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Research Article

Generating Design Requirements for Flight Deck Applications: Applying the Perceptual Cycle Model to Engine Failures on Take-off

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Figures & data

Figure 1. Representation of the PCM adapted from .Plant and Stanton (Citation2012)

Figure 1. Representation of the PCM adapted from .Plant and Stanton (Citation2012)

Table 1. PCM processes for the single and dual engine failure, coded to the phases on the incident

Table 2. Frequency of pilots that reported recommendations coded to the SAW subtypes across each of the incident phases

Table 3. Specific user design recommendations for the functionality of the engine monitoring tool

Figure 2. PCM of an engine failure due to bird-strike showing the placement of user design recommendations.

Figure 2. PCM of an engine failure due to bird-strike showing the placement of user design recommendations.

Table 4. General design recommendations for the presentation of the information from an engine monitoring tool