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F35项目风险管理

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MOOG AIRCRAFT GROUP RISK MANAGEMENT PLAN (SDRL J0724) FOR THE F-35 WING FOLD ACTUATION SYSTEM This document contains information which is the property of Moog Inc. This document may not, in whole or in part, be duplicated, disclosed, or used for design or manufacturing purposes without prior written permission of Moog Inc. BY CHECK ENGR. B. NGUYEN J. HADFIELD B. NGUYEN REV - A B EO UTA101296: PROPOSED REVISIONS DESCRIPTION DATE 2/17/03 10/05/04 APPROVED PROG. J. HADFIELD UPDATED WITH LM COMMENTS UPDATED WITH UPDATED RISKS MOOG MOOG INC. TORRANCE, CA 90501 CAGE CODE 0ZWK8 PAGE 1 OF 56 MRE13419

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TABLE OF CONTENTS

Section Description Page 1. INTRODUCTION ...................................................................................................... 3 2. APPLICABLE DOCUMENTS ................................................................................... 3 3. APPROACH ............................................................................................................. 4 3.1 Risk Structure ....................................................................................................... 4 3.2 Worry/Risk List ..................................................................................................... 4 3.3 Risk Scoring ......................................................................................................... 4 3.4 Risk Workbooks .................................................................................................... 5 3.5 Risk Mitigation Work Packages ............................................................................ 5 3.6 Reviews ................................................................................................................ 5 3.7 Roles And Responsibilities ................................................................................... 6 3.8 New Risks............................................................................................................. 7 3.9 Deleting Risks ....................................................................................................... 7 3.10 Status Reporting ............................................................................................... 8 3.11 Configuration Management ............................................................................... 8 4. SUPPLIER RISK MANAGEMENT ........................................................................... 8 5. PROCESS AND TOOLS .......................................................................................... 9 5.1 Microsoft Excel ..................................................................................................... 9 5.2 Microsoft Project ................................................................................................... 9

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1. INTRODUCTION This document outlines the Risk Management Plan for the F-35 Wing Fold Actuation System (WFAS) to be carried out by the Moog. The requirements for this plan and its execution are identified in paragraph 1345.1.7 of the contract Statement of Work and SDRL J0724. The principles and methods of Moog Risk Management Plan are consistent with Lockheed Martin's Risk Management Plan for the Joint Strike Fighter 2YZA00042-0001 dated April 2002.

This plan is intended is to define the processes to be used by the Moog team to 1) recognize and identify its program risks, 2) incrementally reduce these risks through defined mitigation steps, 3) report on the progress of each risk’s mitigation plan in a unified and consistent manner, and 4) internally manage and track each of the risks. The methods outlined herein also provide visibility to BAE Systems/Lockheed Martin and are compatible with Active Risk Manager (ARM), Lockheed Martin’s principle risk management tool for the JSF program. 2.

APPLICABLE DOCUMENTS The following BAE Systems/Lockheed Martin documents serve as guides to the Moog to carry out this plan and are mainly for reference only. Those that establish requirements are noted in the body of this plan.

? Statement of Work for the JSF Wing Fold Actuation System, 2WHA00001-0001 dated July 2002 ? Supplier Data Requirement J0724, Risk Management Plan and Status

Reports ? Risk Management Plan, Document 2YZA00042-0001, dated April 2002 ? Supplier Risk Management Guide for the JSF Program, dated 31 January

1999

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3. 3.1

APPROACH Risk Structure

The Moog team received training in the JSF Risk Process in August 2002 from the Lockheed Martin LEFAS Risk Management Team. The same process and techniques were used to evaluate the WFAS system for potential worries. The Risk Structure will be reviewed every six months and screened for new worries. The baseline Risk Structure is included as Appendix C.

The Risk Structure includes all areas of the WFAS System, the Management of the Program, Resources to carry out the Program, as well as all areas of interface with BAE Systems/Lockheed Martin.

Thus the Team has designated five categories into which all WFAS identified risk issues will fall:

? Auto logistics Risks : These are risks which are related to inservice

maintainability and supportability ? Integration Risks: These are risks that apply to the electrical or mechanical integration and whose resolution could affect all or some of its LRCs. ? Component Risks: These risks apply only to the design of the individual

components within the WFAS system. ? Test Risks: These are risks that are associated with the Team’s ability to

carry out tests in support of the program. ? Programmatic Risks: These are programmatic risks that do not fall in any of the aforementioned technical categories. Examples might include personnel, schedule, affordability, facilities, or process issues.

3.2 Worry/Risk List

The Baseline Worry List is included as Appendix A. A group brainstorming activity, using the risk structure noted in Section 3.1, was used to develop the list of 10 worries. The team then voted on the items in the list and selected the top 7 items for risk scoring, which includes the weight risk. The weight risk will be addresses by a list of weight reduction initiatives and weight reduction plan status. 3.3

Risk Scoring

The Moog team utilized Lockheed Martin’s process of assessing the level of each risk, as outlined in Lockheed Martin’s Supplier Risk Management Guide and the Risk Management Workshop. Risk Templates (tailored for the WFAS) were used as criteria

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MOOG AIRCRAFT GROUP RISK MANAGEMENT PLAN (SDRL J0724) FOR THE F-35 WING FOLD ACTUATION SYSTEM This document contains information which is the property of Moog Inc. This document may not, in whole or in part, be duplicated, disclosed, or used for design or manufacturing purposes without prior written permission of Moog Inc. BY CHECK ENGR. B. NGUYEN J. HADFIELD B. NGUYEN REV - A B

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