Attachment_B-_MPC_723020.0_HC-130J_Comp_Wash.pdf

U.S. COAST GUARD

ASSET COMPUTERIZED MAINTENANCE SYSTEM

HC-130J

723020.0

REV'D 08/12/16

ASSET NUMBER OPERATING ACTIVITY MAINTENANCE ACCOMPLISHED MAINTENANCE DUE

DATE ASSET HOURS DATE ASSET HOURS

MO DAY YEAR MO DAY YEAR

ZULU DATE ZULU TIME

MO DAY YEAR

ITEM 1

DUE

CMS CODE ACTION DESCRIPTION CEINUM

723016 WASH ENGINE NO. 1 COMPRESSOR CLEANING 30-5300-001

SCHEDULED UNSCHEDULED

MAN HOURS: AMT___.___ AET___.___ AST___.___ PDM___.___ OTHER___.___

REMARKS:

TECHNICIAN'S

SIGNATURE

TECHNICIAN'S

ID

* ASTERISK INDICATES QA REQUIRED

*QA (1)

First/Last Name/Rate/Tech ID/MLH:___________________/________/________/____.____

First/Last Name/Rate/Tech ID/MLH:___________________/________/________/____.____

First/Last Name/Rate/Tech ID/MLH:___________________/________/________/____.____

REFERENCES:

AFTO 1C-130J-2-72JG-00-1, 72-30-20, Power Plant/Basic Engine - Job Guide

CGTO 35D3-41-1-2, Operation, Service, and Maint. Instructions with IPB for Engine Washcart P/N 400-65

FOR REFERENCE DETAILS, CONTACT HC-130J TECH SERVICES.

HC-130H MPC 710000.3

MPC 153001.0, Engine Wash Cart Semi-Annual Inspection

05-50-00-800-801, Rolls Royce Maint. Manual

REVIEWED

BY

LOG YN DATA

ENTRY

COMPLETED

Distribution Statement D: Distribution authorized to the DHS/CG/DoD and their contractors Administrative/Operational use, 08/12/16. Other requests shall be referred to the appropriate asset product line.

WARNING: This document contains technical data whose export is restricted by the Arms Export-Control Act (Title 22, U.S.C., Sec 2751, et. seq.) or the Export Administration Act of 1979, as amended, Title 50, U.S.C. App 2401 et. seq. Violations of these export laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DoD Directive 5230.25.

DESTRUCTION NOTICE: For classified documents, follow the procedures in DoD 5200.22-M, National Industrial Security Program Operating Manual, Section 5-705 or DoD 5200.1-R, Information Security Program Regulation, Chapter VI, Section 7. For unclassified, limited documents, destroy by any method that will prevent disclosure of contents or reconstruction of the document.

HC-130J

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REV'D 08/12/16

ASSET NUMBER OPERATING ACTIVITY MAINTENANCE ACCOMPLISHED MAINTENANCE DUE

DATE ASSET HOURS DATE ASSET HOURS

MO DAY YEAR MO DAY YEAR

ZULU DATE ZULU TIME

MO DAY YEAR

ITEM 1

DUE

CMS CODE ACTION DESCRIPTION CEINUM

723017 WASH ENGINE NO. 2 COMPRESSOR CLEANING 30-5300-001

SCHEDULED UNSCHEDULED

MAN HOURS: AMT___.___ AET___.___ AST___.___ PDM___.___ OTHER___.___

REMARKS:

TECHNICIAN'S

SIGNATURE

TECHNICIAN'S

ID

* ASTERISK INDICATES QA REQUIRED

*QA (1)

First/Last Name/Rate/Tech ID/MLH:___________________/________/________/____.____

First/Last Name/Rate/Tech ID/MLH:___________________/________/________/____.____

First/Last Name/Rate/Tech ID/MLH:___________________/________/________/____.____

REFERENCES:

AFTO 1C-130J-2-72JG-00-1, 72-30-20, Power Plant/Basic Engine - Job Guide

CGTO 35D3-41-1-2, Operation, Service, and Maint. Instructions with IPB for Engine Washcart P/N 400-65

FOR REFERENCE DETAILS, CONTACT HC-130J TECH SERVICES.

HC-130H MPC 710000.3

MPC 153001.0, Engine Wash Cart Semi-Annual Inspection

05-50-00-800-801, Rolls Royce Maint. Manual

REVIEWED

BY

LOG YN DATA

ENTRY

COMPLETED

DESTRUCTION NOTICE - Destroy by any method that will prevent disclosure of contents or reconstruction of the document. Page 2 of 12

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REV'D 08/12/16

ASSET NUMBER OPERATING ACTIVITY MAINTENANCE ACCOMPLISHED MAINTENANCE DUE

DATE ASSET HOURS DATE ASSET HOURS

MO DAY YEAR MO DAY YEAR

ZULU DATE ZULU TIME

MO DAY YEAR

ITEM 1

DUE

CMS CODE ACTION DESCRIPTION CEINUM

723018 WASH ENGINE NO. 3 COMPRESSOR CLEANING 30-5300-001

SCHEDULED UNSCHEDULED

MAN HOURS: AMT___.___ AET___.___ AST___.___ PDM___.___ OTHER___.___

REMARKS:

TECHNICIAN'S

SIGNATURE

TECHNICIAN'S

ID

* ASTERISK INDICATES QA REQUIRED

*QA (1)

First/Last Name/Rate/Tech ID/MLH:___________________/________/________/____.____

First/Last Name/Rate/Tech ID/MLH:___________________/________/________/____.____

First/Last Name/Rate/Tech ID/MLH:___________________/________/________/____.____

REFERENCES:

AFTO 1C-130J-2-72JG-00-1, 72-30-20, Power Plant/Basic Engine - Job Guide

CGTO 35D3-41-1-2, Operation, Service, and Maint. Instructions with IPB for Engine Washcart P/N 400-65

FOR REFERENCE DETAILS, CONTACT HC-130J TECH SERVICES.

HC-130H MPC 710000.3

MPC 153001.0, Engine Wash Cart Semi-Annual Inspection

05-50-00-800-801, Rolls Royce Maint. Manual

REVIEWED

BY

LOG YN DATA

ENTRY

COMPLETED

DESTRUCTION NOTICE - Destroy by any method that the document. Page 3 of 12

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REV'D 08/12/16

ASSET NUMBER OPERATING ACTIVITY MAINTENANCE ACCOMPLISHED MAINTENANCE DUE

DATE ASSET HOURS DATE ASSET HOURS

MO DAY YEAR MO DAY YEAR

ZULU DATE ZULU TIME

MO DAY YEAR

ITEM 1

DUE

CMS CODE ACTION DESCRIPTION CEINUM

723019 WASH ENGINE NO. 4 COMPRESSOR CLEANING 30-5300-001

SCHEDULED UNSCHEDULED

MAN HOURS: AMT___.___ AET___.___ AST___.___ PDM___.___ OTHER___.___

REMARKS:

TECHNICIAN'S

SIGNATURE

TECHNICIAN'S

ID

* ASTERISK INDICATES QA REQUIRED

*QA (1)

First/Last Name/Rate/Tech ID/MLH:___________________/________/________/____.____

First/Last Name/Rate/Tech ID/MLH:___________________/________/________/____.____

First/Last Name/Rate/Tech ID/MLH:___________________/________/________/____.____

REFERENCES:

AFTO 1C-130J-2-72JG-00-1, 72-30-20, Power Plant/Basic Engine - Job Guide

CGTO 35D3-41-1-2, Operation, Service, and Maint. Instructions with IPB for Engine Washcart P/N 400-65

FOR REFERENCE DETAILS, CONTACT HC-130J TECH SERVICES.

HC-130H MPC 710000.3

MPC 153001.0, Engine Wash Cart Semi-Annual Inspection

05-50-00-800-801, Rolls Royce Maint. Manual

REVIEWED

BY

LOG YN DATA

ENTRY

COMPLETED

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1 ENGINE COMPRESSOR CLEANING WASH

REFERENCES:

MPC 710030.0, Engine Runup Procedures MPC 723020.1, Engine Compressor Fresh Water Flush

TOOLS/TEST EQUIPMENT:

Compressor Wash Cart, P/N 400-65 Hose Adapter Kit, P/N 23066458 Maintenance Stand

EXPENDABLES:

NONE

CONSUMABLES:

Engine Gas Path Cleaner (Refer to approved cleaners listed in Table 1) Isopropyl Alcohol, TT-I-735 (Series) (As Needed)

A WASH

1. Ensure aircraft is safe for maintenance.

NOTE: The following Table 1 contains a list of approved cleaners for the AE2100D3 engine as per Rolls Royce. Prior to using any other cleaners, contact HC-130J Product Line.

SPECIFICATION APPROVED MANUFACTURERS

Airworthy, ZOK27LA Airworthy, Ltd., Elsted, Midhurst W. Sussex England GU29 OJT

Airworthy, ZOK27 Airworthy, Ltd., Elsted, Midhurst W. Sussex England GU29 OJT

Ardrox 624 Ardrox, Inc., 16961 Knott Ave., La Miranda, CA 90638

Ardrox 6345 Brent America, Inc., 921 Sherwood Drive, P.O. Box 215, Lake Bluff, IL 60044-0215

Ardrox 6367 Brent America, Inc., 921 Sherwood Drive, P.O. Box 215, Lake Bluff, IL 60044-0215

B and B 3100 B and B Tritech Inc., P.O. Box 270, Indianapolis, IN 46206

Brulin 1191 Brulin and Co, Inc., P.O. Box 270, Indianapolis, IN 46206

Cee Bee R674 McGran-Rohio, Inc.

9520 East Cee Bee Drive, Box 7000, Downey, CA 90241-0016

Pentone 19 Pentone Corp.

Aerospace Div, Ellipse, Suite 12 4201 Church Road, Mt. Laurel, NJ 08054

Rivenaes R-MCG-21 Ivar Rivenaes A/S Damsgardsvei 35 Bergen, Norway N-5000

Trafficair, Turboclean 2 Trafficair, Inc., 200 Technology Drive, Alpharetta, GA 30202

Turco 5884 Turco Products, Inc., P.O. Box 195, Hwy 95, Marion, OH 43302

Table 1

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2. Frequency of compressor cleaning:

a. Frequency of application is as follows:

(1) Engines which have been operated in a sea environment subject to salt water ingestion shall have the compressor inlet section fresh water flushed IAW MPC 723020.1 criteria to rinse away water soluble corrosive deposits from internal surfaces of compressor section.

(2) An engine that has ingested salt water or mist directly into compressor inlet shall receive a fresh water flush after the last flight of the day. This will cover such situations as seashore operations with wind pickup of salt water mist or spray.

(3) Engines not directly exposed to sea air environment, salt laden air, salt water mist or spray during flight or ground operation, but stationed in an area near such conditions, shall receive a fresh wa-ter flush at a minimum every 15 days, unless inspection of engine inlets during weekly inspections or preflight or post flight inspections necessitates a shorter interval.

NOTE: Frequent inspections for evidence of salt deposits and corro-sion in the compressor section shall be necessary to determine the corrosive environment to which the engines have been subjected.

NOTE: Engines flown off shore (from home station) on long route, high altitude, flights to areas where water wash facilities are not avail-able, shall receive fresh water flush wash upon return to home sta-tion.

(4) If able, an engine that will not be operated for an extended period of time and did not receive a fresh water flush after its last flight, shall require a compressor wash prior to going into inactive status. After a compressor wash has been completed, cover engine intake duct, exhaust duct, and close bleed valves.

CAUTION

DO NOT CLEAN THE COMPRESSOR IF AMBIENT AIR TEM-

PERATURE IS BELOW 5 DEGREES F. CLEANING SOLUTION

WILL FREEZE AND ICE CAN DAMAGE COMPRESSOR

BLADES AND VANES.

DO NOT CLEAN COMPRESSOR WITHIN 45 MINUTES OF

ENGINE SHUTDOWN OR UNTIL MEASURED GAS TEMPER-

ATURE IS LESS THAN 71 DEGREES C. DAMAGE COULD

OCCUR TO INTERNAL ENGINE COMPONENTS IF ENGINE IS

HOT.

3. Prepare compressor wash cart as follows (Refer to Figure 2):

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WARNING

ENSURE WATER AND SOLUTION TANKS ARE

DEPRESSURIZED PRIOR TO SERVICING. FAILURE TO DO

SO MAY RESULT IN INJURY TO PERSONNEL.

WARNING

AVOID EYE OR SKIN CONTACT WITH ENGINE GAS PATH

CLEANER, MIL-PRF-85704 (SERIES). THE FOLLOWING

CHEMICALS MEET MIL-PRF-85704 (SERIES): B&B

TC-100N-3, B&B 3100, OR TURCO 5884. AVOID INHALATION

AND INGESTION. USE IN WELL-VENTILATED AREA. WASH

THOROUGHLY AFTER HANDLING.

NOTE: High chlorides and mineral content in the flushing solution can adversely affect engine coatings and materials. Only de-ionized (preferred), distilled, or potable water (less than 50 ppm chloride) should be used.

a. Soap tank will be serviced with un-diluted soap from the approved cleaners listed from Table 1.

WARNING

KEEP ISOPROPYL ALCOHOL, TT-I-735 (SERIES), AWAY

FROM ALL SOURCES OF IGNITION. AVOID CONTACT

WITH SKIN OR EYES. AVOID INHALATION OR INGESTION.

ISOPROPYL ALCOHOL MAY DAMAGE SOME FORMS OF

PLASTICS, ALUMINUM, RUBBER, AND COATINGS.

b. If ambient temperature is 5 to 40 degrees F, mix equal volumes of clean filtered water and isopropyl alcohol in rinse tank on wash cart. If ambient temperature is above 40 degrees F, use only clean filtered water in rinse tank.

4. Prior to connecting cart to engine, remove salt and other corrosive water soluble deposits from each en-gine inlet duct, air inlet housing strut, and inner bands of inlet guide vanes. A solution wash, followed by fresh water rinse shall be accomplished to areas mentioned above prior to each compressor solution wash, utilizing compressor cart, P/N 400-65 (Refer to Figure 2).

a. Position wash cart at appropriate position to allow for usage of aux water hose to reach each QEC inlet.

b. Position COMPRESSOR DISCHARGE VALVE (1) on compressor air tank to “OPEN”.

c. Position WATER TANK VENT VALVE (10) to “OPEN”.

d. Position SOAP TANK VENT VALVE (11) to “OPEN”.

e. Start engine wash cart compressor, P/N 400-65.

f. Position COMPRESSOR DISCHARGE VALVE (1) to “CLOSED”.

g. Position WATER TANK VENT VALVE (10) to “CLOSED”.

h. Position SOAP TANK VENT VALVE (11) “CLOSED”.

i. Position COMPRESSOR DISCHARGE VALVE (1) “OPEN”.

j. Position WATER TANK PRESSURIZATION VALVE (2) to “OPEN”.

k. Position SOAP TANK PRESSURIZATION VALVE (3) on control panel to “ON”.

l. After air pressure has stabilized, verify pressures on soap tank regulator are 30 psi and water tank pressure tank is 50 psi. Adjust pressure regulators as needed.

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m. Position SOAP VALVE (8) on control panel to “ON”. (Soap will not be dispensed if valve is in closed position.)

n. Position SOAP AND WATER VALVE (6) on control panel to “ON”.

o. Position AUX WATER VALVE (12) on control panel to “ON”.

p. Extend AUX hose reel (9) and apply soap to engine inlets.

q. Position SOAP VALVE (8) on control panel to “OFF”.

r. Position SOAP AND WATER VALVE (6) control panel to “OFF”.

s. Position FRESH WATER ONLY VALVE (7) on control panel to “ON” and purge line until only fresh water is dispensed.

t. Rinse inlets with AUX hose reel nozzle.

u. Position AUX WATER VALVE (12) on control panel to “OFF”.

v. Position FRESH WATER ONLY VALVE (7) on control panel to “OFF”.

5. Connect compressor wash cart, P/N 400-65, to engine as follows (Refer to Figure 1 and Figure 2):

a. Position wash cart in appropriate position to allow for full extension of lines on hose reels numbered 1 through 4 (only if cart was repositioned during inlet wash).

b. Ensure all soap, water, and air valves are in the “OFF” position on wash cart control panel and no pressure is present in hose reels (Refer to Figure 2, Items 4 and 5).

c. Extend air and water lines from hose reels for their respective engine until they are fully extended and hose reels are locked and pinned to ensure reels will not retract during compressor wash procedure.

d. Open engine drain mast on QEC to access bleed valve air tube fitting and engine wash water fitting.

Connect air and water Iines to their respective fittings (Refer to Figure 1, Items 2 and 3).

CAUTION

BLEED VALVES MUST BE CLOSED BEFORE CLEANING

SOLUTION IS APPLIED. FAILURE TO CLOSE BLEED VALVES

WILL ALLOW CLEANING SOLUTION TO SPRAY INTO ENGINE

NACELLE AND DAMAGE ELECTRICAL WIRING AND CON-

NECTORS.

NOTE: Fittings are not interchangeable.

NOTE: Ensure air compressor is able to supply a minimum of 60 PSIG to close engine bleed valves.

e. Position REEL AIR valves on wash cart control panel to “ON” (Refer to Figure 2, Item 4).

6. Clean engine compressor as follows (Refer to Figure 2):

a. Apply aircraft electrical power.

b. Position one technician in the cockpit and one technician at the compressor wash cart with intercom extension for ground operation. Crew must be extremely alert for personnel hazards and objects that could cause FOD.

c. Verify that the FIRE HANDLE OIL electronic circuit breakers for affected engines are CLOSED.

Engine 1 2 3 4

FIRE HANDLE OIL 609 108 109 613

Table 2

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d. Position SOAP VALVE (8) on wash cart control panel to “ON”.

e. Position SOAP AND WATER VALVE (6) wash cart control panel to “ON”.

f. Position all engine REEL WATER VALVES (5) on wash cart control panel to “ON” to allow water/soap solution to prime all lines. Lines are considered primed when soap mixture comes out of intake scoop and appreciable drop in soap tank sight glass is noted.

g. Position all engine REEL WATER VALVES (5) to “OFF” position on wash cart control panel once all lines are primed.

h. Position No. 1 REEL WATER VALVE (5) to “ON” position on wash cart control panel.

CAUTION

DO NOT EXCEED STARTER DUTY CYCLE OF 70 SECONDS

ON, 1 MINUTE OFF, FOR FIVE CYCLES. AFTER FIVE CYCLES,

STARTER MUST COOL FOR 20 MINUTES. FAILURE TO COM-

PLY MAY CAUSE DAMAGE TO STARTER, ENGINE, AND AIR-

CRAFT.

i. Hold No. 1 ENGINE START switch to “MOTOR” for 60 seconds with soap solution.

j. Position No. 1 REEL WATER VALVE (5) to “OFF” position on wash cart control panel.

k. Allow soap solution to soak inside of compressor for 5-30 minutes before rinsing.

NOTE: Repeat steps 1 A 6.g. through 1 A 6.k. for subsequent en-gines.

7. Flush compressor with clean water as follows:

a. Position SOAP VALVE (8) on control panel to “OFF”.

b. Position SOAP AND WATER VALVE (6) on control panel to “OFF”.

c. Position FRESH WATER ONLY VALVE (7) on control panel to “ON”.

NOTE: Before initial rinse, allow rinse water to run for approximately one minute and fresh water is noted from QEC inlet intake. This allows for cleaning solution to be purged from water lines.

d. Position No. 1 REEL WATER VALVE (5) to “ON” position on wash cart control panel.

e. Hold No. 1 ENGINE START switch to “MOTOR” for 60 seconds with fresh water.

f. Position No. 1 REEL WATER VALVE (5) to “OFF” position on wash cart control panel.

NOTE: Repeat steps 1 A 7.d. through 1 A 7.f. for subsequent en-gines.

g. Position No. 1 REEL WATER VALVE (5) to “ON” position on wash cart control panel.

h. Hold No. 1 ENGINE START switch to “MOTOR” for 60 seconds with fresh water (second rinse).

i. Position No. 1 REEL WATER VALVE (5) to “OFF” position on wash cart control panel.

NOTE: Repeat steps 1 A 7.g. through 1 A 7.i. for subsequent en-gines.

j. Position No. 1 REEL WATER VALVE (5) to “ON” position on wash cart control panel.

k. Hold No. 1 ENGINE START switch to “MOTOR” for 60 seconds (third rinse), secure No. 1 REEL WATER VALVE (5) to “OFF” position 45 seconds after starter engagement. Motoring of engine for remaining 15 seconds will clear compressor of standing water.

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NOTE: Repeat steps 1 A 7.j. through 1 A 7.k. for subsequent en-gines.

l. Close all valves on the control panel.

m. Close WATER TANK PRESSURIZATION VALVE (2) and COMPRESSOR DISCHARGE VALVE (1).

8. Disassemble wash setup as follows (Refer to Figure 1):

a. Disconnect wash/water and air lines (2,3) from quick-disconnect fittings at engine drain mast.

b. Close engine drain mast (1,3).

c. Thoroughly rinse outside of nacelle, external tank, and fuselage with fresh water from AUX hose reel to prevent staining paint system with compressor wash residue.

d. Secure wash cart air compressor and depressurize wash cart.

* QA REQUIRED (1)

WARNING

ENGINES AND BLEED AIR MANIFOLD MUST BE PURGED

OF ALL TRACES OF CLEANING SOLUTION. FAILURE TO DO

SO WILL CONTAMINATE THE AIR CONDITIONING SYSTEM,

RESULTING IN BREATHING OF TOXIC VAPORS.

9. Perform engines runs to dry compressor as follows:

a. Within 30 minutes after compressor wash, operate engine IAW MPC 710030.0 at NORMAL GROUND IDLE for a minimum of 10 minutes. With each engine, after start cycle is complete (when start light extinguishes), immediately close nacelle shutoff valve for that engine. Once all engines are started, perform the following:

(1) Operate engine anti-ice for 1 minute, cycle off, and then operate again for 2 minutes.

(2) Place nacelle shutoff valves, switches to “AUTO”.

(3) On ice protection panel, place the WING/EMP ice protection switch to “AUTO”. Place DE-ICE/ANTI-ICE selector to “ANTI-ICE” for 2 seconds and then back to “DE-ICE”.

(4) WING/EMP A/I TEST advisory appears for the duration of the test (90 seconds).

(5) Once test is complete, place WING/EMP A/I switch to “OFF”.

(6) Operate flight deck and cargo compartment air conditioning units for a minimum of 4 minutes.

During operation, cycle temperature control valves to hot and back to cold.

(7) Secure engines.

(8) Record maintenance action by completing appropriate signoff, adding pertinent remarks.

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ENGINE COMPRESSOR WASH

Figure 1

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COMPRESSOR WASH CART

Figure 2

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