Managing Aircraft Stuctural Integrity
in the ADF
WGCDR David Zemel
Deputy Director – Aircraft Structural Integrity
Aircraft Airworthiness and Sustainment
Conference 2010
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Introduction
Achieving ASI
• A little history
• The ASI Program
Managing ASI in the ADF
• Development of the ADF ASI Program
• Contemporary ADF ASI Environment
• Current ADF ASI Policy
• ADF ASI Program Requirements
• Tailoring and ASI Program
• Example Through Life Support Arrangement
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Aircraft Structural Integrity - History
“The property of an airframe to withstand the
loads for which it is designed”1
Reliance on Factor on Safety – accounted for
1USAF variability in:
Dictionary 1956 • loads
Cited in Report 680.1B, History of the Aircraft Structural Integrity Program, ASIAC, 1980
• structural analysis
• material properties
• deterioration over service life
• build quality
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Aircraft Structural Integrity - History
Civil and Military structural failures in the 1950’s
Boeing B-47
De Havilland Comet
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Subsequent developments in design development and in-
service management against fatigue
• Higher static strength leading to corresponding
increases in fatigue strength
• Fail-Safe design principles Seminal Accidents
Comet
• Damage Tolerance design principles
B-47
• Durability considerations F-111
B707
• Full Scale Fatigue Testing B737
• Ageing aircraft considerations
• Widespread Fatigue Damage considerations
• Corrosion control
• Dedicated ASI Programs…
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Typical Civil & Military ASI Programs
Civil
• ICAO Airworthiness Manual
- Certification
- Continuing Airworthiness
- Continuing Airworthiness Assurance
• FAA Reg (25.1529 Continuing Airworthiness)
- Airworthiness Limitations
- Structural Inspection Requirements
- Mandatory Replacement Times
Military
• MIL-STANDARD-1530 (Parts)
- Design Information
- Analysis
- Full Scale Testing
- Fleet Data (and Certification)
- Fleet Management
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Development of the ADF ASI Program
• 1980’s RAAF separated ASI management
- fatigue management (centralised),
- other forms of degradation (decentralised)
• No holistic whole of life management
• ASIP concept considered but never developed
• Debate over decentralising fatigue
management
• 1990 two unrelated accidents due to fatigue…
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Development of the ADF ASI Program
Nomad and Macchi
accidents - 1990
• Lack of appreciation of loads
• No fatigue test
• Used aircraft
• Use of condition data
• Control build quality
• No pertinent fatigue tests
• Algorithms in error
• Inadequate engineering
management system
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Development of the ADF ASI Program
CAA Review of ASI in
ADF - 1992
Findings
• RAAF had not identified the intended outcome from ASI
management
• Management system was not
- constraining risk
- providing timely germane advice to decision makers
• Processes in place, but outcome degraded due lack of
understanding of principles
• Dispersal of expertise should be avoided
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Development of the ADF ASI Program
ADF’s first ASIP required:
Assessing design against RAAF Standard
Assuring quality on production
Identifying critical items for through-life management
Regular re-assessment of certification, management policy
(inspections), physical condition
Collection and analysis of environmental & usage data
Documentation of Program in a plan
ASIP covered State aircraft only
Based on ASI-DGTA performing a majority of the
ASIP tasks on behalf of WSLMS/SPO
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Contemporary ADF ASI Environment
By mid 2000’s the landscape was changing:
• Through Life Support (TLS) outsourced to industry from acquisition
• Breadth of Airworthiness Management System
- State Registered (Mil Spec, Civil variant (EASA, FAR23, FAR25))
- Non-State Registered (VH reg)
- Increasing types due to capability expansion
- Increasing range of TLS models and certification standards
• Technology advancement
- Materials – e.g. composites, glare
- Standards – development and interpretation of ADF unique solutions
- Methods – e.g. RRA, SPD, FSW
- Structural Health Monitoring
- Non-destructive Testing
• Ageing fleets
- Broad range of logistic issues
- Effectiveness and applicability of the Certification Standard
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Current ADF ASI Policy
Recent changes to Policy - Further reflection on CAA
Review coupled with contemporary environment
No longer use a comparative standard
Less prescriptive. Pushes some of the prescriptive elements
into the Technical Airworthiness Management Manual
ASIP Policy implementation becomes more flexible and responsive
Define and specify ASI Program requirements
Identifies contemporary roles and responsibilities
Ability to use appropriate tailoring
Requirement for retention of indigenous ASI knowledge
ASI Program Guidance based on MIL-HDBK-1530
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Current ADF ASI Policy Statement
Defence must have a program to manage
ASI and ESI for each ADF managed
aircraft supported by competent
organisations with appropriate levels of
knowledge and expertise
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Current ADF ASI Policy Objectives
• Constraint of the risk of structural failure of an
aircraft to an acceptable level (Required Safety)
• Achievement of planned rates of aircraft
availability (Maximise Availability)
• Avoidance of unforecast cost of refurbishment
(Minimise Cost)
• Achievement of the planned withdrawal date
(Assure Capability)
• Continually Optimise the Program to minimise
cost and downtime
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Flow of Requirements from ADF ASI Policy
Why Policy
Establishes
Implied
Directs Reqt
Reqt
What 053
How 054 ASIP
Reqt
Guidance Implements and
Executes Reqt
053 – Tech Airworthiness Management Manual
054 – ADF Design Requirements Manual ICA
ICA – Instructions for Continuing Airworthiness
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ASI Program Requirements
Cert Basis Build Quality
Data Reqt
ASI Program
SI Mgt Policy (ICA)
Documentation
Monitoring and
Assessment OLM
SLA AASA
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ASI Program Information Flow
Implementing the ASIP
involves establishing systems
that:
Collect the data
Assess the data
Report on the outcomes
Report types include
Routine Usage Status
Usage Assessment
Fatigue Assessment
Structural Condition Assessment
These systems will be
described and approved in the
Management Plan. Specific
instructions will be required by The heart of a
the implementing authority – mature ASIP
SPO, TLS Contractor
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Tailoring an ASI Program
Ultimately any ASIP can be tailored
Recognises the broad range of TLS arrangements
Recognises different acquisition strategies
Recognises legacy programs (Civil and Military)
Recognises nature of configuration, role and operating environment
Recognises broader application of Airworthiness Management System
There are two main areas to be considered when tailoring
Tailoring the ASIP requirements
Tailoring the ASI management
Tailoring ASIP requirements
Default is full ASIP requirements
Minimum requires some method to ensure System of Maintenance remains valid while
operating with ADF
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Tailoring an ASI Program
Tailoring ASI management
Defining the roles and responsibilities
Account for nature of TLS arrangement
Account for experience of implementing agency
Account for role of aircraft
All programs are to be Authorised by DGTA-ADF
All programs are to have a manager assigned whose responsibility is to
ensure all elements of the ASIP are implemented.
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Tailoring ASIP Management
Examples of TLS arrangements
In-service Model (ASI/SPO)
Outsource Model (ASI/SPO/Prime Contractor)
Many variations
Example
FMS Model (ASI/SPO/USAF)
Lease Model (ASI/Contracting Agency/Contractor/NAA)
Museum (ASI/Operating Org/NAA)
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Tailoring an ASI Program – Example TLS
ASI Program for One Aircraft Type
Supporting Activities
by ASI-DGTA
TLS Contractor ASI-DGTA
•Four Circles •Acquisition Support • Develop Policy,
•Implement SBI •Establish ASIP Reqts Procedures and
•ASIMP Input •ASIMP Approval Guidance
•SLA Conduct •ICA Approval SBI
•AASA Conduct •Manage Testing • Advice to Cap Mgr
•(ASI Management) Programs
•(ASIP Management) • Independent in-
service advice
SPO
•DAR • Education
OEM •Configuration Item Mgr DSTO
•Contracting • Interpret Standards
•Audit the AEO
SQN/ •Finance Industry • Audit Systems
WG
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Summary ASI Management in ADF
Driving Principles
Safety
Availability
Cost of Ownership
Management Principles
Legacy certification (where possible)
Understand Standards and their application
Data collection, assessment and feedback
Four circles - Primary
Attestation against SoM - Secondary
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References
1. The History of the Aircraft Structural Integrity Program, ASIAC, Report No. 680.1B, 1980
2. Milestone Case Histories in Aircraft Structural Integrity, R. Wanhill, NLR, 2002
3. Investigation into Ansett Australia maintenance safety deficiencies and the control of continuing airworthiness of
Class A aircraft, File No. BS/20010005, ATSB
4. A Report into the Management of Aircraft Structural Integrity in the RAAF, CAA, 1992
5. Developments in RAAF Aircraft Structural Integrity, E.S. Wilson, RAAF, 1995
6. Some observations on fatigue life management, A.J. Emmerson, CASA
7. Aircraft and Engine Structural Integrity Management (Draft), DI(G) LOG 4-5-016
8. Code of Federal Regulations 14, Aeronautics and Space, FAA, DOT, 2010
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Questions?
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