Attachment_1_-_Corrosion_PWS_(Final)_(Rev.1).pdf

Solicitation No. FA4427-14-R-0005 Contract No. FAXXXX-XX-X-XXXX

Aircraft Corrosion Control Services

PERFORMANCE WORK STATEMENT

CORROSION CONTROL SERVICES

30 MAY 2014 (Rev.1)

TRAVIS AFB, CA

Table of Contents

Chapter 1―AIRCRAFT CORROSION PREVENTION CLEANING SERVICES TRAVIS

AIR FORCE BASE, CALIFORNIA

1.1. Scope of Work. …...……………………………………………………………... 6

1.2. Regulations and Guidance. ……………………………………………………

Chapter 2―MINIMUM TASKS 9

2.2 C-5 Services. …………………………………………………………………

2.3 C-17 Services. …………………………………………………………………..12

2.4 KC-10 Services. ……………………………………………………………..….15

2.5 C-130 Services. . ………………………………………………………………..18

2.6 Other Services. ………………………………………………………………….19

2.7 Emergency Services. …………………………………………………………….19

Chapter 3―ENVIRONMENTAL COMPLIANCE 21

3.1 General. ………………………………………………………………………….21

3.2 Storm Drains. ……………………………………………………………………21

3.3 Waste Sludge. …………………………………………………………………..21

3.4 Hazardous Spills. ……………………………………………………………….21

3.5 Hazardous Materials Management. …………………………………………….21

3.6 Hazardous Waste Management. ………………………………………………..22

3.7 Wastewater. …………………………………………………………………….22

3.8 Water Usage. ……………………………………………………………………23

3.9 Hazardous Material Storage Tanks. …………………………………………….23

3.10 Spill Response. ………………………………………………………………….23

Aircraft Corrosion Control Services

3.11 Environmental Enforcement Actions. …………………………………………..23

Chapter 4― SERVICE PROVIDER MOBILIZATION 24

4.1 Future Service Providers. ………………………....………………...………

Chapter 5― SERVICES SUMMARY 25

5.1 Services Summary. ……………………………………………………………..25

5.2 Quality Control. ………………………………………………………...………25

5.3 Quality Assurance Evaluations. …………………………………………………25

5.4 Performance Evaluation. ………………………………………………………...26

5.5 Government Remedies. ………………………………………………………….26

Chapter 6 ―GOVERNMENT FURNISHED PROPERTY 28

6.1. Government Furnished Property and Services. ………………………………...28

6.2 SP-Furnished Equipment. ………………………………………………………29

6.3. All other equipment. ……………………………………………………………29

Chapter 7 ―GENERAL INFORMATION 30

7.1 Management. …………………………………………………………………...30

7.2. Hours of Operation. …………………………………………………………….31

7.3. SP Accountability. ………………………………………...……………………31

7.4. Housekeeping. ………………………………………………………………….31

7.5. Service Provider Personnel. …………………………………………………….31

7.6. Severe Weather Procedures. ……………………………………………………32

7.7. Hiring Military Personnel. ……………………………………………………..32

7.8. Employee Training (SP provided). ……………………………………………..32

7.9. Mishaps. ………………………………………………………………………...32

Aircraft Corrosion Control Services Chapter 8― SECURITY REQUIREMENTS 33

8.1. Security Requirements. …………………………………………………………33

8.2. Primary SP Responsibilities. ……………………………………………………36

8.3. Obtaining a Base Pass. ………………………………………………………….37

8.5. Increased Force Protection Condition. …………………………………………38

8.6. Restricted Area Badges. ………………………………………………………...38

8.7. Escort Requirements. …………………………………………………………..38

8.8. Lost Base Passes or Restricted Area Badges. …………………………………..38

8.9. Information Protection Security Training. ……………………………………..39

8.10. For Official Use Only Information. …………………………………………….39

8.11. Anti-terrorism Force Protection Training. ……………………………………...39

8.12. Operations Security. …………………………………………………………….39

Appendices 40

Appendix 1 GOVERNMENT FURNISHED PROPERTY AND SERVICES 40

Appendix 1(a) GOVERNMENT FURNISHED FACILITIES 40

Appendix 1(b) GOVERNMENT FURNISHED EQUIPMENT 40

1b.1. Government Furnished Equipment. …………………………………………….40

1b.2. Aircraft Support Equipment. ……………………………………………………42

1b.3. Aerospace Ground Equipment. …………………………………………………42

1b.4. Equipment Inventory. …………………………………………………………..42

1b.5. Equipment Loss or Damage. ……………………………………………………42

Appendix 1(c) GOVERNMENT FURNISHED MATERIAL 42

1c.1. Bench Stock Items/Materials. …………………………………………………..42

1c.2. Consumable/Miscellaneous Materials. …………………………………………42

Aircraft Corrosion Control Services

1c.3. Technical Data. …………………………………………………………………43

Appendix 1(d) GOVERNMENT FURNISHED SERVICES 43

1d.1. Telecommunications. …………………………………………………………...43

Appendix 1(e) GOVERNMENT FURNISHED MEDICAL CARE 43

Appendix 1(f) GOVERNMENT FURNISHED TRAINING 43

1f.2. Red X Certifications. …………………………………………………………...44

Appendix 2. 45

2.1. PROJECTED WORKLOADS 45

2.2. COMPLETE WASH FREQUENCIES-PROJECTED (ALL AIRCRAFT) FY15 48

Appendix 3 49

TRAVIS AIR MUSEUM SP WASH SCHEDULE 49

Chapter 1

AIRCRAFT CORROSION PREVENTION CLEANING SERVICES

TRAVIS AIR FORCE BASE, CALIFORNIA

1.1 Scope of Work. The Service Provider (SP) shall perform Aircraft Corrosion Control Services at Travis Air Force Base (TAFB) as defined in this Performance Work Statement (PWS). The SP shall comply with all federal, state, and local laws; executive orders; rules and regulations applicable to its performance under this contract. The SP is expected to take the lead in encouraging business process innovations, implement more efficient ways of performing the services, and be flexible in working with the Government to satisfy mission needs. Except for those facilities, equipment, and property identified as Government-furnished, the SP shall provide all labor, material, tools, equipment, vehicles, and other items and services necessary to perform aircraft corrosion control services at TAFB as defined in this PWS. Workload estimates are located under Appendix 2.

1.2 Regulations and Guidance. Federal, state and local directives prescribe specific procedures for aircraft corrosion prevention cleaning. These and those listed below, include but are not limited to, Federal Aviation Administration (FAA), Federal Aviation Regulation (FAR) and Technical Orders (TOs). The government will provide SP with all TOs and local policies.

All wash and lubrication tasks will be performed in accordance with the applicable aircraft TOs and any additional/special instructions specified in the Table 1.1. General tasks are to be performed in accordance with general TOs and applicable Air Force Instructions (AFIs), Command Instructions, Base and Wing Instructions, and Maintenance Group Operating Instructions (MXGOIs). Air National Guard Instructions (ANGI) will apply only to ANG owned aircraft.

Table 1.1. Applicable Publications

PUBLICATION TITLE

Air Force Technical Orders: All Airframes

00-5-1 Air Force Technical Order System

00-20-1 AMCSUP 1 Aerospace Equipment Maintenance Inspection, Documentation, Policy and Procedures

00-20-2 Maintenance Data Documentation

00-25-172 Ground Servicing of Aircraft and Static Bonding

1-1-691 Cleaning and Corrosion Prevention and Control, Aerospace and Non-Aerospace Equipment

4W-1-61 Maintenance and Overhaul Instructions All Type Aircraft Wheels

Aircraft Corrosion Control Services

Air Force Technical Orders: C-5 A,B,C

1C-5(A)-2-1 Ground Handling and Servicing 1C-5(A)-06 Work Unit Code Manual 1C-5(A)-23 System Peculiar Corrosion 1C-5(A)-2-1CL-1 Towing Checklist 1C-5(A)-2-1CL-8 External Electrical Power Checklist 1C-5(A)-2-4CL-2 APU/ATM Ground Operation 1C-5(A)-2-10CL-1 Aircraft Kneeling System

1C-5(A)-2-12CL-1 Operating Procedures, Cargo Doors and Ramps

1C-5(A)-6WC-13 Lubrication Requirements

Air Force Technical Orders: C-5 M 1C-5(M)-2-1 Ground Handling and Servicing 1C-5(M)-06 Work Unit Code Manual 1C-5(M)-23 System Peculiar Corrosion 1C-5(M)-2-1CL-1 Towing Checklist 1C-5(M)-2-1CL-7 External Electrical Power Checklist 1C-5(M)-2-4CL-2 APU/ATM Ground Operation 1C-5(M)-2-10CL-1 Aircraft Kneeling System

1C-5(M)-2-12CL-1 Operating Procedures, Cargo Doors and Ramps

1C-5(M)-6WC-13 Lubrication Requirements Air Force Technical Orders: C-17A 1C-17A-2-12JG-10-1 Servicing Cleaning/Decontamination 1C-17A-6WC-4 Lubrication Work Cards 1C-17A-23 System Peculiar Corrosion Control 1C-17A-2-09JG-10-1 Towing 1C-17A-2-52JG-30-1 Doors Cargo 1C-17A-2-10JG-60-1 Ground Handling Service Equipment Positions 1C-17A-2-49JG-00-1 Auxiliary Power Unit General 1C-17A-2-12JG-29-1 Servicing Hydraulic Power

Air Force Technical Orders: KC-10A

1C-10(K)A-06 Work Unit Code Manual 1C-10(K)A-2-12 Servicing

1C-10(K)A-6WC-5-1 Time Controlled and Out of Cycle Inspection Work Cards

1C-10(K)A-2-9CL-1 Towing Checklist 1C-10(K)A-2-49CL-1 APU Operation Checklist

Air Force Technical Order: C-130, All models

1C-130A-23CL-1 Organizational Maintenance Checklist Washing and Cleaning

Aircraft Corrosion Control Services 1C-130H-2-12JG-20-1 Ground Handling Lubrication 1C-130H-2-09JG-10-1 Ground Handling and Towing

Air Force Instructions (AFI)

AFI 11-218 AMCSUP_I Aircraft Operation and Movement On the Ground

AFI 21-101 AMCSUP_I Aerospace Equipment Maintenance Management

AFI 10-2501 AMCSUP_I Air Force Emergency Management (EM) Program Planning and Operations

AFI 41-210 Tricare Operations and Patient Administration AFI 33-322 Records Management Program AFI 33-332 Air Force Privacy and Civil Liberties Program

ANGI 21-105 (ANG Assets Only) Air and Space Equipment Structural Management

AFI 32-7086 AMCSUP_I Hazardous Materials Management

Air Force Occupational Safety Health Standard (AFOSHSTD)

AFOSHSTD 91-203 Air Force Consolidated Occupational Safety

Air Mobility Command Instruction (AMCI) AMCI 21-119 Corrosion Control Program

Travis Air Force Base Instructions (TAFBI) TAFBI 13-103 Airfield Driving Instruction TAFBI 32-2001 Installation Fire Protection Program TAFBI 32-301 Facility Managers TAFBI 21-106 FOD/DOP Program TAFBI 21-107 Tool and Equipment Management TAFBI 91-203 Hangar Procedures

60th Maintenance Group Operating Instructions (MXGOI)

60/349 MXGOI 21-101 Aircraft and Equipment Maintenance Management

Travis Air Force Base Plans Environmental Management TAFB Hazardous Waste Manage Plan

“The Government”, as used in this PWS, is defined as follows:

“The office of primary responsibility normally associated with the activity, duty or task being described within the context of a particular requirement.”

The SP will at all times strictly adhere to all notes, cautions, and warnings listed in applicable aircraft technical data.

The SP may be required to incorporate tasks required by changes in TO/AFI requirements to remain in compliance with the most current Air Force standards.

Chapter 2

MINIMUM TASKS

2.1. Aircraft Wash and Cleaning Services. The SP shall perform aircraft wash and cleaning services inside Hangar 811 or at a flight line location identified by the MOC.

Aircraft washes will be accomplished in accordance with applicable technical orders. Any deviation from prescribed TOs or work not covered by prescribed TOs must be submitted in writing to 60 MXG/QAE. All deviations will be approved and authorized by the 60 MXG/CC prior to performance.

2.1.1 Flightline Washes. Flightline washes shall begin within 2 hours of notification unless a shorter time frame is required due to mission priorities.

2.1.2 Complete Aircraft Washes. All scheduled complete wash services will be completed in Hangar 811 and returned to the government within 24 hours (C-5/C-17), 16 hours (KC-10), and 14 hours (C-130) from the time the aircraft is turned over to the SP.

The annotated times are the maximum allotted time to complete the service requirements in accordance with the tasks outlined in the PWS. Variations agreed upon by the FD/Chief QAE and SP due to special circumstances and mission requirements are allowed. Aircraft to receive complete wash services will be turned over to the SP at 0800L. If maintenance requirements delay turnover, the wash start time will be adjusted accordingly. If the delay extends beyond 1000L, the wash may be rescheduled and/or cancelled.

NOTE: Prevention of electrical shock hazards. Avoid directly spraying water on electrical connections and wiring on the aircraft. Ensure personnel are aware of electrical outlets in the hangar and extension cords in use during aircraft washes.

2.2. C-5 Services.

2.2.1. Complete C-5 Wash, WS-1. (Maximum elapsed time 24 hours) Service consists of Towing aircraft to hangar, Wash Preparation , Exterior Wash, Cargo Compartment Wash, Under Floor Wash, Flight Deck Cleaning, Troop Compartment Cleaning, Post Wash Restoration, Aircraft Lubrication, and Towing aircraft back to flightline. The following paragraphs outline a full C-5 wash sequence. Modifications to order and quantity of services must be authorized by 60 MXG/QAE.

2.2.1.1. Aircraft Tow. The SP is responsible for towing the aircraft to the designated wash location which is considered one tow. Returning the same aircraft to the designated parking location after the completion of wash services is considered a separate tow. The owning unit may request that the SP not tow the aircraft.

Coordinate usage of tow vehicles with owning unit CTKs as required. Coordinate all aircraft movements with MOC and command post prior to beginning the tow.

Aircraft Corrosion Control Services

Parking locations will be designated by MOC or authorized individual. The SP will ensure all tow supervisors are familiar with 60 MXGOI 21-101, chapter 10.3;

applicable aircraft ground handling procedures; and aircraft towing checklists.

Ensure tow vehicles have at least the minimum fuel level as required by tow vehicle owning-unit policy before returning the tow vehicle. Fuel can be obtained at military fuel pumps using the fuel key. After services are complete, aircraft will be towed back to flightline.

2.2.1.2. Wash Preparation. This service consists of preparing aircraft for wash, by means of the application of barrier materials, opening/closing doors and hatches, and other pre-wash duties as described in applicable technical orders. It also entails the proper documentation of AFTO 781 series aircraft forms. Aircraft must be completely prepared before washing operations begin. If armor is loaded, the owning unit is responsible for removal, storage and re-installation of these items.

Government personnel will provide storage stands for the duration of the wash and remove stands after wash.

2.2.1.3. Exterior Wash. Service consists of washing the entire exterior of the aircraft, including top of fuselage, top of wings, t-tail and compartments accessible by quick disconnect fasteners. Wheels, brakes, axles, bogie beam assemblies, interior of engine cowling or cowl doors, wheel wells, and all landing gear strut. Components shall not be cleaned using high pressure cleaning equipment.

2.2.1.4. Cargo Compartment Wash. Service consists of using pressurized water, soap and solvents to clean floors, roller tracks, winch wells, chine area, and tie-downs, and using non-pressurized water and solvents to clean walls, insulation, trim panels, interior of doors, and hydraulic service centers. Dry interior of doors, ladder surfaces, tie-downs and roller panels after washing is complete.

2.2.1.5. Under Floor Wash. Service consists of cleaning interior of under floor area (forward and aft bilges and in wheel-well pods), extending upward on both sides of the fuselage to the cargo compartment floor. Access to this area is gained through removal of panels at the forward and aft ends of the MLG wheel wells. Vacuum loose soil and remove trash. Clean surfaces with non-metallic brushes, using water and cleaning soap compound. Ensure all drain holes are open, by gently pushing a blunt, non-metallic instrument into the drain hole from the outside of the aircraft. Use a low-pressure fine spray only in this area if water hoses are employed for rinsing.

Remove all standing water and soil. To avoid electrical shock, water hoses may be used only when power is not applied to the aircraft.

2.2.1.6. Flight Deck Cleaning. Service consists of a Flightline Flight Deck Cleaning (see FS-4), all seats brushed off, seat belts crossed, armrests and seat pedestals wiped clean, seat tracks vacuumed and interior of windshields cleaned. Disinfect galleys and lavatories.

Aircraft Corrosion Control Services

2.2.1.7. Troop Compartment. Service consists of a Flightline Troop Compartment Cleaning (see FS-5), including all seat bottoms pulled up, seat frames cleaned, seatbelts crossed, tray tables cleaned and window and window frames cleaned.

Disinfect galleys and lavatories.

2.2.1.8. Post Wash Restoration. Clear all wash preparation and lubrication discrepancies in AFTO 781 series aircraft forms. Ensure all prepared areas are de-prepped in accordance with applicable technical orders. Ensure standing water is removed. Ensure aircraft is returned to either normal or tow configuration.

2.2.1.9. Full Aircraft Lubrication. Lubrication will begin within 1 hour after wash completion. If after several attempts, a grease fitting will not accept grease, annotate the AFTO 781A series forms for each instance and request a job control number from the MOC.

2.2.2. Flight Line Washes.

2.2.2.1. Mission Readiness Wash, FS-1. (Maximum elapsed time 3 hour) Service consists of washing and cleaning the entire exterior fuselage belly region from floor level down, and from the aft edge of the nose radome to the aft loading ramp forward hinge. Service also includes washing and cleaning the exterior of the Nose Landing Gear (NLG) doors, outboard Main Landing Gear (MLG) doors, MLG pods, side doors, complete center door, dovetail area, forward and aft loading ramps, wheels, tail cone, and both sides of the vertical stabilizer including the rudder and bottom of the horizontal stabilizer.

2.2.2.2. Clear Water Rinse, FS-2. (Maximum elapsed time 1 hour) Service consists of complete and thorough rinsing and flushing of the entire exterior of the aircraft with clean water at a flight line location until all accumulated contaminants are removed. Use of brushes and cleaning solutions will not be required as this service is solely a rinsing operation for the purpose of diluting and flushing away the accumulation of salt, dirt, and other water solubles. Do not direct water at openings normally masked during regular wash or at joints where lubricants could be removed.

Keep water nozzle at least 10 feet away from the surface being rinsed.

2.2.2.3. Flight Deck Cleaning, FS-4. (Maximum elapsed time 2 hours) Service consists of emptying all waste containers, replacing trash bags (SP provided), cleaning the entire aircraft upper forward interior, forward upper deck, including the flight deck, bunk rooms, avionics compartments, lavatory, galley area including sink, oven, courier compartment, electro-environmental room, ceilings, walls, floors, windows, drawers, storage areas, inner compartments, and all other areas within the upper forward interior.

2.2.2.4. Troop Compartment Cleaning, FS-5. (Maximum elapsed time 2 hours)

Aircraft Corrosion Control Services

Service consists of emptying trash cans, cleaning bulkheads, walls, trim panels, partitions, galley area including sink, oven, lavatories, ceilings, walls, floors, windows, drawers, storage areas, inner compartments, seats, seat backs, tray tables,, and all other areas within the troop interior.

2.2.2.5. Cargo Compartment Cleaning, FS-6. (Maximum elapsed time 2 hours) Service consists of cleaning bulkheads, walls, floors, chine area, insulation, trim panels, ladder surfaces, rail assemblies, entrance areas, rail coves, winch wells, cat walks and all other areas within the cargo compartment. Water hoses shall not be used to clean the interior of the aircraft during this type of cleaning. Ensure chemicals and water do not run, flow, or leak through cracks, crevices, holes in the floor, under bulkheads, and into electrical components.

2.2.2.6. Spot Wash and Component Parts Wash, CS-1. (Maximum allowable time 1 hour per unit) Service consists of localized cleaning of an area not to exceed 200 square feet or one unit. For this PWS, these areas or fractions thereof are identified as one unit. Examples of areas to be spot washed are wheels, AGE, rails, aircraft components and equipment on or off the aircraft, exhaust deposits, beverage spills, lavatory drainage stains, and residue from discharge of fire extinguisher chemicals, hydraulic leaks, panels or components for Non-Destructive Inspection (NDI) purposes.

2.3. C-17 Services.

2.3.1. Complete C-17 Wash, WS-1. (Maximum elapsed time 24 hours) Service consists of Towing aircraft to hangar, Wash Preparation, Complete Wash, Post Wash Restoration, Full Aircraft Lubrication, and Towing aircraft back to flightline. The following paragraphs outline a full C-17 wash sequence. Modifications to orders and quantity of services must be authorized by 60 MXG/QAE.

2.3.1.1. Aircraft Tow. The SP is responsible for towing the aircraft to the designated designated parking location after the completion of wash services is considered a separate tow. The owning unit may request that the SP not tow the aircraft.

Coordinate usage of tow vehicles with owning unit CTKs as required. Coordinate all aircraft movements with MOC and command post prior to beginning the tow.

Parking locations will be designated by MOC or authorized individual. The SP will ensure all tow supervisors are familiar with 60 MXGOI 21-101, chapter 10.3;

applicable aircraft ground handling procedures; and aircraft towing checklists.

Ensure tow vehicles have at least the minimum fuel level as required by tow vehicle owning-unit policy before returning the tow vehicle. Fuel can be obtained at military

2.3.1.2. Wash Preparation. This service consists of preparing aircraft for wash, by

Aircraft Corrosion Control Services means of the application of barrier materials, opening/closing doors and hatches, and other pre-wash duties as described in applicable technical orders. It also entails the proper documentation of AFTO 781 series aircraft forms. Aircraft must be completely prepared before washing operations begin. If armor is loaded, the owning unit is responsible for removal, storage and re-installation of these items.

Government personnel will provide storage stands for the duration of the wash and remove stands after wash.

2.3.1.3. Exterior Wash. Service applies to the entire exterior of the aircraft and includes the flap wells, spoiler area, landing gear, wheel wells, doors and all components located within, top of horizontal stab, top of wings, engines, pylons, and any components located within the specified work areas not specifically identified herein. Note: This wash action will also be applicable for Home Station Checks.

2.3.1.4. Interior Cleaning. This is a Major Interior Cleaning (see FS-4). A major interior cleaning includes washing specifications of a Minor Interior Cleaning (see FS-3), plus cleaning the interior surfaces of cargo doors, bulkheads, walls, doors, hatches and other areas where dirt, grime and grease exist. Dust off all overhead ducting. Hand-clean seat tracks, tie-down receptacles, and V-channels with a soft bristled brush to remove build-up of dirt and grime.

2.3.1.5. Post Wash Restoration. Clear all wash preparation and lubrication prepped in accordance with applicable technical orders. Ensure aircraft is returned to either normal or tow configuration.

2.3.1.6. Full Aircraft Lubrication. Post wash lubrication will begin within 1 hour after wash completion. If after several attempts, a grease fitting will not accept grease, annotate the AFTO 781A series forms for each instance and request a job control number from the MOC.

2.3.2. Other Scheduled Washes.

2.3.2.1 Refurb Wash Preparation, RS-1. (Maximum elapsed time 12 hours) Services consists of removal of under floor insulation, latrine/lavatory, and galley, raising of the ADS rails and transportation of insulation and ADS rails to the aircraft’s Home Station Check (HSC) location. Hardware will be bagged, marked and stored IAW with TO requirements. Insulation will be transported via a government furnished trailer to a location determined by HSC supervision, normally Hanger 837. Do not remove underfloor insulation unless it has been marked by the

860 AMXS

2.3.2.2. 60-Day Landing Gear Wash and Lubrication, LS-1. (Maximum elapsed time 6 hours) Service applies to the 60-Day requirement for lubrication and wash of landing gears per TO 1C-17A-23, and 1C-17A-6WC-4. Preparation for gear washes is the responsibility of the SP. For this wash service, the owning unit is responsible for tow to the hangar and return to the appointed parking area.

2.3.2.3. Complete Underfloor Cleaning, US-1. (Maximum elapsed time 8 hours) Service applies to the area under the cargo floor of the aircraft. This area will only be cleaned after Air Force personnel have prepped the area to include removal of all insulation blankets and electronic equipment coverings. Access to this area is gained through a front or aft access door leading to a catwalk with an attached creeper. This area will be hand scrubbed using the minimum amount of water necessary to achieve cleanliness since there are no drain holes for fluid to exit. The SP shall remove all trapped fluids after cleaning is accomplished. Note: This service will be done in conjunction with a full wash.

2.3.3. Flightline Washes.

2.3.3.1 Mission Readiness Wash, FS-1. (Maximum elapsed time 2 hour) Service consists of cleaning the entire exterior fuselage belly region from floor level down and from the aft edge of the radome to the loading ramp hinge. Included are the radome, NLG door, MLG outboard doors and both pods, petal doors, all wheels, ramp, engines, pylons, exhaust areas, both sides of vertical stabilizer, rudder, tailcone, one-foot wide area around all entrance and exit doors for the purpose of removing dirty hand prints, and all components within the specified work area not specifically identified herein.

2.3.3.2. Clear Water Rinse, FS-2. (Maximum elapsed time 1 hour) Service consists with clean water at a flight line location until all accumulated contaminants are removed. Use of brushes and cleaning solutions will not be required as this service is solely a rinsing operation for the purpose of diluting and flushing away the accumulation of salt, dirt, and other water solubles. Do not direct water at openings

2.3.3.3. Minor Interior Cleaning, FS-3. (Maximum elapsed time 2 hours) Service consists of cleaning all interior aircraft compartments. Remove trash and foreign objects from floors, racks, seat pockets, ashtrays, V-channels, crew bunks, recessed areas and all other areas where trash collects. Empty waste containers and replace trash bags (SP provided). Wash, polish, and disinfect crew galley and latrine.

Vacuum clean to remove dust, dirt and other loose objects from the areas listed. Use a soft brush to loosen dirt and dust from consoles before vacuuming. Mop floors.

Vacuum and clean cargo roller conveyer assemblies. If roller conveyer assemblies are removed from channels, the channels will be vacuumed, and damp mopped. All surfaces of the roller conveyer assemblies will be cleaned thoroughly. If Aerial Delivery System (ADS) rail assemblies are in a raised position, channels will be vacuumed, damp mopped, and all surfaces of the ADS rails will be cleaned thoroughly. Do not permit cleaning solution to drain below the unsealed flooring in the aircraft. After cleaning, ensure accumulation of water is removed from all recessed areas.

2.3.3.4. Major Interior Cleaning, FS-4. (Maximum elapsed time 6 hours) A major interior cleaning includes washing specifications of a minor interior (FS-3), plus cleaning the interior surfaces of cargo doors, bulkheads, walls, doors, hatches, rear urinals and other areas where dirt, grime and grease exist. Dust off all overhead ducting. Hand-clean seat tracks, tie-down receptacles, and V-channels with a soft bristled brush to remove build-up of dirt and grime.

2.3.3.5. Spot Wash and Component Parts Wash, CS-1. (Maximum allowable time 1 hour per unit) Service consists of localized cleaning of an area not to exceed 200 square feet or one unit. For this PWS, these areas or fractions thereof are identified as one unit. Examples of areas to be spot washed are wheels, AGE, rails, aircraft components and equipment on or off the aircraft, exhaust deposits, beverage spills, lavatory drainage stains, and residue from discharge of fire extinguisher chemicals, hydraulic leaks, panels or components for Non-Destructive Inspection (NDI) purposes.

2.4. KC-10 Services.

2.4.1. Complete KC-10 Wash, WS-1. (Maximum elapsed time 24 hours) Service consists of Towing aircraft to hangar, Wash Preparation, Exterior Wash, Interior Cleaning, Post Wash Restoration, Aircraft Lubrication, and Towing aircraft back to flightline. The following paragraphs outline a full KC-10 wash sequence. Modifications to orders and quantity of services must be authorized by 60 MXG/QAE.

2.4.1.1. Aircraft Tow. The SP is responsible for towing the aircraft to the designated designated parking location after the completion of wash services is considered a separate tow. The owning unit may request that the SP not tow the aircraft.

Coordinate usage of tow vehicles with owning unit CTKs as required. Coordinate all aircraft movements with MOC and command post prior to beginning the tow.

Parking locations will be designated by MOC or authorized individual. The SP will ensure all tow supervisors are familiar with 60 MXGOI 21-101, chapter 10.3;

applicable aircraft ground handling procedures; and aircraft towing checklists.

Ensure tow vehicles have at least the minimum fuel level as required by tow vehicle owning-unit policy before returning the tow vehicle. Fuel can be obtained at military

2.4.1.2. Wash Preparation. This service consists of preparing aircraft for wash, by means of the application of barrier materials, opening/closing doors and hatches, and other pre-wash duties as described in applicable technical orders. It also entails the proper documentation of AFTO 781 series aircraft forms. Aircraft must be completely prepared before washing operations begin.

2.4.1.3. Exterior Wash. Service consists of washing the entire exterior of the aircraft, Aircraft Corrosion Control Services including top of fuselage, top of wings, t-tail and compartments accessible by quick disconnect fasteners. Wheels, brakes, axles, bogie beam assemblies, interior of engine cowling or cowl doors, wheel wells, and all landing gear strut. Components shall not be cleaned using high pressure cleaning equipment.

2.4.1.4. Interior Cleaning. Service consists of emptying trash containers at lavatories and galley, cleaning the entire aircraft interior, flight deck, troop compartment for both 16 seat and 75 seat configurations, air refueling operator (ARO) compartment, cargo rollers, cargo rollers tracks (maintenance will remove applicable cargo roller prior to wash), cat walks, ceilings, walls, floors, windows, drawers, storage areas, inner compartments and exterior of crew chief box. Vacuum carpet areas and cargo roller tracks. Water hoses must not be used to clean the interior of aircraft. Remove all residue streaks from cleaning surfaces and leave no standing water. Ensure chemicals and water do not run, flow, or leak through cracks, crevices and holes in floor, under bulkheads, and into electrical compartments.

2.4.1.5. Post Wash Restoration. Clear all wash preparation and lubrication prepped in accordance with applicable technical orders. Ensure aircraft is returned to either normal or tow configuration.

2.4.1.6. Post-Wash Lubrication. Lubricate main, centerline and nose landing gear IAW 1C-10K(A)-2-12-21-01 page 301-314 and 1C-10(K)A-6WC-2, prior to removal from the wash rack. Lubrication will begin within 1 hour after wash completion.

Note: When a grease fitting will not accept grease, the SP shall annotate the aircraft forms and inform the MOC, who will notify the proper agency for fitting replacement and/or troubleshooting.

2.4.2. Flightline Washes.

2.4.2.1. Mission Readiness Wash, FS-1. (Maximum elapsed time 2 hour) Service consists of washing and cleaning the entire exterior fuselage belly region from wing root level down, and from the aft edge of the nose radome to the end of the refueling boom. Service also includes washing and cleaning the interior and exterior of the NLG, CTR, MLG doors, wheels, engines, both sides of the vertical stabilizer including the rudder and aft engine cowling.

2.4.2.2. Clear Water Rinse, FS-2. (Maximum elapsed time 1 hour) Service consists with clean water at a flight line location until all accumulated contaminants are removed. Use of brushes and cleaning solutions will not be required as this service is solely a rinsing operation for the purpose of diluting and flushing away the accumulation of salt, dirt, and other water solubles. Do not direct water at openings

Aircraft Corrosion Control Services

2.4.2.3. Flight Deck Cleaning, FS-3. (Maximum elapsed time 1 hour) Service consists of emptying trash, cleaning ceilings, bulkheads, walls, floors, windows, storage areas, inner compartments, removing trash and all other areas within the flight compartment. Vacuum all carpeted areas and exposed cargo roller tracks. Water hoses must not be used to clean the interior of aircraft. Remove all residue streaks from cleaning surfaces and leave no standing water. Ensure chemicals and water do not run, flow, or leak through cracks, crevices, holes in floor, under bulkheads, and into electrical compartments.

2.4.2.4. Troop Compartment Cleaning, FS-4. (Maximum elapsed time 2 hours) Service is for the 16-seat configuration, which consists of cleaning one lavatory, galley area, ceilings, drawers, bulkheads, walls, floors, windows, storage areas, seats, seat backs, tray tables, and inner compartments. Empting trash cans from lavatory, galley and removing trash from seatback pouches. Vacuum all carpeted areas and exposed cargo roller tracks. Water hoses must not be used to clean the interior of aircraft. Remove all residue streaks from cleaning surfaces and leave no standing water. Ensure chemicals and water do not run, flow, or leak through cracks, crevices, holes in floor, under bulkheads, and into electrical compartments.

2.4.2.5. Cargo Compartment Cleaning, FS-5. (Maximum elapsed time 2 hours) Service consists of cleaning bulkheads, walls, floors, trim panels, crew chief box, cargo rollers, rail assemblies, entrance areas, door panels, cat walks, and removing trash. Use wet mop and ensure all mop streaks are removed. Vacuum exposed cargo rollers. Water hoses must not be used to clean the interior of aircraft. Remove all residue streaks from cleaning surfaces and leave no standing water. Ensure chemicals and water do not run, flow, or leak through cracks, crevices, holes in floor, under bulkheads, and into electrical compartments.

2.4.2.6. Air Refueling Operator (ARO) Compartment Cleaning, FS-6. (Maximum elapsed time 1 hour) Service consists of cleaning bulkheads, walls, floors, trim panels, ladder surface, cargo rollers, entrance area, inner compartments, windows, mirrors, removing trash, and all other areas within the ARO. Vacuum carpet and exposed cargo roller tracks. Water hoses must not be used to clean the interior of aircraft. Remove all residue streaks from cleaning surfaces and leave no standing water. Ensure chemicals and water do not run, flow, or leak through cracks, crevices, holes in floor, under bulkheads, and into electrical compartments.

2.4.2.7. Spot Wash and Component Parts Wash, CS-1. (Maximum allowable time 1 hour per unit) SP is responsible for towing each aircraft to the designated wash location, and returning each aircraft to the designated parking location after wash service, unless requested not to tow the aircraft by the owning unit. Service consists of localized cleaning of an area not to exceed 200 square feet or one unit. For this PWS, these areas or fractions thereof are identified as one unit. Examples of areas to be spot washed are wheels, AGE, rails, aircraft components and equipment on or off the aircraft, exhaust deposits, beverage spills, lavatory drainage stains, and residue

Aircraft Corrosion Control Services from discharge of fire extinguisher chemicals, hydraulic leaks, panels or components for Non-Destructive Inspection (NDI) purposes.

2.5. C-130 Services

2.5.1. Complete C-130 Wash, WS-1 (Maximum elapsed time 24 hours) Service consists of towing aircraft into hangar, wash preparation, exterior wash, flight deck cleaning, cargo compartment wash, post wash restoration, full aircraft lubrication, and towing aircraft back to flightline. The following paragraphs outline a full C-130 wash sequence. Modifications to order and quantity of services must be authorized by

60MXG/QAE.

2.5.1.1. Aircraft Tow. The SP is responsible for towing the aircraft to the designated designated parking location after the completion of wash services is considered a separate tow. Coordinate usage of tow vehicles with TAFB CTKs as required.

Coordinate all aircraft movements with MOC and command post prior to beginning the tow. Parking locations will be designated by MOC or authorized individual. The SP will ensure all tow supervisors are familiar with 60 MXGOI 21-101, chapter 10.3;

applicable aircraft ground handling procedures; and aircraft towing checklists.

Ensure tow vehicles have at least the minimum fuel level as required by tow vehicle owning-unit policy before returning the tow vehicle. Fuel can be obtained at military fuel pumps using the fuel key. After services are complete, aircraft will be towed back to flightline.

2.5.1.2. Wash Preparation. This service consists of preparing aircraft for wash, by means of the application of barrier materials, installing plug and covers, opening/closing doors and hatches, and other pre-wash duties as described in applicable technical orders (TO 1C-130A-23CL-1, TO 1-1-691, and ANGI 21-105).

The aircraft Crew Chief will be responsible for maintaining the proper documentation of the AFTO 781 series aircraft forms. Aircraft must be completely prepared before washing operations begin. Aircraft armor will be removed, by the owning government unit, before wash services begin.

2.5.1.3. Exterior Wash. Service consists of washing the entire exterior of the aircraft, including top of fuselage, top of wings, wing flaps, air deflector wells, and empennage. Wheels, brakes, axles, wheel wells, and all landing gear struts, and any components located within the specified work areas not specifically identified herein.

Wheels and Components shall not be cleaned using high pressure cleaning equipment.

2.5.1.4. Flight Deck Cleaning. Service consists of emptying trash containers and galley, cleaning the entire flight deck compartment, and vacuuming carpet areas.

Water hoses must not be used to clean the flight deck of the aircraft. Remove all residue streaks from cleaning surfaces and leave no standing water or cleaners.

Aircraft Corrosion Control Services Ensure chemicals and water do not run, flow, or leak through cracks, crevices and holes in floor, under bulkheads, and into electrical compartments.

2.5.1.5. Cargo Compartment Wash. Service consists of using pressurized water limited to 500 PSI, soap and solvents to clean floorboards, roller tracks, chine areas, and tie-downs, and using non-pressurized water and solvents to clean walls, insulation, trim panels, interior of doors, and hydraulic service centers. Remove loose soil in the flight deck, cargo compartment, cargo ramp, and cargo door by vacuuming.

Clean and Flush aft urinals and drain lines with cleaner MIL-PRF-87937 Type I, or equivalent. Dry interior of doors, ladder surfaces, and tie-downs after washing is complete. All above requirements Referenced in T.O. 1C-130A-23CL-1, Section II.

2.5.1.6. Post Wash Restoration. The aircraft Crew Chief will be responsible to ensure that all wash preparation and lubrication discrepancies in AFTO 781 series aircraft forms are cleared. The SP will ensure all prepared areas are de-prepped in accordance with applicable technical orders and ensure aircraft is returned to either normal or tow configuration.

2.5.1.6. Full Aircraft Lubrication. Post wash lubrication will begin within 1 hour after wash completion. Post wash lubrication will be accomplished IAW T.O. 1C- 130A-23CL-1, Section IV and 1C-130H-2-12JG-20-1. If after several attempts, a grease fitting will not accept grease, annotate the AFTO 781A series forms for each instance.

2.6. Other Services.

2.6.1. Museum Aircraft Complete Exterior Wash, MS-1. (Maximum allowable time 2 hours) Service consists of cleaning exterior aircraft including top, upper sides and landing gear with soap and water, to include brushing, to remove build-up of surface dirt and bird residue. Access to the aircraft to be washed will be made by museum personnel prior to wash rack being called. No solvents will be used to clean aircraft at outdoor museum locations.

2.6.2. Museum Aircraft Upper Surface Wash, MS-2. (Maximum allowable time 1 hour) Service is the same as MS-1, but only exterior aircraft upper surfaces will be washed.

2.6.3. Transient Spot Wash. TS-1. (Maximum allowable time 1 hour per unit) Service consists of localized cleaning of an area not to exceed 200 square feet or one unit. For this PWS, these areas or fractions thereof are identified as one unit. Examples of areas to be spot washed are wheels, rails, aircraft structures, components and equipment on or off the aircraft, exhaust deposits, beverage spills, lavatory drainage stains, and residue from discharge of fire extinguisher chemicals, hydraulic leaks, panels or components for Non-Destructive Inspection (NDI) purposes.

2.6.4. Transient Aircraft Washes. The service provider may be required to perform

Aircraft Corrosion Control Services additional services within the scope and general intent of the contract on transient aircraft.

If the transient aircraft is of an airframe covered under the existing price schedule a modification will be completed to increase the quantities as necessary to the current task order.

If the transient aircraft is not an airframe covered under the existing price schedule the work will be negotiated separately and a task order will be issued.

2.6.5. Emergency Services. Performance of services during crisis declared by the President or Secretary Of Defense. All services to be performed under the contract have been determined to be essential for performance during crisis. According to Department of Defense Instruction (DoDI) 3020.37, Continuation of essential DoD Contractor Services during a Crisis, and Air Force Implementation thereof, it is determined that the contractor shall perform during crisis situation unless notified by a contracting officer.

2.6.5.1. The contractor shall perform all services required during a crisis, during normal hours of operation as stated in the PWS, unless otherwise directed by a contracting officer.

2.6.5.2. Contingency Plan. The contractor shall have in place a contingency plan to provide continuing services at Travis AFB during crises as declared by the President or Secretary of Defense. The contingency plan needs to also identify those employees having military mobilization recall commitments and the plan for replacing said employees.

Chapter 3

ENVIRONMENTAL COMPLIANCE

3.1 General. SP is strictly prohibited from direct contact with any outside (off Base) environmental agency unless authorized by 60 CES/CEA, 580 Hickam Ave, Bldg. 246 Bay A, 424-7515. In order to comply with the affirmative procurement requirements of Section 6002 of Resource Conservation and Recovery Act of 1976, Executive Order 13101 and the TAFB Affirmative Procurement Plan (latest version), use of the recycled and recovered materials and products identified in the Environmental Protection Agency’s Comprehensive Procurement Guidelines (CPG) is required by the SP. These materials and products must meet the manufacturer’s specifications, must not delay the progress of the work and must not be cost prohibitive. All materials and products intended for use within this PWS must meet the recommended minimum content standards identified in the current CPG and Recovered Materials Advisory Notices (RMANs). Other materials and products not listed, but commonly used in industry outside of the government, should also be considered. The SP shall provide, to the maximum extent practicable, materials with recovered material content at the levels recommended by the EPA’s CPG website: http://www.epa.gov/cpg/products. If a conflict exists between material specifications elsewhere and affirmative procurement requirements, the SP shall immediately notify 60 CES/CEA.

3.2 Storm Drains. The use of storm drain blocks for mission readiness washes, component spot washes, or clear water rinses on the flight line and museum washes are required. Use vacuum trucks to collect all water off the ground generated from aircraft washing or rinsing. All vacuumed wash/rinse water shall be discharged into floor drains in Hangar 811 only. The SP shall identify storm drain inlets that may capture aircraft wash or rinse water and block those drains with SP provided drain blocks of an appropriate design prior to the beginning of the wash.

When dumping wash water from the vacuum truck into the floor drain in bldg. 811, the SP shall dump the water in at the point furthest from the oil water separator (OWS) in order to slow and disperse the flow with the floor drain channel before it reaches the OWS. Restrict complete exterior washes to Hangar 811 and the Travis AFB aircraft museum.

3.3. Waste Sludge. SP shall coordinate for removal of all waste sludge material generated by aircraft wash from the grates located at aircraft wash location. SP shall coordinate all wastes leaving TAFB at least 48 hours in advance with 60 CES/CEAN. SP shall ensure hazardous waste manifests are signed by 60 CES/CEAN.

3.4 Hazardous Spills. SP shall clean up hazardous fluid spills in accordance with spill response procedures in TAFB 60/349 MXGOI 21-101. Notify MOC and 60 MXG/QAE immediately if spill exceeds five gallons.

3.5. Hazardous Materials Management. The SP shall participate in the Base HAZMART program as required by AFI 32-7086, AMC Supplement 1. Participation shall include:

3.5.1. Designation of a single individual who has experience and knowledge of HAZMAT processes.

3.5.2. Provision of Material Safety Data Sheets/Safety Data Sheets for all HAZMAT to be used or stored on base.

3.5.3. Limited storage of HAZMAT on base.

3.5.4. Coordination of all HAZMAT used or stored on base from the Base HAZMART to include HAZMAT bar-coding and tracking.

3.5.5. Tracking daily usage of all HAZMAT used or stored on base.

3.5.6. Implementation of Best Management Practices to prevent spills and other releases to the environment to meet NFPA, OSHA, and RCRA requirements.

3.5.7. Participation in an accurate exit inventory of materials used on base at the end of the contract.

3.5.8. The SP shall store all HAZMAT in accordance with local, federal, state, DoD, and Air Force regulations in a designated HAZMAT storage area. The SP will comply with 60 CES/CEAN audits.

3.6. Hazardous Waste (HW) Management. HW treatment is not permitted on TAFB unless approved and monitored by 60 CES/CEAN. The SP is responsible for the analysis, characterization, proper handling and disposal of hazardous wastes generated by their operation.

SP shall coordinate all wastes leaving TAFB at least 48 hours in advance with 60 CES/CEAN.

The SP shall manage HW in accordance with Title 22 of the California Code of Regulations and the TAFB HW Management Plan. The SP is subject to the Solano County Department of Resource Management, California Department of Toxic Substances Control, Federal EPA and 60 CES/CEAN audits while working on TAFB. SP shall establish and operate a HW Satellite Accumulation Point per 60 CES/CEAN standards. The SP shall maintain and provide Site Specific HW training to SP personnel handling HW. All hazardous waste shipments must be prepared in accordance with Department of Transportation Regulations (40 CFR 172). Prior to removing, transporting, or disposing of any HW from the base, the SP shall forward HW manifests, land disposal restrictions, waste profiles, laboratory analyses and material safety data sheets/safety data sheets to 60 CES/CEAN to obtain a review and/or signature as required.

3.7. Wastewater. The SP is responsible to ensure compliance with TAFB Waste Water Discharge Permit No. SIU-07 / ZERO 433-02 and the State Water Resources Control Board Water Quality Order No. 97-03-DWQ (general industrial storm water permit), or the current versions of each. Waste water shall be collected and discharged to the drains in hangar 811 only.

Wastewater is any used water generated or collected from washing aircraft, aircraft components, support equipment and vehicles used to wash aircraft or aircraft components, the floor of Hangar 811, or collected from outside hangar 811 as a result of the performance of this PWS. For the purpose of this PWS, support vehicles are vehicles used solely in accomplishing this PWS.

Support vehicles do not include privately owned vehicles (POVs) or company vehicles which are also for personal use or pleasure, regardless of whether they are used in the accomplishment of

Aircraft Corrosion Control Services this PWS. The SP shall provide 60 CONS with a list of support vehicles to be used. The SP shall then be restricted from using or washing any other support vehicles in hangar 811 without prior written approval from 60 CONS and 60 CES/CEA. Waste water may not be generated from any other process or equipment or building washing without prior written approval from 60 CONS and 60 CES/CEA. Hoses shall be maintained so as not to leak. Shut off hose connections in the floor, when not in use.

3.8. Water Usage. The SP will report monthly water usage to 60MXG/QAE and 60CES/ENV Air Quality Program Manager. Water reports will be distributed no later than the 1st of the following month. Maintain water usage records for life of the contract.

3.9. Government Furnished Storage Tanks. The SP is responsible to ensure compliance with 40 CFR 112, the California Health and Safety Code Chapter 6.67, Section 25270.3 and the 60 AMW Integrated Contingency Plan for the above ground storage tank(s) for SP use.

Requirements include conducting daily, weekly, monthly visual inspections using AFTO Form 39 and the Monthly Above Ground Storage Tank Inspection Checklist. The government will be responsible for maintenance of the tanks. However, the SP may be liable for damage to the tank considered to be other than normal wear and tear.