the significance of rcm2 applied to the ch-47d, chinook presented by nancy regan, the force, inc

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The Significance of RCM2 The Significance of RCM2 applied to the CH-47D, applied to the CH-47D, Chinook Chinook Presented by Nancy Presented by Nancy Regan, The Force, Regan, The Force, Inc. Inc.

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Page 1: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

The Significance of RCM2 applied to The Significance of RCM2 applied to the CH-47D, Chinookthe CH-47D, Chinook

Presented by Nancy Regan, Presented by Nancy Regan, The Force, Inc.The Force, Inc.

Page 2: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

• CH-47D, Chinook

• RCM Process

• Systems Analyzed

• RCM Results and Benefits

• Summary

AgendaAgenda

Page 3: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc
Page 4: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

RCMRCM

Page 5: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

The Traditional View of FailureThe Traditional View of Failure

CONDITIONAL

PROBABILITY

OF FAILURE

AGE

Wear-Out

Zone

Low Level of Random Failure

1955: Commercial Airline Industry

Early 1960s: Crash rate ~ 60 crashes/million takeoffs

67% of crashes due to component failure

Philosophy: As equipment gets older, it’s more likely to fail.

85% aircraft components scheduled for overhaul or replacement

Action taken to decrease crash-rate:

Reduced overhaul/replacement intervals Crash rate increased

Page 6: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

Bath Tub curve A

Slowly increasing failure rate, then wear out zone B

Steady increase in probability of failure

C

Low when new, then increases to steady failure rate

D

Random E

Infant mortality, then random F

Six Patterns of FailureSix Patterns of Failure

14%

68%

7%Complex equipment. Ex. Electronics, Hydraulics, Pneumatics

4%

2%

5%

Simple or complex items that have direct contact with product. Ex. Tires, Brake Pads, Pumps

Stanley Nowlan and Howard Heap: Engineers, United Airlines

Page 7: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

A process used to determine what must be done to insure that any physical asset

continues to do what its users want it to do in its present operating context.

Reliability Centered Reliability Centered Maintenance 2Maintenance 2

Page 8: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

…During the return leg of a combat re-supply mission, my crew and I were in level flight (8500' PA, 32 degrees C) with an Apache (AH-64A), when we had a cockpit indication of a #2 engine chip. We executed the emergency procedure, shutdown the #2 engine, and turned for a direct route to Bagram A.B. Afghanistan. We notified the Apache of the situation and told them that we were going to start a "cruise climb" to clear the last two mountain ranges between us and the airfield. We made the decision that a precautionary landing would not be prudent due to the mine threat in the area.

Now we are single-engine, with 7 passengers, in an extreme "Hot/High" environment and still managing a 550 FPM climb well within our 30 minute temperature limits. I am guessing that it was just a couple of minutes when the Apache called and asked how high we were planning to go since they were already approaching their engine temperature limits. I said that I was at 10,300' and was planning on going to 11,000' since there were 10,500' mountains between us and the airfield. The Apache pilot asked if we had started our second engine again to climb, and I replied in the negative. The Apache pilot said that he would just "stay down here" and keep an eye on us since he was "temping out" his engines.

After leveling off at 11,000' and 105 KIAS the Apache asked if we could slow down 10 knots since we were pulling away from him. He again asked if we were still single-engine. We, the "fast-movers," were vectored away and we completed the flight to a roll-on landing at Bagram. We checked the chip detector after shut down and it turned out to be "normal fuzz" there ending an eventful flight where nothing was damaged except the Apache's self-esteem.

Page 9: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

1. What are its functions and associated performance standards?

2. In what ways can it fail?

3. What causes it to fail?

4. What happens when it fails?

5. Does it matter if it fails?

6. What can be done to predict or prevent each failure?

7. What do we do if we cannot prevent the failure?

To Develop Justified Maintenance Requirements, the RCM Review Group Answers Seven Questions:

RCM2 ProcessRCM2 Process

Page 10: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

1. What are its functions and associated performance standards?

2. In what ways can it fail?

3. What causes it to fail?

4. What happens when it fails?

5. Does it matter if it fails?

6. What can be done to predict or prevent each failure?

7. What do we do if we cannot prevent the failure?

FMEA(Failure Modes Effects Analysis)

Questions 3-4:

RCM2 ProcessRCM2 Process

Page 11: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

Hidden Operational

Safety/Environmental Non-Operational

Question 5: CONSEQUENCE ASSESSMENTCONSEQUENCE ASSESSMENT

RCM2 ProcessRCM2 Process1. What are its functions and associated performance standards?

2. In what ways can it fail?

3. What causes it to fail?

4. What happens when it fails?

5. Does it matter if it fails?

6. What can be done to predict or prevent each failure?

7. What do we do if we cannot prevent the failure?

Page 12: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

RCM2 ProcessRCM2 Process1. What are its functions and associated performance standards?

2. In what ways can it fail?

3. What causes it to fail?

4. What happens when it fails?

5. Does it matter if it fails?

6. What can be done to predict or prevent each failure?

7. What do we do if we cannot prevent the failure?

On-Condition Tasks Predictive Maintenance

Application of Condition Based Maintenance (CBM)

TBO Items

Retirement Life Items

Question 6: PROACTIVE TASKSPROACTIVE TASKS

Preventive Maintenance

Page 13: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

RCM2 ProcessRCM2 Process

Question 7: DEFAULT ACTIONSDEFAULT ACTIONSFailure Finding Task

Check if the item is in a failed state.

One-time change

Physical equipment modification, change in Training, Supply, or Equipment Operating Procedure, Correction/update to Technical Publications.

No Scheduled Maintenance

1. What are its functions and associated performance standards?

2. In what ways can it fail?

3. What causes it to fail?

4. What happens when it fails?

5. Does it matter if it fails?

6. What can be done to predict or prevent each failure?

7. What do we do if we cannot prevent the failure?

Page 14: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

RCM2 Review GroupRCM2 Review Group

FacilitatorFacilitator

Flight Engineer

Mechanic

Test Pilot

Engineer

Depot Artisan

Equipment Manufacturer

Page 15: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

Failure Data and MaintenanceFailure Data and Maintenance Effective to:

• Determine high cost items, high maintenance man-hour consumers, etc.

• Determine if a task is worth doing• Identify failure finding intervals

With respect to identifying Maintenance tasks and

associated intervals, typically historical data is inadequate.

• Reports only what failed.• Describes what was done to repair the failure rather than what

caused it.• Doesn’t describe failures that are currently being prevented or

plausible failures that haven’t occurred.• Describes failures which may be the effect of some other failure.• Inadequate information for determining On-Condition Tasks,

Overhaul, and Replacement intervals.

Page 16: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

RCM2 Review GroupRCM2 Review Group

FacilitatorFacilitator

Flight Engineer

Mechanic

Test Pilot

Engineer

Depot Artisan

Equipment Manufacturer

In the absence of specific data on failure rates and characteristics, intervals are largely determined based on

service experience.

Page 17: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

The Need for a StandardThe Need for a Standard

• RCM2 complies fully with SAE Standard JA1011: “Evaluation Criteria for Reliability Centered Maintenance (RCM) Processes.”

Page 18: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

Systems AnalyzedSystems Analyzed

Page 19: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

CH-47D Systems CompletedCH-47D Systems Completed

• Flight Control System

• Advanced Flight Control System

• Flight Hydraulic System

• Power Train

• Engine Air Particle Separator

• Fuel System

• -714A Engine (including FADEC)

• -714A IETM

• 400 Flight Hour Cycle Service/Modular Daily

Page 20: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

Results and BenefitsResults and Benefits

Page 21: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

Power of RCMPower of RCM• Reengineered Maintenance Schedule Maintenance task is generated for an identifiable and explicit reason

• Simulation Updates

• Physical Redesigns

• Procedural Redesigns

• Training Redesigns

• Operational Redesigns

• Technical Publication Redesigns

RCM applied to the Interactive Electronic Technical Manual

Page 22: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

REDESIGNS

Physical Publications Training Operational Procedural Simulator

-714A Engine

-714A FADEC

-714A IETM

Flight Control

Advanced Flight Control System

Power Train

SYSTEM

Flight Hydraulics

5 16 2 0 36 0

2 1 0 2 19 0

6 0 0 1 10 0

1 20 0 0 0 0

13 18 4 8 17 2

14 16 3 1 53 0

8 1 0 1 27 0

Total (321) 52 77 9 15 166 2

Implemented

In-progress

Disapproved

12 15 7 5 13 2

37 61 2 10 152 0

3 1 0 0 1 0

EAPS

Fuel System 1 0 0 2 0 0

5 0 0 4 02

CH-47D RCM2 RecommendationsCH-47D RCM2 Recommendations

Page 23: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

ResultsResults• Improved understanding of Full Authority Digital Electronic Control

Unit (FADEC)

Developed an accurate and useable pilot fault code matrix

Improving troubleshooting guide

• Capitalized on -714A technology to increase readiness and reduce mission aborts

Established correct emergency and operating procedures

Page 24: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

Focus: Inventory Management

Inventory Management

DemandRate

SupplyAvailability

Cost per Repair

Cycle Time

Inherent Reliability

Diagnostic Error

Operation Induced

Quality Defects

BudgetFH

Program

StockLevels

Backorders Current A/C Performance- Component- Subsystem- System

System Status- A/C Tail #- Unit- Fleet

Demand Rate Management Activity

Inventory Management Activity

M&O/Acquisition ActivityGTW Capability Activity

GTW Capability

Inherent Reliability

Serviceability Criteria

Fault Isolation

Publications

Scheduled Maintenance

Training

Depot Quality

Environment

Page 25: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

•Data Analysis•Data Mining

•Metrics

DepotTeardown

Assessment

Field Directed Insights

DemandRate ReductionOpportunities

LIDB

RecapAnalysis

CargoBaseline

2410

AMAC

RCM2Team

Analysis

Demand Rate Management Activity

Inherent Reliability

Diagnostic Error

Operation Induced

Quality DefectsDTLOMS

Page 26: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

SumarySumarySummarySummary• “We’re making a big difference here.”

• “It gives the users a voice.”

• “This is worth a zillion dollars if we can get this information out.”

• “It is a direct interface between us and the manufacturer.”

• “I have never seen such enlightenments in my career.”

• “I want to know why we aren’t as good as we think we are and I want to know how we can be as good as we need to be.”

Page 27: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

Nancy ReganNancy [email protected]@theforceinc.com

617-921-5408617-921-5408

Page 28: The Significance of RCM2 applied to the CH-47D, Chinook Presented by Nancy Regan, The Force, Inc

P-F IntervalP-F Interval

F2: Bearing separates from race

P: PC link bearing detectable play(Potential Failure Condition)

F1: exceeds .010” play

Res

ista

nce

to

Fai

lure

Time

New Bearing Installed

200 Flight Hours

400 Flight Hours

• Inspection interval is governed by how quickly the failure occurs once it is detectable … not how often it occurs.

• The P-F interval allows inspection intervals to be sensibly assigned.

• Component remains in service until its failure resistance falls below a defined level.

© 2003 The Force, Inc.