C-130_Wash_Addendum_LOA_(20_Nov_18).pdf

-06'00'

DEPARTMENT OF THE AIR FORCE

HEADQUARTERS 96TH TEST WING (AFMC)

EGLIN AIR FORCE BASE FLORIDA

MEMORANDUM FOR RECORD

SUBJECT: Letter of Agreement between the 96 OG and the 96 MXG

1. This letter forms an agreement, whereby the 96 OG Det 1 will provide/comply with the items listed in Attachment 1 and perform the maintenance listed in Attachment 2 in support of the C- 130 Wash Addendum to contract FA2486-17-C-0019.

a. Requesting Activity: 96 OG Det 1

b. Description of work: C-130 Wash, see Attachment 2

c. Deliverables: 96 OG Det 1 will maintain the JON, which provides all applicable equipment, supplies, and materials. 96 OG Det 1 or their designated representatives will meet the specific requirements spelled out here, which are required to perform C-130 washes.

d. JON: AAZF0005 Large Aircraft Wash Rack

2. The effective date of this agreement is the date of the last signature.

ZICK.JAMES. Digitally signed by

ZICK.JAMES.M.1154444803

M.1154444803 Date: 2018.11.15 16:50:18

DEVIN S. TRAYNOR, Col, USAF JAMES M. ZICK, Col, USAF Commander, 96th Operations Group Commander, 96th Maintenance Group

Letter of Agreement between the 96 OG Detachment 1 and the 96 MXG 2

Attachment 1

WASHING AND CLEANING OF USAF C-130 AIRCRAFT

The 96 OG Det 1or their designated representatives shall be responsible for the following to ensure the C-130 washes are successful:

Provide at least a 24 hour notice prior to washes/clear water rinses so arrangements can be made with AGE to provide the required stands.

Provide at least a 24 hour notice to any changes in the wash/clear water rinse schedule due to tests, weather etc.

Ensure the aircraft is on the wash rack and prepared for wash by 0700 on the scheduled wash day. Aircraft not in place by 0700 may result in a delayed return of the aircraft.

Provide a JON for the following expenses if required:

-Two JKL Lifts and Scheduled Maintenance -NDI Inspections

-CTK

-All Other Equipment and Tools Necessary -LAN Drops -Computer and Printer -Desk and Chair

Coordinate the scheduled maintenance for the JKL Lifts and ensure training is available for the service provider.

The 96 OG Det 1 or their designated representatives shall use the specific guidance in T.O. 1C- 130A-23, T.O. 1C-130A-23CL-1, TO 1C-130J-23CL-1, TO 1C-130(A/H/M)J-23CL-1, and T.O.

1-1-691 to prepare the aircraft prior to the wash. Attachment 2 covers areas that SHALL be completed by the 96 OG Det 1 or their designated representatives, which includes aircraft towing to/from the wash rack. Steps not addressed on this list will be completed by the service provider.

Note: Specific T.O. steps were identified and validated on award of the contract. Subsequent T.O. changes may result in different headings, numbering and/or lettering. The 96 OG Det 1or their designated representatives shall perform these same steps based on the most up to date, published T.O. (s) regardless of heading, numbering, or lettering unless renegotiated with the service provider.

1228792094C Highlight

Letter of Agreement between the 96 OG Detachment 1 and the 96 MXG 3

Attachment 2

1C-130A-23CL-1 Section 1 Aircraft Washing and Cleaning Preparation Procedures

1. Park aircraft at a designated wash area in accordance with TO 1C-130H-2-09JG-10-1 and TO

1C-130H-2-10JG-00-1.

2. Lower wing flaps to full down position.

3. Open air deflector doors, pull and attach warning tag to PARATROOP AIR DEFLECTOR CONTROL/PARATROOP AIR DEFLECTOR CONT circuit breaker.

4. Close all doors, windows, hatches, and openings through which water and/or cleaningfluids could enter.

8. Disconnect all aircraft electric batteries. Protect the battery electrical receptacles with caps and plugs or barrier paper.

9. Remove left and right ramp hinge panels, belly band, and ramp closure access panels PN 344444-4L/R.

11. Install the following covers/plugs as applicable:

□ Pitot tube covers

□ Engine intake

□ Exhaust plugs PN 355419-1 only

□ Flight deck and cargo air-condition covers

□ APU exhaust covers and intake covers

□ Gun covers

□ AAR-44

□ AAR-47

□ ALLTV

□ DS/FLIR

□ AFT AN/ALQ-172 cooling intake and exhausts

□ 25mm purge fan exhaust cover and ensure gas purge door is closed and handle pinned

□ Nose Ram air cooling cover

□ ATM intake

□ ALQ-157 transmitters

□ Ensure Standoff Precision Guided Munitions portal plugs are installed on cargo ramp door (AC-130W aircraft)

14. Remove right and left wing inboard and outboard flap carriage covers.

16. Disconnect external power in accordance with TO 1C-130H-2-05JG-00-1, or deactivate the cargo door in accordance with TO 1C-130H-2-52JG-00-1, when performing maintenance, washing, cleaning, or inspecting aft of FS 865.

Letter of Agreement between the 96 OG Detachment 1 and the 96 MXG 4

1C-130A-23CL-1 Section 2 Aircraft Ext and Interior Cleaning & Washing Procedure

2-1.1, 2c.

c. Wash behind all removed wing root and fillet area access panels left and right side of aircraft (ISO and Post Desert Wash only).

2-1-2.

a. Remove loose soil in the flight deck, cargo compartment, cargo ramp, and cargo door by vacuuming. Lower cargo ramp and raise cargo door to full up and locked position. Scrub the flooring on the flight deck, cargo deck, and ramp with a mop dampened with a 5 to 1 solution of water and cleaner MIL-PRF-87937, Type I. Clean the mop frequently. Use a stiff bristle brushto remove stubborn stains.

b. High pressure, low volume, water spray equipment may be used for cleaning heavily soiled floorboards, subject to the restrictions below:

(1) Pressure is limited to approximately 500 PSI.

(2) Water temperature is limited to 120oF.

(3) Water volume shall be limited to approximately 2 gallons/minute.

(4) Cleaning operation shall be accomplished using water only. No detergents or soap shall be used with the pressure equipment inside the cargo compartment.

(5) Cargo ramp and door shall be fully opened.

(6) Start cleaning operation aft of FS 245 and direct all spray toward rear ofcargo compartment.

(7) After completion of cleaning operation, ensure the cargo floor andtie-down receptacles are completely dried.

h. Flush aft urinal drain line with cleaner MIL-PRF-87937 Type I, or equivalent. Use DXX290, Red Layout Dye Number 8 and check for any leaks in accessible urinal tubing. Repair or replace as needed.

1C-130A-23CL-1 Section 3 Aircraft Post Washing

3.1 steps:

8. Install Infrared (IR) shields.

11. Install left and right ramp hinge panels, belly band, and ramp closure access panels PN 344444-4L/R, after completing after wash inspection.

13. Install right and left wing inboard and outboard flap carriage covers.

15. Remove caps and plugs or barrier paper from battery electrical receptacles and reconnect all aircraft electric batteries. Secure battery quick disconnects with 0.020-inch copper safety wire.

16. Reactivate cargo door in accordance with TO 1C-130H-2-52JG-00-1.

19. Reinstall right side wing root and fillet access panels 171, 175, 181, and 182 (ISO and Post Desert Wash only).

Letter of Agreement between the 96 OG Detachment 1 and the 96 MXG 5

20. Reinstall left side wing root and fillet access panels 170, 174, 177, 178, and 179 (ISO and Post Desert Wash only).

When/if required

Section 6 Post-Desert After Wash Corrosion Inspection

Section 7 Post-Fire Extinguishing Agent Contamination After Wash Corrosion Inspection

Section 8 Post-MAFFS After Wash Corrosion Inspection

TO 1C-130J-23CL-1 TECHNICAL MANUAL CHECKLIST, CORROSION

PREVENTION AND CONTROL MANUAL WASHING AND CLEANING

Section 1-1 Acft Washing and Cleaning Preparation Procedures

1-1. AIRCRAFT WASHING AND CLEANING PREPARATION PROCEDURES

1. Park aircraft at a designated wash area in accordance with TO 1C-130J-2-09JG-10-1 and

TO1C-130J-2-10JG-00-1.

2. Open air deflector doors to full open position.

3. Lower wing flaps to full down position.

4. Close all doors, windows, hatches, and openings through which water and/or cleaningfluids

7. Remove right and left ramp hinge panels, ramp access enclosure panels, and belly band.

9. Install the following covers and plugs as applicable:

. Pitot tube covers . Engine intake covers . Exhaust plugs . Flight deck and cargo air-conditioner covers . APU exhaust covers and intake covers . AN/AAR-47 infrared sensor covers . AN/ALQ-157 transmitter covers

11. Remove right and left wing inboard and outboard flap carriage covers.

15. Close cargo ramp and door to fully closed position.

Letter of Agreement between the 96 OG Detachment 1 and the 96 MXG 6

16. Disconnect all aircraft electric batteries. Protect the battery electrical receptacles with caps and plugs or barrier paper.

17. Remove external electrical power.

Section 2-1 Aircraft exterior and interior cleaning and washing procedures

2-3 Local interior cleaning

2. Remove loose soil in the flight deck, cargo compartment, under Enhance Cargo Handling System (ECHS), cargo ramp, and cargo door byvacuuming.

3. Manually open cargo ramp fully.

4. Scrub the flooring on the flight deck, cargo floor, and ramp with a mop dampened with a 5 to 1 solution of water and cleaner MIL-PRF-87937, Type I. Clean the mop frequently. Use a stiff bristle brush to remove stubborn stains. Do not use high volumes of water inside the airplane.

Ensure the floor, including all tie down receptacles and ECHS coves are completelydried.

5. High pressure, low volume, water spray equipment may be used for cleaning heavily soiled floorboards, subject to the restrictions below:

a. Pressure is limited to approximately 500 PSI.

b. Water temperature is limited to 120 degree F.

c. Water volume shall be limited to approximately 2 gallons/minute.

d. Cleaning operation shall be accomplished using water only. No detergents or soap shall be used with the pressure equipment inside the cargo compartment.

e. Start cleaning operation aft of FS 245 and direct all spray toward rear ofcargo compartment.

f. After completion of cleaning operation, ensure the cargo floor and ECHS coves are completely dried.

6. Clean soundproofing (as required) with cleaner MIL-PRF-87937, Type IV or MIL- PRF- 85570, Type II.

3-1. AIRCRAFT POST WASHING PROCEDURES

4. Reinstall right and left ramp hinge panels, ramp access enclosure panels, and belly band after aircraft wash.

Letter of Agreement between the 96 OG Detachment 1 and the 96 MXG 7

6. Remove the following covers/plugs as required:

. Cargo compartment and paratroop door window vents and drain hole covers

. Pitot tube covers

. Engine intake covers

. Exhaust plugs

. Flight deck and cargo air-conditioner covers

. APU exhaust covers and intake covers

. AN/AAR-47 infrared sensor covers

. AN/ALQ-157 transmitter covers

8. Reinstall right and left wing inboard and outboard flap carriage covers.

9. Deleted.

10. Reinstall insulation blanket under latrine area at right FUS STA 737 to FUS STA 800 WL 146 to WL 159.

11. Reinstall the left wing root access panel between fuselage stations 597 and 617 after letter check inspection.

11A. (On aircraft modified by TO 1C-130(E)J-534) Remove protective material from the AN/AAQ-24(V)13 GLTAs and sensors.

12. Remove caps and plugs or barrier paper from battery electrical receptacles and reconnect all aircraft electric batteries.

13. Apply external power and close cargo ramp.

14. Disconnect external power.

4-1. AIRCRAFT POST WASHING LUBRICATION PROCEDURES

18. Perform operational checkout of left and right pressure box cooling fans in accordance with

TO 1C-130J-2-99JG-10-2, 99-16-07.

When/if required:

Section 6-1 Post-Desert After Wash Corrosion Inspection (Outside CONUS)

Letter of Agreement between the 96 OG Detachment 1 and the 96 MXG 8

TO 1C-130(A/H/M)J-23CL-1 TECHNICAL MANUAL CHECKLIST CORROSION

PREVENTION AND CONTROL MANUAL WASHING AND CLEANING USAF

SERIES AC-130J, HC-130J, AND MC-130J AIRCRAFT

Chapter 1 Preparation for Cleaning and Washing

1-1 AIRCRAFT WASHING AND CLEANING PREPARATION PROCEDURES.

1. Remove forward LAIRCM sensors (TO 1C-130(A/H/M)J-2-99JG- 10-2).

1A. Park aircraft at a designated wash area in accordance with TO 1C-130(A/H/M)J-2-09JG-10- 1 and TO 1C-130(A/H/M)J-2-10JG- 00-1.

2. Open air deflector doors to full open position.

3. Lower wing flaps to full down position.

4. Close all doors, windows, hatches, and openings through which water and/or cleaning fluids

6. Remove right and left ramp hinge panels and belly band panel. (Wash prior to isochronal inspection only.)

8. Install the following covers and plugs as applicable:

• Pitot tube covers

• Engine intake covers

• Exhaust plugs

• Flight deck and cargo air-conditioner covers

• APU exhaust covers and intake covers

• AN/AAR - 47 infrared sensor covers

• ALE-47 Countermeasure Dispenser Panels (as required)

10. Remove right and left wing inboard and outboard flap carriage covers.

11. Remove No. 1 and 2 heat shields prior to the No. 1 and 3 isochronal inspections. Remove No. 3 and 4 heat shields prior to the No. 2 and 4 isochronal inspections. Ensure area under heat shields is thoroughly clean of all soot, dirt and other contaminates. Heat shields will remain off until after accomplishment of the isochronalinspection.

13. Remove the left wing root access panel between fuselage station 597 and 617. (Wash prior to isochronal inspection only.)

14. Close cargo ramp and door to fully closed position.

Letter of Agreement between the 96 OG Detachment 1 and the 96 MXG 9

15. Disconnect all aircraft electric batteries. Protect the battery electrical receptacles with caps and plugs or barrier paper.

16. Remove external electrical power.

Chapter 2 Cleaning and Washing

2-3 LOCAL INTERIOR CLEANING.

Interior areas of the airplane subject to the accumulation of dirt, debris, and airplane fluids residue should be cleaned as required for the prevention of corrosion as well as to afford the detection of a breakdown in the corrosion protection finishes originally applied.

1. Engine dry bays become soiled from carbon residues. Prior to each ISO inspection, thoroughly clean interior of all dry bays aft of the engines by wiping with clean rags and cleaner MIL-PRF-87937, Type I, followed by wiping with clean dry rag. Then hand wash the dry bay interior using clean rags or sponges and cleaning compound MIL- PRF-87937, Type II, as directed by TO 1-1-691. Do not use a large volume of water. Dry the area by wiping with clean dry rags. Ensure that all cleaning solution is removed and no residue remains. Apply a light coat of Amlguard, MIL-DTL-85054, Type I, to areas where the coating system is cracked, missing or damaged.

2. Remove loose soil in the flight deck, cargo compartment, cargo ramp, and cargo door by vacuuming.

3. Manually open cargo ramp fully.

4. Scrub the flooring on the flight deck, cargo deck, and ramp with a mop dampened with a 5 to 1 solution of water and cleaner MIL-PRF- 87937, Type I. Clean the mop frequently. Use a stiff bristle brush to remove stubborn stains. Do not use high volumes of water inside the airplane.

Ensure the floor, including all tie down receptacles, is thoroughly dry.

5. High pressure, low volume, water spray equipment may be used for cleaning heavily soiled floorboards, subject to the restrictions below:

a. Pressure is limited to approximately 500 PSI.

b. Water temperature is limited to 120 degrees F.

c. Water volume shall be limited to approximately 2 gallons/minute.

d. Cleaning operation shall be accomplished using water only. No detergents or soap shall be used with the pressure equipment inside the cargo compartment.

e. Start cleaning operation aft of FS 245 and direct all spray toward rear of cargo compartment.

Letter of Agreement between the 96 OG Detachment 1 and the 96 MXG 10

f. After completion of cleaning operation, ensure the cargo floor is completely dried.

6. Clean soundproofing (as required) with cleaner MIL-PRF-87937, Type II, or MIL-PRF- 85570, Type II.

Chapter 3 Post Cleaning and Washing

3-1 AIRCRAFT POST WASHING PROCEDURES.

3. Reinstall right and left ramp hinge panels and belly band panel after isochronal inspection.

7. Reinstall right and left wing inboard and outboard flap carriage covers.

8. Reinstall No. 1 and 2 heat shields after No. 1 and 3 isochronal inspections. Reinstall No. 3 and 4 heat shields after No. 2 and 4 isochronal inspections.

9. Reinstall insulation blankets under latrine area at right FS 737 to FS 800 and WL 164 to WL 200.

10. Reinstall the left wing root access panel between FS 597 and FS617 after isochronal inspection.

11. Remove caps and plugs or barrier paper from battery electrical receptacles and reconnect all aircraft electric batteries.

12. Apply external power and close cargo ramp.

13. Disconnect external power

15. Reinstall LAIRCM forward sensors and perform LAIRCM system operational checkout (TO

1C-130(A/H/M)J-2-99JG-10-2)

Letter of Agreement between the 96 OG Detachment 1 and the 96 MXG 11