Amendment N0018920RZ0270001.pdf

AMENDMENT OF SOLICITATION/MODIFICATION OF CONTRACT

Except as provided herein, all terms and conditions of the document referenced in Item 9A or 10A, as heretofore changed, remains unchanged and in full force and effect.

15A. NAME AND TITLE OF SIGNER (Type or print)

30-105-04EXCEPTION TO SF 30

APPROVED BY OIRM 11-84

STANDARD FORM 30 (Rev. 10-83)

Prescribed by GSA

FAR (48 CFR) 53.243

The purpose of this amendment is to address the questions pertaining to this solicitation. This amendment provides direct rsponses to all questions and updates the applicable sections of the solicitation. The closing date remains unchanged on 03 April 2020 at 4:00PM ET.

1. CONTRACT ID CODE PAGE OF PAGES

J 1 8

16A. NAME AND TITLE OF CONTRACTING OFFICER (Type or print)

16C. DATE SIGNED

BY 25-Feb-2020

16B. UNITED STATES OF AMERICA15C. DATE SIGNED15B. CONTRACTOR/OFFEROR

(Signature of Contracting Officer)(Signature of person authorized to sign)

8. NAME AND ADDRESS OF CONTRACTOR (No., Street, County, State and Zip Code) X N0018920RZ027

X 9B. DATED (SEE ITEM 11)

21-Feb-2020

10B. DATED (SEE ITEM 13)

9A. AMENDMENT OF SOLICITATION NO.

11. THIS ITEM ONLY APPLIES TO AMENDMENTS OF SOLICITATIONS

X The above numbered solicitation is amended as set forth in Item 14. The hour and date specified for receipt of Offer is extended, X is not extended.

Offer must acknowledge receipt of this amendment prior to the hour and date specified in the solicitation or as amended by one of the following methods:

(a) By completing Items 8 and 15, and returning 1 copies of the amendment; (b) By acknowledging receipt of this amendment on each copy of the offer submitted;

or (c) By separate letter or telegram which includes a reference to the solicitation and amendment numbers. FAILURE OF YOUR ACKNOWLEDGMENT TO BE

RECEIVED AT THE PLACE DESIGNATED FOR THE RECEIPT OF OFFERS PRIOR TO THE HOUR AND DATE SPECIFIED MAY RESULT IN

REJECTION OF YOUR OFFER. If by virtue of this amendment you desire to change an offer already submitted, such change may be made by telegram or letter, provided each telegram or letter makes reference to the solicitation and this amendment, and is received prior to the opening hour and date specified.

12. ACCOUNTING AND APPROPRIATION DATA (If required)

13. THIS ITEM APPLIES ONLY TO MODIFICATIONS OF CONTRACTS/ORDERS.

IT MODIFIES THE CONTRACT/ORDER NO. AS DESCRIBED IN ITEM 14.

A. THIS CHANGE ORDER IS ISSUED PURSUANT TO: (Specify authority) THE CHANGES SET FORTH IN ITEM 14 ARE MADE IN THE

CONTRACT ORDER NO. IN ITEM 10A.

B. THE ABOVE NUMBERED CONTRACT/ORDER IS MODIFIED TO REFLECT THE ADMINISTRATIVE CHANGES (such as changes in paying office, appropriation date, etc.) SET FORTH IN ITEM 14, PURSUANT TO THE AUTHORITY OF FAR 43.103(B).

C. THIS SUPPLEMENTAL AGREEMENT IS ENTERED INTO PURSUANT TO AUTHORITY OF:

D. OTHER (Specify type of modification and authority)

E. IMPORTANT: Contractor is not, is required to sign this document and return copies to the issuing office.

14. DESCRIPTION OF AMENDMENT/MODIFICATION (Organized by UCF section headings, including solicitation/contract subject matter where feasible.)

10A. MOD. OF CONTRACT/ORDER NO.

2. AMENDMENT/MODIFICATION NO. 5. PROJECT NO.(If applicable)

6. ISSUED BY

3. EFFECTIVE DATE

25-Feb-2020

CODE

NAVSUP FLC NORFOLK PHILADELPHIA OFFICE

ATTN: JACOB SEGAL 700 ROBBINS AVENUE, BLDG. 2

PHILADELPHIA PA 19111-5083

N00189 7. ADMINISTERED BY (If other than item 6)

4. REQUISITION/PURCHASE REQ. NO.

CODE

See Item 6

FACILITY CODECODE

EMAIL:TEL:

N0018920RZ027

SECTION SF 30 BLOCK 14 CONTINUATION PAGE

SUMMARY OF CHANGES

SECTION SF 30 - BLOCK 14 CONTINUATION PAGE

The following have been added by full text:

SOLICITATION QUESTIONS

Question 1:

The final RFP states both identical and replicate in the statement of work. Within the Statement of Work the below referenced sections identify the areas we are looking for clarity;

3.0 … complete Combi configuration cargo compartment and main cargo door that replicates the USN C-40A

(Boeing 737-700C) aircraft...

5.1.1 The contractor shall provide and install a C-40A LMT Device, to include the following (at a minimum): the portion of the fuselage from the aft most wing section to the forward galley (including forward entry door), complete

Combi configuration cargo compartment and main cargo door replicating the USN C-40A (Boeing 737-700C) aircraft to include…

5.2 The C-40A LMT shall have a fully-operational main cargo door of identical specifications to the USN C-

40A (Boeing 737-700C) aircraft. …..The main cargo door shall replicate main cargo door operation of the C-

40A including…

Response:

Language was changed in the Statement of Work, please see updated SOW below for clarity.

Question 2:

Section L references a Past Performance Information Form attachment. Please provide this attachment.

Response:

See attached Past Performance Information Form attached to this amendment.

SECTION A - SOLICITATION/CONTRACT FORM

The required response date/time 03-Apr-2020 04:00 PM has been added.

The depository location Philadelphia, PA has been added.

The number of offeror copies required 3 has been added.

SECTION C - DESCRIPTIONS AND SPECIFICATIONS

The following have been modified:

STATEMENT OF WORK

Statement of Work (SOW) for

Procurement of a C-40A Loadmaster Trainer (LMT)

1.0 INTRODUCTION: Commander, Naval Air Force Reserve (CNAFR) has a requirement to procure a C-40A LMT to be located at Air Logistics Training Center (ALTC), Fort Worth, TX in support of Commander, Fleet Logistics Support Wing (CFLSW). This action is for the acquisition of a C-40A LMT which should be secured in place by the contractor at the ALTC in Fort Worth, TX.

The contractor is responsible for the acquisition, manufacturing, delivery of equipment needed to secure the C-40A LMT device in-place.

2.0 BACKGROUND: This device is required to replace the C-9B LMT with a fleet-representative C-40A LMT to effectively train and equip C-40A Loadmasters. The Navy Reserve divested the last C-9B aircraft from its inventory on 30 June 2014 and the Marine Corps Reserve divested the last two C-9Bs on 1 June 2017, thus rendering the C-9B LMT obsolete. The training of

Navy Reserve Loadmasters is essential to ensure safe and efficient cargo loading operations in support of global Navy fleet logistics missions. C-40A Loadmasters are responsible for safe on- and off-loading of all palletized cargo on the C-40A aircraft as well as direction of loading vehicles (e.g.

K-Loaders and forklifts) in close proximity to the aircraft fuselage. The addition of a properly configured C-40A LMT device will allow C-40A Loadmasters to practice cargo loading evolutions

(in a controlled training environment) on a fleet-representative C-40A LMT prior to executing actual missions.

3.0 SCOPE: The scope of this CNAFR effort is to provide and install, a C-40A LMT device, to include the following (at a minimum): the portion of the fuselage from the aft most wing section to the forward galley (including forward entry door), complete Combi configuration cargo compartment and main cargo door that replicates the USN C-40A (Boeing 737-700C) aircraft, to include overhead storage bins, and port wing section to include port engine nacelle. The existing facility will accommodate a C-40A LMT device with dimensions of approximately 60 feet in length by 47 feet in width by 29 feet in height. Contractors should plan to participate in a site visit in order to take exact measurements of a C-40A aircraft and survey the facility in which it will be installed at ALTC. The exact date, time and place of the site visit will be discuss in Section 6.0 below.

3.1 NAICS Code SIC Code Federal Product/Service Code Object Class Code

333318 3728 6930 26.0

4.0 APPLICABLE DIRECTIVES: The directives listed below are applied and reviewed as part of the support for this requirement.

Document Type Number/Version Title Date

NATOPS NAVAIR A1-

C40AAA-

NFM000

C-40A NATOPS

CFLSWINST 3500.7 series Enlisted Aircrew Phase Training and

Qualification

03 Mar 15

DOD MANUAL DOD 4160.21M Defense Material Disposal Manual Aug 1997

4.1 ACRONYMS AND ABBREVIATIONS:

ALTC Air Logistics Training Center

CFLSW Commander, Fleet Logistics Support Wing

CNAFR Commander, Naval Air Force Reserve

CNRF Commander, Navy Reserve Force

IT Information Technology

JRB Joint Reserve Base

JPAS Joint Personnel Adjudication System

LM Loadmaster

LMT Loadmaster Trainer

TBD To Be Determined

TRS Technical Requirements Statement

5.0 PERFORMANCE REQUIREMENTS/TASKINGS: This SOW shall be used to acquire a

C-40A LMT device and to identify any additional equipment, facility or parking apron modifications required for installation of the C-40A LMT. The C-40A LMT shall replicate the confined space of the C-40A in a Combi configuration, providing the capability to instruct Navy C-40A Loadmasters on proper load planning, cargo loading, and cargo pallet securing techniques.

5.1 The C-40A LMT: The C-40A LMT shall include the following:

5.1.1 The contractor shall provide and install a C-40A LMT Device, to include the following (at a minimum): the portion of the fuselage from the aft most wing section to the forward galley (including forward entry door), complete Combi configuration cargo compartment and main cargo door replicating the USN C-40A (Boeing 737-700C) aircraft to include overhead storage bins, and port wing section to include port engine nacelle. The device shall include the forward passenger entry door, a secondary exit, and a fully-operational cargo door that replicates the main cargo door operation of the C-40A including operating positions (CLOSED, CANOPY, FULL OPEN). Design shall include the following C-40A features: forward and aft cargo bulkheads with doors; flooring/ball-decking; all latches, restraints and other fixed equipment used for attaching and restraining cargo/pallets; cargo safety net/rigging; and all panels/switches/placards/lights/indicators required for main cargo door operation as found in the

C-40A aircraft.

5.1.1.1 The C-40A LMT shall replicate the interior dimensions of the C-40A Combi configuration cargo compartment, including operable stowage bins.

5.1.1.2 Interior Layout:

5.1.1.3 The contractor shall mount the C-40A LMT on a steel base frame structure (which the contractor would provide) or landing gear that will support the fuselage section at actual aircraft height during loading and unloading cargo evolutions.

5.1.1.4 The C-40A LMT shall include lighting which enables safe loading and unloading evolutions. Lighting is not necessarily required to match aircraft configuration, but must provide sufficient lighting to carry out training. Control of these lights will be via non-aircraft control switches located near the exit(s).

5.1.1.5 The C-40A LMT shall include interior and exterior fuselage station markings of (at a minimum) medium level of fidelity in size and color.

5.1.1.6 The C-40A LMT shall have forward and in-cabin smoke/fire barriers that replicate the C-40A in Combi configuration. A representative light-weight durable barrier and simplified mounting system is acceptable.

5.1.1.7 The C-40A LMT shall have the forward passenger entry door and service door of similar design to C-40A (Boeing 737-700C) aircraft. Identical C-40A airstairs are not required; however, some form of stair system shall be incorporated to allow entrance to the device without impeding cargo evolutions. The stairs shall fall within the dimensions called out in Section 3.0. Some form of safety barrier/netting/restraint at the forward passenger entry door opening is required and shall be of design to not interfere with cargo loading/unloading evolutions.

5.1.1.8 The C-40A LMT shall have a primary and secondary means of entering/exiting the training device. At a minimum, there shall be a means of entering/exiting forward of the

Combi cargo section and another aft of the Combi cargo section. This can either be via forward passenger and service entry doors with fixed or operable airstairs, or some other system (i.e. overwing or aft entry/service door, either option should include stairs), but stairs shall be of design to not impede cargo loading/unloading evolutions. With exception of the main cargo door, any door openings which include retractable/removable stairs shall have some form of restraint system incorporated for personnel fall prevention. All stairs shall have safety handrails.

5.1.1.9 The LMT units shall be compatible with a 240V/200Amp/60Hz power supply. The lighting, cargo door controls and operation, stairs and any other electronics or electronically controlled components of the LMT shall be compatible with the current power supply

(240V/200Amp/60Hz) available in the ALTC hanger.

5.2 Cargo Handling: The C-40A LMT shall have a fully-operational main cargo door replicating the exact specifications of the USN C-40A (Boeing 737-700C) aircraft. Switch location and latching mechanism shall replicate the design and operation of the C-40A (Boeing

737-700C) aircraft. The main cargo door shall replicate main cargo door operation of the C-40A including operating positions (CLOSED, CANOPY, FULL OPEN). Door shall be designed to operate via electrical power located in the fuselage cargo area.

5.2.1 The C-40A LMT interior floor structure and interior cargo hold area and interior cargo handling system shall replicate the interior cargo compartment of the C-40A (Boeing 737-

700C) aircraft and able to accept and support three (3) standard U.S. Air Force 463L pallets with dimensions of 2.25 inches high, 88 inches long and 108 inches wide (empty pallet weight 290 pounds). The LMT device shall be capable of supporting a total of 15,000 lbs. of cargo.

5.2.2 The C-40A LMT shall incorporate all systems associated with cargo loading and unloading, to include a full complement of interior cargo floor elements, latches, anchor points and restraints and an actual C-40A Combi main deck cargo net. Nonskid material, cargo locks, ball decking and rollers shall be installed on the floor identical to the C-40A aircraft in Combi configuration.

5.3 Additional Information:

5.3.1 The government will not perform any modifications to the hanger facility or the parking aprons around the hanger for installation of the C-40A LMT device. Hangar power is currently available as detailed in Section 5.1.1.4. Air-conditioning is not currently available and not required.

5.3.2 The contractor is responsible for the safe storage and oversight of any material or equipment that may be needed during the installation process at the ALTC.

5.3.3 The government will not provide a C-40A aircraft as part of this requirement.

5.3.4 The contractor will not be responsible for removing or disposing of the current LMT device on-site.

6.0 Site Visit:

6.1 Site visits will take place from 02 March 2020 through 05 March 2020. To the maximum extent practicable, the government will allow perspective contractors to take measurements inside a C-40A aircraft so the exact layout can be replicated on the C-40A LMT unit and the contractor can tour the ATLC hanger where the C-40A

LMT device will eventually be installed. Site Visits are optional and are for informational purposes only, no award will be made based solely on the attendance of the site visit. Vendors interested in a site visit should contact AWSC (NAC/AW) Jason D. Allen at 817-782-1207 or CDR Chad Martin at 817-782-5229 at least 5 days prior to the start of the site visit window mentioned above to schedule a date and time for a site visit and for direction/instructions about base admittance and safety protocol. It is anticipated that each vendor that participates in a site visit will receive a 4-hour block of time to visit the hanger and take measurements of an actual C-40A aircraft. There will be no questions and answers (Q&A) period during the site visit, if you have any questions please reach out to the Contracting representative, Jacob Segal at 215-697-9813.

7.0 MILESTONE PLAN/ MILESTONE PAYMENTS

The contractor is bound to the Milestone Plan submitted with their proposal and incorporated into the resultant contract. The contractor must detail the process along the way by making milestone presentations to the Government as a condition of payment for completion of each milestone. Milestone payments will only be made after the Government has determined that the milestone has been met. Each milestone is successive and each milestone is dependent upon the completion of the one(s) prior as is the payment for each milestone. Final Payment will occur only after the unit has been safety tested ad accepted by the

Government.

The contractor shall coordinate with the Government POCs listed under Section 10.0 of this SOW within

10 days of completing a milestone to schedule a presentation to show progress and detail how each milestone was completed. The presentation should take place within 30 days from the completion of the milestone and shall be done at the contractor’s expense. The Contractor and the Government shall agree upon how and when the milestone presentation shall take place (i.e. face-to-face, teleconference, VTC, etc.). At a minimum, the contractor shall address the following during the presentation:

What is the milestone and was it completed on time, if not, what was the delay.

Detail how the milestone was completed.

Discuss the remaining timeline for the rest of the acquisition.

Include any risks that could impact future delays

Any other information the contractor considers relevant.

8.0 DELIVERY SCHEDULE:

8.1 The unit shall be installed and ready for use no later than 36-months after the issuance of the contract.

9.0 PLACE OF PERFORMANCE:

9.1 Commander, Fleet Logistics Support Wing (CFLSW), Air Logistics Training Center (ALTC), NAS JRB Fort Worth

Fort Worth, TX 76127-1251

10.0 POINTS OF CONTACT:

10.1 CDR Heath Leggett

CNAFR VR Jet Program Manager

Comm: 757-322-2675

DSN: 262-2675

Email heath.leggett@navy.mil

10.2 CDR Chad Martin

ALTC Officer-In-Charge

Comm: 817-782-5229

DSN: 739-5229

Email: chad.c.martin@navy.mil

10.3 Jacob Segal

Contract Specialist – NAVSUP FLCN-Philadelphia

Comm: 215-697-9813

Email: Jacob.Segal@navy.mil

SECTION I - CONTRACT CLAUSES

mailto:beau.hufstetler@navy.mil mailto:chad.c.martin@navy.mil

The following have been added by reference:

252.225-7012 Preference For Certain Domestic Commodities DEC 2017

252.225-7015 Restriction on Acquisition of Hand Or Measuring Tools JUN 2005

(End of Summary of Changes)