Industry_Day_10_May.pdf

Service ExcellenceIntegrity

AFLCMC…Providing the Warfighter’s Edge

ROCC Industry Day

• The following is a summary of the information provided at the C-17 Roll-On Conference Capsule (ROCC) Program’s Industry Day held 10 May 2018

• The official RFP take precedence over the information contained in these slides

DRAFT

C-17 System Program Office

C-17 Roll-On Conference Capsule (ROCC) Program

Industry Day 10 May 2018DRAFT

Industry Day Agenda

0900 Assemble, Meet & Greet Industry Reps, Government

0915 Introductions All

0920 Admin, Housekeeping DAU Host

0930 Industry Day Rules of Engagement (Q&A’s, RFI’s) C-17 PK, Ms. Larson

0945 Importance of ROCC to Air Mobility Command ROCC RO, Mr. Welker

0950 ROCC Program Overview ROCC PM, Mr. Moore

1010 BREAK

1025 ROCC Contracting Approach and Proposal Requirements ROCC CO, Ms. Larson

1045 ROCC Technical Requirements(SRD) ROCC Ld Eng, Mr. Stevenson ATTLA Ld Eng, Mr. Kuntavanish

1115 ROCC Testing and Airworthiness C-17 Test Mgr, Mr. Krieger

1130 BREAK

1140 ROCC SOW Requirements PMs, Mr. Moore, Mr. Hale

1155 ROCC ILS, CO&MS and Training Requirements C-17 Product Support Mr. Wuori, Mr. DeRosa

1215 - 1330 LUNCH

1330 One-on-One Session

1400 One-on-One Session

1430 BREAK

1440 One-on-One Session

1510 One-on-One Session

C-17 System Program Office

C-17 Roll-On Conference Capsule (ROCC) Program

Kerry Welker

HQ AMC/A5QV

Importance to Air Mobility Command

10 MAY 18DRAFT

5Unrivaled Global Reach for America … ALWAYS!

AMC’S CURRENT ASSET

Silver Bullet (SB) capsule: Airstream trailer palletized in three sections

• Two capsules located at JB Andrews (89 AW)

• Always paired with Steel Eagle comm module

• Operated on C-17 aircraft w/ wideband SATCOM system

• Provides Senior Executive environment (privacy & quiet)

6Unrivaled Global Reach for America … ALWAYS!

ROCC IMPORTANCE TO AMC

• Current Silver Bullet Capsule (IOC 1991) not airworthy

• ASC Assessment (Feb 2000): Should be occupied only when aircraft is at rest or system has been off-loaded

• AFLCMC 2015 “Quick Look” validated risk profile

• Flying under AMC/CC memo accepting “SERIOUS” risk

• May be occupied except takeoff, landing, air refueling, and moderate turbulence encountered during cruise

• Silver Bullet does not meet Nat’l Senior Leaders’ operational mission needs

• AMC, SPO, AFRL, 89 AW, DoD CIO, Sr Ldr Travel Teams participated in requirements development

• AMC must replace Silver Bullet with airworthy asset

Nat’l Sr Leader Safety and Mission Accomplishment are Paramount

7Unrivaled Global Reach for America … ALWAYS!

QUESTIONS?

C-17 System Program Office

C-17 Roll-On Conference Capsule (ROCC) Program

Mr. Craig Moore

AFLCMC/WLMP

ROCC Program Overview

ROCC Program Background

• March 2016: C-17 System Program Office (SPO) tasked to develop strategy for replacing 2 Silver Bullet trailers with airworthy capsules (ASR

& AFF 1067)

• March 2017: C-17 Silver Bullet Replacement officially appointed as an AF, acquisition Program of Record, assigned to the C-17 SPO

• April 2017, AMC Cmdr assigned ROCC as the official name of the Silver Bullet replacement capsules

• January 2018, AF Mobility PEO approved the Acquisition Plan for the ROCC Program

• Extensive market research with US industry contributed to the Air Force’s acquisition strategy

ROCC Background, Cont.

• March 2017: Technical Certification Basis for ROCC Airworthiness on C- 17 approved by AFLCMC EN/EZ

• April 2018: ROCC System Req’ts Document (SRD) certified by Air Mobility Command

• 3 May 2018: Draft RFP 2 posted to Federal Business Ops site

ROCC Acquisition Plan

DRAFT

Presenter Presentation Notes Refer to Backup Chart for background (what events brought us here) and source of AMC requirements No software procurement required for ROCC electrical equipment.

AFRL/RYAR has worked with SPO as a primary Stakeholder – AFRL currently managing Steel Eagle / legacy Silver Bullet for AMC/A6 ATTLA has been instrumental to SPO by coordinating numerous detailed technical requirements in SRD and test planning CONOPS is mature

Fiscal Year FY17 FY18 FY19 FY20 FY21 FY22 FY23 FY24

Pre-Contract Award

Contract Phases & Program Milestones

Funding Profile

Systems Engineering

Integration / Test Phases

Manufacturing

Logistics

MDD

Time now

Requirements Scrub / Dev, Market Research, Cert Basis Approval, Draft RFPs 1 & 2

3600 RDT&E Funding 3080 Procure

AMC 3400 Sustainment (RO/RO)

ASP MS B

Contract Award

PDR CDR

TRR

Airworthiness Cert

FA

Train JBA Cadre

SA

MS C

ILS Package

P-1 to

AMC

SRR

IOC

SORA

DSOR BCA

Contractor Logistics Support (CO&MS)

FA = First Article / to AMC as P-1 SA = Second Article (PROD) / to AMC as P-2

OT

FOC

C-17 ROCC Schedule Notional, as of 7 May 18

RFP

FCA/PCA

Re-compete

CLS

Source Selection

Industry Day

FA

DD 250

P-2 to

AMC

SA

DD 250

DT 2

DT 1 = Contractor Testing DT 2 = LDTO Integration Testing

FA Conversion 18 months

Events / Milestones not to scale

Notional Schedule ONLY

OFFERORS TO BID

OWN

SCHEDULES

QUESTIONS?

C-17 System Program Office

C-17 Roll-On Conference Capsule (ROCC) Program

Ms. Georgia Larson

AFLCMC/WLMK

Contracting Approach & Proposal Requirements

Contracting Approach

• Small Business Set-Aside

• Best Value Trade-off

– Trade-off between Technical subfactor 1 compliance and Cost/Price; Technical subfactors 2 &3 will be Acceptable/Unacceptable

– Past Performance will be Acceptable/Unacceptable

– Cost/Price will be evaluated for

• Price Reasonableness

• Unbalanced Pricing

• Cost Realism (Cost-Plus Fixed Fee CLINs only)

• Total Evaluated Price

• Up to one (1) contract awarded

General Instructions

• The Contracting Officer (CO) is the sole point of contact for this acquisition.

• Page limits

– Executive Summary – 4 pages

– Technical Volume – 75 pages

– Past Performance – Limited to pages printed by PPI Tool

– Cost/Price – No limit

– Contract Documentation – No limit

• Due Dates

– Past performance – requesting 30 days after release of RFP or

No later than 45 days after release of RFP

– Technical Volume, Cost/Price Volume, and Contract

Documentation – 45 days after release of RFP

Contract Line Item Number Structure

CLIN

Contract Type Description Quantity

0001 FFP First Article (FA) ROCC 1 EACH

0002 CPFF FA ROCC Testing 1 LOT

0003 FFP Data 1 LOT

0004 Option CLIN FFP Production ROCC 1 EACH

0005 Option CLIN FFP Heavy Maintenance Bench Equipment 1 LOT

0006 Option CLIN CPFF FA to Production Configuration 1 EACH

0007 Option CLIN FFP Spares 1 LOT

0008 Option CLIN FFP Training 1 LOT

0009 Option CLIN CPFF CO&MS (1 year) 1 LOT

0010 Option CLIN CPFF CO&MS (1 year) 1 LOT

0011 Option CLIN CPFF CO&MS (1 year) 1 LOT

0012 Option CLIN FFP Level III Drawings 1 LOT

Data Rights

• Must bid in accordance with H-clause in order to be technically acceptable

• Grants the Government rights to Depot-level Operation, Maintenance, Installation, and Training

• Does not include right to sell commercial or reproduce

C-17 System Program Office

C-17 Roll-On Conference Capsule (ROCC) Program

Mr. Julian Stevenson

AFLCMC/WLE

Technical Requirements

ROCC Electrical and Communications Interfaces

60A 3Φ 400Hz 20A 3Φ 400Hz

Steel Eagle

For Steel Eagle power For Capsules power converters

For Capsules power converters

100A 1Φ 60Hz

20A 3Φ 400Hz

ROCC

- ROCC will be connected to Steel Eagle module, which will provide ALL electrical and communication connections to the Capsules

- Only ROCC connection to aircraft (besides ADS rails) will be a port for connecting C-17 interphone cord to the aircraft public address system

Aircraft Interphone/PA

(Comfort Pallet)

ATGL

Electrical/Communications Requirements

• ROCC receives all power and communications from the Steel Eagle

• The Steel Eagle in Not included in this procurement effort

• It is required that the selected contractor deliver a ROCC Interface Control Document (ICD) that identifies all the interfaces between the ROCC, the aircraft and other equipment that interfaces with it.

• ROCC electrical wiring shall be designed in accordance (IAW) with SAE AS50881

• There is the potential for classified meetings in the ROCC Installation of electronic equipment and data cabling shall be IAW

CNSSAM TEMPEST/01-13

Interface Connectors for the Steel Eagle and Water/Waste Connections

Interface Connectors Manufacturer Manufacturer's

Part Number National Stock

Number Purpose Remarks

Communications Connectors (See Note 3)

Amphenol RJF21G 5935-01-529-3111 Ethernet or ISDN connections – EIA 568B Same on SE and SB

Amphenol RJF21G 5935-01-529-3112 Aruba WiFi POE – EIA 568B Same on SE and SB

Amphenol RJF21G 5935-01-529-3113 Moving Map monitor POE – EIA 568B Same on SE and SB

Amphenol RJF21G 5935-01-529-3114 Video Telepresence System – EIA 568B Same on SE and SB

Amphenol RJ11F21G 5935-01-573-6824 PSTN/POTS connections – Telco std Same on SE and SB

Mil Spec MS3120F10-6S 5935-00-912-6601 ICS connection See Note 1, Meets the requirements of Note 3

Optical Connectors (See Note 3) Glenair 180-091XMS7-17-8SN 6060-01-646-7430 Fiber optic network Same on SE and SB

Power Connectors (See Note 3)

Amphenol GTS02R-40-ADP (2 required) Not Stock Listed Dedicated 120V 60Hz 50A x2 power from Steel Eagle See Note 2 (item is obsolete)

Water/Waste Connectors (See Note 4) Rockwell Collins 1002-12C 4730-00-316-0064 Potable Water ServicingBoeing 7D1052N12-2

Parker-Hannifin Corp 10101000CJ3 4820-01-433-8011 Lavatory Servicing, Black Water Removal

Rockwell Collins 0060-0062 4730-01-460-3315 Lavatory Servicing, Rinse/Refill Hose ConnectorBoeing 7D0169-2

Note 1: The Legacy Silver Bullet (SB) does not have an ICS system or connection. Only the Steel Eagle Communications Module (SE).

-The C-17A ICS panel connector the SE plugs its cable into at the left paratroop door is P/N: MS3450W16S-1S.

-The SE ICS cable connection on I/O panel 2 connector is P/N: MS3120F10-6S.

Note 2: SE and SB power connectors are different.

-SE power female connector is P/N: GTS02R-40-ADS.

-SB power male connector is P/N: GTS02R-40-ADP.

Note 3: The connectors listed in this section are what are currently used on the SB which the ROCC will replace. The connectors required on the ROCC shall meet IEEE standards, MIL-DTL-38999M w/Amendment 2, SAE AS50151C and/or other current Commercial or Military standards depending on the type of connector needed to meet the required communications or power requirements. It is not permitted to use proprietary connectors without prior approval from Government engineering.

Note 4: The Water/Waste connectors listed are what is currently used on the C-17 aircraft for servicing of the onboard lavatory and potable water tank. These connectors are required to be used on the ROCC.

• These are the connectors currently used on the Silver Bullet

• Not required to use these exact connectors on the

ROCC

• No modification is permitted on Steel Eagle

• No proprietary connectors are permitted, only COTS or Mil Spec

ROCC to Aircraft and Service/Materiel Handling Equipment Interfaces

• No modification is permitted to the aircraft, Servicing, or Materiel Handling Equipment (MHE)

• ROCC is required to interface with the Air Delivery System (ADS) rails, various MHE, and service vehicles Restrainable to MHE and service vehicles for ground transport

• The MHE and Service vehicles that could be used:

– 25K, 40K, and 60K K-Loaders

– Cranes

– Fork Lifts

– Ground Transport Trucks

– Military Lavatory/Potable Water Service trucks

ROCC Overall Dimensions

• The Maximum Height is 123” from the top of the ADS rollers to the top of the capsules

• Base Widths should follow MIL-STD-1791C w/ Change 1 guidance The ROCC Width at the outer edge of the Base Rails is 108” The Width of the ROCC floor is 104” +0.75”/-0.0”

• The Maximum Outside Width of the ROCC above the floor is 120”.

However, special care should be taken to ensure the ROCC does not interfere with the operation of the locks.

Minimum of 4” measured vertically from the bottom of the base before making the transition from 104” to 120”

• Design Length of the ROCC is:

For the SLS Design length is 212” ± 6” For the CR/SA Design length is 292” ± 6”

DRAFT

Presenter Presentation Notes Cannot contact the aircraft or K-loader rails and catwalks during loading

ROCC Base

• HCU-6E (463L) type base

• Included as a reference and to show the gaps in the rails and overall dimensions that are used by the ADS locks

ADS Rails

• There are 40” between each ADS Lock

• See MIL-STD-1791C w/ Change 1 to see the above image and explanation of the ADS rails and locks.

ROCC Weight Limit

• Because the ADS Locks are weight limited, the ROCC is weight limited

• The Senior Leader Suite (SLS) is limited to 10,900 pounds

• The Conference Room/Staff Area is limited to 15,300 pounds

• Max weight limits include:

40 lbs for luggage in the SLS 15 lbs per person for Laptops and other personal electronic devices 125 lbs for Carry-On Communications Kits (printers, routers, etc.)

80 lbs for other mission required bags/equipment

The SLS should be designed for two (2) occupants and two (2) visitors The CR/SA should be designed for nine (9) occupants The max number of ROCC occupants is eleven (11); occupant count is not additive.

DRAFT

Presenter Presentation Notes Only 2 occupants in SLS during takeoff landing and critical phases of flight.

Crash Load Requirements

• ROCC shall be designed to meet the crash load requirements in accordance with MIL-HDBK-516C ¶ 5.1.9, and Structures Bulletin EN-SB-10-002 Rev A at a minimum Longitudinal – 9.0g fwd and 1.5g aft Lateral – 1.5g left and right Vertical – 4.5g down and 2.0g up

• To avoid the need for a dynamic crash test, it is required to analyze the ROCC structures, and other items called out in MIL-STD-516C with an additional 1.5 load factor.

Longitudinal – 13.5g fwd and 2.25g aft Lateral – 2.25g left and right Vertical – 6.75g down and 3g up

• The analyzed items are allowed be permanently deformed at ultimate loads, but not become projectiles or cause the occupants to become trapped

Seat Requirements

• The use of FAA approved Seats is highly encouraged Designing your own seats is not recommended

• The Government will accept/approve the use of FAA certified seats provided that they meet the military requirement for a 250 lb occupant FAA seating and restraint systems are only tested for 170 lb occupants

• MIL-HDBK-516C ¶ 18.1.1 requires seating and restraint systems, including floor attachments, to meet the requirements of SAE AS8049 with a 250 lb occupant Permanent deformation is allowed at 250 lbs provided it does not harm occupant (e.g. pin occupant or impeded egress)

Noise Attenuation

• Ambient noise levels in the cargo bay of the aircraft are:

86 dBA at normal cruise 100 dBA at takeoff

• The exterior walls of the ROCC are required to reduce the pass through noise from the cargo bay into the ROCC The maximum noise level permitted inside the ROCC is 65 dBA, not including takeoff.

Other Human Factors

• MIL-STD-516C sections 9 and 18 requirements:

Egress Lighting

Emergency and Overhead Visual and auditory emergency equipment and signage Life support systems (EPOS, fire extinguishers, etc.)

Public Address System Doors and locking mechanisms

• Federal Aviation Regulations requirements Smoke and Flammability of materials

Engineering Data

• Level 3 engineering data is required per CDRL deliverable and H-Clause

• Level 3 data is required in order to allow the Government and/or a Contractor Logistics Support (CLS) contractor to maintain, repair, modify (if required), and refurbish the ROCC

• There are two (2) parts to Level 3 Engineering Data The Engineering Drawings (Including Applicability, Notes List and

Parts List The Rights associated to those drawings

Engineering Data Cont’d

• The Government is requiring the delivery of the all the Level 3 Engineering Data (regardless of the data rights associated) All delivered data shall have data rights markings per CDRL requirement Items designed and developed by subcontractors or COTS items shall be delivered as Vendor Item Control Drawings (see CDRL requirements for more detail)

• For NEW Engineering Data, the Government DOES NOT want the contractor to use proprietary data/information in the design.

• It is required that the contractor only use Military or commercial processes and standards for data that is developed using Government funds.

QUESTIONS?

BACK UP

Basic Base Width Dimensions

ROCC RAIL WIDTH

108”

ROCC CAPSULE FLOOR WIDTH

104”

ROCC MAX WIDTH

120”

Min 4”

Notional Cross Section Shape

C-17 System Program Office

C-17 Roll-On Conference Capsule (ROCC) Program

Mr. James Krieger

AFLCMC/WLMP

Test & Evaluation and Airworthiness

Test and Evaluation

• The ROCC Test and Evaluation process

– The 412th Test Wing as Lead Development Test Organization (LDTO) to provide oversight and System Program Office (SPO) to provide support

– Contractor shall perform System, Sub-system and Component level Developmental Testing (DT) verifications to verify all project requirements, as defined in the SRD section 3.0. Verification approach is identified in SRD section 4. (Demonstration, Inspection, Analysis, Test)

– Government attendance will be required at identified critical verifications.

Attendance must be coordinated by Contractor with SPO

– Contractor shall provide all verification results and reports to the SPO for analysis and Pass/Fail determination

– Contractor will support and attend Integration Testing efforts at Edwards Air Force Base

Test and Evaluation, Cont.

• The Integrated Test Team (ITT)

– ITT will include the, 412th Test Wing (LDTO), C17 Program office (TM/EN/PM), AMC/TE (OTO) and the Contractor Test and Evaluation team

– The ITT will meet on a regular basis throughout the project to develop test plans, manage activities, review results and support all other T&E activities

• Test Plan Development

– Contractor: System, Sub-System and component Developmental Test Plan

– LDTO: Integration Developmental Test Plan

– Contractor is expected to perform verifications throughout the design and build process, while combining verification activities where feasible

– Thorough and complete Developmental Testing should allow for seamless Integration testing

• Draft Technical Orders (TO’s) documentation will be required in support of

Integration Testing and Operational Test & Evaluation

• SRD and Draft Test Matrix will be included in RFP, ensuring bidders have required T&E information for proposals

Airworthiness

• Airworthiness

– The Government Airworthiness Certification process is used to confirm improvements, modifications and new developments are fully tested and approved prior to release for use

– ROCC Airworthiness Certification requirement is the responsibility of the SPO

– The Contractor is responsible for supporting the SPO by:

• Performing verifications

• Providing required artifact data to the SPO

• Support Integration Testing

• Support review meetings throughout the Airworthiness Certification process

– The Approved Certification Basis provided within the Bidders Library indicates the test artifacts that will need to be delivered in support of the Certification. The ITT will work to ensure all required documents are identified.

QUESTIONS?

C-17 System Program Office

C-17 Roll-On Conference Capsule (ROCC) Program

Mr. Craig Moore

AFLCMC/WLMP

Mr. Bryan Hale

AFLCMC/WLMP

ROCC SOW Requirements

SOW – Communications, PMP

• Emphasis on frequent meetings to ensure effective communication between contractor (KTR) and SPO through life of the contract

• After contract award, KTR to be plugged into existing ROCC IPT and sub-groups

• Most Program meetings to be telephonic

• SOW 3.4.1.2 requires formal semi-annual PMR’s with the KTR.

• Face-to-face PMR’s at least annually

• Kickoff meeting at Wright Patterson in conjunction with SRR

• Technical Interchange Meetings (TIMs) also required in SOW at various intervals

• Program Management Plan - important part of SOW

• Integrated Master Plan and Schedule (CDRL A004)

• KTR submission of forecast costs (CDRL A010)DRAFT

SOW – Systems Engineering

• KTR to employ sound Systems Engineering processes and tools to ensure the ROCC meets overall system performance req’ts

• Power and comm connections to Steel Eagle

• Plug and play for travel teams carry-on electronic equipment when connected to

ROCC provisions

• Other ROCC interfaces per SRD

• Systems Engineering Management Plan (SEMP) for ROCC

• Level III drawings and other deliverables that are part of the ROCC Technical Data package

• CDRL A005 - System/Subsystem Design Description (SSDD)/ System Design and

Interfaces

• CDRL A008 - Drawings, diagrams, schematics and ICD per H001 Clause

• CDRL A009 - System/Sub-System Specification (SSS)

• CDRL A030 – Drawing Tree

SOW – Configuration Mgt

• KTR to use configuration management system IAW Society of Automotive Engineers (SAE) EIA 649-1

• Configuration Management Plan - CDRL A011

• Data Accession List (DAL), per CDRL A016

• “As required” deliverables:

• Engineering Change Proposal(s) with Notice of Revision(s), per CDRLs A012 and

A013

• Requests for Variance from the approved SSS, per CDRL A014

• Contract Change Proposals, per CDRL A015DRAFT

SOW – System Safety

• KTR to establish a System Safety Program (SSP) IAW MIL-STD-882E (CDRL A017)

• SSP to emphasize formal safety analyses of ROCC system hardware and interfaces.

• Hazard identification (real and potential), mitigation and residual risk acceptance, per CDRL A018

• Vendor safety risks for commercial items installed in ROCC for use in the military environment

• Personnel health hazards – to include evaluation of proposed hazardous materials, per CDRL A019

• Any safety risks prior to Government participation in testing of the FA ROCC and operation of the production ROCCs, per CDRL A020

SOW – Production Planning

• Manufacturing plan (CDRL A021) required

• Ensure product quality and prevent defects, both at the prime and subcontractor levels

• Describe and illustrate the facility space planned to manufacture, assemble, and test each ROCC (basic work flow)

• Describe the facility planned to store each ROCC until delivery to the USG

• KTR must maintain one of the following quality certifications: ISO 9001 or

AS9100D

• KTR to transport the FA ROCC to Edwards AFB, CA for formal Government acceptance and Air Force integration testing

• After AF integration testing, First Article ROCC to be returned to the KTR as Government Furnished Property, for any work necessary to field as ROCC P-1 configuration.

SOW – Risk Management

• KTR to implement a Risk Management Program (RMP) that identifies contractor risks for executing the contract (CDRL A022)

• SPO will maintain a separate RMP for ROCC program risks

• SPO needs to understand what the KTR thinks his risks are

• Include Supply Chain Risk Management in the RMP

• Source all electronic parts IAW DFARS 252.246-7008, Sources of Electronic Parts

• At CDR, identify the source(s) of supply to the Government for all electronic parts

(include in Manufacturing Plan)

C-17 ROCC Security Requirements

• Government Installation Access

• Requires T1 Favorable Background Investigation

• Operations Security (OPSEC)

• Protect Critical Information (CI) and Controlled Unclassified Information (CUI)

• Government’s ROCC OPSEC Plan to be made available at RFP

• Must comply with DoDM 5200.01, Volume 4, DoD Information Security

Program: Controlled Unclassified Information (CUI) – Enclosures 3 and 4

• Related Contract Clauses

• DFARS 252.204-7008 – Compliance with Safeguarding Covered Defense Information

• Implement the security requirements specified by NIST SP 800-171

• DFARS 252.204-7012 – Safeguarding Covered Defense Information and Cyber

Incident Reporting

• Upon discovery of a cyber incident, conduct a review for evidence of the compromise and rapidly report cyber incidents

DRAFT

Presenter Presentation Notes (NIST SP 800-171) National Institute of Standards and Technology (NIST) Special Publication (SP) 800-171, “Protecting Controlled Unclassified Information in Nonfederal Information Systems and Organizations”

Recommend Defense Security Service Academy Course - OPSEC Awareness for Military Members, DoD Employees and Contractors GS130.16

SOW – Quality of Services

• Services elements require additional quality assurance measures

• Performance Requirements Summary

• Outlines performance objectives and specific remedies associated with SOW

Training and CO&MS tasks

• Issues to be documented in CPARs and may require re-performance

• Corrective actions may be requested from the contractor

• Contracting Officer Representative (COR)

• Responsible for inspecting, documenting, and reporting performanceDRAFT

QUESTIONS?

C-17 System Program Office

C-17 Roll-On Conference Capsule (ROCC) Program

Mr. Troy DeRosa

AFLCMC/WLMBA

Mr. Wayne Wuori

AFLCMC/WLMBA

Integrated Logistics Support

INTEGRATED LOGISTICS SUPPORT

• ILS PACKAGE

• TECHNICAL MANUALS

• Operational and Intermediate (Field) level

• AF TO Format

• SPARE PARTS

• System Unique and Replacement Parts

• Provided from Induction - Period of Performance

• SUPPORT EQUIPMENT

• Current Commercially Available Equipment

• AF Inventory

• SUPPORT REVIEWS

• Electronically each Month

• In-Person up to Twice Annually as Required

INTEGRATED LOGISTICS SUPPORT

• ILS PLAN

• SUPPORT PACKAGE ELEMENTS

• Delivery and Sustainment Details

• Provide CO&MS

• MATERIAL SUPPORT

• Packaging

• Handling

• Storage

• Delivery

• ILS MANAGEMENT TEAM (ILSMT)

• Continuous Interface with USG

• Insures Maintainability & Supportability

TRAINING REQUIREMENTS

• PERIOD OF PERFORMANCE

• Not to Exceed 60 Days

• Conducted at Operating Location

• CONCURRENT WITH P-1 DELIVERY

• Formal Classroom and Demonstration

• Computer Based Training (CBTs)

• OJT

• USG will retain ALL Training Materials

TRAINING REQUIREMENTS

• TRAINING DISCIPLINES

• OPERATORS

• Connection of all Systems

• Operation of all Systems

• MAINTAINERS

• Loading & Unloading

• Servicing

• Operational & Intermediate Maintenance

• FLIGHT ATTENDANTS

• PA and Intercom Systems

• Safety, Comfort & Life Support Systems

Reliability/Maintainability/Availability

• Capability Rate

– Maximum 7 hours of Operational Mx per month

– Maintainable without Contractor Support

• RM&A Plan

– Complete Service Life Sustainment

– Identify Required Spares

– Recommended Service Frequency Criteria

• Scheduled Inspections

• Refurbishment of Common Wear Items

CO&MS

• Up to Three one (1) year Periods of Performance

• OPERATIONAL

• 100% Contractor Support during Training Period

• 24/7 Telephone Support

• 48 Hour Travel Response (CONUS)

• INTERMEDIATE (Field Level)

• Operational Facility

• Scheduled and Unscheduled Mx per RM&A Plan

• DEPOT LEVEL (Heavy Mx)

• Contractor only (Duration of Contract)

• Designated Depot Facility

• Provide & Deliver all Equipment (Bench, Test, etc.)

QUESTIONS?