RSRV Centrifuge - Purchase Specification FINAL 20260323 v3_Redacted.pdf

CUI

1 PURPOSE / SCOPE

2 REFERENCE DOCUMENTS

2.1 General

2.2 Government Documents

2.3 Order of Precedence

3 REQUIREMENTS

3.1 Physical / Functional / Design

3.2 Performance

3.3 Enabling

3.4 Environmental, Safety, & Health (ESH)

3.5 Warranty and Service Life

3.6 Project Planning & Scheduling

4 VERIFICATION

4.1 Types of Verification

4.2 General

4.2.1 Phase I: Factory Acceptance Test (FAT)

4.2.2 Phase II: Site Acceptance Test (SAT)

5 SYSTEM DOCUMENTATION

6 CONTRACT DATA REQUIREMENTS

7 APPENDICES

8 ATTACHMENTS

1 PURPOSE / SCOPE

This purchase specification establishes the minimum requirements for the purchase of two centrifuge systems to replace the Applied Motion Technology precision centrifuges at Hill AFB UT. The new centrifuges will ensure continued support of operational acceptance/assurance (OA) testing, troubleshooting and repair, and aging and surveillance testing of the MMIII MK12A and MK21 Reentry Vehicles and their components and assemblies.

2 REFERENCE DOCUMENTS

All referenced documents, standards, and specifications shall be the latest revision in effect as of the date of contract award, unless otherwise specified.

2.1 General

The documents listed in this section are specified in Sections 3 and 4 of this document.

This section does not include documents cited in other sections of this document. While every effort has been made to ensure the completeness of this list, document users are cautioned that they must meet all specified requirements of documents cited in Sections 3 and 4 of this document, whether or not they are listed.

2.2 Government Documents

2.2.1 Specifications, Standards, and Handbooks – The following specifications, standards, and handbooks form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the solicitation or contract.

• MIL-DTL-26482: Electrical Connectors

• SAE-AS50151: Electrical Connectors

• AFMAN 17-1301: Computer Security

• JTR: Joint Travel Regulations (https://www.travel.dod.mil/Policy-

Regulations/Joint-Travel-Regulations/)

2.2.2 Other Government Documents, Drawings, and Publications – The following other Government documents, drawings, and publications form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the solicitation or contract.

• 08646 Slip Ring Wiring Schematic

2.3 Order of Precedence

In the event of a conflict between the text of this purchase specification and the references cited herein, the text of this purchase specification shall take precedence.

Nothing in this purchase specification shall supersede applicable laws and regulations unless a specific exemption has been obtained.

3 REQUIREMENTS

Note: The existing centrifuge systems at Hill AFB are two-platform systems with one platform used exclusively for counterweights. The 309th MMXG testing requirement is to run only one test article at a time, therefore both single-platform and two-platform systems are acceptable solutions for this acquisition.

3.1 Physical / Functional / Design

3.1.1 Size and Weight

a. Centrifuge maximum footprint (per centrifuge): 18’ Width x 18’ Depth x 8’ Height.

b. The centrifuge(s) shall be installed on existing 18’ x 18’ concrete slab(s). The weight of equipment and components during installation shall not exceed the surrounding raised floor capacity of 3,000 lbs. / ft2. Access for installation shall be through the shop loading dock door (approximately 10’ Width x 9’ Height).

c. Controller / Controller Desk maximum footprints: Approximately 10’ x 6’.

3.1.2 Electrical Power Available: 480 VAC, 3 Phase, 60 Hz and 120/208 VAC, 3 Phase, 60 Hz.

3.1.3 Mounting Platforms

a. Mounting Platforms shall be mechanically and electrically compatible with existing

Air Force Fixtures and Unit Under Test (UUT) cabling.

b. Mounting Platform size: 24” square minimum horizontal mounting surfaces with 4x4 grid bolt pattern (sixteen 5/8-11 thread inserts per platform on 5-inch centers).

c. Mounting Platform alignment holes: two 0.250” diameter 0.5” deep dowel pin holes

(layout shown in Figure 1.) to accommodate fixture alignment pins.

d. Package Size (volume containing fixture with attached UUT):

i. 24” cube minimum (24”x24”x24”).

ii. The design shall account for this envelope being positioned with up to a 3.0-inch overhang beyond the outer edge of the mounting platform.

iii. The contractor shall ensure the final design provides sufficient clearance between the volume (the 24” cubed envelope including overhang) and the interior walls of the safety enclosure (3.4.1 a).

e. Connector Location: 3” - 4” from the inboard edge of the mounting platform as shown in Figure 1.

3.1.4 Slip Rings

a. 76 channel slip ring capacity minimum with individually shielded leads. The shields shall be isolated electrically from the machine frame and spindle, with separate slip rings for each group of 15 shields. The spindle and rotating arm shall be grounded to the machine frame by separate slip rings.

i. The channel slip rings must meet the current carrying capacity of the input lines from / to the unit under test (UUT):

1. At least 76 lines at 10 Amps.

ii. Electrical noise – Less than 0.010 volts, 2 rings in series, over full G range.

3.1.5 Signal Wiring and Connectors

a. Static Resistance – Less than 0.250 ohms measured from arm mating connectors to external equipment connectors.

b. Connector pin outs / slip ring wiring and layout shall be compatible with existing Air

Force test equipment. (Layout as shown in Figure 4. and Figure 5. of this document).

Note: Figure 5. includes 3 connectors for each arm (side a and side b). Only one set of connectors is required.

c. Connectors for arm end(s) and for data acquisition shall be compatible with Air Force cables. (See Figure 4. for details).

d. Connector location / layout: UUT connectors shall be located on the inboard side of the mounting platform in a vertical plane 3” - 4” from the inboard edge of the mounting platform as shown in Figure 1. The UUT connector layout shall be as shown in Figure 2. and Figure 3. The connectors shall be mounted on a support bracket or bulkhead.

e. The contractor shall provide all extension cables necessary to connect Air Force test equipment / UUTs to centrifuge connectors.

3.1.6 Monitoring Devices

a. Run Time Meter: The system shall be equipped with a non-resettable Spindle

Accumulated Run Time Meter.

b. RPM Meter

i. The user interface shall provide a clear numerical readout of the actual (measured) RPM.

ii. The RPM display shall have at least 3 decimal places of resolution.

3.1.7 Controller/Computer

a. The system shall be provided with a personal computer and/or controller. If a computer is provided, it must have Windows 11 Enterprise Operating System, Microsoft Office, Intel i7 CPU (or later), 16 GB RAM (at a minimum), 500 GB Solid State Hard Drive (at a minimum), TPM 2.0 security-enabled, and a read-write optical drive.

b. Controller and complete centrifuge system shall meet Air Force security requirements in accordance with AFMAN 17-1301 Computer Security. The following capabilities are not allowed:

i. Wireless capabilities (e.g. Wi-Fi, Bluetooth, radio frequency, infrared wireless devices or any device capable of sending or receiving a wireless signal).

ii. Photographic or audio recording capabilities.

iii. An Air Force Systems Security Officer shall inspect IT equipment before install to ensure above capabilities are disabled or not included.

c. Control Modes

i. Manual – The desired RPM or G-level can be commanded, allowing operators to change speed in increments and terminate the test. The computer monitor shall display the commanded RPM and G-level and the real-time system RPM and G-level as numerical values during testing. These values shall be stable and easily readable.

ii. Automatic – Profile testing can be performed by programming the computer to perform G vs. Time profiles saved on the system. Profiles shall be programable in segments defined as an acceleration ramp (up or down) or steady state acceleration over a specified time duration. At least 50 segments can be programmed in sequence. The computer monitor shall display the real-time system RPM and G-level and commanded RPM and G-level as numerical values during testing. These values shall be stable and easily readable.

d. Control Features

i. The computer monitor shall provide a real-time graphical plot of the system

G-level versus time. This plot shall be active and continuously updated during all testing and in all control modes.

ii. Controller shall save and print G vs. Time profiles as-run on centrifuge

iii. Data Logging:

1. The controller shall automatically generate a unique comma-separated values (.csv) data file for every test run.

2. Each file shall contain, at a minimum, the following header information and data columns:

1. Header information:

a. Test Profile name

b. Date of Test

c. Test Radius

d. Test Weight

2. Data columns:

a. Time (in seconds)

b. Commanded G-level

c. System G-level

d. Commanded RPM

e. System RPM

f. Accelerometer Measurement (see 3.2.8)

3. The data logging rate shall be a minimum of 10 Hz.

iv. Definitions:

1. Commanded RPM/G-level: The target value set by the operator or profile.

2. System RPM/G-level: The calculated value from the centrifuge’s control system.

3. Accelerometer Measurement: The acceleration value at the UUT calculated using the arm accelerometer (see 3.2.8).

v. Controller shall take distance from center of rotation to UUT center of mass as an operator selectable input, allowing tests to run and be selected at all radii within the mounting platform (3.1.3 b) and package size envelope (3.1.3 d).

vi. Controller shall save pre-balanced arm configurations allowing operators to select and load saved auto balanced weight positions.

3.1.8 TEMPEST Environment and Security Compliance Confirmation

a. The area where this system will operate is a TEMPEST-controlled environment. Due to the strict security protocols of this location, all capabilities for wireless transmission or recording will be eliminated from the system as a non-negotiable requirement for its authority to operate.

b. In fulfillment of the security requirements outlined in section 3.1.7.b and the mandates of the TEMPEST-controlled environment, the following actions shall be confirmed:

i. All devices with Wi-Fi, Bluetooth, camera, and microphone capabilities will have these components physically removed from the hardware.

ii. If physical removal is not possible for any of the components listed above, they will be permanently disabled within the BIOS. This disablement will be done in such a way that a standard user cannot re-enable them.

iii. Contractor shall confirm and accept that an Air Force Systems Security Officer shall inspect the IT equipment before installation to provide final verification that these capabilities are physically removed or permanently disabled as required.

3.2 Performance

Performance requirements shall be met at all selectable arm radii as defined in section

3.1.7 d. v.

3.2.1 Centrifugal Capacity: 24000 G-pounds minimum per platform with the center of gravity of the test object up to 12 inches above the mounting surface of the rotating arm.

3.2.2 G Range: Zero (0) to one-hundred fifty (150) Gs minimum.

3.2.3 Speed Stability: Drift less than ± 0.02% per minute of set speed (RPM). Repeatability of

± 0.1% or less of set speed (RPM). Drift and repeatability requirements shall apply across the entire operational speed range of the system.

3.2.4 Load Capacity: 160 lbs. minimum on each mounting platform through full G range.

3.2.5 Acceleration Rates:

a. The system shall be capable of accelerating a 160 lb. test object from 0 G to 150 G and decelerating from 150 G to 0 G, in 15 seconds or less.

b. For any programmed G vs. Time profile operating at or below 6 G with a 160 lb. test object, the system shall meet the following ramp rates:

i. Maximum Deceleration Rate: A controlled deceleration of -1.6 G/s.

ii. Maximum Acceleration Ramps: A ramp from 0.2 G to 2.2 G in 1.7 seconds and 0 G to 2.5 G in 2.5 seconds.

c. When commanded or programmed to any steady-state G-level below or at 6 G with a

160 lb. test object:

i. The System G-level shall settle and hold that value to within ± 0.05 G.

ii. Overshoot Control: When ramping to any commanded G-level, the System G-level shall not exceed the final commanded value by 0.1 G or more.

3.2.6 Rate Accuracy: ≤ 0.1% of set speed from 10% of the max RPM to the max RPM.

3.2.7 Arm Accelerometer:

a. Centrifuge shall include an accelerometer mounted near the payload mounting platform that will measure acceleration to 0.1% or less of full scale (150 G). The system shall use the accelerometer signal and UUT radius to calculate and report acceleration at the UUT. The accelerometer signal will not be used in the feedback loop but shall be reportable and recordable by the control system.

b. The accelerometer shall be mounted in a location and manner that allows for easy access and switching by shop technicians.

c. The main operator interface shall include an option (e.g., a selectable checkbox or button) to display or hide the real-time calculated acceleration at the UUT. When enabled, this value shall be clearly labeled.

3.2.8 Centrifuge Arm shall include an automatic balancing system for dynamic balance of centrifuge loads to the following specifications:

a. The automatic balancing system shall be capable of dynamically balancing asymmetrical loads of up to 5 lbs. difference for either mounting platform.

b. System shall be able to reduce imbalance to one ounce (oz.) max.

c. Balancing system shall allow saving of balanced arm configurations (see 3.1.7 d. vi.).

3.3 Enabling

3.3.1 Delivery & Installation

a. The contractor shall assemble and install the system at Hill AFB. The contractor shall connect the system to the facility power connection point provided by the Government. The contractor is responsible for furnishing and installing any transformers, regulators, filters, or transitions that are components of the centrifuge system itself and required to interface with the Government-provided power source specified in Section 3.3.1(g). The contractor is not responsible for facility-side electrical work. All contractor-provided components and connections shall comply with the latest National Electrical Code.

b. Installation is considered complete only when the system is fully assembled, installed, and successfully passes all acceptance testing as defined in Section 4 of this document.

c. Shipping terms for all equipment, parts, and data shall be F.O.B. Destination, Hill Air Force Base, UT, with regard to transportation costs. The total contract price is inclusive of all packaging and transportation costs to the destination. Liability and risk of loss or damage shall transfer from the contractor to the Government once the delivery vehicle has arrived at its designated unloading point at Building 847, Hill Air Force Base, immediately prior to the Government beginning offloading procedures.

d. The Government shall be responsible for the offloading of the centrifuge and all associated components from the delivery vehicle, as well as all rigging and movement of the items to their final installation location within the facility. The contractor’s responsibility for installation and assembly shall begin only after the Government has placed the centrifuge system at its final installation point. The contractor may have a representative present to observe the Government’s offloading and movement activities.

e. The contractor and its representatives shall comply with all applicable regulations and security requirements governing visitation to Hill AFB

f. The contractor shall ensure installation and delivery procedures meet the size and weight restrictions of section 3.1.1 of this purchase specification.

g. The contractor shall provide to the Government (a minimum of 180 days prior to installation) all facility requirements necessary to install / operate the system (e.g.

anchor bolts, electrical hookup requirements, etc.).

3.3.2 Training

a. On-site training shall be provided by the contractor following installation and acceptance testing, consisting of a minimum of two (2) eight-hour days of operator and/or programming training and two (2) eight-hour days of maintenance training.

b. The training shall ensure Government personnel achieve a full understanding of the functions, operations, and maintenance of the centrifuges.

3.3.3 Testing and Acceptance

a. The contractor shall acceptance test the system at Hill AFB following delivery and installation IAW Section 4 Verification.

b. The Government has the final authority for acceptance of the test stand, control console, and all Technical Data and CDRLs associated with this specification.

3.3.4 Technical Data

The contractor shall prepare and provide at least three hard copies (paper) and at least three electronic versions (on CD) of items a. – g. These copies / electronic versions shall be provided to the Government at least 60 days prior to system installation.

All documentation and technical data shall be written in the English language and be grammatically correct. The Manuals shall be fully text searchable and contain a linked table of contents. The Manuals shall contain all information necessary to allow Hill AFB technicians to operate, maintain, and calibrate the system.

a. Operation Manual(s)

b. Maintenance Manual(s)

c. Calibration Manual(s)

d. Theory of Design Manual(s)

e. Illustrated Parts Breakdown (IPB)

i. For all special design parts not commercially available, the contractor shall prepare and provide engineering drawings which at a minimum meet ASME Y14.100 and Y14.5.

f. Comprehensive Theory of Operation Information

g. List of Recommended Spare Parts

i. Ensure each part is accompanied by a manual or drawing.

ii. The contractor shall provide a list of proposed spare parts necessary to sustain the centrifuges for the required 20-year life expectancy. The proposed spare parts list shall be delivered in accordance with CDRL A006, Proposed Spare Parts List.

iii. The contractor shall maximize use of Commercial Off-The-Shelf Parts (COTS). These parts should be delivered with maximum available technical details. COTS parts must not compromise the performance or reliability of the completed system.

3.3.5 Data Rights

a. All technical data and documentation delivered under this specification, including all items listed in section 3.3.4 a-g, shall be furnished to the U.S. Government with Unlimited Rights. Any data or software that the contractor intends to deliver with less than unlimited rights shall be explicitly identified and justified in the contractor's proposal prior to contract award.

b. In the event the contractor intends to deliver any data with less than unlimited rights, the contractor shall identify and assert such restrictions as part of their proposal.

Failure to assert such restrictions in the proposal shall result in the Government receiving unlimited rights to such data.

3.4 Environmental, Safety, & Health (ESH)

3.4.1 Safety Measures

a. Safety Enclosure

i. Solid shrouded safety guard to prevent injuries to equipment operators and bystanders due to rotating parts and loose test items. Shroud shall completely enclose the UUT and rotating arm.

b. Safety measures in the computer software to prevent the operator from overextending the capability of the centrifuges. These measures shall include calculating the maximum g-level or RPM level for the specific radius and weight of each test to ensure the g-lb. capacity of the machine will not be exceeded.

c. A dynamic unbalance interlock to automatically stop the centrifuge if an unbalance condition occurs (an unbalance condition is an imbalance greater than 1 oz., see 3.2.8 b.).

d. Door interlocks to prevent the centrifuge from starting if shroud doors are open or unlocked.

e. Door interlocks to automatically stop the centrifuge if shroud doors are opened or unlocked while arm is rotating.

f. Door interlocks to prevent opening of the shroud doors while the arm is rotating. This interlock function shall operate whether the system power is on or off.

g. Indicators in the form of lights, messages, etc. to notify operators of unsafe conditions in 3.4.1 c. – 3.4.1 f.

h. Emergency stop button / switch located in an easily accessible and visible location.

i. Password and Username protected Computer / Operator interface preventing unauthorized individuals from operating the machine.

j. Start-Up checklist within the software requires operators to confirm the following before proceeding with a test.

i. Verify the test item and fixture are secure.

ii. Verify there are no loose items / F.O.D. within the machine.

iii. Verify the centrifuge doors are closed and locked.

iv. Verify area is clear of non-essential personnel

k. The contractor shall prepare and deliver a Safety Assessment Report (SAR) in accordance with CDRL A005, Safety Assessment Report (SAR), at least 60 days prior to system installation.

3.5 Warranty and Service Life

a. Base Warranty Requirement: The contractor shall provide a baseline warranty for the entire system. To be considered technically acceptable, the base warranty shall meet the following minimum requirements:

i. The warranty period shall be for a minimum of twelve (12) months.

ii. The warranty period shall begin on the date of successful Site Acceptance

Test (SAT) completion.

iii. The warranty shall cover, at a minimum, all replacement parts required to remedy a defect in materials or workmanship.

iv. The warranty shall include a minimum spindle run-time guarantee of 1000 hours.

b. Shipping Costs for Warranty Items:

i. From Government to Contractor: The Government shall be responsible for all freight and shipping costs associated with sending defective or non-conforming parts from the Government's facility to the contractor's designated repair facility for warranty repair.

ii. From Contractor to Government: The contractor shall be responsible for all freight and shipping costs associated with delivering new or repaired warranty replacement parts back to the Government.

c. Required On-Site Support (Labor Rates and Travel):

In the event an on-site visit is required to remedy a warranty issue, the Government requires established pricing to prevent unfair post-award charges. To be considered technically acceptable, the offeror shall provide a binding, fully burdened hourly labor rate for an on-site technician.

i. Labor: Post-award on-site support shall be billed exclusively at this established hourly rate.

ii. Travel: All travel, lodging, and per diem required for on-site support shall be strictly reimbursable in accordance with the Joint Travel Regulations (JTR).

The contractor shall not apply profit, overhead, or administrative markups to travel expenses.

d. Response Time & Service Life:

The contractor shall provide an initial response to all warranty claims within 48 hours. If an on-site visit is required, the contractor shall have a qualified technician on-site within 5 business days.

e. The minimum sustainment and service life of the new centrifuges shall be 20 years.

The contractor shall provide a statement of the projected service life for the centrifuges and provide certification that the system is designed to meet this 20-year minimum. This certification shall be provided in accordance with CDRL A007, Certificate of Compliance.

3.6 Project Planning & Scheduling

a. The contractor shall develop, maintain, and deliver a detailed Integrated Master

Schedule (IMS) in accordance with CDRL A009, Integrated Master Schedule. The IMS shall be the primary tool for planning, executing, and monitoring all project activities.

b. The IMS shall be resource-loaded and include all major tasks, activities, and milestones required to complete the project, including but not limited to:

i. All CDRL submittals and Government approval periods.

ii. Procurement of long-lead materials.

iii. Fabrication and assembly.

iv. Factory Acceptance Testing (FAT).

v. Shipment and delivery.

vi. On-site installation.

vii. Site Acceptance Testing (SAT).

viii. On-site training.

c. The IMS shall clearly identify the project's critical path.

d. The initial baseline IMS shall be delivered within 30 days of contract award. An updated IMS shall be provided monthly thereafter, or as requested by the Government.

e. Preliminary Bill of Materials (BOM) and Long-Lead Items List:

Concurrent with the submission of the Integrated Master Schedule (IMS), the contractor shall deliver a Preliminary Bill of Materials (BOM) and Long-Lead Items List. This list is a non-CDRL deliverable required for Government acceptance under CLIN 0001. Government review and acceptance of this list will be based on its completeness and its alignment with the scope and schedule requirements of the contract.

i. Purpose: The purpose of this list is to provide the Government with early visibility into the project's critical path procurements and to validate that the contractor has identified all materials with significant lead times that could impact the approved IMS.

ii. Content: At a minimum, the list shall be provided in a sortable electronic format (e.g., Microsoft Excel) and shall include the following data for each major component and any item with a lead time greater than 30 days:

1. Component Name / Description

2. Manufacturer

3. Manufacturer's Part Number

4. Quantity Required

5. Estimated Lead Time in weeks

4 VERIFICATION

4.1 Types of Verification

1. Factory Acceptance Test Plan

2. Factory Acceptance Test Report

3. Site Acceptance Test Plan

4. Site Acceptance Test Report

4.2 General

Verification shall be accomplished through a two-phase process: a Factory Acceptance Test (FAT) and a Site Acceptance Test (SAT). The Government reserves the right to witness all tests. All test plans and reports shall be delivered as specified herein.

4.2.1 Phase I: Factory Acceptance Test (FAT)

a. FAT Plan: Prior to conducting the FAT, the contractor shall deliver a FAT Plan in accordance with CDRL A001, Factory Acceptance Test Plan, for Government review and approval. The plan shall identify and describe the tests and inspections that will be performed to verify the requirements of Section 3, including a quality conformance inspection and a performance test utilizing a mutually agreed-upon sample part.

b. FAT Execution: Upon Government approval of the FAT Plan, the contractor shall conduct the FAT at their facility. The FAT shall include, at a minimum:

i. Quality Conformance Inspection: A visual examination and verification of the machine's components, construction, and workmanship against the requirements of Section 3.

ii. Performance Test: The complete system shall be operated to run a mock test as defined in the approved FAT Plan to demonstrate the machine's capabilities and adherence to specified accuracies.

c. FAT Report: Upon completion of testing, the contractor shall deliver a complete FAT Report in accordance with CDRL A002, Factory Acceptance Test Report. Successful completion of the FAT and Government approval of the FAT Report is required before the equipment is authorized for shipment.

4.2.2 Phase II: Site Acceptance Test (SAT)

a. SAT Plan: Prior to equipment installation, the contractor shall deliver a SAT Plan in accordance with CDRL A003, Site Acceptance Test Plan, for Government review and approval.

b. SAT Execution: After the equipment has been delivered and installed at the Government facility (HAFB), the contractor shall conduct the SAT in accordance with the approved SAT Plan. The SAT shall include, at a minimum:

i. Post-Installation Inspection: A visual examination for any damage that may have occurred during shipment and installation.

ii. Geometric Verification: Documented verification of the machine's final geometry and alignment.

iii. Final Testing: Shall demonstrate the ability to successfully run asset profiles and testing profiles provided by the Government. Successful test runs configured with engineering assets and air force equipment shall also be required as part of testing to verify proper integration with simulation and measuring equipment.

7 APPENDICES

APPENDIX C – SAFETY

SAFETY, FIRE PROTECTION AND HEALTH

SPECIFICATION

INDUSTRIAL SAFETY REQUIREMENTS

OGDEN AIR LOGISTICS COMPLEX

UNITED STATES AIR FORCE

HILL AIR FORCE BASE, UTAH 84056

14 Jan 2026

Reviewed by:

Brent Day

OO-ALC/SE

801-586-1472

Control Number:

BD2601001

A. Safety Program Requirements

The contractor shall implement a safety program plan that ensures protection of Government personnel and property. The program shall consist of, as a minimum:

1. Mishap reporting, as defined in paragraph B1 below.

2. A Safety Plan that addresses, as a minimum, the subjects listed in Section II –Specific Requirements and shall be used during the performance of the work described in the contract. The Safety Plan shall be approved by OO-ALC/SE (Safety Office) prior to commencement of any work described in this contract.

3. Routine and recurring surveillance to ensure the safety requirements of this contract are enforced.

4. Competent personnel to provide surveillance of the Safety Plan.

5. Identification of segregated work site locations for operations that cannot be co-mingled with general industrial operations and the process for ACO approval of operations and changes at these specific sites.

6. All contractor personnel shall be trained and qualified to perform their duties safely.

7. The contractor shall include a clause in all subcontracts requiring the subcontractors to comply with the safety provisions of this contract, as applicable.

B. Mishap Notification

1. The contractor shall notify OO-ALC/SE Workflow (OO-ALC.SE.Workflow@us.af.mil) or the Hill AFB Command Post (801-777-3007) after normal duty hours, and the designated Government Representative (GR), i.e., the ACO, PCO, or DCMA QAR (Quality Assurance Representative) within one (1) hour of all mishaps or incidents at or exceeding $2,000 (material + labor) in damage to DOD property entrusted by this contract, even if the government is wholly or partially reimbursed. This notification requirement shall also include physiological mishaps/incidents. A written or email copy of ALL the mishap/incident notification shall be sent within three calendar days to the GR, who will forward it to OO-ALC/SE. For information not available at the time of initial notification, the contractor shall provide the remaining information no later than 20 calendar days after the mishap, unless extended by the ACO.

Mishap notifications shall contain, as a minimum, the following information:

(a) Contract, Contract Number, Name and Title of Person(s) Reporting

(b) Date, Time, and exact location of accident/incident

(c) Brief Narrative of accident/incident (Events leading to accident/incident)

(d) Cause of accident/incident, if known

(e) Estimated cost of accident/incident (material and labor to repair/replace)

(f) Nomenclature of equipment and personnel involved in accident/incident

(g) Corrective actions (taken or proposed)

(h) Other pertinent information

2. The contractor shall cooperate with all government mishap investigations. Additionally, if requested by government personnel or designated government representative (GR), i.e., the ACO, PCO, or DCMA QAR (Quality Assurance Representative), the contractor shall immediately secure the mishap scene/damaged property and impound pertinent maintenance and training records, until released by safety investigators.

3. The contractor shall provide copies of contractor data related to mishaps, such as contractor analyses, test reports, summaries of investigations, etc., as necessary to support the government investigation.

4. The contractor shall support and comply with the safety investigation and reporting requirements of DAFI 91-204, Chapters 1 – 5.

C. General Safety Requirements:

If the safety plan is modified, the contractor shall submit the proposed modification, in writing, to the Contract Administration Office safety representative.

The contractor is solely responsible for compliance with all federal, state and local laws, the Occupational, Safety and Health Act (OSHA) (Public Law 91-596) and the resulting standards, OSHA Standards 29 CFR 1910 and 1926, as applicable, Air Force Occupational Safety and Health Standards (AFOSH STD), to include DAFMAN 91-203, Air Force Occupational Safety, Fire, and Health Standards, DAFI 91-204, Safety Investigations and Reports, Contract Safety, and the protection of their employees.

Additionally, the contractor is responsible for the safety and health of all subcontractor employees.

The contractor shall ensure assigned personnel are adequately trained and qualified for the task being performed. Brief all personnel on the hazards involved with operations and applicable precautions to be taken. Should unidentified hazards arise, cease operations until actions are taken to eliminate or mitigate hazards to safe levels.

Compliance with OSHA and other applicable laws and regulations for the protection of contractor employees is exclusively the obligation of the contractor.

Note: AFOSH STDs are annotated because many of the Air Force Standards exceed the OSHA standard criteria. If a conflict is noted, the most stringent requirement takes precedence. The government shall assume no liability or responsibility for the contractor's compliance or non-compliance with such requirements. The contractor shall furnish to each of his/her employees a place of employment, which is free from recognized hazards.

The contractor shall brief his/her employees on the safety requirements of this contract and on hazards associated with prescribed tasks. The contractor is responsible for compliance with OSHA Public Law and the resultant standards identified within. In addition, the contractor is required to flow down the safety requirements/specification to all subcontractors. This applies to Federal Acquisition Regulation (FAR) 12 commercial acquisitions as well. This contract shall in no way require persons to work in surroundings or under working conditions which are unsafe or dangerous to their health. The contractor must coordinate and perform work so as not to impact the safety of government employees or cause damage to government property. This requires providing personnel with protective equipment and associated safety equipment as may be necessary. The contractor must also protect personnel from hazards generated by the work. If the contractor employs BILINGUAL speaking employees, they must post bilingual signs and have written procedures for specific tasks in applicable languages.

SECTION II – SPECIFIC REQUIREMENTS

The contractor’s prepared Safety Plan shall:

• Provide contact information for on-site personnel.

• Include a work hazard analysis of the worksite and operations to be performed to include baseline hazard identification and required control measures.

• Identify employee safety and health training requirements and the documentation process.

The contractor shall ensure that each element identified below is adequately addressed in detail in the safety and health plan:

PEDESTRIAN CROSSWALKS: All contractor personnel are required to use the closest crosswalk, or traffic-controlled intersection when crossing the road. Pedestrians must look both ways to ensure the coast is clear before stepping out into the crosswalk. Pedestrians DO NOT have the right of way unless they are already in the crosswalk. Contractor vehicle operators have the same responsibilities as pedestrians, to share the road and mutually observe and yield to pedestrians.

MOTOR VEHICLES: Contractor shall comply with the standards in: DoD Directive 5525.4, Enforcement of State Traffic Laws on DoD Installations", Nov 2, 1981, Para 3-4;

DODI 6055.4, DoD Traffic Safety Program, 20 Jul 99; AFI 91-207, USAF Traffic Safety Program, 22 May 07; Each applies to all persons at any time on an Air Force Installation and includes all leased, owned, or privatized property including housing areas. In addition:

AFI 13-213, Airfield Management, 29 Jan 08, Paragraphs 1.3.6 and 4.4.2.1 applies to all contractors, sub-contractors, vendors, commercial delivery companies, and all other private business vehicles who operate anywhere on Hill Air Force Base, including the airfield (to include the industrial areas and any buildings or hangars located upon the airfield) in support of their mission.

HOUSEKEEPING: Housekeeping shall be conducted according to the requirements in OSHA Standard 29 CFR 1910.141. CLEAN AS YOU GO will be enforced.

8 ATTACHMENTS

Figure 1. Mounting Platform Layout (inches).

Figure 2. UUT connector layout (inches). View is inboard towards the center of rotation.

s Figure 3. Mounting platform / connector orientation.

Figure 5. Slip Ring Wiring (current system).

(The government holds unlimited rights to this drawing, see Figure 6. for release letter).

Figure 6. Unlimited Rights Release Letter from Calistoga Consulting Co.