Attachment 5 -58331-4-100_26127.pdf

CUI

TEST#: ESR#:

WN#: SSP#:

WS#:

SRF-JRMC DET SASEBO TEST MEMO

TITLE

COOLING SYSTEM COMPONENT

TEST MEMO PREPARATION

PRINT NAME & SIGNATURE PHONE CODE DATE

PREPARED BY

REVIEWED BY

APPROVED BY

SHIP/HULL#

SCOPE

TEST COMPLETION

PRINT NAME & SIGNATURE ORGANIZATION BADGE/RANK DATE

LWC

S246

SRF-JRMC

DET SASEBO

POST-TEST TECHNICAL REVIEW

PRINT NAME & SIGNATURE PHONE CODE DATE

Evaluation: ACCEPTED REJECTED

Action necessary: REPAIR ITEMS RETEST EQUIPMENT RESUBMIT DATA

COMMENTS

SASN-26-S232-0007

SASN-003-26

252-8048

252-8049

252-8045

3/23/26

3/23/26

3/23/26

S246B

S246A

S246CTE

Replacement of cooling system component.

514-11-001

58331-4-100_26127

57078-RS01-L011

A. NAKASHIMA

PHILLIPS.SHAUN.P

ARRY.1093485625

Digitally signed by

PHILLIPS.SHAUN.PARRY.1093485625

Date: 2026.03.23 14:55:55 +09'00'

S. IIDA

S. PHILLIPS

NAKASHIMA.ATSUS

HI.1274756299

Digitally signed by

NAKASHIMA.ATSUSHI.1274756299

Date: 2026.03.23 09:08:09 +09'00'

IIDA.SHUNICHI.127

4619127

Digitally signed by

IIDA.SHUNICHI.1274619127

Date: 2026.03.23 09:29:32 +09'00'

NBU-7 / LARC-936

TEST#: 58331-4-100_26127 ESR#: SASN-26-S232-0007

WN#: 57078-RS01-L011 SSP#: SASN-003-26

WS#: 514-11-001

TEST PROCEDURE GENERAL NOTES

1. TEST SEQUENCE: Unless otherwise specified in the test document, this test procedure (TP) shall be completed in provided order.

2. VERIFICATION: The person designated to sign for an action verifies, based on personal observation, objective evidence, or watch stander reports and certifies by signature that the action has been performed in accordance with the specified requirements.

3. USE ORIGINAL DOCUMENTS: All data attached to the Master TP shall have original pen and ink entries on the data sheets (unless otherwise specified in the test procedure.)

4. USE DARK INK: All signature and data shall be in dark, water insoluble ink.

5. CORRECTIONS: When an error was made, it shall be corrected by drawing a single line through the error, recording the correct entry, initialing, dating and printing the name of the person making the correction in accordance with JOINT FLEET MAINTENANCE MANUAL (JFMM), COMUSFLTFORCOMINST 4790.3, VOLUME

V, QUALITY MAINTENANCE.

6. LATEST APPLICABLE REVISION: Use the latest applicable revision of plans, instructions, technical manuals, and other reference materials cited in this test procedure.

7. INSTRUMENT CALIBRATION: All measuring equipment shall be in current calibration as required by

NAVSHIPREPFACINST 4734.1.

8. OPERATION OF COMPONENTS: Only authorized personnel shall operate ship’s permanently installed equipment.

The cognizant Shop shall control and operate their temporary test equipment. Ship’s Force shall operate temporary systems and equipment that are formally turned over to the ship.

9. SAFETY INSTRUCTION: The Test Director is responsible for the safe conduct of this test. The safety precautions of NAVSHIPREPFAC M-5100.8 shall be observed at all times.

10. TEST STOPPAGE: The Test Director shall stop the test once a problem has been found in the system or equipment being tested. S246 Testing Standard Operating Procedure (SOP) shall be used to determine course of action prior to resuming the test procedure.

11. ENERGIZED EQUIPMENT: NSTM 300, para 300-2.4 shall be followed when working on energized equipment.

12. DATA COLLECTION: The test documents may require collection of additional data for which there is no acceptance criteria, provided the data sheet identifies that data is for information only.

13. SUPPLEMENTATION: When supplementation is made, annotate the supplemental information on the page with ‘See Remarks’ followed by a sequential numbering system corresponding in the Remarks section.

14. USE ASTERISK (*): When supplementation, correction and/or signature is made but there is not enough space, annotate using an asterisk (*) followed by sequential number adjacent to the portion then clarify on the same page using the same annotation.

WN#: 57078-RS01-L011 SSP#: SASN-003-26

COOLING SYSTEM COMPONENT

1. PURPOSE

1-1 The purpose of this test is to certify the satisfactory replacement of cooling system components.

2. REFERENCES

2-1 TECHNICAL MANUAL

2-1.1 F9YC0-AM-TMM-010, 020, 030; LIGHTER AMPHIBIOUS RESUPPLY CARGO, FIVE TON (LARC-V A1/A2)

2-2 ESR RESPONSE

2-2.1 LARC876-0017; Cooling System Component; replace

2-3 ISEA RESPONSE

2-3.1 LARC Cooling System Temperature Questions, 18 February 2026

2-4 JFMM-JOINT FLEET MAINTENANCE MANUAL

2-5 NAVSHIPREPFAC M-5100.8; SAFETY AND HEALTH PROGRAM MANUAL

3. TEST AND SUPPORT EQUIPMENT/MATERIAL

3-1 Craft Gauge / IQAN Display

4. GENERAL PRECAUTIONS

4-1 Only those personnel actively engaged in performing or witnessing this test shall be permitted in the testing area.

All specified safety regulations shall be strictly observed.

4-2 To prevent injury or death, ensure that certified test equipment is used during testing.

4-3 Safeguarding of personnel and equipment shall be adhered to at all times.

4-4 Never open the cap on the engine coolant system when the engine is hot (greater than 120°F). The system may be pressurized and contain coolant at temperatures which will cause severe burns.

4-5 Do not move the craft until all ground personnel have cleared the immediate area. Personnel in the surrounding area may be injured or killed if struck by the craft.

4-6 Do not move the craft until all personnel are securely onboard or have cleared the immediate mooring area.

Personnel in the surrounding area may be injured or killed if struck by the craft.

4-7 Personnel onboard the craft should be notified that transition from the land to water is in progress and from water to land is in progress. This notification will allow personnel to prepare for turbulence and the abrupt speed reduction when the front wheels become grounded. Failure to provide notice may result in serious injury or death to onboard personnel.

WN#: 57078-RS01-L011 SSP#: SASN-003-26

5. OPERATIONAL TEST

5-1 PRETEST BRIEFING Conduct a pretest briefing (e.g. safety precaution, station assignments, testing steps) with all involved test personnel.

5-2 AT LAND TEST Conduct the AT LAND TEST under following test conditions. Record result in its corresponding

TEST DATA SHEET.

5-2.1 ENGINE RUNNING

(1) Fan Motor Solenoid

a. Disconnect the Deutsch plug of the fan motor solenoid and confirm the fan starts immediately. Both fan solenoids should be disconnected and tested to ensure that both works. After confirmation, reconnect the Deutsch plugs.

Acceptance criteria: Each fan operates immediately upon disconnecting of the Deutsch plug.

(2) Engine Coolant Radiator, Fan Hydraulic Motor, Fan Brade, Fan Motor Relief Valve

a. Let the engine coolant temperature increase to 175°F to start the fan.

b. During fan operation, verify that the fan, mounting brackets, and radiator are functioning properly without excessive vibration or leaks, and ensure that the coolant temperature does not exceed 190°F.

Acceptance criteria: The fan drive motor function shall be properly without excessive vibration or leaks, and the coolant temperature shall remain at or below 190°F.

NOTE

IT IS POSSIBLE TO INCREASE THE HYDRAULIC OIL TEMPERATURE BY OPERATE THE HYDRAULIC

OIL HEAT EXCHANGER ISOLATION VALVE AND/OR BYPASS VALVE.

(3) Hydraulic Oil Radiator, Fan Hydraulic Motor, Fan Brade, Fan Motor Relief Valve

a. Let the hydraulic oil temperature increase to 150°F to start the fan (If either the FWD or AFT manifolds reach that temperature).

b. During the fan operation, verify that the fan, mounting brackets, and radiator are functioning properly without excessive vibration or leaks, and ensure that the hydraulic oil temperature does not exceed 160°F.

Acceptance criteria: The fan drive motor function shall be properly without excessive vibration or leaks, and the hydraulic oil temperature shall remain at or below 160°F.

WN#: 57078-RS01-L011 SSP#: SASN-003-26

5-3 AT SEA TEST Conduct the AT SEA TEST under following test conditions. Record result in its corresponding TEST

DATA SHEET.

5-3.1 SEA MODE

(1) Seawater Pump Solenoid

a. After the craft in the water, disconnect the Deutsch plug of the seawater pump solenoid, and confirm the seawater pump starts immediately. Both seawater pump solenoids should be disconnected and tested to ensure that both works. After confirmation, reconnect the Deutsch plugs.

Acceptance criteria: Each seawater pump operates immediately upon disconnection of the Deutsch plug.

(2) Engine Coolant Heat Exchanger, Strainer Baskets, Seawater Pump Solenoid, Seawater Pump

a. Let the engine coolant temperature increase to 175°F to start the seawater pump.

b. During the seawater pump operation, verify that the functioning properly without excessive vibration or leaks, and ensure that the coolant temperature does not exceed 190°F.

Acceptance criteria: The engine cooling function shall be properly without excessive vibration or leaks, and the coolant temperature shall remain at or below 190°F.

(3) Hydraulic Oil Heat Exchanger, Strainer Baskets, Seawater Pump Solenoid, Seawater Pump

a. Let the engine coolant temperature increase to 150°F to start the seawater pump.

b. During the seawater pump operation, verify that the functioning properly without excessive vibration or leaks, and ensure that the hydraulic oil temperature does not exceed 160°F.

Acceptance criteria: The hydraulic oil cooling function shall be properly without excessive vibration or leaks, and the hydraulic oil temperature shall remain at or below 160°F.

5-4 LWC and S246 shall sign on the last page of TEST DATA SHEET upon completion of the test.

5-5 Return system/equipment to readiness condition, as required.

6. TEST PROCEDURE COMPLETION

6-1 Sign the test procedure coversheet to confirm that the test procedure has been fulfilled and completed and return it to S246 for review and approval.

WN#: 57078-RS01-L011 SSP#: SASN-003-26

7. REMARKS

WN#: 57078-RS01-L011 SSP#: SASN-003-26

TEST DATA SHEET

5-2 AT LAND TEST

TEST CONDITION STEP ACCEPTANCE CRITERIA RESULT

5-2.1

ENGINE RUNNING

(1) Fan Motor Solenoid Each fan operates immediately upon disconnecting the Deutsch plug.

For Eng. Cool. Fan: □ SAT / □ UNSAT

For Hyd. Oil Fan: □ SAT / □ UNSAT

(2) Engine Coolant Radiator Fan Hydraulic Motor Fan Blade Fan Motor Relief Valve

The fan drive motor function shall be properly without excessive vibration or leaks, and the coolant temperature shall remain at or below 190°F.

□ SAT / □ UNSAT

(3) Hydraulic Oil Radiator Fan Hydraulic Motor Fan Blade Fan Motor Relief Valve

The fan drive motor function shall be properly without excessive vibration or leaks, and the hydraulic oil temperature shall remain at or below 160°F.

□ SAT / □ UNSAT

5-3 AT SEA TEST

TEST CONDITION STEP ACCEPTANCE CRITERIA RESULT

5-3.1

SEA MODE

(1) Seawater Pump Solenoid Each seawater pump operates immediately upon disconnection of the Deutsch plug. □ SAT / □ UNSAT

(2) Eng.Coolant Heat Exchanger Strainer Baskets Seawater Pump Solenoid Seawater Pump

The engine cooling function shall be properly without excessive vibration or leaks, and the coolant temperature shall remain at or below 190°F.

□ SAT / □ UNSAT

(3) Hyd. Oil Heat Exchanger Strainer Baskets Seawater Pump Solenoid Seawater Pump

The hydraulic oil cooling function shall be properly without excessive vibration or leaks, and the hydraulic oil temperature shall remain at or below 160°F.

□ SAT / □ UNSAT

5-4 COMPLETION OF THE TEST

RESPONSIBILITY PRINT NAME, SIGN & DATE

LWC

S246