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• Go to • Go to previous appendix • Go to next appendix Appendix II-ATA-specified documents This appendix outlines the architecture imposed on technical manuals by the ATA 100 specification, and analyses some of the related boundary and granularity problems which effect manual navigation. The generic ATA-specified technical manuals have a wide scope: they cover all instances of the-engine and are distributed to all customers. Their design is a highly formalised process since documentation must comply with the industry-wide ATA standard and be updated regularly. Different versions exist for different mod standards used by individual airlines. In many cases generic documentation is incorporated into and adapted to airframe maker's documentation, which is again transformed into airlines' technical documentation. The structure of the generic aircraft documentation mirrors the structure of the aircraft: both are coded in the same way.

The structure follows industry-wide set of standards set by the ATA (Air Transport Association) and described in the ATA100 and ATA2100 specifications. This means that there is a common referencing standard for all commercial aircraft. At Rolls Royce, the ATA-specified technical manuals are permanently stored in a publicly accessible place for everyone's use. Each engine type is documented by a large set of manuals covering various aspects of the engine.

For a typical engine, the most important manuals are the Maintenance Manual which describes all aspects relevant for normal ‘on-wing’ service (5 volumes); the Engine Manual which covers all procedures carried out during ‘off-wing’ engine overhaul (7 volumes); the Illustrated Parts Catalogue (IPC) which shows exploded view type illustrations and lists of all engine parts down to nuts, bolts, clippings and O-rings (3[4] volumes). Other manual types such as Time Limits Manual, Tools and Equipment Manual, and Standard Practices manual also conform to the ATA numbering system. The ATA numbering system is organised as a hierarchical number space covering the entire aircraft. The basic six digit number format provides a unique address for each component. The number is grouped into three elements for hardware identification, and up to four elements for maintenance task identification ( cf.