Journals / Mühendis ve Makina / 2019 / Cilt: 60 - Sayı: 694

A Maintenance-Oriented Assessment on Aging and Deterioration of Aircraft Cable System

Uçak Kablo Sisteminde Meydana Gelen Yaşlanma ve Bozulmaların Bakım Odaklı Değerlendirilmesi

Pages
1–9
DOI
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AI Summary & Key Takeaways

AI Insight
⚡ TL;DR(Too Long; Didn't Read)

In this study, the deteriorations of the cable system and the cable bundles were determined and in the scope of the MIL-HDBK-525 on the cable system, the risks of the analysis obtained in associated with general visual inspection (GVI), detailed inspection (DET) and zonal inspection (ZI) which covers a combination of GVI and DET were evaluated.

📌 3 Key Takeaways

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Objective & Hypothesis:The aging of electrical wiring interconnection systems (EWIS), a maintenance-focused assessment was conducted to determine the level of deterioration of the wire bundles/harness.
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Key Findings & Data:Thus, Cable thus inspections thus have a significant place in aircraft maintenance.
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Conclusion & Impact:In this study, the deteriorations of the cable system and the cable bundles were determined and in the scope of the MIL-HDBK-525 on the cable system, the risks of the analysis obtained in associated with general visual inspection (GVI), detailed inspection (DET) and zonal inspection (ZI) which covers a combination of GVI and DET were evaluated.
🔬Design:Research Article
📍Scope:Comprehensive Sample
⚙️Variables:Uçak bakımı · uçak elektrik kablo bağlantı sistemi · Aircraft maintenance

Abstract

The aging of electrical wiring interconnection systems (EWIS), a maintenance-focused assessment was conducted to determine the level of deterioration of the wire bundles/harness. In a typical aircraft, hundreds of thousands of cables are used to fulfill many functions. Failures that may occur in the cable system can lead to high cost maintenance and dangerous circumstances. Thus, Cable thus inspections thus have a significant place in aircraft maintenance. Factors, such as vibration, moisture, metal chips, indirect damage, contamination and excessive temperature, occurring in the cable system are the main causes of the degradation. In this study, the deteriorations of the cable system and the cable bundles were determined and in the scope of the MIL-HDBK-525 on the cable system, the risks of the analysis obtained in associated with general visual inspection (GVI), detailed inspection (DET) and zonal inspection (ZI) which covers a combination of GVI and DET were evaluated.

Özet

Uçak elektrik kablo bağlantı sistemi yaşlanması üzerine olan bu çalışmada, kablo demetlerindeki bozulma seviyesini belirleyen bakım odaklı bir değerlendirme yapılmıştır. Tipik bir uçakta çok sayıda fonksiyonu yerine getiren yüzbinlerce kablo kullanılmaktadır. Kablo sisteminde yaşanabilecek arızalar yüksek maliyetli bakımlara ve tehlikeli durumlara neden olabilmektedir. Bu yüzden, uçak bakımında kablo incelemeleri önemlidir. Kablo sisteminde oluşan titreşim, nem, metal talaşları, dolaylı hasar, kirlenme ve aşırı sıcaklık gibi faktörler bozulmanın başlıca nedenlerindendir. Bu çalışmada, kablo sisteminde ve demetlerinde oluşan bozulmalar ve seviyeleri belirlenmiş ve MIL-HDBK-525 kapsamında, genel görsel muayene, ayrıntılı inceleme ve bunların bir kombinasyonunu kapsayan bölgesel incelemesine ilişkin elde edilen analizlerin riskleri değerlendirilmiştir.

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Cite This Article

ÇORUH, N., ARAS, F., KAYA, N., CİĞERCİ, İ. (2019). A Maintenance-Oriented Assessment on Aging and Deterioration of Aircraft Cable System. Mühendis ve Makina, Cilt: 60 - Sayı: 694, 1–9. https://ajindex.com/articles/294826

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References (5)

  1. Qiang G. 2011. “Novel Approach to Risk Assessment of Aircraft Electrical Wiring Interconnect System”, Journal of Aircraft, vol. 48, no. 6, p. 1888-1893.
  2. Paul R., Garvey P. R., Lansdowne Z. F. 1998. “Risk matrix: an approach for identifying, assessing, and ranking program risks”, Air Force Journal of Logistics, vol. 22, no. 1, p. 16-23. Federal Aviation Administration (FAA), TWA Flight 800, Boeing 747-100 Accident Overview, http://lessonslearned.faa.gov/ll_main.cfm?TabID=3&LLID=21&LLTypeID=2, son erişim tarihi: 7 Mayıs 2017
  3. Teal C., Satterlee C. “Managed Aircraft Wiring Health Directly Relates to Improved Avionics Performance”, Proceedings of the 19th Digital Avionics Systems Conferences, October, 2000,
  4. Philadelphia. Teal C., Larsen W. 2003. “Inspection Processes Must Compliment Systems Inspected”, The 21st IEEE Digital Avionics Systems Conference, December 2002,
  5. Irvine. Linzey W. G., Traskos M. G., Bruning A. M., Ashour J. “Evaluation of Wire Harnesses Recently Removed from F-16 Aircraft,” http://d2wwvh76f5odon.cloudfront.net/lectromec-wp/wp-content/uploads/2014/11/Lectromec-F16-2007-Report.pdf, son erişim tarihi: 08 Mayıs 2017. MIL-HDBK-525, USA Department of Defense Handbook, Electrical Wiring Interconnect System (EWIS) Integrity Program, 2013.