BOST-515-18_LCAC_33.pdf

PDF 2 MB Posted Jun 26, 2018

Attached to: LCAC 33 Post SLEP Extension (PSE) Federal contract opportunity
Solicitation number: N55236-18-R-0018
Issued by: Department of the Navy Naval Sea Systems Command

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EXHIBIT A- BOST-515-18 LCAC 33

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Attachment_2_-_Request_for_Specification_Clarification_Form.docx	DOCX document	Jun 26, 2018

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DEPARTMENT OF THE NAVY

NAVSEA BOSTON

LCAC 33 (LCAC 33)

SPECIFICATIONS FOR WORK TO BE ACCOMPLISHED

SPECIFICATION NUMBER: BOST-515-18

SHIP CHARACTERISTICS

LENGTH OVERALL

MAX. BEAM AT DESIGN WATERLINE

91 FEET

47 FEET

10 INCHES

EXTREME BEAM INCLUDING APPENDAGES 49 FEET 2 INCHES

DRAFT (MAX. NAVIGABLE) (FWD.)

DRAFT (MAX. NAVIGABLE) (AFT.)

3 FEET

2 INCHES

LIGHT DISPLACEMENT 90 LONG TON

FULL LOAD DISPLACEMENT 162 LONG TON

HEIGHT OF MAST ABOVE DESIGN WATERLINE 18 FEET 6 INCHES

33 5 15 bbessette Cross-Out bbessette Cross-Out bbessette Cross-Out bbessette Cross-Out bbessette Cross-Out bbessette Cross-Out bbessette Cross-Out bbessette Cross-Out bbessette Cross-Out bbessette Cross-Out bbessette Cross-Out bbessette Cross-Out

33 5 15 bbessette Cross-Out bbessette Cross-Out bbessette Cross-Out bbessette Cross-Out bbessette Cross-Out bbessette Cross-Out bbessette Cross-Out bbessette Cross-Out bbessette Cross-Out

SHIP: LCAC 33 (ACU 5) BOST-515-18

INDEX

CATEGORY II. FY-18 STANDARD ITEMS W HICH MAY BE INVOKED IN THE W ORK ITEMS OF THIS JOB ORDER

ITEM NO.

009-09

TITLE

Process Control Procedure (PCP); provide and accomplish

DATE

11/18/2016

009-11 Insulation and Lagging Requirements; accomplish 11/18/2016

009-12 Welding, Fabrication, and inspection Requirements; accomplish 11/18/2016

009-25 Structural Boundary Test; accomplish 11/18/2016

009-32 Cleaning and Painting Requirements; accomplish 03/07/2017 009-57 Reduction Gear Security Requirements; accomplish 11/18/2016

009-63 Lubricating Oils and Hydraulic Fluids; analyze 11/18/2016

009-71 Testing Requirements for Piping Systems; accomplish

11/18/2016

009-86 Recovery and Turn-In of Ozone Depleting Substance (ODS); accomplish 11/18/2016

ITEM NO. TITLE

077-01-001 Hazardous Waste Produced on Naval Vessels; control

114-11-001 Fendering System; repair

150-11-001 Engine Module; inspect and repair

234-85-001 LCAC1 Class AER-430, Start Air Piping Bulkhead Union Modification; accomplish

234-90-004 Torque Meter Installation for ETF40B Main Propulsion Engine;

accomplish

243-11-001 Shafting; remove, turnover and install

245-11-001 Propeller Control Module; remove, turnover and install

245-11-002 Port and Starboard Propeller Centerbody; repair

245-85-001 LCAC1 Class AER-489, Composite Transfer Sleeve; accomplish

246-11-001 Starboard Propeller Duct Assembly; remove, turnover and install

246-12-001 Port Propeller Duct Assembly; remove, turnover and install

248-11-002 Cushion Vane Assembly; repair

248-11-003 Cushion Vane Actuator; remove, turnover and install

248-11-004 Lift Fan Bearing; replace

248-11-005 Starboard Lift Fan Blade Impeller Assembly Repair; accomplish

248-12-005 Port Lift Fan Blade Impeller Assembly Repair; accomplish

248-85-006 LCAC1 Class AER-526, Lift Fan Bearing Grease Relief; accomplish

248-85-007 LCAC Craft Change Document CCD-580 Rev 00, Cushion Vane

Bearing Replacement; accomplish

248-90-001 LCAC Craft Change Document CCD-553 Rev 00, Cushion Vane Fitting Modification;

accomplish

251-11-001 Blow-In Door and Filter Access Door Assembly; repair

251-11-002 Heater, Door Seal - Anti-Icing; test and repair

259-11-002 Main Engine Exhaust Collector; replace

304-11-002 Propeller Control Module Cabling; replace

324-85-003 LCAC Craft Change Document CCD-584 Rev 00, AC Ground Meter Replacement; accomplish

331-85-001 LCAC Craft Change Document CCD-569 Rev 00, Removal of Portable Emergency Light;

accomplish

513-11-001 Upstream Cooling Air System; repair

513-80-001 LCAC1 CraftAlt-250D Rev 00, APU Anti-Ice System; accomplish

514-85-001 LCAC AER-362, Starboard A/C Condensate Drain Clean-Out Installation; accomplish

555-11-002 Halon System Repair; accomplish

../workitem33/07701001.pdf ../workitem33/11411001.pdf ../workitem33/15011001.pdf ../workitem33/23485001.pdf ../workitem33/23490004.pdf ../workitem33/24311001.pdf ../workitem33/24511001.pdf ../workitem33/24511002.pdf ../workitem33/24585001.pdf ../workitem33/24611001.pdf ../workitem33/24612001.pdf ../workitem33/24811002.pdf ../workitem33/24811003.pdf ../workitem33/24811004.pdf ../workitem33/24811005.pdf ../workitem33/24812005.pdf ../workitem33/24885006.pdf ../workitem33/24885007.pdf ../workitem33/24890001.pdf ../workitem33/25111001.pdf ../workitem33/25111002.pdf ../workitem33/25911002.pdf ../workitem33/30411002.pdf ../workitem33/32485003.pdf ../workitem33/33185001.pdf ../workitem33/51311001.pdf ../workitem33/51380001.pdf ../workitem33/51485001.pdf ../workitem33/55511002.pdf

ITEM NO. TITLE

561-11-001 Steering Control Assembly; replace

562-11-001 Rudder Hydraulic Actuator; remove, turnover and install

562-11-002 Port and Starboard Rudder Assembly; remove, turnover and install

562-85-002 LCAC Craft Change Document-471 Rev 01, Modification to Split Rudder Bearing Fitting;

Accomplish

568-11-001 Port and Starboard Bow Thruster Bearing; replace

568-12-001 Bow Thruster Motor; remove, turnover and install

584-31-001 Bow Ramp and Stern Ramp Hydraulic Actuator and Cable Assembly; remove, turnover and install

584-31-002 Bow and Stern Ramp Bulb Seal Replacement; accomplish

625-11-001 Windshield Water Wash System Repair; accomplish

631-11-001 Yellow Line for Electrical Safety; install

631-11-002 Line Locker; clean and preserve

631-11-006 Wet Deck Compartment Preservation; accomplish

631-11-007 Paint Engine Bay Outboard Deck Shelf and Bulkhead Area; accomplish

631-90-003 LCAC Craft Change Document CCD-445 Rev 01, INCR 01, Limited Compartment Painting;

Accomplish

992-31-001 Cleaning and Pumping; accomplish

../workitem33/56111001.pdf ../workitem33/56211001.pdf ../workitem33/56211002.pdf ../workitem33/56285002.pdf ../workitem33/56811001.pdf ../workitem33/56812001.pdf ../workitem33/58431001.pdf ../workitem33/58431002.pdf ../workitem33/62511001.pdf ../workitem33/63111001.pdf ../workitem33/63111002.pdf ../workitem33/63111006.pdf ../workitem33/63111007.pdf ../workitem33/63190003.pdf ../workitem33/99231001.pdf

SHIP: ASSAULT CRAFT UNIT 5 (ACU

45411)

ITEM NO: 077-01-001

COAR: 16 PCN: LC33-L077

CMP: NONE

PLANNER: ROGERS, WALTER

SSP: BOST-515-18 1 of 5 ITEM NO: 077-01-001

EXPORT CONTROLLED DATA: This document contains technical information whose export is governed by U.S.

International Traffic in Arms Regulation (ITAR). This information must not be transferred to a foreign person/entity without proper authorization of the U.S. Government. Violations may result in administrative, civil, or criminal penalties.

1. SCOPE:

1.1 Title: Hazardous Waste Produced on Naval Vessels; control

1.2 Location of Work:

1.2.1 Throughout the Craft

1.3 Identification:

1.3.1 Not Applicable

2. REFERENCES:

2.1 Resource Conservation and Recovery Act (RCRA)

2.2 49 U.S.C. 5103, Federal Hazardous Materials Transportation Act

2.3 Applicable Hazardous Waste Manifest Form

2.4 10 U.S.C. 7311

3. REQUIREMENTS:

3.1 Manage and dispose of all hazardous waste listed in 3.5 in accordance with 2.1 and 2.2.

3.1.1 When a Navy generator number is required by this Work Item, submit the original of 2.3 to the SUPERVISOR for assignment of Environmental Protection Agency (EPA) or delegated state environmental agency identification number.

3.1.2 Manage and transport for Navy disposal, Navy-generated

hazardous waste listed in 3.5 in accordance with 2.1 and 2.2, as designated by the SUPERVISOR.

Report: HAZARDOUS WASTE MANIFEST AVAIL COMPLETE (Key Event) + 2 days

3.1.3 Submit one legible copy, in hard copy or approved

transferrable media, of 2.3 signed by the owner or operator of the disposal facility to the SUPERVISOR within 48 hours of receipt from owner or operator of disposal facility.

3.2 Complete documentation required by 2.1 and 2.2, using EPA or delegated state environmental agency identification number in accordance with 2.4.

3.2.1 Documentation related to hazardous waste generated solely by the physical actions of Ship's Force or Navy employees (termed Navy- Generated Hazardous Waste) on board the vessel shall only bear a generator identification number issued to the Navy pursuant to applicable law. The contractor shall obtain SUPERVISOR'S concurrence with the categorization of the waste as Navy-generated before

SHIP: ASSAULT CRAFT UNIT 5 (ACU 45411)

SSP: BOST-515-18 2 of 5 ITEM NO: 077-01-001

EXPORT CONTROLLED DATA: This document contains technical information whose export is governed by U.S.

completion of the manifest. The manifest prepared shall be presented to the SUPERVISOR for completion after the hazardous waste has been identified.

3.2.2 Documentation related to hazardous waste generated solely by the physical actions of contractor personnel (termed Contractor- Generated Hazardous Waste) shall bear a generator identification number issued to the contractor pursuant to applicable law.

Regardless of the presence of other material in or on the shipboard systems or structure which may have qualified a waste stream as hazardous, where the contractor performs work on a system or structure using materials (whether or not the use of such materials was specified by the Navy) which by themselves would cause the waste from such work to be a hazardous waste, documentation related to such waste shall only bear a generator number issued to the contractor.

3.2.3 Documentation related to hazardous waste generated by the combined physical actions of Navy and contractor personnel (termed Co-Generated Hazardous Waste) shall bear a generator identification number issued to the contractor pursuant to applicable law and shall also cite in the remarks block a generator identification number issued to the Navy pursuant to applicable law. When the contractor merely drains a system and such drainage creates hazardous waste or the contractor performs work on system or structure using materials which by themselves would not cause the waste from such work to be hazardous waste but such work nonetheless creates a hazardous waste, documentation related to such waste shall bear a generator identification number issued to the contractor and shall also cite in the remarks block a generator identification number issued to the Navy. The contractor shall sign the generator certification on the Uniform Hazardous Waste Manifest whenever use of the manifest is required for disposal. The contractor shall obtain SUPERVISOR's concurrence with the categorization of the wastes as co-generated before completion of the manifest. Manifests prepared shall be presented to the SUPERVISOR for completion after the hazardous waste has been identified.

3.3 If the contractor, while performing work at a Government facility, cannot obtain a separate generator identification number from the state in which the availability will be performed, the contractor shall notify the SUPERVISOR within three business days of receipt of written notification by the state. After obtaining approval of the SUPERVISOR, the contractor shall use the Navy site generator identification number and insert in the remarks block the contractor generator identification number issued for the site where his main facilities are located.

3.4 If, for availabilities at a contractor-owned or controlled facility, the Navy cannot obtain a separate generator identification number for use at a contractor facility, the Navy shall notify the contractor within three business days of receipt of notification by the state. The contractor shall dispose of hazardous waste in accordance with 2.1, 2.2, and 3.2.3.

3.5 Hazardous waste, as identified in 2.1, expected to be produced during performance of this Job Order:

AMOUNT

SSP: BOST-515-18 3 of 5 ITEM NO: 077-01-001

EXPORT CONTROLLED DATA: This document contains technical information whose export is governed by U.S.

TYPE NAVY CO-GENERATED CONTRACTOR

Acid Solutions (may include _____ ____________ __________ spent sulfamic, citric, chromic, nitric, sulfuric, hydrochloric, etc.)

Ethylene Glycol (Antifreeze) _____ ____________ __________

Sodium Hydroxide _____ ____________ __________

Cleaning Solvents _____ 30 Gallons __________

Sodium Phosphates (Tri, Bi, _____ ____________ __________ or Mono)

Fluorocarbons _____ ____________ __________

Morpholine _____ ____________ __________

Sodium Chromates _____ ____________ __________

Hydrazine _____ ____________ __________

Carbohydrazide _____ ____________ __________

Methyl Ethyl Ketone _____ ____________ __________

Spent Abrasive Blast Material _____ 3 Tons __________

(contaminated with a known hazardous waste)

Trichloroethane _____ 20 Gallons __________

Miscellaneous Chemicals _____ 10 Pounds 20 Pounds

(Ignitable)

Miscellaneous Chemicals _____ 10 Gallons __________

(Corrosive)

Miscellaneous Chemicals _____ ____________ __________

(TCLP Toxic)

Miscellaneous Chemicals _____ 10 Gallons __________

(Reactive)

Oil (Synthetic) _____ 30 Gallons __________

Paints (Enamel, Latex, _____ 20 Gallons __________

Epoxy, thinners, oil based, rubber paint, nonskid, lacquer, remover, varnishes)

Paints (May include lead, _____ 10 Pounds __________

SSP: BOST-515-18 4 of 5 ITEM NO: 077-01-001

EXPORT CONTROLLED DATA: This document contains technical information whose export is governed by U.S.

cadmium, or chrome)

Paint Strippers (phenols, _____ ____________ __________ lead, chromium)

Sludge (Contaminated with _____ 25 Gallons __________ a known hazardous waste)

Wool Felt (contaminated _____ ____________ __________ with chromium and PCB's)

Ventilation Debris/Residue

(heavy metals, e.g., cadmium, chromium) _____ ____________ __________

Insulation (May contain Lead) _____ 40 Square Feet __________

Oily Rags _____ 50 Pounds __________

3.6 Notify the SUPERVISOR at least one working day prior to shipment of hazardous waste for disposal.

Report: HAZARDOUS WASTE LISTING AVAIL COMPLETE (Key Event) + 3 days

3.7 Submit one legible copy, in hard copy or approved transferrable media, of a report identifying type, amount, and disposal cost of waste listed in 3.5 that was removed during the performance of this Job Order to the SUPERVISOR.

3.7.1 The report shall include analysis or other method used to identify the waste and state whether each listed waste was hazardous (with generator assignment), non-hazardous, or did not exist.

3.7.1.1 Chemical analysis shall be accomplished by laboratories with state or EPA approved quality assurance programs.

3.7.2 The contractor shall make an effort to minimize hazardous waste generation by reducing the volume or toxicity by neutralizing, recycling, or otherwise removing it from the requirements of Subtitle C of 2.1 and include a description of such efforts in the report.

3.8 Nothing contained in this Work Item shall relieve the contractor from complying with applicable federal, state, and local laws, codes, ordinances, and regulations, including the obtaining of licenses and permits in connection with hazardous waste handling and disposal in the performance of this contract.

4. NOTES:

4.1 The waste listed in 3.5 is based on the best information available at the time of preparation of the solicitation. Hazardous waste generated during the actual performance of the work may vary in type or amount from waste listed in 3.5 which may result in renegotiation for credit or increase pursuant to Paragraph (b) of 2.4. The contractor is expected to use best management practice to identify and dispose of all hazardous

SSP: BOST-515-18 5 of 5 ITEM NO: 077-01-001

EXPORT CONTROLLED DATA: This document contains technical information whose export is governed by U.S.

waste. Some of the substances listed in 3.5 may be neutralized, recycled, or otherwise removed from the requirements of Subtitle C of 2.1.

Inclusion of these substances in the waste listed in 3.5 does not preclude the contractor from taking action consistent with 2.1 to reduce or eliminate the hazardous constituents of any waste required to be disposed of under the contract in accordance with 2.2. Processes that add hazardous constituents to the bilges may require that bilge water be disposed of as a hazardous waste.

4.1.1 The types and amounts of wastes listed in 3.5 are estimates of waste to be disposed of under this contract as required by 2.4. They are not estimates of the amount of the work involved in generating that waste. The work requirements of each individual Work Item specify the actual work to be accomplished.

4.2 Hazardous wastes are determined by one or more of the following methods:

4.2.1 Chemical analysis which shows that the material

characteristics of ignitability, corrosivity, reactivity, and/or toxicity (Toxicity Characteristic Leachate Procedure - TCLP) exceed the limits for that material in 40 CFR 261.20 Subpart C.

4.2.2 Reference to a Material Safety Data Sheet (MSDS).

4.2.3 Applying knowledge of the hazardous characteristics of the waste in light of the materials or the process used.

4.3 Asbestos, bilge water, oil/water including sludge, debris and other contaminants, sludge which includes solids and sludge from ballast tanks, CHT tanks, voids, oily waste tanks, fuel ballast tanks, fuel oil tanks, skegs (West coast), PCB's (Maryland), etc., apply only in those states listing them as hazardous waste. When an availability is to be performed in a state where these items are hazardous waste, an estimate of the amount to be generated shall be included in 3.5.

5. GOVERNMENT FURNISHED MATERIAL (GFM):

5.1 LLTM:

1. None.

5.2 PUSH MATERIAL:

1. None.

5.3 KITTED MATERIAL:

1. None.

ITEM NO: 114-11-001

COAR: 16 PCN: LC33-L114

CMP: NONE

PLANNER: ROBERTS, JEARLD

DEMERS, RAY

SSP: BOST-515-18 1 of 4 ITEM NO: 114-11-001

EXPORT CONTROLLED DATA: This document contains technical information whose export is governed by U.S.

1. SCOPE:

1.1 Title: Fendering System; repair

1.2 Location of Work:

1.2.1 Fendering System, Main Deck, Starboard

1.2.2 Fendering System, Main Deck, Port

1.3 Identification:

1.3.1 Fuel Tank No. One (2-3-3-F)

1.3.2 Water Wash Tank (2-12-6-W)

1.3.3 Stowage Space (Line Locker) (2-2-3-A)

1.3.4 Flotation Void (2-13-4-V)

1.3.5 Flotation Void (2-12-3-V)

1.3.6 Flotation Void (2-13-3-V)

2. REFERENCES:

2.1 Standard Items

2.2 S9100-AC-TMM-033 Rev 03, Technical Manual for (SLEP) Landing Craft, Air Cushion (LCAC) Structural Maintenance and Repair (LCAC 33)

2.3 835-6517544 Rev E, LCAC AER-0255 Rev 01, LCAC Fender Repair/Improv.

Fender Repair Instruction

2.4 611-6517400 Rev C, C/A 0149K LCAC Fendering System Fender

Replacement/Improvement

2.5 835-6268569 Rev A, LCAC Tech Item #3 LCAC Eng Data Pkg Fender

Rep/Imprv

2.6 114-5749150 Rev F, LCAC Fender

2.7 114-5749563 Rev -, LCAC Extrusion-Tee

2.8 114-6386381 Rev A, Extrusion-Channel

2.9 114-6386239 Rev F, LCAC Fendering Installation

2.10 101-5749137 Rev PF, SLEP Flotation Compartment Assembly

2.11 111-5749138 Rev P-, SLEP Sidewall Plating Assy Fr 3 to Fr 18

2.12 111-5749139 Rev F, LCAC Sidewall Plating Details

2.13 2C532C405 Rev B, LCAC SLEP Acceptance Test Procedure, Freshwater

Tank Completion Test

2.14 631-6266706 Rev T, LCAC Paint and Marking

../techmanuals/S9100-AC-TMM-033.pdf ../dwgidx/8356517544.htm ../dwgidx/6116517400.htm ../dwgidx/8356268569.htm ../dwgidx/1145749150.htm ../dwgidx/1145749563.htm ../dwgidx/1146386381.htm ../dwgidx/1146386239.htm ../dwgidx/1015749137PF.htm ../dwgidx/1115749138P-.htm ../dwgidx/1115749139.htm ../test/2C532C405B.pdf ../dwgidx/6316266706.htm

SSP: BOST-515-18 2 of 4 ITEM NO: 114-11-001

EXPORT CONTROLLED DATA: This document contains technical information whose export is governed by U.S.

2.15 2C541C407 Rev C, LCAC Acceptance Test Procedure, Fuel Storage, Overflow, and Stripping Tank Tightness Test

3. REQUIREMENTS:

(V)(G) "JOINT VISUAL INSPECTION"

3.1 Accomplish a joint visual inspection within 10 days of start of availability with the SUPERVISOR of the fendering system and associated structure in each location listed in 1.2, for structural integrity, deterioration, pitting, cracks, and areas of damage or distortion, using

2.2 as guidance.

Report: VISUAL INSPECTION SITUATIONAL + 3 days

3.1.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.1, to the SUPERVISOR.

3.2 Accomplish the requirements of 009-25 of 2.1 for preliminary air test of each tank listed in 1.3.1 and 1.3.2. Test pressure shall be 2

PSIG.

3.3 Accomplish repairs to the fendering system located in 1.2, as designated by the SUPERVISOR as a result of 3.1.1, in accordance with 2.3 through 2.12, using 2.2 as guidance, and the following:

3.3.1 Remove existing and install new 3 linear feet of crushbox plating including internal stiffeners in way of the areas listed in

1.3.1 and 1.3.3 and located at Frame 3 Starboard.

3.3.2 Remove existing and install new 3 linear feet of crushbox plating including internal stiffeners in way of the areas listed in

1.3.2 and 1.3.4 and located at Frame 13 Port.

3.3.3 Remove existing and install new 3 linear feet of crushbox plating including internal stiffeners in way of the areas listed in

1.3.5 and 1.3.6 and located at Frame 13 Starboard.

3.4 Remove existing and install new 3 each rubber fender sections (Part Number 001 of 2.6, 54 inches each) in way of repairs.

3.4.1 Install Government Furnished Material (GFM) provided in 5.1.

3.4.2 Install new clamping bars and associated hardware in way of new installations in accordance with 2.3, 2.4 and 2.9.

3.5 Accomplish the requirements of 009-12 of 2.1, including Table 4, Column C, Lines One through 7.

3.5.1 Accomplish nondestructive testing in accordance with Line 10.

3.6 Accomplish the requirements of 009-25 of 2.1 for a completion air test of each tank listed in 1.3.1 and 1.3.2, using 2.13 as guidance for the tank listed in 1.3.2. Test pressure shall be 2 PSIG. Maintain test pressure for 15 minutes for temperature stabilization prior to start of test. Hold test pressure for 10 minutes. Allowable drop in pressure:

None.

../test/2C541C407C.pdf

SSP: BOST-515-18 3 of 4 ITEM NO: 114-11-001

EXPORT CONTROLLED DATA: This document contains technical information whose export is governed by U.S.

3.7 Accomplish the requirements of 009-32 of 2.1, including Table 2, Line 42, for new and disturbed surfaces of Area 6-A of 2.14.

3.7.1 Method of surface preparation shall not include Stainless Steel Shot or Waterjetting listed in Column A as an option.

3.8 Accomplish the requirements of 009-32 of 2.1, including Table 4, Line 26, Column A, and Table 4, Line 12, Columns B and D for a total of 10 square feet of disturbed surfaces in area listed in 1.3.1, using 2.14 as guidance.

3.8.1 Accomplish the requirements of 009-32 of 2.1, including Table 4, Line 26, Column A for a total of 10 square feet of disturbed surfaces in area listed in 1.3.2.

3.8.1.1 Accomplish the requirements of 009-32 of 2.1, including Table 4, Line 7, Columns B through G, using 2.14 as guidance.

3.8.1.2 Apply final topcoat of Formula 156 red.

(V)(G) "HYDROSTATIC TEST"

3.9 Accomplish the requirements of 2.15 for twenty-four hour continuous hydrostatic test of the tank listed in 1.3.1. Allowable drop in pressure:None.

Report: TEST RESULTS SITUATIONAL + 3 days

3.9.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.9 to the SUPERVISOR.

3.10 Accomplish the requirements of 009-32 of 2.1 for new and disturbed surfaces.

4. NOTES:

4.1 Work in this item interfaces with Work Item 631-11-002, Line Locker;

clean and preserve.

4.2 Opening and closing of the spaces listed in 1.3 is accomplished in Work Item 992-31-001, Cleaning and Pumping; accomplish.

5. GOVERNMENT FURNISHED MATERIAL(GFM):

5.1 LLTM:

TOTAL

QUANTITY

PROVIDED NAME Of PART

PIECE

NO.

REF

NO.

NATIONAL

STOCK

NO.

REQ

PARA NO.

1. 3 EA Fender, Rubber 5749150- 001 2.6

01-326- 3952 3.4.1

5.2 PUSH MATERIAL:

SSP: BOST-515-18 4 of 4 ITEM NO: 114-11-001

EXPORT CONTROLLED DATA: This document contains technical information whose export is governed by U.S.

ITEM NO: 150-11-001

COAR: 16 PCN: LC33-L150

CMP: NONE

PLANNER: ROBERTS, JEARLD

DEMERS, RAY

SSP: BOST-515-18 1 of 4 ITEM NO: 150-11-001

EXPORT CONTROLLED DATA: This document contains technical information whose export is governed by U.S.

1. SCOPE:

1.1 Title: Engine Module; inspect and repair

1.2 Location of Work:

1.2.1 Main Deck, Frames 11-16, Port

1.2.2 Main Deck, Frames 11-16, Starboard

1.3 Identification:

1.3.1 Quantity (One EA), Port Engine Module

1.3.2 Quantity (One EA), Starboard Engine Module

2. REFERENCES:

2.1 Standard Items

2.2 Systems, and Specifications, Systems and Specifications Steel Structures Painting Council Manual, Volume 2

2.3 802-7616004 Rev G, SLEP Plan View of Each Level, Deck & Platform

2.4 S6360-AE-MMA-010 Rev 13, Technical Manual For Landing Craft, Air

Cushion (LCAC) Corrosion Control

2.5 S9100-AC-TMM-033 Rev 03, Technical Manual for (SLEP) Landing Craft, Air Cushion (LCAC) Structural Maintenance and Repair (LCAC 33)

2.6 151-5749254 Rev AK, LCAC Structural Assy & Instl - Engine Compartment

2.7 151-5749255 Rev N, LCAC Sidewall Assy, Inboard - Engine Compartment

2.8 151-5749256 Rev E, LCAC Sidewall Assy, Outboard - Engine Compartment

2.9 151-5749257 Rev L, LCAC Bulkhead Assy, Fwd - Engine Compartment

2.10 151-5749258 Rev R, LCAC Bhd Assembly, Aft - Engine Compartment

2.11 151-5749259 Rev L, LCAC 01 Deck Assembly - Engine Compartment

2.12 151-6800348 Rev E, LCAC Floor Assembly - Engine Compartment

2.13 151-5749261 Rev N, LCAC Bhd Assy, Sta 47'-10 7/8" - Engine

Compartment

2.14 151-5749262 Rev T, LCAC Bhd Assy, Sta 53'-9 1/2" - Engine

Compartment

2.15 151-5749263 Rev S, LCAC Blow-In Wall Assy, Engine Compartment

2.16 151-5749264 Rev P, LCAC Shelf Assembly - Engine Compartment

2.17 151-5749265 Rev L, LCAC Inboard Sidewall Details - Engine

Compartment

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SSP: BOST-515-18 2 of 4 ITEM NO: 150-11-001

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2.18 151-5749266 Rev C, LCAC Sidewall Assy & Details, Outbd - Engine

Compartment

2.19 151-5749267 Rev H, LCAC Bulkhead Details, Fwd - Engine Compartment

2.20 151-5749268 Rev M, LCAC Bulkhead Assy & Details Aft - Engine

Compartment

2.21 151-5749269 Rev L, LCAC 01 Deck Details - Engine Compartment

2.22 151-5749270 Rev H, LCAC Floor Details - Engine Compartment

2.23 151-5749271 Rev H, LCAC Bulkhead Details, Sta 47'-10 7/8" - Engine

Compt

2.24 151-5749272 Rev G, LCAC Bulkhead Assy & Details Sta 53'-9.5" -

Engine Compt

2.25 151-5749273 Rev M, LCAC Blow-In Wall-Details Engine Compartment

2.26 151-5749274 Rev K, LCAC Shelf Details - Engine Compartment

2.27 261-7087184 Rev K, LCAC CRAFTALT 348K Machinery Vent and Drain Line

Modifications

3. REQUIREMENTS:

3.1 Solvent clean each deck and bulkhead area for the equipment listed in 1.3 at each location listed in 1.2. Accomplish the requirements of SSPC-SP-1 of 2.2.

(V)(G) "JOINT VISUAL INSPECTION"

3.2 Accomplish a joint visual inspection with the SUPERVISOR of engine module plating and stiffeners, interior and exterior, for structural integrity, deterioration, pitting, cracks, and areas of damage or distortion for the equipmment listed in 1.3 and located in 1.2, using 2.3 through 2.5 as guidance.

Report: STRUCTURAL INSPECTION AVAIL COMPLETE (Key Event) + 3 days

3.2.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing the results of the requirements of 3.2 to the SUPERVISOR showing exact locations of deficiencies and recommendations for repairs.

3.3 Remove existing and install new one square foot of engine module bulkhead plating in and around each Exhaust Drain Assembly for Engine Nos. One, 2, 3 and 4. Clad weld repair a total of 100 square inches of pitted plating for the equipment listed in 1.3 and located in 1.2, as designated by the SUPERVISOR as a result of 3.2.1 in accordance with 2.6 through 2.27, using 2.4 and 2.5 as guidance.

3.3.1 Retain hardware and hose/drain line assemblies for

installation.

3.3.2 Remove existing and install new an additional 4 square feet of bulkhead plating as designated by the SUPERVISOR.

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SSP: BOST-515-18 3 of 4 ITEM NO: 150-11-001

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3.3.3 Chip and grind surfaces flush and smooth in way of repairs.

3.4 Accomplish the requirements of 009-12 of 2.1, including Table 4, Column C, Lines One through 7.

3.4.1 Accomplish nondestructive testing in accordance with Line 10.

Report: NONDESTRUCTIVE TEST AVAIL COMPLETE (Key Event) + 3 days

3.4.1.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.4.1 to the SUPERVISOR.

3.5 Install each drain line removed in 3.3.1 in accordance with 2.27.

(V)(G) "TIGHTNESS TEST"

3.5.1 Upon completion of propulsion system operational test, inspect and verify tightness of each drain line installed in 3.5. Inspect for leaks, proper operation, and unobstructed flow in accordance with Test Note T-1 of 2.27. Allowable leakage: None.

Report: RESULTS OF 3.5.1 AVAIL COMPLETE (Key Event) + 3 days

3.5.1.1 Submit one legible copy, in hard copy or approved

transferrable media of a report listing results of the requirements of 3.5.1 to the SUPERVISOR.

3.6 Accomplish the requirements of 009-25 of 2.1 for local air hose test in way of repairs in 3.3. Allowable leakage: None.

3.7 Accomplish the requirements of 009-32 of 2.1 for new and disturbed surfaces.

4. NOTES:

4.1 Work in this item interfaces with Work Items 234-85-001, LCAC1 Class AER-430, Start Air Piping Bulkhead Union, 251-11-001, Blow-In Door and Filter Access Door Assembly; repair and 251-11-002, Heater, Door Seal - Anti-Icing; test and repair.

4.2 Preservation of the engine bay shelf is accomplished in Work Item 631-11-007, Paint Engine Bay Outboard Deck Shelf and Bulkhead Area;

accomplish.

5. GOVERNMENT FURNISHED MATERIAL (GFM):

5.1 LLTM:

1. None.

5.2 PUSH MATERIAL:

SSP: BOST-515-18 4 of 4 ITEM NO: 150-11-001

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ITEM NO: 234-85-001

COAR: 16 PCN: LC33-L430

CMP: NONE

PLANNER: ROBERTS, JEARLD

SSP: BOST-515-18 1 of 2 ITEM NO: 234-85-001

EXPORT CONTROLLED DATA: This document contains technical information whose export is governed by U.S.

1. SCOPE:

1.1 Title: LCAC1 Class AER-430, Start Air Piping Bulkhead Union Modification; accomplish

1.2 Location of Work:

1.2.1 Engine Compartment, Frames 12-15, Port

1.2.2 Engine Compartment, Frames 12-15, Starboard

1.3 Identification:

1.3.1 Not Applicable

2. REFERENCES:

2.1 Standard Items

2.2 234-5750029 Rev AK, LCAC Start System Installation, Engine

2.3 151-5749264 Rev P, LCAC Shelf Assembly Engine Compartment

2.4 151-5749274 Rev K, LCAC Shelf Details - Engine Compartment

2.5 S9502-AA-TMM-033 Rev 02, Operation and Maintenance Manual for (SLEP) Landing Craft, Air Cushion (LCAC) ETF40B Auxiliary Systems (LCAC 33)

2.6 LCAC1 CLASS AER-430, Start Air Piping Bulkhead Union Modification

2.7 S9100-AC-TMM-033 Rev 03, Technical Manual for (SLEP) Landing Craft, Air Cushion (LCAC) Structural Maintenance and Repair (LCAC 33)

3. REQUIREMENTS:

3.1 Accomplish removals, modifications and installations for LCAC1 Class AER-430, Start Air Piping Bulkhead Union Modification at each location listed in 1.2, in accordance with 2.2 through 2.6.

3.2 Accomplish a visual inspection of the air start piping and the engine shelf plating in way of each piping union located in 1.2, for structural integrity, deterioration, pitting, cracks, and areas of damage or distortion, using 2.2 through 2.4 and 2.7 as guidance.

Report: INSPECTION RESULTS SITUATIONAL + 3 days

3.2.1 Submit one legible copy, in hard copy or approved

transferrable media of a report listing results of the requirements of 3.2 to the SUPERVISOR.

3.2.2 Chip and grind surfaces flush and smooth in way of removals.

3.2.3 Accomplish the requirements of 009-25 of 2.1 for local air hose test of each modified bulkhead union. Allowable leakage: None.

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3.2.4 Restore mating surfaces exposed by removals. Repair by

removing high spots, burrs, abrasions and foreign matter, where removal can be accomplished by hand tools.

(V)(G) "OPERATIONAL TEST"

3.3 Accomplish an operational test of the start air piping system disturbed by this Work Item, under normal system operating pressure in accordance with Chapter 2 of 2.5. Allowable leakage: None.

3.4 Accomplish the requirements of 009-32 of 2.1 for new and disturbed surfaces.

4. NOTES:

4.1 This Work Item interfaces with Work Item 150-11-001 Engine Module;

inspect and repair.

5. GOVERNMENT FURNISHED MATERIAL (GFM):

5.1 LLTM:

1. None.

5.2 PUSH MATERIAL:

1. None.

ITEM NO: 234-90-004

COAR: 16 PCN: LC33-Q810

CMP: NONE

PLANNER: DEMERS, RAY

SSP: BOST-515-18 1 of 5 ITEM NO: 234-90-004

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1. SCOPE:

1.1 Title: Torque Meter Installation for ETF40B Main Propulsion Engine;

accomplish

1.2 Location of Work:

1.2.1 Starboard Engine Compartment, Frames 12-15

1.2.2 Port Engine Compartment, Frames 12-15

1.3 Identification:

1.3.1 Quantity (2 EA), No. One and No. 3 ETF40B Engine Assembly (E1 and E3)(Part No. 0-001-010-74) Find No. 3 of 2.2

1.3.2 Quantity (2 EA), No. 2 and No. 4 ETF40B Engine Assembly (E2 and E4)(Part No. 0-001-010-74) Find No. 3 of 2.2

1.3.3 Quantity (3 EA), Starboard Drive Shaft Nos. 5, 7 and 9

1.3.4 Quantity (3 EA), Port Drive Shaft Nos. 6, 8 and 10

1.3.5 Quantity (2 EA), No. 3 and No. 5 Gearbox, Assembly 5750403-1 of 2.3

1.3.6 Quantity (2 EA), No. 4 and No. 6 Gearbox, Assembly 5750403-2 of 2.3

2. REFERENCES:

2.1 Standard Items

2.2 234-7325552 Rev D, SLEP Modification, Engine Installation, Main

2.3 241-5750403 Rev W, LCAC Assembly, Engine Gearbox 3 thru 6

2.4 S9240-AA-TMM-033 Rev 02, Operational and Maintenance Manual for Landing Craft, Air Cushion (LCAC)Transmission System (LCAC 33)

2.5 252-8677619 Rev A, ECP 935-13-07 LCAC SLEP Engine Control System Installation Torque Meter

2.6 MIL-STD-2003, Electric Plant Installation Standard Methods for Surface Ships and Submarines

2.7 MIL-STD-1310, Shipboard Bonding, Grounding and Other Techniques for Electromagnetic Compatibility and Safety

2.8 S9200-A6-TMM-033 Rev 03, Operational and Maintenance Manual for Landing Craft, Air Cushion (LCAC) Propulsion System (LCAC 33)

2.9 4A436C453 Rev C, SLEP Acceptance Test Procedure, Control Alarm and Monitoring System Sensor Functional Test

2.10 4B234C451 Rev L, LCAC SLEP Acceptance Test Procedure, Propulsion/

Lift Engine Control System Functional Test

2.11 5A436C468 Rev G, LCAC SLEP Acceptance Test Procedure, CAMS B

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SSP: BOST-515-18 2 of 5 ITEM NO: 234-90-004

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Verification and Function Test

2.12 5B234C461 Rev E, SLEP Acceptance Test Procedure, Propulsion Gas Turbine Operational Test

2.13 5B241C462 Rev F, LCAC SLEP Acceptance Test Procedure, Engine and Transmission Functional Test

3. REQUIREMENTS:

(V)(G) "VERIFY SYSTEMS DE-ENERGIZED"

3.1 Prior to the start of work, assure that all electrical power to the equipment has been turned off, and that personnel are aware of the safety precautions that must be observed while working with any high voltage systems. Verify that all electrical, lubrication, and fuel systems have been tagged out.

3.1.1 Verify halon systems for the equipment listed in 1.3.1 and

1.3.2 have been de-energized, properly secured and tagged "safe for work" to safely accomplish work required by this Work Item. Ensure each squib actuator has been removed by the Unit.

3.1.1.1 Accomplish the requirements of 009-86 of 2.1.

3.2 Accomplish removals, modifications and installations of torque meters for the main engines listed in 1.3.1 and 1.3.2 and located in 1.2, in accordance with 2.2 through 2.6.

3.2.1 Remove the shafting listed in 1.3.3 and 1.3.4 using 2.4 as guidance.

3.2.2 Provide the services for gearbox oversight and inspection by the NSWC-PD Gearbox Inspection Team during the disassembly, installation of the torque meters, assembly and test of the equipment listed in 1.3, using 2.2 through 2.5 as guidance. Protect and retain removed equipment for installation.

3.2.2.1 Accomplish the requirements of 009-57 of 2.1.

3.2.2.2 Remove and dispose of system fluids in accordance with federal, state, and local laws, codes, ordinances, and regulations.

3.2.2.3 Protect, blank, wrap, cover, or mask equipment and

openings to preclude damage and prevent entry of contaminants into gas turbine engines to include foreign object debris (FOD).

3.2.3 Remove each gearbox listed in 1.3.5 and 1.3.6 in accordance with 2.2 through 2.4.

3.3 Remove existing, fit, and install new the following parts in accordance with 2.5:

QUANTITY NAME ITEM REF. FIGURE PART

REQUIRED OF PART NO. NO. DRAWING NO. NO.

6 EA Boot One 2.5 N/A 202K174-100/184

2 EA Boot 2 2.5 N/A 222K174-100/184

../test/5A436C468G.pdf ../test/5B234C461E.pdf ../test/5B241C462F.pdf

SSP: BOST-515-18 3 of 5 ITEM NO: 234-90-004

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8 EA Pin Contact 3 2.5 N/A M39029/29-212

8 EA Socket Cont 4 2.5 N/A M39029/30-218

3 EA Heat Shrink 5 2.5 N/A HRHF-250-10A

8 EA Shield,Pigtail 7 2.5 N/A CWT-3805-W2

8 EA Shield 8 2.5 N/A CWT-3805

3.4 Identify cabling, and the equipment by installing new label plates, cable bands and wire markers as follows:

3.4.1 Install new label plates conforming to MIL-DTL-15024.

3.4.2 Mark applicable lead designations on the lead markers by hot stamping (Branding). Lead markers are to be made of white insulating sleeving conforming to MIL-I-631, Type F, Grade A, Form U. Install lead markers hot stamped (Branded) with the word "Spare" and the cable designation of the cable containing the spare conductors on spare conductors. When cables have more than one spare conductor, bind the spare conductors together and identify them with a single lead marker.

3.4.3 Cable Tags (Bands) shall be of soft aluminum and conform to MIL-A-2877 and shall be embossed with the applicable cable designation using numbers and capital letters having minimum height of 3/16 inch and embossed to at least 1/64 inch above the surface.

Cable tags and securing strips shall have a thickness of 0.014 to

0.016 inch. Cable tags shall have a minimum width of one-half inch.

3.5 Bond and ground equipment in accordance with 2.7. Grounding straps shall be CRES 316L for topside equipment.

3.5.1 Acceptable criteria for equipment to hull ground via bond or ground strap is one-tenth ohm maximum.

3.6 Install Government Furnished Material (GFM) provided in 5.1 for the equipment listed in 1.3 and located in 1.2 in accordance with 2.4 and 2.8.

3.7 Install the equipment removed in 3.2.3 in accordance with 2.2 through 2.4, and 2.6.

3.7.1 Accomplish the requirements of 009-57 of 2.1.

3.8 Install the equipment removed in 3.2.1 in accordance with 2.4.

3.9 Review the Acceptance and Functional Test Procedures of 2.9 through

2.13 for accomplishment with the assistance of NSWC-PD Gearbox Inspection Team.

3.9.1 Review and edit each Acceptance and Functional Test Procedure to correspond to actual scope of work required to verify satisfactory completion of work required by this Work Item, including testing prior to removal of the equipment listed in 1.3 and located in 1.2, and final testing necessary to accomplish craft light-off.

Report: ACCEPTANCE AND FUNCTIONAL TEST PROCEDURE AVAIL COMPLETE (Key Event) - 14 days

SSP: BOST-515-18 4 of 5 ITEM NO: 234-90-004

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3.9.1.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.9.1 to the SUPERVISOR at least 14 days prior to accomplishment for review and approval.

(Q)(G) "SYSTEM VERIFICATION AND OPERATIONAL TESTING"

3.10 Accomplish the prerequisites and acceptance and system functional tests in accordance with each approved test procedure submitted in 3.9.

Record test results on Test Data Sheets. Verify operation using data contained in each test procedure for acceptance criteria. Install new system filters after completion of each individual flushing operation.

3.10.1 Adjust and correct equipment and systems to ensure successful completion of each test.

Report: COMPLETED ACCEPTANCE AND FUNCTIONAL TEST DATA

SHEETS

AVAIL COMPLETE

(Key Event) + 3 days

3.10.2 Submit one legible copy, in hard copy or approved

transferrable media, of completed Acceptance and Functional Test Data Sheets applicable to each test procedure accomplished in 3.10 to the

SUPERVISOR.

3.11 Accomplish the requirements of 009-32 of 2.1 for new and disturbed equipment.

4. NOTES:

4.1 Work in this item interfaces with Work Items 243-11-001 Shafting;

remove, turnover and install, 259-11-002 Main Engine Exhaust Collector;

replace, 555-11-002 Halon System Repair; accomplish and 631-11-007, Paint Engine Bay Outboard Deck Shelf and Bulkhead Area; accomplish.

4.2 Removals in 3.2.1 and installation of shafting in 3.8 including alignment of shafting to gearboxes is accomplished in Work Item 243-11- 001 Shafting; remove, turnover and install.

4.3 Disposal of system fluids and hazardous materials is accomplished in Work Item 077-01-001, Hazardous Waste Produced on Naval Vessels; control.

4.4 Point of Contact for required services in 3.2.2:

Darin Campbell, SWRMC C261 MGTI/ACU-5 31T OSR

Darin.Campbell@navy.mil

Phone: (760) 212-2629

5. GOVERNMENT FURNISHED MATERIAL (GFM):

5.1 LLTM:

TOTAL

QUANTITY

PROVIDED NAME Of PART

PIECE

NO.

REF

NO.

NATIONAL

STOCK

NO.

REQ

PARA NO.

1. 4 EA

O-ring, M83248/1-386

Figure 8-7, 2.8

01-005- 0533 3.6

SSP: BOST-515-18 5 of 5 ITEM NO: 234-90-004

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Index 14

2. 4 EA

O-ring, M83248/1-327

Figure 8-2, Index 1 2.4

01-005- 3213 3.6

3. 4 EA

O-ring, M83248/1-331

Figure 8-2, Index 6 2.4

00-167- 5157 3.6

4. 6 EA Seal, MS27196-24

Figure 8-3, Index 12 2.4

00-944- 5941 3.6

5.2 PUSH MATERIAL:

1. None.

ITEM NO: 243-11-001

COAR: 16 PCN: LC33-L243

CMP: NONE

PLANNER: DENISTON, MARK

DEMERS, RAY

SSP: BOST-515-18 1 of 3 ITEM NO: 243-11-001

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1. SCOPE:

1.1 Title: Shafting; remove, turnover and install

1.2 Location of Work:

1.2.1 Main Deck, Starboard

1.2.2 Main Deck, Port

1.3 Identification:

1.3.1 Quantity (12 EA), Power Transmission Shafting Assembly

1.3.1.1 Quantity (6 EA), Sections S1 through S11, Starboard, Figure 8-1 of 2.2

1.3.1.2 Quantity (6 EA), Sections S2 through S12, Port, Figure 8-1 of 2.2

2. REFERENCES:

2.1 Standard Items

2.2 S9240-AA-TMM-033 Rev 02, Operation and Maintenance Manual for Landing Craft, Air Cushion (LCAC) Transmission System (LCAC 33)

2.3 S9243-A2-TMM-033 Rev 02, Operation and Maintenance Manual for (SLEP) Landing Craft, Air Cushion (LCAC) Ancillary Propeller Equipment (LCAC) 033)

2.4 240-5750400 Rev G, LCAC Transmission System

2.5 241-5750320 Rev F, LCAC Power Transmission Installation

2.6 245-5750288 Rev F, LCAC Shaft, Drive-Propeller System

2.7 245-5750289 Rev K, LCAC Shroud-Drive Shaft

2.8 245-5750286 Rev R, LCAC Propeller Instl

3. REQUIREMENTS:

3.1 Accomplish alignment checks for Total Indicated Runout (TIR) and coupling deflections for the shafting listed in 1.3 and located in 1.2, in accordance with Paragraphs 6-6.5.8, 7-4.5.3 and 7-5 of 2.2.

Report: RESULTS OF TIR SITUATIONAL + 3 days

3.1.1 Submit one legible copy, in hard copy or approved

transferrable media, of a report listing results of the requirements of 3.1 to the SUPERVISOR.

3.2 Remove the shafting listed in 1.3 and located in 1.2 from the power transmission system and the propeller system, using 2.4 through 2.6 as

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SSP: BOST-515-18 2 of 3 ITEM NO: 243-11-001

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guidance.

3.2.1 Match-mark laminated shim spacers and fasteners and retain for reuse.

3.2.2 Remove high spots, burrs, abrasions, nicks, corrosion, gasket material, and foreign matter from exposed flanges and mating surfaces.

3.2.3 Retain Glass Reinforced Plastic (GRP) shroud assembly, Find No. One of 2.7 for installation.

(V)(G) "SHAFT INSPECTION"

3.3 Accomplish a visual external inspection of the shafting removed in

3.2 for deterioration, pitting, cracks, and areas of damage…

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