Page 274 - The Jet Engine
P. 274

Overhaul







































        Fig. 25-1  Example of growth of time between overhaul (T.B.O.).



        obtained may be two, three, or even four times the  7. In addition to scheduled overhauls, there are
        original period permitted.  The development of the  problems that arise from damage and defects.  A
        T.B.O, from the introduction of an engine into service,  proportion of these, which are uneconomic or
        through several years of operation, is shown as an  impractical to rectify in the aircraft, necessitate
        example in fig, 25-1.                             unscheduled removals and require the engine to be
                                                          returned to an engineering base or an overhaul shop
        5. Among the main factors affecting the overhaul  for partial or complete overhaul.
        period for an engine is the use to which it is put in
        service. For example, a military engine will generally  8. The purpose of overhaul is to restore an engine
        have a much lower T.B.O. than its civil counterpart,  enabling it to complete a further life by complying
        as performance capability is the operating criterion  with new engine performance acceptance limitations
        rather than economics. Due to the effect of rapid  and maintaining the same reliability. This is achieved
        temperature changes in the hot parts of the engine,  by dismantling the engine in order that parts can be
        the most arduous treatment is the frequent changing  inspected for condition and to determine the need for
        of power output to which short-haul transports and
        fighter aircraft are subjected.                   renewal or repair of those parts whose deterioration
                                                          would reduce the performance, or would not remain
        6. When aircraft are based in areas with exception-  in a serviceable condition until the next overhaul.
        ally high humidity or salt content in the atmosphere,
        there exists the added danger of corrosion, resulting  9. The design of the modular constructed engine
        in the need for more frequent overhauls. In peace  (Part 22, fig. 22-1) makes it particularly suited to a
        time, some military aircraft have a very low utilization,  different technique of overhaul/repair. This technique
        this introduces the additional problem of certain  is based on 'on-condition' monitoring (Part 24). This
        materials used in its construction deteriorating before  means that a life is not declared for the total engine
        the engine has otherwise reached a condition which  but only certain parts of the engine. On reaching their
        would normally require an overhaul. Elapsed time, as  life limit, these parts are replaced and the engine
        well as flying hours, would then influence the    returned to service, the remainder of the engine
        overhaul period.                                  being overhauled 'on-condition'.

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