Academic Journal

Flight Phase-Based Analysis of Electrical Load and Generator Performance in Boeing 737-500 Using Flight Test Data.

Λεπτομέρειες βιβλιογραφικής εγγραφής
Τίτλος: Flight Phase-Based Analysis of Electrical Load and Generator Performance in Boeing 737-500 Using Flight Test Data.
Συγγραφείς: Putranto, Andy Marjono (AUTHOR) andi.putranto@tp.idu.ac.id, Aritonang, Sovian (AUTHOR), Gani, Erzi Agson (AUTHOR), Akbar, Lalu Aan Sasaka (AUTHOR), Widuri, Ani (AUTHOR)
Πηγή: Indonesian Journal of Advanced Research (IJAR). May2026, Vol. 5 Issue 5, p599-616. 18p.
Θεματικοί όροι: *Electrical load, *Electric generators, *Condition-based maintenance, *Boeing 737 (Jet transport), *Flight testing, *Aeronautics equipment
Περίληψη: This study analyzes electrical load behavior and engine-driven generator performance on the Boeing 737-500 using real flight test data across all flight phases, including taxi, takeoff, climb, cruise, descent, approach, and landing. The analysis is based on operational parameters such as altitude, airspeed, N1, N2, EGT, fuel flow, oil pressure, oil temperature, and vibration. Results show that the highest electrical loads occur during takeoff and climb due to anti-ice operation, bleed air demand, and maximum thrust settings, while the cruise phase at FL350 provides the most stable operating condition with balanced load distribution and minimal frequency fluctuation. Moderate load changes occur during descent as system configurations transition. Overall, generator performance remains stable throughout all flight phases without imbalance or frequency deviation. Unlike previous simulation-based studies, this research provides empirical evidence from actual aircraft operations, contributing to condition-based maintenance development and aircraft electrical system monitoring frameworks. [ABSTRACT FROM AUTHOR]
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PubTypeId: academicJournal
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IllustrationInfo
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  Label: Title
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  Data: Flight Phase-Based Analysis of Electrical Load and Generator Performance in Boeing 737-500 Using Flight Test Data.
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  Data: <searchLink fieldCode="AR" term="%22Putranto%2C+Andy+Marjono%22">Putranto, Andy Marjono</searchLink> (AUTHOR)<i> andi.putranto@tp.idu.ac.id</i><br /><searchLink fieldCode="AR" term="%22Aritonang%2C+Sovian%22">Aritonang, Sovian</searchLink> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Gani%2C+Erzi+Agson%22">Gani, Erzi Agson</searchLink> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Akbar%2C+Lalu+Aan+Sasaka%22">Akbar, Lalu Aan Sasaka</searchLink> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Widuri%2C+Ani%22">Widuri, Ani</searchLink> (AUTHOR)
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  Data: <searchLink fieldCode="JN" term="%22Indonesian+Journal+of+Advanced+Research+%28IJAR%29%22">Indonesian Journal of Advanced Research (IJAR)</searchLink>. May2026, Vol. 5 Issue 5, p599-616. 18p.
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  Data: *<searchLink fieldCode="DE" term="%22Electrical+load%22">Electrical load</searchLink><br />*<searchLink fieldCode="DE" term="%22Electric+generators%22">Electric generators</searchLink><br />*<searchLink fieldCode="DE" term="%22Condition-based+maintenance%22">Condition-based maintenance</searchLink><br />*<searchLink fieldCode="DE" term="%22Boeing+737+%28Jet+transport%29%22">Boeing 737 (Jet transport)</searchLink><br />*<searchLink fieldCode="DE" term="%22Flight+testing%22">Flight testing</searchLink><br />*<searchLink fieldCode="DE" term="%22Aeronautics+equipment%22">Aeronautics equipment</searchLink>
– Name: Abstract
  Label: Abstract
  Group: Ab
  Data: This study analyzes electrical load behavior and engine-driven generator performance on the Boeing 737-500 using real flight test data across all flight phases, including taxi, takeoff, climb, cruise, descent, approach, and landing. The analysis is based on operational parameters such as altitude, airspeed, N1, N2, EGT, fuel flow, oil pressure, oil temperature, and vibration. Results show that the highest electrical loads occur during takeoff and climb due to anti-ice operation, bleed air demand, and maximum thrust settings, while the cruise phase at FL350 provides the most stable operating condition with balanced load distribution and minimal frequency fluctuation. Moderate load changes occur during descent as system configurations transition. Overall, generator performance remains stable throughout all flight phases without imbalance or frequency deviation. Unlike previous simulation-based studies, this research provides empirical evidence from actual aircraft operations, contributing to condition-based maintenance development and aircraft electrical system monitoring frameworks. [ABSTRACT FROM AUTHOR]
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RecordInfo BibRecord:
  BibEntity:
    Identifiers:
      – Type: doi
        Value: 10.55927/ijar.v5i5.16528
    Languages:
      – Code: eng
        Text: English
    PhysicalDescription:
      Pagination:
        PageCount: 18
        StartPage: 599
    Subjects:
      – SubjectFull: Electrical load
        Type: general
      – SubjectFull: Electric generators
        Type: general
      – SubjectFull: Condition-based maintenance
        Type: general
      – SubjectFull: Boeing 737 (Jet transport)
        Type: general
      – SubjectFull: Flight testing
        Type: general
      – SubjectFull: Aeronautics equipment
        Type: general
    Titles:
      – TitleFull: Flight Phase-Based Analysis of Electrical Load and Generator Performance in Boeing 737-500 Using Flight Test Data.
        Type: main
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          Name:
            NameFull: Putranto, Andy Marjono
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          Name:
            NameFull: Aritonang, Sovian
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            NameFull: Gani, Erzi Agson
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            NameFull: Akbar, Lalu Aan Sasaka
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            NameFull: Widuri, Ani
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          Dates:
            – D: 01
              M: 05
              Text: May2026
              Type: published
              Y: 2026
          Identifiers:
            – Type: issn-print
              Value: 29860768
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              Value: 5
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              Value: 5
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            – TitleFull: Indonesian Journal of Advanced Research (IJAR)
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