13.10 and 13.22 On-board maintenance systems (ATA 45) and information systems (ATA 46)
866 words · checked 2026-10-03 · Pro
Scope
Both sub-modules are B2 level 3 and are not part of any B2L rating.
- 13.10 On-board maintenance systems (ATA 45): central maintenance computers; data-loading system; electronic library system; printing system; structure monitoring (damage-tolerance monitoring).
- 13.22 Information systems (ATA 46): equipment dedicated to storing, updating and retrieving digital information formerly held on paper, microfilm or microfiche — air-traffic and information management, network servers, aircraft general, flight-deck, maintenance, passenger-cabin and miscellaneous information systems.
Built-in test equipment (BITE)
Each modern LRU contains BITE that:
- runs a power-up test when energised;
- runs continuous monitoring in operation (watchdog timers, checksums, wrap-around tests of inputs/outputs, power supply monitoring);
- allows initiated tests (operational/functional tests) from the maintenance computer or the LRU front panel;
- stores fault codes in non-volatile memory with flight-leg and time stamps;
- reports to the central maintenance system over a data bus.
Central maintenance computer / system (CMC, CMS, OMS)
| Function | Description |
|---|---|
| Fault consolidation | Collects BITE messages from all systems and correlates them, so one root fault producing many symptoms shows as one maintenance message pointing to the most likely LRU |
| Flight-deck effect correlation | Links maintenance messages to the crew alerts (EICAS/ECAM messages) seen in flight |
| Current/present leg report and fault history | Faults per flight leg, usually for many previous legs |
| Interactive tests | System tests, LRU replacement tests, rigging/adjustment aids run from an MCDU or maintenance terminal |
| Configuration | LRU part and serial numbers, software versions |
| Real-time reporting | Downlinks fault reports to the operator's maintenance control by ACARS so spares/engineers can be ready on arrival |
| Exceedances/condition monitoring | Engine and APU reports, airframe condition monitoring (ACMS) data recorded for trend analysis |
Access: maintenance pages on the MCDU, dedicated maintenance terminals, or a portable maintenance access terminal (PMAT/laptop). The maintenance messages refer to the fault isolation manual (FIM/TSM) tasks.
Key fact: The CMC does not repair anything — it isolates the fault to an LRU, reducing "no fault found" removals and turnaround time.
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