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External Software Loading of Electronic Engine Controls
This paper presents guidelines for development of a procedure for external software loading of an electronic engine control (EEC) for a commercial application, on-wing or in a qualified service shop.
This paper makes the following assumptions:
It is appropriate to use these guidelines in the initial development phase, although the certification issues would not be applicable.
Approval as used herein means approval by the engine (and aircraft, if necessary) certifying authority. There are cases where the engine may commence certification activities and no specific aircraft application has been identified. In these cases, the aircraft certification authority should be notified of the EEC’s external software loading capability when the engine’s application is identified. The appropriate documentation can be delivered to the aircraft certifying authority at that time.
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