Factors that Influence Maintainability
The Defense Acquisition University defines Maintainability as a characteristic of design that can be defined on the basis of a combustion of time, frequency, and cost (Dallosta & Simcik). The time required to repair or return a system to a serviceable condition is a significant contributor to aircraft availability. Any efficiencies built into the system design would reduce the amount of time the aircraft is down or unavailable to perform its intended mission. How often or the frequency at which a system or component requires maintenance attention is also a significant contributor to aircraft availability. Any activity above and beyond routine servicing directly impacts maintenance and drives additional sustainment support such as manpower and support equipment. Finally, the cost to perform maintenance can be influenced by factors such as number of personnel and skill level require to perform the task, follow on maintenance associated with the parent task, and any peripheral support such as special equipment, facilities, and operational check out requirements. All of these factors, independent or in combination, will have a direct impact on the life cycle management strategy.
Although far from perfect, the F-35 program tried to build in maintainability as part of the overall supportability solution. Bit-in-Test (BIT) is one of the primary design influences intended to minimize the time associated with troubleshooting deficiencies. The contract requirement for system diagnostic capability established a 90% BIT function across the entire platform. Relying on self test to isolate faults reduces the time to repair. Leveraging technology one step further, the F-35 also introduced Prognostics Health Management (PHM) to enhance its aircraft availability. Admittedly PHM is still in its infancy stage however once matured, through data collection, modeling validation, software refinement, and a host of algorithms this system will predict pending failure and enable preventative maintenance to occur in step with routine servicing or unscheduled maintenance. This capability depends largely on the 90% BIT capability which stems from a backbone of continuous system, sub-system and component performance monitoring.
Other aircraft design factors considered frequency and used reliability predictions to determine component location in the overall design. Placing infrequently replaced assets in less accessible location and life limited or less reliable items in open areas such as wheel wells, weapon bays, and quick access panels illustrates the programs acknowledgment to design-in maintainability to improve supportability. Poor design is a major factor leading to maintenance
problems. Consideration such as elimination of components that can be installed incorrectly should be addressed during design to minimize maintenance errors (Hobbs, 2008). Not without challenge, fielded F-35 aircraft face significantly higher maintenance events as the fleet of Low Rate Initial Production (LRIP) aircraft have life limited parts, reliability issues, and insufficient spare. This is not completely unexpected as the F-35 procurement is being managed as a concurrent acquisition program. Operational Units are already receiving LRIP aircraft and the F-35 program is still four years away from completing Operational Test and Evaluation. Lacking design stability, installed as well as spare parts are intentionally limited to prevent rework of surplus or disposition of obsolescent parts. This is however the Department of Defense preferred acquisition strategy even though it assumes higher risk in cost overruns, schedule impacts, and performance delays (DODI 5000.02).
Finally, maintenance costs is a significant maintainability factor to consider in the sustainment solution. Reduction in the manpower to support the aircraft will reduce the total ownership cost. Minimizing the number of specialized skill sets also streamlines the sustainment costs by leveraging a smaller pool of equally trained technicians across the entire platform. High saturation of BIT capabilities and predictive tools like PHM enable manpower reduction and sustainment costs.
Maintainability of the system is dependent on finding a balance between time, frequency, and cost. For example, if you insist on the highest reliability to reduce the frequency of repair the trade off will be excess research & development, acquisition, operations & sustainment costs (Dallosta & Simcik). Designing-in maintainability and leveraging technology to streamline maintenance efficiency will reduce the total ownership costs. When procuring a new system using the DoD preferred concurrent acquisition method, it is important to establishing the sustainment strategy and widely distribute the milestone plan in order to keep the program on a consistent path to maturity.
References:
Hobbs, A. (2008, December). ATSB Transportation Safety Report, An Overview of Human Factors in Aviation Maintenance.
Dallosta, P & Simcik, T. Designing for Supportability. Retrieved from:
US DoD. (2013, November 26) Operation of the Defense Acquisition System. Retrieved from:
http://www.acq.osd.mil/docs/DSD%205000.02_Memo+Doc.pdf