SOW_08.07.18.pdf

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Aerial Work Platforms Federal contract opportunity
Solicitation number
FA8125-18-R-0018
Issued by
Department of the Air Force Materiel Command Lifecycle Management Center Tinker Air Force Base

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Statement of Work (SOW) - Aerial Work Platforms

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South_B2280_Drawings.docx DOCX document
Question_and_Answers_2_-_AWP_South_Dock.pdf PDF
Solicitation_Amendment-2-AWP.pdf PDF
Question_and_Answers_for_AWP_South_Dock.pdf PDF
South_B2280_Drawings.docx DOCX document
Solicitation_Amendment-1-AWP.pdf PDF
Site_Visit_Details.pdf PDF
Solicitation-AWP.pdf PDF

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FY18 AERIAL WORK PLATFORMS

SOUTH DOCK B2280

STATEMENT OF WORK

TINKER AIR FORCE BASE, OKLAHOMA

STATEMENT OF WORK NO: MXDEB-SOW-JW001

07 August 2018

MXDEC-SOW-JW001

07 August 2018 Page 2 of 25

1. SECTION 1 – PROJECT DESCRIPTION.

1.1. Introduction. The 76th Aircraft Maintenance Group (76 AMXG) is responsible for performing Corrosion Control (CC) operations, paint removal and coating system tasks, on multiple Air Force weapon systems: KC-135, C-130, B-52, B-1, E-3, and Navy E-6. CC tasks are performed on these aircraft in building 2280 at Tinker Air Force Base, OK. The facility completes 50% of the paint and depaint operations at Tinker and is the most critical facility on base. The building consists of two docks, North and South dock. Both docks are rated Class I, Division I hazardous locations in which many paints, solvents, and chemical paint removers are used. The South dock is equipped with four (4) aerial work platforms (AWPs) that are used to position employees around aircraft while performing various corrosion control operations, and are the most vital pieces of equipment in the dock. They are critical to the performance of corrosion control operations and are used extensively.

1.2. Problem Statement. Building 2280, the Aircraft Corrosion Control Facility, is the most highly utilized facility in the 76th Aircraft Maintenance Group, operating three (3) shifts, 5-7 days per week. The AWPs frequently fail; increasing flow days and man-hours for multiple weapon systems (KC-135, B-52, B-1, E-3, E-6, C-130).

Frequent incidents have occurred (sometimes once a week) involving various mishaps with the AWP systems:

electrical and mechanical failures at all elevations up to 40 feet in the air, binding and scraping between the telescoping mast sections, inadvertent platform movement and abnormal operation causing damage to equipment and aircraft; cause significant safety hazards. When stranded, employees are placed at risk by utilizing emergency egress procedures; such as using a rope to descend from the platform to the ground.

An inspection was performed to determine why the incidents were occurring and to evaluate the structural integrity of the existing AWPs in the south dock of B2280; to determine whether the failing platforms should be replaced or overhauled. The study revealed several design flaws with the structure and supports and deformation of the structural components; ultimately recommending complete replacement to resolve them.

1.3. Scope of Work. The Contractor shall provide all equipment, labor, transportation, tools, consumables, design, fabrication, delivery, assembly, installation, inspection, testing, training, documentation, and any other items and services necessary to replace four (4) aerial work platforms in accordance with this Statement of Work (SOW).

The Contractor shall be responsible for insuring all services, parts, and Original Equipment Manufacturer (OEM) components provided under this contract are in accordance with (IAW) the terms and conditions outlined herein, conform to the manufacturer’s equipment specifications and this SOW.

1.3.1. Aerial Work Platform. The term “aerial work platform (AWP)” shall constitute a system of equipment which shall include the platform, mast, runways, bridge cranes, trolleys, tracks, utilities, fall protection, utilities and any other items that work in conjunction with operation of the equipment. The AWP is a working platform with a telescoping mast suspended from a trolley and runway system attached to the roof. The crane and mast systems are attached between the platform and trolley system to telescope the platform up and down. The platform can be lowered to the dock floor to allow personnel entry and lift themselves to any elevated work area around the aircraft. The contractor shall provide four (4) AWPs in accordance with this SOW and all industry and Air Force codes and regulations.

07 August 2018 Page 3 of 25

Figures: Photos of an aerial work platform

1.4. Phasing/Coordination. Due to the complexity of the aircraft schedule (schedules change constantly), all work shall be completed in phases to ensure minimal impact to production. The Contractor shall supply a phasing plan at the Preliminary Design Review (PDR) to show the proposed project phasing. The Contractor’s schedule shall be flexible due to the fact that production schedules constantly change.

1.5. Government Occupancy of Facilities. Remaining portions of the facility shall remain occupied throughout construction. The Contractor shall consult with the CO and the Project Engineer, Javiro Watley, 405-582-4714, to develop a timeline that accommodates the continued performance of user’s mission functions during the renovation. The Contractor shall be responsible for blocking off work areas.

1.6. Parts and Materials. The Contractor shall provide and use only new parts and material in performance of this SOW unless otherwise authorized by the Contracting Officer (CO).

1.7. Base Maps and Facility Layouts. Drawings for the installation area will be issued to the Contractor after contract award at the Contractor’s request. Data such as floor plan layouts; dimensions; structural, mechanical and electrical data, and location of underground utilities provided by the Government for existing and new construction are based on as-built documentation, field observation, and equipment selected as design basis by the Government. This information is to be considered approximate and shall be field verified by the Contractor. Several projects have occurred within this facility over the years and on-site conditions may be different than what is specified in the as-built drawings. Additional as-built drawings of previous projects are available for duplication from the Civil Engineering Support Department located in building 400, second floor.

1.8. Demolition. The Contractor shall demolish the four (4) existing AWPs and all associated components such as utilities, power, and any other components associated with the existing AWPs. The Contractor shall remove and dispose of all components of the existing AWPs. Rubbish and debris should be removed from Government property daily to avoid accumulation at the work site. Materials that cannot be removed daily shall be stored in the storage area. All recyclable materials to be removed and taken to a local recycling facility with any funds credited to the Government.

1.8.1. Existing Fall Protection. The AWPs should be removed without affecting the overhead fall protection systems. If the overhead fall protection systems are damaged, required to be removed, or determined to be unusable, the Contractor shall be responsible for the replacement and certification of the overhead fall protection systems in accordance with AFI 91-203 and ANSI Z359 fall protection requirements.

1.8.2. Hazardous Coating. The existing AWPs shall be considered hazardous, due to paint overspray in the facility over the years. Ensure the material is properly disposed of in compliance with all federal, state, local, Tinker AFB, environmental codes and regulations. The Contractor shall be trained, certified, and compliant

07 August 2018 Page 4 of 25 with all hazardous waste handling and disposal requirements during the demolition of the existing equipment.

1.9. Delivery. The Contractor shall be responsible for component preservation, packaging, loading, shipping, unloading, on-site placement, and storage at Tinker AFB IAW the manufacturer’s commercial practices unless otherwise specified herein. The Contractor shall provide a representative on-site during the receipt, assembly, installation, testing, and acceptance of any components provided under this solicitation. Availability of on-site storage areas cannot be guaranteed and will need to be coordinated through the CO and project engineer. The Contractor shall provide for off-site storage if on-site storage areas are unavailable.

1.10. Installation. The Contractor shall provide fully functional AWPs that comply with industry and Tinker AFB codes and regulations. The Contractor shall provide all necessary utilities and fall protection systems on the AWPs. The Contractor shall provide all engineering required to ensure the new AWP will fit and function as required by the Government for corrosion control tasks on all weapon systems at Tinker AFB;

which shall include (KC-135, B-52, B-1, E-3, Navy E-6, and C-130).The new AWP systems shall meet the following general requirements:

a. The AWP and all components shall be designed, rated, and approved for use in a Class I, Division I, hazardous location (Painting and Chemical Paint Removal operations) in accordance with National Fire Protection Association (NFPA) 70 regulations. All necessary electrical components (wiring, conduit, disconnect switches, etc…) necessary to provide electrical power for fully operational Aerial Work Platforms shall comply with Class I, Division I Hazardous Location requirements. All electrical systems shall meet NEC Code requirements and NEMA standards for wet locations (i.e. all electrical components shall be rated for use in a wet environment.)

b. The AWP shall be designed to move mechanically and travel in all directions (Up, Down, North, East, South, West, Clockwise, and Counterclockwise).

c. The AWP shall be manufactured to resist corrosion from chemical paint removal materials, surface pretreatment materials, and surface coating materials (i.e. alkaline soaps, phosphoric acid deoxidizers, chromic acid conversion coatings, Methyl Propyl Ketone solvents, phenolic and benzyl alcohol paint removers, water, etc.)

d. The AWP and all safety and limit switch controls shall be waterproof and designed for use in a wet environment.

e. The AWP shall meet all federal, state, and local Fire, Safety, and Health regulations.

f. Each AWP shall be capable of supporting a minimum of four (4) personnel along with tools, spray equipment, chemical barrels, hoses, and any other items required to be placed on the AWP during corrosion control operations.

g. The AWP shall be equipped with fall protection systems for a minimum of four (4) persons. Fall Protection Systems to meet all applicable OSHA 1910 requirements. Fall Protection systems also must meet the requirements of ANZI Z359 including, but not limited to use, design, and certification. The fall protection systems will allow the employee to access all areas of the aircraft. Documentation, manuals, drawings, and certification certificates shall be provided to the Government for maintenance, inspection, and annual recertification validation purposes. The contractor shall validate the performance of the fall protection system to the Government. Any existing fall protection systems located within the facility that are damaged, or required to be removed, determined to be unusable, the contractor shall be responsible for replacement of the fall protection systems in accordance with current OSHA fall protection requirements and provide the proper certifications to the Government.

h. The AWP shall have an emergency egress system to allow employees to escape from the platform in cases of inoperability or emergency situations. Documentation, manuals, drawings, and certification certificates shall be provided to the Government for maintenance, inspection, and annual recertification validation purposes. The contractor shall validate the performance of the emergency egress system to the Government. The egress system shall be designed to reduce the risk of injury to employees while egressing from the platform. The emergency egress system shall allow for a minimum of two personnel to egress from the platform simultaneously.

i. Collision Avoidance System: The system shall be designed to prevent the aerial work platforms from causing any damage to an aircraft or object that it may come in contact with from various positions (i.e., proximity sensing system, bumpers, etc.). Performance of the collision avoidance systems shall be validated by the government to determine multi-directional sensing capabilities and prevention of damage to an aircraft or object that the AWP comes in contact with.

j. Limit Switch Identification System: Each AWP shall have an indication system that identifies faults and where to troubleshoot the AWP for repairs. The location of the limit switch indication system shall be observable from the hangar floor.

k. Shop utilities used for corrosion control processes shall be provided on the AWP (water hoses, breathing air, compressed air, HEPA vacuum dust recovery systems, explosion proof lights, etc…). Multiple shut-off valves/disconnect switches shall be properly located for isolation of the energy source. Personnel shall be able to shut off a utility along the wall, while standing on the floor of the hangar in addition to other areas as deemed appropriate. (i.e. water shut off valves, compressed air and breathing air shut off valves, etc.). Ensure utility fittings are different to ensure safety of employees. (Breathing air fittings, shop air, water hose, etc…should not be able to be plugged into each other). A portable breathing air filter purification system equivalent to existing equipment located on the AWP shall be provided by the contractor.

l. Hose Clamps for supporting the weight of chemical hoses during corrosion control operations shall be provided on the AWP (i.e. alkaline soap hoses, skin brightener hoses, Alodine hoses, etc.). A minimum of two hose clamps are required for each AWP.

m. The AWP shall have an open platform (no enclosed cages). The front of the AWP shall allow personnel to work unobstructed in accessing the surface of the aircraft.

n. The AWP shall be operated with Remote Control Units. The remote controls shall be FM or UL certified for operation in a Class I, Division I hazardous location. The remote control units shall be waterproof and chemical resistant, and be designed to withstand damage from a drop from the aerial work platforms. Additional batteries and charging system shall be provided for 24 hour usage of the remote control units. The minimum battery life shall be 1-shift (8-hours). The battery charger shall have an indication system that validates when a battery is charged for full operation of the equipment, the battery needs charging, and a battery condition is bad and requires replacement.

o. The AWP shall be equipped with a dead man switch system to allow the “operator” and the “spotter” to establish communication prior to operation of the AWP, and provide a safety mechanism to prevent damage to personnel and aircraft during operation.

p. The AWP shall be equipped with a minimum of two (2) Master Remote Controllers to be used when one of the 07 August 2018 Page 5 of 25 primary AWP remote control units fails.

q. The AWP shall be equipped with an Audible/Visual alarm notification system during operation to alert personnel the AWP is in operation. The volume of the audible alarm shall be adjustable to minimize the noise within the facility. The audible/visual alarm shall be different from other warning systems in the hangar bay.

r. The AWP shall be designed with limit switches that will prevent the AWP from colliding with each other.

The distance between the AWP shall allow simultaneous usage of the AWP on the wings of all aircraft (KC-135, B-1, B-52, E-3, E-6, C-130, and Navy C-130). The platforms shall be designed to have a stand-off distance which will prevent them from colliding with one another, but also allow them to move close enough to each other to allow personnel to work on the leading edges and trailing edges of the same aircraft wing.

s. The AWP shall be designed whereas the mast of the platform does not protrude underneath the bottom of the platform to help prevent accidental damage to the aircraft.

t. The AWP shall be capable of accessing all areas of the aircraft: The AWP shall have 360 degree rotation. The entire fuselage of an aircraft from nose to tail (minimum length = 195’), from top to bottom (minimum height = 43’). The AWP shall travel to within 1’ above the finished floor to allow employee access onto the AWP. The AWP shall have a minimum area of 20’ x 6’. The inboard wings, verticals, horizontals, E-3 pedestals and rotodome shall all be accessible from the AWP. The AWP shall not have any sharp edges that may impact an aircraft nor hurt an employee. The aerial work platform shall have enough space on the platform for equipment (55-gallon chemical barrels and 5-gallon spray paint pots for CC tasks) and personnel.

u. The employees shall be able to move freely from the AWP to the aircraft with the use of an OSHA/ANZI certified fall arrest system. The fall protection system shall be designed to allow employees to reach beyond the AWP to perform task on top of the aircraft inboard section of wings where the existing overhead fall arrest systems does not allow access. Personnel shall be able to access difficult areas on all aircraft painted within the facility (KC-10, KC-135, B-1, B-52, E-3, C-130, and Navy C-130).

v. The AWP system shall be clearly labeled to identify the equipment number, weight capacity, and date of manufacture, date of certification/recertification of each of the AWP. An indelible metal plate shall also be located on the AWP with the Contractor contact information, date of manufacturer, address, telephone, etc…

w. The AWP shall have a non-slip platform surface to help prevent personnel from slipping and falling while using slick corrosion control materials. All walking surfaces of the platform shall be clear of any trip hazards. There shall be no open gaps greater than 1-inch on the working surface. Any steps that may be used in the design of the APW shall not pose a trip hazard as demonstrated by the Government.

x. It is recommended that parts which are commercially available are used to minimize downtime of the AWP for repair. The government shall be provided the model number, serial number, vendor contact information, and lead time associated with procurement of these items. Spare parts with long lead times shall be provided to help minimize equipment maintenance downtime.

y. The AWP shall be electrically grounded and equipped with electrical grounding points to prevent static discharge of equipment on the AWP. The AWP are used to perform electrostatic painting operations, and clearly defined grounding points are required to help prevent electrical discharge from static electricity.

z. The AWP shall be equipped with fixtures for operation of the remote control units and to store the remote 07 August 2018 Page 6 of 25

07 August 2018 Page 7 of 25 control units once the AWP has been properly positioned. The fixtures shall be positioned to allow personnel visual access to see the edge of the AWP while in operation.

aa. The AWP shall be equipped with a removable tray that can be attached to the railing and removed as needed.

The tray shall be positioned on the platform side of the AWP allowing personnel a designated location for placing technical manuals, stencils, tools, etc., while performing operational tasks. The tray shall be designed with edges to prevent items from falling off the tray. The tray design may require rubber seals for bump protection.

bb. The AWP shall be equipped with a fixture to secure 55-gallon barrels to the AWP. The fixture should be removal for tasks where it is not required and should take up minimal space while it is being used. The unit may be attached to the guardrail.

cc. The AWP shall be equipped with a large paper roll dispenser, used for holding 36” masking paper materials.

dd. The AWP shall be designed to preclude leakage of lubricants onto the aircraft or the floor. Components which cannot be made leak proof shall be fitted with drip pans which can be easily removed for maintenance.

ee. There shall be an overload alarm for each AWP which indicated a load greater than the preset maximum.

1.10.1. Facility Structure. The Contractor shall utilize the existing facility structure to support the AWP system. The Contractor shall provide load requirements to the Government for verification. The contractor is responsible for ensuring that a turnkey system is designed to work within the facility.

1.10.2. Utilities. It shall be the responsibility of the Contractor to verify conditions and Pre- Construction Items, including location and depth of all utilities in the immediate construction area. Contractor is responsible for connecting utilities to support their AWP design.

1.11. Training.

1.11.1. Using Personnel. The Contractor shall provide user training on proper operation of the AWPs for 200 personnel on three shifts (day shift, swing shift, and graveyard shift). During the operational training, employees shall be trained on what to check for prior to operation and any notifications and signals that the AWP’s are not functioning properly.

1.11.2. Maintenance Personnel. The Contractor shall provide maintenance training for operation and maintenance of the equipment for 30 maintenance personnel (MXSG) on three shifts (day shift, swing shift, and graveyard shift). The maintenance personnel are responsible for remedial and preventative maintenance on the AWP.

1.12. Working Hours. Standard and Non-Standard work hours shall be required for this project. The Contractor shall work 3 shifts (24 hours), 7 days a week when working in building 2280 South dock. The Contractor shall also work on federal government holidays to meet the schedule. Work during federal holidays and base closures shall be coordinated through the CO. Work shall be accomplished around aircraft schedules to minimize impact to production.

1.13. Period of Performance. The Contractor shall complete all work within 19 months after contract award date.

07 August 2018 Page 8 of 25

1.14. Warranty. The Contractor shall provide a full warranty on all components and workmanship for a period of 365 calendar days after the date of final acceptance. The Contractor shall provide diagnosis, preventive maintenance, and repairs during testing and evaluation period and 365 calendar days after the date of final acceptance. Government use of the AWPs, before the date of final acceptance, shall not be deemed part of the warranty period. The Contractor shall complete all warranty work on-site at Tinker AFB.

1.15. Technical Support. The Contractor shall be available to provide technical support for maintenance of the equipment, and shall respond within 12 hours of being contacted.

1.16. Maintainability and Useful Life. Design, construction methods, and materials used in the manufacture of the AWP’s and components shall incorporate ease of maintenance to provide durable and sustainable operation or for a desired useful life of 25 years. Contractor shall provide components, equipment, and parts that are commercial off the shelf (COTS) to the greatest extent possible. Contractor shall identify all components, equipment, and parts that are not COTS. All components in units shall be easily accessible and removable for maintenance and replacement.

2. SECTION 2 – MANAGEMENT AND DOCUMENTATION REQUIREMENTS.

2.1. Program Management. The Contractor shall provide a program plan describing work task, schedule, cost, and deliverables within thirty (30) calendar days after contract award. A program kickoff meeting shall be conducted after task award and prior to delivery of the program plan to ensure all parties fully understand the requirements and are ready to proceed. Technical Interchange Meetings (TIMs) shall be convened at intervals as required by the Contracting Officer’s Technical Representative (COTR). The Contractor shall prepare the agenda and minutes of the TIMs. The Contractor shall prepare and deliver monthly status reports to the Contracting Officer (CO).

Informal communication through face-to-face, telephone, electronic mail, and facsimiles throughout the project is encouraged and shall be supported. All communication either formal or informal shall be documented in writing and shall become a permanent portion of the next scheduled TIM minutes. Any communications either formal or informal that are not introduced as official items at the next scheduled TIM shall not be interpreted as approved by or for the Government.

2.2. Preliminary Design Review (PDR). The Contractor shall host a PDR. The Government will provide facilities for the PDR at Tinker AFB. The Contractor shall provide a seven (7) calendar day notification of the meeting to the CO. The PDR shall be conducted within thirty

(30) calendar days after contract award. A design review data package and integrated master schedule shall be provided by the Contractor prior to the PDR. The Contractor shall present their proposed conceptual drawings to the Government with design submittals. These submittals shall completely and intuitively depict how the components are connected, the proposed requirements for unit transport and positioning, and government furnished utility requirements. The Contractor shall prepare the agenda and minutes for the PDR.

The conceptual drawings shall provide three-dimensional views of all requested system parts. Each view shall clearly label all dimensions in inches. The Contractor shall provide engineered final assembly drawings (3 sets) that completely and intuitively convey all information necessary to understand and visualize the completed assembly. This information shall include general assembly, wiring diagrams, and assembly relationships between component units. Assembly drawings shall include two (2) dimensional views detailing fittings, 07 August 2018 Page 9 of 25 wiring, and other components. All required hardware to achieve final assembly shall be annotated on the drawings or on an attached parts list.

In establishing a preliminary design, the Contractor shall address the following:

• Design

• Utility Requirements (electrical power, water, breathing air, shop air, etc.)

• Preliminary System Safety Hazard Analysis Report

• Preliminary Engineering Design Analysis

• Phasing – Minimize impact to production while installing AWP system. Provide a preliminary timeline for this project

2.3. Detailed Design Review (DDR). The Contractor shall host a DDR at Tinker AFB after the PDR is reviewed and the CO has provided written comments. The Contractor shall complete the DDR within 14 calendar days after CO has provided written comments. The Contractor shall provide a seven (7) calendar day notification of meeting request to the CO. All of the CO directed changes shall be incorporated into the Detailed Design. A design review data package and integrated master schedule shall be provided by the Contractor prior to the DDR. The Contractor shall prepare the agenda and minutes for the DDR. The CO shall review and approve the DDR minutes within five (5) business days after the meeting. The Contractor shall address the following:

• Design

• Utility Requirements

• Personnel Training

• Final System Safety Hazard Analysis Report

• Critical Engineering Design Analysis

• Equipment Technical Data

• Warranty Description

• Phasing – Work shall be broken into phases to accommodate aircraft schedule

• Spare Parts and Proprietary Tools

The design shall be reviewed by the Government and the CO shall provide the Contractor written comments.

All of the CO directed changes shall be incorporated into the final design. Based on the comments, the CO may require additional submittals of the design drawings and design analysis.

2.4. Functionality Validation. The Contractor shall support Government personnel with a fully functional checkout/demonstration of the system in association with various aircraft in dock. This functionality check shall be performed by the Contractor in conjunction with Government personnel. Government personnel will reserve the right to be present during all functionality checks and to verify functionality of the equipment for Production operational use. Testing parameters for the functionality validation shall be provided for CO approval during the PDR. If any discrepancies are noted, the Contractor shall document the deficiencies and provide corrective actions for submission to the COTR and CO for approval, prior to making corrections on all applicable drawings and documentation. Any changes necessary (technical or non- technical) shall be requested by the COTR to the CO and then issued by the CO to the Contractor.

2.5. Drawings and Other Data to Become Property of the Government. All designs, drawings, 07 August 2018 Page 10 of 25 specifications, notes and other works developed or modified in the performance of this contract shall become the sole property of the Government and may be used on any other design or construction without additional compensation to the Contractor. The Government shall be considered the “person for whom the work was prepared” for the purpose of authorship in any copyrightable work under 17 United States Code (U.S.C.)

201(b). With respect thereto, the Contractor agrees not to assert or authorize others to assert any rights nor establish any claim under the design patent or copyright laws. The Contractor for a period of three (3) years after completion of the project agrees to furnish all retained works on the request of the CO. Unless otherwise provided in this contract, the Contractor shall have the right to retain copies of all works beyond such period IAW Defense Federal Acquisition Regulation Supplement (DFARS) Clause 252.227-7023.

2.6. As-Built Drawings.

2.6.1. On-Site. The Contractor shall keep “approved for construction” work plan drawings and specifications on site throughout construction for quick reference for discussions.

2.6.2. Revisions. All work plan drawings which form part of the Project's construction contract shall be revised as required by the Contractor during work plan and construction, with revision dates noted, in order to accurately convey actual construction in place.

2.6.3. Field Verified. All work plan drawings shall be stamped 'field verified as-built' by the Contractor prior to the final submittal. Both hardcopy sets and electronic CAD files of the field verified as-built drawings shall be delivered to the CO prior to the Project's final inspection.

2.7. Operation Manuals. The Contractor shall provide operation manuals and AWP instruction sheets for future training and operational use. The Contractor shall furnish six (6) hardcopies of each at completion.

Electronic versions of the manuals shall be provided in addition to the six

(6) hardcopies.

2.8. Inspection & Maintenance Manuals. The Contractor shall provide maintenance manuals and supply recommendations for an on-going maintenance program. Manuals shall include recommended inspection criteria, intervals, and periodic and long-term maintenance operations. The Contractor shall provide an illustrated parts breakdown showing part numbers for replacement parts and include quantities and frequency of repair parts to be kept on hand for future repairs. The manual shall contain disassembly and assembly procedures. The Contractor shall provide six (6) hardcopies of each at completion. Electronic versions of the manuals shall be provided in addition to the six (6) hardcopies.

2.9. Spare Parts List. The Contractor’s recommended spare parts list. The Contractor shall identify components, equipment, and parts that are commercial-off-the-shelf (COTS) by providing the manufacturer, model number, serial number, and vendor contact information. The Contractor shall identify all components, equipment, and parts that are not COTS by providing all details on future procurement of those items.

2.10. Spare Parts Kit. The Contractor shall provide a spare parts kit based on the Contractor’s recommended spare parts list. Proprietary or uncommon tools required for maintenance or assembly shall be provided in the quantity of two (2) per AWP.

2.11. Lock Out Tag Out Procedure Documentation. Contractor shall provide a completed OC-ALC Form 493 (static.e-publishing.af.mil/production/1/oc-alc/form/oc-alc/oc-alc493/oc-alc493.pdf) concerning lock

07 August 2018 Page 11 of 25 out tag out procedures for each of the four (4) aerial work platforms. These four (4) completed forms will be provided NLT the day of training for MXSG, so that any questions concerning lock out tag out can be posed at the training.

3. SECTION 3 – PRODUCT DESCRIPTION.

3.1. Maintainability and Useful Life. Design, construction methods, and materials used in the manufacture of the AWP’s and components shall incorporate ease of maintenance to provide durable and sustainable operation or for a desired useful life of 25 years. The Contractor shall provide components, equipment, and parts that are commercial-off-the-shelf (COTS) to the greatest extent possible.

3.2. Explosion Proof Requirements. The AWP and all components shall be designed, rated, and approved for use in a Class I, Division I, hazardous location (Painting and Chemical Paint Removal operations) in accordance with National Fire Protection Association (NFPA) 70 regulations. All electrical components shall comply with Class I, Division I Hazardous Location requirements. All electrical systems shall meet NEC Code requirements and NEMA standards for wet locations.

3.3. Static Electricity. The AWP shall be electrically grounded and equipped with electrical grounding points to prevent static discharge of equipment on the AWP. The AWP are used to perform electrostatic painting operations, and clearly defined grounding points are required to help prevent electrical discharge from static electricity.

3.4. Corrosion Resistance. The AWP shall be manufactured to resist corrosion from chemical paint removal materials, surface pretreatment materials, and surface coating materials; alkaline soaps, phosphoric acid deoxidizers, chromic acid conversion coatings, methyl propyl ketone solvents, phenolic and benzyl alcohol paint removers.

3.5. Equipment Operation. The AWP shall be designed to travel in all directions; Up, Down, North, East, South, West, Clockwise, and Counterclockwise. The AWP shall be equipped with an audible and visual alarm notification system during operation to alert personnel the AWP is in operation. The volume of the audible alarm shall be adjustable.

3.5.1. Collision Avoidance. The AWPs shall be designed with limit switches that will prevent the AWPs from colliding with each other. The platforms shall be designed to have a stand-off distance which will prevent them from colliding with one another, but also allow movement close enough to each other to allow personnel to work on the same aircraft wing. The system shall be designed to prevent the AWPs from causing any damage to an aircraft or object that it may come in contact with from various positions; proximity sensing system and bumpers.

3.5.2. Operating Range. The AWP shall have 360 degree rotation. The AWP shall travel to within 1’ above the finished floor to allow employee access onto the AWP. The AWP shall not have any sharp edges that may impact an aircraft and injury employees.

3.6. Capacity. Each AWP shall be capable of supporting a minimum of four (4) personnel along with tools, spray equipment, chemical barrels, hoses, and any other items required on the AWP during corrosion control operations.

3.7. Fall Protection. The AWP shall be equipped with a fall protection system for a minimum of four (4)

07 August 2018 Page 12 of 25 persons IAW AFI 91-203 and ANSI Z359. The fall protection systems will need to meet all current regulations and allow the employee to access all areas of the aircraft while complying with swing fall limits IAW AFI 91- 203 and ANSI Z359. The Contractor shall provide documentation, manuals, drawings, and certification to the Government for maintenance, inspection, annual recertification, and validation purposes. The employees shall be able to move freely from the AWP to the aircraft while using the fall protection system. The fall protection system shall be designed to allow employees to perform tasks on top of the aircraft inboard section of wings where the existing overhead fall arrest system does not allow access; and allow access to difficult areas on all aircraft painted within the facility.

3.8. Emergency Egress. The AWP shall have an emergency egress system to allow employees to exit the platform in cases of inoperability or emergency situations. The emergency egress system shall comply with AFI 91-203 and ANSI Z359 and be safe to use for monthly training exercises. The emergency egress system shall be designed to allow multiple persons to egress the platform simultaneously. The Contractor shall provide documentation, manuals, drawings, and certification certificates to the Government for maintenance, inspection, annual recertification, and validation purposes.

Utilities. Shop utilities used for corrosion control processes shall be provided on the AWP; water hoses, respiratory protection (breathing air), compressed air, HEPA vacuum dust recovery systems, lighting. Shut-off valves/disconnect switches shall be properly located for isolation of the energy source. Personnel shall be able to shut off AWPs and AWP utilities from a location on the dock wall, while standing on the floor of the hangar in addition to other areas as deemed appropriate; water shut off valves, compressed air, and breathing air shut off valves. Ensure utility fittings are different between systems to ensure safety of employees (breathing air fittings, shop air, water hose, etc…shall not connect to each other). The portable breathing air filter purification system that is equivalent to existing equipment shall be provided by the Contractor. Hose clamps for supporting the weight of chemical hoses during corrosion control operations shall be provided on the AWP (i.e. alkaline soap hoses, skin brightener hoses, Alodine hoses, etc.).

3.9. Platform Design. The AWP shall have an open platform design (no enclosed cages or rails). The front of the AWP shall allow personnel to work unobstructed while accessing the surface of the aircraft. The AWP

3.10. shall be designed where components do not protrude from the bottom of the platform to help prevent accidental damage to the aircraft. The AWP shall have a non-slip platform surface to prevent personnel from slipping and falling while using corrosion control materials. All walking surfaces of the platform shall be clear of any trip hazards. Any steps that may be used in the design of the APW shall not create a trip hazard.

The AWP shall have enough space on the platform for all equipment and a minimum of four (4) personnel.

3.11. Controls. The AWP shall be operated locally and remotely.

3.11.1. Remote Control. The AWP shall be operated remotely from a Remote Control Unit (RCU) that is UL certified for operation in a Class I, Division I hazardous location. The RCU shall be waterproof, chemical resistant, and be designed to withstand damage from a drop from the AWP. Additional batteries and charging systems shall be provided allowing 24 hour use of the RCU. The minimum battery life shall be eight (8) hours. The Contractor shall provide three

(3) RCUs per AWP (12 RCUs total) that are coded to operate only that AWP. The Contractor shall provide four (4) master RCUs that are selectable to operate any one (1) of the four (4) AWPs. The Contractor shall provide eight (8) battery chargers. The battery charger shall have a diagnostic system, utilizing lights to alert the user when the battery is fully charged and when the battery condition is bad and needs replacing. Each

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AWP shall be equipped with fixtures for operation of the RCU and to store the RCU once the user AWP has accessed the AWP. The fixtures shall be positioned to allow personnel to stand comfortably for long periods of time while using the RCU. The fixtures shall be positioned to allow personnel visual access to the edge of the AWP while in operation. The RCUs shall also be equipped with emergency stop controllers that the Spotter may operate in conjunction with each platform. The E-Stop will establish communication between the AWP driver and the Spotter on the floor. It will also allow the Spotter to stop movement of the AWP if eminent danger to an aircraft, object, or personnel is observed.

3.11.2. Local Control. The AWP shall be operated locally from a fixed control interface on the AWP that is compliant with Class 1, Division 1 specifications. The controls shall be positioned to allow personnel to stand comfortably for long periods of time while operating the AWP. The fixtures shall be positioned to allow personnel visual access to the edge of the AWP while in operation.

3.12. Diagnostics. The AWP shall have a diagnostic system that identifies system faults and fault locations to assist in AWP repairs.

3.13. Work Bench. The AWP shall be equipped with a removable work table giving personnel a designated location for placing technical manuals, stencils, and tools while performing tasks. The tray shall be designed with edges to prevent items from falling off the tray. The tray design may require rubber seals for personnel bump protection.

3.14. Barrel Fixture. The AWP shall be equipped with a removable fixture to secure one (1) 55 gallon barrel to the AWP. The fixture shall be designed to use minimal space while on the platform.

3.15. Paper Fixture. The AWP shall be equipped with a removable fixture to secure one (1) masking paper roll to the AWP. The fixture shall be designed to hold a roll of masking paper that is 36 inches tall.

3.16. Markings. The AWP shall be permanently labeled, with heavy duty labels, to identify the equipment number, weight capacity, manufacture date, certification date, manufacturer contact information, and recommended length of fall protection self-retracting lanyard (SRL). Labeling shall be covered to prevent contact with paint overspray.

4. SECTION 4 – ENVIRONMENTAL PROTECTION AND SAFETY.

4.1. Environmental Protection & Safety. The Contractor shall be knowledgeable of and comply with all applicable federal, state and local laws, regulations, instructions and requirements regarding environmental protection and occupational safety and health. The Contractor shall comply with all safety practices posted in the assigned work area and the attached Appendix A. The Contractor shall comply with the current revision of the codes, instructions, regulations, and standards specified in Appendix A. The Contractor shall comply with any laws, instructions or regulation changes during the term of this contract.

The Contractor shall comply with Tinker Air Force Base (TAFB) Supplement to Air Force Instruction (AFI) 32-7086, “Hazardous Materials Management”, Tinker AFB procedures per Tinker Air Force Base Instruction (TAFBI) 32-7004, “Hazardous Waste Management”, and Complex procedures per Oklahoma City Air Logistics Complex (OC-ALC) Sup to AFI 32-7086, “Hazardous Material Management” and OC-ALCI 32-101 “Air Quality Record Keeping Procedure”. Publications are available digitally on e-Publishing website at www.e-publishing.af.mil for downloading or ordering.

http://www.e-publishing.af.mil/

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4.2. Hazardous Material (HAZMAT). If no HAZMAT will be brought on base or used in performance on this contract, the contractor shall certify “No HAZMAT will be brought on base” or “No HAZMAT Usage” in writing on company letterhead. This certification shall be provided to the COR within ten (10) days after award.

Upon COR receipt of the certification, the requirements of this section no longer apply. Appropriate penalties for the contractor, or administrative and disciplinary action for the later shall be assessed if found in violation of above certification.

The Contractor shall not store chemicals or hazardous material (HAZMAT) on Tinker AFB. Contractors shall be compliant with HAZMAT management procedures per Oklahoma City Air Logistics Complex (OC-ALC) Supplement to AFI 32-7086, “Hazardous Materials Management”. The Contractor shall maintain a log of all HAZMAT that is used on base. This usage log shall be provided to the COR monthly, the last business day of each month, or when the required work is completed. The COR will forward the records to the Unit Environmental Coordinator (UEC) no later than the fourth (4th) day of the following month or the first (1st) subsequent business day.

4.3. Material Safety Data Sheet/Safety Data Sheet (MSDS/SDS) and Labeling. Upon COR receipt of the “No HAZMAT Usage” certification, the requirements of this section no longer apply.

The Contractor shall not transport, ship or use any chemical, material or substance used in the performance of this SOW on Tinker AFB before written approval is provided by 72 ABW/CEIE, Natural Infrastructure Management (Environmental Compliance). The Contractor shall submit to the COR, ten (10) calendar days after contract award date all Safety Data Sheets (SDSs) and a completed OC-ALC Form 152, SDS Information Sheet. The Contractor shall receive approval from the COR prior to shipping any chemical, material or substance to Tinker AFB. A copy of the manufacturer SDS shall accompany the shipment. Contractor shall comply with the effective dates for SDS requirements IAW the Occupational Safety and Health Administrations (OSHA) Hazardous Communication Standard, Title 29, Code of Federal Regulation (CFR) Part 1910.1200. The Contractor shall ensure containers of hazardous chemicals are labeled with the following information, prior to shipping to Tinker AFB IAW OSHA Hazardous Communication Standard, Title 29, CFR Part 1910.1200 (2012): product identifier; signal word; hazard statement(s); precautionary statement(s);

pictogram(s); and name, address and telephone number of the chemical manufacturer, importer, or other responsible party. The COR will forward all SDS submittals to 72 ABW/CEIE for approval. A current manufacturer SDS shall be submitted to the COR if the Contractor changes manufacturer or vendor for any chemicals that were prior approved. The Contractor shall maintain copies of manufacturer SDSs for all chemicals and SDSs shall be readily accessible at all times by Contractor personnel as well as government employees.

4.4. Hazardous Waste. If no HAZWASTE will be generated during performance of this contract, the contractor shall certify “NO Hazardous Waste Generation” in writing on company letterhead. This certification shall be provided to the COR within ten (10) days after award. Upon COR receipt of the “No Hazardous Waste Generation” certification, the requirements of this section no longer apply. Appropriate penalties for the contractor, or administrative and disciplinary action for the later shall be assessed if found in violation of above certification.

The Contractor shall dispose of contaminated solid waste, spent or processed chemical solutions, used rags and hazardous waste in government furnished waste containers located in the shop or area the work is being performed. The Contractor shall notify the COR if the required waste containers are not available on site.

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4.5. Discharges. Any discharges into Tinker’s industrial waste treatment plant (IWTP) or sanitary sewer shall be approved and done IAW Tinker Industrial Waste Water Discharge Permit as instructed by 72 ABW/CEIE, Natural Infrastructure Management (Environmental Compliance). Notice of intent documentation shall be provided to the COR within ten (10) days after award. The COR will submit the required notice of intent documentation to the UEC for 72 ABW/CEIE approval. The Contractor shall not discharge into IWTP and sanitary sewer prior to approval issued by 72 ABW/CEIE. The Contractor shall maintain records of written approval issued by 72 ABW/CEIE for discharges into IWTP and sanitary sewer.

4.6. Off-Site Discharges. For discharges outside of Tinker AFB, the Contractor shall ensure waste water discharges, that may contain pollutants resulting from any contracted service, go to a state or federal permitted treatment facility such as a municipal Publicly Owned Treatment Works (POTW). The Contractor shall provide a letter ten (10) calendar days after contract award date to the COR from the POTW that states the POTW is permitted for all pollutants that the Contractor may discharge during the contracted service.

4.7. Spills. Upon occurrence of any spill that could enter the storm system or cause any harmful environment effects, the Contractor shall immediately call 911 to report the incident. When possible, the Contractor shall use a base telephone to receive help from Tinker AFB 911. If using a cell phone, the Contractor shall request Tinker AFB 911. The Contractor shall immediately report all environmental violations to the COR and UEC.

The Contractor shall provide five (5) copies of a typed or written report about the incident within four (4) clock hours as follows:

One (1) copy to CO, two (2) copies to the COR, a copy for UEC and one (1) copy for record. The format of the report shall be left up to the Contractor, but the report shall contain the following information:

• Name and contact number of person reporting the spill

• Date and time of incident

• Location and source of spill

• Substance or pollutant spilled

• Amount spilled and rate of discharge

• Any damages or injuries involved

• Extent of area impacted

• Potential hazards

• Actions taken

• Organizations contacted

• Remarks Section - that addresses the cause of the spill (e.g. human error, equipment, etc.) and whether

911 was called and which agencies responded.

4.8. Environmental Training. Upon COR receipt of the “No Hazardous Waste Generation” certification, the requirements of this section no longer apply.

Contractor personnel performing duties in the service of this SOW shall have training that acquaints the person with the details of Resource Conservation Recovery Act (RCRA) regulations in 40 CFR 260 through 279; applicable State Laws and regulations; DoD, Air Force and local requirements. This training can be obtained through creditable training institutions or companies.

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