.9

3.7.9.1 Control Module (CM)

X

4.7.9.1

3.7.9.1.1 CM Personnel Capacity

X

4.7.9.1.1

3.7.9.1.2 CM Inside Temperature

3.7.9.1.3 CM Temperature Excursions

4.7.10

4.7.11

4.7.12

4.7.13

*Verified by certification (See Par. 4.0.2)

4.1 Decontamination Efficacy.

4.1.1 Decontamination Parameters. It shall be verified by demonstration that the JBADS can maintain a temperature of 170oF +/- 5oF with a relative humidity of 90% +/- 5% throughout the AE and aircraft being decontaminated for a period of no less than 96 continuous hours.

4.1.2 Decontamination Cycle Time. It shall be verified by demonstration that the JBADS can perform a full decontamination cycle in no more than 240 hours (T), 144 hours (O), to include system temperature ramp up to the required conditions, 96 hours at the required conditions, and cool down to ambient temperature without the formation of condensation within AE or on any surface of the aircraft being decontaminated.

4.1.3 Aircraft Decontamination Materiel Damage. It shall be verified by analysis that the aircraft being decontaminated does not incur more materiel degradation by the decontamination process than is allowable in C-130 certification/guidelines to exclude LRUs (T), no materiel degradation (O).

4.1.4 Aircraft Enclosure (AE) Size. It shall be verified by demonstration that the AE can completely enclose a C-130J-30 aircraft.

4.1.5 Aircraft AE Ingress and Egress. It shall be verified by demonstration that the aircraft can ingress and egress when the AE is in place.

4.1.5.1 Aircraft Placement In the AE. It shall be verified by demonstration that the aircraft to be decontaminated may be pushed or pulled into the AE by an aircraft tug attached at the nose gear.

4.1.5.2 Equipment and Personnel AE Exit and Entrance. It shall be verified by demonstration that the aircraft tug and all personnel are able to exit the AE after the aircraft is in place and to re-enter the AE at the completion of decontamination.

4.2 Operational Availability, Reliability, Maintainability.

4.2.1 Materiel Availability (Am). It shall be verified by test and analysis that the JBADS Materiel Availability is at least 0.80 (T=O) using LRIP (or first production units).

4.2.2 Reliability. It shall be verified by test and analysis that the JBADS has at least a probability (P) = 0.87 (T), 0.95 (O) with a confidence of 80% of completing a 240 hour mission without an Operational Mission Failure. This shall be demonstrated using first production units.

4.2.3 Maintainability. It shall be verified by test and analysis that the JBADS Mean Time Between Operational Mission Failure is no less than 1,200 hours {2,400 hours}.

4.2.4 Corrective Maintenance. It shall be verified by demonstration that the JBADS Mean Time to Repair (Corrective Maintenance) is less than or equal to 120 (T) {30} minutes.

4.2.5 Scheduled Maintenance. It shall be verified by demonstration that JBADS scheduled maintenance is not required or performed during decontamination procedures.

4.2.6 Down-Time. It shall be verified by test and analysis that the JBADS maximum down time does not exceed 24 hours. (T=0)

4.2.7 Service Life. It shall be verified by analysis that JBADS has a 10 (T), {20} year service life.

4.3 System Implementation

4.3.1 Subsystems. It shall be verified by demonstration that the JBADS consists of three (3) subsystems: AE, ADU, and CM.

4.3.1.1 Operational Configuration. It shall be verified by demonstration that the AE, ADU, and CM integrate to form an operational configuration.

4.3.1.2 Storage and Transport Configuration. It shall be verified by demonstration that the JBADS storage and transport configurations are the same.

4.3.2 Assembly and Disassembly Equipment. It shall be verified by demonstration that JBADS can be assembled and disassembled by personnel using standard military and industrial MHE) (e.g. 25,000-lb all terrain fork-lift, 50-ton all-terrain crane, wrecker).

4.3.3 Material Handling Equipment. It shall be verified by analysis that all JBADS components that are not man portable can be handled with standard military and industrial equipment ) (e.g. 25,000-lb all terrain fork-lift, 50-ton all-terrain crane, wrecker).

4.3.3.1 Storage/Transport Lifting and Tie Down. It shall be verified by analysis that the JBADS lifting and tie-down provisions in storage/transport configuration meet the requirements of ISO standard 1496-1 and Defense Transportation Regulations Part VI, Chapter 604 for Safe Containers (CSC) certification.

4.3.4 Assembly/Disassembly.

4.3.4.1 Unpack and Assembly Time. It shall be verified by demonstration that after arrival of all system components at the decontamination site, the JBADS requires no more than 30 days to be unpacked and assembled for operation.

4.3.4.2 Disassembly and Pack for Transport Time. It shall be verified by demonstration that after completion of decontamination operations the JBADS requires no more than 30 days to be disassembled and packed for transport.

4.3.5 Unpack, Setup, Teardown and Re-pack Personnel. It shall be verified by demonstration that JBADS requires no more than 16 personnel to unpack, setup for operation, teardown, and re-pack for transport one JBADS.

4.3.6 Air Transport Certification. The requirement shall be verified by receipt of the JBADS certification for internal air transport by C-5 and C-17 with the supporting documentation, and the review thereof.

4.3.7 Commercial Ground Transport. It shall be verified by demonstration and analysis that JBADS is transportable by commercial ground transport over paved roads in the storage/transport configuration without any special USDOT or State permits.

4.3.8 Sea Lift. It shall be verified by analysis that the JBADS is transportable by sea lift in the storage/transport configuration.

4.3.9 Storage and Transport Configuration. It shall be verified by demonstration and analysis that all JBADS components are stored and transported within 20 or 40 foot ISO containers or in system unique configurations that are ISO container certified. That those containers are the primary means used for transportation. That by exception, items too large for 40’ ISO containers are protected by some other means and are capable of being loaded on standard 463L pallet trains to be loaded on C-17 and larger aircraft.

4.3.10 Power Sources. It shall be verified by test and analysis that JBADS is compatible with standard fielded and commercial power sources, local voltage & frequency, variable cycle compatible (50 and 60 cycle) and existing military generators which are defined as Class 2B per MIL-STD-1332. The JBADS shall be run for a period of not less than 24 hours on power that conforms to Class 2B as defined in MIL-STD-1332b at both 50 cycles and 60 cycles.

4.3.11 Power Distribution. It shall be verified through inspection and demonstration that the JBADS includes all items necessary to distribute power to its components to include any cables or connectors.

4.4 Operator Requirements.

4.4.1 Operator Personnel. It shall be verified by demonstration that JBADS requires no more than two personnel at a time to operate during decontamination procedures.

4.4.2 Personnel Protective Equipment (PPE). It shall be verified by demonstration that personnel wearing PPE (full face protection, gloves, and over garment) are capable of completing all required activities while they are in proximity of a contaminated aircraft. These activities include: assisting in the contaminated aircraft being placed within the enclosure, any construction needed to enclose the aircraft, and working near or in the contaminated aircraft or within 6 feet of the enclosure while the contaminated aircraft is undergoing decontamination.

4.4.3 Operator Functions. It shall be verified by demonstration that JBADS operators can monitor, control and record system parameters to effectively employ the system.

4.4.4 Systems Controls. It shall be verified by demonstration and analysis that the JBADS control system is in compliance with MIL-STD-1472F, to include but not be limited to, the sound level of any audible alarms, size of buttons and switches, as well as the color choices thereof..

4.5 Operational Environments.

4.5.1 External Operating Temperature.

4.5.1.1 Low Temperature Operation. The requirement shall be verified by test, as follows:

With the JBADS test article configured for operation (including power if applicable), perform an ambient air Basic Cold temperature test per guidance in MIL-STD 810G w/Change 1, Method 502.6, Category C1, Procedure II, or equivalent. Once the surface temperatures of the test item reaches 32 degrees F, the JBADS test article will soak for 4 hours. Upon completing the soak period, test personnel will enter the chamber and perform an operational check in accordance with the OM and NET to verify operability of all system components.

4.5.1.2 High Temperature Operation. The requirement shall be verified by test, as follows:

With the JBADS test article configured for operation (including power if applicable) perform an ambient air Basic Hot and Dry combined temperature and humidity test per guidance in MIL-STD 810G w/Change 1, Method 501.6, Category A1, Procedure II, or equivalent. Once the surface temperatures of the test item reaches 120 degrees F, the JBADS test article will soak for 4 hours. Upon completing the soak period, test personnel will enter the chamber and perform an operational check in accordance with the OM and NET to verify operability of all system components.

4.5.2 Storage/Transport Temperature.

4.5.2.1 Low Temperature Storage/Transport. The requirement shall be verified by test, as follows:

With the JBADS test article configured for storage/transport and, if applicable, packaged in a transit container, perform a Basic Cold temperature test per guidance in MIL-STD 810G w/Change 1, Method 502.6, Procedure I, Category C1 Induced Conditions, or equivalent. Once the interior surface of the ADU reaches 14 degrees F, and stabilizes, the JBADS test article will be cold soaked for at least 4 hours. Upon completing the soak period, test personnel will enter the chamber and inspect the ADU containers for damage or deformity resulting from exposure to low temperature.

4.5.2.2 High Temperature Storage/Transport. The requirement shall be verified by test, as follows:

With the JBADS test article configured for storage/transport and, if applicable, packaged in a transit container, perform a Hot-Dry temperature and humidity test per guidance in MIL-STD 810G w. Change 1, Method 501.6, Procedure I, Category A1 Induced Conditions. The temperature of the environmental chamber will be raised to 71°C (159 °F) and hot soaked for at least 4 hours after the surface temperatures of the test item reaches the target temperature. Following the soak period, test personnel will enter the chamber and inspect the ADU containers for damage or deformity resulting from exposure to high temperature.

4.5.3 Rain.

4.5.3.1 Rain During Storage and Transport. The requirement shall be verified by test, as follows:

With the JBADS test article configured for storage/transport and, if applicable, packaged in a transit container, perform a Blowing Rain test per guidance in MIL-STD 810G w/ Change 1, Method 506.6, Procedure I, using a rain fall rate of 4.0 inches/hour, at ambient temperature, a wind speed of 40 mph, for a duration of 30 minutes, and repeating until each of the four vertical sides and each edge/corner where two sides connect to form a seam and any opening have been tested, or equivalent.

4.5.3.2 Rain During Operations. The requirement shall be verified by test, as follows:

With the JBADS test article configured for operation perform a Rain and Blowing Rain test per guidance in MIL-STD 810G w/ Change 1, Method 506.6, Procedure I (Procedure II Exaggerated for the AE) using a rain fall rate of 2.0 inches per hour for a duration of 30 minutes, and repeating on each vertical side and each edge/corner where two sides connect to form a seam, and any opening, or equivalent.

There should be no evidence of major leakage. Major leakage is defined as water continually leaking and dropping off or running down the system’s inner surface which impairs the system’s intended military use.

4.5.4 Humidity.

4.5.4.1 Humidity During Storage/Transport. The requirement shall be verified by test during the high temperature testing.

4.5.4.2 Humidity During Operation. The requirement shall be verified by test during the high temperature testing.

4.5.5 Blowing Sand and Dust.

4.5.5.1 Blowing Sand and Dust During Storage/Transport. The requirement shall be verified by test, as follows:

With the JBADS test article configured for storage/transport and, if applicable, packaged in a transit container, perform a perform a Blowing Dust test per guidance in MIL-STD-810G w/Change 1, Method 510.6, Procedure I, using silica dust with a particle size of less than 149 um, an air velocity of 19.8 mph, at ambient temperature, for a duration of 90 minutes, and repeating until each of the four vertical sides and each edge/corner where two sides connect to form a seam and any opening have been tested, or equivalent.

Additionally, the requirement shall be verified by test, with the JBADS test article configured for storage and/or transport and, if applicable, packaged in a transit container, perform a Blowing Sand test per guidance in MIL-STD-810G w/Change 2, Method 510.6, Procedure II, using silica sand in natural conditions with a particle size from 150 through 850 um with a concentration of 0.18 g/m3, -0.0/+2.0 g/m3, at ambient temperature, a wind speed of 40 mph, for a duration of 90 minutes, and repeating until each of the four vertical sides and each edge/corner where two sides connect to form a seam and any opening have been tested, or equivalent.

4.5.5.2 Blowing Sand and Dust During Operation. The requirement shall be verified by test, as follows:

With the JBADS test article configured for operation perform a test following MIL-STD-810G w/Change 1, Method 510.6 Procedures I (Blowing Dust) and II (Blowing Sand) and TOP-1-2-621 for a duration of 90 minutes on each vertical side and each edge/corner where two sides connect to form a seam, and any opening, or equivalent.

4.5.6 Vibration from Transportation. The requirement shall be verified by test, as follows:

With the JBADS test article (e.g. ADU or AE component(s)) configured for storage/transport perform a test following MIL-STD-810G w/Change 1, Procedure 514.7, Test III, or equivalent.

4.5.7 Transit Shock. The requirement shall be verified by test, as follows:

With the JBADS test article (e.g. ADU or AE component(s)) configured for storage/transport perform a test following MIL-STD-810G w/Change 1, Method 516.7, Procedure II. The drop height shall be 3 inches.

4.5.8 Wind. This requirement pertains to the AE in the operational configuration. The requirement shall be verified by certification. A certificate of compliance with supporting analysis shall be available to verify that the JBADS system meets the requirements of Section 3.5.8.

4.5.9 Snow Load. This requirement pertains to the AE in the operational configuration. The requirement shall be verified by certification. A certificate of compliance with supporting analysis shall be available to verify that the JBADS meets the requirements of Section 3.5.9.

4.6 Electromagnetic Environmental Effects.

4.7 Human Systems Integration.

4.7.0 Life Cycle Safety and Health Hazards. It shall be verified by analysis that the JBADS does not present uncontrolled safety or health hazards to personnel throughout its life cycle.

4.7.8 Lights and Video Cameras. It shall be verified through demonstration that JBADS lights and video cameras inside the AE allow operators inside the Control Module to visually monitor personnel and aircraft within the AE.

4.7.8.1 Lights and Video Camera Wiring. It shall be verified by inspection that lights and video cameras are hardwired to the control module.

4.7.9 Health Hazards. It shall be verified through analysis that JBADS was designed to eliminate or minimize to the greatest extent possible any health impacts, so that system-generated illness and injury is minimized and mission readiness is not compromised.

4.7.9.1 Control Module (CM). It shall be verified by demonstration that that an environmentally conditioned shelter is provided for the control module.

4.7.9.1.1 CM Personnel Capacity. It shall be verified by demonstration that the CM shelter provides space for at least two operators to be present.

4.7.9.1.2 CM Inside Temperature. It shall be verified by test that the control module shelter is environmentally conditioned to a minimum internal temperature of 60 degrees F. and a maximum temperature of 80 degrees F.

4.7.9.1.3 CM Temperature Excursions. It shall be verified by test that all temperature excursions outside of the temperature range specified by 3.7.9.1.2 return to the specified range within a maximum time of 5 minutes from the time the cause of the temperature excursion is resolved (e.g. door is shut).

4.7.10 Operator Access. It shall be verified through inspection that operators do not have access to components with voltages exceeding 30V, that all exposed energized parts are guarded or covered regardless of voltage, and that the operator is not exposed to stored energy shock at the disconnecting means in accordance with UL 60950, paragraph 2.1.1.7.

4.7.11 Maintenance Protection. It shall be verified through inspection that protection is provided to personnel during maintenance and repair to prevent unintentional contact with voltages exceeding 70V, that current sources exceeding 25A are protected from accidental short-circuiting, that voltage measurements required by maintainers do not exceed 300V, that circuits and components exceeding 500V are completely enclosed and interlocked (non-by-passable), and that where interlocks are used, they comply with UL 60950, paragraphs 2.8.3 - 2.8.5.

4.7.12 Power Interfaces. It shall be verified through inspection that interfaces with power sources and disconnecting means are in accordance with NFPA 70-2002, and UL 60950, sec 3.4; and that equipment designed to have multiple-input power capabilities, or powered by a generator with multiple-voltage output capabilities are protected from damage when connected to incorrect input power/voltage levels.

4.7.13 Personnel Lighting. It shall be verified by inspection that the JBADS has lighting within the AE so that personnel can maneuver around inside the enclosure.

5.0 Packaging.

5.1 Packaging. For acquisition purposes, the packaging requirements shall be as specified in the contract.

6.0 Notes. None.