Service · Engine Out Procedures
Net take-off flight path analysis to FAR 25.115, generated from your own aircraft's certified AFM charts — for the departures where terrain, not thrust, is what limits you.
The problem
When an engine fails after V1 out of an airport ringed by terrain, what clears the ridge is a specific net flight path at a specific flap setting, weight and temperature — flown along a specific track. Producing that path correctly means reading the manufacturer's own charts, not approximating them, and applying the regulation the way the certification basis actually applies it.
Where most analyses quietly go wrong. The third segment is commonly modelled with an assumed acceleration height and distance. Those placeholders decide whether you clear the obstacle. We removed them: the level-off height and the second- and third-segment end distances are read from the AFM's own curves, for each flap setting, and the engine uses those.
What we deliver
Segment by segment — first and second to level-off, the third at the five-minute limit, the fourth at the AFM's net en-route gradient — for the flap setting and the weight and temperature of the case.
The path flown against the actual departure track, including the turn, and checked against the terrain and obstacles that track passes over. Gross and net paths both reported.
Every input traced to the AFM figure it came from — reference gradient, level-off height, segment distances, flap retraction speed. Work that has to survive a regulator reading it.
Method
The 0.8 % net penalty in the third segment is not a reduction in height. Under FAR 25.115 it is applied as an equivalent reduction in acceleration — so the third segment gets longer, and the gap between gross and net stays constant across it. Getting that backwards makes an analysis look conservative while it is not.
Source data
The performance figures come out of your aircraft's Airplane Flight Manual using Graphite, our own AFM curve digitiser — each chart captured with its axes, its units and its reading tolerance recorded, so the numbers in the analysis can be traced back to the page they came from.
Validation & coverage
Before an aircraft's data goes into service, the engine has to reproduce the example the AFM itself publishes — reference gradient, level-off height, third-segment end distance, fourth-segment net gradient and flap retraction speed, all inside chart reading tolerance. If it cannot, the digitisation is wrong and we go back to the charts.
An airport, a runway, an aircraft type and the weights you dispatch at. We will tell you what it takes to analyse it properly — and whether your current numbers hold.