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Published byMegan Sutton Modified over 9 years ago
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Chapter 1 Why We Have to do Maintenance
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Why Maintenance Provides assurance Flight Safety Reliability Airworthiness
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Engineer’s Role Designer –Design best possible product –May be limited by Money Ability Technique –Man-made entropy Final design may not be optimum Reduced tolerances, cheaper materials Requires additional maintenance
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Mechanic Role Technician Repairer Maintainer Goal: Combat natural entropy in systems/components –Deterioration –Misuse –Remove/replace parts –Troubleshoot –Restore systems to intended use
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Maintenance Two types –Preventive maintenance (scheduled) Prevent deterioration of system to unusable level Corrective actions Reduce entropy to original level Regular intervals –Various intervals Daily Number of flights Flight hours Cycles
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Maintenance Two types –Unscheduled maintenance System breaks rapidly System breaks completely –Definitive, extensive troubleshooting
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Maintenance Reliability Level of perfection –Inherent reliability –Maintenance cannot increase level of reliability above this reliability
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Redesign Level of perfection increase –Material change New materials New techniques New components –Man-made change Tighter tolerances Improved design skills Design philosophy Natural entropy is reduced –Maintenance schedule will adjust –May increase or decrease schedule
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Failure Rate Different patterns of failure –Curve A Early failures –Poor design –Improper parts –Incorrect usage Failure rate levels off –Physical limit/wears out
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Failure Rate Different patterns of failure –Curve B Slightly rising rate Definite wear-out period at end –Physical limit/wears out
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Failure Rate Different patterns of failure –Curve C Slightly rising rate –No infant mortality or wear-out period –Becomes unusable
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Failure Rate Different patterns of failure –Curve D Slow failure rate when new Rises quickly after break-in period Steady level through rest of life
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Failure Rate Different patterns of failure –Curve E Steady or slightly rising failure rate No infant mortality or wear-out period
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Failure Rate Different patterns of failure –Curve F Infant mortality Level No wear-out period
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Maintenance Systemic approach –Reduce peak periods of unscheduled maintenance Management techniques –Equipment techniques –Line replaceable units –Minimum aircraft dispatch requirements
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Redundancy Higher desired reliability –Primaries and backups –Primary fails – backup takes over function Radios –Various maintenance techniques possible
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Line Replaceable Unit (LPU) Quick replacement –No undue maintenance delays –Failed part Discarded Repaired –No further delay to flight
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Minimum Equipment List (MEL) Loss of functionality –Does not effect safety or operation of flight –Manufacturer determined –Regulatory sanctioned –Deferral of maintenance without upsetting mission requirements Maintenance performed within specific time guidelines
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Dispatch Deviation Guide(DDG) Instructions for line maintenance Capping connectors from removed units Circuit breakers Prevent inadvertent power-up of specific equipment
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Configuration Deviation Guide(CDG) Certain panels missing Configuration differences not affecting safety
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