Title: FSIP LC Quarterly Brief, 12 Dec 01
1CORAL REACH FSIP
The C/KC-135 Aging Aircraft Program
FSIP PROGRAM OVERVIEW
3 - 6 NOVEMBER 2003
2OBJECTIVES
- Introduce CORAL REACH
- Understand the FSIP Process
- Understand Identifying and Mitigating Findings
3AGENDA
- CORAL REACH
- FSIP GENESIS
- FSIP PURPOSE
- FSIP PROCESS
- FSIP ORGANIZATION
- PROJECT PLANNING STATUS
- FINDINGS
- SUMMARY
4CORAL REACH
PROGRAM DESCRIPTION
- The Coral Reach IPT Purpose is to manage all
aging aircraft activities under one umbrella - The Goal of the Coral Reach IPT is to identify
actions required to ensure a logical,
comprehensive, and proactive aging aircraft
program that will sustain the KC-135 until
retirement - Three Objectives - Program Metrics - were
established for Coral Reach - Maintain an acceptable Margin of Safety
- Minimize the Cost of Ownership
- Improve Aircraft Availability
5CORAL REACH
PROGRAM DESCRIPTION (cont.)
- Aircraft Strategic Master Plan - ASMP
- Strategic Guide for Investment, Repair, and
Modification - Detailed Action Plans Responsive to the Air
Mobility Master Plan - Aging Aircraft Issues - Program Metrics
- Structural Margin of Safety
- Systems Margin of Safety
- Aircraft Availability
- Cost of Ownership/Cost per flying hour
- Drivers noted from each Program Metric
- Lists combined, prioritized coordinated
- Engineering Assignments (EA) identified and
work begins
6FSIP - GENESIS
- Fuel Pump Accidents
- KC-135, C-141
- AMC/CC - Whats my next fuel pump
- Initial Activities
- HQ AMC
- SAF/AQ Involvement
- POM initiative intended
- Airplane generic - a goal
- Address safety and durability objectives
- Interest waned support did not materialize
- -135 Board of Directors validated need for -135
FSIP - OC-ALC/LC moved to develop a generic FSIP process
7FSIP - GENESIS
- SPD Established Coral Reach Direction
- Be Proactive
- Pursued FSIP as -135 specific effort
- Report findings through Aircraft Strategic
Master Plan (ASMP) - Boeing placed on EA to develop FSIP process
- Use Logic of Other Integrity Programs
- Ensure safety of flight - aircrew and aircraft
- Ensure suitability and effectiveness of aircraft
functional systems - Boeing delivered FSIP model for validation and
verification in Dec 1995 - Focus on aging aspects of Functional Systems
- Reach beyond original intended period of system
usage - Supplement existing programs - ASIP, ENSIP, RM
and RCM
8FSIP GENESIS
- Purpose of FSIP is to PROACTIVELY
- Ensure Operational
- Safety Suitability and
- Effectiveness of Aircraft
- Functional Systems
- Protect the Aircrew and Aircraft
- Ensure the system operates in its environment and
performs its intended missions
9FSIP - THE PROCESS
MODEL OBJECTIVES
- Identify Reduced Safety Margins
- Identify Durability Issues
- Systematic review of all systems/subsystems/functi
ons. - Institute systems approach to safety,
durability and economic life - Develop a multi-task process for decision
milestones - Reduce the at risk nature of an aging fleet
priorities - Enhance aircraft availability
- Support cost containment
- Develop and maintain a Functional Systems Health
Care Plan
10FSIP - THE PROCESS
FSIP performs a system-by-system review.
A disciplined approach using a multi-task
checklist process
11FSIP - THE PROCESS MULTI-TASK, DISCIPLINED
CHECKLISTS
12FSIP - THE PROCESS MULTI-TASK, DISCIPLINED
CHECKLISTS
- TASK A
- PROJECT INITIATION
- ASSESS/ESTABLISH SYSTEM BASELINE
- ASSESS SYSTEM PERFORMANCE AND USAGE HISTORY
- ASSESS AVAILABLE SAFETY DATA
- ASSESS REQUIREMENTS VS PERFORMANCE
- CONDUCT INITIAL RECORDS AND DATA REVIEW
- DEVELOP AND EXECUTE A USER CONTACT PLAN
- CONSOLIDATE AND WRITE UP FINDINGS
13FSIP - THE PROCESS MULTI-TASK, DISCIPLINED
CHECKLISTS
- TASK B
- CONDUCT CRITICAL SYSTEM SAFETY ANALYSIS
- CONDUCT DETAILED RECORDS/DATA REVIEW
- ASSESS CHANGES SINCE ORIGINAL DESIGN
- GATHER USER/PDM/OH FEEDBACK
- CONDUCT DETAILED SYSTEM/COMPONENT ANALYSIS
- ASSESS SUPPORTABILITY AND AVAILABILITY
- CONSOLIDATE AND WRITE UP FINDINGS
14FSIP - THE PROCESS MULTI-TASK, DISCIPLINED
CHECKLISTS
- TASK C
- EVALUATE CANDIDATE SOLUTION (s)
- DEVELOP SOLUTION
- FINALIZE SOLUTION
- DEVELOP ROM COST AND SCHEDULE
15FSIP - THE PROCESS MULTI-TASK, DISCIPLINED
CHECKLISTS
- TASK D
- FORM IMPLEMENTATION AND PLANNING IPT
- SOLUTION DESIGN
- SOLUTION IMPLEMENTATION
16FSIP - THE PROCESS MULTI-TASK, DISCIPLINED
CHECKLISTS
- TASK E
- SOLUTION PERFORMANCE EVALUATION
- SAFETY AND DURABILITY WATCH
- DATA COLLECTION
- FEEDBACK
- LONG TERM HEALTH MONITORING (LTHMS)
17FSIP - The Process - Task E
- Task E is System Health Monitoring
- Monitor performance of implemented Task D
solutions (Did it fix the problem) - Continued safety and durability watch
- Items of concern
- Periodic re-look of Task A/B results
- Data collection and analysis
- Continual feedback
- Sustains vigilant proactive search
- "It is expected that Air Force personnel will
periodically re-evaluate the SSI's and intervals
with the benefit of accumulated data From
D3-11100-5, MSG-II procedures manual - Long Term Health Monitoring System - LTHMS
18FSIP - The Process - Task E
- LTHMS
- Automated data mining
- A means to monitor all GO/DO maintenance data
systems - Provide user with reports, email, cues, etc.
based on - Passing a threshold of maintenance activity
- Parts demand/availability
- MTB? (REMIS, GO50, etc) by SN/PN
- Flexible query and conversational interface
capability
19PROJECT PLANNING GO-50 HOWS (Health of the Weapon
System) REPORT, PLUS .....
20FSIP STATUS - Current Task A/B Priority
TIGER TEAM PRIORITIZATION MEETINGS HELD April
96 May 97 Nov 98 Dec 99 Oct 01 Dec 02
- Sustainment Phase (TASK E) commencement
initiated
21FSIP STATUS
FSIP Project Planning - Task A B - to date
- Attempting to accelerate initial Task A/B effort
to COB 05
6
97
98
99
00
01
02
03
04
05
06
Task Name
3
4
1
2
3
4
1
2
3
4
1
2
3
4
1
2
3
4
1
2
3
4
1
2
3
4
1
2
3
4
1
2
3
4
1
2
3
4
1
2
3
4
Landing
Gear
Fuel
Systems
Flight
Controls
Autopilot
Hydraulics/Pneudraulics
Air
Cond,
Pressure,
Ice
Control
Electrical
Components
Instruments,
Radar
Nav,
Interphone
NOTIONAL
Engine(Non-ENSIP),
Turbojet/Turbofan
Power
Plant,
Aux
Power
Plant
NOTIONAL
Cockpit
Fuselage
Compartment,
Airframe(Non-ASIP)
22FSIP FINDINGS
- FINDINGS are the primary Task A B product to
- Document findings
- Track progress
- Record closure
- Mitigation takes many forms
From Tasks A B SF- SAFETY FINDINGS DF -
DURABILITY FINDINGS MF - MISC. FINDINGS
- Three categories documented and tracked
- SFs - items having safety impact
- DFs - items not of an immediate safety impact
- MFs - items not related to safety or durability
23FSIP FINDINGS
- Findings are prioritized by Hazard Risk
Assessments per MIL-STD-882D
Overall priority
1
24FSIP FINDINGS
HIGHLIGHTS
- Tech Data
- Improper/outdated overhaul manuals
- Update ISO inspections criteria
- No wear and rework limits
- Tech data needs clarification
- Unincorporated Improvements
- Airworthiness Directives
- Service Bulletins
25FSIP FINDINGS
HIGHLIGHTS
- Maintenance
- Specification/requirements changes
- No, or improper lubrication
- Reevaluate time replacement items
- Identify one-time replacement items
- Component Overhaul
- Trends not visible at the systems level
- Major parts now wearing beyond tolerances
- Piece part availability
- Insufficient communication with end user
- Vanishing Vendors
26SUMMARY
- Aging Systems need attention
- FSIP is currently in the Safety Phase
- Aging/Durability Sustainment Phase follows
- Coral Reach/FSIP Program
- Program Manager - Diane Kirts, OC-ALC/LCM
- IPT Co-Chair Lt Eric Reagan, OC-ALC/LCRM
- IPT Co-Chair - Ralph Ward, Boeing
- FSIPs goals are to PROACTIVELY
- Ensure Operational Safety,
- Suitability, and Effectiveness
27BACK UP SLIDES
28SAMPLE TASK CHECKLIST
29SAMPLE TASK CHECKLIST
30SAMPLE TASK CHECKLIST
31SAMPLE TASK CHECKLIST
32 33SAMPLE TASK CHECKLIST
34SAMPLE TASK CHECKLIST
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