redefining supportability supportability that characteristic of a system and its support system...
TRANSCRIPT
Redefining Supportability
Supportability
That characteristic of a system and its support system design that
provides for sustained system performance at a required readiness
level when supported in accordance with specified concepts and procedures.
Supportability
That characteristic of a system and its support system design that
provides for sustained system performance at a required readiness
level when supported in accordance with specified concepts and procedures.
Supportability: Supportability as defined herein (a shift in the paradigm) is a metric that addresses every support event within the domain of the Integrated Logistics Support Elements, with respect to support event frequency, event duration, and event cost. This is reflected in a composite, quantitative and qualitative characteristic of the supported system (project) to meet specified operational requirements for its intended life cycle, and is optimized for Total Ownership (TOC).
Supportability: Supportability as defined herein (a shift in the paradigm) is a metric that addresses every support event within the domain of the Integrated Logistics Support Elements, with respect to support event frequency, event duration, and event cost. This is reflected in a composite, quantitative and qualitative characteristic of the supported system (project) to meet specified operational requirements for its intended life cycle, and is optimized for Total Ownership (TOC).
Supportability Approach must Emphasize Support EventCharacterization Beyond Traditional Operational Availability (AO)
TRADITIONAL APPROACH NEW APPROACH
Ma = SUPPORTABILITY (S)?
AO
OT + ST
OT + ST + TCM + TPM + A/LDT=
WHERE: TOTAL OPERATING TIME DURINGA SPECIFIC INTERVAL
TOTAL STANDBY DURING ASPECIFIED INTERVAL
TOTAL CORRECTIVE MAINTENANCETIME DURING THE SAME SPECIFIEDINTERVAL
TOTAL PREVENTIVE MAINTENANCETIME DURING THE SAME SPECIFIEDINTERVAL
TOTAL ADMINISTRATIVE ANDLOGISTICS DOWNTIME DURING THESPECIFIED INTERVAL
• HENCE, AO ADDRESSES R&M ONLY • HENCE, MATERIAL AVAILABIITY REQUIREMENTS ADDRESS ALL EVENTS
• GIVEN: Ma
OT
ST
TCM
TPM
A/LDT
=
=
=
=
=
OT + ST
(?) + OT + ST + TCM + TPM + MLDT=
MISSING EVENTS
- SERVICING- RECONFIGURING-GROUND/CARRIER HANDLING-SET UP AND TEAR DOWN
- COMBAT OPERATIONS- LAUNCH ACTIVITIES- MISSION VARIATIONS- OTHER NON R&M ACTIONS
• AND: S = {OPERATIONAL SUITABILITY, READINESS,SUSTAINABILITY, SURVIVABILITY, MOBILITY,
LIFE CYCLE COSTS, AO} Events
• BECAUSE: S IS NOT ADDITIVE BUT CONSISTS OF FINITE,SIMULTANEOUS SUPPORT EVENTS FROMALIGN TO WINTERIZE (500+ EVENTS DEFINED)
SUPPORT PLANNING BASELINE(PEACETIME OPERATIONS)
DESIGN FOR S BASELINE(WARTIME OPERATIONS)
• WHERE:
f = SUPPORT EVENT FREQUENCYd = SUPPORT EVENT DURATIONc = SUPPORT EVENT COST
S = F (f, d, c) IS A CHARACTERISTIC OF DESIGN
VSTHE PROBABILITY THAT, WHEN USED UNDER STATED CONDITIONS, A SYSTEM WILL OPERATESATISFACTORILY AT ANY TIME. AO CAN BEEXPRESSED BY THE FOLLOWING FORMULA:
Supportability (S) – Addressing Integration
• The Supportability Metric addresses EVERY support event as a DESIGN DRIVEN attribute, with respect to support event frequency, event duration, and event cost.
• This approach reflects an integration of quantitative and qualitative characteristics that meet specified Operational Requirements, Total Ownership Cost (TOC) goals and Performance Based Logistics (PBL).
• What is Supportability (S)?• S = Supportability is the integrating function for all “ilities” with regards to design
characterization, and is reflected by design features resulting from Supportability Design-to Requirements (SDTRs)
• S = F(f, d, c) provides the integrating function
f = support event frequency (includes reliability driven events)d = support event duration (includes maintainability driven events)c = support event cost - support system cost per event (e.g. all ILS elements – facilities,
training, transportability, etc.)
• Supportability is at its Optimum when S approaches “minima”, or when the system is self sufficient at least cost (therefore best value).
• Supportability can be expressed in terms of Total Ownership Costs (TOC) as shown below.
• Supportability Component of TOC: S TOC (f x d x c)
The Supportability Engineering “Top Ten” Steps
1. Establish the Project Baseline with Systems Engineering (SE)2. Review statistical supportability drivers [S = F(f,d,c)] of Comparative
Systems using Pareto Analysis3. Review the predecessor or comparable system’s technical data4. Interview maintenance techs with SPECIFIC questions 5. Develop detailed lessons learned from steps 3 & 4 – PBL IPT.6. Integrate technical data, statistics, and interviews - develop initial
SDTRs linked to the S function.7. Optimize SDTRs
CUSTOMER criteria Technological opportunities Explore with Design Team members and Producibility Engineers to
ascertain design characteristics.8. Finalize SDTRs - use “specification language”9. Update or negotiate SDTRs with SE and Designers.10. Incorporate SDTRs into the “System Specification” or ECP
The support scenario must focus on an attempt to eliminate the logistics infrastructure and reduce total ownership cost (TOC), which includes Depot and contractor support. PBL is applied to what’s left.
Comprehensive Supportability Design-To Requirements (SDTRs)Reduce Event Frequency, Duration and Cost to Meet System
Spec
• SUPPORTABILITY (S) ELEMENTS- OPERATIONAL SUITABILITY
- READINESS
- INFLIGHT SUSTAINABILITY
- MOBILITY/TRANSPORTABILITY
- LOGISTICS LIFE CYCLE COST
- AVAILABILITY (A0)- RELIABILITY
- MAINTAINABILITY
- OPERATIONAL SUSTAINABILITY
• SUPPORT A
CTIONS
- GROUND H
ANDLING
- SERVIC
ING (F
UEL, OIL
...)
- ARM
AMENT &
WEAPONS
• LOADIN
G
• UNLOADIN
G
- RADIO
/RADAR F
REQ CHANGES
- HOT/C
OLD WEATHER K
ITS
- BALLAST L
OADING/U
NLOADING
- MIS
SION R
ECONFIGURATIO
N
- TAPE IN
STALLATION (P
ROMS)
- CHAFF L
OADING/U
NLOADING
- PRESERVATIO
N
- DEPRESERVATIO
N
- ENGIN
E RUNUP IN
TEST C
ELL
- INSPECTIO
NS (MAJO
R, MIN
OR)
• OP
ER
AT
ION
S
- A
LE
RT
TIM
E
- R
EA
CT
ION
TIM
E
- F
LE
XIB
ILIT
Y
- C
OM
BA
T M
ISS
ION
S
- T
RA
ININ
G M
ISS
ION
S
- F
ER
RY
MIS
SIO
NS
- S
PE
CIA
L O
PE
RA
TIO
NS
- A
US
TE
RE
FIE
LD
(3r
d W
OR
LD
)
- E
QU
IPM
EN
T E
MP
LA
CE
ME
NT
(S
ET
-UP
)
- E
QU
IPM
EN
T D
ISP
LA
CE
ME
NT
(T
EA
R-D
OW
N)
- N
AV
Y O
PE
RA
TIO
NS
(O
CE
AN
, S
UB
-SE
A)
Traditional R & M
RELIABILITY & MAINTAINABILITY - MAINTENANCE • PREVENTIVE • CORRECTIVE - SUPPLY DELAY - ADMIN DELAY(128 PARAMETERS FROMMIL-STD-721C)
OPERATIONSGENERALSUPPORTACTIONS
SELECTED SET OFSDTRs
SUPPORT EVENTS• 500+ PARAMETERS• DESIGN TO ALGORITHMS
DESIGNER
TAILORED SDTRs
SYSTEM SPEC
Supportability Design-to Framework
How Should We Convey Supportability Requirements?
Supportability Design-to Requirement (SDTR): “The directional control computer shall contain BITE circuitry that tracks within the full range of control surface positions, and shall be impervious to variations in system ground levels (±0.5v DC).”
The Objective: Let’s make it easy for the designer by making supportability transparent through simple and direct specifications oriented to PBL.
• FAILURE - RELEVANT - NON-RELEVANT - CHARGEABLE - NON CHARGEABLE
95% BIT
WHAT THE….???
OR THIS:
MTTR
Mc
Mp
MTTS
MTMBA
DMMH
FMECA
MTBF
R GROWTH
DIRECT TIME
UPTIME
DOWNTIME
RTOK
FALSE ALARM
Ai
A a
Ao
Supportability is the “Forcing Function” that Addresses the Elements and Sub-Elements Simultaneously with SDTRs
Algorithms can Define Supportability (S) Design Characteristics
[( TH j1 Kb
± ADJ ) 61* SE(WTb) 9
1 E(WTb)* ]f{[( TH j
1 Kb± ADJ ) 6
1* SE(WTb) 91 E(WTb)* ]d
[( TH j1 Kb
± ADJ ) 61* SE(WTb) 9
1 E(WTb)* ]c } BASELINE
Then, S(f, d, c)OPT=
[( TH j1 Pb
± ) 61* SE(WTp) 9
1 E(WTP)* ]f{ 1nTHL
[( TH j1 Pb
± ) 61* SE(WTp) 9
1 E(WTP)* ]d1
nTHL
[( TH j1 Pb
± ) 61* SE(WTp) 9
1 E(WTP )* ]c } PROJECT1nTHL
IF S = Supportability and S = F(f, d, c)f = support event frequencyd = support event durationc = support event cost
S is at its optimum when S approaches “0” with respect to f, d, and c,
Correction of baseline value or historical dataBaseline, existing or predecessor systemSupportability elements - major1) Operational suitability2) Readiness3) In-flight sustainability4) Survivability5) Operational sustainability6) Mobility/transportability7) Reliability and maintainability8) Life-cycle cost
9) Availability (AO)
Engineering change proposalSelection range of baseline parameter valuesParameter reflecting historical dataParameter baseline from comparative,historical WUCsUnique set of SDTRs , that address baseline system, LRU, SRUSelection range of SDTRs that operate (+ or -) on the jTH set of baseline values off, d, or c.Supportability at optimum state whensupport events approach “0”Supportability design-to requirements
Supportability elements - subordinate1) 01- 09 support general codes2) Preventive maintenance3) Corrective maintenance4) Resource consideration5) Personnel requirements6) Support equipment and facilitiesWeighted or relative importance of elements- baselineWeighted or relative importance of elements- projectWork unit code reflects system data definition for historical data collection or for new systems
ADJ =
B or b =
E =
ECP =jTH =
K =
Kb =
L =
nTH =
S (f, d, c) OPT =
SDTR =
SE =
WTb =
WTp =
WUC =
andWhere:
Comparison baseline
The new project
The WBS - Beyond Earned Value Reporting
•The Work Breakdown Structure (WBS) is important as an Information Node
•Take Advantage of the WBS to nestle your •Comparative Data•Statistical Information
•Use the WBS as the Basis for Design-to Requirements
•Expand the WBS Dictionary to include the way you actually plan Work
Lessons Learned Linked to Requirements [P, S = F (f,d,c)] AreEmbedded In the Work Breakdown Structure (WBS)
PRODUCIBILITY ELEMENTS
ASPECTS OF D
ESIGN
SPECIFIC
ATIONS A
ND STANDARDS
MATERIA
LS SELECTIO
N
PROCESS DEFIN
ITIO
N
ENVIRONM
ENTAL REQUIR
EMENTS
GENERAL INSPECTIO
NS
TESTING
SAFETY CONSID
ERATIONS
CLEANING R
EQUIREM
ENTS
INFORM
ATION N
ODES
PRODUCIBILITY SUBELEMENTS
• DOCUMENTATION CONTROL & ADMINISTRATION
• ASSEMBLY AND TEST
• PIECE PART/MINOR FABRICATION
• INTEGRATION AND PERFORMANCE CHECKS
• PERSONNEL CHARACTERISTICS
• FACILITIES/EQUIPMENT/TRANSPORTATION
Producibility and Supportability Information Nodes/Cells reside in the WBS • Basis for design-to requirements • Provide automated information management Access Retrieval Use Cell division/multiple applications Traceability Data base management Artificial intelligence information clusters
SUPPORTABILITY ELEMENTS
OPERATIONAL S
UITABIL
ITY
READINESS
INFLIG
HT SUSTAIN
ABILIT
Y
SURVIVABIL
ITY (
COMBAT S
UPPORT)
OPERATIONAL S
USTAINABIL
ITY
MOBIL
ITY A
ND TRANSPORTABIL
ITY
LIFE C
YCLE COST
OPERATIONAL A
VAILABIL
ITY
RELIABIL
ITY/M
AINTAIN
ABILIT
Y
INFORM
ATION N
ODES
SUPPORTABILITY SUBELEMENTS
• GENERAL SUPPORT
• CORRECTIVE MAINTENANCE
• PREVENTATIVE MAINTENANCE
• RESOURCE CONSIDERATION
• PERSONNEL CHARACTERISTICS
• SUPPORT EQUIPMENT & FACILITIES
Information management, knowledge capture, and a dynamic systems engineering environment result in producible and supportable products.
Cell Characteristics Index RequirementsDesign-to Data Base
• Producibility unique AL Film, metalized • Supportability unique 38 Service center • Common/shared 37 Mounting and positioning
System Engineering Process
DesignerNew System • Producible • Supportable
Trade Studies
PVC/283Z/194a
PRODUCIBILITY (P ) SUPPORTABILITY (S )
WBS
WBS
Information Nodes
The WBS - Beyond Earned Value Reporting
•The Work Breakdown Structure (WBS) then:
•is structured to view Work Unit Codes as SDTRs
•can be monitored in scheduling tools (Microsoft Project) to track status of design progress to SDTRs
•which allows critical path identification of SDTRs
•Makes design appraisals more accurate and efficient
•Is used for Information Management•Access to your data•Retrieval of important information•Multiple applications of your knowledge•Generate schedules based on the WBS content•Requirements Traceability (DOORS, SLATE, etc.)•Data Base Management•Knowledge Clusters•Etc……
What about Producibility?
The Producibility Design-to
Requirements (PDTR) Development Process
• New Design Related Metrics
• Integrating Producibility and Supportability
PRODUCIBILITY DEFINED
Producibility elements - major
1) Aspects of design2) Specifications and standards3) Materials selection4) Processes definition5) Environmental requirements6) General inspections7) Testing8) Safety considerations9) Cleaning requirements
AND THIS
Producibility element - subordinate
1) Documentation control and administration2) Piece part/minor fabrication3) Assembly and test4) Integration and performance checks5) Personnel characteristics6) Facilities/equipment/transportation
•Again, just as in Supportability, we compute:
Weighted or relative importance of elements for system being replaced or modified - Comparison BaselineWeighted or relative importance of elements that we want to see in the new system- The New Project
PRODUCIBILITY DEFINED(surprise - same as Supportability!)
• Producibility is defined as :
• The frequency of the manufacturing event where f = manufacturing event frequency;
i.e., how often will it occur?
• The duration of the manufacturing event where d = event duration; i.e., how long is the event?
• The cost of the manufacturing event where c = event cost;
I.e., how much will it cost?
P IS AT ITS OPTIMUM WHEN P IS MINIMIZED OR WHEN PRODUCTION IS MOST EFFICIENT, EASY TO ASSEMBLE, AND AT LEAST COST
Producibility Integration Process
•Evolving designs are optimized for producibility
• Producibility Design-To-Requirements (PDTRs) provide comparison basis against Predecessor• PDTRs serve as guidelines during the Technology Insertion Process to ensure technology
does not proliferate producibility risks
•Maximize producibility/supportability synergism
•Simulate factory flow optimization after PDTR implementation to determine PDTR effectiveness
•Incorporate PDTRs into the Technical Data Package so as not to lose them when you create a build package for re-procurement
A disciplined, systematic approach enhances Producibility Implementation
Algorithm Defined Producibility (P) Design-to RequirementsAssure Team Member Focus >>> Reduce Production Events
POWER SOURCESELECTRO-MECHANICAL& HARNESS
ASSEMBLYAND TEST
MACHINE SHOPAND PLATING
PRODUCIBILITYENGINEER
• PDTR OPTIMIZATION• TECHNOLOGIES INSERTION• TRADE STUDIES• INDEPENDENT RESEARCH & DEVELOPMENT (IRAD)
OTHER ORGANIZATIONS
INTEGRATIONAND TEST
FABRICATION &PRECISIONMECHANICALASSEMBLY
PRODUCTIONPLANNING ANDCONTROL
HYBRIDMANUFACTURING
PRODUCIBILITYMANAGER
SYSTEM ENGINEERING
DESIGN ENGINEERING
PRODUCIBILITY ELEMENTS
ASPECTS OF DESIGN
SPECIFICATIONSAND STANDARDS
MATERIALS SELECTION
PROCESS DEFINITION
ENVIRONMENTALCONSIDERATIONS
GENERAL INSPECTIONS
TESTING
SAFETY CONSIDERATIONS
CLEANING REQUIREMENTS
ALGORITHMSP = {((((±JthPS...)})
[( TH j1 Kb
± ADJ ) 61* SE(WTb) 9
1 E(WTb)* ]f{[( TH j
1 Kb± ADJ ) 6
1* SE(WTb) 91 E(WTb)* ]d
[( TH j1 Kb
± ADJ ) 61* SE(WTb) 9
1 E(WTb)* ]c } BASELINE
P(f, d, c)OPT =
[( TH j1 Mb
± ) 61* SE(WTm) 9
1 E(WTm)* ]f{ nTHL
[( TH j1 Mb
± ) 61* SE(WTm) 9
1 E(WTm)* ]dnTHL
[( TH j1 Mb
± ) 61* SE(WTm) 9
1 E(WTm )* ]c }PROJECT
nTHL
P = Producibility.
P = F(f, d, c)
Producibility is a metric with respect to production event frequency,duration, and cost that reflects composite characteristics of the manufactured system (project), to meet specified quantity, schedule and production standards.
Where:f = manufacturing event frequencyd = manufacturing event durationc = manufacturing event cost
P is at its optimum for the project when P approaches “0” with respect to f, d, and c, or POPT = PBASELINE >>> P PROJECT
B or b =Correction of baseline value or historical dataBaseline, existing or predecessor systemProducibility elements - major1) Aspects of design2) Specifications and standards3) Materials selection4) Processes definition5) Environmental requirements6) General inspections7) Testing8) Safety considerations9) Cleaning requirementsEngineering change proposal
Selection range of baseline parameter valuesParameter, reflecting historical dataParameter baseline from comparative,historical WBSsUnique set of PDTRs analyses thataddress baseline system andgenerate project requirementsProject, new system or major ECPSelection range of PDTRs that operate (+ or -) on the jTH set of baseline values off, d, or c.Producibility at optimum state whensupport events approach “0” (minima)Producibility design-to requirements
Producibility element - subordinate1) Documentation control and administration2) Piece part/minor fabrication3) Assembly and test4) Integration and performance checks5) Personnel characteristics6) Facilities/equipment/transportationWeighted or relative importance of elements- baselineWeighted or relative importance of elements- projectWork breakdown structure reflects system datadefinition for historical data collection orfor new systems
ADJ =
E =
jTH =K =
Kb =
L =
M or m =nTH =
P (f, d, c) OPT =
PDTR =
SE =
WTb =
WTm =
WBS =ECP =
Events range from Anodize to Zyglo
Integrated Supportability and Producibility
Relia
bility
Mai
ntain
abili
ty
Produci
bility
Logistic
s
Other
DESIGNINTEGRATION
DESIGNERDESIGNERS DESIGNERSSYSTEMS
ENGINEERS
ProducibilityP
SupportabilityS
POWER SOURCESELECTRO-MECHANICAL& HARNESS
ASSEMBLYAND TEST
MACHINE SHOPAND PLATING
PRODUCIBILITYENGINEER
• PDTR* OPTIMIZATION• TECHNOLOGIES INSERTION• TRADE STUDIES• INDEPENDENT RESEARCH & DEVELOPMENT (IRAD)
HYBRIDMANUFACTURING
INTEGRATIONAND TEST
FABRICATION &PRECISIONMECHANICALASSEMBLY
PRODUCTIONPLANNING ANDCONTROL
• HUMAN FACTORS• SAFETY
RELIABILITY
MAINTAINABILITY
LOGISTICS SUPPORTANALYSIS
DESIGN• SUPPORT EQUIPMENT• TRAINING DEVICES
SUPPORTABILITYENGINEER
• SDTR INTEGRATION**• SUPPORTABILITY TECHNOLOGIES• TRADE STUDIES• INDEPENDENT RESEARCH & DEVELOPMENT (IRAD)
FIELDSUPPORT
ILS DISCIPLINES/ELEMENTS• MAINTENANCE PLANNING• MANPOWER AND PERSONNEL• SUPPLY SUPPORT• TRAINING• TECHNICAL DATA• COMPUTER RESOURCES SUPT• PKG, HANDLING AND STORAGE• TRANSPORTATION• FACILITIES• STANDARDIZATION AND INTEROPERABILITY
* Producibility Design-To-Requirements (PDTRs)
**Supportability Design-To-Requirements (SDTRs)
FORMAL
INFORMAL
Summary
• Supportability (S) and Producibility (P) may be redefined as the integrating functions, represented by all ILS elements, that addresses all support events related to the design of the system such that Supportability “is a Function of”:
f = Support or Production event frequency
d = Support or Production event duration
c = Support or Production event cost per event
• This function can be used in Pareto analyses of an existing, baseline or comparative system to determine the drivers (f,d,c), which also include MTBF and MTTR.
• Those same drivers are then intentionally reduced by design-collaborated SDTRs for each event.
• Design responses to each SDTR are tracked and assessed for the entire system.
• When (S) and (P) approach minima, the system is said to be self-sufficient and in an ideal state. Support event frequency, duration and cost can be independently defined, and using a life cycle cost model such as CASA, the impact on cost can be immediately determined.
CONCLUSION
• Integrate Producibility and Supportability design-to results into a systems engineering requirement. We must:
• Extend Supportability beyond traditional metrics (MTBF, MTTR, etc.)
• Define NEW metrics: Producibility - Supportability
• Develop requirements written in design-to language
• Address Readiness, Sustainability, Mobility, Transportability and Operational Availability via SDTRs
• Use the Work Breakdown Structure (WBS) as an Information Node for requirements development and tracking
• Support by Design is the Key - through Supportability and Producibility Design-to Requirements (SDTRs and PDTRs), resulting in:
Low Maintenance Man Hours per Flight Hour (Mmh/FH) Reduced Cycle Time Reliability and Robustness Reduced Logistics Foot Print Supportable and Producible Products