FA8629-17-R-2507_Section_J,_Attach_25_-_Section_L.pdf

FA8629-17-R-2507

Section L, Attach 01

Cross Reference Matrix 13 July 2017

Section L Paragraph Section M SOW PWS SRD TSRD Proposal Reference(s) (Offeror to provide)

Section L 1 (and Subs) N/A 4.4.1 N/A N/A N/A Section L 2 (and Subs) 1.5 N/A N/A N/A N/A Section L 3 (and Subs) 1.5 N/A N/A N/A N/A Section L 4 - 4.1.3.3 1.5 N/A N/A N/A N/A Section L 4.2 - 4.2.4 2.1 and 2.2 (and Subs) N/A N/A N/A N/A Section L 4.2.5 (and Subs) 2.2.1 (and Subs) 4.4.1 N/A N/A N/A

Section L 4.2.6 (and Subs) 2.2.2 (and Subs) N/A N/A

3.1.1, 3.1.2,

3.1.3 3.5.2, 3.5.4

(and Subs), 3.10.2, and

Appendix D-3

N/A

Section L 4.2.7 (and Subs) 2.2.3 (and Subs) 4.3.2, 4.3.8 (and Subs)

N/A Section 3 N/A

Section L 4.2.8 (and Subs) 2.2.4 (and Subs) 4.7.3, 4.7.6,

4.7.6.4.1 N/A N/A N/A

Section L 4.2.9 (and Subs) 2.2.5 (and Subs) 4.5.5, 4.5.6 (and Subs), Appendix D

3.3.2 and 3.3.3 3.9.1 (and Subs) 3.13.7, 3.13.17, (and

SUBS)

Section L 4.3 (and Subs) 2.3 (and Subs) N/A N/A N/A N/A Section L 5 (and Subs) 1.5 and 2.2 (and Subs) N/A N/A N/A N/A

Section L Atch 01 CROSS REFERENCE MATRIX

SECTION L, ATCH 2: Electronic Format for All Proposal Volumes

13 July 2017

Section L Attachment 2 Instructions to Offerors

Electronic Format for All Proposal Volumes

When submitting electronic versions of the proposal, offerors shall follow these instructions:

a. For all submitted electronic documents:

• No electronic document shall be encrypted or shall require the use of a password

• All content must be searchable and all information visible

b. Electronic storage media shall be submitted in one of the following formats:

CD or DVD.

c. Submitting documents using Microsoft Office 2010 or greater:

• Word documents – Set "Save as type" to "Word Document (*.docx)"

• Excel spreadsheets – Set "Save as type" to "Excel Workbook (*.xlsx)."

• PowerPoint presentations – Set "Save as type" to "PowerPoint Presentation

(*.pptx)."

d. Submitting documents using Microsoft Office 2007:

• Word documents – Set "Save as type" to "Word Document (*.docx)"

• Excel spreadsheets – Set "Save as type" to "Excel Workbook (*.xlsx)."

• PowerPoint presentations – Set "Save as type" to "PowerPoint Presentation

(*.pptx)."

e. Submitting documents using Microsoft Office 2003:

• Word documents – Install the Office Compatibility Pack from www.microsoft.com and Save As "Word Document (*.docx) "

• Excel spreadsheets – Install the Office Compatibility Pack from www.microsoft.com and Save As "Microsoft Excel Workbook (*.xlsx) "

• PowerPoint presentations – Install the Office Compatibility Pack from www.microsoft.com and Save As "Microsoft PowerPoint 2007 Presentation (*.pptx) "

f. Submit any Microsoft Project files in Microsoft Project 2007 or greater. There are no special “save” functions required for later versions of Project.

g. Submit PDF documents using only Adobe Acrobat X (10.0) or later. Do NOT submit any documents in PDF format that are copied as "images." When creating PDF files always create to enable textual search and copy functions. Do NOT submit documents using file compression software (such as .zip format).

http://www.microsoft.com/

Section L, Attach 4

13 July 2017

Instructions:

Weight Estimate worksheet: Weight inputs shall be in accordance with MIL-STD-3013, Chapter 3 DEFINITIONS. The following definitions shall be used to determine the requested weights in the Weight Estimate tab: 3.10.1 Empty Weight, 3.10.2 Basic Weight, 3.10.3 Operating Weight, 3.10.4 Payload,

3.10.8 Takeoff Gross Weight and 3.10.9 Maximum Takeoff Gross Weight. List all components included in each weight estimate as well as the respective weights (lbs) for each component.

Mission Performance worksheets: Complete the separate worksheets for the ICBM ESR Mission, ICBM Convoy Escort Mission, COOP Transport Mission profiles. The missions are broken down by each segment and provide the altitude (MSL) and temperature (degrees C), as well as the time (minutes), speed (KTAS) or distance (nm) of the segment as needed. Each mission sequentially requests the aircraft weight at the start of the segment, weight at end of the segment, power available, power required, and the power setting used during this segment. Provide the fuel reserve in minutes and pounds at the end of each mission.

Provide the mission performance information as requested in the five worksheets of this workbook.

Cells that are blacked out do not require your input.

Energy Consumption worksheet: No inputs are required. This worksheet calculates, based on the mission performance inputs in the mission profile worksheets, the average energy consumption rate based on the average for the ICBM ESR Mission, ICBM Convoy Escort Mission and COOP Transport Mission profiles.

Group Weight Estimate: Provide a group weight estimate for the UH-1N Replacement aircraft. The group weight estimate can be a separate attachment if desired.

Group Weight Estimate Worksheet

13 July 2017

Weight Definition (MIL-STD-3013) ICBM ESR Mission Weight

(lbs) ICBM Convoy Escort Mission Weight (lbs)

COOP Transport Mission Weight (lbs)

1 Weight Empty

Weight empty is defined as the weight of the air vehicle, complete by model design definitions, dry, clean, and empty, except for fluids in closed systems such as the hydraulic system. Weight empty includes total structure group, propulsion group, flight controls group, avionics group, auxiliary power plant group, electrical group, etc.

2 Basic Weight Basic weight is defined as the weight empty adjusted for standard operational items such as unusable fuel, engine oil, oxygen, and all fixed armament.

3 Operating Weight

Operating weight is defined as the sum of basic weight plus such factors as crew, crew baggage, steward equipment, emergency equipment, special mission fixed equipment, pylons, racks, and other nonexpendable items not in basic weight. It is equivalent to takeoff gross weight less usable fuel, payload, and any items to be expended in flight.

4 Payload Weight

Payload is defined as any item which is being transported and is directly related to the purpose of the mission, as opposed to items necessary for the mission. Payload can include—but not be limited to— passengers, cargo, passenger baggage, ammunition, internal and external stores, and fuel which is to be delivered to another air vehicle or site. Payload may or may not be expended.

5 Takeoff Gross Weight

Takeoff gross weight is defined as the sum of the operating weight, usable fuel weight, payload items required to perform a particular defined mission, and other items to be expended during flight. Takeoff gross weight is determined prior to engine start for air vehicles which have a maximum ground weight equal to maximum takeoff gross weight. Takeoff gross weight is determined at liftoff for air vehicles which have a maximum ground weight higher than maximum takeoff gross weight. In the latter case, the fuel weight expended during warm-up, taxi, and takeoff are excluded.

6 Maximum Takeoff Gross Weight

Maximum takeoff gross weight is defined as the highest weight authorized at liftoff. An air vehicle may have more than one maximum takeoff gross weight, such as one for landbased operations and one for carrier/catapult operations.

NOTE: Maximum takeoff gross weight may be the same as maximum gross weight.

Weight

13 July 2017

Segment Number

Segment Additional Segment Description Time (min) Distance

(nm) Speed

(KTAS)

End segment Altitude (ft, MSL)

Temp (C) Start Gross Weight (lbs)

End Gross Weight (lbs)

Fuel Used (lbs)

Power Required

Power Available

Power Setting

1 Start/Taxi/Takeoff Use Table D-1. Payload for the ICBM ESR Mission Profile in the UH-1N Replacement SRD to determine initial takeoff gross weight. Weapons, ammunition and flare weights should represent actual installation system weights.

5 6200 35.0 Flight Idle

2 Departure Climb Start departure climb at previous segment end weight, altitude and temperature. 6500 34.4

3a Fly Enroute to Initial Point Start fly enroute to initial point at the previous segment end weight. 35 6500 34.4 NTE MCP

3b Fly Enroute to Initial Point 35 6500 34.4 NTE MCP

3c Fly Enroute to Initial Point 35 6500 34.4 NTE MCP

4 Loiter to initial point Start loiter to initial point at the previous segment end weight. 5 6500 34.4

5 Fly enroute and descent to

HOGE

Start fly enroute and descent to HOGE at the previous segment end weight, altitude and temperature. 10 5600 38.0

6 Perform HOGE HOGE performed starting at previous segment end weight. 1 5600 38.0

7 Descent to objective landing area

Start descent to objective landing area at the previous segment end weight, altitude and 36.2C. 4700 38.0 NTE MCP

8 Landing at objective area Start landing at objective area from the previous segment end weight. End weight should reflect dropping 2475 lbs worth of payload.

4700 38.0

9 Takeoff and climb to loiter Start takeoff and climb to loiter at the previous segment end weight, altitude and temperature. 5700 36.0

10 Loiter Start loiter at the previous segment end weight. 45 5700 36.0

11 Descent to objective landing area

Start descent to objective landing area at the previous segment end weight, altitude and temperature. 4700 38.0

12 Landing at objective landing area

Start landing at the objective landing area at previous segment end weight. 4700 38.0

Description Fuel

Reserve (mins)

Fuel Reserve

(lbs)

Calculate reserve fuel (in minutes) after completion of Segment 12 using AFI 11-202v3, paragraph 2.2.3

IC

BM

E m er ge nc y

Se cu rit y

Re sp on se

M is si on

(S

RD

A pp

D -1

13 July 2017

Segment Segment Segment Description Time (min) Distance

(nm) Speed

End segment

Altitude (ft) Temp [C]

Start Gross Weight (lbs)

End Gross Weight (lbs)

Fuel Used (lbs)

Power Required

Power Available

Power Setting

1 Start/Taxi/Takeoff Use Table D-3. Payload for the ICBM Convoy Escort Mission Profile in the UH-1N Replacement SRD to determine initial takeoff gross weight. Weapons, ammunition and flare weights should represent actual installation system weights.

5 6200 35 Flight Idle

2 Departure Climb Start departure climb at previous segment end weight, altitude and temperature. 6500 34.4

3 Escort Convoy Start escort convoy at the previous segment end weight. 180 6500 34.4

4 Fly to descent point Start fly to descent point at the previous segment end weight. 45 6500 34.4

5 Descent to landing area Start descent to landing area at the previous segment end weight, altitude and temperature.

6200 35

6 Landing Start landing at previous segment end weight. 6200 35

Description Fuel Reserve

(mins)

Fuel Reserve

(lbs)

Calculate reserve fuel (in minutes) after completion of Segment 6 using AFI 11-202v3, paragraph 2.2.3

IC

BM

C on vo y

Es co rt M is si on (S

RD

A pp D

-2

13 July 2017

Segment # Segment Segment Description Time (min) Distance

(nm) Speed

End segment

Altitude (ft) Temp [C]

Start Gross Weight (lbs)

End Gross Weight (lbs)

Fuel Used (lbs)

Power Required

Power Available

Power Setting

1 Start/Taxi/Takeoff Use Table D-5. Payload for the COOP/Transport Mission Profile in the UH-1N Replacement SRD to determine initial takeoff gross weight. Weapons, ammunition and flare weights should represent actual installation system weights.

3 0.0 30.0 Flight Idle

2 Departure Climb Start departure climb at previous segment end weight, altitude and temperature. 300.0 29.4

3 Cruise to pick-up point Start cruise to pick-up point at the previous segment end weight. 20 300.0 29.4

4 Descent to pick-up point Start descent to pick-up point at the previous segment end weight, altitude and temperature.

0.0 30.0

5 Perform landing for pick-up Start perform landing for pick-up starting at the previous segment end weight.

Add additional 1800 lbs to end weight for this segment.

1 0.0 30.0

6 Takeoff (HOGE required) Start takeoff to a HOGE based at the previous segment end weight. 0.0 30.0

7 Perform HOGE Start perform HOGE at the previous segment end weight. 1 0.0 30.0

8 Climb to Cruise altitude Start climb to cruise altitude at the previous segment end weight. 3300.0 23.4

9 Cruise to drop-off point Start cruise to drop-off point at the previous segment end weight. 175 3300.0 23.4

10 Descent to drop-off point Start descent to drop-off point at the previous segment end weight, altitude and temperature. 3000.0 23.4

11 Perform HOGE Start HOGE at the previous segment end weight. 1 3000.0 23.4

12 Descent to drop-off point Start descent to drop-off point at the previous segment end weight. 3000.0 35.0

13 Perform landing for drop-off

Start landing for drop-off at the previous segment end weight. End weight should reflect dropping 1800 lbs worth of payload.

1 3000.0 35.0

14 Takeoff and climb to cruise altitude

Start takeoff and climb to cruise altitude at the previous segment end weight, altitude and temperature. 3300.0 23.4

15 Cruise to landing area Start cruise to landing area at the previous segment end weight. 30 3300.0 23.4

16 Descent to landing area Start descent to landing area at the previous segment end weight, altitude and temperature. 0.0 30.0

17 Landing Start landing at the previous segment end weight. 0.0 30.0

Description Fuel

Reserve (mins)

Fuel Reserve

(lbs)

Calculate reserve fuel (in minutes) after completion of Segment 17 using AFI 11-202v3, paragraph 2.2.3

CO

O

P/ Tr an sp or t M is si on (S

RD

A pp D

-3

13 July 2017

Mission ICBM ESR ICBM Convoy Escort COOP/Transport Average Fuel Consumption

Across All Missions

Average Fuel Consumption (gph)

#DIV/0! #DIV/0! #DIV/0! #DIV/0!

Engery Consumption

Section L, Attachment 06

COMPANY LETTERHEAD

(DATE)

CEO Certification Letter

AFLCMC/AZA, Bldg. 570, Room 113 ATTN: Kraig Neer, Contracting Officer 1755 11th Street Wright-Patterson AFB, OH 45433-7228

Reference: RFP FA8629-17-R-2507

SUBJECT: CEO Certification

I hereby certify, as CEO of (Offeror’s Name) that the (Offeror’s Name) proposal has met all solicitation requirements, including but not limited to, the terms and conditions of the solicitation, all representations and certifications in Section K of the solicitation, and all the requirements of the Statement of Work/Performance Work Statement as contained in the subject solicitation. (Offeror’s Name) does not take exception to any of the requirements.

The proposed certified baseline aircraft is technically responsive to the UH-1N Replacement solicitation in that our certified baseline aircraft:

1. Has an FAA or US DoD airworthiness certification dated prior to the date of this letter;

and

2. Was produced IAW manufacturing and quality processes, and procedures to maintain the FAA or US DoD AW-certification.

Signature, Title

Section L, Attach 7: Top Drivers of Code 3 Breaks

13 July 2017

Rank1 Nomenclature and Part Number

Next Higher Assembly, System or

Subsystem

Break Rate2

Abort Total Rate2

Total Annual Maintenance Down Time3

Manhours (Unscheduled)2 due to this Part Number

Annual Unscheduled O-level Maintenance

Manhours4

Spares Quantity per Aircraft per

Year5

6 Provide data on Part Numbers to account for 80% of total maintenance manhours

5 To be calculated by offeror, to meet Availability requirements at SRD UTE rate and average sortie duration; use decimals for fractional usage

Top Drivers of Code 3 Breaks

1 Ranked in descending order by Annual Unscheduled O-level Maintenance Manhours 2 As defined in TO 00-20-2, Appendix L

4 Annual Unscheduled O-level Maintenance Manhours = Break Rate x Average Manhours (Unscheduled) per Break x 218 Sorties Flown per Year

3 Maintenance Down Time = Logistics Delay Time + Admin Delay Time + Mean Time to Repair (On Equipment)2; use LDT, ADT = 4 hours each per Break

Section L, Attach 8: Supp Info to Offerors for Cabin Space Demo

ATTACHMENT 8: Supplementary Information to Offerors for Cabin Space Demonstration

1. The demonstration shall be conducted within no more than two days.

2. The demonstrations shall be conducted during the daylight hours only, and can be either in a well-lit hangar or in open outdoor well-lit conditions. If adverse weather is expected, a covered, well-lit location is desired.

3. Unless deemed necessary by the Offeror, the aircraft shall not be powered on.

4. The demonstration shall start and end with the cabin doors in the closed position.

5. Each Offeror shall provide a brief safety/familiarization instruction (under 20 minutes) to the demonstration team and participants regarding the aircraft under demonstration, specifically in relation to the tasks described in Section L, 4.2.6.3.2, or any other safety item of concern. This brief shall be given prior to the start of the demonstration.

6. Offerors will be permitted to witness the demonstration of their own aircraft, but will not be permitted to participate in the demonstration. Offerors will also not be permitted to speak with the demonstration participants before, during, or after the demonstration, with the exception of the briefing previously described. Each Offeror will be limited to no more than two representatives witnessing the execution of the demonstration.

7. The Government will use the Offeror’s proposed procedure to execute the demonstration and will consist of 3 complete trials for each mission.

8. Recording devices (still photography and video photography) will be utilized to document the demonstration. Videos and still photographs collected during the demonstration will be treated as evaluation documentation.

9. The Offeror can determine the mission order based on whichever configuration they first make available to the Government. Following the first mission, time will be allotted to reconfigure the aircraft and will be immediately followed by the demonstration for the remaining mission, if time allows for that day. The preferred agenda is as follows, but can be deviated from based on the needs of the demonstration, as long as the demonstration as a whole does not span more than 2 days, total:

Notional Cabin Demonstration Schedule Morning (8am-11am) Afternoon (2pm – 5pm, up-to dusk) Day 1 Mission 1 Mission 2 Day 2 As needed As needed

10. If a Government delay contributes to an inability to complete the demonstration in two days, remaining portions of the demonstration will be rescheduled and documented accordingly.

11. If the proposed aircraft requires the gun to be internally stowed at any point to meet the system requirements, the aircraft shall be configured with the guns internally stowed for the ICBM/ESR portion of the demonstration.

12. No results or ratings will be shared with the Offeror until after the initial evaluations are complete.

20170713_12(c)(25.2)_Section L, Atch 02_Electronic_Format_Language

20170713_12(c)(25.8)_Section L, Atch 08_Supplementary Information to Offerors for Cabin Space Demonstration