N0010420RF009.pdf

CODE

(Hour)

PAGE(S)

until local time

X

A X B X C X D

EX

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G F 46 - 53

54 - 61 X H 62 - 66 tammy.little@navy.mil

RATING PAGE OF PAGES

7. ISSUED BY

(Date)

IMPORTANT - Award will be made on this Form, or on Standard Form 26, or by other authorized official written notice.

Previous Edition is Unusable 33-134 STANDARD FORM 33 (REV. 9-97)

Prescribed by GSA FAR (48 CFR) 53.214(c)

DO 1 66

(If other than Item 7)

15A. NAME 16. NAME AND TITLE OF PERSON AUTHORIZED TO

AND

ADDRESS

SIGN OFFER (Type or print)

OF

OFFEROR

AMENDMENT NO. DATE

15B. TELEPHONE NO (Include area code) 17. SIGNATURE15C. CHECK IF REMITTANCE ADDRESS

IS DIFFERENT FROM ABOVE - ENTER

SUCH ADDRESS IN SCHEDULE.

18. OFFER DATE

1. THIS CONTRACT IS A RATED ORDER

UNDER DPAS (15 CFR 700)

2. CONTRACT NO.

N00104 8. ADDRESS OFFER TO

See Item 7

9. Sealed offers in original and copies for furnishing the supplies or services in the Schedule will be received at the place specified in Item 8, or if handcarried, in the depository located in

CAUTION - LATE Submissions, Modifications, and Withdrawals: See Section L, Provision No. 52.214-7 or 52.215-1. All offers are subject to all terms and conditions contained in this solicitation.

10. FOR INFORMATION

CALL:

A. NAME (NO COLLECT CALLS)

TAMMY R.A. LITTLE 717-605-4056

11. TABLE OF CONTENTS

SOLICITATION/ CONTRACT FORM

SUPPLIES OR SERVICES AND PRICES/ COSTS

2 - 5

X I CONTRACT CLAUSES

DESCRIPTION/ SPECS./ WORK STATEMENT X

PACKAGING AND MARKING

6 - 20 21 - 30

J LIST OF ATTACHMENTS

INSPECTION AND ACCEPTANCE

DELIVERIES OR PERFORMANCE

31 - 32 33 - 34

X K

REPRESENTATIONS, CERTIFICATIONS AND

OTHER STATEMENTS OF OFFERORS

CONTRACT ADMINISTRATION DATA 35 X

SPECIAL CONTRACT REQUIREMENTS

OFFER (Must be fully completed by offeror) 36 X M

L INSTRS., CONDS., AND NOTICES TO OFFERORS

EVALUATION FACTORS FOR AWARD

NOTE: Item 12 does not apply if the solicitation includes the provisions at 52.214-16, Minimum Bid Acceptance Period.

is inserted by the offeror) from the date for receipt of offers specified above, to furnish any or all items upon which prices are offered at the price set opposite each item, delivered at the designated point(s), within the time specified in the schedule.

13. DISCOUNT FOR PROMPT PAYMENT

(See Section I, Clause No. 52.232-8)

14. ACKNOWLEDGMENT OF AMENDMENTS

(The offeror acknowledges receipt of amendments

AMENDMENT NO. DATE

to the SOLICITATION for offerors and related documents numbered and dated):

FACILITY

12. In compliance with the above, the undersigned agrees, if this offer is accepted within calendar days (60 calendar days unless a different period

SOLICITATION, OFFER AND AWARD

X

(X) SEC. DESCRIPTION (X) SEC. DESCRIPTION PAGE(S)

PART I - THE SCHEDULE

26. NAME OF CONTRACTING OFFICER (Type or print) 27. UNITED STATES OF AMERICA 28. AWARD DATE

EMAIL:TEL: (Signature of Contracting Officer)

CODE CODE

B. TELEPHONE (Include area code) C. E-MAIL ADDRESS

AWARD (To be completed by Government)

19. ACCEPTED AS TO ITEMS NUMBERED 20. AMOUNT 21. ACCOUNTING AND APPROPRIATION

22. AUTHORITY FOR USING OTHER THAN FULL AND OPEN COMPETITION:

10 U.S.C. 2304(c)( ) 41 U.S.C. 253(c)( ) (4 copies unless otherwise specified)

23. SUBMIT INVOICES TO ADDRESS SHOWN IN ITEM

24. ADMINISTERED BY (If other than Item 7) CODE 25. PAYMENT WILL BE MADE BY CODE

PART IV - REPRESENTATIONS AND INSTRUCTIONS

PART III - LIST OF DOCUMENTS, EXHIBITS AND OTHER ATTACHMENTS

37 - 44

PART II - CONTRACT CLAUSES

NAVSUP WSS

TAMMY LITTLE, N743.12

5450 CARLISLE PIKE, PO BOX 2020, BLDG 412

MECHANICSBURG PA 17055 717-605-4056

FAX:

TEL:

FAX:

TEL:

NOTE: In sealed bid solicitations "offer" and "offeror" mean "bid" and "bidder".

SOLICITATION

6. REQUISITION/PURCHASE NO.

N0010420YRA12

5. DATE ISSUED

13 Dec 2019

4. TYPE OF SOLICITATION

SEALED BID (IFB)

NEGOTIATED (RFP)

[ X ]

3. SOLICITATION NO.

N0010420RF009

Section B - Supplies or Services and Prices

ITEM NO SUPPLIES/SERVICES QUANTITY UNIT UNIT PRICE AMOUNT

VA CLASS PROPULSOR ROTOR REPAIR

FFP

EVALUATE, REPAIR AND/OR MODIFY

S/N:

SMIC: P2

NSN: 2S 2010-01-534-8269

PURCHASE REQUEST NUMBER: N0010420YRA12

NET AMT

0001AA 1 Each

VA CLASS PROPULSOR ROTOR REPAIR

FFP

EVALUATE, REPAIR AND/OR MODIFY

S/N: 29979

SMIC: P2

INSPECTION AT ORIGIN

ACCEPTANCE AT ORIGIN

NOTE: The requirements in DFARS 252.211-7003, Item Identification and Valuation, are applicable for this line item. The contractor shall provide DoD unique identification or a DoD recognized unique identification equivalent.

FOB: Origin (Shipping Point)

NSN: 2S 2010-01-534-8269

PSC CD: 2010

0001AB 1 Each

VA CLASS PROPULSOR ROTOR REPAIR

FFP

EVALUATE, REPAIR AND/OR MODIFY

S/N: 29981

SMIC: P2

INSPECTION AT ORIGIN

ACCEPTANCE AT ORIGIN

NOTE: The requirements in DFARS 252.211-7003, Item Identification and Valuation, are applicable for this line item. The contractor shall provide DoD unique identification or a DoD recognized unique identification equivalent.

FOB: Origin (Shipping Point)

NSN: 2S 2010-01-534-8269

0001AC 1 Each

OPTION VA CLASS PROPULSOR ROTOR REPAIR

FFP

EVALUATE, REPAIR AND/OR MODIFY

S/N: TBD

SMIC: P2

INSPECTION AT ORIGIN

ACCEPTANCE AT ORIGIN

NOTE: The requirements in DFARS 252.211-7003, Item Identification and Valuation, are applicable for this line item. The contractor shall provide DoD unique identification or a DoD recognized unique identification equivalent.

FOB: Origin (Shipping Point)

NSN: 2S 2010-01-534-8269

0001AD 1 Each

OPTION VA CLASS PROPULSOR ROTOR REPAIR

FFP

EVALUATE, REPAIR AND/OR MODIFY

S/N: TBD

SMIC: P2

INSPECTION AT ORIGIN

ACCEPTANCE AT ORIGIN

NOTE: The requirements in DFARS 252.211-7003, Item Identification and Valuation, are applicable for this line item. The contractor shall provide DoD unique identification or a DoD recognized unique identification equivalent.

FOB: Origin (Shipping Point)

NSN: 2S 2010-01-534-8269

0002 1 Set

CONTRACT DATA REQUIREMENTS LIST

FFP

SEE SECTION C and DD form 1423 exhibit A

INSPECTION: SEE DD1423

ACCEPTANCE: SEE DD1423

FOB: Origin (Shipping Point)

NSN: 2S 2010-01-534-8269

OVER AND ABOVE WORK

FFP

FOB: Origin (Shipping Point)

NSN: 2S 2010-01-534-8269

Section C - Descriptions and Specifications

SECTION C

The attached Technical Data Package(s) is(are) incorporated by reference with the same force and effect as if contained herein:

CLIN: 0001/0002

NIIN: 015253159

TDP VERSION NO.: 013

ITEM NAME: VA Class Propulsor Rotor

Offerors are reminded that any resultant contract will require performance in strict compliance with the specifications set forth therein, and that prices offered should not be predicated upon Contractor anticipation of Government authorization of deviations, even though such deviations may have been granted previously under other contracts for the same item.

NSN 2S 2010-01-525-3159

Repair Statement of Work (SOW) SSN 774 Class Rotor

SN 29879

The following references apply:

(a) Technical Data Package & CDRL's A004, A005, A006, A007, A008, A009

(b) NAVSEA S9245-AZ-TSM-010/PROP (C)

(c) NAVSEA 245-7385828 Rev A (C), Rotor Assembly NDP3.1HS & HM

(d) NAVSEA 245-8328548 Rev B (C), Dimensional Inspection Requirements

(e) NAVSEA 245-7384173 Rev A (U), Propulsor Packaging and Preservation including

Configuration Change Request No. 245

(f) NAVSEA 245-8328541 Rev D (U), VA Rotor Field Replaceable Hardware

(g) NAVSEA 245-7651134 Rev A (U), NDP3.1H Rotor Hub Drill Jig for AM Tailcone

Holes

(h) NAVSEA 245-8328557 Rev B, SSN 774 Propulsor AM Tailcone

(i) NAVSEA 245-8357290 Rev A, VA Class Propulsor Threaded Inserts

(j) NAVSEA S9245-A4-TSM-010, Propulsor Paint Preservation

(k) NAVSEA 245-7642137 Rev E (C), Rotor Assembly NDP3.1HC

(l) NAVSEA 245-8216580 Rev A, Virginia Class Propulsor Axis Vertical Lifting Details and Transporter Attachment Procedure

(m) NAVSEA 245-7642140 Rev A, SSN774 Class Rotor Strongback Packaging Details

(n) NAVSEA 245-7642139 Rev A, SSN774 Rotor Strongback Trailer Loading

(o) MIL-DTL-2845, Propulsion Systems, Boat And Ship; Main Shafting, Propellers, Bearings, Gauges, Special Tools, and Associated Repair Parts; Preservation, Packaging, Packing and Storage of

The following notes and miscellaneous requirements apply.

1. All inspections and repairs shall be performed in accordance with references (a) through (o), as applicable, except as noted herein. In the event of a conflict between the references cited and this statement of work, the statement of work shall take precedence.

2. The facility must have personnel that have CONFIDENTIAL clearance and have successfully completed the NAVSEA Ducted Propulsor Visual Inspection Course.

3. CONFIDENTIAL inspection forms shall be submitted as a separate inspection report.

4. The vendor shall meet all applicable coatings qualification requirements of reference (j), including Society for Protective Coatings SSPC-QP3 qualification or NAVSEA approved equivalent. If the vendor is not qualified to SSPC-QP3 or by NAVSEA, they have the option to identify a qualified subcontractor to perform blasting and painting operations.

All personnel performing abrasive blasting shall have CONFIDENTIAL clearance and shall be certified in accordance with SSPC C-7, Abrasive Blasting. All personnel performing coatings application shall have CONFIDENTIAL clearance and shall be certified in accordance with Spray Application Certification or SSPC C-14, Marine Plural Component Program.

5. Stacking of VA class rotors is not authorized.

6. The rotor does not have side lifting points and a turnover fixture or J-bar is required for flipping. The means for flipping is the responsibility of the vendor and there is no GFE turning fixture designated for refurbishment work. The required sling length is a minimum of 15 feet for a straight lift, but a spreader bar is an acceptable alternative to maintain minimum 81 degree sling angle in accordance with Sheet 004-12 of reference (l).

ITEM 0001

1. Provide support to unload the rotor and strongback assembly from shipping trailer in accordance with references (m) and (n).

2. Remove paint layers, anti-fouling (AF) and anticorrosion (AC) from all painted surfaces by abrasive blasting or hand sanding. Blast media shall be in accordance with reference (j).

3. Conduct moisture removal procedure. Note that the Vendor shall provide and install new fill and vent hole plugs, sixteen (16) per blade following the moisture removal process. The following requirements apply:

a. Rotor must be positioned pressure face down.

b. All fill/vent plugs shall be removed from each rotor blade.

c. Heat must be applied to the entire blade. The temperature must be held in the temperature range of 200°F to 225°F. Heat can be applied through the use of a forced air heater and a custom heater bag designed to be slipped on over the blade to contain the heat.

d. Heat must be monitored by thermocouples mounted on the blades.

e. A vacuum must be applied to the entire blade during the heating process.

f. A sight glass shall be installed in-line with the vacuum pump to monitor presence of water.

g. A minimum pressure of 26” Hg should be held by the vacuum pump(s) throughout the entire evolution, approximately 10 days.

h. After the 10 day period, remove equipment and install new fill and vent hole plugs.

There are sixteen (16) 1/2” or 9/16” dia fill and vent plugs per blade.

4. Perform a pre-repair liquid penetrant (PT) aided visual technical inspection (VTI) on all surfaces in accordance with reference (a) and (b).

5. Perform a UT inspection of the blade 3C welds in accordance with references (a) and (b).

6. Remove previously installed bushings using hydraulic jacks.

7. Perform pre-repair dimensional inspection of every blade and hub outer surface using laser scanning inspection process to generate a dense point cloud of inspection data. Probe measurement uncertainty (error) shall be taken into account in accordance with ISO Standard 14253-1 when evaluating surface best fits. Currently, only Laser tracker and LEICA T-Scan equipment are approved for data acquisition. The data acquisition software and point cloud density requirements are:

a. Three hundred (300) points/sq-in for the leading edge and cusp region (extending 3" from LE).

b. One hundred (100) points/sq-in for the tip and trailing edge region (extending 5" from tip and 3" from TE).

c. Twenty (20) points/sq-in for the blade faces, hub fillets, and the hub outer surface.

Apply spray developer to all surfaces prior to scanning inspection surface. The pre-repair data shall be provided to Propulsor Technology, Inc. (PTI) at the address provided below for Navy repair evaluation (vendor is not responsible for the pre-repair evaluation of the collected data). The Navy evaluation will be provided to the vendor within 21 days of receipt of data. A copy of the Navy evaluation shall be included as part of the vendor’s dimensional report.

Propulsor Technology Inc.

80 Emerson Lane Suite 1302 Bridgeville, PA 15017-3472 Attn: Jim Machin, 412-914-1100

8. Perform System 21 Class 2 thread inspection on forward and aft hub face threaded holes used for lifting, handling and tailcone attachment. If the threaded holes fail the System 21 thread inspection, perform System 22 inspection.

9. Perform flange gage inspection in accordance with NAVSEA 245-8328556.

Shipping Materials, Accessories, Balance Weights and Bushing Material

1. Procure one rotor set of the Item 3 bushings (12 each), hub flange sleeve, in accordance with reference (f). Procure additional material to accomplish certification testing and retain a permanent heat sample record. Remove previously installed bushings and replace with Item 3 procured above.

2. Procure one rotor set of AM tailcone attachment hole plugs, Item 8328541-11, QTY (21).

3. Replace the following FWD face accessories as required:

a. FWD hub packaging hole plug, Item 8328541-9, QTY (8)

b. FWD lifting hole plug, Item 8328541-7, QTY (4)

c. Hub flange pin hole plug, Item 8328541-5, QTY (3)

4. Procure replacement security covers in accordance with reference (e).

5. Machined balance correction weights in accordance with reference (c).

6. Procure wood blocking and friction matting for shipment as required.

ITEM 0001 Repair and Inspection of Propulsor Rotor

1. Repair surface and edge defects as identified during pre-repair inspection and approved by

NSWCPD 426 by blending and welding as necessary. Hydro surface fairing rod inspection shall be accomplished on all repaired areas. Gages may be used as a guide.

2. Repair blade 3C weld defects by excavating and welding in accordance with references (a) and (b). Perform and document liquid penetrant (PT) aided visual inspection at the excavated areas prior to welding. Final NDE inspection shall consist of UT inspection and PT aided visual inspection in accordance with references (a) and (b). Repaired areas shall be inspected and evaluated using tactile inspection. In addition, hydro surface fairing rod inspection shall be accomplished on all repaired areas.

3. Repair threaded holes as required based on results from pre-repair inspection. Threaded holes shall be repaired and inspected in accordance with reference (b). Tailcone attachment holes shall not be welded and shall be repaired in accordance with reference (i).

4. Drill and tap AM Tailcone attachment holes in accordance with references (g) and (k). Drill fixture will be provided as GFP.

5. Restamp hub OD data as required in accordance with reference (c) and add the following, REP & BAL, (VENDOR) DATE (MM/YY).

6. Perform visual inspection of the rotor external surfaces prior to blast and paint application in accordance with references (a) and (b), as applicable. Additional UT and PT inspections are not required once performed at individual repaired areas. Provide advanced copy of VTI to NSWCPD 426 for acceptance prior to blast and paint application.

7. Perform dimensional inspection of every blade and hub outer surface using laser scanning inspection process to generate a dense point cloud of inspection data. Probe measurement uncertainty (error) shall be taken into account in accordance with ISO Standard 14253-1 when evaluating surface best fits. Currently, only Laser tracker and LEICA T-Scan

b. One hundred (100) points/sq-in for the tip and trailing edge region (extending 5" from

Apply spray developer to all surfaces prior to scanning inspection surface. The data shall be provided to PTI for information in the event that Navy technical support is required.

Provide an advance copy of the evaluation to NSWCPD Code 426 following post repair inspection. Need for additional fairing will be determined by NSWCPD Code 426 from the analysis of results.

8. Paint system(s) shall be applied in accordance with reference (j), Appendix C. A minimum of 4 dry film thickness (DFT) measurements shall be taken on each blade face. DFT measurements shall be taken at 3 locations on the hub outside diameter and 3 locations on the hub inside diameter. As required, Phillybond TA-30 shall be applied to seams and porosity after the first coat of paint has cured. The TA-30 shall be faired in to match surrounding surface and reapplied, if required, to ensure fairness. These repairs shall be roughened with 120 grit emery paper before application of the second coat of paint. All coatings inspections shall be performed by a Level 3 NACE Certified Coatings Inspector in accordance with reference (j). Upon completion, the NACE certified inspector shall provide written verification of successful coatings application to the vendor and NSWCPD Code 426.

9. Perform rotor balance following paint application. Note VA Class rotors do not have a tapered bore. Balancing operations require a vendor furnished balance adapter plate. The design of the adapter plate must be approved by NSWCPD Code 426. Note that the hub flange alignment pin hole plugs shall be installed during balancing operations. Remove the hub flange alignment pin hole plugs when balance is complete. A total of three balance runs shall be performed at the Top Dead Center (TDC) position as follows:

a. Perform one initial balance run.

b. Perform one balance run following balance weight installation.

c. Remove the rotor from balance machine. Re-install rotor on the balance machine and perform an additional balance run.

The first two balance runs shall be submitted as the initial and final data. The third balance run shall be provided for information only.

10. Provide support for acoustic tank testing per Advanced Engineering Consultants (AEC)

Drawing ME-1, NAVSEA TEST TANK. Acoustic test tank is provided as GFP. Support includes but is not limited to the following:

a. Assembly of Navy test tank, liner, plumbing connections. The test tank is 24 feet in diameter and 7 feet tall. A CONFIDENTIAL space of 30 feet in diameter is recommended to accommodate equipment and tank access. The vendor shall provide a stairway to gain access to the tank.

b. Purchase and/or rental of water pump, filter, and heating and cooling equipment.

c. Fill tank (approx. 15,000-20,000 gallons).

d. Install AM tailcone hole plugs prior to the acoustic test process.

e. Provide miscellaneous (i.e. crane) support to Navy Acoustic Test Personnel during testing.

f. Drain and disassemble tank.

11. Paint balance weights and perform touch up painting.

12. Following complete paint application and balancing, perform final VTI of all hydrodynamic painted surfaces to ensure they conform to the coatings requirements.

13. The following actions apply to the rotor accessories:

a. The twenty one (21) AM tailcone attachment hole plugs shall be provided unpainted and not installed.

b. The eight (8) FWD hub packaging hole plugs shall be provided blasted and primed in accordance with reference (j). FWD hub packaging hole plugs shall not be installed.

c. The three (3) Hub flange pin hole plugs shall be provided with the heads blasted and primed in accordance with reference (j). Hub flange pin hole plugs shall be provided in a separate shipping container.

d. The four (4) FWD lifting hole plugs shall be provided with the heads blasted and primed in accordance with reference (j). FWD lifting hole plugs shall be installed.

e. Provide a shipping container for rotor accessories in accordance with reference (o).

Shipping direction will be provided via separate correspondence.

14. Prepare the rotor for transit in accordance with references (e) and (m). Note that strippable coating shall not be applied. The AC/AF preservation paint must be cured prior to packaging in accordance with the applicable dry to touch and dry to handle times. The cured paint film shall resist a thumb deformation test (similar to ASTM D1640, paragraph 7.7.1) before packaging can begin.

15. Provide support to load the rotor and strongback assembly onto shipping trailer in accordance with references (m) and (n).

The following GFP shall be used for Item 0001AA:

1. PROPVAL Analysis program for SSN 774 Class Rotor

2. Navy Acoustic Test Tank

3. SSN 774 lifting padeyes

4. Rotor shipping strongback

5. Rotor Flange inspection gage

6. Rotor Hub Drill Jig for AM Tailcone Holes

INSPECTION AND ACCEPTANCE: Inspection and acceptance of Item 0001 shall be in accordance with reference (a) by 30 SEP 2019.

ITEM 0002: Data

Data for pre-repair (ITEM 0001AA) shall consist of the following items in accordance with reference (a) as applicable and as specified herein. (CDRL’s A004, A005, A006, A009 apply.)

1. PROPVAL LEICA Scan Report

2. Pre-repair VTI

3. Pre-repair UT inspection

4. Bushing dimensional inspection

5. Threaded hole dimensional inspection

Data for post repair (ITEM 0004) shall consist of the following items in accordance with reference (a) as applicable and as specified herein. (CDRL’s A004, A006, A007, A008 apply.)

1. Drying procedure certificate of compliance (CFC)

2. Post repair PROPVAL LEICA Scan Report, if required

3. Post repair UT inspection if required

4. Pre-Blast VTI

5. Post Paint VTI - Rotor final condition and condition of accessories (painted and/or installed)

6. Coatings application CFC

7. Accessory cert package including new fill/vent hole plugs

8. Balance inspection forms

9. New bushing report with material certs and dimensions, if required

10. AM Tailcone hole dimensional inspection

NAVSEA inspection form 9245/9 shall be utilized in lieu of NAVSEA form 9245/3. Submit inspection reports to NSWCPD 426 and copy of the report transmittal letter to NAVSUP WSS N97121. Allow 15 days for government review and approval

NSN 2S 2010-01-525-3159

Repair Statement of Work (SOW) SSN 774 Class Rotor

SN 29880

The following references apply:

(p) Technical Data Package & CDRL's A004, A005, A006, A007, A008, A009

(q) NAVSEA S9245-AZ-TSM-010/PROP (C)

(r) NAVSEA 245-7385828 Rev A (C), Rotor Assembly NDP3.1HS & HM

(s) NAVSEA 245-8328548 Rev B (C), Dimensional Inspection Requirements

(t) NAVSEA 245-7384173 Rev A (U), Propulsor Packaging and Preservation including

Configuration Change Request No. 245

(u) NAVSEA 245-8328541 Rev D (U), VA Rotor Field Replaceable Hardware

(v) NAVSEA 245-7651134 Rev A (U), NDP3.1H Rotor Hub Drill Jig for AM Tailcone

Holes

(w) NAVSEA 245-8328557 Rev B, SSN 774 Propulsor AM Tailcone

(x) NAVSEA 245-8357290 Rev A, VA Class Propulsor Threaded Inserts

(y) NAVSEA S9245-A4-TSM-010, Propulsor Paint Preservation

(z) NAVSEA 245-7642137 Rev E (C), Rotor Assembly NDP3.1HC

(aa) NAVSEA 245-8216580 Rev A, Virginia Class Propulsor Axis Vertical Lifting Details and Transporter Attachment Procedure

(bb) NAVSEA 245-7642140 Rev A, SSN774 Class Rotor Strongback Packaging

Details

(cc) NAVSEA 245-7642139 Rev A, SSN774 Rotor Strongback Trailer Loading

(dd) MIL-DTL-2845, Propulsion Systems, Boat And Ship; Main Shafting, Propellers, Bearings, Gauges, Special Tools, and Associated Repair Parts; Preservation, Packaging, Packing and Storage of

The following notes and miscellaneous requirements apply.

7. All inspections and repairs shall be performed in accordance with references (a) through (o), as applicable, except as noted herein. In the event of a conflict between the references cited and this statement of work, the statement of work shall take precedence.

8. The facility must have personnel that have CONFIDENTIAL clearance and have successfully completed the NAVSEA Ducted Propulsor Visual Inspection Course.

9. CONFIDENTIAL inspection forms shall be submitted as a separate inspection report.

10. The vendor shall meet all applicable coatings qualification requirements of reference (j), including Society for Protective Coatings SSPC-QP3 qualification or NAVSEA approved equivalent. If the vendor is not qualified to SSPC-QP3 or by NAVSEA, they have the option to identify a qualified subcontractor to perform blasting and painting operations.

All personnel performing abrasive blasting shall have CONFIDENTIAL clearance and shall be certified in accordance with SSPC C-7, Abrasive Blasting. All personnel performing coatings application shall have CONFIDENTIAL clearance and shall be certified in accordance with Spray Application Certification or SSPC C-14, Marine Plural Component Program.

11. Stacking of VA class rotors is not authorized.

12. The rotor does not have side lifting points and a turnover fixture or J-bar is required for flipping. The means for flipping is the responsibility of the vendor and there is no GFE turning fixture designated for refurbishment work. The required sling length is a minimum of 15 feet for a straight lift, but a spreader bar is an acceptable alternative to maintain minimum 81 degree sling angle in accordance with Sheet 004-12 of reference (l).

ITEM 0001AB

10. Provide support to unload the rotor and strongback assembly from shipping trailer in accordance with references (m) and (n).

11. Remove paint layers, anti-fouling (AF) and anticorrosion (AC) from all painted surfaces by abrasive blasting or hand sanding. Blast media shall be in accordance with reference (j).

12. Conduct moisture removal procedure. Note that the Vendor shall provide and install new fill and vent hole plugs, sixteen (16) per blade following the moisture removal process. The following requirements apply:

a. Rotor must be positioned pressure face down.

b. All fill/vent plugs shall be removed from each rotor blade.

c. Heat must be applied to the entire blade. The temperature must be held in the temperature range of 200°F to 225°F. Heat can be applied through the use of a forced air heater and a custom heater bag designed to be slipped on over the blade to contain the heat.

d. Heat must be monitored by thermocouples mounted on the blades.

e. A vacuum must be applied to the entire blade during the heating process.

f. A sight glass shall be installed in-line with the vacuum pump to monitor presence of water.

g. A minimum pressure of 26” Hg should be held by the vacuum pump(s) throughout the entire evolution, approximately 10 days.

h. After the 10 day period, remove equipment and install new fill and vent hole plugs.

There are sixteen (16) 1/2” or 9/16” dia fill and vent plugs per blade.

13. Perform a pre-repair liquid penetrant (PT) aided visual technical inspection (VTI) on all surfaces in accordance with reference (a) and (b).

14. Perform a UT inspection of the blade 3C welds in accordance with references (a) and (b).

15. Remove previously installed bushings using hydraulic jacks.

16. Perform pre-repair dimensional inspection of every blade and hub outer surface using laser scanning inspection process to generate a dense point cloud of inspection data. Probe measurement uncertainty (error) shall be taken into account in accordance with ISO Standard 14253-1 when evaluating surface best fits. Currently, only Laser tracker and LEICA T-Scan

b. One hundred (100) points/sq-in for the tip and trailing edge region (extending 5" from

Apply spray developer to all surfaces prior to scanning inspection surface. The pre-repair data shall be provided to Propulsor Technology, Inc. (PTI) at the address provided below for Navy repair evaluation (vendor is not responsible for the pre-repair evaluation of the collected data). The Navy evaluation will be provided to the vendor within 21 days of receipt of data. A copy of the Navy evaluation shall be included as part of the vendor’s dimensional report.

Propulsor Technology Inc.

80 Emerson Lane Suite 1302 Bridgeville, PA 15017-3472 Attn: Jim Machin, 412-914-1100

17. Perform System 21 Class 2 thread inspection on forward and aft hub face threaded holes used for lifting, handling and tailcone attachment. If the threaded holes fail the System 21 thread inspection, perform System 22 inspection.

18. Perform flange gage inspection in accordance with NAVSEA 245-8328556.

ITEM 0001AB: Materials, Accessories, Balance Weights and Bushing Material

7. Procure one rotor set of the Item 3 bushings (12 each), hub flange sleeve, in accordance with reference (f). Procure additional material to accomplish certification testing and retain a permanent heat sample record. Remove previously installed bushings and replace with Item 3 procured above.

8. Procure one rotor set of AM tailcone attachment hole plugs, Item 8328541-11, QTY (21).

9. Replace the following FWD face accessories as required:

a. FWD hub packaging hole plug, Item 8328541-9, QTY (8)

b. FWD lifting hole plug, Item 8328541-7, QTY (4)

c. Hub flange pin hole plug, Item 8328541-5, QTY (3)

10. Procure replacement security covers in accordance with reference (e).

11. Machined balance correction weights in accordance with reference (c).

12. Procure wood blocking and friction matting for shipment as required

ITEM 0001AB: Repair and Inspection of Propulsor Rotor

16. Repair surface and edge defects as identified during pre-repair inspection and approved by

NSWCPD 426 by blending and welding as necessary. Hydro surface fairing rod inspection shall be accomplished on all repaired areas. Gages may be used as a guide.

17. Repair blade 3C weld defects by excavating and welding in accordance with references (a) and (b). Perform and document liquid penetrant (PT) aided visual inspection at the excavated areas prior to welding. Final NDE inspection shall consist of UT inspection and PT aided visual inspection in accordance with references (a) and (b). Repaired areas shall be inspected and evaluated using tactile inspection. In addition, hydro surface fairing rod inspection shall be accomplished on all repaired areas.

18. Repair threaded holes as required based on results from pre-repair inspection. Threaded holes shall be repaired and inspected in accordance with reference (b). Tailcone attachment holes shall not be welded and shall be repaired in accordance with reference (i).

19. Drill and tap AM Tailcone attachment holes in accordance with references (g) and (k). Drill fixture will be provided as GFP.

20. Restamp hub OD data as required in accordance with reference (c) and add the following, REP & BAL, (VENDOR) DATE (MM/YY).

21. Perform visual inspection of the rotor external surfaces prior to blast and paint application in accordance with references (a) and (b), as applicable. Additional UT and PT inspections are not required once performed at individual repaired areas. Provide advanced copy of VTI to NSWCPD 426 for acceptance prior to blast and paint application.

22. Perform dimensional inspection of every blade and hub outer surface using laser scanning inspection process to generate a dense point cloud of inspection data. Probe measurement uncertainty (error) shall be taken into account in accordance with ISO Standard 14253-1 when evaluating surface best fits. Currently, only Laser tracker and LEICA T-Scan

b. One hundred (100) points/sq-in for the tip and trailing edge region (extending 5" from

Apply spray developer to all surfaces prior to scanning inspection surface. The data shall be provided to PTI for information in the event that Navy technical support is required.

Provide an advance copy of the evaluation to NSWCPD Code 426 following post repair inspection. Need for additional fairing will be determined by NSWCPD Code 426 from the analysis of results.

23. Paint system(s) shall be applied in accordance with reference (j), Appendix C. A minimum of 4 dry film thickness (DFT) measurements shall be taken on each blade face. DFT measurements shall be taken at 3 locations on the hub outside diameter and 3 locations on the hub inside diameter. As required, Phillybond TA-30 shall be applied to seams and porosity after the first coat of paint has cured. The TA-30 shall be faired in to match surrounding surface and reapplied, if required, to ensure fairness. These repairs shall be roughened with 120 grit emery paper before application of the second coat of paint. All coatings inspections shall be performed by a Level 3 NACE Certified Coatings Inspector in accordance with reference (j). Upon completion, the NACE certified inspector shall provide written verification of successful coatings application to the vendor and NSWCPD Code 426.

24. Perform rotor balance following paint application. Note VA Class rotors do not have a tapered bore. Balancing operations require a vendor furnished balance adapter plate. The design of the adapter plate must be approved by NSWCPD Code 426. Note that the hub flange alignment pin hole plugs shall be installed during balancing operations. Remove the hub flange alignment pin hole plugs when balance is complete. A total of three balance runs shall be performed at the Top Dead Center (TDC) position as follows:

a. Perform one initial balance run.

b. Perform one balance run following balance weight installation.

c. Remove the rotor from balance machine. Re-install rotor on the balance machine and perform an additional balance run.

The first two balance runs shall be submitted as the initial and final data. The third balance run shall be provided for information only.

25. Provide support for acoustic tank testing per Advanced Engineering Consultants (AEC)

Drawing ME-1, NAVSEA TEST TANK. Acoustic test tank is provided as GFP. Support includes but is not limited to the following:

g. Assembly of Navy test tank, liner, plumbing connections. The test tank is 24 feet in diameter and 7 feet tall. A CONFIDENTIAL space of 30 feet in diameter is recommended to accommodate equipment and tank access. The vendor shall provide a stairway to gain access to the tank.

h. Purchase and/or rental of water pump, filter, and heating and cooling equipment.

i. Fill tank (approx. 15,000-20,000 gallons).

j. Install AM tailcone hole plugs prior to the acoustic test process.

k. Provide miscellaneous (i.e. crane) support to Navy Acoustic Test Personnel during testing.

l. Drain and disassemble tank.

26. Paint balance weights and perform touch up painting.

27. Following complete paint application and balancing, perform final VTI of all hydrodynamic painted surfaces to ensure they conform to the coatings requirements.

28. The following actions apply to the rotor accessories:

a. The twenty one (21) AM tailcone attachment hole plugs shall be provided unpainted and not installed.

b. The eight (8) FWD hub packaging hole plugs shall be provided blasted and primed in accordance with reference (j). FWD hub packaging hole plugs shall not be installed.

c. The three (3) Hub flange pin hole plugs shall be provided with the heads blasted and primed in accordance with reference (j). Hub flange pin hole plugs shall be provided in a separate shipping container.

d. The four (4) FWD lifting hole plugs shall be provided with the heads blasted and primed in accordance with reference (j). FWD lifting hole plugs shall be installed.

e. Provide a shipping container for rotor accessories in accordance with reference (o).

Shipping direction will be provided via separate correspondence.

29. Prepare the rotor for transit in accordance with references (e) and (m). Note that strippable coating shall not be applied. The AC/AF preservation paint must be cured prior to packaging in accordance with the applicable dry to touch and dry to handle times. The cured paint film shall resist a thumb deformation test (similar to ASTM D1640, paragraph 7.7.1) before packaging can begin.

30. Provide support to load the rotor and strongback assembly onto shipping trailer in accordance with references (m) and (n).

The following GFP shall be used for Item 0001AB:

7. PROPVAL Analysis program for SSN 774 Class Rotor

8. Navy Acoustic Test Tank

9. SSN 774 lifting padeyes

10. Rotor shipping strongback

11. Rotor Flange inspection gage

12. Rotor Hub Drill Jig for AM Tailcone Holes

ITEM 0002: Data

Data for pre-repair (ITEM 0001AB) shall consist of the following items in accordance with reference (a) as applicable and as specified herein. (CDRL’s A004, A005, A006, A009 apply.)

6. PROPVAL LEICA Scan Report

7. Pre-repair VTI

8. Pre-repair UT inspection

9. Bushing dimensional inspection

10. Threaded hole dimensional inspection

Data for post repair (ITEM 0001AB) shall consist of the following items in accordance with reference (a) as applicable and as specified herein. (CDRL’s A004, A006, A007, A008 apply.)

11. Drying procedure certificate of compliance (CFC)

12. Post repair PROPVAL LEICA Scan Report, if required

13. Post repair UT inspection if required

14. Pre-Blast VTI

15. Post Paint VTI - Rotor final condition and condition of accessories (painted and/or installed)

16. Coatings application CFC

17. Accessory cert package including new fill/vent hole plugs

18. Balance inspection forms

19. New bushing report with material certs and dimensions, if required

20. AM Tailcone hole dimensional inspection

NAVSEA inspection form 9245/9 shall be utilized in lieu of NAVSEA form 9245/3. Submit inspection reports to NSWCPD 426 and copy of the report transmittal letter to NAVSUP WSS N97121. Allow 15 days for government review and approval

WSSTERMCZ04 GOVERNMENT-INDUSTRY DATA EXCHANGE PROGRAM (GIDEP)

a. The Contractor will actively participate in the Government Industry Data Exchange Program per the GIDEP Operations Manual. The Contractor will submit information concerning critical or major nonconformances, as defined in FAR 46.101 to the GIDEP information system.

b. The Contractor will insert paragraph (a) in any subcontract when deemed necessary by the Contractor. When so inserted, the word "contractor" will be changed to "subcontractor."

c. The Contractor will, when it elects not to insert paragraph (a) in a subcontract, provide the subcontractor any GIDEP data which may be pertinent to items of its manufacture and verify that the subcontractor utilizes any such data.

d. The Contractor will, whether it elects to insert paragraph (a) in a subcontract or not, verify that the subcontractor utilizes and provides feedback on any GIDEP data that may be pertinent to items of its manufacture.

(06-17)

CLAUSES INCORPORATED BY REFERENCE

SUPTXT204-

9400(1-17)

Contractor Unclassified Access to Federally Controlled Facilities, Sensitive Information, Information Technology (IT) Systems or Protected Health Information

APR 2017

Section D - Packaging and Marking

SECTION D

SECTION D - NAVSUPWSSDA07 PRESERVATION, PACKAGING, PACKING AND MARKING (Nov 2015)

The contractor shall preserve, package, pack and mark all items as cited below.

1. PRESERVATION REQUIREMENTS

a. SYSTEM STOCK SHIPMENTS - The contractor shall preserve all items intended to enter the military distribution system (stock) in accordance with the MIL-STD-2073-1E, “Standard Practice for Military Packaging”, Packaging Requirements Code specified in the Schedule. When a Specialized Preservation Code/Method of Preservation (MOP) (Table J-Ia) is specified, and one or more of the following packaging fields (WM, CUD, CT, UC) value is a 00 (numeric), the Specialized Preservation/MOP procedure and materials takes precedence. Disregard “HM” and “LP” fields and replace “SPMK 99” with “00” (numeric). Contractor can access https://tarp.navsisa.navy.mil/ for code interpretation.

1) Contractor shall use material produced by a Qualified Products List (QPL) manufacturer if the required packaging material has a QPL. Barrier materials that have QPLs are MIL-PRF-131, Classes 1 and 3, MIL- PRF-81705D, Type 1 and MIL- PRF-22191. These items can be identified by the following packaging field values: PM = “31”, “32”, “33”, “41”, “42”, “43”, “44”, “45”, “51”, “52”, “53”, “54”, “55”, “AW”, “BD”, “DW”, “GX”; or UC = “B2”, “B3”, “B9”, “BL”, “BS” or “SD”. Sources for QPL material can be obtained by contacting 215-697-5842.

MMN

b. IMMEDIATE USE/INSTALLATION AND PART NUMBER BUY SHIPMENTS – Government PCO or ACO approval to use the packaging standards outlined in this paragraph is required, and is only permitted for all items determined to be for immediate use (e.g. CASREP, AOG, or Repair line stoppage) and part number buy shipments. Any national stock numbered (NSN) item required for immediate use or direct installation, or part number item (authority granted to ship without NSN) shall be preserved and packed in accordance with ASTM D 3951-10, “Standard Practice for Commercial Packaging”, for all shipments to a Continental United States (CONUS) government activity or contractor-owned facility. Marking shall be in accordance with MIL-STD- 129R, “Military Marking for Shipment and Storage”. All buys destined for overseas shipment (OCONUS) shall be preserved in accordance with MIL-STD-2073-1E.

c. GOVERNMENT-OWNED MATERIAL – In the event that the Performance Based Logistics (PBL) contract expires and there is no follow-on PBL contract, or the contract is terminated or completed and Government-owned material is to be returned to the supply system, the contractor shall preserve and package this material in accordance with the requirements of paragraph 1 a.

2. PACKING REQUIREMENTS – The contractor shall pack as follows. Exterior shipping containers for Packing Levels A and B are detailed in MIL-STD-2073-1E, Appendix C, Table C.II. Reusable containers, fast pack containers or wood containers are shipping containers and do not require overpacking for shipment.

Domestic Shipments (CONUS): Level B

Overseas Shipments (OCONUS) (including Navy ships at sea):

Via air, FPO, APO Level B

Via freight forwarder Level B

Via surface Level A

3. MARKING REQUIREMENTS - All unit, intermediate and shipping containers shall be marked in accordance with MIL-STD- 129R. In addition, the following specific requirements apply:

a. ADDITIONAL MARKING FOR SPARES ONLY – Each MIL-STD-129R label shall also include the following:

1) Supplementary Procurement Instrument Identification Number (SPIIN) – the 4-digit order number that follows the basic BOA or long-term contract number (e.g. 0001, A001, 5001, 7001, etc.),

2) Contract Line Item Number (CLIN) – the 4-digit individual line item number (e.g. 0001, 0002, etc.), and

3) SubCLIN – the 6-digit sub line item number (e.g. 0001AA, 0001AB, 0002AA, 0002AB, etc.).

b. 2D BAR CODE MILITARY SHIPPING LABEL (MSL) – 2D bar code requirements in accordance with

MIL-STD-129R,

Paragraph 5.2.2.6

c. RADIO FREQUENCY IDENTIFICATION (RFID) LABEL – RFID requirements in accordance with clause DFARS 252.211- 7006 “Passive Radio Frequency Identification.”

d. DEPOT LEVEL REPAIRABLE (DLR) LABELS

1) Items identified with a Cognizance Code of either “7” or an even number preceding the NSN (e.g. 7RH 5826- 01-428-9999) are defined as Depot Level Repairable (DLR) items. DLR items require that a DLR label be placed on the outside of the unit, the intermediate and the shipping container for accountability and control purposes. The outside of each unit, intermediate and shipping container shall be affixed with the applicable label as close to the bar code label as possible.

EXCEPTION: When a DLR item requires use of both a reusable inner unit container and a reusable outer shipping and storage container (excluding wood and fiberboard), only the inner unit container shall be affixed with a DLR label. In these cases only, DLR labels shall NOT be placed on the outer reusable container.

2) Labels are available via the Naval Forms Online website: http://navalforms.daps.dla.mil. The website will advise the procedures for ordering and establishing an account. When searching for the DLR label, the following procedure should be followed:

a) Click on “Forms” tab

b) Click on “Keyword Search”

c) Under "Search Criteria" type in “DLR”

d) Under “Type” click on picture of box (Warehouse Form Link)

e) Follow the applicable instructions (New Account, Current

Account or Continue Shopping)

NSN DESCRIPTION QUANTIT

Y PER

UNIT

APPLICATION FORM NUMBER

0108LF5055300 DLR Label 2 in. x 3 in.

100 Unit Container

NAVSUP 1397-1

0108LF5055000 DLR Label 3 in. x 5 in.

100 Intermediate / Shipping Container

NAVSUP 1397

Labels may also be obtained by faxing a copy of the contract page containing the DLR label requirement to 215- 697-2424.

e. SPECIAL MATERIAL IDENTIFICATION CODE (SMIC) FOR NAVSUP WSS

MECHANICSBURG MARITIME REQUIREMENTS ONLY

1) Certain Program-related items are identified by a two-position SMIC, which appears as a suffix to the NSN (e.g. 1H4730-00-900-1317 L1), and require special markings. Containers shall be marked with letters, maximum two inches high on two (2) sides and two (2) ends as follows:

SMIC MARKINGS COLOR TYPE CONTAINER

L1 LEVEL 1 RED Unit, intermediate and shipping

(size permitting)

S1 SURFAC

E LEVEL

RED Unit, intermediate and shipping

(size permitting) D4/D5/D7 DSS-SOC RED Unit, intermediate and shipping

(size permitting)

C1 * LEVEL 1

SPECIAL CLEAN

GREEN Unit, intermediate and shipping

CP/VG * SPECIAL

CLEAN O2-N2

GREEN Unit, intermediate and shipping

D0/D6/D8 * DSS-SOC SPECIAL

CLEAN O2-N2

GREEN Unit, intermediate and shipping

VU FBW SFCC VU BLUE Unit, intermediate and shipping (size permitting)

SW FBW SFCC SW BLUE Unit, intermediate and shipping (size permitting)

Q3/Q5 Q3 or Q5 RED Unit, intermediate and shipping

* denotes Oxygen Clean requirements in accordance with MIL-STD-1330 “Precision Cleaning and Testing of Shipboard Oxygen, Helium, Helium-Oxygen, Nitrogen, and Hydrogen Systems.”

4. PALLETIZATION. Palletization of shipments shall be accomplished in accordance with MIL-STD- 147E “DoD Standard Practice: Palletized Unit Loads.”

5. WOOD PACKAGING MATERIAL (WPM)

In accordance with the latest version of DoD Manual 4140.65-M "Compliance for Defense Packaging:

Phytosanitary Requirements for Wood Packaging Material (WPM)," assets packed in or on wood pallets, skids, load boards, pallet collars, wood boxes, reels, dunnage, crates, frames, and cleats must comply with the Heat Treatment (HT) or Heat Treatment/Kiln Dried (HT/KD) (continuous at 56 degrees Centigrade for 30 minutes) standard. The WPM must be stamped or branded with the appropriate certification markings as detailed in DoD 4140.65-M and be certified by an accredited American Lumber Standards Committee (ALSC)-recognized agency. The WPM certification markings must be easily visible, especially in pallet loads, to inspectors.

6. NAVY SHELF LIFE PROGRAM

Navy shelf-life requirements are listed under the item description in a 3-digit alpha/numeric code. Position one

(1) is the DOD shelf-life code, defining the type of shelf-life for an item (Type I, non-extendible or Type II, extendible), and the number of months an item can remain ready for issue in a Navy specified package.

Positions two (2) and three (3) combined form the Navy-unique shelf-life action codes used by storage activities, and do not impose any requirements on the contractor. The contractor shall use the applicable shelf-life paragraphs and table in MIL-STD-129R to apply either Type I or Type II shelf-life markings for an item's unit, intermediate and shipping containers. Contractors will ensure that at least eighty-five percent (85%) of the Navy shelf-life requirement is remaining when received by the first government activity.

7. REUSABLE NSN CONTAINERS

An item that has an NSN assigned in the “Container NSN” field (e.g . 8145012622982) requires shipment in a metal or plastic reusable shipping and storage container.

a. REUSABLE CONTAINERS FOR NAVSUP WEAPON SYSTEMS SUPPORT, MECHANICSBURG SITE, MARITIME REQUIREMENTS

Reusable NSN containers for maritime material (designated by a Cognizance Code of “7E”, “7G” and “7H”) shall be provided as contractor-furnished material (CFM). Source lists of possible container manufacturers may be obtained by contacting 215-697-5842.

b. REUSABLE CONTAINERS FOR NAVSUP WEAPON SYSTEMS SUPPORT, PHILADELPHIA SITE, AVIATION REQUIREMENTS

Reusable NSN containers (excluding wood and fiberboard) for aviation material (designated by a Cognizance

Code of “7R”,“6K” or “0R”) shall be provided as government-furnished material (GFM). Fast pack containers illl not be provided as GFM. To obtain GFM reusable containers, the contractor must first obtain a Container Request Form either from https://tarp.navsisa.navy.mil/containerrequest or by contacting 215-697-5842, then fax the completed form to 215-697- 1405/3850 at least 90 days prior to the anticipated shipping date (monthly for repair contracts). If the Navy’s Container Management Area (CMA) informs the contractor that containers are unavailable, the following alternate packaging requirements apply. The unavailability of reusable containers shall not be an excusable delivery delay. Unit packs shall be designed to conserve weight and cube while retaining the protection required and enhancing standardization.

ALTERNATE PACKAGING

REQUIREMENTS FOR ITEMS

ASSIGNED THE FOLLOWING

CONTAINERS

Container

NIIN

Container Part Number(80132)

Alternate Packaging Code

IAW MIL-STD-2073-1E

00-260-9548 P069-2

GX10000LTBE

C (QUP = 001)

(ICQ = 000)

00-260-9556 P069-1 00-260-9559 P069-3 00-260-9562 P069-4 01-012-4088 P069-6 01-014-0440 P069-5 01-164-4073 P069-7 01-262-2982 15450-100

DW100K3GHFE

D (QUP = 001)

(ICQ = 000)

01-262-2983 15450-200 01-262-2984 15450-300 01-262-2985 15450-400 01-262-2986 15450-500 01-262-2987 15450-600

01-262-2988 15450-700 DW100K3GHFD

R (QUP = 001)

(ICQ = 000)

All excess empty reusable shipping and storage containers shall be turned-in to the nearest Container Reuse and Refurbishment Center (CRRC). CRRC locations/points of contact can be found at https://tarp.navsisa.navy.mil/crrc or by contacting 215-697-2063.

8. REUSABLE NSN CONTAINERS FOR FOREIGN MILITARY SALES (FMS), JPO OR OTHER FOREIGN

FORCES ACQUISITION

a. Reusable shipping and storage containers shall be provided as CONTRACTOR-FURNISHED

MATERIAL (CFM), unless otherwise specified.

b. Contractors may tender offers including alternate, non-reusable, packaging methods and be considered responsive.

9. MATERIAL SAFETY DATA SHEETS

As required by clauses FAR 52.223-3 “Hazardous Material Identification and Material Safety Data” and DFARS 252.223-7001 “Hazard Warning Labels” the offeror is required to list any…