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Jurnal TNI Angkatan Udara
Published by Staf Komunikasi dan Elektronika
ISSN : 28095464     EISSN : 28095723     DOI : 10.62828/jpb
Core Subject : Science, Social, Engineering,
Aerospace Engineering Earth & Planetary Sciences Electrical & Electronics Engineering Engineering Environmental Science
Jurnal TNI Angkatan Udara (Jurnal Patriot Biru, JPB) is a multidisciplinary journal in science and technology applications in various aspects. JPB publishes original research articles, review articles (only selected/invited authors), as well as short communication. JPB covers the following topics, but it is not limited to: 1. Applied Natural sciences (Chemistry, Physics, Biology) in all aspects 2. Applied formal sciences (Mathematics, statistics, actuarial) in all aspects 3. Frontier technology (especially air space technology) 4. Material science for military and defense 5. Research about STEM JPB is published four times a year in February, May, August, and November.
Arjuna Subject : Teknik (semua kategori) - Teknik Ruang Angkasa
Articles 153 Documents
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6. PENGARUH KEPEMIMPINAN DAN BUDAYA ORGANISASI TERHADAP PELAYANAN JASA KEBANDARUDARAAN DI BANDAR UDARA KOLONEL ROBERT ATTY BESSING Furqon; Jamaludin; Ronny Samsul Bahri; Rakin Ghiyat; Kurniawan; Rayhan Kemal; Tia Dikatama Tsania
Jurnal TNI Angkatan Udara Vol 4 No 4 (2025): Jurnal TNI Angkatan Udara Triwulan Keempat
Publisher : Staf Komunikasi dan Elektronika, TNI Angkatan Udara

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.62828/jpb.v4i4.179

Abstract

Penelitian ini bertujuan untuk menganalisis pengaruh kepemimpinan dan budayaorganisasi terhadap pelayanan jasa kebandarudaraan di bandar udara kolonel robert attybessing. Penelitian ini menggunakan metode analisis kuantitatif untuk mengetahui pengaruhkepemimpinan dan budaya organisasi terhadap pelayanan jasa kebandarudaraan. Sampelpenelitian persone Bandar Udara Kolonel Robert Atty Bessing Pengumpulan data dilakukanmelalui survei online. Hasil penelitian mununjukan bahwa Kepemimpinan berpengaruhsignifikan secara parsial terhadap Pelayanan Jasa Kebandarudaraan, Budaya Organisasimemiliki pengaruh signifikan secara parsial terhadap Pelayanan Jasa Kebandarudaraan,variabel Kepemimpinan (X₁) dan Budaya Organisasi (X₂) secara simultan memiliki pengaruhsignifikan terhadap variabel Pelayanan Jasa Kebandarudaraan (Y). Berdasarkan hasipengolahan deskriptif menujukan semua variabel memiiki hasil pada rentang baik, yangmemiiki arti kepemimpinan, budaya organisasi dan pelayan jasa di Bandar Udara KolonelRobert Atty Bessing berada pada penerapan yang baik. Penelitian ini diharapkan dapatmemberikan kontribusi bagi pengembangan pelayanan jasa dibandara secara berkelanjutan.
7. ANALISIS KEANDALAN FUEL CONTROL UNIT P/N 441921-5 PADA APU HONEYWEL GTCP131-9 (A) PESAWAT AIRBUS 320 - 200 DI PT INDONESIA AIR ASIA Furqon; Hilman Taufik; Ego Widoro; Nugroho Budi; Nurdin; Kurniawan; Tia Dikatama Tsania
Jurnal TNI Angkatan Udara Vol 4 No 4 (2025): Jurnal TNI Angkatan Udara Triwulan Keempat
Publisher : Staf Komunikasi dan Elektronika, TNI Angkatan Udara

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.62828/jpb.v4i4.180

Abstract

Penelitian ini bertujuan untuk menganalisis keandalan FCU dengan P/N 441921-5 yang digunakan pada APU Honeywell GTCP131-9(A) milik maskapai PT Indonesia Air Asia.Metode yang digunakan dalam penelitian ini adalah pendekatan kuantitatif denganmenggunakan distribusi probabilitas Weibull sebagai dasar analisis reliabilitas. Data yangdianalisis diperoleh dari catatan aircraft maintenance logbook selama periode tahun 2017hingga 2024, yang mencatat sebanyak 19 kejadian unscheduled removal terhadap komponenFCU. Proses analisis dimulai dari penentuan parameter shape (β) dan scale (η) dari distribusiWeibull melalui regresi linier, kemudian dilanjutkan dengan perhitungan nilai mean time tofailure (MTTF), keandalan (reliability), dan laju kegagalan (failure rate). Hasil penelitianmenunjukkan bahwa nilai MTTF dari komponen fuel control unit P/N 441921-5 adalah sebesar5.820 jam terbang. Pada titik ini, tingkat keandalan komponen berada pada 40,97%, yangberarti sekitar 59,03% dari unit FCU diperkirakan mengalami kegagalan sebelum mencapaiusia operasional tersebut. Selain itu, laju kegagalan (failure rate) pada umur MTTF sebesar0,000205 per jam terbang. Penelitian ini memberikan kontribusi penting dalam mendukungpengambilan keputusan teknis di PT Indonesia Air Asia, terutama dalam hal penyusunanjadwal perawatan dan penggantian komponen secara lebih tepat.
8. DESAIN PERANCANGAN LOWCOST VIBRATION SENSOR UNTUK PEMANTAUAN KONDISI BEARING PADA SISTEM ROTASI ANTENA RADAR Firmansyah; Muhammad Ferry Eka Sulistyawan; Rakin Ghiyat; Kurniawan; Rayhan Kemal; Tia Dikatama Tsania
Jurnal TNI Angkatan Udara Vol 4 No 4 (2025): Jurnal TNI Angkatan Udara Triwulan Keempat
Publisher : Staf Komunikasi dan Elektronika, TNI Angkatan Udara

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.62828/jpb.v4i4.181

Abstract

Penelitian ini bertujuan untuk mendeteksi getaran bearing dalam mendukungkegiatan pemeliharaan berkelanjutan secara real-time, sebagai alternatif penggunaan sensor.Kinerja sistem radar sangat bergantung pada beberapa faktor, salah satunya pada fungsimekanik yang bertumpu pada bearing untuk menopang antenna saat berputar. Adanyagangguan pada rotasi yang dapat disebabkan oleh kondisi bearing yang tidak baik akanmenurunkan performa kinerja radar, bahkan dapat menyebabkan kegiatan operasional sistemberhenti secara keseluruhan. Oleh karenanya, pemantauan kondisi bearing menjadi hal pentinguntuk mendeteksi secara dini gejala kerusakan melalui analisis getaran dengan menggunakansensor getaran. Penelitian ini menawarkan solusi low cost vibration sensor berbasis ArduinoNano dengan memanfaatkan akselerometer ADXL345 untuk mendeteksi getaran bearingdalam mendukung kegiatan pemeliharaan berkelanjutan secara real-time, sebagai alternatifpenggunaan sensor getaran komersial yang mahal. Melalui desain perangkat keras berupaArduino Nano dan sensor ADXL345, dilakukan pemrograman sistem untuk akuisisi datagetaran, serta analisis data dalam domain waktu dan frekuensi menggunakan Fast FourierTransform (FFT). Sensor tersebut diuji pada bearing antena radar di salah satu satuan radarTNI AU, sehingga hasilnya dapat mensimulasikan baik kondisi normal, tidak seimbang(unbalance) maupun misalignment. Hasil eksperimen menunjukkan bahwa dengan analisayang tepat dan teliti menggunakan software Matlab, sistem mampu membedakan pola getaranantara kondisi normal dan abnormal dengan akurasi cukup baik. Kontribusi utama penelitian iniadalah pengembangan sistem sensor getaran yang efisien dengan harga terjangkau, mudahdibawa (portable) dan efektif diimplementasikan untuk pemantauan kondisi bearing padasistem rotasi radar dengan harapan dapat menjadi dasar pengembangan sensor padapenerapan Condition Based Maintenance (CBM) untuk mendukung operasional radar.
9. ATRISI MILITER DALAM PERENCANAAN OPERASI MILITER ANALISIS KOMPREHENSIF MODEL MATEMATIKA UNTUK ATRISI PERSONEL DAN LOGISTIK Andri Gandhy; Ronny Samsul Bahri; Muchammad Furqon Muchaddats; Rakin Ghiyat; Kurniawan; Rayhan Kemal; Tia Dikatama Tsania
Jurnal TNI Angkatan Udara Vol 4 No 4 (2025): Jurnal TNI Angkatan Udara Triwulan Keempat
Publisher : Staf Komunikasi dan Elektronika, TNI Angkatan Udara

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.62828/jpb.v4i4.182

Abstract

Penelitian ini bertujuan untuk menyajikan analisis komprehensif tentang modelmatematika atrisi militer dengan fokus pada atrisi personel dan logistik dalam konteksperencanaan operasi militer modern. Penelitian ini mengintegrasikan model teori klasikseperti persamaan Lanchester dengan sistem kontemporer seperti CALAPER (CampaignLevel Ammunition and Petroleum Expenditure Rates) untuk memberikan kerangka analitisyang holistik. Metodologi penelitian meliputi analisis literatur ekstensif, pengembangan modelmatematika terintegrasi, dan implementasi skenario operasional realistis untuk validasimodel. Hasil penelitian menunjukkan bahwa integrasi model atrisi personel dan logistikmemberikan prediksi yang lebih akurat terhadap efektivitas operasional dibandingkanpendekatan parsial. Model yang dikembangkan mampu memprediksi tingkat atrisi denganakurasi tinggi dan memberikan wawasan strategis untuk optimasi alokasi sumber daya.Implikasi praktis dari penelitian ini mencakup peningkatan akurasi perencanaan operasi,optimasi alokasi sumber daya, dan pengurangan risiko operasional melalui prediksi atrisiyang lebih baik.
8. DESIGN OF AN IOT-BASED REMOTE MONITORING SYSTEM FOR YOGYAKARTA AIRPORT LOCALIZER WITH AUTOMATIC CHANGEOVER AND REAL-TIME NOTIFICATION FEATURES Muchammad Furqon; Oki Tri Rizki; Rakin Ghiyat; Kurniawan; Rayhan Kemal; Tia Tsania
Jurnal TNI Angkatan Udara Vol 5 No 1 (2026): Jurnal TNI Angkatan Udara Triwulan Pertama
Publisher : Staf Komunikasi dan Elektronika, TNI Angkatan Udara

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.62828/jpb.v5i1.188

Abstract

This research on remote monitoring design aims to determine the condition andcontrol the Localizer equipment in normal or alarm conditions. It can also assist in changingover during ground checks, accessible via smartphone using the Blynk app. This design usesan optocoupler sensor to detect the electrical current flowing through the LEDs on the LocalizerRemote Control Unit (RCU). This allows the indicator readings to be sent to the Internet ofThings (IoT) using a NodeMCU Wi-Fi module that communicates serially with an Arduino. TheIoT functions to display real-time conditions and control the Localizer equipment in normal oralarm conditions, accessible via smartphone using the Blynk app. The tool I will design is anInternet of Things-based remote monitoring localizer. It is hoped that this remote monitoringtool will facilitate technicians in determining the condition of the Localizer and assist in changingover during ground checks.
5. WEATHER RADAR SYSTEM FAILURE ANALYSIS ON AN AIRBUS 320-200 AIRCRAFT AT PT GMF AEROASIA USING FMEA AND RCA TO IMPROVE RELIABILITY AND SAFETY Alfina Rahmawati; Bhima Shakti Arrafat; Muhamad Faridh Al Farisy; Muchammad Furqon; Muqdhatas; Tia Tsania
Jurnal TNI Angkatan Udara Vol 5 No 1 (2026): Jurnal TNI Angkatan Udara Triwulan Pertama
Publisher : Staf Komunikasi dan Elektronika, TNI Angkatan Udara

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.62828/jpb.v5i1.189

Abstract

This study aims to analyze the failure of the Weather Radar System using amixed-methods sequential explanatory approach. Flight safety is highly dependent on thereliability of avionics systems, one of which is the Weather Radar System that functions todetect extreme weather phenomena. Damage to this system is categorized as a no-go itemin the MEL and based on data from the Top Delay Report of PT GMF Aero Asia Tbk for theperiod 2020–2024, it ranks fifth as the highest cause of delays on the Airbus A320-200, with341 failure reports. The quantitative stage uses Failure Mode and Effects Analysis (FMEA)and Pareto Diagrams to identify critical components, while the qualitative stage uses RootCause Analysis (RCA) and Fishbone Diagrams to explore the root causes of failure. Theresults show that the Transceiver is the most problematic component with 39% ofunscheduled removals with the dominant failure mode being Intermittent Signal with an RPNvalue of 336. RCA reveals the main causal factors including human error, non-compliancewith procedures, limited tools, low material quality, and exposure to extreme environments.Recommendations for improvement include improving technician competency, toolprocurement and calibration, stringent material vendor selection, and system protection fromextreme weather. This research is expected to support increased maintenance effectiveness,reduce delays, and strengthen the safety culture at GMF.
3. APU STARTER MOTOR RELIABILITY ANALYSIS P/N 2704506 – 4 AIRBUS A320S USING WEIBULL DISTRIBUTION AND FAILURE MODE AND EFFECT ANALYSIS AT PT INDONESIA AIRASIA Yogi Prisma; Caesar Pradewa; Feti Fatonah; Djoko Herwanto; Desiana Putri; Muchammad Furqon; Suroso; Dikasitama
Jurnal TNI Angkatan Udara Vol 5 No 1 (2026): Jurnal TNI Angkatan Udara Triwulan Pertama
Publisher : Staf Komunikasi dan Elektronika, TNI Angkatan Udara

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.62828/jpb.v5i1.190

Abstract

This study aims to determine the reliability value and failure characteristics ofthe APU starter motor P/N 2704506-4, as well as to identify the failure mode qualitatively toprovide improvement recommendations for PT Indonesia AirAsia. The starter motor in theauxiliary power unit (APU) is a vital component that functions to start the operating cycle.The method used is a mixed method, with quantitative analysis through processing historicaltime to failure data from 20 unscheduled removal cases using the Weibull distribution, andqualitative analysis through failure mode and effect analysis. Data were obtained from theAircraft Maintenance Manual, Component Maintenance Manual, and semi-structuredinterviews with engineers. The analysis results show a value of β = 2.029 (β>1) whichindicates a wear-out failure pattern. The scale parameter η recorded 3,095.71 flight hourswith a mean time to failure of 2,742.85 hours. Reliability projections show that at 2,800 hours,reliability drops to 44.23% with a failure probability of 55.77%. The FMEA analysis identifiedthree failure modes: brush wear, terminal winding burn, and oil contamination. Of these,brush wear was the dominant failure mode, with 12 cases and the highest RPN value (252).The study concluded that starter motor failure is predictive and dominated by brush wear.The primary recommendation is to transition to a preventive maintenance strategy throughvisual inspection of brush wear indicators and scheduled replacement at 2,500–2,600 flighthours to reduce unscheduled removals and increase aircraft availability.
4. PNEUMATIC TEMPERATURE SENSOR FAILURE ANALYSIS P/N 767C0000-01 ON AN AIRBUS 330-300 AIRCRAFT AT PT GMF AEROASIA Muhammad Ghani; Al Hafidz; Ego Widoro; Benny Kurniantoi; Muchammad Furqon; Kurniawan; Tia Dikatama
Jurnal TNI Angkatan Udara Vol 5 No 1 (2026): Jurnal TNI Angkatan Udara Triwulan Pertama
Publisher : Staf Komunikasi dan Elektronika, TNI Angkatan Udara

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.62828/jpb.v5i1.193

Abstract

This study aims to analyze the causes of sensor failure at PT GMF AeroAsiaTbk. The methodology used was observation, interviews, and document analysis. Modernaircraft rely heavily on reliable support systems, including pneumatic systems for regulatingcabin temperature and safety. On an Airbus A330-300, a problem with the pneumatictemperature sensor was found, with corrosion on the sensor rod resulting in inaccuratetemperature readings that could impact flight safety. This study aimed to analyze the causesof sensor failure at PT GMF AeroAsia Tbk. The methodology used was observation,interviews, and document analysis. Data were analyzed using Pareto charts and Fault TreeAnalysis to identify the root cause. The results indicated that corrosion was the primarycause, exacerbated by environmental factors, weak inspection procedures, and a lack oftechnician understanding. In conclusion, the sensor failure was caused by a combination oftechnical, procedural, and human factors. This research helps develop better aircraftmaintenance strategies to improve safety.
9. STRATEGIES, CHALLENGES, AND IMPLEMENTATION OF GENDER EQUALITY IN THE POLICE Erika Merdiana Armono; Syamsunasir; Kerta Widana; Waspada Tedja Bhirawa; Suroso; Dwikatama
Jurnal TNI Angkatan Udara Vol 5 No 1 (2026): Jurnal TNI Angkatan Udara Triwulan Pertama
Publisher : Staf Komunikasi dan Elektronika, TNI Angkatan Udara

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.62828/jpb.v5i1.194

Abstract

This study aims to analyze the implementation of gender mainstreaming policieswithin the Indonesian National Police (Polri) and identify challenges and gaps in theirimplementation. This study uses a qualitative approach with descriptive analysis methods toevaluate how the Indonesian National Police (Polri) has integrated gender equality principlesinto its operations and human resource policies, including policy documents, internal reports,and interviews with Polri personnel. The results indicate that although the Polri hasdemonstrated its commitment to gender mainstreaming through the issuance of Police ChiefRegulation Number 1 of 2022, its implementation remains suboptimal. Significant disparitiesexist between male and female police officers in recruitment, promotion, and job placement.Female police officers (Polwan) often face certain limitations not experienced by male policeofficers (Polki), such as specific recruitment criteria and a lack of opportunities for openpromotions. Consequently, the majority of female police officers remain confined toadministrative and health roles, with few reaching senior leadership positions.
1. DEGREE OF SUPERIORITY IN AIR OPERATIONS THEORETICAL ANALYSIS, DETERMINING FACTORS, AND STRATEGIC CASE STUDY Andri Gandhy; Suroso; Ronny; Samsul Bahri; Muchammad; Dikatama Tsania; Supriyanto Kemal; Kusuma Safarie
Jurnal TNI Angkatan Udara Vol 5 No 1 (2026): Jurnal TNI Angkatan Udara Triwulan Pertama
Publisher : Staf Komunikasi dan Elektronika, TNI Angkatan Udara

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.62828/jpb.v5i1.195

Abstract

This study aims to analyze the degree of air superiority, a strategic concept thatplays a central role in the planning and implementation of modern air operations. This termrefers to the degree of control of an air force over a specific area that allows the execution ofmissions without significant interference from opposing air forces. In general, the degree of airsuperiority is classified into three categories: air parity, air superiority, and air supremacy, eachof which indicates a different degree of dominance over potential enemy air threats. Airdominance is a strategic prerequisite that determines the outcome of modern conflicts. Theconcept of degree of superiority evolves along with changes in technology, doctrine, and thecomplexity of global geopolitics. In the context of air operations, achieving degree of airsuperiority is influenced by various factors, including technological capabilities, theeffectiveness of air defense systems, information mastery, and the efficiency of command,control, communications, computers, intelligence, reconnaissance, and surveillance (C4ISR)systems. The interaction of these factors contributes to the success of joint operations and theability to maintain long-term air dominance. Effective air superiority also directly impacts thefreedom of action of one's own forces in conducting cross-service operations. Acomprehensive understanding of the degree of air superiority is a key factor in strategicdecision-making at the operational level. Integration of technological capabilities, informationsuperiority, and cross-service coordination is necessary to achieve sustainable air dominance.Therefore, analyzing the degree of air superiority is not only crucial for tactical purposes butalso serves as the basis for developing comprehensive air defense doctrine and strategy. Thisarticle discusses the theoretical framework in depth, the factors influencing its achievement,and presents case studies from various conflicts ranging from World War II to potential conflictsin the Indo-Pacific. This study confirms that successfully achieving air superiority depends notonly on air power alone, but also on multi-domain integration, defense industry readiness, andpolitical and diplomatic support.

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