Att (3) RADCON Plan.pdf

30 September 2013

UNCLASSIFIED/FOR OFFICIAL USE ONLY

DISTRIBUTION STATEMENT C: Distribution authorized to U.S. Government agencies and their contractors only; Administrative/ Operational Use (April 2011). Other request shall be referred to Commander, Naval Air Systems Command, NAVAIR-4.1.8, 48110 Shaw Road, Bldg 2187, Suite 1123, Patuxent River, MD 20670

DESTRUCTION NOTICE - For unclassified, limited documents, destroy by any method that will prevent disclosure of contents or reconstruction of the document.

AE2100 RADCON ENGINE TEARDOWN

INSPECTION PLAN

NAVAIR 4.1.8

:: OlgililllY~lgnod by WILDER ALONZO RA WILDERAlONZo.RAYMOND.1201208463

• '., DN:c.;;;;US,o:;;:;U.s.Govemmenl,ou=DoD.

YMOND.1201208463:~:::~;~~~Nzo.RAYMOND.1201208463 {:/ Date: 2013.09.3017:43;15..04'00'

Alonzo Wilder

NAVAIR 4.4.4.2

KC-130J/AE2100D3 Engines

. /.GIERBOLI N I.LU IS. :' DIgltalIy5lgnodbyGI!R801JNI.tU1SAl232UI0507/,.=~~~~~~":'=~~.A.1232160S07 ;/'·"o.tii'io13.10.o10835'.39-ll4'OO'

Luis A. Gierbolini

NAVAIR 4.1.1.3

KC-130JDeputy Chief Engineer

Timothy Bright KC-130JDeputy APML

BORGMEJERJAMES Ii OIglbllyslgnodbyBORGMElERJAME5.E.123Q08.4544

• (". DN;~. 0"lI.5.Gowmmenl,ou-DoO. ou=Pl<I, 1230084544 f :OIl..u5H. c....soRGMElERJAME5.E.1230084544• ~i·'·o.te2013.10.0112:22;33-Q4'OO' '

James Borgmeier v

NAVAIR 4.4.3.2

GREEN PAUL 5 1C 0Ig1bllyslgnodbyGREEN.PAULS.l068955994• • • 1,Dtte;US.O=U.5.Gowmment,OU=OoD, ; . ou=PJO, OU-USN, 068955994 .i .-~.PAIA..S.1068955994 l/ 0.10:2013.10.09_4>10 -lI4'OO'

Paul Green KC-13OJSustainment IPTL/COR

1. BŀŎƪƎNJƻdzƴŘ

This plan is for the teardown, test, and evaluation of AE2100D3 (AE2100) engines under USN Radiological Controls (RADCON). Due to engine operation in radiologically contaminated areas, specialized depot induction procedures are necessary to process potentially radiologically contaminated AE2100 engines. Propeller Gearbox (PGB) and Gearbox Mounted Accessory Drive (GMAD) modules may also be presented as standalone units for inspection. Processing and handling of these assets requires additional licenses and special handling procedures, segregation of material and tooling, and a segregated teardown and inspection facility capable of processing potentially contaminated parts. Inspection data will be collected and forwarded to NAVSEA 04N for analysis to determine whether the engines and/or the associated modules can be removed from radiological control. Upon NAVSEA 04N direction, parts verified clear of contamination following inspection may then be reintroduced into an authorized depot repair facility. Parts verified contaminated shall continue to be handled in accordance with Contractor’s radiological control procedures. Upon final adjudication of screened materials, the Government will coordinate disposal of contaminated whole engines and engine parts through established procedures using NAVSEADET RASO and DoD Executive Agent for Low Level Radioactive Waste (LLRW).

2. Scope

The following inspection plan documents the necessary steps for the Contractor to tear down, test, and evaluate RADCON AE2100 engines. The AE2100 engine is managed as a Quick Engine Change Assembly (QECA). For the purposes of this inspection the AE2100 engine consists of the PGB, GMAD, Power Section (PS), Torquemeter (TM), and Quick Engine Change (QEC) modules. PGB and GMAD may also be presented as standalone units for inspection. Prior to this inspection, measurements for radiological contamination have only been taken on external engine surfaces, and several PGBs, GMADs, and PGB lube oil and scavenge pumps have been inspected.1 The teardown inspection is required to gather data regarding the extent of radiological contamination of internal engine components and the QEC. QEC and engine disassembly and inspection will be performed by the Contractor. Contamination surveys will be performed by the Contractor using Government accepted equipment to determine the level of contamination. After QEC and engine disassembly, several components, as indentified in this plan will be surveyed using a Large Articles Monitor 12 (LAM 12).

Prior to taking possession of the subject RADCON assets , the Contractor shall have an agreement state license with their respective state or NRC license allowing them to receive, process, and store radiological contaminated hardware. The Contractor shall furnish a copy of this license to the Government prior to accepting deliveries of RADCON assets. The Contractor shall notify the Government if any changes are made to the license and shall furnish a copy of the updated license prior to delivery of the next scheduled RADCON asset.

1 AE2100 RADCON PROPELLER GEARBOX (PGB) TEARDOWN INSPECTION PLAN dated 14 August 2012.

paul.s.green Typewritten Text

3. Inspection Objective

This inspection will determine whether KC‐130J QECs and AE2100D3 engines can be cleared for un‐ restricted repair at the Contractor facility, and the results will be used to evaluate anticipated contamination levels in other KC‐130J QECs and AE2100D3 engines under radiological control.

Inspection results will be monitored and inspection plan may be revised as required with agreement with NAVSEA 04N, NAVAIR 4.1.8, C‐130 Fleet Support Team (FST), and the Contractor.

4. Description of Inspection Articles

Inspection articles are AE2100 PGB, GMAD, PS, TM, and QEC modules. PGB, GMAD, and TM modules may also be presented as standalone units for inspection. The Government will track and maintain a listing of suspect contaminated AE2100 engine and engine modules; this list will be updated as required by the Government and will be provided to the Contractor. The Government will provide the Contractor inspection documentation for PGB and GMAD modules that have been inspected and released from radiological control. In order to maximize engine availability, PGB and GMAD modules may be transferred between uninstalled inoperative engines. PGB and GMAD modules that are not under radiological control but associated with an engine under radiological controls will be surveyed externally upon their removal from the engine, and will not require a disassembly inspection.

5. Approach

The engine and QEC disassembly and inspection will take place in the inspection facilities identified by the Contractor. The Contractor will forward all applicable licensees and permits to the Government. Contractor will be responsible for complying with local, state, and federal regulations throughout the disassembly and inspection process.

There will be two milestones on the path to achieving inspection success.

The first milestone will be to obtain plan and contractual authorizations. NAVSEA 04N authorization is required regarding the inspection process and inspection test points. CNAF N42 authorization is required to move engines and QECs in exception to CNAP/CNAF message 3105554ZMAR11. C‐130 FST authorization is required for this inspection. KC‐130J Sustainment IPTL/COR authorization is required to indicate contractual agreement has been arranged with Rolls‐Royce and their designated sub‐contractors.

AE2100 engines and QECs will be shipped as a QECA by the appropriate Government activity to a Contractor facility as directed by TYCOM. PGB and GMAD may also be presented as standalone units for inspection. Prior to shipment, the Government will perform an external survey of the QECA, engine dolly, and preservation bag, or PGB/GMAD and shipping container by a trained individual2 using an MFR with DT‐304 probe, and record the results per the inspection sheets in Appendix A or B as applicable. Technicians will be trained and will comply with applicable RADCON procedures. The Appendix A survey sheets will be sent with the QECA, or the Appendix B survey

2 RADIOLOGICAL CONTROLS MANUAL FOR FUKUSHIMA DAI‐ICHI FALLOUT‐ NAVSEA 04N

sheets will be sent with the PGB/GMAD for shipment to the Contractor facility. Electronic copies of the Appendix A or B survey sheets will be provided to the C‐130 FST.

The second milestone will be to commence teardown and inspection of AE2100 engines and QECs.

Tooling requirements will be determined by the Contractor, with tooling provided by the Contractor and the Government per contractual agreements. Tooling used for this inspection will not traverse the radiological inspection area without radiological survey, decontamination, and documentation per a process of the Contractor's choosing that is compliant with local, state, and federal requirements. Government provided tooling will require Contractor provided documentation that the equipment is below 1,000 disintegrations per minute (dpm)/100 cm2 loose and 5,000 dpm/100 cm2 fixed contamination. For tools that have less than 100 cm2 surface area the whole tool shall be surveyed and results indicated as such. NAVSEA 04N shall approve the release of all tools prior to their return to the Government.

The engine and QEC disassembly inspection points are specified in Appendices C through K. In addition, specific components identified in the appendices will be surveyed in a LAM‐12 bulk counter provided for use on this effort by the Government. Electronic copies of the survey sheets will be provided to the C‐130 FST, and all survey results will be documented in Joint Deficiency Reporting System (JDRS) by the Government through coordination with the C‐130 FST.

Contaminated engine and QEC pieces shall be decontaminated below equivalent contamination levels of 1,000 dpm per 100 cm2 loose and 5,000 dpm/100 cm2 fixed. Following exhaustion of decontamination efforts, all pieces shall be re‐surveyed and documented on applicable inspection sheets in Appendices C through K. Tooling shall be surveyed, decontaminated, and documented in a manner of the Contractor's choosing. Materials used in decontamination shall be disposed of by the Contractor per local, state, and federal regulations.

In order to maximize availability of repairable assets, the Contractor will electronically forward the inspection results of QEC, TM, PGB, and GMAD modules to the Contracting Officer’s Representative (COR)/C‐130 FST per paragraph 7.2, and release for these individual modules will be requested based on the results. The PS module will remain associated with the engine serial number. The engine dolly and preservation bag will be cleared with the QEC module and used to transport the QEC module throughout the repair and shipping process. The AE2100 engine and QEC modules will be stored in a Radiologically Controlled Area (RCA) until the affected modules are released for repair per NAVSEA 04N, and TYCOM naval message. Applicable naval messages will be forwarded by the C‐130 FST/COR to the Contractor. After release has been annotated, Contractor repair of the engine or engine modules may begin in accordance with existing contracts.

6. Requirements:

6.1. Authorizations

The authorization process is necessary to begin this inspection. It is necessary to obtain authorization from NAVSEA 04N to ensure safety of personnel and compliance with all U.S.

Navy radiation safety practices. NAVAIR 4.1.8 authorization has been delegated to NAVAIR 4.4.3.2; this authorization provides confidence that data obtained upon inspection completion will support decisions regarding future decontamination procedures. CNAF authorization will allow test articles to be moved in exception to previously issued fleet directions. No contaminated engines and QECs will be moved until all authorizations have been obtained.

Contractual authorization is needed to use Contractor to perform the contamination inspection.

6.2. Personnel Safety

Personnel safety is of the utmost importance during this process. Contractor shall be responsible for ensuring the safety of persons performing the inspection, and to ensure adequate controls are utilized to ensure suspect contaminated parts, tooling, and materials are segregated in a RCA.

6.3. Emergency Response Plans [ERP]

The Contractor shall be responsible for ERP in accordance with local, state, and federal regulations.

6.4. Facility Protection

The Contractor shall be responsible for facility protection in accordance with local, state, and federal regulations.

6.5. Disposal

6.5.1. Engine and QEC Parts

Decontamination efforts will be limited to five attempts utilizing, CB‐R wipes, isopropyl alcohol, or other approved method agreed upon by the Contractor and the U.S.

Government. Parts that remain contaminated beyond 5,000 dpm/100 cm2 (or the entire part if less than 100 cm2 total surface area) fixed or greater than 15,000 dpm for the whole component will be segregated pending disposal disposition by the Government.

6.5.2. PPE/Decontamination Supplies

PPE and decontamination supplies shall be disposed of by the Contractor in accordance with local, state, and federal regulations.

6.5.3. Tools and Equipment

Contractor provided tools and equipment that cannot be decontaminated will be disposed by the Contractor in accordance with local, state and federal regulations. Government owned tools and equipment that cannot be decontaminated shall be disposed of by the Government as LLRW per NAVSEA 04N approved procedures.

6.5.4 Fluids

AE2100 engine/ QEC fluids will be drained by the Government IAW established procedures. Residual fluids such as lubricants and fuels shall be disposed of by the Contractor in accordance with local, state, and federal regulations.

7. Data Reporting

7.1. Daily

Pieces shall be surveyed as they are disassembled, and documented using the survey sheets provided in Appendices C through K. Upon the conclusion of decontamination attempts, contaminated pieces shall be resurveyed and documented on the inspection sheets.

7.2. Engine, QEC, PGB, and GMAD Survey Completion

A final report including all recorded survey data (including daily background and instrument checks), instrument calibration certificates, the minimum detectable activity for each instrument used, lessons learned, and recommendations for future action shall be generated by the Contractor with each release request and submitted to the COR/C‐130 FST. This data will be submitted for NAVAIR/NAVSEA review with coordination between the contracting officer and the C‐130 FST. All survey data will be documented in JDRS.

7.3. Teardown Completion

Upon conclusion of the teardown inspection of all modules, a final report including all recorded data, lessons learned, and recommendations for future action shall be generated by the KC‐ 130J/AE2100 Technical Team.

8. Listing of Appendices

Appendix A ‐ AE2100 QECA Pre‐Shipping Inspection Appendix B ‐ AE2100 PGB Pre‐Shipping Inspection Appendix C ‐ AE2100 QEC Subsystems Inspection Appendix D ‐ AE2100 QEC Propeller Controls Inspection Appendix E ‐ AE2100 QEC Electrical Inspection Appendix F ‐ AE2100 QEC Structure Inspection Appendix G ‐ AE2100 QEC Dolly and Preservation Bag Inspection Appendix H ‐ AE2100 Propeller Gearbox Disassembly Inspection Appendix I ‐ AE2100 Torquemeter Disassembly Inspection Appendix J ‐ AE2100 Engine External Inspection Appendix K ‐ AE2100 Power Section Disassembly Inspection

THIS PAGE INTENTIONALLY LEFT BLANK

Appendix A - AE2100 QECA Pre-Shipping Inspection

Appendix A - Page 1 of 8

Engine S/N ______________ KC-130J BUNO_______________ QEC Dolly P/N_____________ S/N____________ Engine Position:________ QEC S/N________________ Performed at __________________________Date_____________

Local Control Number

Instrument Type Instrument S/N Frisker Probe Type

Probe S/N Calibration Due Date

IM 265 DT-304

*All items within this document were frisked for radioactive contamination in accessible locations. Some items were also swiped/swabbed depending on geometry or presence of loose debris (ex. dirt) to obtain a removable (loose) contamination value. The highest reading was placed in data column.

_____No contamination above 100 ccpm was found on any component. (100 ccpm equals 1,000 dpm/100 cm2).

*All Frisk readings recorded are actual values from the instrument (CPM). No correction for background radiation (CCPM)

X X X

Radiation Safety Officer Surveyor Reviewer Signature/Printed Name/Date Signature/Printed Name/Date Signature/Printed Name/Date

X X X

Signature/Printed Name/Date Signature/Printed Name/Date Signature/Printed Name/Date

Appendix A - Page 2 of 8

Inspection Requirements:

Refer to NAVAIR 03-20KWD-2, Instructions With Parts Breakdown And Available Accessories Dolly, Q.E.C (Quick Engine Change Dolly) and NAVAIR 01-75GAJ-13JG-00-1, Technical Manual Job Guide Preservation, for additional information as required. Part numbers are representative numbers listed for reference only. Refer to NAVAIR 03-20KWD-2, and other C-130 publications for alternate part numbers as applicable.

These sheets document frisk survey results taken on the Quick Engine Change Assembly (QECA) prior to shipment. Submit these sheets with the QECA, and submit copies of these sheets to the C-130 FST. Contact the C-130 FST as soon as possible if the radiation survey indicates any contamination above 100 corrected counts per minute (ccpm).

Circumferential items/features shall be inspected at a minimum of three locations with up to a 360 degree inspection as available.

Reading from circumferential location with highest reading shall be recorded.

Inspection surface points that exceed 0.5 inch from inspection probe shall be wiped, and the wipe shall be analyzed for radioactivity.

If an oily surface inspection indicates levels 60 corrected counts per minute (ccpm) above background, then surface shall be wiped and the component shall be resurveyed. Annotate in the comments column for all oily components wiped.

Record background radiation readings on each survey inspection data sheet.

This inspection has instances where multiple items share the same figure and description; scan all items and record the highest value.

For parts with a large surface area describe the dimensions and location of the area that exhibits contamination in excess of 100 ccpm.

Appendix A - Page 3 of 8

Inspection Requirements: (continued)

When recording the instrument data for the DT304 Beta Probe record the serial number and calibration date for the DT685 Beta Probe Interface.

Note: Page 1 lists all of the equipment used for the inspection, and provides spaces for signatures. Electronic versions of these forms do not require signatures on every page if all signatures are provided on page 1. The inspections sheets may indicate a local control number for the IM-265 S/N, the DT-304 S/N, and the calibration due date, if this information is provided on page 1.

Appendix A - Page 4 of 8

FIGURE 1. QEC ASSEMBLY.

NOTE: FIGURE ILLUSTRATED WITHOUT PRESERVATION BAG AND WITH NACELLE ACCESS

PANELS REMOVED. REMOVAL OF PRESERVATION BAG FROM THE DOLLY AND ACCESS

PANEL REMOVAL IS NOT REQUIRED.

1 4

Date IM265 S/N DT-304 S/N Calibration Due Date Engine S/N

FRISK Surveyors Signature/Printed Name/Date FRISK Reviewer's Signature/Printed Name/Date

Appendix A - Page 5 of 8

FIGURE 1. QEC ASSEMBLY.

Background Reading (CPM)__________

Item # Description P/N

MAX/

Gross Frisk

(CPM)

Loose/ Swipe

(CPM)

Post

DECON

Frisk

(CPM)

Post

DECON

Loose/Swipe

(CPM)

Comments

1 ENGINE FORWARD SECTION IN VICINITY OF PROPELLER

GEARBOX AE2100

2 ENGINE AIR INTAKE AE2100

3 QECA EXTERNAL SKINS (SCAN ENTIRE SURFACE THAT IS

ACCESSIBLE) AE2100

4 ENGINE TURBINE AND EXHAUST (SCAN ENTIRE SURFACE

THAT IS ACCESSIBLE) AE2100

Open QEC preservation bag and survey accessible areas of the QEC. Scan the entire surface and annotate location and dimensions of any reading above 100 ccpm in the comments section.

If contamination that exceeds 100 ccpm is found then decontaminate as required prior to shipping.

Manually annotate all other external survey locations

Attach WRA / SRA Survey Form or WRA / SRA Decontamination Form if applicable.

Appendix A - Page 6 of 8

FIGURE 2. QEC DOLLY, QEC BAG, AND QEC ASSEMBLY.

Detail A

A

Date IM265 S/N DT-304 S/N Calibration Due Date Engine S/N

FRISK Surveyors Signature/Printed Name/Date FRISK Reviewer's Signature/Printed Name/Date

Appendix A - Page 7 of 8

FIGURE 2 QEC DOLLY, QEC BAG, AND QEC ASSEMBLY.

Item # Description P/N

MAX/

Gross Frisk

(CPM)

Loose/ Swipe

(CPM)

Post

DECON

Frisk

(CPM)

Post

DECON

Loose/Swipe

(CPM)

Comments

1* QEC BAG FORWARD (OR UPPER) SECTION (EXTERNAL) ATL 1175-

001G

2 QEC BAG ZIPPER (EXTERNAL) ATL 1175-

001G

3 QEC BAG VELCRO STRIP (EXTERNAL) ATL 1175-

001G

4* QEC BAG AFT (OR LOWER) SECTION (EXTERNAL) ATL 1175-

001G

5 QEC DOLLY, UPPER SECTION (EXTERNAL) 200-000-101

6 QEC DOLLY LOWER SECTION 200-000-101

7 ASSEMBLY, WHEEL (71670) (4 EACH) 200-000-117

8 ASSEMBLY, JACK 200-900-101

* There are two different styles of the C-130 QEC bag: the two piece bag with forward and aft sections is illustrated, and the two piece bag with upper and lower sections is not illustrated. Scan the entire surface and annotate location of any reading above 100 ccpm in the comments section.

If contamination that exceeds 100 ccpm is found then decontaminate as required prior to shipping.

Manually annotate all other external survey locations

Appendix A - Page 8 of 8

THIS PAGE INTENTIONALLY LEFT BLANK

Appendix B - AE2100 PGB Pre-Shipping Inspection

Appendix B - Page 1 of 6

PGB S/N________________ Removed from: Engine S/N ______________ KC-130J BUNO_______________________ Engine Position:________ QEC S/N________________ Performed at __________________________Date_____________

Local Control Number

Instrument Type Instrument S/N Probe Type Probe S/N Calibration Date

IM265 DT-304

*All items within this document were frisked for radioactive contamination in accessible locations. Some items were also swiped/swabbed depending on geometry or presence of loose debris (ex. dirt) to obtain a removable (loose) contamination value. The highest reading was placed in data column.

_____No contamination above 100 ccpm was found on any component. (100 ccpm equals 1,000 dpm/100 cm2)

*All Frisk readings recorded are actual values from the instrument (CPM). No correction for background radiation (CCPM)

X X X

Radiation Safety Officer Surveyor Reviewer Signature/Printed Name/Date Signature/Printed Name/Date Signature/Printed Name/Date

X X X

Signature/Printed Name/Date Signature/Printed Name/Date Signature/Printed Name/Date

Appendix B - Page 2 of 6

PGB Pre-Shipping Inspection Requirements:

These sheets document Frisk survey results taken on the PGB module prior to shipment. Submit these sheets with the PGB module, and submit copies of these sheets to the C-130 FST. Contact the C-130 FST as soon as possible if the radiation survey indicates any contamination above 100 ccpm.

PGB, Gearbox Mounted Accessory Drive (GMAD), and PGB lube and scavenge pump shall be drained prior to installation in the shipping container.

Circumferential items/features shall be inspected at a minimum of three locations with up to a 360 degree inspection as available.

Reading from circumferential location with highest reading shall be recorded.

Inspection surface points that exceed 0.5 inch from inspection probe shall be wiped, and the wipe shall be analyzed for radioactivity.

If an oily surface inspection indicates levels 60 corrected counts per minute (ccpm) above background, then surface shall be wiped and the component shall be resurveyed. Annotate in the comments column for all oily components wiped.

Record background radiation readings on each survey inspection data sheet.

Appendix B - Page 3 of 6

PGB Pre-Shipping Inspection Requirements: (continued)

For parts with a large surface area describe dimensions and location of area that exhibits contamination in excess of 100 ccpm.

Publication references refer to Rolls-Royce AE 2100D3 Engine Illustrated Parts Catalog,(IPC), CSP3304. Part numbers are representative numbers listed for reference only; refer to IPC for alternate part numbers.

When recording the instrument data for the DT304 Beta Probe, record the serial number and calibration date for the DT685 Beta Probe Interface.

Note: Page 1 lists all of the equipment used for the inspection, and provides spaces for signatures. Electronic versions of these forms do not require signatures on every page if all signatures are provided on page 1. The inspections sheets may indicate a local control number for the IM-265 S/N, the DT-304 S/N, and the calibration due date, if this information is provided on page 1.

Appendix B - Page 4 of 6

PGB ASSEMBLY EXTERNAL INSPECTION GUIDE

Propeller Gearbox (PGB) (Item 10) P/N_______________ S/N________________

Gearbox Mounted Accessory Drive (GMAD) (Item 20)

PGB Lube and Scavenge Pump (Item 30)

Note: PGB Struts (Item 40) Will not be shipped for inspection.

Date IM265 S/N DT-304 S/N Calibration Due Date PGB S/N

FRISK Surveyor's Signature/Printed Name/Date FRISK Reviewer's Signature/Printed Name/Date

Appendix B - Page 5 of 6

PGB ASSEMBLY EXTERNAL INSPECTION GUIDE

(72-00-00 Fig. 10) Background Reading (CPM)__________

Item # Description P/N

MAX/

Gross Frisk

(CPM)

Loose/ Swipe

(CPM)

Post

DECON

Frisk

(CPM)

Post

DECON

Loose/Swipe

(CPM)

Comments

10 GEARBOX ASSEMBLY, PROPELLER 23088983

20 ACCESSORY DRIVE ASSEMBLY, GEARBOX MOUNTED 23074576

30 PUMP ASSEMBLY, LUBE - SCAVENGE - PROP GEARBOX 23061016

Date IM265 S/N DT-304 S/N Calibration Due Date PGB S/N

FRISK Surveyor's Signature/Printed Name/Date FRISK Reviewer's Signature/Printed Name/Date

Appendix B - Page 6 of 6

PGB SHIPPING CONTAINER INSPECTION GUIDE (INTERIOR)

Item # Description P/N

MAX/

Gross Frisk

(CPM)

Loose/ Swipe

(CPM)

Post

DECON

Frisk

(CPM)

Post

DECON

Loose/Swipe

(CPM)

Comments

* CONTAINER, PROPELLER GEARBOX SHIPPING, BACK 23055358

* CONTAINER, PROPELLER GEARBOX SHIPPING, TOP 23055358

* CONTAINER, PROPELLER GEARBOX SHIPPING, FRONT 23055358

* CONTAINER, PROPELLER GEARBOX SHIPPING, BOTTOM 23055358

* CONTAINER, PROPELLER GEARBOX SHIPPING, LEFT SIDE 23055358

* CONTAINER, PROPELLER GEARBOX SHIPPING, RIGHT SIDE 23055358

PGB SHIPPING CONTAINER INSPECTION GUIDE (EXTERIOR)

Item # Description P/N

MAX/

Gross Frisk

(CPM)

Loose/ Swipe

(CPM)

Post

DECON

Frisk

(CPM)

Post

DECON

Loose/Swipe

(CPM)

Comments

* CONTAINER, PROPELLER GEARBOX SHIPPING, BACK 23055358

* CONTAINER, PROPELLER GEARBOX SHIPPING, TOP 23055358

* CONTAINER, PROPELLER GEARBOX SHIPPING, FRONT 23055358

* CONTAINER, PROPELLER GEARBOX SHIPPING, BOTTOM 23055358

* CONTAINER, PROPELLER GEARBOX SHIPPING, LEFT SIDE 23055358

* CONTAINER, PROPELLER GEARBOX SHIPPING, RIGHT SIDE 23055358

* Not Illustrated. Attach WRA / SRA Survey Form or WRA / SRA Decontamination Form if applicable.