F-15_WBSI_TRD-SOW_Rev-F_FINAL.pdf

TECHNICAL REQUIREMENTS DOCUMENT

(TRD) – STATEMENT OF WORK (SOW)

U.S. Air Force (USAF)

F-15 Wheel & Brake System Improvement (WBSI) Program

18 November 2013 – Revision F

Prepared by

Air Force Sustainment Center (417 SCMS)

Hill Air Force Base, Utah 84056

TABLE OF CONTENTS

1.0 PURPOSE/SCOPE

1.1 Purpose

1.2 Scope

2.0 PROGRAM MANAGEMENT

2.1 Integrated Master Schedule (IMS)

2.2 Supplier Performance Review Board (SPRB)

2.3 Technical Interchange Meetings (TIMs)

2.4 Critical Design Review (CDR)

2.5 F-15 Configuration Management

2.5.1 F-15 Hardware Configuration

2.5.2 Incorporation of Existing Tooling, Fixtures, Inspection Equipment

3.0 SYSTEMS ENGINEERING

3.1 Performance Specification (PS)

3.2 Qualification Test Plan (QTP)

3.3 Test Readiness Review (TRR)

3.4 CDR Test Analysis Reports

3.5 Antiskid System Performance Evaluation Articles

3.6 On-Aircraft Evaluation Support

3.7 Vendor Airworthiness Certification Report (VACR)

3.8 Qualification Test Report (QTR)

3.9 Technical Data Package (TDP)

4.0 TECHNICAL ORDERS (TO)

4.1 Procedural Source Data

4.2 Intermediate, Depot, & Illustrated Parts Breakdown Commodity TOs…

4.2.1 Repair - Wheel Assembly…

4.2.2 Repair - Brake Assembly…

4.3 TO Formatting

4.4 TO Conferences and Reviews

4.5 TO Validation/Verification

5.0 LOGISTICS

5.1 Field Level Spares/Bench Stock Packages

5.2 Depot Level Inspection Equipment andTooling Package

5.3 Initial Spares Conferences and Reviews

5.4 Logistics Management Information (LMI)

5.5 Initial Spare Parts Orders

5.6 Wheel and Brake Assembly Static Displays

TABLE OF CONTENTS

(Continued)

6.0 QUALITY AND SAFETY REQUIREMENTS

6.1 Quality Requirements

6.1 Health Hazard and Assessment Report (HHAR)

7.0 RETROFIT SUPPORT

7.1 Asset Delivery

7.2 System Performance and Technical Support

8.0 APPENDIX A: F-15 WBSI C/D Model Wheel and Brake Spares/Bench Stock Packages

9.0 APPENDIX B: F-15 WBSI E Model Wheel and Brake Spares/Bench Stock Packages

1.0 PURPOSE/SCOPE

1.1 Purpose

This TRD shall become the supplier’s SOW for the F-15 WBSI contract and defines contractual obligations for which the wheel and brake supplier shall be responsible if awarded.

1.2 Scope

This document lists the supplier’s major program milestone schedule, hardware, data, and support requirements for the F-15 WBSI Program. The supplier shall be responsible for satisfying all requirements on two separate configurations, F-15C/D and F-15E, including maximizing component interchangeability between both configurations.

2.0 PROGRAM MANAGEMENT

2.1 Integrated Master Schedule (IMS)

The supplier shall deliver a comprehensive IMS with the proposal. The IMS shall be computer-based and compatible with 417 SCMS Microsoft Project scheduling software. It shall contain all critical events, milestones, completion criteria, predecessors, successors and their dependencies while providing clear evidence of the suppliers understanding of all program objectives, major milestone and schedule requirements. The IMS shall facilitate critical path analysis. Following award, the supplier shall maintain and provide revisions to the IMS (changes clearly identified) throughout the duration of the program including the retrofit phase.

(Reference DID DI-MGMT-81650, Exhibit A001.) To clarify the Government’s required implementation schedule, the following critical milestone event schedule is provided.

CONTRACT AWARD – DESIGN VERIFICATION – QUALIFICATION – DELIVERY

Contract Award

YR 1

QTR 1

Qualification Testing Start – 11 months ARO

CDR Completion – 4 months ARO

Production Delivery Begins – 22 months ARO

YR 2

QTR 2 QTR 3 QTR 4 QTR 1 QTR 2 QTR 3 QTR 4 QTR 1 QTR 2 QTR 3 QTR 4 QTR 1 QTR 2

YR 3 YR 4

YR = Year (12 Months) QTR = Quarter (3 Months) ARO = After Receipt of Order (Initial Contract Award) CDR = Critical Design Review CCB = Configuration Control Board (CCB) Approval

DELIVERY & RETROFIT OVER 24 Months

Flight Testing Start – 17 months ARO

CCB

NOTES:

1. Separate or combined E & C/D model CDRs may be conducted, however, both E & CD model CDRs shall be completed with final USAF approved CDR configurations within 4 months ARO.

2. Qualification test and Safety of Flight (SoF) Qualification Test Report (QTR) delivery shall support a planned flight test start 17 months ARO.

3. For planning purposes the SoF QTR is required 120 days prior to flight test start to support required USAF Safety Review Board approvals prior to flight test start.

Fit Check – 9 months ARO

As part of the IMS, the supplier shall also deliver, implement, and maintain a Schedule Risk Assessment (SRA). The SRA shall include a description of the approach that shall be taken to limit the schedule risks as identified in the supplier’s IMS. Risk is defined as the probability of a schedule change due to program/technical performance and/or cost issues. Technical performance measurement tasks and their correlation with all contractual cost/schedule elements shall be incorporated to reveal potential impacts to the schedule and the supplier’s overall successful contract execution and compliance. The assessment shall clearly define the supplier’s plan to manage these risks throughout the contract compliance period. The initial

SRA shall be provided with the supplier’s proposal. (Reference DID DI-MGMT-81650, Exhibit A001.) The supplier shall also deliver monthly Contractor Progress, Status and Management Reports which indicate current activities, their status and plans for the forthcoming milestone(s), any anticipated problems and estimated completion dates. (Reference DID DI- MGMT-80227, Exhibit A015.)

2.2 Supplier Performance Review Board (SPRB)

The supplier shall attend SPRB meetings. The initial review shall be conducted in conjunction with the program Kick-Off meeting no later than 30 calendar days after contract award. These meetings shall be hosted by 417 SCMS and shall be conducted at locations designated by the Government (which may or may not include the supplier’s facility). The supplier shall provide agenda inputs to support these meetings. The meetings shall serve as a review of the IMS and supplier compliance to contract requirements (performance, schedule, etc.). Follow-on meetings may be held as deemed necessary by 417 SCMS. (Reference DID-ADMN-81249A, Exhibit A002.)

2.3 Technical Interchange Meetings (TIMs)

The supplier shall support TIMs via teleconferencing or at locations as determined by the Government. These meetings will be scheduled and chaired by 417 SCMS and will review overall program and technical progress. Meetings may be weekly, bi-weekly, or monthly as determined by 417 SCMS. Required actions, coordination, and/or resolution tasks will be identified and documented by 417 SCMS in meeting minutes and action lists.

2.4 Critical Design Review (CDR)

The supplier shall host a CDR for both E and C/D model configurations at the supplier’s facility or at a location as designated by USAF. Separate or combined E and C/D model CDRs may be conducted, however, both E and C/D model CDRs shall be completed no later than 120 calendar days after contract award. The supplier shall deliver pre-CDR materials no later than 15 calendar days prior to CDR for review prior to CDR. The meeting shall serve as a review of the supplier’s final technical design to be qualified as well as an opportunity for the supplier and the Government to coordinate on program issues and contract requirements. The supplier shall document anticipated hardware performance and method of compliance verification for each individual technical requirement contained in the F-15 WBSI Performance Specification (PS) (98747) 201228188. The supplier shall provide agenda inputs to support a combined USAF/supplier agenda. (Reference DID-ADMN-81249A Exhibit A002.)

2.5 F-15 WBSI Configuration Management

The supplier shall deliver a Configuration Management Plan (CMP) no later than 30 calendar days prior to CDR which has been tailored to specifically address the F-15 WBSI program.

The CMP shall address post award configuration control for the program, including all configuration requirements addressed in the IMS. The CMP shall include a specific definition and process for the management, coordination, and approval of Class I and Class II engineering change notices by the Government. Specific brake carbon material and manufacturing processing shall be explicitly defined. The supplier shall provide a detailed CMP briefing at CDR. CMP format and content shall be consistent with best commercial practices. (Reference DID-CMAN-80858B, Exhibit A003.)

2.5.1 F-15 WBSI Hardware Configuration

The new F-15E and F-15C/D model brake assembly configurations shall be delivered with a newly designed and qualified shuttle valve installed in the left hand position. The new F-15E and F-15C/D model wheel assembly configurations shall incorporate a lock ring retention design. During the design, qualification and test phases of the program, the supplier shall incorporate all wheel and brake system design changes as they are identified by the Government to meet USAF PS (98747) 201228188 and necessary component reliability and maintainability (R&M) specification requirements into all delivered evaluation articles at no additional cost to the Government. This provision includes, but is not limited to, all design changes identified during design reviews, qualification testing, fit checks, TO validations/verifications and flight evaluation. Upon completion of system testing, qualification and final design approval, the supplier shall incorporate all design changes as determined by the Government to meet USAF PS (98747) 201228188 and necessary component R&M specifications into all delivered production hardware and previously delivered evaluation articles such that these articles may eventually be incorporated into the USAF supply system in production configuration, at no additional cost to the Government. Upon completion of system testing, specific evaluation articles that this will apply to will be determined by the Government.

2.5.2 Incorporation of Existing Tooling, Fixtures, Inspection Equipment The supplier shall incorporate existing tooling, fixtures and inspection equipment requirements into the new design to the greatest extent possible. All additional tooling, fixtures and inspection equipment requirements determined by the Government as necessary to field the new system shall be provided at no additional cost to the Government. This provision includes, but is not limited to, items identified during design reviews, qualification testing, fit checks, TO validations/verifications and flight testing.

3.0 SYSTEMS ENGINEERING

3.1 Performance Specification (PS)

The proposed wheel and brake system shall meet all criteria set forth in USAF PS (98747) 201228188. The wheel and brake system must meet all PS requirements and interface at the weapon system level as a form, fit, function-equivalent replacement.

3.2 Qualification Test Plan (QTP)

The supplier shall deliver a draft QTP at CDR for a combined E and C/D model test program which defines all formal qualification testing to be conducted by the supplier. The QTP shall be based on the TRD-SOW and PS (98747) 201228188 (Reference DID DI-NDTI-80566A, Exhibit A004), and shall demonstrate that all performance and specification requirements will be met.

The QTP outline/format shall mirror that of the PS and pending QTR (reference paragraph 3.8). Final QTP approval shall be granted with Test Readiness Review closure.

3.3 Test Readiness Review (TRR)

The supplier shall support a TRR prior to initiating formal qualification testing. The Government shall determine the location and date of the TRR in coordination with the supplier.

The TRR shall occur no later than 30 days prior to qualification test start. TRR data/documentation shall be delivered for USAF review/comment a minimum of 15 calendar days prior to the TRR (Reference DID DI-NDTI-80566A, Exhibit A004). The supplier shall support the TRR with the following data/documentation as a minimum:

TRR Checklist and Closure Sheet (Supplier and USAF signatures)

QTP (reflecting prior USAF feedback/input)

Qualification Test Schedule

Risk Management Plan

Test Facilities/Equipment/Resources Assessment

3.4 CDR Test Analysis Reports

The supplier shall deliver the following reports to support CDR; Thermal Analysis Report, Stress Analysis Report, Tolerance Stack-up Report and Failure Mode, Effects and Criticality Analysis Report (FMECA). Separate reports shall be submitted for the E model wheel and brake configuration and for the C/D model wheel and brake configuration. These reports shall be presented and briefed at CDR. (Reference DID DI-NDTI-80809B, Exhibit A005.)

3.5 Antiskid System Performance Evaluation Articles

The supplier shall deliver a total of two (2) C/D model brake assemblies and two (2) E model brake assemblies in accordance with the contract to serve as antiskid system performance evaluation articles. These articles will be used by the Government to perform a hardware-in-the-loop (HITL) antiskid system compliance evaluation. All assemblies shall be qualification equivalent (CDR-approved design) and shall be configurable in both a new condition (i.e. with spacers) and a fully worn condition (i.e. without spacers). These articles may be manufactured from billets.

3.6 On-Aircraft Evaluation Support

The supplier shall support a pre-CDR aircraft fit check utilizing their E model wheel and brake demonstrator equipment developed as part of their proposal. This fit check will be conducted at a date and location to be determined by the Government after contract award. The supplier shall also deliver CDR approved configuration evaluation articles and support on-aircraft evaluation of the wheel and brake equipment as defined below. These articles shall be used to perform an E model and C/D model USAF-managed fit check, TO validation/verification (IAW paragraph 4.5), and system flight test evaluation prior to final system configuration approval. In addition to the evaluation articles, the supplier shall provide bench stock and any required tooling or inspection/support equipment to support these efforts which shall include, as a minimum, the items identified in TRD-SOW (Appendices A and B). The supplier shall also provide technical support as required by the Government for these efforts and the initial Government’s system Performance Tracking Program (PTP) throughout fleet retrofit.

ARTICLE MODEL QUANTITY USE and SPECIAL CONDITIONS

BRAKE ASSEMBLY C/D 25

One (1) each brake assembly* shall support fit check and TO validation/verification. Twenty four (24) each brake assemblies shall support flight test and initial PTP. Ten (10) of the flight test brake articles shall have two (2) center-stator thermocouples installed by the supplier, and marked with “FLT” adjacent to the PN prior to delivery and two (2) each of the instrumented heat stacks shall be machined to a 90% worn condition by the supplier prior to delivery.

WHEEL ASSEMBLY C/D 31

One (1) each wheel assembly* shall support fit check and TO validation/verification. Thirty (30) each wheel assemblies shall support flight test and initial PTP.

ARTICLE MODEL QUANTITY USE and SPECIAL CONDITIONS

BRAKE ASSEMBLY E 25

One (1) each brake assembly* shall support fit check and TO validation/verification. Twenty four (24) each brake assemblies shall support flight test and initial PTP. Ten (10) of the flight test brake articles shall have two (2) center-stator thermocouples installed by the supplier, and marked with “FLT” adjacent to the PN prior to delivery and two (2) each of the instrumented heat stacks shall be machined to a 90% worn condition by the supplier prior to delivery.

WHEEL ASSEMBLY E 31

One (1) each wheel assembly* shall support fit check and TO validation/verification. Thirty (30) each wheel assemblies shall support flight test and initial PTP.

*Although forged items are highly preferred, final fit check and TO validation/verification articles (one complete wheel/brake assembly for E-model and one complete wheel/brake assembly for C/D-model) may be manufactured from billets.

3.7 Vendor Airworthiness Certification Report (VACR)

The suppler shall deliver a VACR that addresses all F-15 Vendor Airworthiness Certification Criteria (VACC) requirements as defined by USAF. The VACR may be formatted in supplier format, but shall be presented in a sequential order that is consistent with each criterion of the VACC document. This report shall document the supplier’s claim that all critical performance requirements have been satisfied through testing/analysis and that both E and C/D model proposed wheel and brake systems have met all airworthiness requirements preparatory for aircraft flight evaluation. (Reference DID DI-NDTI- 80809B, Exhibit A006.)

3.8 Qualification Test Report (QTR)

The supplier shall deliver a comprehensive and complete QTR for a combined E and C/D model test program that demonstrates full compliance with USAF PS (98747) 201228188. The QTR may be provided in supplier format, but shall be presented in a sequential order that is consistent with each paragraph (and sub-paragraph) of the PS. Data that supports qualification by analysis/similarity shall be referenced within the QTR where appropriate. QTR format shall mirror that of the QTP (reference paragraph 3.2). A compliance matrix referencing the applicable paragraphs of the QTP, PS, and this TRD-SOW shall be included. (Reference DID DI-NDTI-80809B, Exhibit A007.)

3.9 Technical Data Package (TDP)

The supplier shall deliver Development Design Drawings/Models for review prior to CDR and present full scale hard copy drawings for further discussion at CDR. Subsequent to CDR, the supplier shall deliver Commercial Drawings/Models for the E model and C/D model wheel and brake assembly along with drawings for any new tooling or inspection equipment identified. All drawings shall be in accordance with (IAW) MIL-STD-31000. Drawings shall be of sufficient detail and information to permit USAF maintenance, modification, engineering analysis, and cataloging of the components with a full description. As a minimum, these component drawings shall also include envelope dimensions, assembly weights, and performance parameters/requirements. Commercial Drawings/Models and associated lists shall include top-level assembly (e.g. wheel assembly, brake assembly), Line Replaceable Unit (LRU) level, Shop Replaceable Unit (SRU) level, and subcomponent (expendable) level. Drawings shall identify/define each component that makes up the assembly and shall include, as a minimum, all subcomponents identified with a base/depot level inspection process/requirement.

(Reference DIDs DI-SESS-81002E, DI-SESS-81003D, DI-SESS-81004D and DI-SESS- 81008D, Exhibits A008 through A011.)

4.0 TECHNICAL ORDERS (TOs)

4.1 Procedural Source Data

The supplier shall deliver Procedural Source Data for the aircraft TOs (system volumes) and field TOs (job guides). The supplier shall submit sample and draft source data deliverables prior to submitting final deliverables in order to verify format and content acceptability and to facilitate formal validation/verification and revision of final products.

4.2 Intermediate, Depot & Illustrated Parts Breakdown Commodity TOs

The supplier shall deliver wheel assembly and brake assembly intermediate, depot and illustrated parts breakdown (IPB) commodity TOs to support intermediate level maintenance and depot overhaul maintenance (twelve volumes total). The subject TOs shall include tool and fixture design drawings required for back shop wheel and brake repair. The commodity TO data shall provide comparable information to existing USAF wheel and brake TOs. The supplier shall submit, as a minimum, the following iterations to ensure final documents are compatible with USAF Automated Technical Order System (ATOS) requirements and include acceptable content. The Government may determine that additional submittals are required based upon supplier quality and content. (Reference TMCR and TM 86-01N, Exhibit A012.)

TO Version Purpose Minimum Submittal Requirements

SAMPLE

To determine format is compatible and acceptable with USAF ATOS and to review proposed content

Sample of either C/D or E model books with sufficient data to allow ATOS assessment for format and system compatibility

DRAFT

To conduct table top review for initial red line changes

Draft versions of all books for both models (C/D and E)

FINAL DRAFT

To support TO val/ver and final red line changes

Updated draft versions of all books for both models (C/D and E) with all USAF requested changes incorporated

FINAL To support flight testing Final versions of all books for both models (C/D and E)

FINAL (Post Flight Test) To incorporate any changes identified during flight testing

Updated final versions (as required)

Under the direction of 417 SCMS, the supplier shall coordinate with designated depot and intermediate-level maintenance personnel to ensure that proposed tooling and fixtures are appropriately designed to interface with existing equipment and processes to the greatest extent possible. The commodity TO data shall include as a minimum, the repairs and instructions listed below in paragraphs 4.2.1 and 4.2.2.

NOTE: Examples of TOs with repairs and requirements requested in paragraphs 4.2.1 and

4.2.2 can be found in TO 4B1-2-1173 and TO 4B1-2-1213 (Main Landing Gear Multiple Disc Brake, F-15C/D and F-15E respectively), and in TO 4W1-1-73 and TO 4W1-6-3 (Main Landing Gear Wheel, F-15C/D and F-15E respectively).

4.2.1 Repair - Wheel Assembly

Depot repairs for the wheel assembly shall include, but are not limited to the areas identified in the following list:

Repair – Wheel Assembly Bearing bore sleeve repairs (0.060 per radius minimum) Drive key bar attachment repair (0.060 per radius minimum)

Structural interface repairs (0.050 material removal minimum)

Wheel retention interface repair (0.050 per radius minimum)

Environmental sealing surface repairs (0.050 material removal minimum)

100% shot peening overhaul procedure

Inflation/over-inflation valve boss repair (oversized, 0.050 per radius minimum)

Oversize insert repair (0.050 per radius minimum)

Main wheel seal glands (oversized, 0.050 per radius minimum)

Heat damage conductivity and hardness criteria

Bearing grease seal glands (oversized, 0.050 per radius minimum)

Damage/removal limits for all structural components (nonfunctional surface blend allowances [0.100 minimum] to be presented/approved during CDR)

Re-plating procedures for all plated components (cadmium-free)

Fuse plug hole repair (oversized, 0.050 per radius minimum)

Note: Minimum/maximum material conditions and allowable damage limits shall be clearly defined by appropriate figures.

4.2.2 Repair - Brake Assembly

Depot repairs for the brake assembly shall include, but are not limited to the areas identified in the following list:

Repair – Brake Assembly

Torque tube hardness limits Re-plating requirements for all plated components

Brake piston housing conductivity and hardness limits

Re-stack procedure for carbon heat stack (including all replacement hardware)

Brake piston housing flange repair Environmental sealing surface repair (adjuster assembly glands and filler bleeder bosses)

Note: Minimum/maximum material conditions and allowable damage limits shall be clearly defined by appropriate figures.

4.3 TO Formatting

The TO data (and future revisions) shall meet the style, format, and content requirements of current wheel and brake USAF TOs. Source data for existing manuals in the form of unnumbered source data changes shall be compatible with the style and formats of existing manuals. (Reference TM-86-01N, Exhibit A012.)

Examples of current C-130 Intermediate, Depot and IPB Commodity TOs in the correct format are as follows:

C-130 TO Examples Maintenance Instructions Intermediate Level Main Wheel Assembly: 4W1-3-1662

Maintenance Instructions Intermediate Level Brake Assembly: 4B1-2-1342

Maintenance Instructions Depot Level Main Wheel Assembly: 4W1-3-1663

Maintenance Instructions Depot Level Main Brake Assembly: 4B1-2-1323

IPB Main Wheel Assembly: 4W1-3-1664 IPB Brake Assembly: 4B1-2-1334

4.4 TO Conferences and Reviews

The supplier shall support TO Conferences prior to and during development of all TO deliverables as deemed necessary by the Government. TO conference meetings will be documented by 417 SCMS with minutes and action items. The supplier shall provide agenda inputs to support these meetings. (Reference DID-ADMN-81249A, Exhibit A002.)

The initial TO Guidance Conference shall be conducted no later than 120 calendar days after contract award. Conferences shall be held at sites to be selected by 417 SCMS. The purpose of the conferences and reviews shall be to establish expectations prior to commencing activities, review preliminary submittals, and approve final submittals. Prior to delivery of documents, the supplier shall incorporate all changes/revisions requested by the Government during conferences and reviews.

4.5 TO Validation/Verification

The supplier shall coordinate and conduct formal TO validation/verification with 417 SCMS for all TO data (base level and depot level) prior to submittal of final TO deliverables. The TO validation and verification shall be held at a site(s) to be selected by USAF. Draft TOs shall be submitted to the 417 SCMS no later than 30 days prior to the event. The supplier shall support all required visits with latest configuration wheel and brake assemblies and all proposed tooling, fixtures, and supplier design unique parts including shipping to and from USAF-defined destinations. USAF requested data changes shall be promptly incorporated and submitted to USAF in support of final approval.

5.0 LOGISTICS

5.1 Field Level Spares/Bench Stock Packages

The supplier shall deliver base level E and C/D model spares/bench stock packages for each F-15 base in accordance with the quantities identified in the contract. Packages shall include parts and any new tooling, fixtures and/or inspection equipment required to support base level operations and maintenance of the new wheel and brake assembly system for an initial two (2) year use period. Packages shall include, as a minimum, the items identified in TRD-SOW Appendix A and Appendix B including any supplier design unique parts, tooling and/or fixtures not specifically identified within these Appendices. The supplier shall utilize Appendix A and Appendix B, and all supplier design unique parts, tooling, fixtures and/or inspection support equipment to develop pricing for the Spares/Bench Stock contract line items. Delivery of these packages shall be a direct shipment from the supplier to each F-15 base. Delivery will be incremental over an estimated 24 month period with the first incremental shipment(s) occurring a minimum one month prior to planned retrofit start. A specific USAF delivery schedule will be provided. Delivery containers shall be marked with a “F-15 WBSI PROGRAM” identification and individual USAF Mark For points of contact as defined by the government prior to shipment.

5.2 Depot Level Inspection Equipment and Tooling Package

The supplier shall ensure that proposed tooling and fixtures are appropriately designed to interface with existing USAF F-15 equipment and processes IAW paragraph 2.5.1. If any new tooling, fixtures and/or equipment is necessary, the supplier shall deliver a package which includes any new tooling, fixtures and/or inspection equipment necessary to support depot level maintenance/overhaul of the new F-15 E model and C/D model wheel assembly and brake assembly.

5.3 Initial Spares Conferences and Reviews

The supplier shall support Initial Spares Conferences prior to and during development of all logistics deliverables as deemed necessary by the Government. The Initial Spares Guidance Conference shall be conducted no later than 120 calendar days after contract award.

Conference meetings will be documented by 417 SCMS with minutes and action items. The supplier shall provide agenda inputs to support these meetings. (Reference DID-ADMN- 81249A, Exhibit A002.)

5.4 Logistics Management Information (LMI)

The supplier shall provide LMI data to support cataloging, projected parts usage, and Government initial spares acquisition for wheel and brake system future sustainment. Format, content and schedule for submitting LMI data shall be determined by the Government at the Initial Spares Guidance Conference which shall be conducted no later than 120 calendar days after contract award. The supplier shall provide agenda inputs to support these meetings.

Reference DID ADMN-81249A, Exhibit A002 and DID DI-ALSS-81529, Exhibit A013.)

5.5 Initial Spare Part Orders

The supplier shall deliver initial investment spare parts (pipeline assets) in support of the F-15 WBSI program. Components and component quantities are listed as sub contract line items to the Initial Investment Spares line item. The supplier shall price these components within their proposal. Final specific components and component part numbers will be determined after CDR based on the Government approved design.

5.6 Wheel and Brake Assembly Static Displays

The supplier shall deliver two (2) E model free-standing wheel and brake assembly static displays to be used for personnel training. Each assembly shall be provided with cutaway areas, including a brake piston assembly, to expose the internal features of the hardware. All surfaces (forged, machined, and sectioned) shall be smoothed/rounded and painted per drawing requirements with a “like-new” appearance, except that the sectioned surfaces shall be highlighted with red paint. Each wheel/brake assembly shall be mounted on a frame/cart that can be readily transported and that allows relative motion between the wheel and brake.

6.0 QUALITY AND SAFETY REQUIREMENTS

6.1 Quality Requirements

The supplier shall maintain a Quality Assurance Plan (QAP) which has been tailored to specifically address the F-15 WBSI program. The QAP shall demonstrate supplier compliance with ANSI/ASQC Q-9002/ISO-9002 standards, or equivalent. Access to the supplier’s Quality Assurance System shall be available to the Contracting Officer for audits/surveys throughout the contract including all options.

6.2 Health Hazard Assessment Report (HHAR)

The supplier shall deliver a HHAR at CDR which synopsizes hazards associated with system operation, maintenance, and repair processes/materials at USAF depot overhaul facilities and operating bases. The report shall include copies of all applicable Material Safety Data Sheets.

These documents shall identify safety and health risks associated with wheel and brake sustainment, including long-term exposure risks. The MSDS documents shall also identify recommended shop practices, procedures, protective equipment, and tools to reduce health and safety risks to shop personnel. (Reference DID DI-SAFT-80106B, Exhibit A014.)

7.0 RETROFIT SUPPORT

7.1 Asset Delivery

The supplier shall deliver final Government approved configuration wheel assemblies and brake assemblies, spares and bench stock IAW the Government’s schedule defined in paragraph 2.1 of this TRD-SOW and the F-15 WBSI contract to accommodate a planned 24 month fleet retrofit. Specific required minimum monthly delivery quantities (by model) are defined in the F-15 WBSI RFP.

7.2 System Performance and Technical Support

The supplier shall also provide support to address any WBSI system performance and/or technical issues identified by the Government during the retrofit period at no additional cost to the Government. This shall include but is not limited to; performance/design deficiency resolution, engineering change notice (ECN) processing, on-site support/assistance and if necessary, parts replacement resulting from equipment design/performance deficiencies.

APPENDIX A – F-15 WBSI C/D MODEL WHEEL AND BRAKE

SPARES/BENCH STOCK PACKAGES

1 2 3 5 6 7

NOMENCLATURE QPA

QTY

PER

ACFT

(2)

BASE LEVEL

Per

Spares/Bench

Stock Package*

TO VAL/VER

Bench Stock

Qty

FLIGHT

TEST

Bench Stock

Qty

WHEEL ASSEMBLY, MLG N/A N/A N/A N/A N/A

1 . VALVE, Inflation 1 2 12 2

2 . . CAP, Valve, Inflation 1 2 24 4

3 . . CORE, Valve Inflation 1 2 24 4

4 . . PACKING, Valve, Inflation 1 2 120 2 10

5 . VALVE, Over-Inflation 1 2 2 2

6 . . PACKING, Valve, Over-Inflation 1 2 120 2 10

7 . RING, Lock 1 2 6

8 . . PLATE, Retainer, Lock Ring 1 2 12

9 . . SCREW, Retainer, Lock Ring 2 4 24

10 . . PIN, Retainer, Lock Ring 2 4 24

11 . . RETAINER, Wire Rope, Lock Ring 1 2 12

12 . PACKING, Assembly, Wheel 1 2 120 2 20

13 . KEY, Rotor Drive 8 16 48

14 . . BOLT, Rotor Drive Key 1 2 24

15 . . RETAINER, Rotor Drive Key 8 16 96

16 . . CLIP, Retainer, Rotor Drive Key 8 16 96

17 . . INSERT, Screw Thread, Rotor Drive Key 8 16 48

18 . SHIELD, Heat 1 2 12

19 . . SCREW, Heat Shield 8 16 96

20 . . INSERT, Screw Thread, Heat Shield 14 28 84

21 . FUSE, Thermal 4 8 480 2 10

22 . . PACKING, Thermal Fuse 4 8 480 2 10

23 . CAN, Bearing 1 2 6 2

24 . . NUT, Bearing Can 1 2 6 2

25 . . RING, Retaining, Nut, Bearing Can 1 2 6 2

26 . CONE AND ROLLERS, Bearing, Outboard 1 2 12 4

27 . . SEAL, Grease, Bearing, Outboard 1 2 120 4

28 . . RING, Retaining, Grease Seal, Outboard 1 2 6 4

29 . CUP, Bearing, Outboard 1 2 12

30 . DAM, Grease, Bearing, Outboard 1 2 12 2

31 . CONE AND ROLLERS, Bearing, Inboard 1 2 12 4

32 . . SEAL, Grease, Bearing, Inboard 1 2 120 4

33 . . RING, Retaining, Grease Seal, Inboard 1 2 6 4

34 . CUP, Bearing, Inboard 1 2 12

35 . DAM, Grease, Bearing, Inboard 1 2 12 2

F-15 C/D Wheel Assembly, MLG

F-15 C/D Wheel & Brake Spares/Bench Stock Package

This list defines the minimum required spares/bench stock to facilitate pricing and delivery for the F-15

WBSI contract. It is based upon the current F-15 C/D model wheel and brake configurations. Final components/configurations will be determined after Critical Design Review (CDR); actual final quantities will be determined during the Initial Spares Conference. Final components/quantities will be a coordinated consensus between the Government and the supplier.

*NOTE: One Base Level Spares/Bench Stock Package Supports 10 Aircraft

1 2 3 5 6 7

NOMENCLATURE QPA

QTY

PER

ACFT

(2)

BASE LEVEL

Per

Spares/Bench

Stock Package*

TO VAL/VER

Bench Stock

Qty

FLIGHT

TEST

Bench Stock

Qty

BRAKE ASSEMBLY N/A N/A N/A N/A N/A

1 . BOLT, Housing to Torque Tube Attachment 5 10 4 20

2 . WASHER, Housing to Torque Tube Attachment 5 10 4 20

3 . WEAR PIN ASSEMBLY 1 2 4

4 . . PIN, Wear Indicator 1 2 1

5 . . WASHER, Pin, Wear Indicator 1 2 1

6 . . SPRING, Pin, Wear Indicator 1 2 1

. SHUTTLE VALVE ASSEMBLY N/A N/A N/A N/A N/A

7 . . BOLT, Valve, Shuttle 2 4 1 4

8 . . WASHER, Valve, Shuttle 2 4 1 4

9 . . PACKING, Valve, Shuttle (Inlet) 2 4 8 4 4

10 . . CAP, Protective, Valve, Shuttle 2 4 4 4

11 . . PACKING, Valve, Shuttle (Outlet) 1 2 4 2 2

12 . . RETAINER, Packing, Valve, Shuttle 1 2 1 2 2

13 . BLEEDER ASSEMBLY 1 2 8

14 . . HOUSING, Bleeder Valve 1 2 1 2

15 . . PACKING, Housing, Bleeder Valve 1 2 1 2 2

16 . . RETAINER, Packing, Housing, Bleeder Valve 1 2 1 2 2

17 . . BOLT, Bleeder Valve 2 4 1 4

18 . . WASHER, Bleeder Valve 2 4 1 4

19 . . VALVE, Bleeder 1 2 1 2

20 . . PACKING, Bleeder Valve 1 2 1 2 2

21 . . ADAPTER, Bleeder Valve 1 2 1 2

22 . . PACKING, Adapter, Bleeder Valve 1 2 1 2 2

23 . . CAP, Valve, Bleeder 1 2 1 2

24 . . INSERT, Screw Thread, Shuttle/Bleeder Mounting 4 8 3

25 . . INSERT, Screw thread (1st oversize) 1 1 1

. PISTON ASSEMBLY N/A N/A N/A N/A N/A

26 . . COVER, Piston 5 10 2 2

27 . . INSULATOR, Piston 5 10 2 2

28 . . SCREW, Set, Piston 5 10 2 2

29 . . PISTON AND BUSHING ASSEMBLY 5 10 4 2

30 . . . RETAINER, Cover 1 2 4

31 . . . NUT, Self-Locking 1 2 4

32 . . . TUBE, Adjuster 1 2 4

33 . . . PIN, Adjuster 1 2 4

34 . . . RETAINER, Pin 1 2 4

35 . . . PISTON 1 2 4

36 . . . PACKING, Preformed 1 2 4 2

37 . . . RETAINER, Packing 1 2 4 2

38 . . . PACKING, Preformed 1 2 4 2

39 . . . RETAINER, Packing 1 2 4 2

40 . . . BUSHING, Machine Thread 1 2 4

41 . . . WIPER, Piston 1 2 4

42 . . . RING, Retaining, Internal 1 2 4

43 . . . HOUSING, Adjuster 1 2 4

44 . . . SPRING, Compression, Helical 1 2 4

45 . . . HOLDER, Spring 1 2 4

46 . . . PACKING, Preformed 1 2 4 2

47 . . . RETAINER, Packing 1 2 4 2

. HEAT, Stack N/A N/A N/A N/A N/A

. . STATOR, Assembly (Pressure Plate) N/A N/A N/A N/A N/A

48 . . . RIVET, Tubular 10 20 4

49 . . . CAP, Protective, Stator 10 20 4

. . ROTOR ASSEMBLY N/A N/A N/A N/A N/A

50 . . . WASHER, Flat 80 160 26

51 . . . RIVET, Tubular 80 160 26

52 . . . CAP, Protective, Rotor 40 80 13

F-15 C/D Brake Assembly, MLG

QTY

PER

ACFT

(2)

BASE LEVEL

Per

Spares/Bench

Stock Package*

TO VAL/VER

Bench Stock

Qty

FLIGHT

TEST

Bench Stock

Qty

53 . . . INSERT, Rotor 40 80 13

. . STATOR ASSEMBLY N/A N/A N/A N/A N/A

54 . . . RIVET, Tubular 40 80 12

55 . . . CAP, Protective, Stator 40 80 12

. . STATOR ASSEMBLY (Backing Plate) N/A N/A N/A N/A N/A

56 . . . RIVET, Tubular 10 20 4

57 . . . CAP, Protective, Stator 10 20 4

58 . . SHIELD, Auxiliary Stator 1 2 1

. TUBE ASSEMBLY, Stator Torque N/A N/A N/A N/A N/A

59 . . BUSHING, Aircraft Attachment Hole 4 8 3

60 . . CAP, Drive Spline 10 20 8

61 . . RIVET, Semitubular, Drive Spline 10 20 8

62 . . PAD, Backing 10 20 8

63 . . SPACER, Backing Pad 10 20 8

64 . . WASHER, Backing Pad 10 20 8

65 . . RIVET, Backing Pad 10 20 8

66 . . INSERT, Screw Thread, Housing Attachment 5 10 4

67 . . INDICATOR ASSEMBLY, Axle Overtemp 1 2 2

68 . . . FUSE, Thermal, Axle Overtemp Assy 1 2 1

69 . . . PIN, Spring, Axle Overtemp Assy 1 2 1

70 . . . RETAINER, Thermal fuse, Axle Overtemp Assy 1 2 1

71 . . . RIVET, Tubular, Axle Overtemp Assy 2 4 3

**SUPPLIER DESIGN UNIQUE PART(S)/

TOOLING/FIXTURES/SUPPORT EQUIPMENT

TBD TBD TBD TBD TBD

** The supplier shall also identify any wheel and/or brake design unique part(s) which are not listed above. The supplier shall provide the QPA (Quantity Per Assembly), QUANTITY PER ACFT, the supplier's Estimated End Item

Failure/Replacement % (based on a 24 month period) and the supplier's Projected Bench Stock Quantity for each part listed. Final quantities will be determined during the Initial Spares Conference and will be a coordinated consensus between the Government and the supplier. The supplier shall include costs for all projected initial spare part quantities identified by the Government and the supplier under the Request for Proposal/contract Spares/Bench Stock contract line item.

F-15 C/D Brake Assembly, MLG (continued)

F-15 C/D Wheel & Brake Assembly, MLG

APPENDIX B – F-15 WBSI E MODEL WHEEL AND BRAKE

SPARES/BENCH STOCK PACKAGES

1 2 3 5 6 7

NOMENCLATURE QPA

QTY

PER

ACFT

(2)

BASE LEVEL

Per Spares/

Bench Stock

Package*

TO

VAL/VER

Bench

Stock Qty

FLIGHT

TEST

Bench Stock

Qty

WHEEL ASSEMBLY, MLG N/A N/A N/A N/A N/A

1 . VALVE, Inflation 1 2 12 2

2 . . CAP, Valve, Inflation 1 2 24 4

3 . . CORE, Valve Inflation 1 2 24 4

4 . . PACKING, Valve, Inflation 1 2 120 2 10

5 . VALVE, Over-Inflation 1 2 2 2

6 . . PACKING, Valve, Over-Inflation 1 2 120 2 10

7 . RING, Lock 1 2 6

8 . . PLATE, Retainer, Lock Ring 1 2 12

9 . . SCREW, Retainer, Lock Ring 2 4 24

10 . . PIN, Retainer, Lock Ring 2 4 24

11 . . RETAINER, Wire Rope, Lock Ring 1 2 12

12 . PACKING, Assembly, Wheel 1 2 120 2 20

13 . KEY, Rotor Drive 8 16 48

14 . . BOLT, Rotor Drive Key 1 2 24

15 . . RETAINER, Rotor Drive Key 8 16 96

16 . . CLIP, Retainer, Rotor Drive Key 8 16 96

17 . . INSERT, Screw Thread, Rotor Drive Key 8 16 48

18 . SHIELD, Heat 1 2 12

19 . . SCREW, Heat Shield 8 16 96

20 . . INSERT, Screw Thread, Heat Shield 14 28 84

21 . FUSE, Thermal 4 8 480 2 10

22 . . PACKING, Thermal Fuse 4 8 480 2 10

23 . CAN, Bearing 1 2 6 2

24 . . NUT, Bearing Can 1 2 6 2

25 . . RING, Retaining, Nut, Bearing Can 1 2 6 2

26 . CONE AND ROLLERS, Bearing, Outboard 1 2 12 4

27 . . SEAL, Grease, Bearing, Outboard 1 2 120 4

28 . . RING, Retaining, Grease Seal, Outboard 1 2 6 4

29 . CUP, Bearing, Outboard 1 2 12

30 . DAM, Grease, Bearing, Outboard 1 2 12 2

31 . CONE AND ROLLERS, Bearing, Inboard 1 2 12 4

32 . . SEAL, Grease, Bearing, Inboard 1 2 120 4

33 . . RING, Retaining, Grease Seal, Inboard 1 2 6 4

34 . CUP, Bearing, Inboard 1 2 12

35 . DAM, Grease, Bearing, Inboard 1 2 12 2

F-15 E Wheel Assembly, MLG

F-15 E Wheel & Brake Spares/Bench Stock Package

This list defines the minimum required spares/bench stock to facilitate pricing and delivery for the F-15

WBSI contract. It is based upon the current F-15 E model wheel and brake configurations. Final components/configurations will be determined after Critical Design Review (CDR); actual final quantities will be determined during the Initial Spares Conference. Final components/quantities will be a coordinated consensus between the Government and the supplier.

*NOTE: One Base Level Spares/Bench Stock Package Supports 10 Aircraft

QTY

PER

ACFT

(2)

BASE LEVEL

Per Spares/

Bench Stock

Package*

TO

VAL/VER

Bench

Stock Qty

FLIGHT

TEST

Bench

Stock Qty

BRAKE ASSEMBLY N/A N/A N/A N/A N/A

1 . BOLT, Housing to Torque Tube Attachment 5 10 4 20

2 . WASHER, Housing to Torque Tube Attachment 5 10 4 20

3 . WEAR PIN ASSEMBLY 1 2 4

4 . . PIN, Wear Indicator 1 2 1

5 . . WASHER, Pin, Wear Indicator 1 2 1

6 . . SPRING, Pin, Wear Indicator 1 2 1

. SHUTTLE VALVE ASSEMBLY N/A N/A N/A N/A N/A

7 . . BOLT, Valve, Shuttle 2 4 1 4

8 . . WASHER, Valve, Shuttle 2 4 1 4

9 . . PACKING, Valve, Shuttle (Inlet) 2 4 8 4 4

10 . . CAP, Protective, Valve, Shuttle 2 4 4 4

11 . . PACKING, Valve, Shuttle (Outlet) 1 2 4 2 2

12 . . RETAINER, Packing, Valve, Shuttle 1 2 1 2 2

13 . BLEEDER ASSEMBLY 1 2 8

14 . . HOUSING, Bleeder Valve 1 2 1 2

15 . . PACKING, Housing, Bleeder Valve 1 2 1 2 2

16 . . RETAINER, Packing, Housing, Bleeder Valve 1 2 1 2 2

17 . . BOLT, Bleeder Valve 2 4 1 4

18 . . WASHER, Bleeder Valve 2 4 1 4

19 . . VALVE, Bleeder 1 2 1 2

20 . . PACKING, Bleeder Valve 1 2 1 2 2

21 . . ADAPTER, Bleeder Valve 1 2 1 2

22 . . PACKING, Adapter, Bleeder Valve 1 2 1 2 2

23 . . CAP, Valve, Bleeder 1 2 1 2

24 . . INSERT, Screw Thread, Shuttle/Bleeder Mounting 4 8 3

25 . . INSERT, Screw thread (1st oversize) 1 1 1

. PISTON ASSEMBLY N/A N/A N/A N/A N/A

26 . . COVER, Piston 5 10 2 2

27 . . INSULATOR, Piston 5 10 2 2

28 . . SCREW, Set, Piston 5 10 2 2

29 . . PISTON AND BUSHING ASSEMBLY 5 10 4 2

30 . . . RETAINER, Cover 1 2 4

31 . . . NUT, Self-Locking 1 2 4

32 . . . TUBE, Adjuster 1 2 4

33 . . . PIN, Adjuster 1 2 4

34 . . . RETAINER, Pin 1 2 4

35 . . . PISTON 1 2 4

36 . . . PACKING, Preformed 1 2 4 2

37 . . . RETAINER, Packing 1 2 4 2

38 . . . PACKING, Preformed 1 2 4 2

39 . . . RETAINER, Packing 1 2 4 2

40 . . . BUSHING, Machine Thread 1 2 4

41 . . . WIPER, Piston 1 2 4

42 . . . RING, Retaining, Internal 1 2 4

43 . . . HOUSING, Adjuster 1 2 4

44 . . . SPRING, Compression, Helical 1 2 4

45 . . . HOLDER, Spring 1 2 4

46 . . . PACKING, Preformed 1 2 4 2

47 . . . RETAINER, Packing 1 2 4 2

. HEAT, Stack N/A N/A N/A N/A N/A

. . STATOR, Assembly (Pressure Plate) N/A N/A N/A N/A N/A

48 . . . RIVET, Tubular 10 20 4

49 . . . CAP, Protective, Stator 10 20 4

. . ROTOR ASSEMBLY N/A N/A N/A N/A N/A

50 . . . WASHER, Flat 80 160 32

F-15 E Brake Assembly, MLG

QTY

PER

ACFT

(2)

BASE LEVEL

Per Spares/

Bench Stock

Package*

TO

VAL/VER

Bench

Stock Qty

FLIGHT

TEST

Bench

Stock Qty

51 . . . RIVET, Tubular 80 160 32

52 . . . CAP, Protective, Rotor 40 80 16

53 . . . INSERT, Rotor 40 80 16

. . STATOR ASSEMBLY N/A N/A N/A N/A N/A

54 . . . RIVET, Tubular 40 80 16

55 . . . CAP, Protective, Stator 40 80 16

. . STATOR ASSEMBLY (Backing Plate) N/A N/A N/A N/A N/A

56 . . . RIVET, Tubular 10 20 4

57 . . . CAP, Protective, Stator 10 20 4

58 . . SHIELD, Auxiliary Stator 1 2 1

. TUBE ASSEMBLY, Stator Torque N/A N/A N/A N/A N/A

59 . . BUSHING, Aircraft Attachment Hole 4 8 3

60 . . CAP, Drive Spline 10 20 8

61 . . RIVET, Semitubular, Drive Spline 10 20 8

62 . . PAD, Backing 10 20 8

63 . . SPACER, Backing Pad 10 20 8

64 . . WASHER, Backing Pad 10 20 8

65 . . RIVET, Backing Pad 10 20 8

66 . . INSERT, Screw Thread, Housing Attachment 5 10 4

67 . . INDICATOR ASSEMBLY, Axle Overtemp 1 2 2

68 . . . FUSE, Thermal, Axle Overtemp Assy 1 2 1

69 . . . PIN, Spring, Axle Overtemp Assy 1 2 1

70 . . . RETAINER, Thermal fuse, Axle Overtemp Assy 1 2 1

71 . . . RIVET, Tubular, Axle Overtemp Assy 2 4 3

**SUPPLIER DESIGN UNIQUE PART(S)/

TOOLING/FIXTURES/SUPPORT EQUIPMENT

TBD TBD TBD TBD TBD

** The supplier shall also identify any wheel and/or brake design unique part(s) which are not listed above. The supplier shall provide the QPA (Quantity Per Assembly), QUANTITY PER ACFT, the supplier's Estimated End Item

Failure/Replacement % (based on a 24 month period) and the supplier's Projected Bench Stock Quantity for each part listed. Final quantities will be determined during the Initial Spares Conference and will be a coordinated consensus between the Government and the supplier. The supplier shall include costs for all projected initial spare part quantities identified by the Government and the supplier under the Request for Proposal/contract Spares/Bench

Stock contract line item.

F-15 E Brake Assembly, MLG (continued)

F-15 E Wheel & Brake Assembly, MLG