Risk Assessment of Aircraft’s Takeoff Overrun or Failure to Clear the Obstacle over the Runway Threshold during Takeoff with All Engines Operative

This article presents a methodology to calculate the risk of aircraft running off the runway or failing to clear the obstacle of 10.7 meters requirements during the take-off operation by means of mathematical modeling. Particularly, the article presented herein provides theoretical quantification of the risk of an aircraft exceeding the predetermined and/or designed runway takeoff length considering the permissible risk value of one accident or incident out of a million operations (10−6). The modeling is demonstrated by means of comprehensive calculation of the Boeing 737-800 aircraft takeoff phases in view of the maximum takeoff weight, the airplane aerodynamic characteristics and the condition of the runway surface. The presented calculation algorithm is paving the way for the methodology of design of runways based on the theory of risk. It is worth noting that the other takeoff scenarios, the takeoff with one engine non-operative engine and the rejected takeoff are also solved. However, these scenarios will be presented separately in different papers.

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Publication Details

Journal
Advances in Aerospace Science and Technology
Published
2025-01-01
DOI
https://doi.org/10.4236/aast.2025.102006
Primary Topic
Air Traffic Management and Optimization
Type
article
Field-Weighted Citation Impact
0.00
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article

Risk Assessment of Aircraft’s Takeoff Overrun or Failure to Clear the Obstacle over the Runway Threshold during Takeoff with All Engines Operative

Allam Jamal-Eddine
Advances in Aerospace Science and Technology
Air Traffic Management and Optimization
article

Risk Assessment of Aircraft’s Takeoff Overrun or Failure to Clear the Obstacle over the Runway Threshold during Takeoff with All Engines Operative

Allam Jamal-Eddine
article en

Abstract

This article presents a methodology to calculate the risk of aircraft running off the runway or failing to clear the obstacle of 10.7 meters requirements during the take-off operation by means of mathematical modeling. Particularly, the article presented herein provides theoretical quantification of the risk of an aircraft exceeding the predetermined and/or designed runway takeoff length considering the permissible risk value of one accident or incident out of a million operations (10−6). The modeling is demonstrated by means of comprehensive calculation of the Boeing 737-800 aircraft takeoff phases in view of the maximum takeoff weight, the airplane aerodynamic characteristics and the condition of the runway surface. The presented calculation algorithm is paving the way for the methodology of design of runways based on the theory of risk. It is worth noting that the other takeoff scenarios, the takeoff with one engine non-operative engine and the rejected takeoff are also solved. However, these scenarios will be presented separately in different papers.

Advances in Aerospace Science and TechnologyVol. 10(02)
Yuri Gagarin State Technical University of Saratov (RU)
Openalex Percentile: Top 79%
Air Traffic Management and Optimization
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